Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
Pilot’s Operating Handbook (POH) and
FAA Approved Airplane Flight Manual
GLASAIR SUPER II-S FT – N11HC
Date Shipped: 8 Sept 1994
Kit Number: 2329
Date Started: 8 Sept 1994
Date First Flight: June 6, 2012
Date Unlimited Duration Airworthiness Certificate Issued: Jan. 17,
2013
Manufacturer:
Original Kit from Stoddard-Hamilton Aircraft (out of business)
Current Glasair Kit Manufacturer is New Glasair
N11HC Produced and Assembled by: Philip Conway and Friends
Model: Glasair Super II-S FT
Serial Number: 2329
Registration Number: N11HC
Part Number 632-0127-103
FAA approved in the Aerobatic Category based on FAR23.3(c).
See Section 2 for restrictions.
This handbook includes the material required to be furnished to the
pilot by the federal aviation regulations and additional information
provided by the manufacturer, and constitutes the FAA approved
airplane flight manual.
This document (in paper or electronic format) must be carried in
the airplane at all times.
Approved by the Federal Aviation Administration
By: Todd L. Elliefson, DAR, May 6, 2012
12-10-2014
Intro to POH for N11HC
Intro – 1
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
INTENTIONALLY LEFT BLANK
Intro – 2
Intro to POH for N11HC
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
Contents
This Section ............................................................... Introduction Pages
Section 1 .................................................................. General Information
Section 2 ................................................................................. Limitations
Section 3 ............................................................ Emergency Procedures
Section 4 .................................................. Normal Operating Procedures
Section 5 ..............................................................................Performance
Section 6 ......................................................................Weight & Balance
Section 7 ............................................................... Systems Descriptions
Section 8 ...................................... Handling, Servicing and Maintenance
Section 9 ............................................................................. Supplements
Section 10 ................................................... Safety and Operational Tips
Section 11 .............................. Changes, Logs, Updates and Inspections
Section 12 ..................................................................... Flight Test Cards
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Intro to POH for N11HC
Intro – 3
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
NOTE
Hyperlinks or bookmarks for this POH in electronic format:
 All section TOC pages are hyperlinked (bookmarked). This
Intro TOC is hyperlinked when reading the PDF version of
the entire POH.
 In addition to clicking on a TOC line, you may click the
BOOKMARK icon on the left side of Adobe Reader.
The official website is “http://11HC.44RF.com.” This site contains
many publications and information relevant to this airplane and flying in
general.
For additional information contact:
Richard Fechter
FPS@44RF.com
Intro – 4
Intro to POH for N11HC
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
Section 1 - General Information
Table of Contents
1-1. INTRODUCTION ...................................................................... 1-3
1-2. TYPES OF GLASAIRS ............................................................. 1-4
1-3. USE OF THE POH ................................................................... 1-5
1-4. REVISING/UPDATING THE POH ............................................ 1-5
1-5. PRINTING THE POH ............................................................... 1-6
1-6. WARNINGS, CAUTIONS AND NOTES ................................... 1-6
1-7. AIRPLANE THREE VIEW ........................................................ 1-7
1-8. AIRCRAFT DESCRIPTION ...................................................... 1-8
1-9. REFERENCES TO OTHER PUBLICATIONS .......................... 1-8
1-10. SPECIFICATIONS .................................................................... 1-9
1-11. SYMBOLS, ABBREVIATIONS AND TERMINOLOGY .......... 1-10
1-11.1. General Airspeed and AOA ................................................ 1-10
1-11.2. Speed Terminology ............................................................ 1-11
1-11.3. Meteorological Terminology ............................................... 1-12
1-11.4. Power Terminology............................................................. 1-13
1-11.5. Aircraft Performance Terminology ..................................... 1-13
1-11.6. Weight and Balance ........................................................... 1-14
1-11.7. Other Abbreviations ............................................................ 1-15
1-12. °C TO °F & °F to °C CONVERSION TABLE .......................... 1-17
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
INTENTIONALLY LEFT BLANK
1-2
Section 1 – General Information
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
1-1.
INTRODUCTION
The sole purpose of this Pilot’s Operating Handbook (POH) is to
explain the safe and efficient operation of N11HC –. Glasair Super ll-S
FT.
The Glasair Super ll-S FT is a two-place, low-wing, aircraft that
features fixed tricycle landing gear and an airframe made entirely from
female-molded fiberglass composite components.
The Glasair is designed to provide the highest utility possible in a
home built aircraft. The aerodynamically clean airframe is responsible
for the Glasair's high top speed and its exceptional operating
efficiency. The excellent high speed performance is complemented by
good slow flight characteristics and an honest, predictable stall. The
rugged landing gear permits operation from rough, short fields. The
Glasair Super ll-S FT's comfortable side-by-side seating, ample
baggage capacity and good range make it an unparalleled crosscountry traveler. Thanks to the light, responsive controls, sport
aerobatics in the Glasair are pure delight. The integration of all these
capabilities in a single aircraft makes the Glasair Super ll-S FT the
ultimate in performance and versatility.
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
1-2.
TYPES OF GLASAIRS
TD=Tail Dragger, FT=Fixed Tricycle, or RG=Retractable Gear
 Glasair I
o Kits 1 thru 803
o delivered through about 1985
o Compared to current version:
 Approximately 2 ½” narrower in the fuselage (shoulder
width)
 1” shorter in canopy height
 Builders had to make their own canopy frames by
cutting the frame out of the fuselage shells and
reinforcing and finishing off the frame to be a good fit.
 Canopies were cut out as either an internal sliding
canopy or gull wing style.)
 Glasair II
 Kits 1001 thru 1119
 Compared to Glasair 1:
o 2 1/2” wider fuselage but same length
o 1” taller fuselage
o Flange joggles at the firewall, belly panel, wingtips, cowl,
inspection holes, windshield, canopies, etc.
o Canopy frames, gear box structures, stabilizer and
elevator ribs and spars were included as formed
assemblies
 Glasair IIS
o Kits 2001 thru 2184
o “S” is for Stretch
o Compared to Glasair II
 fuselage was lengthened in the aft end
 CG slightly too far aft with light engine and/or prop.
 Many builders ended up modifying their IIS to Super IIS
configuration
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Section 1 – General Information
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
 Glasair Super IIS
o Kits 2201 thru XXXX
o Currently in production
o Compared to the original Glasair IIS:
 longer horizontal stabilizer
 wing in the original location (2 ½” back)
 6” added to nose for leg room
 Has a wider CG range
 Baggage weight carrying increased
 Improved stability and control
1-3.
USE OF THE POH
This N11HC – Glasair Super ll-S FT POH is designed to maintain
documents necessary for the safe and efficient operation of the
aircraft. This manual attempts to follow the guidelines of the General
Aviation Manufacturers Association’s “Specification for Pilot’s
Operating Handbook.”
The POH is divided into major sections which are listed in the “Intro”
section under “Contents” at the front of the manual. Each section also
has its own individual Table of Contents which, in MS Word or Adobe
PDF format, is hyperlinked to that specific paragraph. When viewing
this POH in Adobe Acrobat, the Table of Contents in the intro section is
also hyperlinked to each chapter’s Table of Contents.
Speeds in this manual are in knots. To convert to MPH, multiply the
knots by 1.15.
1-4.
REVISING/UPDATING THE POH
Revise this POH as needed and required by testing, experience and
factory requirements as a MS Word document. To make updates
easier, use the “Styles” provided with Word 2007 and higher. Don’t
forget to update the footer dates and TOC.
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
1-5.
PRINTING THE POH
The font is Arial 16 so it can be printed in half-sheet format to go into
an 8.5” x 5.5” loose-leaf notebook.
Page Layout should be “Fit-to-Page Printing”. It is formatted for
“mirrored” margins with the inside (hole-punch margin) at 1.1” and the
outside at 0.3”.
1-6.
WARNINGS, CAUTIONS AND NOTES
The following definitions apply to WARNINGS, CAUTIONS and
NOTES throughout this manual.
WARNING
Procedures, practices, etc., which may result in Personal
injury or loss of life if not carefully followed
CAUTION
Procedures, practices, etc., which if not strictly observed may
result in damage or destruction of equipment
NOTE
An operating procedure, condition, etc, which is considered
essential to emphasize.
1-6
Section 1 – General Information
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
1-7.
AIRPLANE THREE VIEW
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
1-8.
AIRCRAFT DESCRIPTION




Low Wing with Slotted Flaps
Wing loading – 24.04 lb/ft2
2-Seat (Side-by-Side)
Single Engine (see section 7 for more engine information)
o Lycoming IO-360-B1E
o 180 HP at 2700 RPM
o Air cooled
o Normally aspirated
o Horizontally Opposed
o 4 cylinder
o Fuel Injected
 Propeller (see section 7 for more propeller information)
o Constant Speed (Engine Oil Pressure Activated)
o Two Blade Hartzell
o Direct Drive
o 68 Inch
 Fixed Tricycle Gear
1-9.
REFERENCES TO OTHER PUBLICATIONS
 Most references to other publications are directly hyperlinked
 References within the “Lycoming Operator’s Manual” can be
found by actual page number (x-x at the bottom of each page) or
the PDF page number (x/x on the Adobe tool bar) or by using
Bookmarks .
1-8
Section 1 – General Information
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
1-10.
SPECIFICATIONS
Gross Weight ................................................................................... 2200
Gross Weight for Aerobatic Flight ............................................... 1900 lbs
Empty Weight.............................................................................. 1403 lbs
Useful Load ................................................................................... 797 lbs
Person & Baggage Weight available with full fuel ........................ 497 lbs
Fuel Capacity ................................................................... 50 gal / 300 lbs
Top Speed (sea level).............................................................. 168 KTAS
Cruise Speed - 75% @ 8,000' ................................................. 153 KTAS
Cruise Speed - 65% @ 8,000' ................................................. 147 KTAS
Rate of Climb at light weight ....................................................... 900 fpm
Rate of Climb at gross ................................................................ 700 fpm
Vso - Stall @ Gross .................................................................... 58 KIAS
Vs - Stall @ Gross ...................................................................... 67 KIAS
Vy (best rate) .............................................................................. 85 KIAS
Vx (best angle) ............................................................................ 75 KIAS
Vref (approach speed) (Instrument Cat A) ................................. 90 KIAS
Vfe (flap extension) ................................................................... 122 KIAS
Va (maneuvering ...................................................................... 126 KIAS
Vno (top of green arc) ............................................................... 174 KIAS
Nne (Red line) .......................................................................... 226 KTAS
1900 lb limit load ..................................................................... +6.0 / -4 G
2200 lb limit load ..................................................................... +3.8 / -1 G
Roll Rate ................................................................................. 85 deg/sec
Fuel Consumption at 65% power ..................................................8 GPH
Service Ceiling ..............................................................................17,500’
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
1-11. SYMBOLS, ABBREVIATIONS AND TERMINOLOGY
1-11.1.
General Airspeed and AOA
1G – AOA
(One Green Light
Cruise
L/D Max
2G-1Y – AOA
Max Endurance
(Between Two Green and First Yellow Lights)
Max Glide Range
~85 KIAS
VX
2Y – AOA
(Two Yellow Lights)
~75 KIAS
Optimum
Approach
CAS / KCAS ..... Knots Calibrated Airspeed is the indicated speed of an
airplane corrected for position and instrument error.
Calibrated airspeed is equal to true airspeed in
standard atmosphere at sea level.
GS .................... Ground Speed is the speed of an airplane relative to
the ground.
IAS / KIAS ........ Knots Indicated Airspeed is the speed of an airplane
as shown on the airspeed indicator when corrected for
instrument error. IAS values published in this
handbook assume zero instrument error.
TAS / KTAS ...... Knots True Airspeed is the airspeed of an airplane
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Section 1 – General Information
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
relative to undisturbed air which is the CAS corrected
for altitude, temperature, and compressibility.
1-11.2.
Speed Terminology
MPH ................................... Speed where 1 MPH = traveling 5280 ft in
one hour
Knots .................................. Speed where 1 knot = traveling 6076 feet in
one hour (1 knot = 1.150779448 mph)
Va ....................................... Maneuvering Speed is the maximum speed
at which application of full available
aerodynamic control will not over stress the
airplane.
Vfe ...................................... Maximum Flap Extended Speed is the
highest speed permissible with wing flaps in
a prescribed extended position.
Vg ....................................... Best Glide (L/D Max)
Vne ..................................... Never exceed speed is the speed limit that
may not be exceeded at any time.
(Redline).
Vno ..................................... Maximum Structural Cruising Speed is the
speed that should not be exceeded except
in smooth air and then only with caution.
Vs ....................................... Stalling Speed or the minimum steady flight
speed at which the airplane is controllable.
Vso ..................................... Stalling Speed or the minimum steady flight
speed at which the airplane is controllable
in the landing configuration.
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
Vr ........................................ Rotate is about 1.05 x Vs for flap setting.
Vref ..................................... Reference in Pattern or Instrument
Category, 1.3 x Vs (90 KIAS w/EWT)
Votf ..................................... Over the Fence – 1.2 x Vs
Vx ....................................... Best Angle-of-Climb Speed is the airspeed
at which delivers the greatest gain of
altitude in the shortest possible horizontal
distance.
Vy ....................................... Best Rate-of-climb Speed is the airspeed
which delivers the greatest gain in altitude
in the shortest possible time.
V speeds change with wgt . (√W 1 / Wg) x V. Where: W 1=current wgt,
Wg=Max Gross Wgt, V=Published V-speed
1-11.3.
Meteorological Terminology
ISA ..................................... International Standard Atmosphere is a
nominal atmosphere where air is a dry
perfect gas with a temperature of 15°C
(59°F) at sea level. The pressure at sea
level is 29.92 in. Hg. The temperature
gradient from sea level to 36,089 ft is 1.98°C per 1,000 ft.
OAT .................................... Outside Air Temperature is the free static
air temperature. It is obtained from
meteorological sources or in-flight
instruments adjusted for instrument error
and compressibility effects.
PA ...................................... Pressure Altitude is the altitude read from
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Section 1 – General Information
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
an altimeter when the altimeter’s barometric
scale has been set to 29.92 inches Hg
assuming zero position and instrument
error (instrument error is assumed to be
zero in this POH).
1-11.4.
Power Terminology
BHP .................................... Brake Horsepower is the power developed
by the engine.
RPM ................................... Revolutions Per Minute is engine speed.
MP ...................................... Manifold Pressure is a pressure measured
in the engine’s induction system and is
expressed in inches of mercury (in Hg).
1-11.5.
Aircraft Performance Terminology
Climb Gradient ................... Climb Gradient is the ratio of the change in
height during a climb, to the horizontal
distance covered in the same time interval.
Demonstrated Crosswind .. Demonstrated crosswind velocity is the
velocity of the crosswind component for
which adequate control of the aircraft
during takeoff and landing has been
demonstrated during flight tests. The value
shown is not considered to be limiting.
Usable Fuel ........................ Usable Fuel is the fuel that can be safely
used in flight.
Unusable Fuel .................... Unusable Fuel is the fuel that cannot be
safely used in flight.
GPH ................................... Gallons Per Hour is the amount of fuel (in
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
US gallons) consumed per hour.
G’s ...................................... Acceleration due to gravity.
1-11.6.
Weight and Balance
Datum: ................................ An imaginary vertical plane from which all
horizontal distances are measured for
balance purposes.
Station: ............................... A location along the airplane fuselage
usually given in terms of distance from the
reference datum.
Arm: .................................... The horizontal distance from the reference
datum to the center of gravity (CG) of an
item.
Moment: ............................. The product of the weight of an item
multiplied by its arm.
MAC: .................................. Mean Aerodynamic Chord. The value that.
When multiplied by the span, results in the
wing area.
CG: ..................................... Airplane Center of Gravity. The point at
which an airplane would balance if
suspended. Its distance from the reference
datum is found by dividing the total moment
by the total weight of the airplane.
CG Arm: ............................. The arm obtained by adding the airplane's
individual moments and dividing the sum by
the total weight.
CG Limits: .......................... The extreme center of gravity locations
within which the airplane must be operated
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Section 1 – General Information
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
at a given weight.
Empty Weight:.................... Weight of an airplane including full
operating fluids, unusable fuel, full oil, and
optional equipment.
Max Gross Wgt: ................. Maximum weight approved for flight
operations.
Useful Load: ....................... Difference between maximum gross weight
and empty weight.
Payload: ............................. Weight of occupants and baggage.
Tare: ................................... The weight of chocks, blocks, stands, etc.,
used on the scales when weighing an
airplane
1-11.7.
Other Abbreviations
AOA ................................... (Angle of Attack) The angular difference
between the wing cord and the relative
wind.
CG ...................................... (Center of Gravity) The point where the
weight of the front of the aircraft equals the
weight of the back of the airplane.
CHT .................................... (Cylinder Head Temperature) The
temperature of the cylinders.
EGT .................................... (Exhaust Gas Temperature) The
temperature of the exhaust gases at the
exhaust manifold.
ELT .................................... (Emergency Locator Transmitter) A
transmit only radio that can be set off by a
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
crew member or impact forces. It transmits
information on an emergency frequency.
EOR ................................... (End of Runway) Sometimes referred to as
“Run-up” or “Last Chance.” It is where the
pilot accomplishes the last engine, aircraft,
navigation and instrument checks before
taking off.
FOD .................................... (Foreign Object Damage) Damage to an
aircraft, propeller or engine from a “foreign
object” (example: bird, rocks, dirt, parts of
other aircraft, etc.)
EWT ................................... Extended Wing Tips, or W/EWT is With
Extended Wing Tips.
MFD ................................... (Multi Function Display) The G3X(s) which
is displaying multiple items – usually the
center and maybe the right G3X.
MP ..................................... (Manifold Pressure) The absolute pressure
as measured at the appropriate point in the
induction system and expressed in inches
of mercury.
PFD .................................... (Primary Flight Display) Usually the G3X
on the left displaying flight attitude.
POH ................................... Pilots Operating Handbook
RPM ................................... Revilutions per minute of the propeller and
crankshaft.
SWT .................................. Standard Wing Tips or W/SWT is With
Standard Wing Tips.
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Section 1 – General Information
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
1-12. °C TO °F & °F to °C CONVERSION TABLE
Centigrade to Fahrenheit Conversion Table
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
INTENTIONALLY LEFT BLANK
1-18
Section 1 – General Information
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
Section 2 – Limitations
Table of Contents
2-1. INSTRUMENT MARKINGS ......................................................... 3
2-2. AIRSPEED LIMITATIONS ........................................................... 3
2-2.1. ...... Va Changes with Weight ....................................................... 4
2-2.2. ...... Airspeed Indicator Markings .................................................. 4
2-3. POWERPLANT LIMITATIONS .................................................... 5
2-3.1. ...... Installed Engine ..................................................................... 5
2-3.2. ...... Stabilized operation is prohibited .......................................... 5
2-3.3. ...... Tachometer (RPM) ................................................................ 6
2-3.4. ...... Manifold Pressure ................................................................. 7
2-3.5. ...... Cylinder Head Temperature .................................................. 8
2-3.6. ...... Oil Temperature..................................................................... 9
2-3.7. ...... Oil Pressure ......................................................................... 10
2-3.8. ...... Mixture Settings ................................................................... 10
2-4. FUEL .......................................................................................... 11
2-4.1. ...... Fuel Grade ........................................................................... 11
2-4.2. ...... Fuel Flow ............................................................................. 11
2-4.3. ...... Fuel Pressures .................................................................... 11
2-4.4. ...... Fuel Capacity....................................................................... 12
2-4.5. ...... Fuel Tank Markings ............................................................. 12
2-4.5.1. Header (Aux)Tank
12
2-4.5.2. Wing (Main) Tank
12
2-4.6. ...... Fuel Controls ....................................................................... 12
2-5. ELECTRICAL ............................................................................. 13
2-5.1. ...... Load ..................................................................................... 13
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips IO-360, C/S Prop
2-5.1.1. Main Alternator
13
2-5.1.2. Standby Alternator
13
2-5.2. ...... Voltage ................................................................................. 14
2-6. WEIGHT LIMITS ........................................................................ 14
2-7. CENTER OF GRAVITY LIMITS................................................. 15
2-8. FLIGHT LOAD FACTORS ......................................................... 15
2-9. AEROBATIC MANEUVERING LIMITATIONS .......................... 15
2-10. INTENTIONAL SPINS PROHIBITED ........................................ 17
2-11. FLIGHT IN ICING CONDITIONS ............................................... 17
2-12. FLIGHT IN THE VICINITY OF THUNDERSTORMS ................. 17
2-13. PRECAUTIONS CONCERNING SLIPS .................................... 18
2-14. MINIMUM EQUIPMENT LIST .................................................... 19
2-15. PLACARDS and MARKINGS .................................................... 22
2-15.1. ... Experimental ........................................................................ 22
2-15.2. ... Data Plate ............................................................................ 22
2-15.3. ... Passenger Warning ............................................................. 23
2-15.4. ... AOA Exterior Placards ......................................................... 23
2-15.5. ... Canopies .............................................................................. 23
2-15.6. ... Arm-Rest Labels: ................................................................. 23
2-15.7. ... Other Instrument Panel Labels: ........................................... 23
2-15.8. ... Control Stick Grip Placards ................................................. 24
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
2-1.
INSTRUMENT MARKINGS
Screen shots of the G3X instrument markings are at:
http://aswebs.com/44rf/11hc/panel/inst_markings/inst_markings.htm
2-2.
AIRSPEED LIMITATIONS
Speed
Vne
Never Exceed
Vno
Maximum Structural
Cruising
Va
Maneuvering Speed
Vfe
Limit for Slotted Flaps
CIAS
226
(TAS)
174
126
122
Remarks
Do not exceed this speed in any
operation (Red Line)
Do not exceed this speed except in
smooth air and then only with
caution. (Yellow Arc)
Do not make full or abrupt control
movements above this speed
Do not extend flaps or operate with
flaps extended above this speed
NOTE
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips IO-360, C/S Prop
Definitions of these airspeeds are given in FAR Part 1, and
Section 1 of this POH. All airspeeds are calibrated airspeeds
(CAS) except Vne is TAS.
2-2.1.
Va Changes with Weight
Va is 126 KIAS only at the GW of 2200 lbs. It reduces by about 3
knots for every 100 lbs below 2200 lbs. {Va = 126*sqrt(A/C Wgt / GW)}
A/C Wgt
Va
w/EWT
A/C
Wgt
Va
w/EWT
2200
126
1800
114
2100
123
1700
111
2000
120
1600
107
1900
117
1500
104
2-2.2.
Airspeed Indicator Markings
Color Coded
Speed
White
Strip/Arc
Green
Strip/Arc
2-4
KIAS Range
Significance
Stby Gauge
55 – 122
Full flap operating range.
Lower Limit = Stall speed with flaps
down at maximum weight.
Upper Limit = Maximum Speed with
Flaps Extended.
Normal Operating Range
Lower Limit = Stall speed with flaps up
at maximum weight.
Upper Limit = Maximum Structural
Cruise Speed
G3X Gauge
58 - 122
67 - 174
Section 2 – Limitations
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
Yellow
Strip/Arc
174-226
Red Line
226 TAS
2-3.
Caution Range.
Approved for Smooth Air Only.
Lower Limit = Maximum Structural
Cruise Speed.
Upper Limit = Never Exceed Speed.
Maximum Speed for all Operations
POWERPLANT LIMITATIONS
NOTE
References within the “Lycoming Operator’s Manual” can be
found by actual page number (x-x at the bottom of each
page) or the PDF
page number (x/x on the Adobe tool
bar) or by using
Bookmarks .
Another source of limitations is from the Original POH from
Glasair (pg 95-200).
2-3.1.
Installed Engine
N11HC has a 180 hp Lycoming IO-360 B1E Engine. See Section 7 for
details on the engine.
2-3.2.
Stabilized operation is prohibited
IAW FAA Document: “Type Certificate Data Sheet No. P-920”, page 8
of 13 (8/13).
> 25” MP and ................................................................ 2300-2350 RPM
< 15” MP and ................................................ > 2600 RPM (white range)
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Section 2 – Limitations
2-5
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips IO-360, C/S Prop
2-3.3.
Tachometer (RPM)
Maximum RPM (Red Line)....................................................... 2700 rpm
Gauge Range .................................................................... 0 to 2800 rpm
2700-2800 RPM ................................................ Red Range + Alert
2600-2700 RPM ............................. White Range – keep MP > 15“
2300-2350 RPM .............................. Cyan Range – keep MP < 25”
600-2700 RPM......................... Green Range with MP Restrictions
400-600 RPM – Yellow Range – Low RPM
Note
Stabilized operation is prohibited when MP is greater than
25” and RPM is between 2300 and 2350 RPM (cyan range).
Stabilized operation is also prohibited when MP is less than
15” and RPM is greater than 2600 RPM (white arc).
Therefore do not continuously run both RPM & MP indicators
in the cyan arcs or both indicators in the white arcs at the
same time.
2-6
Section 2 – Limitations
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
2-3.4.
Manifold Pressure
Operating Range ........................................................ >10.0 to 29.6” Hg
Gauge Range............................................................... 10.0” – 30.0” HG
25” – 29.6” ......Cyan Range – Keep RPM out of 2300-2350 Range
15” – 25” ..................................................................... Green Range
10” – 15” ............................ White Range – Keep RPM Below 2600
Rule of thumb for MP at altitudes up to 15,000 ft or so is 29" minus the
actual altitude in thousands. i.e. 22" at 7,000', 26” at 3000’.
Between 1800 & 2300 RPM, MP can be 4.5 above square.
Between 2400 & 2700 RPM, MP can be 2 above square.
Reference POH Section 5 Performance chart
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Section 2 – Limitations
2-7
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips IO-360, C/S Prop
2-3.5.
Cylinder Head Temperature
IAW Lycoming Operators Manual page 3-6 (23/51)
(General
Rules): For maximum service life, cylinder head temperatures should
be maintained:
 Below 435°F during High performance cruise operation
 Below 400°F for economy cruise power.
IAW Lycoming Operators Manual page 3-13 (30/51)
(Sec 3-8.
Fuel, Oil Burn & CHTs): For maximum service life of the engine
maintain cylinder head temperatures between 150°F and 400°F during
continuous operation.
Minimum in-flight CHT should be 149°F
Gauge Range ................................................................. 150°F to 500°F
495-500°F ............................ Red Range + Alert – Maximum Temp
435°F to 495°F .......................................................... Yellow + Alert
400°F to 435°F ............................................................ Cyan Range
High Performance Cruise
150°F to 400°F .......................................Green – Best CHT Range
2-8
Section 2 – Limitations
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
2-3.6.
Oil Temperature
IAW Lycoming Operators Manual page 3-11 (28/51)
(Sec 3-8. Oil
Grades for Temps): Engine oil temperature should not be below 140°F
during continuous operation.
IAW the Original POH from Glasair (pg 95-200) the green arc is 160°F220°F.
Ambient Air Temps vs. Desired Oil Temps
Ambient Air Temps
Desired Oil Temps
30°F to 90°F /
180°F
0°F to 70°F
170°F
< 10°F
160°F
Engine oil temperature should be >140°F during continuous operation.
Gauge Range.................................................................... 130°F - 250°F
>245°F .............Red Range + Alert - Maximum All Ambient Temps
220°F to 245°F .............................................. Yellow Range + Alert
160°F to 220°F ............................... Green Range – Normal Range
180°F ........................... White Line – Recommended Temperature
140°F to 160°F ...................... Yellow Range–Min. Continuous Ops
130°F to 140°F ..................... Red Range – Below min continuous
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Section 2 – Limitations
2-9
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips IO-360, C/S Prop
2-3.7.
Oil Pressure
IAW Lycoming Operators Manual page 3-12 (29/51) ( Sec 3-8. Oil
Pressure):
Engine Gauge Range ............................................................ 20-120 psi
115 psi .............................. Cyan Line (Start & Warm-up Maximum)
95-120 psi ..... Red Range + Alert (95 psi Maximum for Operation)
90-95 psi....Yellow Range (Buffer between Normal and Maximum)
60-90 psi.....................................Green Range (Normal Operating)
55-60 psi.....Yellow Range (Buffer between Normal and Minimum)
55 psi ............................... Cyan Line (Normal Operation Minimum)
25-55 psi...................... Yellow Range + Alert (OK for Ground Idle)
20-25 psi............................................... Red Line + Alert (Too Low)
CAUTION
If at least 25 psi oil pressure is not indicated within 30
seconds, stop engine and determine trouble
2-3.8.
Mixture Settings
> 75% power ............................................................................. Full Rich
.......................................... Except takeoffs at high elevations
75% Max Power Cruise .................................................... < 150°F ROP
< 75% Power .................................................................................... LOP
Descents ........................................................................ Smooth Engine
2-10
Section 2 – Limitations
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
2-4.
FUEL
2-4.1.
Fuel Grade
IAW Lycoming Operators Manual page 3-10 (27/51)
(Sec 3-8. Fuel
& Oil): Aviation grade 100LL fuels in which the lead content is limited
to 2 c.c. per gal are approved for continuous use. Also the minimum
grade aviation fuel is 91/96 or 100/130.
2-4.2.
Fuel Flow
Gauge Range......................................................................... 0-25 gal/hr
Takeoff & Climb (Yellow Range) ................................. 11-25 gal/hr
Operating Range (Green Range) .................................. 7-11 gal/hr
Less than 65% power (White Range) .............................. 1-7 gal/hr
Flameout (Red Range + Alert .......................................... 0-1 gal/hr
(IAW Lycoming Operators Manual page 3-23 (34/51):
 Best Power - 75% power = ~11 gph,
 Best Economy - 65% power = 8.5 gph
2-4.3.
Fuel Pressures
IAW Lycoming Operators Manual page 3-10 (27/51)
Pressure): Inlet to fuel pump.
(Sec 3-8. Fuel
Gauge Range.......................................................................... 0 - 36 psi
Red Range + Alert .......................................................... 35 - 36 psi
Green Range .................................................................... 2 - 35 psi
Red Range + Alert .............................................................. 0 - 2 psi
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Section 2 – Limitations
2-11
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips IO-360, C/S Prop
2-4.4.
Fuel Capacity
Header (Aux) Tank ..........................................................................7 Gal
Wing Tank .....................................................................................43 Gal
2-4.5.
Fuel Tank Markings
2-4.5.1.
Header (Aux)Tank
Gauge Range ..................................................................................... 0-7
3-7 Gal ....................................................................... Green Range
2-3 Gal ........................................................... Yellow Range + Alert
0-2 Gal ............................................................... Red Range + Alert
2-4.5.2.
Wing (Main) Tank
Gauge Range ................................................................................... 0-43
13-43 Gal .................................................................... Green Range
10-13 Gal ....................................................... Yellow Range + Alert
0-10 Gal (No Slips Below 10 gal) ...................... Red Range + Alert
2-4.6.
Fuel Controls
Use the Header Tank for landings if:
 Header If X-Wind / slipping and ≤ 10 gal in wing tank
 Header If slipping for > 30 seconds while on wing tank
2-12
Section 2 – Limitations
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
This is due to possible uncovering of the wing tank sumps due to
sloshing or slipping maneuvers during landings.
Do not takeoff if fuel quantity display indicates less than 10 gal total
fuel.
2-5.
ELECTRICAL
2-5.1.
Load
2-5.1.1.
Main Alternator
Gauge Range.......................................................................... 0-61 amps
60-61 ................................................................... Red Range + Alert
55-60 ............................................................... Yellow Range + Alert
1-55 ............................................................................. Green Range
0-1 ....................................................................... Red Range + Alert
2-5.1.2.
Standby Alternator
Gauge Range.......................................................................... 0-20 amps
15-20.................................................................... Red Range + Alert
0-15.............................................................................. Green Range
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Section 2 – Limitations
2-13
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips IO-360, C/S Prop
2-5.2.
Voltage
Gauge Range .......................................................................... 11-15.1 V
15.0-15.1 Volts................................................... Red Range + Alert
14.1-15.0 Volts............................................... Yellow Range + Alert
13.4-14.1 Volts........................................................... Green Range
12.4-13.4 Volts............................................... Yellow Range + Alert
12.0-12.4 Volts................................................... Red Range + Alert
2-6.
WEIGHT LIMITS
Maximum Takeoff/Landing Weight (Gross) ................................ 2200 lb
Maximum Baggage Weight ........................................................... 100 lb
Maximum Aerobatic Weight (Gross) ........................................... 1900 lb
WARNING
These figures depend on the airplane being within safe
Center of Gravity limits. Do not fly the airplane if its
computed flight CG falls outside of the published limits.
Due to variables such as fuel, passenger, and baggage
weight, these figures may be reduced somewhat. Before
each flight, compute the CG to determine whether the
aircraft is within safe CG limits.
2-14
Section 2 – Limitations
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
2-7.
CENTER OF GRAVITY LIMITS
See Section 6 of this POH for CG limits.
2-8.
FLIGHT LOAD FACTORS
Between 1900 lbs and 2200 lbs .................................... +3.8 to -1.0 Gs
At an aerobatic weight of <1900 lbs. .............................. +6.0 to -4.0 Gs
2-9.
AEROBATIC MANEUVERING LIMITATIONS
During the flight test period, the below maneuvers were successfully
tested and logged by the test pilot. These maneuvers are now
approved in N11HC:
Aileron rolls
Loops
Split-S
Slow rolls
Cuban eights
Barrel rolls
Continuous rolls
Cloverleaf
Immelmanns
To add any aerobatic maneuvers beyond the nine listed above as
approved in N11HC will require putting the aircraft back into a Phase I
program and testing the new maneuvers for safety
The Glasair is not a competition class aerobatic aircraft. It was
designed as a sport aerobatic type plane.
NOTE
These listed aerobatic maneuvers are maneuvers that can be
performed in N11HC; pilot ability and skill will determine
whether they can be accomplished safely. It is recommend
that pilots new to N11HC get some aerobatic dual in N11HC
to become proficient in them before attempting any solo
aerobatics in the N11HC. Treat any aerobatic maneuvers
with respect and approach all practice with a calm,
disciplined attitude. Wear a parachute at all times and never
attempt any maneuvers below 4000 feet AGL.
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Section 2 – Limitations
2-15
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips IO-360, C/S Prop
NOTE
Adhere to FAR Part 91.303 when engaging in aerobatic
maneuvers. Refer to FAR Part 91.307 on the use of
parachutes.
WARNING
Snap rolls, tail slides, torque rolls, Lomcevaks, or any
other high empennage or fuselage loading maneuvers
are prohibited in the Glasair.
WARNING
The Glasair is a high performance aircraft. Aerobatics in
the Glasair are to be approach with caution and only
after dual from an experienced instructor. The aircraft
has such a low drag coefficient that in the event of falling
out of a maneuver, red line velocity can be reached or
exceeded in very little time.
WARNING
Do not exceed the structural design limits of the aircraft.
The limits are +6 Gs and -4 Gs at an aerobatic weight of
less than 1900 lb. Structural failure can occur if these
limits are exceeded.
WARNING
The wing tip extensions reduce the roll rate but do not
reduce the strength limitation. The reduction of roll rate
makes aerobatic maneuvers more challenging.
2-16
Section 2 – Limitations
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
WARNING
N11HC does NOT have an inverted oil system. Any
negative, slipping, or cross-controlling maneuvers are
prohibited.
2-10.
INTENTIONAL SPINS PROHIBITED
Due to many variables that affect spin recovery, intentional spins are
prohibited. Some of the variables that are cause of concern are: pilot
technique, the manner in which the spin is entered, slight differences in
wing and horizontal stabilizer incidence angles, center of gravity
location, number of turns into the spin, spin direction, aileron position,
power carried, and control rigging and adjustment
2-11.
FLIGHT IN ICING CONDITIONS
Flight in icing conditions is prohibited in the Glasair Super II-S FT. The
Glasair must not be exposed to icing encounters of any intensity. If the
airplane is inadvertently flown into icing conditions, the pilot must make
an immediate diversion by flying out of the area of visible moisture or
going to an altitude where icing is not encountered.
2-12.
FLIGHT IN THE VICINITY OF THUNDERSTORMS
The FAR Part 23 Airworthiness Standards for Normal, Utility, and
Acrobatic Category Airplanes require that the airplane’s structure be
protected from the catastrophic effects of lightning, and that the
airplane’s fuel system be designed to prevent the ignition of fuel vapor
by lighting
WARNING
The Glasair Super II-S FT does not comply with FAR Part
23 Standards for lightning protection because of its
composite structure which is transparent to an electrical
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Section 2 – Limitations
2-17
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips IO-360, C/S Prop
charge. For this reason, the Glasair Super II-S FT is
prohibited from flight in conditions that would expose
the airplane to the possibility of a lightning strike.
2-13.
PRECAUTIONS CONCERNING SLIPS
In order to help prevent fuel starvation as the result of slips or other
uncoordinated flight, a pair of fuel tank check valves are installed in the
wing tank. They help ensure that the wing tank fuel sump will remain
covered with fuel as fuel transfers from one side of the wing to the
other.
If drawing from the wing tank:
Slips are prohibited – with less than 10 gal. of fuel in the wing tank.
Slips longer than 30 seconds are prohibited.
WARNING
If the aircraft is parked on sloping ground with one wing
low and with a partially empty wing fuel tank, fuel slowly
transfers into the low wing creating a wing-heavy
condition that can cause control difficulty after takeoff.
Making tight turns while taxiing can have the same
effect. A heavy left wing is especially critical since the
resulting left-turning tendency exacerbates the effects of
engine torque. If you suspect an unbalanced fuel
condition, taxi to level ground and allow sufficient time
for the wing tank fuel level to equalize before attempting
takeoff.
NOTE
Because of the total drag with flaps extended, slips should
rarely be needed in the Glasair Super II-S FT.
2-18
Section 2 – Limitations
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
2-14.
MINIMUM EQUIPMENT LIST
Builders of Experimental Category aircraft must comply with Part 91.33
of the Federal Aviation Regulations which specifies the minimum
instrumentation and equipment that must be installed and operational
for various flight conditions. Equipment is specified for both VFR and
IFR flight and for both day and night conditions.
IFR Day
IFR Night
ELECTRICAL POWER
Alternators
Battery System
COCKPIT DISPLAY SYSTEM
Primary Flight Display (PFD)
Multifunction Display (MFD)
GMU 44 Magnetometer Unit
GSU 73 ADAHRS Air Data,
Attitude, Heading and
Reference System
EIS – Engine Information
System
VFR Night
System and/or Equipment
VFR Day
Switches on the control stick of N11HC are duplicated on the panel
except for flap operation and PTT. A PTT alternative is a handheld
mike or a portable PTT switch inserted into a TRS receptacle.
1
1
1
1
2
2*
2
2* *Stby ADI Battery
1
0
0
1
1
1
1
1
1
1
1
1
0
1
1
1
1
1
1
1
GTP 59 Temperature Probe
PMA8000B Audio Panel
GT-50 G-Meter, clock etc.
0
0
0
1
1
0
1
1
0*
1
1
0*
Current Database
0
0
0*
0*
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Section 2 – Limitations
Remarks and/or
Exceptions
Min day VFR: MP,
Tach, Fuel Gauge,
Oil Temp & Press
For ADC
* If another clock is
available
* If VOR nav and paper
or electronic charts are
2-19
IFR Night
IFR Day
VFR Night
System and/or Equipment
VFR Day
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips IO-360, C/S Prop
Remarks and/or
Exceptions
available
RADIOS
G430W
SL40 or G430W
Control Stick PTT
0
Intercom
ELT
0
1
STANDBY INSTRUMENTS
Airspeed Indicator 1*
Attitude Indicator 0
Altimeter 1*
Magnetic Compass 1*
FLIGHT CONTROLS
Elevator Trim Tab 1
Trim Tab Indicator 0
Flap System 1
AOA System 0
Toe Brakes 1
Parking Brakes 0
AUTOPILOT
Autopilot System 0
Disconnect Functions 0
FUEL
Electrically Driven Boost Pump
Engine Driven Boost Pump
Fuel Selector Valve
2-20
1
1
1
0
1
1
0
1
1
0
0
1
0
1
0
1
1
0
1*
1*
1
1
1
1
1
1
1
1
1
0
1
0
1
0
1
0
1
0
1
0
1
0
1
0
1
0
0
0
0
0
0
0
1
1
1
1
1
1
1
1
1
Section 2 – Limitations
For Nav (GPS or VOR)
For Comm
Provided alternate mic
available
Remote Switch N/R if
ELT is operative in
ARMED mode
* If inop on PFD
* If inop on PFD
* If inop on PFD
Provided deactivated
Provided alternate
disconnect available
12-10-2014
System and/or Equipment
VFR Day
VFR Night
IFR Day
IFR Night
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
Fuel Gauge
ICE AND RAIN PROTECTION
Emergency Static Air System
Pitot Heat
LIGHTS
Cockpit and Display Lighting
Landing Light
Navigation Lights
Strobe Light
Flashlight
RESTRAINT SYSTEM
Seat Belt and Shoulder
Harness
ELT
DOCUMENTS(FAA required)
1
1
1
1
0
0
0
0
1
1
1
1
0
0
0
0
0
1
0
3
1
1
0
0
0
0
0
1
0
3
1
1
1
1
1
1
1
5
1
5
1
5
1
5
Remarks and/or
Exceptions
Each Tank
(per occupied seat)
Airworthiness,
Registration, FCC (outof-US, POH, W&B,
Limitations,
When the left PFD is inoperative, the system is limited to DAY VFR
operations only and the autopilot may be inoperative.
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Section 2 – Limitations
2-21
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips IO-360, C/S Prop
2-15.
PLACARDS and MARKINGS
Most labels are printed on Staples 1" x 2 5/8" compatible with Avery
5160/8160. The text for these labels are located here.
Labels for the control stick are printed on 2x3 rectangle ULTRA WaterResistant White Vinyl Inkjet Label Sheets from
www.labelsbythesheet.com. One label can be used for all decals and
there are 12 labels per sheet. The text for the labels are within one .gif
picture located here and can be printed onto one label.
NOTE
All placards should be highly visible and easy to read.
Advise passengers of pertinent placards.
2-15.1.
Experimental
The FAA required word “EXPERIMENTAL”, in 2 inch high block letters
to be displayed near each entrance to the cabin is displayed on the
baggage hat rack.
2-15.2.
Data Plate
The FAA requires a permanently installed; fireproof identification plate
must be permanently stamped or engraved with the information
required by FAR 45.13. The data plate must be located on the exterior
of the aircraft, either just aft of the entry door or on the fuselage near
the tail surfaces and must be legible to a person standing on the
ground. Data Plate for N11HC is located just under the leading edge of
the left horizontal stabilizer and states::
 Builder - “Philip J. Conway”
 Model – “Glasair Super II-S FT
 Serial No – “2329”
2-22
Section 2 – Limitations
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
2-15.3.
Passenger Warning
The Passenger Warning Placard, is permanently installed on the panel
in full view of the occupants with the words: “PASSENGER WARNING
– THIS AIRCRAFT IS AMATURE BUILT AND DOES NOT COMPLY
WITH FEDERAL SAFETY REGULATIONS FOR STANDARD
AIRCRAFT.”
2-15.4.
AOA Exterior Placards
Around top and bottom of left wing AOA holes
2-15.5.
Canopies
Located near the latch handle for each gull wing canopy:
“WARNING – DO NOT OPEN CANOPY IN FLIGHT”, then
“OPEN” with arrow in proper direction
2-15.6.
Arm-Rest Labels:
 RT CTRL STK BUTTONS Disable (with up arrow) – near control
switch on armrest.
 12 VDC 5 Amp Max – by auxiliary electrical receptacle
 TRIM UP/DN with arrows – next to trim
2-15.7.
Other Instrument Panel Labels:
 “AOA” “NOT TO BE USED AS A PRIMARY INSTRUMENT”
“Stabilized operation is prohibited: > 25” MP and 2300-2350 RPM
/ < 15” MP and >2600 RPM”.LOW VOLTAGE – On Instrument
panel under autopilot.
 THROTTLE Push To Increase – above throttle
 MIXTURE Push To Increase – above mixture
 PROP RPM Push To Increase – above prop control
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Section 2 – Limitations
2-23
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips IO-360, C/S Prop
 PARKING BRAKE PULL ON While Applying Toe Brakes – above
parking brake knob.
 “AOA” – below AOA indicator
 “LOW VOLTAGE” – below red light below AOA indicator.
 IPS DISABLE (with down arrows) – by white toggle switch beside
rheostats
 SWITCHES – by left rheostat controlling switch lighting
 INSTRUMENTS – by center rheostat controlling standby
instrument lighting
 G3X – by right rheostat controlling G3X lighting
2-15.8.
2-24
Control Stick Grip Placards
Section 2 – Limitations
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
Section 3 - Emergency Procedures
Table of Contents
3-1. INTRODUCTION ........................................................................ 3-3
3-2. OFF AIRPORT LANDING .......................................................... 3-4
3-3. ENGINE FAILED OR FAILING – Time to Analyze..................... 3-4
3-4. ABORTS ..................................................................................... 3-5
3-4.1. Abort Takeoff – While on Runway ........................................ 3-5
3-4.2. Abort After Takeoff – Land on Runway ................................ 3-5
3-5. FIRE ............................................................................................ 3-5
3-5.1. Fire Extinguisher................................................................... 3-5
3-5.2. Engine Fire – During Start .................................................... 3-6
3-5.3. Engine Fire – In Flight .......................................................... 3-6
3-5.4. Cabin / Wing Fire – In Flight ................................................. 3-7
3-5.5. Electrical Fire – On Ground .................................................. 3-8
3-5.6. Electrical Smoke or Fire – In Flight ...................................... 3-8
3-6. ENGINE PROBLEMS ................................................................. 3-9
3-6.1. Low Oil Pressure & Normal Oil Temperature ....................... 3-9
3-6.2. Low Oil Pressure & High Oil Temperature ........................... 3-9
3-6.3. Rough Running Engine - Suddenly .................................... 3-10
3-6.4. Rough Running Engine – Slowly ........................................ 3-10
3-7. ELECTRICAL OR AUTOPILOT ............................................... 3-10
3-7.1. Alternator Failure (Main or Standby) .................................. 3-10
3-7.2. Autopilot Malfunction .......................................................... 3-11
3-8. ADC OR AHRS ......................................................................... 3-11
3-9. EMERGENCY DESCENT ........................................................ 3-12
3-10. GLIDE ................................................................................... 3-12
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Section 3 – Emergency Procedures
3-1
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
3-11.
3-12.
3-2
SPIRAL DIVES ..................................................................... 3-12
SPINS ................................................................................... 3-13
Section 3 – Emergency Procedures
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
3-1.
INTRODUCTION
The following basic rules apply to all aircraft emergencies and should
be thoroughly understood by all aircrews:
Maintain Aircraft Control.
Analyze the situation and take proper action
Land as soon as practicable.
The emergency procedures described in this section are applicable to
most aircraft including the Glasair Super II-S FT. These procedures
are suggested as the best course of action for coping with the
particular condition described, but are not a substitute for sound
judgments and common sense. Since emergencies rarely happen,
their occurrence is usually unexpected, and the best corrective action
may not always be obvious. Pilots should familiarize themselves with
the procedures given in this section and be prepared to take
appropriate action should an emergency arise.
These are only recommended procedures and might need to be
modified depending upon the situation. Each pilot must make the final
decision as to the correct procedure under the circumstances and is
responsible for the final decision.
The Lycoming aircrat engine is very reliable and the probability of a
catasrophic engine failure without some type of advance warning is
quite low. Early indications of an engine failure are lowering oil
pressure, increasing oil temprature, high cylinderhead temperatures,
excessive mechanical noise, lowering fuel pressure, and so on. Pilot
induced failures on the other hand are far more common: mixture set
too lean, fuel starvation etc. Keep these in mind if an engine problem
or failure should arise.
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
3-2.
OFF AIRPORT LANDING
Airspeed / AOA............................................................ Vg (1Y ~85 K)
Best Field ............................................................................ Into Wind
Fuel Pump ...................................................................................... Off
3 Power Knobs .............................................................................. Aft
Fuel Selector ................................................................................. Off
Mags ............................................................................................... Off
Seat Belts ................................................................................... Tight
Flaps ................................................................................ As Required
Talk .................................................................................... Emergency
Squawk ........................................................................................ 7700
High Key / Low Key.......................................................... 1000’ & 500’
Before Touchdown
Master Switch ................................................................................ Off
ELT.......................................................................................... Activate
Touch down at the minimum controllable airspeed, being careful not to
stall and drop the airplane in. Especially if forced to land in trees, allow
the airplane to fly into the trees rather than stalling and dropping to the
ground through the trees.
In very rough terrain, try to fly the airplane so that the fuselage area
misses the larger objects, such as the biggest tree trunks and rocks.
Sacrifice other parts of the airframe to absorb the impact energy.
Tall soybean fields are more apt to flip the airplane on its back than a
corn field.
3-3.
ENGINE FAILED OR FAILING – Time to Analyze
Airspeed /AOA............................................................. Vg (1Y ~85 K)
Best Field ...................................................GPS Nearest / Into Wind
Fuel Pump ...................................................................................... On
3 Power Knobs ....................................................... 1/4 Open / In / In
Fuel Selector ......................................................................... Change
Mags ....................................................................................... Change
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Section 3 – Emergency Procedures
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
Engine Instruments .................................................................... Check
Talk .................................................................................... Emergency
Squawk ........................................................................................ 7700
Refer to "OFF AIRPORT LANDING " (If Required)
Land ............................................................................................ ASAP
NOTE
A rough engine may be caused by a bad magneto, induction
problems, improper leaning, plug fouling, fuel starvation,
water in the fuel, etc.
3-4.
ABORTS
3-4.1.
Abort Takeoff – While on Runway
Flaps........................................................................................ Retract
Mixture ................................................................................. Idle Cutoff
Master Switch ..................................................................................Off
Mags ................................................................................................Off
Fuel Selector ....................................................................................Off
3-4.2.
Abort After Takeoff – Land on Runway
DIVE........................................................ Best Glide AOA (1-Yellow)
Flaps.............................................................................................. Full
Mixture ................................................................................. Idle Cutoff
Master Switch ..................................................................................Off
Mags ................................................................................................Off
Fuel Selector ....................................................................................Off
3-5.
FIRE
3-5.1.
Fire Extinguisher
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Section 3 – Emergency Procedures
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
A Halon 1211 fire extinguisher is installed behind the right seat. Unclip
from the mounting bracket, pull the safety pin and spray at base of fire.
3-5.2.
Engine Fire – During Start
If Engine is NOT Running
o Continue Cranking with Starter
This is an attempt to pull the fire back into the engine
o Mixture ...................................................................... Idle Cutoff
o Throttle....................................................................... Full Open
o Fuel Selector ......................................................................... Off
o If Sill on Fire ..................................................Use Extinguisher
If Engine IS Running
o Continue Running for a few Seconds then…
o Mixture ...................................................................... Idle Cutoff
o Throttle....................................................................... Full Open
o Fuel Selector ......................................................................... Off
o If Sill on Fire ..................................................Use Extinguisher
3-5.3.
Engine Fire – In Flight
Fuel Selector ................................................................................. Off
3 Power knobs............................................................................... Aft
Heat/Defrost & Air Vents .............................................................. Off
ADI Backup Battery ........................................................ On (If IMC)
Master Switch ................................................................................ Off
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Section 3 – Emergency Procedures
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
NOTE
The G3X’s and AOA will become inoperative with the battery
and alternators off. Only the standby instruments will be
available.
Prop .......................................................................... Stop (If Possible)
Door .................................................................... Jettison (if Required)
Refer to .............................................. Off Airport Landing – No Power
WARNING
Open the door in flight only as a last resort effort. Never
attempt this procedure under normal circumstances as
the doors will depart the aircraft. Remember to let go of
the door as it departs.
NOTE
Consider going fast to blow out the fire and get on the ground
faster. Consider slipping to get the flames to one side of the
aircraft.
3-5.4.
Cabin / Wing Fire – In Flight
Vents, Heat/Defrost................................................................ Closed
ADI Backup Battery ........................................................ On (If IMC)
Master Switch ................................................................................ Off
NOTE
The G3X’s and AOA will become inoperative with the battery
and alternators off. Only the standby instruments will be
available.
Attitude ......................................................................................... Slip
Fire Extinguisher ................................................................. Activate
Land .......................................................................................... ASAP
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Section 3 – Emergency Procedures
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
3-5.5.
Electrical Fire – On Ground
All Electrical Switches .................................................................. Off
Mixture ................................................................................ Full Lean
Extinguisher ............................................................................. Use It
3-5.6.
Electrical Smoke or Fire – In Flight
Master Switch ................................................................................ Off
Heat/Defrost ................................................................................... Off
ADI Backup Battery ........................................................ On (If IMC)
WARNING
The G3X’s and AOA will become inoperative with the
battery and alternators off. Only the standby
instruments will be available if the Stby ADI battery
switch is on.
All Electrical Switches ..................................................................... Off
Speed .................................................................................. < 80 Knots
Air Vents ....................................................................... Open (maybe)
Fire Extinguisher ........................................................Use (If Possible)
Slip ................................................................................... If Necessary
NOTE
Consider slipping to get the flames away from the aircraft.
Door ................................................................. Jettison (if Required)
WARNING
Open the door in flight only as a last resort effort. Never
attempt this procedure under normal circumstances as
the doors will depart the aircraft. Remember to let go of
the door as it departs.
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Section 3 – Emergency Procedures
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
NOTE
If smoke or fire ceases and equipment is necessary,
individually restore only the required electrical equipment –
one system at a time.
Flap Switches ............................................................... Off (Centered)
Battery..............................................................................................On
Standby Alternator ...........................................................................On
Required Electrical Equipment .......................................One at a time
Land ................................................................... As Soon As Practical
3-6.
ENGINE PROBLEMS
3-6.1.
Low Oil Pressure & Normal Oil Temperature
Maybe the oil pressure gauge or relief valve is malfunctioning
A leak in the line to the gauge is not necessarily cause for an
immediate precautionary landing because an orifice in this line will
prevent a sudden loss of oil from the engine sump.
Engine Power ................................................ Set Then Leave Alone
Land ............................................................................................ ASAP
Refer to .................................................................. Off Airport Landing
3-6.2.
Low Oil Pressure & High Oil Temperature
Imminent Engine Failure ..................................................... Suspect
Engine Power ................................................ Set Then Leave Alone
Refer to .................................................................. Off Airport Landing
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
3-6.3.
Rough Running Engine - Suddenly
................................. If it came on SUDDENLY, suspect a mag problem
Mag Switch .......................................................... Choose Best Power
Power Settings .........................................................................Change
Mixture ....................................................................................... Enrich
Land ............................................................................................ASAP
3-6.4.
Rough Running Engine – Slowly
............................... If it came on SLOWLY, suspect a fouled spark plug
Mag Switch .......................................................... Choose Best Power
Mixture Control ......................... Select Bad Mag & Lean Aggressively
Problem Continues ..................................................................... Land
NOTE
A rough engine may be caused by a bad magneto, induction
problems, improper leaning, plug following, fuel starvation,
water in the fuel, etc.
3-7.
ELECTRICAL OR AUTOPILOT
3-7.1.
Alternator Failure (Main or Standby)
Zero amps and volts indicates an alternator failure
Standby Alternator .......................................................................... On
Main Alternator ...........................................OFF Momentarily then ON
If Output is Restored .............................................................. Continue
If Output is NOT restored ................................ Failed Alternator - OFF
Nonessential Equipment ......................................... OFF (as required)
Good Alternator ........................................................................ Monitor
Land ............................................................................................ASAP
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Section 3 – Emergency Procedures
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
3-7.2.
Autopilot Malfunction
The Autopilot can be disconnected by:
Control Stick Disconnect Button ................................................. Press
AP Key on MFD .......................................................................... Press
AP Key on AP Controller ............................................................ Press
Autopilot Rocker Switch ...................................................................Off
AP Circuit Breaker ......................................................................... Pull
3-8.
ADC OR AHRS
The Attitude and Heading Reference System (AHRS) performs
attitude, heading, and vertical acceleration calculations for the G3X
System, utilizing GPS, magnetometer, and air data in addition to
information from its internal sensors. Attitude and heading information
are updated on the PFD while the AHRS receives appropriate
combinations of information from the external sensor inputs.
Loss of GPS, magnetometer, or air data inputs is communicated
to the pilot by message advisory alerts. Any failure of the internal
AHRS inertial sensors results in loss of attitude and heading
information (indicated by red ‘X’ flags over the corresponding
flight instruments).
If GPS input fails, the AHRS can continue to provide attitude and
heading information to the PFD as long as magnetometer and airspeed
data are available and valid.
If the magnetometer input fails, the AHRS continues to output valid
attitude information; however, the heading output on the PFD Page is
flagged as invalid with a red ‘X’.
Failure of the air data input has no effect on the AHRS output while
AHRS is receiving valid GPS information. Invalid/unavailable airspeed
data in addition to GPS failure results in loss of all attitude and heading
information. Likewise, loss of magnetometer (heading) data, in
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Section 3 – Emergency Procedures
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
combination with loss of GPS data results in a loss of all attitude and
heading information.
3-9.
EMERGENCY DESCENT
Throttle .......................................................................................... Idle
Propeller ..................................................................... In – High RPM
Flaps ................................................................................... Full Down
Airspeed ..................................................................... 122 Knots Max
3-10.
GLIDE
Throttle ............................................................................. As Required
Propeller ....................................................................... Aft – Low RPM
Flaps ................................................................................................Up
Speed/AOA
Best Glide (Vy) .......................................................................... 104? K
Best Endurance (Vx) ..................................................................... 86 K
3-11.
SPIRAL DIVES
Throttle ........................................................................................... Idle
G ............................................................................................... Unload
Wings ...........................................................................................Level
Aircraft Pitch .................................................................................Level
A spiral dive is a situation that develops when the nose of the aircraft
begins dropping out of a turn. (A spin, on the other hand, develops
from excessive yaw during a stall.) In a spiral dive, speed builds
rapidly as the nose drops and, if the pilot attempts to raise the nose by
applying back pressure, the turn will tighten and G forces will begin to
build. If allowed to continue, the aircraft will either strike the ground at
high speed or will suffer in-flight structural failure from excessive G
loads.
The proper recovery from a spiral dive is to first reduce power by
bringing the throttle control back to prevent exceeding Vne.
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Section 3 – Emergency Procedures
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
Simultaneously with the power reduction, level the wings and then
apply gentle back pressure to stop the dive.
A spiral dive is a common result (usually fatal) of flying into instrument
conditions without proper training or proper instrumentation. For this
reason, pilots who are not rated and current in IFR flight must avoid
flight in conditions of reduced visibility.
3-12.
SPINS
WARNING
Intentional spins are prohibited in the Glasair Super II-S
FT.
Since the wing must be stalled for a spin to occur, inadvertent spins
can be prevented by avoiding inadvertent stalls. The pilot must be
thoroughly familiar with the Glasair’s stall and pre-stall behavior to
avoid inadvertent stalls. Remember that a stall can occur at any
airspeed and attitude. A pilot who is thoroughly familiar with the
Glasair’s stall behavior under all conditions will be unlikely to enter an
inadvertent spin.
The stall strips must be installed on the inboard wing leading edges to
help ensure that there is no tendency for a wing to drop during the stall
and to provide a good margin of pre-stall buffet or stall warning.
If a spin is entered inadvertently, immediately apply standard spin
recovery control inputs.
Rudder .......................................................FULL Opposite Rotation
Stick ........................................ Neutral (full aft for developed spin)
Power ............................................................................................ Idle
Flaps................................................................................................Up
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Section 3 – Emergency Procedures
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
As rotation stops
Rudder................................................................................ Neutralize
Stick................................................................ Release or Neutralize
Dive ......................................................................................... Recover
AOA............................................................................................. Use It
G ................................................................................................ +6 / -4
WARNING
If a spin is entered inadvertently, do not push full forward
stick. This action will substantially delay recovery,
accelerate the spin, and could prevent recovery.
Recommended action is full aft stick until rotation stops.
This holds the elevator in the up position which provides
more airflow over the rudder to help stop rotation. As
rotation stops, release back pressure to recover from the
stall. Also, keep the ailerons neutral. Aileron opposite
to the spin direction will flatten the spin, making
recovery more difficult
If a wing drops during a stall, immediately apply “top” rudder to catch
the wing drop and then apply forward stick to break the stall before the
situation can progress to a fully developed spin.
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Section 3 – Emergency Procedures
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
Section 4 - Normal Operating Procedures
Table of Contents
4-1. INTRODUCTION ...................................................................... 4-3
4-2. PREFLIGHT CHECKLIST ........................................................ 4-3
4-2.1. PREFLIGHT / WALK AROUND INSPECTION .................. 4-3
4-3. PRE-START, START & TAXI CHECKLIST ............................. 4-6
4-3.1. BEFORE STARTING ENGINE........................................... 4-6
4-3.2. STARTING ......................................................................... 4-7
4-3.3. AFTER STARTING ............................................................ 4-7
4-4. TAXI .......................................................................................... 4-8
4-5. EOR (LAST CHANCE) ............................................................. 4-8
4-6. TAKEOFF ............................................................................... 4-10
4-6.1. TAKEOFF - Normal .......................................................... 4-10
4-6.2. CLIMB ............................................................................... 4-10
4-6.3. Stabilized operation is prohibited ..................................... 4-10
4-7. CRUISE .................................................................................. 4-11
4-7.1. Cruise Performance ......................................................... 4-11
4-7.2. Cruise Settings ................................................................. 4-11
4-8. LEANING ................................................................................ 4-12
4-8.1. Limits ................................................................................ 4-12
4-9. VFR DESCENT & LANDING .................................................. 4-13
4-9.1. PRE DESCENT ................................................................ 4-13
4-9.2. DESCENT ........................................................................ 4-13
4-9.3. PATTERN ......................................................................... 4-14
4-9.3.1. 45° to Downwind ...................................................... 4-14
4-9.3.2. Downwind (FGuMPSS) ............................................ 4-14
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
4-9.3.3. Base / Final ............................................................... 4-14
4-9.3.4. Traffic Pattern Picture ............................................... 4-15
4-9.4. Rollout ............................................................................... 4-16
4-9.5. CLEAR OF RUNWAY....................................................... 4-16
4-9.6. SHUTDOWN..................................................................... 4-16
4-9.7. REFUELING ..................................................................... 4-16
4-10. IFR DESCENT, APPROACH & LANDING ............................. 4-17
4-10.1. PRE DESCENT ................................................................ 4-17
4-10.2. DESCENT......................................................................... 4-18
4-10.3. IAF – IF ............................................................................. 4-18
4-10.4. IF – FAF ............................................................................ 4-18
4-10.5. FAF ................................................................................... 4-19
4-10.6. 500’ AGL ........................................................................... 4-19
4-10.7. MISSED APPROACH ....................................................... 4-19
4-11. AEROBATICS ......................................................................... 4-20
4-11.1. Over-The-Top Maneuvers ................................................ 4-21
4-11.2. HASELL Check ................................................................. 4-21
4-11.3. Entry Parameters .............................................................. 4-21
4-11.4. Spin Recovery – Primed ................................................... 4-21
4-12. MOORING .............................................................................. 4-22
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Section 4 – Normal Operating Procedures
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
4-1.
INTRODUCTION
This section describes the normal operating procedures for both
ground and flight operations. See Section 10 – Safety and Operational
Tips for additional information plus Warnings, Cautions, and Notes
concerning items in this section.
Items highlighted in yellow are items that could cause embarrassment
if not complied with.
4-2.
PREFLIGHT CHECKLIST
Before every flight, inspect the exterior and interior of the aircraft for
anything that looks suspicious or out of line. Use the following preflight
walk-around checklist as a guide when “preflighting” the aircraft.
4-2.1.
PREFLIGHT / WALK AROUND INSPECTION
Walk-up
 If < 40°F / 4°C ......................................................... Preheat Engine
 FSS Called........................................................Wx, TFR, NOTAMS
 Oil Qty .................................................................................... Check
o 6 qt minimum (Double Ring = 6 qt)
 Oil Dip-Stick & Door .............................................................. Secure
 Windows ................................................................................. Clean
 Remove:
o Rudder Control-Lock
o Tie-downs
o Chocks
o Pitot Cover
o Tow Adaptor
 Tires ......................................................................50 nose, 35 main
 Wings ....................................................................................... Level
o Expect heavy wing on T/O if tanks not full
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
Cabin
 Fire Extinguisher ................................................................ Charged
 #1 POH .............................................................................. ARROW
o Airworthiness, Registration, Restrictions Letter. POH, W&B
 #2 POH – VOR Log & GPS dB ............................................ Current
 Controls ..................................................................................... Free
 Cross-Cockpit Air Vent ............................................................... Set
 ELT .................................................................................... No lights
 Circuit Breakers ............................................................................ In
 Small Toggle Switches ................................. Up, Test/Down, Down
o IPS Switch, ADI Backup Battery, A/P Source
 Mag Switch ..............................................................Off, Key Handy
 Battery ......................................................................................... On
 Lights ........................................................................... On to Check
 Power Levers .............................................................. Out / In / Out
 Fuel Selector ........................................................................ Header
 Static - Alternate Air ..................................... Cycle - Horz is Closed
 Pitot Heat .................................................................................... On
 PFD ..................................................................... Log Hobbs & Fuel
 Fuel Gauges .......................................................................... Check
 Bat Voltage ............................................................................ Check
 Battery ......................................................................................... Off
 Rocker Switches ......................................................................... Off
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Section 4 – Normal Operating Procedures
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
Left Wing / Sumps / Left Gear






Pitot Tube .............................................................. Warm and Clear
AOA Air/Water Separator .................................................... Drained
AOA Pressure Ports (2) ........................................................... Clear
Fuel Cap ............................................................................... Secure
Belly Panel Screws ............................................................... Secure
Left Gear ...................................................... Condition/Inflation (35)
Nose & Right Gear








Nose Gear ............................................. Condition/Inflation (50 psi)
Air Intakes ................................................................................ Clear
Alternator Belt .......................................................... Check Tension
Header Fuel Cap .................................................................. Secure
Oil Stick and Door ................................................................. Secure
Exhaust Pipe......................................................................... Secure
Right Gear ................................................... Condition/Inflation (35)
Belly Panel Screws ............................................................... Secure
Right Wing, Left Fuselage




Fuel Cap ............................................................................... Secure
Aileron ................................................. Free, Secure, Counter Wgts
Flap ....................................................................................... Secure
Static Port ................................................................................ Clear
Remainder






Strobe ............................................................................... Complete
Elevators & Rudder ............................ Free, Secure, Counter Wgts
Static Port ................................................................................ Clear
OAT Sensor .................................................................. No Damage
Flap ....................................................................................... Secure
Aileron ................................................. Free, Secure, Counter Wgts
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
4-3.
PRE-START, START & TAXI CHECKLIST
4-3.1.
BEFORE STARTING ENGINE
IAW Lycoming Operators Manual page 3-2 (19/51)
Procedures)














4-6
(Starting
Key ................................................................................................ In
Cell Phones................................................................................. Off
Master Switch ............................................................................. On
Exterior Preflight ............................................................... Complete
o Chocks .......................................................................... Removed
o Oil Cap and Door ................................... In Place / Tight / Closed
Brakes ............................................................................. Test & Set
Belts, S/H ........................................................... Adjust and Locked
Cockpit .......................................................... Organized & Secured
Crew Briefing
o Responsibilities, Who’s PIC, Quiet Cockpit
o Door Operation, Vents, Seat Belts, Fire Ext
Control Stick Enable Rocker Switch .............................. As Desired
Trim ............................................................................................. Set
Fuel Selector ............................................................................ Wing
Power Levers ................................................................. In / In / Out
PFD Engine – Fuel ............................................. Set Fuel on Board
PFD Engine – Main .......................................... Fuel Pressure Page
Section 4 – Normal Operating Procedures
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
4-3.2.
STARTING
 Strobes ........................................................................................On
 Boost Pump ................................................................... On (If Req)
 Mixture .................................................................... In / Out (If Req)
Until a slight but steady fuel flow noted (approx 3-5 sec)
 Boost Pump .................................................................................Off
 Throttle ................................................................. 1 turn in from idle
o (½ way in if Flooded or in if hot)
 Starter .................................................................................. Engage
 Mixture ........................................................... SLOWLY to Full Rich
 Throttle ................................................................... 900 - 1000 RPM
o <= 1000 RPM until oil temp registering
o < 1200 RPM until oil temp > 90°
 Oil Pressure .......................................................................... Check
o Idling .................................................................................>24 psi
o Normal out of idle ..........................................................60-90 psi
o Minimum ............................................................................. 55 psi
o Maximum ............................................................................ 95 psi
4-3.3.
AFTER STARTING






Rocker Switches ...................................................................As Req
Flaps ............................................................................................ Up
Mixture ................................................................ Lean Aggressively
G3Xs/G430 dB currency............................................. Menu2/Aux2↓
Transponder ..................................................................... 1200 / Alt
AOA .......................................................................................... Test
o Red Tests, Black Dims
o All lights for several sec & audio
 Autopilot ........................................................................... AP / EFIS
o HDG .......................................................................... Moves Stick
o Alt & Vert Speed ....................................................... Moves Stick
o Control Stick .............................................................Disconnects
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Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
 Flap Switches.............................................................................. Off
 Flight Instruments .................................................................. Check
o Standby Compass ............................................................. Check
o Heading Indicators (2) ....................................................... Check
o Attitude Indicators (3)......................................................... Check
o Altimeters (3) ................................................Field Elevation ±75’
4-4.
TAXI
 Parking Brake ............................................................................. Off
 Toe Brakes............................................................................. Check
 Turning Taxi .......................................................................... Check
o Attitude indicators
o Rate of Turn
o Skid Indicator (Ball)
o Heading indicators
4-5.
EOR (LAST CHANCE)
IAW Lycoming Operators Manual page 3-4 (21/51) ( Ground Check)
 Flight Controls ....................................................... Free and Correct
 Avionics........................................................................ Check & Set
o Radios .....................................................................Comm & Nav
o Altimeters ................................................................................ Set
o Altitude & Heading ........................................................ Preselect
o CDI ............................................................................ Nav Source
o Transponder ........................................................................... Set
o Flight Plan ........................................................................Entered
o Destination ....................................................................... Correct
o DTK, Miles, Time ............................................................. Correct
 Flight Instruments ............................................ PFDs & Stby Check
 Engine Instruments .......................... (before > 1200 RPM) GREEN
 Mixture ............................................................ As Lean As Possible
4-8
Section 4 – Normal Operating Procedures
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
 Alternator Checks ..................................................... Oil temp > 90°
o MFD .......................................................................... Engine/Elec
o RPM ..................................................................................... 1200
o Voltage............................................................... 13.4 - 14.1 Volts
o Amps............................................................................. Indicating
o MAIN ALT ............................................... Off (Checking Bat Pwr)
o STBY ALT .......................................... On (STBY Picks Up Load)
o MAIN ALT .................................................... On (Relieves STBY)
o STBY ALT ................................................................................Off
 MAG / Prop Check .............................................. MFD Engine Main
o RPM ................................... (Enrichen Mixture if Required) 1700
o Prop ................................................. (If Oil Cold) Cycle Quickly
o MAG ....................(Check EGT Rise on Single MAGs) B-L-R-B
 Pitot Heat, Lights, Etc ..................................................... As Desired
 Fuel Pump ...................................................................................On
 Flaps ......................................................................................... ~20°
 Doors, Seats & Seatbelts ...................................................... Check
 Mixture ...................................................................................... Rich
 Warning/Caution Lights ..............................................................Out
 Engine Gauges ...................................... (Oil Temp > 100°) Normal
 DOUBLE CHECK DOORS!
 If Mags check bad:
o Mixture .......................................................................... Full Rich.
o Throttle....................................................................... 2200 RPM.
o Mixture ...................................... Lean slowly to slight roughness.
o Mixture ......................... Enrich slightly to obtain smooth running.
o Timer.................................................... Start, run for 60 seconds.
o Mixture .......................................................................... Full Rich.
o Throttle........................................................................ 1700 RPM
o Mags ........................................................................ Check again
12-10-2014
Section 4 – Normal Operating Procedures
4-9
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
4-6.
TAKEOFF
4-6.1.
TAKEOFF - Normal





Prepare to Abort ................................................................ Psyched
Runway Hdg .......................................................................... Check
Power Levers ................................................................. All Forward
Engine Gauges .....................................................................Normal
Rotate (Vr) ....................................................................... ~60 knots
o Vy ................................................................................. 108 knots
o Va & Vclimb ................................................................. 126 knots
o Vx, Vg, L/Dmax, Max End ......................................... 1Y ~85 knots
o Vs, V15, V25, V40 ............................................ 67, 64, 60, 58 knots
4-5 KIAS Slower at 1700 lbs
 Flaps .......................................................Up > 90 KIAS < 122 KIAS
4-6.2.




CLIMB
Flap Switches.............................................................................. Off
Fuel Selector ............................................................................ Wing
Fuel Pump................................................................................... Off
Power ......................................................................Adjust for CHTs
4-6.3.
Stabilized operation is prohibited
> 25” MP and ................................................................ 2300-2350 RPM
< 15” MP and .................................................... > 2600 RPM (white arc)
4-10
Section 4 – Normal Operating Procedures
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
4-7.
CRUISE
4-7.1.
Cruise Performance
The following figures are “starting points” for fuel flow and TAS.
GW 1755
55%
TAS/FF/OAT
65%
TAS/FF/OAT
75%
TAS/FF/OAT
55%
TAS/FF/OAT
65%
TAS/FF/OAT
75%
TAS/FF/OAT
PA 3000’
PA 5000’
PA 7000’
PA 9000’
GW 2150
PA 3000’
PA 5000’
PA 7000’
PA 9000’
4-7.2.
Cruise Settings
 Fuel Selector............................................................................ Wing
 Power .......................................................................................... Set
o Rule of thumb for MP at altitudes up to 15,000 ft or so is 29"
minus the actual altitude in thousands. i.e. 22" at 7,000', 26” at
3000’.
o Between 1800 & 2300 RPM, MP can be 4.5 above square.
o Between 2400 & 2700 RPM, MP can be 2 above square.
o Reference POH Section 5 Performance chart
 Mixture ............................................................................. Fine Tune
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Section 4 – Normal Operating Procedures
4-11
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
 Lights (in & out) ............................................................ As Required
 Power Setting Results ..........................................................Record
Ops Check







Fuel Pump................................................................................... Off
Fuel Selector ............................................................................ Wing
Fuel Quantity........................................................................ Enough
Engine Gauges ...................................................................... Check
Altimeters .................................................................................... Set
Compass vs AHARS .............................................................. Check
Flap Switch ................................................................................. Off
4-8.
LEANING
NOTE:
IAW Lycoming Operators Manual page 3-5 (22/51) (Leaning
Procedures)
N11HC has GAMI injectors so: Stay away from 50° ROP. Always
cross-check the CHT when leaning. Maximum CHT temperatures
have priority over reaching peak EGT temps.
 Maximum Power Cruise (approximately 75% power) – Never lean
beyond 150°F / 66°C ROP.
 Best Economy Cruise (approximately 74% power and below) –
Operate LOP.
4-8.1.





4-12
Limits
CHT No Way – No How (Red Flash) ................................... <500°F
CHT Getting Too High (Red Steady) .............................. 435-499°F
CHT High Performance Cruise (Yellow) ......................... 400-435°F
CHT Economy Cruise (Green) ............................................ <400°F
>75% Power ..................................................................150°F ROP
Section 4 – Normal Operating Procedures
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
 <75% Power ..................................................................... LOP EGT
 Before increasing power ................ Mixture then Prop then Throttle
VFR DESCENT & LANDING
4-9.
(See next main paragraph for IFR Descent)
4-9.1.






PRE DESCENT
Pitot Heat & Defrost ..................................................... As Required
Belts – S/H ............................................................................ Secure
Airport Information .................................................................. Study
ATIS ......................................................................................... Copy
Altimeters (2) .............................................................................. Set
Radios .................................................................................... Preset
4-9.2.
DESCENT
 Altitude ................................................................................... Preset
 Power .......................................................................... CHT > 240°F
 Speed ............................................................................. <170 KIAS
Va = 126 KIAS
 Mixture .......................................................... Enrich during Descent
(<50°F/min or ~ 8°/10 sec)
12-10-2014
Section 4 – Normal Operating Procedures
4-13
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
4-9.3.
PATTERN
4-9.3.1.
45° to Downwind
 Autopilot ...................................................................................... Off
 Lights .................................................................. Aircraft & Runway
 Speed .................................................................... 1Y, 90-110 KIAS
4-9.3.2.
Downwind (FGuMPSS)
 Flaps ............................................................. (Vfe = 122 KIAS) Set
 Gas ....................................................................... Selector & Boost
o Header If X-Wind / slipping and ≤ 10 gal in wing tank
Header If slipping for > 30 seconds while on wing tank
 Mixture ...................................................................................... Rich
 Propeller ........................................................................... High RPM
 Switches ...................................................................................... Set
 Seat Belts – S/H ................................................................... Secure
4-9.3.3.
Base / Final
 Base ............................................................. Best Glide (1Y), ~85 K
 Final ........................................................ AOA Opt App (2Y), ~75 K
o Idle Power Approach ...................................................... Add 5 K
o 20° Flaps .............................................................. 2Y or + 3 knots
o No Flap ............................................................... 2Y or +10 knots
Max Glide
Optimum Approach
Range
(2Y)
L/D Max
(1Y)
4-14
Section 4 – Normal Operating Procedures
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
4-9.3.4.
Traffic Pattern Picture
12-10-2014
Section 4 – Normal Operating Procedures
4-15
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
ROLLOUT, CLEAR OF RUNWAY AND SHUTDOWN
4-9.4.
Rollout
 Flaps ............................................................................................Up
4-9.5.




Flap Switch ................................................................................. Off
Gas – Pump & Selector .................................................... Off & Set
Mixture ................................................................Lean Aggressively
Switches ............................................................................... As Req
4-9.6.











CLEAR OF RUNWAY
SHUTDOWN
P-Lead Check .......................................................... Mags Off & On
Flaps ................................................................................ Full Down
Switches ...................................................................................... Off
Throttle ................................................................... 1000-1200 RPM
Mixture .................................................................................. Cut-off
Fuel Selector ............................................................................... Off
Trim Tab...................................................................................... Set
Postflight Fuel & Hobbs ............................................................. Log
Master & Mags ............................................................................ Off
Cell Phone .................................................................................. On
Flight Plan ............................................................................... Close
4-9.7.
REFUELING
The right fuel cap and the header fuel cap have electrical conductive
chains between the fuel surface and the caps. Always ensure the
electrical potential at the fuel surface is the same as the fuel nozzle
(grounded) before and during refueling. Before unlocking and during
the opening of these fuel caps, hold the grounding cable clip to the cap
4-16
Section 4 – Normal Operating Procedures
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
(Header or right wing as appropriate) and then clip it to the cap’s chain
during refueling. Always have a fire extinguisher nearby.
 Fuel Used .............................................................. Note for Top-Off
 Grounding Cable ......................................... Clipped to Cap Chains
o Hold Grounding Cable Clip onto the right cap or header cap (as
appropriate) while removing caps, then clip to cap chain.
o Header Tank Chain must be touching fuel in tank.
 If Topping off: Cycle between wings but cap low wing when about
10 gal from full
 Fuel Added ........................................................... Log Qty & Hobbs
 Fuel Qty ..................................................................... Reset to Total
4-10.
IFR DESCENT, APPROACH & LANDING
4-10.1.
PRE DESCENT






Pitot Heat & Defrost ..................................................... As Required
Belts – S/H ............................................................................ Secure
Airport Information .................................................................. Study
ATIS ......................................................................................... Copy
Altimeters (2) .............................................................................. Set
Approach plate.......................................................................... Brief
o Waypoint / Chart
o Destination Airport
o Type/Name of approach
o Currency
o Inbound Course
o Comm & Nav freq
o Transition (vectors / IAF)
o Step down fixes, procedure turns, etc
o FAF
o DA / MDA
12-10-2014
Section 4 – Normal Operating Procedures
4-17
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop




o Missed approach fix / procedures
G3X FPL .................................................................... Load External
430 PROC........................................................... Activate Approach
Waypoints & IAP ..................................................................... Same
Radios ......................................................................................... Set
4-10.2.
DESCENT
 Altitude ................................................................................... Preset
 Power .......................................................................... CHT > 240°F
 Mixture .................... Enrich during descent (<50°/min ~8°/10 SEC)
4-10.3.










IAF – IF
Power .................................................................... 50% (110-115 K)
Minimums....................................................... Set (Baro/Minimums)
AP ........................................................................... APPR OR NAV
Comm ......................................................................................... Set
+ Runway Lights Freq
Altimeters .................................................................................... Set
Altitudes ............................................................ Preset & Minimums
Non-GPS
o Nav Aids........................................................................ Freq & ID
o Marker Beacon ....................................................................... On
o CDI Pointers ...................................................................... Ready
Radios .............................................................. Set Tower & Missed
Source, Force, Course ..................... GPS-VLOC, TERM-LPV, A/P
What’s Next & After That?
4-10.4.
IF – FAF
 F-GuMpS
o Flaps .................................................................... 15° (100 KIAS)
o Gas ................................................................... Boost & Selector
4-18
Section 4 – Normal Operating Procedures
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
 Header If X-Wind / slipping and ≤ 10 gal in wing Tk
 Header If slipping for > 30 seconds
o Mixture ........................................................................... Full Rich
o Switches ................................................................................. Set
o Seatbelts & SH ................................................................. Secure
 Altitudes ............................................................ Preset & Minimums
 Source, Force, Course ..................... GPS-VLOC, TERM-LPV, AP
o ILS ........................................................ VLOC - CDI, AP - LOC
o VOR ........................................................ VLOC - CDI, AP-NAV
 What’s Next & After That
4-10.5.








FAF
Time ......................................................................................... Hack
Flaps ........................................................................................... 25°
Glideslope Altitude ................................................................. Check
Power / Speed ........................................................ 30% / 2G ~ 90K
Talk ........................................................................... “FAF Inbound”
Lights .................................................................. Aircraft & Runway
Source, Force, Course ..................... GPS-VLOC, TERM-LPV, A/P
What’s Next & After That?
4-10.6.
500’ AGL
 F-GuMPS ....................................................................... Last Check
4-10.7.






MISSED APPROACH
Autopilot .............................................................. CWS / Disconnect
Power UP, Pitch Up, Clean Up ........................................................
Suspend .................................................................................. Press
CDI ............................................................................................ GPS
Autopilot ..................................................................... Engage / Nav
Talk .....................................................................Missed / Climb out
12-10-2014
Section 4 – Normal Operating Procedures
4-19
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop





Flap Switch ................................................................................. Off
Fuel Selector ............................................................................ Wing
Fuel Pump................................................................................... Off
Source, Force, Course
What’s Next & After That?
4-11.
4-20
Cross Wind Component Graph
Section 4 – Normal Operating Procedures
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
4-12.
AEROBATICS
4-12.1.
Over-The-Top Maneuvers
Start about 150 knots and 3g
4-12.2.
HASELL Check
 Height ...................................................... <8000 MSL, > 4500 AGL
 Airframe ................................................... GW < 1900#, Flaps, Trim
Empty a/c-1350#, Parachutes 15# each, 155# CFI, 220# Student, 6#
trash, 23 gal fuel = 1900#
 Security .......................................... Parachute, Harnesses, Cockpit
 Engine ....................................................Boost Pump, Fuel, Mixture
 Location ........................................................................ Satisfactory
 Lookout .....................................................................Clearing Turns
 G check ..................................................................... (Limits) +6 / -4
 No Rolling Recoveries.
4-12.3.
Entry Parameters
 Altitude ....................................................... >6000 MSL / 4500 AGL
 Airspeed ............................................................................ 150 KIAS
 Over the Top ....................................... (Limits +6 & -4) 3 G then 2Y
4-12.4.
Spin Recovery – Primed
o Power.......................................................................................Off
o Flaps ........................................................................................ Up
o Rudder .................................................. FULL Opposite Rotation
o Stick ...................................... Neutral (full aft for developed spin)
As rotation stops
o Stick .......................................................... Release or Neutralize
o Rudder ......................................................................... Neutralize
o Dive................................................................................. Recover
12-10-2014
Section 4 – Normal Operating Procedures
4-21
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
o AOA .................................................................................... Use It
4-13.
MOORING
The airplane should be moored for immovability, security and
protection. The following procedures should be used for the proper
mooring of the airplane:






Head the airplane into the wind if possible
Retract the flaps
Immobilize the ailerons and elevator
Chalk the wheels
Secure the rudder
Secure tie-down ropes to the wing tie-down
rings and to the tail tie-down ring at
approximately 45° angles to the ground.
Tie-down rings are usually kept in the small
storage area below the baggage
compartment. When using rope of nonsynthetic material, leave sufficient slack to avoid damage to the
airplane should the ropes shrink while drying out.
o Use bowline knots, square knots or locked slip knots. Do not
use plain slip knots
 Install the pitot tube cover
Close and lock the doors
4-22
Section 4 – Normal Operating Procedures
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
Section 5 - Performance
Table of Contents
5-1. AIRCRAFT SPECIFICATIONS .................................................. 5-3
5-1.1. With Wing Tip Extensions .................................................... 5-3
5-1.2. Without Wing Tip Extensions .. Error! Bookmark not defined.
5-2. PERFORMANCE DATA ............................................................. 5-4
5-2.1. With Extended Wing Tips ........ Error! Bookmark not defined.
5-2.2. Without Extended Wing Tips ... Error! Bookmark not defined.
5-3. POWER CHARTS ...................................................................... 5-5
5-4. CLIMB PERFORMANCE............................................................ 5-7
5-5. FUEL, TIME, DISTANCE TO CLIMB ......................................... 5-7
5-6. SPEED POWER PERFORMANCE CRUISE ............................. 5-7
5-7. SPEED POWER ECONOMY CRUISE ...................................... 5-7
5-8. FUEL, TIME, DISTANCE TO DESCEND ................................... 5-7
5-9. GLIDE TIME AND DISTANCE ................................................... 5-7
5-10.
LANDING DISTANCE OVER 50’ OBSTICAL ........................ 5-7
5-11.
LANDING GROUND ROLL DISTANCE ................................ 5-7
12-10-2014
Section 5 – Performance
5-1
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
INTENTIONALLY LEFT BLANK
5-2
Section 5 –Performance
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
5-1.
5-1.1.
AIRCRAFT SPECIFICATIONS
With Wing Tip Extensions
Wing Span .................................................................................... 27.3 ft
Wing Area ................................................................................... 91.5 ft2
Wing Aspect Ratio ........................................................................... 7.64
Wing Loading (gross) ............................................................ 24.04 lb/ft2
Length Overall............................................................................... 20.7 ft
Height Overall (without propeller) ................................................. 6.8 ft?
Wheel Base..................................................................................... 5.1 ft
Wheel Span (Track) ........................................................................ 6.3 ft
Cabin Width .................................................................................... 42 in
Baggage Space ............................................................................. 12 ft3
Baggage Capacity (max) ............................................................ 100 lbs
Gross Weight non-aerobatics. .................................................. 2200 lbs
Gross Weight for Aerobatics ..................................................... 1900 lbs
Empty Weight.......................................................................... ~1350 lbs
Useful Load ............................................................................... ~825 lbs
Fuel Capacity
Wing Tank .............................................................. 43 gal (258 lbs)
Header Tank ............................................................. 7 gal ( 42 lbs)
Oil Capacity....................................................................................... 8 qt
Seats ........................................................................................... 2 Souls
Tire size
Main Gear ...................................................... 5.00 x 5, 6 ply rating
Nose Gear ................................................ 11 x 4.00-5, 8 ply rating
12-10-2014
Section 5 – Performance
5-3
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
5-2.
PERFORMANCE DATA
Top Speed (Sea level, TAS) .................................................... 1??knots
Cruise Speed (75% power @ 8000’, TAS) ............................. 1?? knots
Rate of climb (from sea level)
Solo (approx 1700 lbs) ......................................................... ?00 ft/min
Gross ..................................................................................1100 ft/min
Stall speed with flaps (Vs)......................................................... 58 knots
Stall speed clean ....................................................................... 67 knots
Best Glide.................................................................................. 86 knots
Best Rate of Climb (Vy) .......................................................... 108 knots
Best Angle of Climb (Vx) .......................................................... 85 knots
Approach Speed ....................................................................... 75 knots
Never Exceed Speed (Vne) .................................................... 226 knots
Maneuvering Speed (Va) ........................................................ 126 knots
Maximum Structural Cruising Speed (Vno) ............................ 174 knots
Maximum Flap Extension Speed (Vfe) ................................... 122 knots
Structural Load Limits (2200 lb gross wgt)
Positive .................................................................................... 3.8 g
Negative ................................................................................... 1.0 g
Structural Load Limits (1900 lb aerobatic wgt)
Positive .................................................................................... 6.0 g
Negative ................................................................................... 4.0 g
Service Ceiling (approx)............................................................ 19,000ft
Roll Rate – Extended Wing Tips .............................................. 90 ° /sec
5-4
Section 5 –Performance
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
5-3.
POWER CHARTS
First chart shows representative effect of fuel/air ratio on engine
operation
Second chart gives available horse power for changes in mp, rpm and
altitude.
Third chart gives several extractions from the second chart plus
percent power for different conditions
12-10-2014
Section 5 – Performance
5-5
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
5-6
Section 5 –Performance
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT, N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
5-4.
TAKEOFF PERFORMANCE
There is an Excel Takeoff Distance Spreadsheet at
http://11hc.44rf.com/manuals/manuals.htm that can be used to
approximate takeoff distance. It is based on rules-of-thumb on how
takeoff distance changes with gross weight, Density Altitude,
Headwind/tailwind and runway slope.
5-5.
5-6.
5-7.
5-8.
CLIMB PERFORMANCE
FUEL, TIME, DISTANCE TO CLIMB
SPEED POWER PERFORMANCE CRUISE
SPEED POWER ECONOMY CRUISE
AOA Maximum Range and Glide ................................. Blinking 1-Yellow
5-9.
5-10.
5-11.
5-12.
FUEL, TIME, DISTANCE TO DESCEND
GLIDE TIME AND DISTANCE
LANDING DISTANCE OVER 50’ OBSTICAL
LANDING GROUND ROLL DISTANCE
12-10-2014
Section 5 – Performance
5-7
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
Section 6 - Weight and Balance
Table of Contents
6-1. CG COMPUTATIONS ................................................................ 6-3
6-1.1. Maximum Gross Weight ....................................................... 6-3
6-1.2. Mean Aerodynamic Chord (MAC) ........................................ 6-3
6-1.3. Wing Leading Edge at MAC ................................................. 6-3
6-1.4. Flight CG Limits .................................................................... 6-3
6-1.5. % MAC Computations .......................................................... 6-4
6-1.6. Various Moment Arms (Glasair Super II-S FT) .................... 6-4
6-2. EMPTY WEIGHT CG CALCULATION ....................................... 6-4
6-2.1. CG Computations ................................................................. 6-6
6-3. EXTREME CG CALCULATIONS ............................................... 6-8
6-3.1. Forward CG Limit Check (Extended Wingtips) .................... 6-8
6-3.2. Aft CG Limit Check (Extended Wingtips) ............................. 6-9
12-10-2014
Section 6 – Weight and Balance
6-1
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
INTENTIONALLY LEFT BLANK
6-2
Section 6 – Weight and Balance
12-10-2014
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
6-1.
CG COMPUTATIONS
A N11HC specific Weight and Balance Excel Spreadsheet is available
at: http://aswebs.com/44rf/11hc/manuals/w&b_spreadsheet.xls You
can easily change the blue boxes’ weights and determine if the aircraft
is within weight and balance. Make sure you use beginning and ending
fuel loads. Another option is using the W&B section of the G3X.
Definitions of weight and balance terms are located in section 1 of this
POH.
WARNING
To operate the Glasair safely, it must be flown within the
specified CG limits. These limits must be strictly
adhered to. Flight in either a nose-heavy or tail-heavy
airplane is unsafe and can result in loss of control.
6-1.1.
Maximum Gross Weight
With Wing Tip Extensions ................................................. 2200 lb
Aerobatic ........................................................................... 1900 lb
6-1.2.
Mean Aerodynamic Chord (MAC)
With Wing Tip Extensions..................................................... 43.0”
6-1.3.
Wing Leading Edge at MAC
With Wing Tip Extensions ................................................... 84.11”
6-1.4.
Flight CG Limits
Forward Limit ................................................89.91” / 13.5% MAC
Aft Limit .........................................................97.65” / 31.5% MAC
12-10-2014
Section 6 – Weight and Balance
6-3
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
6-1.5.
% MAC Computations
Extended Wingtips (27.3 ft wing span)
CG Station – 84.11 ÷ 43% = %MAC
6-1.6.
Various Moment Arms (Glasair Super II-S FT)
Cowling Attach Flange Joggle .............................. Station 58.000
Nose Wheel Axle .................................................. Station 40.375
Main Gear Axles ................................................. Station 102.060
Oil (1.9 lb / qt) ....................................................... Station 44.000
Fuel – Wing Tank (6.0 lb / gal .............................. Station 89.850
Fuel – Header Tank (6.0 lb/gal ............................. Station 68.000
Firewall ................................................................. Station 60.000
Baggage ............................................................. Station 136.000
Passengers ......................................................... Station 115.500
Instrument Panel .................................................. Station 89.000
Ballast (~22 lbs) .................................................. Station 196.000
The REFERENCE DATUM is located 58.0” forward of the cowling
attach flange joggle (aft edge of the engine cowling). Stations are
measured in inches from the datum.
6-2.
EMPTY WEIGHT CG CALCULATION
With the wings and waterline 100 level, a plumb bob is used to mark the
location of the cowling attach flange joggle (the aft edge of the cowling)
onto the floor.
NOTE
For procedures on how to mark waterline 100, see “Marking
the Fuselage Reference Lines” in Subsection D of the
Fuselage Assembly section of the Instruction Manuals.
6-4
Section 6 – Weight and Balance
12-10-2014
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
WARNING
Any modifications to the aircraft that add, subtract, or
shift weight change the location of the empty weight CG.
If any such modifications are made, therefore, the empty
weight CG must be determined again to permit accurate
flight CG calculations.
12-10-2014
Section 6 – Weight and Balance
6-5
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
6-2.1.
CG Computations
The aircraft was weighed with full fuel tanks, so the fuel had to be
removed via calculations to arrive at an empty weight and CG for the
aircraft.
6-6
Section 6 – Weight and Balance
12-10-2014
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
12-10-2014
Section 6 – Weight and Balance
6-7
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
6-3.
EXTREME CG CALCULATIONS
CG changes for most forward and most aft CG possible during flight
have been calculated for N11HC. Below are two extremes for fore and
aft CGs.
6-3.1.
6-8
Forward CG Limit Check (Extended Wingtips)
Section 6 – Weight and Balance
12-10-2014
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
6-3.2.
Aft CG Limit Check (Extended Wingtips)
12-10-2014
Section 6 – Weight and Balance
6-9
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
INTENTIONALLY LEFT BLANK
6-10
Section 6 – Weight and Balance
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
Section 7 - Systems Description
Table of Contents
7-1. CHANGES FROM ORIGINAL PLANS ....................................7-7
7-1.1. Parking Brake ......................................................................7-7
7-1.2. Door Unlocked Warning System .........................................7-7
7-1.3. Flap Position Indicator .........................................................7-7
7-1.4. Oil Cooler .............................................................................7-7
7-1.5. Cowl Pin Retainers ..............................................................7-7
7-1.6. Header Tank Vent ...............................................................7-8
7-1.7. External Power Receptacle .................................................7-8
7-2. POWERPLANT .......................................................................7-8
7-2.1. Engine Access .....................................................................7-9
7-2.2. Instrumentation ....................................................................7-9
7-2.3. Accessory Data ...................................................................7-9
7-2.4. Oil System .........................................................................7-10
7-2.5. Fuel Injection System ........................................................7-11
7-2.6. Magneto System................................................................7-12
7-2.7. Additional Information ........................................................7-12
7-2.8. Power Plant Displays ........................................................7-13
7-2.9. Cylinders ............................................................................7-13
7-3. PROPELLER .........................................................................7-13
7-4. STARTER SYSTEM ..............................................................7-15
7-5. FUEL SYSTEM ......................................................................7-15
7-5.1. Fuel Grade .........................................................................7-15
7-5.2. Fuel System Sequence .....................................................7-15
7-5.3. Two fuel tanks. ..................................................................7-15
12-10-2014
Section 7 – Systems Description
7-1
Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
7-5.4. Fuel Pumps ....................................................................... 7-17
7-5.4.1. Engine Driven Fuel Pump ...................................... 7-17
7-5.4.2. Electrical Fuel Pump .............................................. 7-17
7-5.5. Fuel Selector ..................................................................... 7-17
7-6. LANDING GEAR ................................................................... 7-18
7-7. BRAKES ............................................................................... 7-18
7-8. COCKPIT .............................................................................. 7-19
7-8.1. Seating Area ..................................................................... 7-19
7-8.2. Baggage ........................................................................... 7-19
7-8.3. Doors ................................................................................ 7-19
7-9. AIRFOILS.............................................................................. 7-20
7-9.1. Wing .................................................................................. 7-20
7-9.1.1. Airfoil ....................................................................... 7-20
7-9.1.2. Stall Strip ................................................................ 7-21
7-9.2. Flaps ................................................................................. 7-21
7-9.2.1. Type and Purpose .................................................. 7-21
7-9.2.2. Flap Operation ........................................................ 7-21
7-10. HEAT AND VENT SYSTEMS ............................................... 7-22
7-10.1. Heat/Defrost System ........................................................ 7-22
7-10.2. Fresh Air System .............................................................. 7-23
7-10.3. CO Detector ...................................................................... 7-24
7-10.3.1. Pocket CO Operation: ............................................ 7-24
7-11. ELECTRICAL SYSTEM ........................................................ 7-25
7-11.1. Battery/Relay Electrical System ....................................... 7-25
7-11.2. Wiring Picture – Under Right Seat ................................... 7-27
7-11.3. Other Electronic Components .......................................... 7-27
7-11.3.1. Rheostat Control Modules ...................................... 7-27
7-2
Section 7 – Systems Description
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
7-11.3.2. Positive Buss Bar ....................................................7-28
7-11.4. Alternators .........................................................................7-28
7-11.5. MASTER Switch ................................................................7-29
7-11.6. Circuit Breakers .................................................................7-30
7-11.7. Inside Lighting ...................................................................7-30
7-11.7.1. Rheostat Controlled Lights. .....................................7-30
7-11.7.2. Dome Light ..............................................................7-30
7-11.8. Outside Lighting.................................................................7-31
7-11.8.1. Navigation lights ......................................................7-31
7-11.8.2. Strobe Lights ...........................................................7-31
7-11.8.3. Landing Light ...........................................................7-31
7-11.9. Intelligent Power Stabilizer (IPS) .......................................7-32
7-12. ELECTRICAL LOADS ...........................................................7-33
7-13. PITOT-STATIC SYSTEM ......................................................7-34
7-13.1. Diagram .............................................................................7-34
7-13.2. Pitot Tube and Heat ..........................................................7-34
7-14. ANTENNAS ...........................................................................7-35
7-15. MAIN ROCKER SWITCHES .................................................7-35
7-16. INSTRUMENTATION ............................................................7-36
7-16.1. Garmin Sensor Unit (GSU 73)...........................................7-36
7-16.2. G3X PFD/MFD (GDU 370/375) .........................................7-37
7-16.2.1. Configuration mode .................................................7-37
7-16.2.2. Left Screen (PFD1) .................................................7-37
7-16.2.3. Center Screen (MFD) ..............................................7-38
7-16.2.4. Right Screen (PFD2) ...............................................7-38
7-16.2.5. Redundancy and Integration ...................................7-38
7-16.2.6. Part Numbers etc. ...................................................7-38
12-10-2014
Section 7 – Systems Description
7-3
Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
7-16.2.7. G3X Pilot’s Guide ................................................... 7-39
7-16.2.8. Data Bar Fields ....................................................... 7-39
7-16.2.9. G3X Software/Manuals Updates ............................ 7-41
7-16.2.10. Flight Data Files...................................................... 7-43
7-16.2.11. G3X / G430W Subscriptions .................................. 7-43
7-16.2.12. Airspeed V-Speeds and Trend Line ....................... 7-44
7-16.2.13. Gee Wiz .................................................................. 7-45
7-16.2.14. Solid-State ADAHRS (GSU 73) ............................. 7-46
7-16.2.15. Magnetometer (GMU 44) ....................................... 7-46
7-16.3. Garmin GNS 430W ........................................................... 7-47
7-16.3.1. GNS430W is the #2 radio....................................... 7-47
7-16.3.2. Control Stick Operations ........................................ 7-47
7-16.3.3. Data Bar Fields ....................................................... 7-47
7-16.3.4. Integrate Avionics ................................................... 7-48
7-16.3.5. Data Cards ............................................................. 7-48
7-16.3.6. Configuration Mode Operations ............................. 7-49
7-16.4. Autopilot ............................................................................ 7-49
7-16.4.1. TruTrak GX Autopilot .............................................. 7-50
7-16.5. PMA8000B Audio Panel ................................................... 7-51
7-16.5.1. Comm 1 vs. Comm 2: ............................................. 7-51
7-16.5.2. Control Stick Swap Mode: ...................................... 7-51
7-16.5.3. Recorder System .................................................... 7-51
7-16.5.4. Split Mode ............................................................... 7-51
7-16.5.5. More Information .................................................... 7-51
7-16.5.6. Data Plate ............................................................... 7-51
7-16.6. Garmin SL40 Communication Radio ................................ 7-52
7-16.6.1. SL40 is the #1 radio ............................................... 7-52
7-4
Section 7 – Systems Description
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
7-16.6.2. EC – Emergency Channel .......................................7-52
7-16.6.3. MON - Monitor 2 frequencies ..................................7-53
7-16.6.4. RCL – Recall Memory .............................................7-53
7-16.6.5. MEM – Button..........................................................7-54
7-16.6.6. SL40 S/N 258 10 848 ..............................................7-54
7-16.6.7. Garmin GTX 327 Transponder................................7-55
7-16.6.8. Transponder Controls .............................................7-55
7-16.6.9. S/N 837 36 966 .......................................................7-55
7-16.6.10. Transponder Features .............................................7-55
7-16.7. Standby Instruments .........................................................7-56
7-16.7.1. Airspeed ..................................................................7-56
7-16.7.2. Attitude Indicator .....................................................7-56
7-16.7.3. Altimeter ..................................................................7-59
7-16.8. Compass ...........................................................................7-59
7-16.9. GT-50.................................................................................7-59
7-16.10. AOA Indicator...............................................................7-60
7-16.10.1. Checklists ................................................................7-61
7-16.10.2. Preflight ...................................................................7-61
7-16.10.3. Operating Temperatures .........................................7-61
7-16.10.4. AOA Labels .............................................................7-61
7-16.10.5. Indications ...............................................................7-62
7-16.10.6. AOA Buttons ............................................................7-62
7-16.10.7. AOA Test .................................................................7-62
7-16.10.8. AOA Enunciator.......................................................7-62
7-16.10.9. Flap Micro Switch ....................................................7-62
7-17. WING TIP EXTENSIONS ......................................................7-63
7-18. ELT ........................................................................................7-63
12-10-2014
Section 7 – Systems Description
7-5
Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
7-18.1. Operation .......................................................................... 7-63
7-19. CONTROL STICK GRIP ....................................................... 7-64
7-6
Section 7 – Systems Description
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
7-1.
CHANGES FROM ORIGINAL PLANS
There were eight changes made to the original Glasair Kit # 2329.
7-1.1.
Parking Brake
A parking brake was not included in the kit plan. N11HC now
incorporates a parking brake. More information is available in the
“Brakes” paragraph of this section.
7-1.2.
Door Unlocked Warning System
The original plans had no warning if the door latching mechanism was
not in the locked position. One has been added to the G3X display on
N11HC. More information is available in the “Cockpit/Doors”
paragraph of this section.
7-1.3.
Flap Position Indicator
The original plans had no provision for a flap position indicator. One
has been added to the G3X display on N11HC. More information is
available in the “Flaps” paragraph of this section.
7-1.4.
Oil Cooler
The original oil cooler was replaced with a more efficient Glasair III oil
cooler.
7-1.5.
Cowl Pin Retainers
The builder modified the original plans for retaining the cowl’s piano
hinge pins which allows spinning the pins with an electric drill for both
insertion and removal. More information is available in the
“Powerplant/Engine Access” paragraph of this section.
12-10-2014
Section 7 – Systems Description
7-7
Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
7-1.6.
Header Tank Vent
The header vents were removed because they siphoned fuel before
the tank was full and drained it overboard. A venting fuel cap was
made and allows the header tank to be topped off.
7-1.7.
External Power Receptacle
A single pin Piper type plug is mounted under the fuselage just aft of
the right wing flap. More information is available in the “Electrical
System” paragraph of this section.
7-2.
POWERPLANT
Make: ..........................................................................Aero Sport Power
Model: .................................................................................. IO-360-B1E
S/N: ........................................................................................... 0571-SP
Date: ................................................................................... Jan 12, 2004
N11HC’s engine was assembled by Aero Sport Power
(www.AeroSportPower.com) with components from Engine
Components Inc. (http://www.ECi.aero). ECI produces the same parts
for the Lycoming factory for Lycoming certified engines. Even though
the parts are the same as those used in Lycoming certified engines,
this engine is not certified. This is because Lycoming did not assemble
7-8
Section 7 – Systems Description
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
the parts (Aero Sport Power did) making this is a “non-certified”
engine. The Lycoming website is http://www.lycoming.textron.com.
The IO-360-B1E is:
 Similar to –B1B with rear mounted fuel injection and -1200
series impulse coupling Magnetos.
 The B1B is the same as –B1A except for Bendix fuel injection
system.
 The B1A is the same as the O-360-A1D except for the
Simmonds 530 fuel injection system.
 The A1D is similar to –B1B with rear mounted fuel injection and
-1200 series impulse coupling Magnetos.
 (IAW Lycoming Operators Manual….)
7-2.1.
Engine Access
The top cowl is held in place by Camloc fasteners toward the back,
screws in front and piano hinges along the sides. The piano hinge
wires are accessed by first removing the nipples at the front to expose
the wires and then using a drill to spin the wire during both removal
and insertion.
7-2.2.
Instrumentation
See the G3X paragraph in this section concerning the Garmin Sensor
Unit (GSU 73)
7-2.3.
Accessory Data
Part
Fuel Injector
Fuel Pump
Distributor
Left Slick Magneto
Right Slick Magneto
Starter (Kelly Aerospace Power)
12-10-2014
P/N
2576536-2--H
AF-15473
2524232-2
4371
4370
MZ-6222
Section 7 – Systems Description
S/N
72FE3705
06ZL17
0283545
03021764
3121176
D014216
7-9
Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
Alternator (main) B & C Specialty
Products
Alternator (stby) B & C Specialty Products
C/Case
C/Shaft
L60
0792213
SD20
0897617K
AEL365460-0 23-11
AEL36002-1 73472-04
Engine Number ......................................................................... 0571-SP
FAA Type Certificate ....................................................................... 1E10
Rated Horsepower ............................................................................ 180
Rated Speed, RPM ......................................................................... 2700
Oil Capacity ...................................................................................... 8 qt.
Bore, inches ................................................................................... 5.125
Stroke, Inches ................................................................................ 4.375
Displacement, Cubic Inches .......................................................... 361.0
Compression Ratio ....................................................................... 8.5 : 1
Firing Order ..................................................................................1-3-2-4
Spark occurs, Degrees BTC .............................................................. 25°
Valve Rocker Clearance (hydraulic tappets collapsed) .................... 0.28-0.080
Propeller Drive Ratio ........................................................................ 1 : 1
Propeller Drive Rotation (cockpit view) ................................... Clockwise
Weight ..........................................................................................296 lbs
Height / Width / Length (in inches) ............................. 20.70/33.37/32.09
7-2.4.
Oil System
The full pressure wet sump lubrication system is actuated by an
impeller type pump contained within the accessory housing. The
engine oil system uses a mechanical oil pump with a wet sump on the
bottom of the engine.
The oil dipstick does not have engraved numbers indicated oil quantity
in quarts. Instead, there are seven single rings engraved in the
dipstick plus a double rings engraved indicating the six quart level. It is
recommended keeping the oil above the double ring on the dipstick.
7-10
Section 7 – Systems Description
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
7-2.5.
Fuel Injection System
Fuel Injection Servo was replaced about September 2014
The alternate air source of the induction system is a door that functions
automatically if the primary source is obstructed. The alternate air
source is from inside the heated area of the cowling and is unfiltered
air.
IAW Lycoming Operators Manual page 1-4 (9/51) ( Sec 1. The
Bendix fuel injections): “The Bendix RSA
type fuel injection system is based on the
principle of measuring air flow and using the
air flow signal in a stem type regulator to
convert the air force into a fuel force. This fuel force (fuel pressure
differential) when applied across the fuel metering section (jetting
system) makes fuel flow proportional to air flow.”
The IO-360-B1E is the same engine used in the Piper Arrow. Below is
information from Aerotech about its induction system: “The induction
system of the non-turbocharged aircraft incorporates a Bendix RSA5AD1 type fuel injector. The injector is based on the principal of the
differential pressure, which balances air pressure against fuel
pressure. The regulated fuel pressure established by the servo valve
when applied across a fuel control (jetting system) makes the fuel flow
proportional to airflow. Fuel pressure regulation by the servo valve
causes a minimal drop in fuel pressure throughout the metering
system. Metering pressure is maintained above most vapor forming
conditions while fuel inlet pressure is low enough to allow use of a
diaphragm pump. The servo system feature also checks vapor lock
and associated starting problems.
The servo regulation meters fuel flow proportionally with airflow and
maintains the mixture as manually set for all engine speeds. The fuel
flow divider receives metered fuel and distributes fuel to each cylinder
fuel nozzle.
12-10-2014
Section 7 – Systems Description
7-11
Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
The fuel flow portion of the manifold pressure / fuel flow gauge is
connected to the flow divider and monitors fuel pressure. This
instrument converts fuel pressure to an indication of fuel flow in gallons
per hour and percentage of rated horsepower.”
Precision is the company that now makes the Bendix system (and has
re-engineered it to some extent). It is a continuous flow system that
pours a continuous stream of fuel into the inlet port (not directly into the
cylinder). The injector body (the thing that looks a bit like a carburetor)
attempts to measure the mass flow of air entering the engine, and
schedules the appropriate quantity of fuel to be sent to the injectors.
Fuel quantity is regulated by the injector body by changing fuel
pressure. The spider is the really only a way of splitting off 4 smaller
pipes from the larger feed pipe from the injector body (it does also
incorporate a low pressure shut off valve).
Link to Troubleshooting Techniques for the Precision Airmotive RSA
Fuel Metering System. Link to injector service publications.
7-2.6.
Magneto
System
There are two Slick
magnetos. The system
does not incorporate
electronic ignition
because the prop was
not certified for
electronic ignition and it
may cause damaging
harmonics.
7-2.7.
Additional Information
Basic engine information is in section 1.
7-12
Section 7 – Systems Description
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
Lycoming books are in the “Manuals” section on the
http://11HC.44RF.com website
7-2.8.
Power Plant Displays
Basic/ required Power Plant Displays are always on the PFD.
Additional power plant information is displayed on the Engine Default
page of the MFD or the PFD if the MFD is not operating. Section 2 of
this POH shows how the G3X is programmed to display the limits
(Gauge ranges, color codes along with limit numbers).
7-2.9.
Cylinders
IAW Lycoming Operators Manual page 1-1 (6/51) ( Sec 1.
Description): Reference to the left and right side is made with the
observer facing the rear of the engine (as viewed from the pilot’s seat).
Cylinder 1 = front right
Cylinder 2 = front left
Cylinder 3 = rear right
Cylinder 4 = rear left
Mags - left S4LN-1227, right S4LN-1209
7-3.
PROPELLER
Manufacturer (http://www.hartzellprop.com) .............................. Hartzell
Propeller Owners Manual: 115N, 61-00-15, Revision 16, October 2009.
Model (Hub/Blade) .................................. Hub - HC-C2YR-1BF/F7068-2
Hub breakdown
 No prefix = Indicates dowel location with respect to centerline
through blade sockets when viewing hub from flange mounting
face 90 & 270 deg. Clockwise
 HC = Hartzell Controllable
 C = Standard Hub
 2 = Number of blades
12-10-2014
Section 7 – Systems Description
7-13
Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
 Y = Y Shank, Aluminum Blade, Integral Pitch Change Arm
 R = 475” Bolt Circle, N/A Dowels, 6 (1/2”) Bolts
 1 = Constant Speed, non-feathering, no counterweights, governor
oil pressure increases pitch, blade centrifugal force to low pitch
 B = 2 Blade: Different cylinder, P.C. Rod, Spring, low pitch stop
 F = Large pitch change knob, fork
Blade Breakdown





F = a large pitch change knob
Blank = no counterweights
70 = Basic diameter in inches
68 = Basic blade model
-2 = Subtract 2” from the basic 70 giving a 68” diameter prop
Diameter ............................................................................................. 68”
Low Pitch ........................................................................................ 12.2°
High Pitch ........................................................................................ 39.4°
Propeller Serial Number....................................................... CH-32998B
Blade Serial Numbers ............................................. J13227 and J13230
HUB .......................................................................................... D-6529-1
Factory Number ....................................................................... A41559B
On 4/9/2010 this prop was sent to a Hartzell repair shop due to nonuse for several years. It came back as a “Repair Order” (Not
Overhaul) and the following notes:
Repair Order (not overhaul) on 4/19/2010
Serviced IAW Hartzell Manuals
 113B Revision 37
 133C Revision 26
 202A Revision 35
Complied with Hartzell Service letter:
 189 Revision 2
 229 Revision 2
 293 Revision 1
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Section 7 – Systems Description
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
7-4.
STARTER SYSTEM
The starter is a 12 volt system manufactured by Kelly Aerospace. Part
number M2-6228 0014216. It should be serviced every 50 hours.
7-5.
FUEL SYSTEM
7-5.1.
Fuel Grade
IAW Lycoming Operators Manual page 3-10 (27/51)
(Sec 3-8. Fuel
& Oil): Aviation grade 100LL fuels in which the lead content is limited
to 2 c.c. per gal are approved for continuous use. Also the minimum
grade aviation fuel is 91/96 or 100/130.
7-5.2.
Fuel System Sequence
Fuel flows into the fuel selector from either the wing tank or the header
tank (not both at once). From the fuel selector, it goes through the
electric fuel pump (while operating or not), then the fuel flow meter and
on to the fuel filter. From the fuel filter it goes through the engine
driven fuel pump then the fuel control and onto the spider and into the
cylinder fuel injectors.
7-5.3.
Two fuel tanks.
The WING tank is a 43 gallon tank in the wing leading edge D-section.
A very small amount of fuel is unusable.
The HEADER tank is a 7 gallon tank aft of the firewall (in the cockpit)
and is vented by a venting fuel cap.
The wing-tip extensions cannot contain fuel in N11HC.
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Section 7 – Systems Description
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
NOTE
Use only grade 100 (green) or 100LL (blue) fuel with this engine.
The wing fuel tank incorporates a system of baffles and check valves
designed to help prevent fuel starvation resulting from slips or other
uncoordinated maneuvers.
N11HC uses capacitance probe fuel senders in the wing tank. This
tank is vented through the lower wing panel at each tip.
Fuel vent float valves are installed at each wing tip to prevent spilling
fuel when the airplane is parked on uneven ground with full tanks.
Each float valve incorporates a pressure relief valve, which prevents
damage to the fuel tank from thermal expansion of the fuel, and a
check valve, which opens to allow the engine to pull fuel from the tank
in the unlikely event that both float valves stick in the closed position.
A mechanical fuel pump on the engine and an electric auxiliary pump
under the pilot’s seat supply fuel to the fuel injector. A three position
fuel valve with positions for fuel off, wing tank fuel on and header tank
fuel on is used for fuel management. A fuel sump with a fuel drain is
mounted at the bottom of each tank.
A fuel screen is fitted to the fuel pickup in each sump and a cartridge
type fuel filter is mounted at the low point of the fuel line forward of the
firewall.
There is an inverted fuel system for the Header tank on N11HC.
7-16
Section 7 – Systems Description
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
7-5.4.
7-5.4.1.
Fuel Pumps
Engine Driven Fuel Pump
There is a
mechanically
driven main
engine fuel
pump which
operates when
the engine is
turning over. It
was replaced
about September 2014.
7-5.4.2.
Electrical Fuel Pump
There is an electrically driven auxiliary fuel pump located under the
pilot’s seat and activated by the “FUEL PUMP” rocker switch. Monitor
the fuel pressure when turning the fuel pump off,
The aux pump switch should be on:
 For all traffic patterns takeoffs and landings
 When switching fuel tanks
 For engine emergencies or problems
7-5.5.
Fuel Selector
The fuel selector is made by Andair.
The selector has a large red lever with 'Fuel'
engraved on it and a clearly labeled fascia
plate to indicate which tank has been selected.
The lever incorporates a safety detent
mechanism which allows for a good solid detent at each tank position
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Section 7 – Systems Description
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
and also the button on top of the lever must be raised to switch the fuel
off. When switching off check to make sure the locking button is
locked.
7-6.
LANDING GEAR
A fixed tricycle landing gear is used on the Glasair Super II-S FT. The
main gear struts are of the spring type, fabricated from unidirectional
and bidirectional fiberglass laminates. The nose gear is a simple,
rubber shock mounted, heat-treated 4130 steel tube strut.
Grove Brakes and wheels: 5.00 x 5 wheels and brakes are used on
the main gear. A Cleveland 5.00 x 5 wheel, fitted with a Lamb 11 x
4.00-5, 8 ply tire, is used on the nose gear.
The nose gear is free-castering, and steering is accomplished by
differential braking. A friction type shimmy damper is incorporated on
the nose gear.
Toe-in on the main gear is set at 1° per gear or 2° total toe-in.
7-7.
BRAKES
Brake pedals are
installed for both
occupants. The master
cylinder is located at the
pilot’s toe brakes. The
brake fluid reservoir is
mounted to the engine
mount. Toe pressure on
the top of the rudder
pedals actuates the
Grove brakes. A
parking brake is applied
by applying pressure to
the toe brakes while
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Section 7 – Systems Description
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
pulling the parking brake pull knob on the center console. Therefore, it
is part of the toe brake system and not independent.
7-8.
COCKPIT
7-8.1.
Seating Area
N11HC provides comfortable side-by-side seating for two people over
6’ 6” and weighing up to 250 lbs. each. Cabin width is approximately
42 inches.
7-8.2.
Baggage
Baggage is stored directly behind the seat back and should be
securely anchored down when in flight. A small storage area is located
below the baggage area for tools, chocks, spare parts, oil, rags etc.
WARNING
Do not place any small loose articles in the baggage
compartment. Stow all baggage in containers such as packs,
suitcases, or bags. A small article, if misplaced, could bind
up a control linkage causing loss of control of the aircraft.
7-8.3.
Doors
The Glasair Super II-S FT utilizes gull wing canopies with fore and aft
bullet type latches. The latch system uses two-way handles, which
can be operated from both inside and outside of the cockpit. This
provides access from the outside in the event of an emergency.
Canopies can be left open for ventilation during ground taxi. The front
bullet of each door activates a switch in its receptacle when locked. If
the switches are not depressed by the locking mechanism, the G3X
warning area will state “Pilot Door” or “Co-Pilot Door”.
WARNING
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Section 7 – Systems Description
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
Do not open the canopies in flight. They will depart the aircraft.
7-9.
AIRFOILS
Flight Controls
The controls are of a conventional 3-axis design using dual stick
controls for pitch and roll, and dual rudder pedals for yaw. Controls are
light and responsive in all modes of flight. The rudder movement is
small creating sensitive yaw movements.
All flight control interconnections are push-pull tube linkages except for
rudder control. Rudder cables are used between the rudder pedals
and the rudder bellcrank. A push-pull tube connection is used from the
rudder bellcrank to the rudder.
The elevator trim system functions by introducing a spring tension on
the elevator control horn in the direction desired by the pilot. The
system also prevents an oversensitive elevator control and provides
desirable control pressure feel. The elevator trim system is actuated
by an elevator trim control wheel located in the center console. The
trim wheel is geared to a cable drum around which the elevator trim
actuating cable is wound. The ends of the elevator trim cable, with
tension springs installed in line, are routed between the cable drum
and the ends of the elevator actuator arm.
Rudder trim is accomplished by a fixed external trim tab and aileron
trim by either an external trim tab or by rigging the flaps differently.
Aileron and rudder trim are adjustable on the ground only. Adjust the
external trim tabs for optimum cruise conditions. See the instruction
manuals and the flight test section for further details.
7-9.1.
7-9.1.1.
Wing
Airfoil
The Airfoil is GAW-2.
7-20
Section 7 – Systems Description
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
7-9.1.2.
Stall Strip
There are small stall strips toward the inboard side of the leading edge
that cause the air to separate there before it separates outboard and
gives better aileron control at high AOA.
7-9.2.
7-9.2.1.
Flaps
Type and Purpose
N11HC has electrically actuated slotted
flaps.. These flaps reduce the stall
speed by 9-10 knots and shorten the
takeoff and landing distances and lower
approach speeds. They improve
visibility over the nose on landing
approach and have a maximum speed
of 122 knots.
Flap motor information: Part # 73463, Motor # PE2433Q RPM 6000
7-9.2.2.
Flap Operation
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Section 7 – Systems Description
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
The flaps are controlled by the 3position toggle switch next to the
china hat switch on the stick grip.
The center position is the off
position and the switch should be
kept in this position when the
flaps are not in transit. The flaps
only go down as long as the
switch is held down (the switch is
spring-loaded from the down
position to the center position). Moving the switch to the up position
moves the flaps up. A clutch mechanism allows the flap motor to
continue running even when the flaps are fully up or down. Note that
the switch is not spring-loaded from the up position to the off position
which requires the pilot to move the switch to the off position after the
flaps retract. The flap position is indicated on the G3X as: zero
degrees, 15°, 25° and 40°. The flap switch position is not indicated on
the G3X.
7-10.
HEAT AND VENT SYSTEMS
7-10.1.
Heat/Defrost System
When desired, aircrew can direct warm air to provide windshield
defrosting and/or heating for the occupants. A pull/push knob is
located below the throttle quadrant. Heated air is provided by a heat
exchanger mounted on the exhaust system crossover tube from
cylinder #2, with a heater valve mounted on the firewall. The push/pull
knob opens and closes the cabin heat valve.
When the knob is retracted, all heated air from the heat exchanger
goes out the bypass to outside. As the knob extends, it pulls a rotating
lever which turns the heater/defrost valve. As it opens, more heat
goes to the outboard area of the cockpit crew’s feet. As it extends
even more, the heat starts to close and the defrost begins to open.
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Section 7 – Systems Description
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
When fully extended, it provides all defrost. The most heat for the feet
is when the knob’s cable is aligned with the red ring
Originally the system was operated by a robotic arm which was
controlled by a rheostat in the upper right corner of the instrument
panel. The robotic arm proved unreliable and was replaced by the
current pull/push cable. However, for to panel aesthetics, the
disconnected rheostat is still in place.
Left and Right Cabin Heat
Vents
7-10.2.
Fresh Air System
Two fresh air cabin vents are provided for the cockpit area. NACA
style inlet ducts on both sides of the fuselage feed air into boxes which
incorporate “eyeball” vent valves to control the flow of ventilation air
into the cockpit.
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Section 7 – Systems Description
7-23
Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
7-10.3.
CO Detector
The Carbon Monoxide Detector is a Pocket CO Model 300 which will
Velcro attach to the glare shield. The LED will light if there is a
problem.
7-10.3.1.
Pocket CO Operation:
Other Information:
 Pocket CO 300 Manual
 This in PDF or DOCX (select “save”)
 Data Sheet
Notes:
 Wait for the back light to turn on after first push before continuing
with more pushes.
 Vibrator is turned off
 50 PPM Alarm is turned off
Turn On
Push & Release button once
Will stay on for 12 hours or until turned off.
Make sure it says “12 hr”
Push & Release then
Push & hold for 2 seconds (until red flash)
Make sure it’s off and quiet.
Turn Off
Alarm activates when:





125 – 399 PPM
> 400 PPM
OAT < 32°F
OAT > 122°F
During Self test
Alarms every 10 seconds
Alarms every 5 seconds
Shows “COLD”
Shows “HOT”
To get Dosimeter Info if On: Push & Release twice
To get Dosimeter Info if Off: Push & Release button 3 times
Will automatically turn back off
7-24
Section 7 – Systems Description
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
(Shows last operational info)
Codes:





TE – Total Exposure
TWA – Time Weighted Average
MAX – Maximum concentration
TIME – Elapsed Time after turn on that MAX occurred
RUN – Run time in minutes
7-11.
ELECTRICAL SYSTEM
7-11.1.
Battery/Relay Electrical System
Starter Relay System
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Section 7 – Systems Description
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
7-26
Section 7 – Systems Description
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
7-11.2.
Wiring Picture – Under Right Seat
7-11.3.
Other Electronic Components
7-11.3.1.
Rheostat Control Modules
Located on right side of fuselage and behind the panel.
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Section 7 – Systems Description
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
7-11.3.2.
Positive Buss Bar
Located next to Rheostat Control Modules
7-11.4.
Alternators
There are two alternators. The main alternator is operated by the red
Master (ALT BATT) rocker switch and has the capacity of 60 Amps.
The standby alternator is operated by the left most rocker switch
labeled STBY ALT and has the capacity of 20 amps. Typically, the
standby alternator is off during flight. If the low voltage light
illuminates, the pilot should trun the STBY ALT on. A square red
“STBY ALT ON” warning light in the top-middle of the panel will
illuminate if the standby alternator is providing voltage. Turn the
STBYALT on if the main alternator has failed; reached its maximum
output or the load is too high for the main alternator. The standby
alternator must have at least between 1800 and 2000 RPM to operate.
Both alternators are manufactured by B & C Specialty Products
Contact people are Bill Bambridge and Gregg.
7-28
Section 7 – Systems Description
12-10-2014
Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
Main
Standby
Part #
L60
SD20
Volts
14
14-28
S/N
0792213
0897617K
Amps
60
20
TBO
2000 Hrs
1700 Hrs
7-11.5.
MASTER Switch
The Master switch is actually two switches – Alternator and Battery
(Labeled “ALT BATT”). The switch is split and the left side controls the
main alternator while the right side controls the battery. They are
normally moved together except for EOR alternator checks.
The BATT switch activates:






PFD1 (for engine instruments)
AHARS
AOA
Standby ADI
Audio Panel
#1 Communication Radio (SL-40)
All other avionics switches are activated by the MFD, AVI, or Auto Pilot
switches.
NOTE
Turning the battery switch off while external power is connect
may cause the CB located in front of the aircraft battery to
activate.
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Section 7 – Systems Description
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
7-11.6.
Circuit Breakers
Never reset a non-critical circuit breaker in the air. Never reset a
critical circuit breaker more than once without determining the cause of
the tripped circuit breaker.
All circuits are protected by pushpull type circuit breakers located
on the right side of the panel.
Because the Glasair Super II-S FT
does not conduct electricity, there
is a negative bus bar with a return
circuit for every electrical device.
It is located inside the cockpit on
the co-pilot’s side of the firewall.
7-11.7.
7-11.7.1.
Inside Lighting
Rheostat Controlled
Lights.
A rocker switch labeled “INTER
LTS” is the master on/off for the three rheostats located below the right
MFD/PFD. The left rheostat controls the rocker switch backlighting.
The center rheostat controls the standby instrument lights and other
avionics lights. The right rheostat controls the G3X backlighting.
7-11.7.2.
Dome Light
A single adjustable light is
on the overhead. It is an
“EyeBeam Touch” from
Aveo Engineering. It is on
the battery bus and the
on/off button glows. Touching the white or red button produces a
similar beam of light. Brightness is controlled by touching anyplace
along the ± line. It will swivel to shine on where you want the light.
7-30
Section 7 – Systems Description
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
7-11.8.
7-11.8.1.
Outside Lighting
Navigation lights
Navigation lights are installed on the ends of each wingtip and vertical
fin. They are controlled by a rocker switch labeled “NAV LGTS.” The
navigation-position lights consist of an appropriately colored lens (red
for left, green for right and white for tail). Lights are Pulsar-EXP, 13
Watts and manufactured by Aeroleds.
7-11.8.2.
Strobe Lights
Strobe lights are incorporated into the navigation lights and the landing
light has a wigwag function when the strobe rocker switch (STRB
LGTS) is on.
Note
With both alternators on and strobes on plus a heavy
electrical load the square low voltage light will blink in time
with the strobes. Normal work-around is to turn the standby
alternator off.
7-11.8.3.
Landing Light
A landing light is mounted in the lower engine
cowl. It is controlled by a rocker switch labeled
“LAND LGT.” If the “LAND LGT” switch is on
along with “STRB LGTS”, the landing light will
cease the wigwag function and create one solid
beam.
The light is a Sunspot 36HX from Aeroleds.com. 61-0361-001
Product #
01-1030-HA
Voltage Range
9-36VDC
Diameter / Depth
4.24” / 1.9”
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Section 7 – Systems Description
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
Current Draw at 12VDC
3.75 Amps Max / 45 Watts Max
Total LED Lumens
1500+
16 Temperature Range
-55°C to +70°C
7-11.9.
Intelligent Power Stabilizer (IPS)
The IPS-12v-4a Intelligent Power
Stabilizer, IPS, is an electronic
power converter providing aircraft
bus voltage surge and sag
protection for the left G3X. The IPS
system will operate over an input
voltage range from 5 volts to 15
volts and provides a regulated output voltage of greater than 11.25
volts. Prior to the IPS installation in N11HC the PFD would reboot
when the starter was engaged. The reboot was caused by the starter’s
electric draw lowering the voltage to the G3X enough to cause a reboot
of the system. The reboot, in turn, caused a temporary loss of critical
engine instrument monitoring during the start.
A picture of the IPS’s location above the pilot’s left knee area in
N11HC is in the Heating and Ventilation System paragraph this
section.
If the PFD C/B is pulled and the battery switch is on or alternators
operating, the IPS will continue to provide power to the PFD until the
small “IPS” white toggle switch, right of the light dimming knobs, is
turned off.
If the aircraft battery is extremely weak, the IPS system may not be
able to keep the connected equipment operational during engine
starting. If the battery is incapable of driving the starter to rotate the
engine through a complete compression cycle the aircraft battery may
be sagging below 4 volts. During these conditions the IPS system will
protect itself and the attached equipment by shutting down.
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Section 7 – Systems Description
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
Battery replacement is strongly encouraged if this condition exists.
Additionally, if the aircraft battery is deeply discharged, i.e. below 9
volts continuous output with no load attached, then when the aircraft
systems are initially energized (i.e. at aircraft power-up) the IPS
system will not boost the output voltage and it is likely the attached
equipment will not power up. This is a warning the aircraft battery is in
a state of deep discharge and may be in need of service or
replacement.
More information on the IPS is available on the N11HC website
7-12.
ELECTRICAL LOADS
Amperage loads of the components were measured using the analog
amp meter on the external power supply. Therefore the results are not
exact, but probably within 0.5 amps.
Normal Cruise Amps
14.0 A*
Battery Only
2.75A
PFD #1
0.50A
AHRS
0.75A
MFD
1.0 A
Avionics Master Switch
0.25A
PFD #2
0.50A
Audio Panel
0.10A
G430W
1.15A (2.25A while transmitting)
Transponder
0.75A
G-Meter and interior lights
Nill
SL40
0.25A (3.75A while transmittine)
ADI and AOA
0.85A
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Section 7 – Systems Description
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
Autopilot
1.65A
Pitot Heat
11.0 A
Flaps
5.00A
Fuel Pump
5.0 A*
Main Alternator and Sensor
3.00A
Standby Alternator and Sensor
nil
Nav Lights
1.0 A*
Strobe Lights
4.0 A*
Landing Light
2.0 A*
7-13.
PITOT-STATIC SYSTEM
7-13.1.
7-13.2.
Diagram
Pitot Tube and Heat
The Pitot Tube should be covered when not
flying to prevent bugs from plugging the tub. A
rocker switch labeled “PITOT HEAT” controls
heat to the pitot tube. The pitot tube can get
very hot, so do not touch or cover it until it has
time to cool. Periodically check this system by
turning on the battery and pitot heat for several
seconds, then turn them off and feel the pitot
tube. Also insure there is an increase in
electrical load when the pitot heat switch is
turned on.
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Section 7 – Systems Description
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
7-14.
ANTENNAS
The avionics antennas are mounted internally inside the fiberglass
structure except for the transponder antenna and the ELT antenna on
a dome, both of which are on the inside of the fuselage belly.
7-15.
MAIN ROCKER SWITCHES
 STBY ALT ........................................... Standby Alternator
 MFD .................................................... Multi Function Display
 AVI ...................................................... Avionics (G430, Right G3X,
Transponder & G-Meter)
 AUTO PILOT ...................................... GX auto pilot
 NAV..................................................... Navigation Lights (Red,
Green and White)
 STRB .................................................. Strobe Lights (Includes
pulsing landing light)
 LAND .................................................. Landing Light
 INTER LTS ......................................... Interior Lights (Dimmed by
3 rheostats on right)
 PITOT HEAT....................................... Pitot Heat switch
 FUEL PUMP ....................................... Fuel Pump switch
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
7-16.
INSTRUMENTATION
The instrument panel on N11HC consists of:













7-16.1.
Three Garmin G3X PFD/MFDs
GSU 73 Sensor Unit
GMU 44 Magnetometer Unit
GTP 59 Temperature Probe
Garmin GNS 430W
Garmin SL40 Communication Radio
Garmin GTX 327 Transponder
TruTrak GX autopilot
PS Engineering PMA8000B Audio Panel
Standby instruments (Airspeed, Attitude, Altimeter)
AOA Indicator
Flight Data Systems GT50 G meter
406 MHz Emergency Locator Beacon
Garmin Sensor Unit (GSU 73)
The G3X’s incorporate a GSU 73 which senses and displays on the
G3X all engine gauge, ADC, Airframe, and AHRS information.
Located above and forward of the pilot’s left knee.
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
7-16.2.
G3X PFD/MFD (GDU 370/375)
Designed around the GDU 370/375 series of panel-mount displays, the
G3X suite provides a non-TSO’d PFD/MFD system.
7-16.2.1.
Configuration mode
Configuration mode is used to set specific G3X parameters while on
the ground. This mode is entered by starting or rebooting the G3X.
If the PFD is off, turn on electrical power while holding the bottom left
button.
If the PFD is already powered up, press and hold the two bottom
outboard buttons while pressing the RNG down button to start the
reboot. Then hold the bottom left soft key while the system reboots.
Instrument markings are entered in the configuration mode and screen
shots of set markings are on the 11HC website.
NOTE
Turning the battery switch off while external power is connect
may activate the CB located in front of the aircraft battery.
Avoid this by always having the battery on before plugging in
or unplugging the external power.
7-16.2.2.
Left Screen (PFD1)
When the MFD is operating, PFD1 is a dedicated full Primary Flight
Display showing attitude/directional guidance. When the MFD is not
operating, PFD1 shows some engine instruments in the top portion
and the bottom half can provide MFD information including additional
electronic and engine monitoring information.
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7-16.2.3.
Center Screen (MFD)
The center screen is a multifunction display (MFD) showing items such
as detailed moving-maps, instrument approach plates, weather,
terrain, and engine gauges.
7-16.2.4.
Right Screen (PFD2)
The right screen can be use for either a second PFD or second MFD.
The software switch allows for either full MFD mode or full PFD mode
(Full PFD mode does not allow the lower half of the screen to display
MFD information).
There is a toggle switch behind the panel on the lower left side of
PFD2. This switch goes to pin 9 and was originally installed to select
MFD or PFD while on the ground with all power off. Software does this
now and moving the switch when power is on the aircraft could be very
bad for the G3X. Just leave the switch up!!! When the switch is on, it
tells the right G3X that it is a PFD2 system. Old pilot rule – don’t mess
with the dull switches, play only with shiny switches.
7-16.2.5.
Redundancy and Integration
The three displays are interlinked through the built-in network interface.
This allows full reversionary backup for added safety and redundancy.
The G3X displays are also integrated with the GX TruTrac Autopilot,
SL40 and G430W.
7-16.2.6.
Part Numbers etc.
System ID = 22B02D761F096
Information listed on the back of these are:
left PFD is:
 GDU 370 AM GPS
 011-01 747-15
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
 Bar Code 1M8 0000 49
Center MFD is:
 GDU 375
 011-01 747-30
 Bar Code 1LD 0000 76
Right PFD or MFD
 GDU 370 AM GPS
 011-01 747-15
 Bar Code 1M8 0000 296
GSU 73
 S/N 1D 00000 37
7-16.2.7.
G3X Pilot’s Guide
Pilots should check for updates to the G3X Pilot’s Guide by going to:
https://buy.garmin.com/shop/store/manual.jsp?product=010-00G3X00&cID=155&pID=63892&ra=true
7-16.2.8.
Data Bar Fields
The Data Bar Fields are located at the top of each G3X and are
customizable. See the G430W paragraph of this section for its
programmed data fields. As of January 2013, the programmed data
fields are:
PFD1
WPT
DST
DTK
TRK
MFD
BRG
VSR
ETA
UTC
PFD2
ECO
EDR
FF
REM
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Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
Definitions of Available Data Bar Fields:
BRG
DA
DST
DTK
ECO
EDR
ESA
ETA
ETE
FLT
FF
G
GS
7-40
Bearing to Waypoint The compass direction from the
present position to the next waypoint.
Density Altitude
Pressure Altitude adjusted for nonstandard temperature.
Distance to
The distance to the next waypoint in
Waypoint
the Active Flight Plan.
Desired Track
The desired course between the active
“from” and “to” waypoints.
Fuel Economy
This value is calculated by dividing the
current ground speed by the current
fuel flow.
Fuel Enduranc
This value is obtained by dividing the
amount of fuel on board by the current
fuel flow (endurance to empty - no
reserve included).
En Route Safe
The recommended minimum altitude
Altitude
within ten miles left or right of the
desired course on an active flight plan
or direct-to.
Estimated Time of
The estimated time at which the aircraft
Arrival
should reach the next waypoint, based
upon current ground speed and track.
Estimated Time En The estimated time it takes to reach the
Route
next waypoint from the present
position, based upon current ground
speed.
Flight Time
The total time in flight.
Fuel Flow
The current fuel flow.
G-Meter
The amount of positive or negative G’s.
Ground Speed
The velocity that the aircraft is traveling
relative to a ground position.
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
LCL
Time of Day (Local)
MACH Mach Number
MSA
Minimum Safe
Altitude
REM
Fuel Remaining
TRK
Ground Track
USD
Fuel Used
UTC
Time
VSR
Vertical Speed
Required
WPT
Next Waypoint
XTK
Crosstrack Error
7-16.2.9.
The current time and date in 12-hour or
24- hour format
A unit of speed that measures the ratio
of the speed of an airplane to the
speed of sound in the same
atmospheric conditions
Uses Grid MORAs to determine a safe
altitude within ten miles of the aircraft’s
present position.
The current fuel remaining (gal)
adjusted for fuel burn and based on
fuel flow.
Direction of aircraft movement relative
to a ground position.
The quantity of fuel used (gal) based
on fuel flow.
The current time and date in Universal
(UTC) time.
The vertical speed necessary to
descend/climb from the current position
and altitude to the previously selected
VNAV position and altitude, based
upon current ground speed.
The next waypoint in the flight plan or
direct-to route.
The distance the aircraft is from a
desired course in either direction, left or
right.
G3X Software/Manuals Updates
See https://buy.garmin.com/shop/shop.do?cID=155&pID=63892 for
updated G3X information
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
Software Update Instructions
 Download the self-extracting update file onto your hard drive.
 Insert an SD card with at least 20 MB of free space into your card
reader.
 Open the self-extracting update file and follow the instructions
provided by the installer application. You will be prompted to
specify the drive letter of the SD card you wish to use for the
update.
 Apply power to your cockpit display.
 Insert the SD card containing the software update. You will be
prompted to confirm before the update is installed.
 During the software update, the display will indicate 'Loading'. Do
not remove power during the update process.
 When the update is completed, the display will reset itself and
turn on normally.
 Repeat steps 5-7 for each display unit in the aircraft.
 If prompted to perform a GSU 73 software update, follow steps
10-12:
 Enter config mode by holding down the leftmost softkey on PFD1
while powering on the system.
 Scroll to the 'GSU' page and press the 'UPDATE SW' softkey.
 Press the Enter key to begin updating the GSU 73 software. Do
not remove power during the update process.
Note
Even if it does not prompt to perform a GSU-73 software
update, check for one anyway by following the last three
steps above. The GSU page will state if it is out of date and
point to a softkey to update. You can also reload the current
update if you wish via other keystrokes.
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Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
7-16.2.10. Flight Data Files
Flight and engine data are stored on the
removable SD memory cards in each
G3X. You can analyze almost everything
about your flights with this data.
You can uploaded the data to MS Excel
or to cirrusreports.com and review all
your flight and engine data such as EGT,
CHT, oil temp and pressure, fuel flow,
airspeed, ground speed, distance, etc.
It creates an electronic logbook and even summarizes your fuel burn,
ground op time, and flight time for each flight. The next time you repeat
a flight you can go to your flight log and see how much fuel you used
the last time you flew that trip.
If you click on the Google Earth 3DView selection above the map it will
immediately launch Google Earth and export the selected flight into
Google Earth and show the 3D "roller coaster" for that flight. If you click
on the Google Earth Cockpit View it will launch Google Earth and allow
you to re-fly the flight as if you were in the cockpit looking out.
Just go to cirrusreports.com, create a free account (specify aircraft
type as Other and Log Format as G1000 or G900X) and upload your
G3X flight data log files to create your online logbook of flight and
engine data. You can either choose to share this flight data or hide it
from others.
Google Earth GPS Tracking
Vans Air Force net has a great article on how to get the GPS track
from the G3X into Google Earth.
7-16.2.11. G3X / G430W Subscriptions
The most current software must be loaded into the system. Refer to
the Garmin website and the MFD “splash screen”.
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
Database Subscription
Garmin and Jeppesen offer a PilotPak pricing program for multiple
G3X’s in a single aircraft. Below is what’s included in the pilotPak and
their individual costs.










Nav Data (13 updates/year) ............... $160
Obstacle (7 updates/year) .................. $195
Terrain (Single) ................................... $150
Safe Taxi (7 updates/year) ................. $195
AOPA (7 updates/year)....................... $195.00
FlightCharts (13 updates/year) ........... $199.95
Individual Annual Total ....................... $1094.95
PilotPak Price...................................... $500
Additional G430W Nav Data (required for IFR)
............................................................ $410
 XM Weather Aviator ............................ $660
 Total Annual Subscription ................... $1570
 Total Monthly Cost .............................. $131
All avionics updates including 28-day databases must be logged into
the N11HC Avionics Update Table. This table is located in the back of
this POH – Logs for Inspections, Updates and Checks.
The G3X package includes a Terrain dB, so a Garmin USB Aviation
Data Card Programmer, Part Number 010-10579-00 ($195) is not
required as this is only for terrain a GNS430W terrain dB. However, a
Jeppesen Skybound G2 USB Adapter, part number DSKYG241
($49.95) is required for the GNS430W Nav data card.
7-16.2.12. Airspeed V-Speeds and Trend Line
The G3X Airspeed Trend Vector is a vertical, magenta line, extending
up or down on the airspeed scale, shown to the right of the color-coded
speed range strip. The end of the trend vector corresponds to the
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Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
predicted airspeed in 6 seconds if the current rate of acceleration is
maintained. If the trend vector crosses Vne, the text of the actual
airspeed readout changes to yellow. The trend vector is absent if the
speed remains constant or if any data needed to calculate airspeed is
not available due to a system failure.
References speeds for Glide, Vx, and Vy are pilot programmable and
selectable within the G3X. A pointer can be displayed on the right side
of the airspeed display opposite the speed that was programmed. The
pointer are placarded [G] for glide, [Y] for Vy, and [X] for Vx.
NOTE:
Indicated gross weight stall speed with flaps (Vso) for the
white arc and the indicated clean stall speed (Vs) for the
green arc are yet to be determined during flight testing. AOA
will also be documented for these conditions.
7-16.2.13. Gee Wiz
Highly Evolved.
These synthetic vision GDUs feature 7-inch high-definition WVGA
screens, built-in high-sensitivity GPS receivers, rotary joystick cursor
controls for data entry, redundant power inputs, and softkeys for mode
selection. There’s a front-loading SD card slot for easy software and
database updates. Plus, built-in aviation basemaps help provide
realistic visual reference – identifying cities, roads, rivers, lakes, and
other ground features. There’s a built-in terrain elevation database
that uses color-coding to alert you as you approach potentially
hazardous terrain. Both overhead and vertical profile views of this data
are graphically depicted on the terrain page.
Electronic Charts
G3X system includes Geo-Referenced SafeTaxi® airport diagrams and
Garmin FliteCharts®. Plus, there’s also AOPA Airport Directory data
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
that offers detailed information on over 7,400 U.S. airports, along with
airports of entry for Canada, Mexico and the Caribbean.
XM Data
N11HC incorporates XM™ WX satellite datalink capability provides
graphical NEXRAD imagery, METARS, TAFs, TFRs, winds aloft, echo
tops, lightning strikes, storm cell data, and more. It also has an XM
receiver for 170 channels of digital inflight XM Radio.
7-16.2.14. Solid-State ADAHRS (GSU 73)
The G3X system uses the latest in GPS-aided digital ADAHRS (Air
Data and Attitude Heading and Reference Systems). Leveraging solidstate sensors and sophisticated attitude determination and integrity
monitoring algorithms used in Garmin’s high-end G1000 system, the
G3X’s ADAHRS provides highly accurate and reliable referencing of
aircraft position, rate, vector and acceleration data. The complete
sensor package includes: ADAHRS, EIS (engine monitoring),
magnetometer and temperature probe.
Information Printed on the GSU 73 is:
 P/N 001-01817-00
 Bar Code *1D 000 00 37
7-16.2.15. Magnetometer (GMU 44)
The Magnetometer continuously updates the heading indicator of the
G3X and is located about halfway between the tail and the cockpit and
on the upper left side. It is cylinder in shape and must face directly
forward.
Information Printed on the GMU 44 is:
 P/N 001-00870-10
 DO-160D, DO-178B Level B
 TSO-C6d; ETSO-C6d
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
 Bar Code *1CH005064*
7-16.3.
Garmin GNS 430W
To augment the G3X’s non-TSO’d internal VFR GPS, N11HC
incorporates the Garmin GNS 430W WAAS-certified IFR
GPS/Nav/Comm unit – Thus making N11HC IFR capable.
7-16.3.1.
7-16.3.2.
GNS430W is the #2 radio
Control Stick Operations
The control stick on N11HC can control several functions of the GNS
430W. Using the “Chinaman’s Hat” switch and the top round button
next to the Chinaman’s Hat switch:
Forward – flip/flops the Comm frequencies
Aft – flip/flops the Nav frequencies
Left – cycles the CDI (or is the same as pressing the CDI button)
Right – cycles the OBS (or is the same as pressing the OBS
button)
The top round button next to the China
Hat cycles through the channelized Comm frequencies.
See Control Stick Grip diagram toward the end of this section.
7-16.3.3.
Data Bar Fields
As of September 2011 the programmed Data Bar Fields were:
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
XTK
ESA
ETA
TKE
MSA
ETE
See the G3X paragraph for what these abbreviations mean.
Available Data Bar Fields:













BRG .................................................... Bearing to Waypoint
DIS ...................................................... Distance
DTK ..................................................... Desired Track
ESA ..................................................... Enroute Safe Altitude
ETA ..................................................... Estimated Time Arrival
ETE ..................................................... Estimated Time Enroute
GS ....................................................... Ground Speed
MSA .................................................... Minimum Safe Altitude
TKE ..................................................... Tracking Angle Error
TRK ..................................................... Track Over Ground
VSR ..................................................... Vertical Speed Required
WPT .................................................... Waypoint - Next
XTK ..................................................... Cross Tracking Error
7-16.3.4.
Integrate Avionics
GNS 430W is an all-in-one GPS/Nav/Comm and meets TSO C146a
standards for WAAS "sole means" navigation and 10 watts minimum
transmitting communications plus a 200-channel ILS/VOR with
localizer and glideslope.
7-16.3.5.
Data Cards
The GNS 430W has two removable data cards, one with a Jeppesen
database (inserted in the left-most card slot) and the second being a
Terrain database (inserted in the right-most card slot). For information
on removing and installing the data card, see Appendix A – “NavData
Card Use” – in the 400W Series Pilot’s Guide & Reference.
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The Jeppesen database contains all airports, VORs, NDBs,
Intersections, FSS, Approach, DPs/STARs, and SUA information. The
G3X database system includes its own Terrain database, so N11HC is
not carrying an updated Terrain database within the G430W.
7-16.3.6.
Configuration Mode Operations
With power applied to the aviation rack and the 400W Series unit
turned off, press and hold the ENT key and turn the unit on. Release
the ENT key when the display activates. After the Data Base and
Instrument Panel Self-test pages, the first page displayed is the MAIN
ARINC 429 CONFIG page. While in Configuration Mode, pages can
be selected by ensuring the cursor is off and rotating the small right
knob.
To change the data on the displayed Configuration Page, press the
small right knob (CRSR) to turn on the cursor. Rotate the large right
knob to change between data fields. Rotate the small right knob to
change a field that the cursor is on. Once you have made the desired
selection, press the ENT key to accept the entry. For instance,
activating the remote channelization was under Main System Config,
then Configure-Discretes.
More information is available in Chapter 5 of the G430 Install Manual.
7-16.4.
Autopilot
N11HC’s TruTrac GX autopilot
accepts roll-steering
commands from the GNS
430W and can automatically fly
the aircraft through holding
patterns, procedure turns and other position-critical IFR flight
procedures.
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
7-16.4.1.
TruTrak GX Autopilot
Designed to interface with Garmin G3X™ and is controlled through the
G3X.
1.7” x 6.25”
Built-in Ground Track DG
Track Select Mode
Altitude Hold
VS Select Mode
EFIS Mode (Lateral and Vertical Steering)
Control Wheel Steering
Pitch Trim Annunciation
The autopilot is activated and turned off with the “AUTO PILOT” rocker
switch. The control stick also has a switch about half-way down to
engage and disengage the autopilot with a quick click or enter the
“Control Wheel Steering” (CWS) mode by holding the button while
setting the desired aircraft attitude.
N11HC has a GX autopilot and there is a short manual for it. Use the
G3X Pilot's Guide for most operational information. Both are posted on
the 11HC website.
Information printed on the back of the Trutrak GTFP GX Pilot Flat
Pack:
 P/N 8000-138
 S/N 100 503-8000-138-001
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
7-16.5.
7-16.5.1.
PMA8000B Audio Panel
Comm 1 vs. Comm 2:
Comm 1 controls the SL40 and Comm 2 controls the GNS430W radio.
7-16.5.2.
Control Stick Swap Mode:
The “pinky” button on the control stick will flip/flop the MIC button
between Comm 1 and Comm 2.
7-16.5.3.
Recorder System
Push and hold the COM Receive pushbutton associated with the
transmission (~1 sec.). To cancel the playback, press and hold the
playback button for two seconds. The next time the button is pressed
for one second, the next earlier message will be heard.
7-16.5.4.
Split Mode
Pressing Com 1 and Com 2 XMT buttons at the same time puts the left
seat on Com 1 and the right seat on Com 2.
7-16.5.5.
More Information
Operation of the PMA8000B is common to most pilots but much more
information is in its manual.
7-16.5.6.
Data Plate
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
Note that this version of PMA8000B cannot upgrade to the newer
model that will mute the second radio automatically.
7-16.6.
Garmin SL40 Communication Radio
SL40 incorporates active and
standby flip-flop frequency
tuning, direct sunlight-readable
alphanumeric display, easy
access to National Weather Service broadcasts saved and used freq.
storage/recall.
With 8 watts of transmit power and only 35-watt DC input, the SL40 is
cool and efficient.
7-16.6.1.
7-16.6.2.
SL40 is the #1 radio
EC – Emergency Channel
Sets 121.5 into the standby frequency in “Monitor” function.
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Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
7-16.6.3.
MON - Monitor 2 frequencies
Press the MON button to listen to the standby frequency. A small ’m”
is displayed in front of the Standby frequency. When the active
frequency receives a signal, the unit will switch automatically to the
Active frequency and then switch back when activity ceases. An arrow
(< or>) will point to the frequency that you are currently
The SL40's frequency-monitoring function gives the ability to monitor
ATIS or the 121.5 emergency frequencies without leaving an assigned
ATC channel. This allows you to listen to standby frequencies while
giving priority to the active channel, meaning you'll never miss a
transmission.
7-16.6.4.
RCL – Recall Memory
Recall is 4 areas of stored frequencies. Press “RCL” then rotate outer
knob to desired icon (REM, LST, MEM, WTH). Then use inside knob
to select frequency.
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
REM – Remote
Accesses the G430 frequency database. The waypoint type and
frequencies are displayed.
LST - Auto Stack List
Recalls a list of last 8 frequencies.
MEM – User Stored Freq. Memory
Gives list of stored frequencies (after storing with MEM button)
WTH – Weather
Has the standard weather channels. (162.475 is RST)
7-16.6.5.
MEM – Button
Pressing the MEM button puts the Standby freq into user Memory.
Press MEM and turn big knob for “Remove” option. Then turn the
small knob to freq to remove. Then MEM to remove the freq.
7-16.6.6.
7-54
SL40 S/N 258 10 848
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7-16.6.7.
Garmin GTX 327 Transponder
The GTX 327 is a
TSO-certified Mode C
digital transponder.
7-16.6.8.
Transponder Controls
OFF – Powers off the GTX 327. Pressing STBY, ON, or ALT key
powers on the transponder displaying the last active identification
code.
STBY – Selects the standby mode. When in standby mode, the
transponder will not reply to any interrogations.
ON – Selects Mode A. In this mode, the transponder replies to
interrogations, as indicated by the Reply Symbol ( ). Replies do not
include altitude information.
ALT – Selects Mode A and Mode C. In ALT mode, the transponder
replies to identification and altitude interrogations as indicated by the
Reply Symbol ( ). Replies to altitude interrogations include the
standard pressure altitude received from an external altitude source,
which is not adjusted for barometric pressure. The ALT mode may be
selected in aircraft not equipped with an optional altitude encoder;
however, the reply signal will not include altitude information.
Any time the function ON or ALT is selected the transponder becomes
an active part of the Air Traffic Control Radar Beacon System
(ATCRBS). The transponder also responds to interrogations from
TCAS equipped aircraft.
7-16.6.9. S/N 837 36 966
7-16.6.10. Transponder Features
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
GTX 327 features a solid state design, and with no warm up time,
lower power consumption and much lower heat emissions. It provides
200 watts nominal power output and has an easy-to-read DSTN liquid
crystal display which reverses the numbers out of black for optimal
viewing. An innovative keypad makes entering a squawk code a snap,
and a dedicated VFR button allows for quick-and-easy VFR
squawking. The 327 also offers several timing and display functions,
including flight time, count-up and count-down timers, as well as
current pressure altitude.
See the GTX 327 manual for more information.
7-16.7.
Standby Instruments
The 2.25” Standby Instruments are located on the
left side of the panel and are as follows:
7-16.7.1.
Airspeed
The airspeed indicator has a white arc between 59
and 122 knots, a green arc between 67 and 174
knots, a yellow arc between 174 and 225 knots, and
a red line at 126 knots
Information Printed on the back of the AS indicator:




UMA
MFG P/N 16-211-240
P/N Spec ?KGS
S/N A4336
7-16.7.2.
Attitude Indicator
The Attitude indicator is a TruTrak Flight Systems 8300-016 Rev B
indicator. The system incorporates the following information:
Gyro / VS pitch display
Bank Angle display
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
Built-in Ground Track DG
Low Airspeed Warning
Link to: TS Manual or RF Manual
The ADI is easy to fly partly because it contains in one instrument, roll,
pitch, and direction. Beyond this, it is the content of each of these
displays that make this instrument easy to fly.
The direction display is located in the center of the instrument just
below the rotating horizon mask. As is often the case with an
inexperienced pilot caught in IMC, the instrument may be viewed with
tunnel vision. For this reason it is good to have the direction in the
center of the tunnel. Of more importance is that this display is track
instead of magnetic heading in that the modern way to navigate is to fly
track. When track is presented as a gyro display, the numbers move
sequentially one degree at a time. Experience is showing that direction
control with this digital DG placed immediately below the horizon mask
is as easy to fly as the conventional vertical card DG in combination
with the conventional horizon placed nearby.
The bank angle display is driven in a manner similar to that used in the
pictorial turn and bank. The only difference is that in this instrument the
display shows bank angle instead of turn rate. The advantage of this is
that the presentation is instantaneous data only. It cannot drift to
accumulate error as is possible with the more complex AHRS driven
systems. It shows bank angles of up to +/- 45° while the requirement
on conventional gyro horizons is +/- 100°. Note that when flying on
instruments the object is to stay level or at least in shallow banks. This
instrument is therefore designed to keep the pilot out of trouble.
The pitch display is perhaps the most beneficial feature of the ADI
when compared with conventional horizon indicators. For short term or
immediate movement of the nose up or down, this instrument responds
and is flown like any other gyroscopic pitch indicator. The difference is
that after the display has moved in response to an attitude change the
deflection is sustained by the resulting vertical speed. As compared to
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
a pitch attitude display, the vertical speed display makes it easier to
hold altitude and to maintain stable climbs and descents. Also, the
movable airplane symbol does not have to be adjusted to compensate
for the angle the fuselage flies when vertical speed is zero. It is
recognized that an aircraft when at the limit of its altitude capability can
fly at an ever increasing angle of attack when vertical speed indicates
zero. For this reason an airspeed warning in the form of the letters “AS” flashing in the DG display is provided. The answer to this situation is
then to observe the airspeed indicator. For stall prevention airspeed is
the best information short of an angle of attack indicator. (Better than
attitude)
Another plus regarding this display is that when the airplane is going
straight or not turning a wing level presentation is shown. With this
presentation one can disregard the effect of the rudder being out of
trim (ball off center) just as crosswind is not a factor when flying GPS
track for direction. This is easier than trying to fly straight with the
display showing a wing down as is the case with a conventional
horizon display when the rudder is out of trim.
There is an “ADI Backup Battery” toggle switch
just right of the autopilot control panel. Moving
the switch up provides power to the standby ADI
via the internal standby ADI battery.
Information Printed on the TruTrak CPU, which is
mounted on the Aux. fuel tank is:
 ADI BB 12V
 P/N 8000-037
 S/N 091014-3000-037-008
See the manual for more information.
ADI Backup Battery & Servicing:
The servicing of the ADI backup battery is simply a matter of inspection
of the functionality and confirming charge and discharge rates.
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Section 7 – Systems Description
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
Recommendation of a function test during the pre-takeoff checklist to
confirm the LED switch illuminates with activation of the backup
battery. The ADI should function normally in this mode. Once it has
been verified that the backup battery is properly functioning, return the
switch to the normal position.
Information Printed on the back of the TruTrak instrument is:




TruTrac ADI 2
P/N 8000-033
S/N 091029-8000-033-002
Max Amps: 1
7-16.7.3.
Altimeter
From UAM, this simple type (single pointer) is not designed as a
backup IFR altimeter when accomplishing approaches to low
minimums. Altitudes can be read in ± 500’ markings. The altimeter
utilizes a knob adjustable barometric scale, viewed through a Kollsman
Window. It is not connected to the outside static
system. S/N A3122
7-16.8.
Compass
The “Whisky” compass is from Sirs Navigation.
Part number: NV2C-12V, S/N 715962-04. The
spec sheet is also on the N11HC website but is
very small print. A modified version is also on the
website with larger print.
7-16.9.
GT-50
The GT-50 from Flight Data Systems
incorporates the following:
 Instantaneous Accelerometer to
+12/-10 G's
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop






Records MAX and MIN G's
12/24 hour Quartz Chronometer
Timer/Stopwatch
Automatic Flight Timer
Voltmeter
Standard 2-1/4" Instrument
Information printed on the back of the GT-50:
 GT-50 9322, Rev 4a
7-16.10. AOA Indicator
The AOA indicator is from Advanced Flight Systems, Inc
(http://Angle-of-Attack.com). Its 3-color, 8-LED ladder
provides the pilot with critical AOA information such as: best
glide, best approach, high angle and stall critical information
which is consistent even with different G loading or weight.
It is affected by wing contamination such as ice or other
foreign objects which distort the wings ability to create lift.
Stall warning devices and AOA devices are different in design. This
AOA instrument does not meet the FAA TSO requirements for stall
warning devices.
A failure of the Pitot/Static pneumatic system such as taking off with a
covered pitot tube will cause the AOA to give false and unreliable
information.
This system, like other electrical systems, requires a minimum voltage.
The term "angle of attack” is the angle between the relative wind and
the chord of the airfoil. This instrument uses “angle from zero lift” ± a
constant to compute zero AOA. “Angle from zero lift” is when the wing
isn’t creating lift (zero G). This AOA Instrument technically measures
angles from zero lift.
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Section 7 – Systems Description
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
As good as this is, it is not to be used as a primary instrument and
should always be cross-checked with the airspeed indicator for
reasonableness.
Information Printed on the back of the AOA CPU:
 P/N: Sport 111 07 03
 S/N: 40261
7-16.10.1. Checklists
Verification and Calibration checklists are at:
http://44rf.com/11hc/checklists/aoa/aoa_checklists.pdf.
7-16.10.2. Preflight
For proper operation the two wing ports and the aircraft main static
ports must be clear – checked on preflight. Also on preflight, the pilot
must drain the AOA air/water separator.
The top wing port is located 31” from the wing’s end and 17.375” at 90°
from the trailing edge. The bottom wing port is located 33” from the
wing’s end and 17.375” at 90°from the trailing edge. The air/water
separator is located next to the bottom port and just inside about a ¾”
diameter hole on the wing bottom (press to drain).
7-16.10.3. Operating Temperatures
IAW the AOA manual specifications page, the operating temperature of
the CPU is -1 to 43°C (30-110°F) which is why the CPU is in the
heated area of the cockpit (mounted on the header tank).
7-16.10.4. AOA Labels
The AOA Display must be placard with “NOT TO BE USED AS A
PRIMARY INSTRUMENT.”
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
7-16.10.5. Indications
2G-1Y
L/D
Max
1G
Vx
1Y
Cruise Max
Endurance
2Y
Angle
Optimum Advisory
Approach
Critical
AOA
Max Glide
Range
7-16.10.6. AOA Buttons
There are two buttons – test and dim. Pressing them both at the same
time enters the calibrate mode. See the AOA manual concerning
calibration.
7-16.10.7. AOA Test
After pressing the “TEST” button the display will be blank for several
seconds then all the light bars will display for several seconds. The
audio should enunciate “Angle Angle Push”, “Flaps”, “AOA Pass”.
7-16.10.8. AOA Enunciator
When the AOA reaches a high and almost stall condition the
enunciator will enunciate “Angle Angle Push”. When the flaps are
deployed it will enunciate “Flaps”.
7-16.10.9. Flap Micro Switch
There is a micro switch that determines the flap position. When the
flaps are deployed beyond 20°, a different set of AOA settings are
automatically shown which compensates for the change in lift.
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Section 7 – Systems Description
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Slotted Flaps, Extended Wing Tips, IO-360, C/S Prop
When the flaps are deployed, there will be an aural enunciator of
“FLAPS”.
7-17.
WING TIP EXTENSIONS
These wing tip extensions add four feet to the wing-span which
increases the aspect ratio from 6.2 to 7.6. The climb performance is
increased by 150 feet/min., stall speed is reduced up to 9 knots., and
the lateral (roll) stability is greatly improved for cross-country flying.
They add 100 lbs to the maximum gross weight and increase the glide
ratio.
Since the tip extensions reduce the roll rate considerably, they make
aerobatic maneuvers more challenging.
The shorter tips should be installed prior to extensive aerobatic
maneuvering.
The extensions do not reduce maximum G load limits.
The tip extensions serve to lower the wing loading and reduce
approach speed for those
pilots with limited experience
in high performance aircraft.
7-18.
ELT
7-18.1.
Operation
The main on/off switch is
behind the baggage
compartment and is always on.
The cockpit “ON” button (left)
will turn the system on to
transmit a distress signal and
will also activate the center
light. To turn the transition and
light off, press and release the
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Pilot’s Operating Handbook for Glasair Super II-S FT N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
“RESET” button (right)
7-19.
CONTROL STICK GRIP
The control stick grip is from Infinity Aerospace
Just as one peek is worth a thousand crosschecks, so too is one
picture worth a thousand words…
See the Placards and Markings paragraph in Section 2 for details and
downloads for printing these decals.
7-64
Section 7 – Systems Description
12-10-2014
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
Section 8 - Handling, Servicing and Maintenance
Table of Contents
8-1. GENERAL ................................................................................ 8-5
8-2. AIRPLANE INSPECTION PERIODS ....................................... 8-5
8-3. PREVENTATIVE MAINTENANCE ........................................... 8-5
8-4. AIRPLANE PAPERWORK ....................................................... 8-6
8-5. GROUND HANDLING .............................................................. 8-7
8-5.1. Tire Inflation .......................................................................... 8-7
8-5.2. Towing .................................................................................. 8-7
8-5.3. Parking ................................................................................. 8-8
8-5.4. Mooring ................................................................................. 8-8
8-6. ADDITIONAL ITEMS TO CHECK DURING OIL CHANGES ... 8-9
8-7. OIL REQUIREMENTS .............................................................. 8-9
8-8. FUEL REQUIREMENTS .......................................................... 8-9
8-8.1. Fuel Grade............................................................................ 8-9
8-8.2. Draining Fuel Strainer, Sumps and lines ........................... 8-10
8-9. ADVISORY PUBLICATIONS ................................................. 8-10
8-10. CONDITION INSPECTION CHECKLIST ............................... 8-11
8-10.1. Service Lives ...................................................................... 8-11
8-10.2. Inspection Times ................................................................ 8-11
8-10.3. Advisory Publications, AD’s etc. ......................................... 8-11
8-10.4. Parts & Supplies ................................................................. 8-11
8-10.5. Pre Condition Checks & Prep ............................................ 8-12
8-10.5.1. Engine Run-up: ........................................................... 8-12
8-10.5.2. Engine In Flight Checks:............................................. 8-13
8-10.5.3. External Lights ............................................................ 8-14
8-10.6. Powerplant and Propeller ................................................... 8-14
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Section 8 – Handling, Servicing & Maintenance
8-1
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
8-10.6.1. Engine Compression Check ....................................... 8-14
8-10.6.2. Engine Oil & Filter ....................................................... 8-14
8-10.6.3. Plugs ........................................................................... 8-15
8-10.6.4. Magnetos .................................................................... 8-15
8-10.6.5. Engine Controls: ......................................................... 8-16
8-10.6.6. Fuel System: ............................................................... 8-16
8-10.6.7. Engine & Accessories:................................................ 8-17
8-10.6.8. Propeller and Spinner ................................................. 8-18
8-10.6.9. Ground Run-up Check................................................ 8-19
8-10.6.10. Cowling Installation ................................................... 8-20
8-10.7. Cabin & Fuselage ............................................................... 8-20
8-10.7.1. Interior Lighting ........................................................... 8-20
8-10.7.2. General Cockpit Inspection ........................................ 8-21
8-10.7.3. Canopy Latch & Lock Mechanisms ............................ 8-21
8-10.7.4. Interior Panel Removal ............................................... 8-21
8-10.7.5. Forward Cabin Checks ............................................... 8-22
8-10.8. Control System Inspection ................................................. 8-23
8-10.8.1. Under Seat Pan Area ................................................. 8-24
8-10.8.2. Battery inspection: ...................................................... 8-24
8-10.8.3. Control Tunnel Area ................................................... 8-24
8-10.8.4. Aft Fuselage Area: ...................................................... 8-25
8-10.9. External Fuselage & Belly Pan ........................................... 8-25
8-10.9.1. Control Surfaces & Rigging ........................................ 8-25
8-10.9.2. Low Checks ................................................................ 8-26
8-10.10. Wings & Control Surfaces: ........................................... 8-26
8-10.11. Landing Gear ................................................................ 8-27
8-10.12. Post Maint Systems Check: .......................................... 8-28
8-2
Section 8 – Handling, Servicing & Maintenance
08-10-2013
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
8-10.13.
8-10.14.
8-10.15.
08-10-2013
Post Maint In-Flight Checks: ......................................... 8-29
Paperwork ..................................................................... 8-29
Completion Sign-Off: .................................................... 8-30
Section 8 – Handling, Servicing & Maintenance
8-3
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
INTENTIONALLY LEFT BLANK
8-4
Section 8 – Handling, Servicing & Maintenance
08-10-2013
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
8-1.
GENERAL
This section provides general guidelines relating to the handling,
servicing, and maintenance of the Glasair Super II-S FT, N11HC. For
more complete maintenance instructions, refer to the original building
manual.
The owner should stay in close contact with New Glasair
(http://www.glasairaviation.com) and watch the forum posts at
http://www.glasair.org. These will show service bulletins and any new
problems and ideas other users may have.
8-2.
AIRPLANE INSPECTION PERIODS
This aircraft requires an Annual Conditional Inspection and
maintenance of proper documentation in logbooks and / or maintenance
records. The original inspection was May 2012. A checklist for the
Annual Conditional Inspection is toward the end of this section.
8-3.
PREVENTATIVE MAINTENANCE
The holder of a pilot certificate issued under Federal Aviation
Regulations *FAR) Part 61 may perform certain preventive maintenance
as defined in the FARs. This maintenance may be performed only on
an aircraft which the pilot owns and operates and which is not used in
air carrier or air taxi/commercial operations service. Therefore, this
paragraph applies to owners after Phil Conway.
All other aircraft maintenance must be accomplished by a person or
facility appropriately certificated by the FAA to perform that work. In the
case of N11HC, it includes Philip Conway.
Anytime maintenance is accomplished, an entry must be made in the
appropriate aircraft maintenance records. The entry shall include:
 The date the work was accomplished
 Description of the work
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Section 8 – Handling, Servicing & Maintenance
8-5
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
 Number of hours on the aircraft
 The certificate number of the pilot performing the work
 Signature of the individual doing the work.
8-4.
AIRPLANE PAPERWORK
The owner or pilot is required to ascertain that the following Aircraft
Papers are in order and in the aircraft. N11HC’s paperwork is kept in
the 8.5x5.5 3-ring notebook which is kept on the hat rack.
 Aircraft Airworthiness Certificated Form FAA-8100-2. Displayed
under the clear plastic of the outside front cover so it is viewable
without moving the note book.
 Operating Limitations letter from DAR
 Aircraft Registration Certificate Form FAA-8050-3
 Aircraft Radio Station License if flown outside the USA
 This POH which includes current:
o Weight and Balance data (Section 6 of this POH)
o Minimum Equipment list (Section 2 of this POH)
o Copy of the latest Repair and Alteration Form FAA-337, if
applicable.
Although the aircraft, engine and propeller logbooks are not required to
be in the aircraft, they should be made available upon proper request.
Logbooks should be complete and up to date. Good records will give
information about what has or has not been accomplished.
8-6
Section 8 – Handling, Servicing & Maintenance
08-10-2013
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
8-5.
GROUND HANDLING
8-5.1.
Tire Inflation
Use 35-50 PSI on Mains and 50 PSI for Nose gear.
Tire pressures should always be checked with the tire at ambient
temperatures. A temperature change of 5°F (3°C) produces
approximately one percent (1%) pressure change. It can take up to 3
hours or more after a flight for tire temperatures to return to ambient.
If all tires are normally at 50 psi this would require a 1 psi increase
above 50 psi for every 10° F expected decrease in temperature. This
applies to either at the destination or from a heated hangar to local
conditions.
The mains on N11HC are usually kept closer to 35 psi do to tire ware.
8-5.2.
Towing
The airplane can be moved on the ground by the use of the nose wheel
steering bar or power equipment that will not damage or excessively
strain the nose gear steering assembly. A tow bar is stored behind the
seat. Towing receptacles are incorporated into the nose gear.
There is a towing adaptor pin located in the battery area storage
compartment that will let a universal towbar attach using the Beechcraft
setting.
If pushing the aircraft backwards without the nose wheel steering bar,
the nosewheel will caster to its turn limits.
CAUTION
When towing with power equipment, do not turn the nose gear
beyond its steering radius in either direction, as this will result
in damage to the nose gear mechanism.
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Section 8 – Handling, Servicing & Maintenance
8-7
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
8-5.3.
Parking
When parking the airplane, be sure that it is sufficiently protected from
adverse weather conditions and that it presents on danger to other
aircraft. When parking the airplane for any length of time or overnight, it
is suggested that it be moored securely.
 To park the airplane, head it into the wind if possible.
 Set the parking brake by applying toe-brake pressure then pull the
parking brake knob. To release the parking brake, push the parking
brake knob in.
CAUTION
Care should be taken when setting brakes that are overheated
or during cold weather when accumulated moisture may
freeze a brake.
 Aileron and ruder controls should be secured with control locks kept
with the towbar adaptor. Chocks should also be used to properly
block the wheels. The seatbelt can be used to lock the elevator.
8-5.4.
Mooring
Wing and tail tiedown rings are stored behind the battery.
The airplane should be moored for immovability, security and
protection. The following procedures should be used for the proper
mooring of the airplane:
 Head the airplane into the wind if possible.
 Retract the flaps
 Immobilize the ailerons and elevator by looping the seat belt around
the control stick and pulling snug.
 Chalk the wheels
 Secure the rudder
8-8
Section 8 – Handling, Servicing & Maintenance
08-10-2013
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
 Secure tie-down ropes to the wing tie-down
rings and to the tail skid at approximately 45°
angles to the ground. Tie-down rings are
usually kept in the small storage area below the
baggage compartment. When using rope of
non-synthetic material, leave sufficient slack to
avoid damage to the airplane should the ropes shrink while drying
out.
CAUTION
Use bowline knots, square knots or locked slip knots. Do not
use plain slip knots.
 Install the pitot tube cover
 Close and lock the doors
8-6.
ADDITIONAL ITEMS TO CHECK DURING OIL CHANGES
 Air Filter
 Brake Fluid and Pads
 Tire Pressure
8-7.
OIL REQUIREMENTS
 Change the oil every 50 hours or 4 months – whichever is less.
 Minimum oil level is 2 quarts to prevent engine damage and 5.5
quarts for takeoff.
 Use 15W-50 or 20W-50 oil
8-8.
FUEL REQUIREMENTS
8-8.1.
Fuel Grade
See “FUEL / Fuel Grade” paragraph in section 2 of this POH. Normal
fuel is 100LL (blue) Aviation grade fuel
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Section 8 – Handling, Servicing & Maintenance
8-9
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
8-8.2.
Draining Fuel Strainer, Sumps and lines
The fuel system sumps and strainer should be drained daily prior to the
first flight and after refueling to avoid the accumulation of contaminants
such as water or sediment.
 The wing tank drain is located in the center of the fuselage
 The header tank drain is located near the left wing’s leading edge
 The strainer drain is located near the right wing’s leading edge
8-9.
ADVISORY PUBLICATIONS
AD’s, Service Bulletins, Service Letters and Advance Notices of
Revisions are located in the Advisory Publications area of the Glasair
website. This includes certified equipment on the airplane and
advisories from Glasair.
Usually, the Glasair advisories published before 8 Sept 1994 are not
applicable because they would have been incorporated in N11HC’s
September 1994 kit. The last addition to this list was May, 7 2007. The
list will be revisited during each Annual Condition Inspection.
A sorted listing of Service Bulletins applicable to N11HC are in the
Advisory Publications area of the N11HC website. All have either been
accomplished, incorporated into the Condition Inspection Checklist or,
just not applicable. A complete list of Service Bulletins that do and do
not apply are on this linked Excel spreadsheet.
Service Letters with any applicability to N11HC have been considered.
There are no relevant Advance Notices of Revisions for N11HC.
8-10
Section 8 – Handling, Servicing & Maintenance
08-10-2013
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
8-10.
CONDITION INSPECTION CHECKLIST
Date Started:
Date Completed:
Hobbs Start:
Hobbs End:
Pay Minnesota’s Tax
Last/prior annual inspection completed on ___________ at _________hrs.
This annual inspection procedure details a complete and thorough
inspection of the entire airframe, engine and all systems. It is a
recommended guide only. If the regular 50 and 100 hour inspections are
complied with then many of the inspection items and tasks in this document
are redundant and need not apply. These items are noted with an "if
required" comment.
8-10.1.




Service Lives
Main Alternator ....................................................................................... 2000 Hours
Standby Alternator ................................................................................. 1700 Hours
Regulator (Main Alternator) LR3C-14 ....................................................... Indefinite
Regulator (Standby Alternator) SB1B-14 ................................................. Indefinite
8-10.2.
Inspection Times
 Starter ......................................................................................................... 50 Hours
8-10.3.
Advisory Publications, AD’s etc.
 See N11HC Advisory Publications website for list of items to check ....................□
8-10.4.
Parts & Supplies
Parts & Supplies Required For Condition Inspection:
 Hartzell Propeller Owners Manual..........................................................................□
 Lycoming Service Bulletins & Letters (see section IX-A )......................................□
 Oil, Oil Filter (CH-48110) ........................................................................................□
 Oil Analysis Kit ........................................................................................................□
 Filter Wrench, Drain Hose, Trash Bag ...................................................................□
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Section 8 – Handling, Servicing & Maintenance
8-11
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
























Fuel Filter: Fram HPGC1 (NAPA p/n: 3900R), .....................................................□
Filter Bowl Retaining Bolt Stat-a-Seal Washer (S-H p/n: 620-7500-038 ) ............□
Fuel Lube Lubricant (for above washer). ...............................................................□
Bracket Air Filter Element p/n: BA-23 (or entire filter assy BA-110)......................□
Aeroshell 6 Grease (Prop Hub Lube) (if required) .................................................□
Grease Gun (Prop Hub) (if required) ......................................................................□
Wheel Bearing Grease (Blue).................................................................................□
LPS-2 Lubricant or Tri-Flow non-drying penetrating lube. .....................................□
Degreaser Solvent/Cleaner (cowling/engine compartment) ..................................□
Injector Servo Fuel Inlet Fitting Oring (may not be needed - check before
reinstalling) ..............................................................................................................□
.032 Stainless Steel Safety Wire (prop bolts). .......................................................□
Brake Pads (Cleveland #66-106), Rivets, Rivet Tool (if required) ........................□
Torque Wrench .......................................................................................................□
Air Compressor, Hose & Filtered Nozzle ...............................................................□
Tire Pressure Gage.................................................................................................□
Differential Compression Tester .............................................................................□
Magneto Timing Box ...............................................................................................□
Slick Mag Timing Lock Pin (if mags are to be removed for inspection/servicing) .□
Angle Finder (Elevator, Aileron & Flap travel) ........................................................□
Rudder Travel Jig....................................................................................................□
Misc Screws: AN509-10R10 (MS24694-S52) Belly Pan; Wing Tip:S56, S57,
S58 ..........................................................................................................................□
Part Cups/cans/small boxes ...................................................................................□
4 Small jars or cans with tops for soaking fuel injectors. .......................................□
12 mm box wrench or socket for starter terminal nut.............................................□
8-10.5.
Pre Condition Checks & Prep
Preliminary Condition Checks & Preparation
8-10.5.1. Engine Run-up:
 Start the engine and warm it up thoroughly. Check the following: Note
OAT:________ ........................................................................................................□
 Set parking brake and run engine at 2000 RPM for the following checks: ...........□
 Left magneto drop (switch to L position):_______rpm. .......................................□
 Right magneto drop (switch to R position):________rpm. ....................................□
8-12
Section 8 – Handling, Servicing & Maintenance
08-10-2013
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
 Propeller control and governor action (do not exceed 500 RPM drop). ................□
 Oil Temp:_______
Oil Pressure: Idle (800 rpm):________
2000
rpm:_______ .........................................................................................................□
 Static RPM - Idle:______ .......................................................................................□
 Main Alternator output - Idle: Voltage: _________
Amps: _________ ........□
 Secondary Alternator output - Idle: Voltage: _________
Amps: _________□
 Parking brake - operation and will hold at 2000 rpm. ............................................□
 Magneto ground: Shutoff engine with key switch. Warning: let engine come to a
complete stop - do not turn key on or a backfire will occur and damage the
exhaust! Be sure to restart engine and shut down with mixture cut-off to insure
no combustible fuel remains in the cylinders which would create a serious prop
hazard. ....................................................................................................................□
 Remarks:
8-10.5.2. Engine In Flight Checks:
 Prepare for take-off. Perform the following in-flight checks: ..................................□
 Take Off Roll - Full throttle RPM: ________ Manifold Pressure:_________ ......□
 Check engine operation on all fuel selector valve positions (__Header, __Left,
__Right) ...................................................................................................................□
 Alternator full load output - (2000 rpm min): Volts: _________ Amps:________
** ..............................................................................................................................□
 ** Full load output: check with all equipment turned on: Nav lights, Strobe Lights,
Landing Lights, Interior Lights, Fuel Pump, Pitot Heat, All Avionics & COM Xmit.
Cycle gear (in-flight only!) and operate flap motor to draw maximum current. ....□
 Check cabin heat and defrost functioning properly. ...............................................□
 Note OAT:_________ Cruise Oil Temp:_________ Max Climb Oil
Temp:_________ ....................................................................................................□
 Oil Pressure (Hot, 2400 RPM):_____________ ....................................................□
 Accomplish Flight Test Profile items from Jan 2012 Sport Aviation ......................□
 Return to airport & land. ..........................................................................................□
 Mixture cutoff RPM rise at idle:_______ ................................................................□
 Check functioning of ELT - 1st 5 min of the hour: Trigger for 3 cycles max.
Listen on 121.5 .......................................................................................................□
 Remarks:
08-10-2013
Section 8 – Handling, Servicing & Maintenance
8-13
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
8-10.5.3. External Lights





External Lights - Check security and operation - Prior to removing cowling. ........□
Nav Lights - Left (red):_______ Tail (white):_______ Right (green):_______□
Strobe Lights - Left: _______ Right:_______ Tail: _________ .......................□
Landing/Taxi Light: ______ WigWag Lights:_______ .......................................□
Remarks:
8-10.6.
Powerplant and Propeller
8-10.6.1. Engine Compression Check
While engine still Hot (if required):








Remove the engine cowl and check for leaks and stains. .....................................□
Secure oil cooler to fuse/cowl hinge with temporary mounting fixture. .................□
Check engine for any Oil Leaks or Fuel Leaks ......................................................□
Perform compression check per Lycoming Service Instruction 1191-A ................□
#1:
#2:
#3:
#4: ......................□
Record results in Engine Log Book. ....................................................................□
Last (prior) Compression Check @__________ hrs. ............................................□
Remarks:
8-10.6.2. Engine Oil & Filter
Engine Oil & Filter Change, while engine still Hot (if required):





Drain oil & replace spin-on filter. Take oil sample for analysis. .............................□
Safety wire filter. .....................................................................................................□
Refill with new oil. ...................................................................................................□
Last (prior) Oil & Filter Change @_________hrs. .................................................□
Remarks:
8-14
Section 8 – Handling, Servicing & Maintenance
08-10-2013
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
8-10.6.3. Plugs
Plug Rotation Cleaning & Gapping (if required):
 Clean, Gap & Rotate spark plugs (Gap .016-.022)- note measured plug gap as
removed. .................................................................................................................□
[ ]1T<-->4B
1T Gap:
4B Gap:
[ ]2B<-->3T
2B Gap:
3T Gap:
[ ]1B<-->4T
1B Gap:
4T Gap:
[ ]2T<-->3B
2T Gap:
3B Gap:
 Check ignition harness for breaks; check cigarettes and contact springs. ...........□
 Clean cigarettes and contact springs with alcohol - (do not touch springs with
fingers) ....................................................................................................................□
 Re-install spark plugs (420 in-lbs/35 ft-lbs) ............................................................□
 Re-install ignition leads. Torque lead nuts 80-90 in-lbs max (dry). .......................□
 Last (prior) Plug Rotation & Cleaning @__________hrs. .....................................□
 Remarks:
8-10.6.4. Magnetos
Magnetos: 100 hr Inspection (if required):
See Slick service manual for 500 hr inspection, removal & service. .................... □
 Inspect security of mounting bolts & Ignition harness cap. ...................................□
 Check security of P-leads (15 IN-LBS MAX) and check wires for breaks or frays.□
 Check security of Mag ground wires and check wires for breaks or frays. ...........□
 Check and adjust magneto timing per Lycoming: 25 deg BTDC (if not recently
done). ......................................................................................................................□
 Note timing - LEFT Before:______ After:______ Right Before_______
After:_______..........................................................................................................□
 Torque magneto clamp down nuts to 17 ft-lbs (204 in-lbs) max or the flange may
become permanently damaged. .............................................................................□
 Last (prior) Mag 100 hr inspection @_________ hrs. ...........................................□
 Remarks:
08-10-2013
Section 8 – Handling, Servicing & Maintenance
8-15
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
8-10.6.5. Engine Controls:
Check the following controls for security, full range of travel, interference, rubbing
or chafing of the control linkage/arms through the full range of travel. .............................. □
 Lubricate if necessary. ............................................................................................□
 Throttle. ...................................................................................................................□
 Mixture.....................................................................................................................□
 Prop pitch control. ...................................................................................................□
 Inspect each mounting clamp and cable housing end keeper for wear or
looseness. Replace any aluminum keeper with a steel keeper if it shows signs
of wear from vibration. ............................................................................................□
 Remarks:
8-10.6.6. Fuel System:
 Drain the fuel tank sumps and check for contaminants. Remove and clean the
fuel sump strainers (finger screens) if excessive contamination is apparent. .......□
 Inspect & replace fuel filter element & Stat-O-Seal washer. Lube Stat-o-Seal &
bolt
with thin film of fuel lube to prevent rubber seal damage. Safety wire filter
bowl bolt. .................................................................................................................□
 Remove and clean injector servo body fuel inlet screen. Replace o-ring if
necessary. ...............................................................................................................□
 Check fuel flow through fuel line with electric fuel pump ON. ...............................□
 Remove fuel injectors - use 6 point socket. Identify cylinder and keep separate.
- Do not mix injectors or components. ..............................................................□
 Clean Fuel Injector Nozzles w/ Hopps #9 to remove all gum and varnish.
DO NOT SOAK MORE THAN 1 HOUR! ..........................................................□
 Re-install Fuel Injector Nozzles - do not use thread sealant.
Re-torque injectors to 60 in-lbs using 6 point long reach socket.......................□
 Torque injector line B-nuts to 25-50 in-lb max. Do Not Over Tighten. Per SB
1414A ......................................................................................................................□
 Last (prior) Fuel Injector Check & Cleaning done at @_________ hrs;
date:___________ ..................................................................................................□
 Remarks:
8-16
Section 8 – Handling, Servicing & Maintenance
08-10-2013
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
8-10.6.7. Engine & Accessories:
General Engine Compartment and Engine Accessories:
 Inspect alternator: mounting, wiring, terminals for security and condition. ...........□
 Check field connector plug and grip of connectors on spade terminals. Pinch
down female connector for firm/tight sliding grip on male spade terminals if
required. ..................................................................................................................□
 Inspect alternator belt and adjust tension, if needed. ............................................□
 Inspect starter: mounting bolts, wiring & terminals for security & condition. .........□
 Remove cabin heat muff scat hoses and check exhaust for cracks. (Soot on the
inner surface of the heat muff indicates a crack). Remove the heat muff from
the exhaust pipe for further inspection if any trace of exhaust soot is found
indicating a crack exists. .........................................................................................□
 Carefully inspect all welded exhaust joints paying close attention to the welded
"Y" joints. .................................................................................................................□
 Check exhaust springs & safety wire, gaskets and shrouds for security and
cracks. .....................................................................................................................□
 Check cylinder baffles for cracks and proper seal. ................................................□
 Check engine mount and braces for security, rust, chafing, cracks & condition of
rubber bushings and bonding straps. .....................................................................□
 Check engine mount to firewall securing bolts. Torque to 200 in-lbs min. Note
that these become loose over time due to heating of the fiberglass firewall
mounting surface allowing it to shrink and/or compress. .......................................□
 Check engine for loose nuts, bolts and screws. **Check Acc. Case Ground Lug
Bolt** .......................................................................................................................□
 Check oil cooler and lines for security, chafing, signs of leaks and obstructions. □
 Check all breather and overboard lines for security and obstruction.1 .................□
 Inspect injector body, fuel pump and fuel filter fuel lines for security and leaks. .□
 Check fuel distributor/fuel injector fuel lines for cracks, nicks, sharp bends or
leaks. .......................................................................................................................□
 Inspect cabin heat box and control for security. Check hoses for security and
leaks. .......................................................................................................................□
 Inspect manifold pressure hose from cylinder fitting to firewall fitting for security,
chafing and leaks. ...................................................................................................□
 Inspect the induction air filter and clean with compresssed air. Replace if it is
difficult to see light through it due to foreign material or if it has been in service
08-10-2013
Section 8 – Handling, Servicing & Maintenance
8-17
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop









for 12 months or 200 hours since last replacemen (per Brackett Instructions).
BA-110 assy; BA-23 Element. ................................................................................□
Clean engine and cowling, using a suitable solvent or degreaser to remove all
traces of oil, soot, dirt and fuel stains. ....................................................................□
Check cowling for chafing, cracks or heat damage. ..............................................□
Check taxi & landing lights for security. Check wire terminal connections snug. .□
Top up brake fluid reservoir, leave an air space for fluid expansion. ....................□
Check engine for any loose hardware and tools that may have been left in the
engine compartment during maintenance. .............................................................□
Check the main alternator externally for security of mounting and wiring. Belt
tension should be checked by making sure that the alternator pulley may not be
rotated by hand inside the belt. Alternately, approximately 50 Lbs. belt tension
may be used. The belt should be checked for cracking or fraying and replaced if
these conditions are found. (IAW B&C) .................................................................□
Check the Standby alternator externally for security of mounting and wiring (IAW
B&C) ........................................................................................................................□
Check the main and standby regulator (LR3C-14) (SB1B-14) externally for
security of mounting, tightness of terminal screws, and chafing or breakage of
wiring. (IAW B&C). Hyperlink also has info on the calibration of the SB1B-14. ...□
Remarks:
8-10.6.8. Propeller and Spinner
Propeller and Spinner (grease only if > 100 hrs since last grease):
 Remove propeller spinner and check spinner, front plate and back plate for
security and cracks. ................................................................................................□
 Inspect propeller track. ..........................................................................................□
 Check blades for nicks. Repair nicks per Hartzell Propeller Owners Manual. ......□
 Remove mounting bolt safety wire. Check torque of mounting bolts (60-70 ftlbs). Resafety bolts with .032 Stainless Steel safety wire. .....................................□
 Grease propeller hub. Aeroshell 6 per Hartzell Prop Manual No. 115N Rev 5 pg
605-606. Remove the rubber lubricaps from all four fittings (pull off - do not
remove safety wire). Remove the engine-side (rear) fitting from each blade
socket. Remove any hardened grease with safety wire. Pump 1 fl.oz grease
(maximum) into each cylinder-side (front) fitting, or until grease emerges from
the opposite hole where the fitting was removed - whichever occurs first. Note:
8-18
Section 8 – Handling, Servicing & Maintenance
08-10-2013
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
one (1) ounce grease is aprox 6 pumps on hand held grease gun. DO NOT
USE AIR AN ASSISTED GREASE GUN. ..............................................................□
 Reinstall spinner. Do not over tighten spinner screws. .........................................□
 Make an entry in propeller log book of this inspection and any maintenance
performed. ...............................................................................................................□
 Remarks:
8-10.6.9. Ground Run-up Check
Ground Run-up Check (After Engine Maintenance Completed):
 Start the engine and warm it up thoroughly. Check the following: Note
OAT:________ ........................................................................................................□
 Set parking brake and run engine at 2000 RPM for the following checks: ...........□
 Check engine operation on all fuel selector valve positions (__Header, __Left,
__Right) ...................................................................................................................□
 Left magneto drop (switch to L position):_______rpm. .......................................□
 Right magneto drop (switch to R position):________rpm. ....................................□
 Propeller control and governor action (do not exceed 500 RPM drop). ................□
 Suction Gage Vacuum: @Idle:______ 1000
rpm:_______1400:_______2000:_______ ............................................................□
 Oil Temp:_______
Oil Pressure: Idle (800 rpm):________
2000
rpm:_______ .........................................................................................................□
 Static RPM - Idle:______ .......................................................................................□
 Main alternator output - Perform an operational test to determine that the main
alternator maintains the aircraft electrical bus at the approximate regulator set
point as loads are added and removed (at high loads, cruise RPM may be
required). .................................................................................................................□
 Standby alternator -- perform the before takeoff test described under the “Final
Test” described in the B&C installation drawing. ...................................................□
 Main Alternator Regulator -- check to determine that the regulator maintains the
aircraft electrical bus at its approximate set point as loads are added and
removed (at high loads, cruise RPM may be required). ........................................□
 Parking brake - operation and will hold at 2000 rpm. ............................................□
 Magneto ground: Shut off engine with key switch. Warning: let engine come to a
complete stop - do not turn key on or a backfire will occur and damage the
exhaust! Be sure to restart engine and shut down with mixture cut-off to insure
08-10-2013
Section 8 – Handling, Servicing & Maintenance
8-19
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
no combustible fuel remains in the cylinders which would create a serious prop
hazard. ....................................................................................................................□
 Mixture cutoff RPM rise at idle:_______ ................................................................□
 After engine shut-down, carefully check for any oil or fuel leaks. .........................□
 Remarks:
8-10.6.10.
Cowling Installation
 Replace Taxi and/or Landing Lights if necessary. ................................................□
 Adjust taxi and landing light positions if required. ..................................................□
 Pre-Cowling Check: ...............................................................................................□
o Check: Oil cooler secure w/ pins & safety screws. ...........................................□
o Check: Taxi/Ldg Light Connectors ....................................................................□
o Check: Side Hinge Pins Secure .......................................................................□
o Check: Induction SCEET Tube Secure - No Rips. ...........................................□
o Check: Lower Cowling Screws ........................................................................□
 Reinstall upper cowling. Check all screws secure. ............................................□
 Verify operation of Taxi & Landing Lights ..............................................................□
 Remarks:
8-10.7.
Cabin & Fuselage
8-10.7.1. Interior Lighting
Interior Lighting (prior to removing interior component & console):






Baggage Compartment/Interior Flood Light ...........................................................□
Map/Reading Lights ................................................................................................□
Panel Flood Lights ..................................................................................................□
Instrument Post Lights & Dimmer ...........................................................................□
Internal Instrument Lights & Dimmer ......................................................................□
Remarks:
8-20
Section 8 – Handling, Servicing & Maintenance
08-10-2013
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
8-10.7.2. General Cockpit Inspection
 Check instruments for security, legibility and markings. ........................................□
 Check the fuel tank gauges and senders, if applicable, for proper markings,
indication, and freedom of movement. ...................................................................□
 Check the compass for discoloration, compass card displayed. ...........................□
 Check the circuit breakers and switches for security and condition. .....................□
 Check all Plexiglas for cracks. ................................................................................□
 Check canopy hinges and latches for security. Lubricate as required. .................□
 Test Standby ADI Backup Battery IAW Users Guide (pg 2) ..................................□
(Once a year a complete function test of the backup battery system is recommended:
Activate the ADI backup battery and confirm LED is illuminated. Continue in this mode, note the
time of activation and confirm minimum one hour function of the ADI.
If function time is less than one hour then remove backup battery and charge on the bench for a
minimum of eight hours and retry function test above.)
 Remarks:
8-10.7.3. Canopy Latch & Lock Mechanisms
 Remove inside canopy latch handle covers ...........................................................□
 Check actuator bars secure, cir-clips & safety wire secure - not flopping over
pin. ...........................................................................................................................□
 Check security & operation of lock mechanism - clears safety wire loop. ............□
 Check for excessive free-play & rattling of actuator bars. .....................................□
 Lubricate mechanism pivot points and pins with graphite lube. ............................□
 Check mill-fiber handle stop pad is secure - not fractured off canopy frame. .......□
 Remarks:
8-10.7.4. Interior Panel Removal
 Remove: wing attach bracket black covers, overhead console, center console,
baggage bulkheads, rear control tunnel top, carpets, heal rests, seat pans, belly
pan, and gear doors (as necessary).......................................................................□
 Check all seat pan screws - discard & replace screws with chewed heads (they
will wear holes in leather seat cushions) ................................................................□
08-10-2013
Section 8 – Handling, Servicing & Maintenance
8-21
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop




Check the seat pans for cracks or stress marks. ...................................................□
Check the seat belts and shoulder harnesses for security and condition. ............□
Check the wing attach bolts and fittings for security, integrity and safety. ............□
Remarks:
8-10.7.5. Forward Cabin Checks
Fwd cabin - Instrument Panel & Forward, Header Tank, Firewall.
 Check the pitot tube line and static line plumbing and fittings behind the panel. .□
 Check all instrument wiring and plumbing for security and chafing behind the
panel........................................................................................................................□
 Check radio equipment, wiring & antenna connectors for security & proper
connection. ..............................................................................................................□
 Check all cabin ground bus terminal screws tight. .................................................□
 Check all EPI-DPU wire terminal connections snug. Do not over tighten. ............□
 Check the fuel tank, fuel lines, vent lines and fuel standpipes and fittings behind
the panel for security, leaks or contaminants also check all lines and fittings in
the seat pan area and where they pass thru the lower center panel and console.□
 Inspect engine mount points on the aft side of firewall for cracks or stress marks
in the fiberglass. ......................................................................................................□
 Check & tighten Main Bus power feed terminals & Alternator fuse bolts/nuts on
copper bus bar on aft firewall - co-pilot side. .........................................................□
 Check Main Bus Power feed terminal stud bolt is tight (behind breaker panel
section on upper fuselage next to cabin ground bus bar. ......................................□
 Check all Cabin Ground Bus Bar terminal connections are tight. .........................□
 Inspect parking brake cable, cable keeper, security and operation. .....................□
 Check the brake master cylinders and brake line fittings for leaks. ......................□
 Check all brake pedal and cylinder pivot points free with no excessive wear or
free play...................................................................................................................□
 Verify all brake pedal and cylinder pivot bolts/nuts properly cotter-pinned and
secure......................................................................................................................□
 Lubricate brake cylinder pivot points with a light lubricant.....................................□
 Remarks:
8-22
Section 8 – Handling, Servicing & Maintenance
08-10-2013
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
8-10.8.
Control System Inspection
Inspect the following control system components: pushrods, rod end bearings,
cable and linkages for corrosion, safety, security and chafing. Clean and lubricate
all rod-end bearing surfaces, pulleys and gears as necessary. Check the following
systems:
 Aileron system.........................................................................................................□
o Check rod end bearings & jam nuts tight. ...........................................................□
o Check control stick pivot not binding and not loose. ..........................................□
o Check control stick wires not being pinched or binding. ....................................□
o Remove aileron counterweight assemblies and inspect for rust inside tubes
IAW Glasair Service Bulletin #153 ..................................................................... □
 Elevator system (seat pan area, see section II-I for rear control tunnel & aft fuse
area): .......................................................................................................................□
o Check rod end bearings & jam nuts tight on both control tubes. Check tubes
are free and clear with no interference or rubbing on wires, cables etc.
through full range of travel. .................................................................................□
 Trim system:............................................................................................................□
o Check trim cables for any wear, rubbing or binding. ..........................................□
o Check trim cable pullys for free rotation. Check for excessive wear or cable
cuts. .....................................................................................................................□
o Inspect trim spring tension: ................................................................................□
o Inspect each trim cable ferrel for wear and carefully inspect each nico-press
sleeve for signs of slippage - at both the spring end and the control arm end. .□
o Lubricate trim box shafts & gears with graphite lubricant. .................................□
 Rudder system: .......................................................................................................□
o Inspect rudder cables for any wear, rubbing or binding throughout full range of
travel. ...................................................................................................................□
o Check rudder cable pulleys for free rotation. Check for excessive wear or
cable cuts.............................................................................................................□
o Check rudder cable NicoPress swages for corrosion IAW SB152 ....................□
o Check rudder return springs and attach bracket. Inspect spring attach holes
for wear. ...............................................................................................................□
o Lubricate hinge pin and between hinge knuckles with an appropriate grease
lubricant while holding rudder up to open the lower hinge knuckle gaps on
bottom side for grease. .......................................................................................□
o Verify that the rudder hinge is properly safetied and bracket is secure. ............□
 Flap system: Note: Lube flap actuator linkages and pivot points. ........................□
o Inspect flap motor attach and pivot points for security. ......................................□
08-10-2013
Section 8 – Handling, Servicing & Maintenance
8-23
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
o Inspect flap actuator linkage for security with all pivot bolts/nuts cotter pinned.□
o Check linkage free from binding, interference and rubbing on wires, hoses etc.
through the full range of travel. ...........................................................................□
o Check the flap/gear warning cam and micro switch for security. .......................□
o Lubricate the flap linkage with a light lubricant. ..................................................□
 Remarks:
8-10.8.1. Under Seat Pan Area
Seat Pan Area - Fuel Lines & Wiring
 Check the operation of the fuel selector valve. Remove, disassemble and
lubricate if necessary. Check the handle position markings on the console
overlay. ....................................................................................................................□
 Check all fuel lines for leaks, security and chafing in the seat pan area. ..............□
 Check all wiring bundles for security and chafing. .................................................□
 Check wiring terminal blocks for security & check each screw terminal is
tight/secure. .............................................................................................................□
 Inspect gear brackets for corrosion (see website for example pictures) ...............□
 Remarks:
8-10.8.2. Battery inspection:
 Inspect and clean the battery terminals if necessary. Check all terminal
connections on battery master contactor. ..............................................................□
 Inspect and clean the battery box (if installed).......................................................□
 Check the electrolyte level and top up if applicable. ..............................................□
 For an enclosed battery box, inspect the drain tube and vent lines for damage
and obstructions if applicable. ................................................................................□
 Note: Replace the battery every 3 years to guarantee maximum performance
and reserve capacity. 3 years max or at first sign of poor cranking power. ..........□
 Remarks:
8-10.8.3. Control Tunnel Area
 Check all wire bundles secure & not chafing. ........................................................□
8-24
Section 8 – Handling, Servicing & Maintenance
08-10-2013
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop




Check fuel vent lines & fittings secure, not rubbing or loose. ................................□
Check all cables & control tubes free of interference. ...........................................□
Check NicoPress sleeves on cables IAW Glasair Service Bulletin #152 ..............□
Remarks:
8-10.8.4. Aft Fuselage Area:










Check static tube security and connection to static ports & tee. ...........................□
Check ELT Battery replacement date (on back of battery):_________ ................□
Verify ELT switch set to ARMED. ...........................................................................□
Check Transponder Antenna secure. ...................................................................□
Remove transponder antenna connector, check for corrosion, clean & reconnect. ...................................................................................................................□
Check aft elevator control tube secure, jam nuts tight ...........................................□
Check rudder bell-crank, cable clevis's & rudder pushrod secure. .......................□
Check Trim cables & pullys free, not worn & nico press crimps secure. Be sure
to check all cables & sleeves including at the elevator control horn with light &
mirror. ......................................................................................................................□
Lubricate rudder cable clevis's & all rod ends as necessary. ................................□
Remarks:
8-10.9.
External Fuselage & Belly Pan
8-10.9.1. Control Surfaces & Rigging
 Check the stabilizer for security and cracks. ..........................................................□
 Check elevators for security: ..................................................................................□
o Check hinges & hinge bolts tight. .......................................................................□
o Check elevator hinge pivot bolts secure. ............................................................□
o Check elevator pivot points for excessive bushing wear and excessive side
play. .....................................................................................................................□
o Check elevator control horn secure between elevators: No up/down
movement between the left and right elevators when moved independently by
the trailing edges. ................................................................................................□
 Check the elevator counterweights for cracks or any signs of rubbing. ................□
 Lubricate the elevator hinge bushings with a graphite lubricant. ..........................□
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Section 8 – Handling, Servicing & Maintenance
8-25
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
 Remarks:
8-10.9.2. Low Checks
Under wing/belly-pan wiring, plumbing and hardware check:
 Check all hydraulic lines & brake lines that run under the wing for security,
leaks, chafing, corrosion and general condition. ....................................................□
 Check all hydraulic manifold fittings for signs of leaks. Check aft edge of wing
for signs of hydraulic fluid indicating a hydraulic leak somewhere. .......................□
 Check all antenna cables for security, proper routing and general condition. ......□
 Check battery cables security, proper mounting clamps, any chafing, condition,
etc. ...........................................................................................................................□
 Check static system tubing for security, proper mounting, abrasion and
condition. .................................................................................................................□
 Remarks:
8-10.10. Wings & Control Surfaces:




Remove all inspection covers and remove the wing tips. ......................................□
Check the wing tips for cracks and stress marks. ..................................................□
Check all wiring and plumbing for chafing and security. Fuel vent lines secure. ..□
Check all control rods, rod ends and bell cranks for corrosion, safety, security
and chafing:.............................................................................................................□
o Aileron bell cranks secure with full freedom of movement at full elevator
up/down. ..............................................................................................................□
o Aileron control rod ends & jam nuts tight ............................................................□
o Aileron counter weights secure ...........................................................................□
o Remove aileron counterweights and inspect inside tubing for corrosion
(SB#______) if aircraft has been flown in rain or tied down outside. Check for
corrosion every 2 yrs min. ...................................................................................□
 Check the flaps, ailerons and rudder for full freedom of movement (and proper
travel *): ...................................................................................................................□
o Ailerons: 19 deg down, 21 deg up (+/- 1 deg.) Left:_____________
Right:___________ .............................................................................................□
o Flaps: 0 to 40 degrees down (slotted flaps) Full down travel:____________ □
8-26
Section 8 – Handling, Servicing & Maintenance
08-10-2013
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop










o Elevator: 18 degrees down, 30 degrees up.
Measured:________________________...........................................................□
o Rudder: 24 degrees left, 25 degrees right (+/- 1 deg.)
Measured:_______________ .............................................................................□
*Note: Check travel if any control system has been removed or adjusted
since last check.
Check all vent and drain holes in control surfaces are free and unobstructed. ....□
o Ailerons ................................................................................................................□
o Flaps ....................................................................................................................□
o Elevators ..............................................................................................................□
o Rudder .................................................................................................................□
Inspect & lubricate hinges: (Do NOT use graphite on piano hinges!!) ..................□
o Aileron hinges: Check for security and wear. Lubricate with non-drying
penetrating lube. ..................................................................................................□
o Flap hinges: Check for security and wear. Lubricate with non-drying
penetrating lube. ..................................................................................................□
o Rudder hinge: Lubricate hinge pin and between hinge nuckles with grease or
non-drying lubricant while holding rudder up to open hinge nuckle gaps on
bottom. **See above** ........................................................................................□
o Verify that the rudder hinge is properly safetied. ................................................□
Check the wing skins, the leading edge and the wheel wells for cracks, stress
marks and delamination..........................................................................................□
Check the fuel tank, the fuel lines, vent lines and wing tank end rib ground studs
at each wing tip for security, leaks or contaminants. .............................................□
Check the fuel filler caps for proper labeling: .........................................................□
Check all drain and vent holes for obstructions. ....................................................□
Check inside the wings for loose hardware tools or any other FOD. ....................□
Check pitot tube mounting, wiring and hose connection. Check mounting screws
tight. .........................................................................................................................□
Reinstall the inspection covers and wing tips. .......................................................□
Remarks:
8-10.11. Landing Gear
 Check the main tires for cracks, wear and proper inflation. ..................................□
 Remove main wheels. Repack wheel bearings & inspect wheels for cracks and
corrosion..................................................................................................................□
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Section 8 – Handling, Servicing & Maintenance
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Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
 Inspect the brake discs for excessive scoring, the brake lines for leaks or
chafing and the brake pads for wear. Replace the brake pads if necessary.
Check the operation of the brakes and bleed them, if necessary. ........................□
 Check the nose gear shimmy damper for security. Inspect the damper clamps .
Tighten shimmy damper clamp bolts to increase damping friction if required. .....□
 Check inflation & condition of main tire. Replace if necessary. .............................□
 Remove Nose Wheel. Clean and re-pack wheel bearings. ...................................□
 Check the gear doors for damage and security of mounting. ................................□
 Lubricate flap actuator arm/rod clevis pins with a non-drying penetrating
lubricant. ..................................................................................................................□
 Remarks:
8-10.12. Post Maint Systems Check:
 Replace interior components. Check inside fuselage and seat pan areas for any
tools, rags or loose hardware prior to covering up. ................................................□
o Center Console, Seat Pans.................................................................................□
o Overhead Console ..............................................................................................□
o Control Tunnel Top..............................................................................................□
o Aft Baggage Bulkhead - Lower Verify ELT set to ARMED prior to installing
bulkhead. .............................................................................................................□
o Upper Baggage Bulkhead - Upper & Hat Shelf ..................................................□
o Carpets & Seat Cushions ....................................................................................□
o Battery Box/Cover ...............................................................................................□
 External Lights - Check security and operation: ....................................................□
o Nav Lights - Left (red):_______ Tail (white):_______ Right
(green):_______ ..................................................................................................□
o Strobe Lights - Left: _______ Right:_______ Vertical Tail __________ .....□
o Landing Light:_______ WigWag Lights:_______ ............................................□
 Interior Lighting: ......................................................................................................□
o Baggage Compartment/Interior Flood Light .......................................................□
o Map/Reading Lights ............................................................................................□
o Panel Flood Lights ...............................................................................................□
o Instrument Post Lights & Dimmer .......................................................................□
o Internal Instrument Lights & Dimmer ..................................................................□
 Remarks:
8-28
Section 8 – Handling, Servicing & Maintenance
08-10-2013
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
8-10.13. Post Maint In-Flight Checks:
Perform this check after all other inspections and service has been accomplished
and the aircraft is considered airworthy for a test flight.
 Take Off Roll - Full throttle RPM: ________ Manifold Pressure:_________ ......□
 Check cabin heat and defrost functioning properly. ...............................................□
 Remarks:
8-10.14. Paperwork
 Verify compliance with ALL known and applicable ADs for the engine or other
components.□
o Known recurring/repetitive SBs & ADs at time of this writing:............................□
o SB 518 - Thermostatic Bypass Valve (Oil) ........................................................□
o SB 466 - Oil Filter base Adapter Cracks ............................................................□
o SB 388B- Exhaust Valve & Guide Condition Check (Wobble Check) ...............□
 Check that all Stoddard Hamilton Service Bulletins are complied with. ................□
 Additional Inspection Items, Service Items, Replacement Items & Notes: ...........□
o Replace the DPU Battery every 2 years. (Note: new style battery may last 5
yrs?) .....................................................................................................................□
o Replace main 14v 25 amp-hr battery 36 months max. ......................................□
o Pitot Static System & Transponder Check - 24 calendar months. .....................□
o Air Filter - Replace Annually ...............................................................................□
o Fuel Filter - Replace Annually IAW SB’s 101, 130 and 150...............................□
 Make sure the following documents are present, current and properly displayed
if applicable
o Airworthiness Certificate .....................................................................................□
o Registration Certificate ........................................................................................□
o Weight and Balance ............................................................................................□
o Placards ...............................................................................................................□
o Radio Station License (Not required for flights within continental US) ..............□
 Logbook: make the appropriate log book entries, noting any discrepancies and
other pertinent information. Sign off the annual condition inspection as required
by the operating limitations imposed with the Experimental Airworthiness
Certificate. ...............................................................................................................□
o Airframe Logbook Entry: .....................................................................................□
o Engine Logbook Entry: ........................................................................................□
o Propeller Logbook Entry: .....................................................................................□
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8-29
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
 Remarks:
8-10.15. Completion Sign-Off:
Note the date when all of the above inspections have been
completed:_____________
Remarks:
Additional Remarks & Notes to Include In Next Inspection:
END OF ANNUAL CONDITION INSPECTION CHECKLIST
8-30
Section 8 – Handling, Servicing & Maintenance
08-10-2013
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
Section 9 - Supplements
Table of Contents
9-1. SUPPLEMENTS ......................................................................... 9-1
9-1.
SUPPLEMENTS
Because this POH is specifically written for N11HC, there is no
supplemental information for this chapter.
12-10-2014
Section 9 – Supplements
9-1
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
INTENTIONALLY LEFT BLANK
9-2
Section 9 - Supplements
12-10-2014
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
Section 10 - Safety and Operational Tips
Table of Contents
10-1. PILOT ABILITY ..................................................................... 10-3
10-2. FAA REGULATIONS ............................................................ 10-3
10-3. IMPORTANT NOTICE.......................................................... 10-4
10-4. ENGINE OPERATIONS ....................................................... 10-5
10-4.1. Engine Ground Operations .............................................. 10-5
10-4.2. Engine Break-in ................................................................ 10-5
10-4.3. Best Economy Mixture ..................................................... 10-7
10-4.4. Best Power Mixture .......................................................... 10-7
10-4.5. Changing Power Settings -- Sequence ............................ 10-7
10-4.6. Cylinder Head Temperatures ........................................... 10-8
10-4.7. Fuel Pump ........................................................................ 10-9
10-4.8. Engine General Information ........................................... 10-10
10-4.9. Frequency of Flight......................................................... 10-11
10-4.10. Fouled Spark Plugs .................................................... 10-11
10-4.11. Rapid Engine Cool Downs .......................................... 10-12
10-5. PREFLIGHT ....................................................................... 10-12
10-6. TAKEOFFS......................................................................... 10-12
10-6.1. Takeoff - Short Field ....................................................... 10-14
10-6.2. Takeoff - High Density Altitude ....................................... 10-14
10-7. CRUISE .............................................................................. 10-14
10-8. DESCENTS ........................................................................ 10-15
10-8.1. Sudden Cooling .............................................................. 10-15
10-8.2. Descent Mixture ............................................................. 10-16
08-10-2013
Section 10 –Safety and Operational Tips
10-1
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
10-9. SLIPPING THE GLASAIR .................................................. 10-17
10-10. LANDING ............................................................................ 10-17
10-10.1. Slips and Skids ........................................................... 10-17
10-10.2. Use of Flaps ................................................................ 10-17
10-10.3. Crosswind Landings ................................................... 10-18
10-10.4. Other Landing Observations ....................................... 10-18
10-11. STALLS .............................................................................. 10-19
10-11.1. General ....................................................................... 10-19
10-11.2. Power Off Stalls .......................................................... 10-21
10-11.3. Power on Stalls ........................................................... 10-21
10-11.4. Accelerated Stalls ....................................................... 10-22
10-12. TAXIING ............................................................................. 10-22
10-13. FUEL................................................................................... 10-22
10-13.1. Fuel Management ....................................................... 10-22
10-13.2. Fuel En Route ............................................................. 10-23
10-13.3. Fuel Filling (Thermal expansion) ................................ 10-23
10-13.4. Fuel Filling (Grounding) .............................................. 10-23
10-14. TESTING ............................................................................ 10-24
10-14.1. Study Materials ........................................................... 10-24
10-14.2. Aerobatics ................................................................... 10-24
10-14.3. Final Certification ........................................................ 10-25
10-2
Section 10 –Safety and Operational Tips
08-10-2013
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
10-1.
PILOT ABILITY
The Glasair Super ll-S FT is a high performance airplane. To fly it
safely, the pilot needs the necessary skills and confidence to operate
and control the airplane automatically. Activities requiring attention
outside the airplane, such as avoiding traffic and flight path planning,
will occupy much of the pilot's thought and time.
Glasair Super ll-S FT pilots must be honest with themselves about their
experience and ability. N11HC is starting with extended wingtips (EWT)
until the primary pilots gain adequate experience in the aircraft. The
longer wing permits slower approaches that feel more comfortable
during the "training phase." The wing tip extensions will be replaced
with the standard tips only when the primary pilots feel comfortable and
confident enough to do so.
10-2.
FAA REGULATIONS
The airplane must be operated and maintained in accordance with FAA
Airworthiness Directives which may be issued against the power plant,
propeller, and any other parts not manufactured by Glasair Aviation.
WARNING
Revisions or Service Bulletins issued by Glasair Aviation
are mandatory and must be complied with. Review a
current Service Bulletin list to determine which Service
Bulletins apply to Glasair Super ll-S FT Kit 2329 (N11HC).
Applicable bulletins, AD’s, etc. as of January 2013 are on the N11HC
Advisory Publications Website. This site also contains hyperlinks to
PDF copies of applicable bulletins and an excel spreadsheet showing
applicable and non-applicable bulletins.
The Federal Aviation Regulations place the responsibility for
maintenance of this airplane on the owner and operator. All limits
procedures, safety practices, time limits, servicing, and maintenance
requirements contained in this manual are considered mandatory for
08-10-2013
Section 10 –Safety and Operational Tips
10-3
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
continued safe airworthiness and to maintain the airplane in a condition
equal to that of its original construction.
10-3. IMPORTANT NOTICE
This manual is not designed, nor can it serve as a substitute for
adequate and competent flight instruction. It is not intended to be a
guide of basic flight instruction or a training manual.
Most of the information here came from other publications which can be
found at http://11HC.44RF.com under manuals.
This POH should be read thoroughly and carefully by the owner and/or
operator in order to become familiar with the operation of the aircraft. It
is intended to serve only as a guide under most circumstances, but
cannot take the place of good sound judgment during flight operations.
Multiple emergencies, adverse weather, terrain, etc., may require
deviation from the recommended procedures. Furthermore, this Pilot's
Operating Handbook does not provide a discussion of all possible
dangerous situations an owner or operator may encounter.
Flying in itself is not inherently dangerous, but to an even greater extent
than any other mode of travel, it is terribly unforgiving of any
carelessness, incapacity, or neglect. The builder/pilot is entirely
responsible for manufacture, inspection, maintenance, test flight, and
normal operation of the aircraft. Thorough, careful procedures,
therefore, must be carried out in all these phases.
How well the plane is built, maintained, and operated will determine how
safely it performs. Maximum performance and safe operation can only
be achieved by a skilled pilot and a good mechanic. Thorough, careful
construction, continued maintenance, and diligent practice during the
early phases of flight familiarization are mandatory.
The information contained in this POH refers to the Glasair Super ll-S
FT aircraft and more specifically to N11HC. Every attempt will be made
to keep this manual updated to deal with modifications and additional
information.
10-4
Section 10 –Safety and Operational Tips
08-10-2013
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
10-4.
ENGINE OPERATIONS
The following information is from Lycoming Flyer “Operations”
10-4.1.
Engine Ground Operations
The engine ground operation greatly influences formation of lead salt
deposits on spark plugs and exhaust valve stems. Proper operation of
the engine on the ground (warm-up, landing, taxi and engine shutdown) can greatly reduce the deposition rate and deposit formation
which cause spark plug fouling and exhaust valve sticking.
1. Proper adjustment of the idle speed (600 to 650 RPM) fuel mixture,
and maintenance of the induction air system will ensure smooth engine
operation and eliminate excessively rich fuel/air mixtures at idle speeds.
This will minimize the separation of the nonvolatile components of the
high-leaded aviation fuels greatly retarding the deposition rate.
2. The engine should be operated at engine speeds between 1000 and
1200 RPM after starting and during the initial warm-up period. Avoid
prolonged closed-throttle idle engine speed operation (when possible).
At engine speeds from 1000 to 1200 RPM, the spark plug core
temperatures are hot enough to activate the lead scavenging agents
contained in the fuel which retards the formation of the lead salt
deposits on the spark plugs and exhaust valve stems. Avoid rapid
engine speed changes after start-up, and use only the power settings
required to taxi.
10-4.2.
Engine Break-in
A new, rebuilt or overhauled engine should receive the same start,
warm-up and preflight checks as any other engine. A good break-in
requires that the piston rings expand sufficiently to seat with the cylinder
walls. This seating of the ring with the cylinder wall will only occur when
pressures inside the cylinder are great enough to cause expansion of
the piston rings. Pressures in the cylinder only become great enough for
a good break-in when power settings above 65% are used.
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Section 10 –Safety and Operational Tips
10-5
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
Full power for takeoff and climb during the break-in period is not
harmful; it is beneficial, although engine temperatures should be
monitored closely to ensure that overheating does not occur. Cruise
power settings above 65%, and preferably in the 70% to 75% of rated
power range, should be used to achieve a good engine break-in.
Remember that if the new or rebuilt engine is normally aspirated (nonturbocharged), it will be necessary to cruise at lower altitudes to obtain
the required cruise power levels. Density altitudes in excess of 8000
feet (5000 feet is recommended) will not allow the engine to develop
sufficient cruise power for a good break-in.
The use of low power settings does not expand the piston rings enough,
and a film of oil is left on the cylinder walls. The high temperatures in
the combustion chamber will oxidize this oil film so that it creates a
condition commonly known as glazing of the cylinder walls. When this
happens, the ring break-in process stops, and excessive oil
consumption frequently occurs. The bad news is that extensive glazing
can only be corrected by removing the cylinders and rehoning the walls.
This is expensive, and it is an expense that can be avoided by proper
break-in procedures.
To summarize, there are just a few items to remember about engine
break-in:
1. If a preservative oil has been added by the aircraft manufacturer,
drain it no later than the first 25 hours of operation;
2. Follow the engine manufacturer’s recommendation regarding the oil
to be used for break-in and the period between changes;
3. Run the engine at high cruise power levels for best piston
ring/cylinder wall mating;
4. Continue break-in operation for 50 hours or until oil consumption
stabilizes. These simple procedures should eliminate the possibility of
cylinder wall glazing and should prepare the engine for a long and
satisfactory service life.
10-6
Section 10 –Safety and Operational Tips
08-10-2013
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
10-4.3.
Best Economy Mixture
Because N11HC has GAMI injectors, the best economy mixture is LOP.
As long as the engine is running smooth and cool, the leaner the
mixture, the better the economy.
10-4.4.
Best Power Mixture
If running ROP, be at least 100° Rich of peak EGT.
In summary, proper leaning will:
10-4.5.
Changing Power Settings -- Sequence
TO INCREASE POWER
1. Enrich Mixture
2. Increase RPM
3. Follow with Throttle.
TO DECREASE POWER:
1. Reduce Throttle
2. Reduce RPM,
3. Adjust Mixture.
INCREASING POWER
1. Enrich Mixture first to ensure protecting the engine against
damage from higher power when previously leaned out for a lower
power setting.
2. Next, Increase RPM so the engine and propeller will not have
undesirable pressure and stresses with a high manifold pressure
and lower RPM.
3. Then, follow with the appropriate Manifold Pressure, now that the
mixture and RPM have been correctly set to accommodate the
increased throttle.
08-10-2013
Section 10 –Safety and Operational Tips
10-7
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
10-4.6.
Cylinder Head Temperatures
If head temperatures are higher than normal during flight, it should
not be ignored, because there is some reason for it. It may be
caused by hot ambient temperatures, a lean fuel metering device at
higher than cruise power, bad baffles or leaking cowling, or
malfunctioning of the ignition system. Even old and tired engine mounts
that allow the engine to sag slightly may cause a change in the airflow
pattern and an abnormal increase in CHT. It is also possible that a
mechanical problem may be developing in the engine.
When higher than normal cylinder head temperatures are showing on
the gage, the pilot should take steps to bring the temperatures down to
the normal operating range in order to keep the remaining flight safe.
Head temperatures may be reduced by:
1. Enriching the mixture
2. Reducing power
3. Both the above
To help the mechanic diagnose the problem, provide him with the G3X
recorded data. Just read a memory card with MS Excel.
A first step in diagnosing abnormal cylinder head temperatures would
be ensuring that the gages are providing accurate readings. If they are,
the mechanic can then proceed to check engine baffles that may have
deteriorated, proper flow of the fuel metering device, and then other
more time-consuming checks for ignition or mechanical malfunction.
Minimum in-flight CHT should be 149°F / 65˚C, and maximum in
normally aspirated Lycoming engines is 500°F / 260˚C. Although these
are minimum and maximum limits, the pilot should operate his or her
engine at more reasonable temperatures in order to achieve the
expected overhaul life of the power plant. Engines have benefited
during continuous operation by keeping CHT below 392°F / 200˚C in
order to achieve best life and wear of the power plant. In general, it
10-8
Section 10 –Safety and Operational Tips
08-10-2013
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
would be normal during all-year operations, in climb and cruise to see
head temperatures in the range of 350°F / 177˚C to 435°F / 224˚C.
N11HC has bayonet probes in all cylinders; it is not unusual to see
variations in CHT readings on fuel-injected engines of 100°F / 38˚C
between cylinders. Other influences on CHT are such items as cylinder
baffles, cowling, cowling flaps, location of engine accessories and, of
course, manual control of fuel mixture.
10-4.7.
Fuel Pump
Most Lycoming fuel-injected engines are simply primed by turning the
Boost Pump on, opening the mixture briefly to full rich, and cracking the
throttle. Any pumping of the throttle is ineffective until the engine begins
to fire.
It is necessary to supply the engine with a steady, uninterrupted flow of
fuel for all operating conditions. Entrapped air, temperature changes,
pressure drops, agitation in the fuel lines and other factors affect the
release of air and vapor from the fuel system. Under some
circumstances where an engine-mounted fuel pump is provided, it may
not be able to pump a continuous fuel supply free of excessive vapor.
An effective continuous fuel supply is provided by use of the Boost
Pump. As a general recommendation, the Boost Pump should be used
with Lycoming engines in all conditions where there is any possibility of
excessive vapor formation, or when a temporary cessation of fuel flow
would introduce undesirable hazards. The conditions under which
Lycoming recommends operation of the Boost Pump are as follows:
1. Every takeoff.
2. Climb after takeoff.
3. When switching fuel selectors from one separate fuel tank to another,
the Boost Pump should be “on” in the new tank until the operator is
assured there will be no interruption of the fuel flow.
4. Every landing approach.
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5. Any time the fuel pressure is fluctuating, and the engine is affected by
the fluctuation.
6. Hot weather, hot engine ground operation where fuel vapor problems
cause erratic engine operation.
8. If the engine-mounted fuel pump fails.
If the Boost Pump is used during ground operation, don’t fail to check
the condition of the engine-mounted fuel pump before takeoff by turning
the boost pump off briefly, and then back “on” for takeoff. If the enginemounted pump has failed, it would be safer to know that on the ground
rather than in the air when the Boost Pump is turned “off.”
When in doubt, do the safest thing and use the Boost Pump with
Lycoming engines. Don’t be “stingy” with the boost pump. In most
cases, they last the overhaul life of the engine, and are then exchanged
or overhauled themselves.
10-4.8.
Engine General Information
1. Never lean the mixture from full rich during take-off, climb or highperformance cruise operation. However, during takeoff from highelevation airports or during climb at higher altitudes, roughness or
reduction of power may occur at full-rich mixture. In such a case, the
mixture may be adjusted only enough to obtain smooth engine
operation. Careful observation of temperature instruments should be
practiced.
2. Operate the engine at maximum power mixture for performance
cruise powers and at best economy mixture for economy cruise power.
3. Always return the mixture to full rich before increasing power settings.
4. During let-down and reduced-power flight operations, it may be
necessary to manually lean or leave mixture setting at cruise position
prior to the landing pattern. During the landing sequence, the mixture
control should then be placed in the full-rich position, unless landing at
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high-elevation fields where operation at a lean setting may be
necessary.
10-4.9.
Frequency of Flight
Frequency of flight also plays an important part in the operating history
of an engine. Engines flown only occasionally and with extended
periods between oil changes are subject to corrosion because of acids
that build up in the oil and attack internal metallic parts of the engine.
Only regular oil changes can eliminate these acids.
Moisture that enters through the breather or exhaust system can cause
rusting of cylinders and other steel parts. Rings may take a set and stick
in the groove. Condensation in the magnetos may cause shorting of the
breaker points. Flying as often as possible to bring the engine
temperatures up to their normal operating levels will help to eliminate
moisture. A ground run of the engine only is not considered satisfactory.
Frequent flights are needed.
The number of hours that need to be flown each month, and the length
of time between flights cannot be specified for every aircraft and engine.
Variables such as geographic location and local temperature and
humidity must be considered. Inactivity and time will cause hardening of
gaskets, seals and hoses. Long periods between flights can be
expected to cause excessive wear during engine start due to loss of the
protective oil film on bearing surfaces during the long periods of
inactivity. Regardless of the operating hours, those engines that have
not reached the recommended number of operating hours for TBO in a
12-year period should be considered for overhaul or replacement.
10-4.10. Fouled Spark Plugs
If the magneto check before or after flight reveals any roughness
caused by a fouled spark plug, open the throttle slowly and smoothly to
cruise RPM, and lean the mixture as far as possible (yet with a smooth
engine). After several seconds leaned, return to the proper mixture
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position for takeoff and recheck the magneto. If two such attempts do
not clear the fouled plug, then return to the line and report the problem
to maintenance.
10-4.11. Rapid Engine Cool Downs
Rapid engine cool down from low-power altitude changes, low-power
landing approach and/or engine shut-down too soon after landing or
ground runs should be avoided.
10-5.
PREFLIGHT
NOTE
Fuel selector must be on header tank to provide pressure
head of fuel to filter.
10-6.
TAKEOFFS
Use 15° to 25° of flaps for all takeoffs. Anything less will cause a very
high pitch attitude and loss of forward visibility at rotation.
Do not raise takeoff flaps until at least 90 KIAS after liftoff. Raising
them early will cause a settling effect, resulting in a nose-high attitude
and loss of forward visibility.
NOTE
No leaning except MAYBE high altitude takeoffs. During
take-off from high elevation airport or during climb, roughness
or loss of power may result from over-richness. In such a
case adjust mixture control only enough to obtain smooth
operation – not for economy. Observe instruments for
temperature rise.
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NOTE
If the RPM drop exceeds 175 RPM, slowly lean the mixture
until the RPM peaks. Then retard the throttle to 2100 and
repeat the check. If the drop-off does not exceed 175 RPM,
the difference between the magnetos does not exceed 50
RPM, and the engine is running smoothly, then the ignition
system is operating properly. Return the mixture to full rich.
NOTE
N11HC’s Vs is stall speed.
WARNING
If the aircraft is parked on sloping ground with one wing
low and with a partially empty wing fuel tank, fuel slowly
transfers into the low wing creating a wing-heavy
condition that can cause control difficulty after takeoff.
Making tight taxi turns can have the same effect. A
heavy left wing is especially critical since the resulting
left-turning tendency exacerbates the effects of engine
torque. If you suspect an unbalanced fuel condition, taxi
to level ground and allow sufficient time (20 minutes) for
the wing tank fuel level to equalize before attempting
takeoff.
NOTE
Engine is warm enough for take-off when the throttle can be
opened without the engine faltering.
NOTE
Leave the electric Boost Pump on at all times while in the
pattern. When leaving the pattern, attain adequate altitude
before switching the pump off.
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10-6.1.
Takeoff - Short Field
The short field takeoff is the same as the normal takeoff except that,
after lining up on the runway, hold the brakes while advancing the
power. Release the brakes after full power is reached. Use 15° of
flaps. As the airplane passes through Vs ease the stick back to rotate
the wing to a takeoff angle of attack.
Once airborne, the airplane will accelerate quickly to 86 knots which is
the best angle of climb speed (~2 Green on AOA). Establish a climb at
this airspeed until obstacles are cleared. When all obstacles are
cleared, raise the flaps while accelerating to the best rate of climb
speed of 104 knots.
10-6.2.
Takeoff - High Density Altitude
At high density altitude (above 4000 ft MSL), lean the engine during runup for best takeoff power.
10-7.
CRUISE
Hold the plane at the desired altitude, when it is reached, and don’t
throttle back until reaching the approximant cruise airspeed. Then
reduce to the desired cruise MP / RPM. This technique will quickly get
you into a stabilized flight attitude and trim.
CAUTION
Throttle movements from full power to idle or from idle to full
power are full range movements. Full range throttle
movements must be performed over a minimum time duration
of 2 to 3 seconds. Performing a full range throttle movement
at a rate of less than 2 seconds is considered a rapid or
instant movement. Performing rapid movements may result in
detuned counterweights which may lead to failure of the
counterweight lobes and subsequent engine damage.
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10-8.
DESCENTS
10-8.1.
Sudden Cooling
Never pull power off and dive down in cold air. The rapid cooling at idle
and high velocity can be very hard on an engine. When descending
keep a little power on and don’t descend too fast. Another thing to keep
in mind when descending is that the airplane is very clean
aerodynamically. If you are in a 165 to 175 knot cruise, it doesn’t take
much for a descent angle to reach red line, so be cautious. Also
remember that, with a very clean airframe, you are limited to fairly
shallow descents, so plan your descent in advance to reach your
destination airport at pattern altitude.
Generally speaking, pilots hold the key to dodging these problems.
They must avoid fast letdowns with very low power (high-cruise RPM
and low manifold pressure), along with rich mixtures that contribute to
sudden cooling. It is recommended that pilots maintain at least 15" MP
or higher, and set the RPM at the lowest cruise position. This should
prevent ring flutter and the problems associated with it.
Letdown speed should not exceed high cruise speed or approximately
1,000 feet per minute of descent. Keeping descent and airspeed within
these limits will help to prevent the sudden cooling that may result in
cracked cylinder heads, warped exhaust valves and bent pushrods.
The mixture setting also has an effect on engine cooling. To reduce
spark plug fouling and keep the cylinder cooling within the
recommended 50°F / 10˚C per-minute limit, the mixture should be left at
the lean setting used for cruise and then richened gradually during
descent from altitude. The lean mixture, maintaining some power and
using a sensible airspeed should achieve the most efficient engine
temperatures possible.
Be sure your seat belts are fastened snugly when descending. Coming
down from smooth air into turbulent air at a high rate of speed can be
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especially tough on you and the airframe. Maximum structural cruising
speed (Vno) of the Glasair is 175 knots IAS.
Gradually push the mixture control to rich during long descents.
NOTE
Complete the pre-landing check list before entering the
pattern so your attention can be directed outside the airplane
to clear for other traffic while in the pattern. Some Glasair
pilots like to go to full flaps early in the approach (before
turning onto the downwind leg) to provide maximum visibility
over the nose and also to reduce their work load while in the
pattern.
NOTE
When on final, you should be pattern high with your speed
down and a somewhat high angle of descent. This allows
visibility over the nose all the way down through final. Do not
approach the field low and slow with a shallow descent angle.
If you’re low and slow, go around and try again. If you can’t
see the runway numbers all the way down to flare, your
approach is not correct.
10-8.2.
Descent Mixture
Regardless of the field elevation where the pilot intends to land, the
descent from cruise altitude to traffic pattern altitude should be made
with the engine leaned for smooth engine operation. Low elevation
fields (below 5,000 feet density altitude) will require that the mixture be
moved to full rich in the “before landing checklist.” Landing at airports
above 5,000 feet density altitude, the mixture must be leaned to smooth
engine operation during traffic pattern flight and landing; otherwise, the
engine may stop on the runway because of excessive richness.
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10-9.
SLIPPING THE GLASAIR
The Glasair Super II-S FT will slip with full flaps. With the normal high
descent rate with the flaps extended, however, slips should not be
necessary. The amount of slip is limited by the amount of rudder power
available. On a full flap, slipping approach, there is a very rapid sink
rate which must be checked by adding power. Speed should be kept
comfortably above the stall (75-78 KIAS) throughout the approach.
WARNING
If less than ten (10) gallons of fuel remain in the wing
tank, slips are prohibited when drawing fuel from the
wing tank.
CAUTION
Attempt such maneuvers as full flap, full slip approaches only
after becoming thoroughly familiar and proficient with the
normal flying and handling characteristics of your Glasair
Super II-S FT.
10-10.
LANDING
10-10.1. Slips and Skids
Be aware that the rudders are very effective, but have very little
movement. Therefore it is easy to over-control the rudders especially in
the pattern. Rudder pressures that had you coordinated on downwind
may be completely different turning final. Check the ball often in the
pattern to maintain coordinated flight.
10-10.2. Use of Flaps
Always use at least 15° of flaps for landing and 40° is much better.
Without flaps you will lose sight of the end of the runway and might
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misjudge your height above the runway resulting in a hard to very hard
touchdown.
10-10.3. Crosswind Landings
Normal crosswind landing procedures for conventional aircraft apply to
the Glasair Super II-S FT. Recommended technique is to use the winglow method from short approach until the airplane is chalked. Flap
settings do not appear to have a large effect on control response during
crosswind landings. If you don’t like the approach with full flaps, go
around and try less flaps. If 15° still seems like too much, find a
different runway.
The maximum crosswind that can be handled in the Glasair Super II-S
FT is highly dependent on pilot proficiency and technique. The
maximum demonstrated cross wind to date is 17 knots.
10-10.4. Other Landing Observations
If you lose site of the end of the runway with flaps at least 15°, you are
too high – get closer to the runway and land like a good pilot.
The landing in the Glasair Super II-S FT is similar to the landing in any
nose wheel airplane. Due to the high sink rate with flaps extended and
the propeller in flat pitch, the flare may have to be started somewhat
higher above the ground and back pressure applied to the stick more
rapidly in order to break the glide.
Keep the power off sink rate in mind during landing approaches. At a
standard pattern altitude of 1000 ft AGL, a tight pattern must be
maintained to execute a power off glide to the runway. Fly a 2G-1Y
AOA and back it up with IAS. Avoid letting the airspeed get too low
during a power off approach as you will need the excess airspeed (lift
available) to make the round-out and flare. The sink rate increases at
lower approach speeds and you have less excess lift available to arrest
the descent in the flare.
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Touchdown should be in a near stall attitude and speed. There is
enough elevator authority to hold the nose gear off for a long time and
then set it down gently.
CAUTION
If you don’t like the way you’re set up for landing, don’t be
ashamed or too proud to go around and try it again. It is
much better to go around than to damage the plane or
yourself.
On a balked landing (go-around), add full power (applying
right rudder, as necessary), stabilize the plane in a climb, and
ease the flaps up (the last 15° when above 90 KIAS). The
plane has enough power to go around with full flaps, but with
limited performance.
NOTE
It cannot be stressed enough that, if the pilot does not have a
lot of flying experience in aircraft with wing loading and
performance similar to the Glasair Super II-S FT; use the
wing tip extensions. They can be thought of as transforming
your Glasair into an intermediate trainer.
10-11.
STALLS
10-11.1. General
Stall recovery for the Glasair Super II-S FT is typical of most
conventional aircraft – lower the nose with forward stick, and add
power. The stall characteristics are predictable in both power off and
moderate power on stalls. Just before the stall, slight buffeting is felt,
giving an early indication of the stall.
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Note:
Continuing to pull back while N11HC is buffeting will usually
cause it to quickly roll inverted. Therefore going beyond the
buffet stage is not recommended.
The Glasair Super II-S FT should not be intentionally stalled with any
heavy baggage in the baggage compartment unless it is securely
fastened down. When practicing stalls, be sure to check the airspace
for any conflicting traffic.
NOTE
Stall strips are mandatory on the Glasair Super II-S FT to
induce the wing roots to stall first. Without these stall strips
properly installed, the stall may be unpredictable or erratic.
The stall strips make a nice gentle stall possible with an
adequate margin of stall warning.
WARNING
Intentional spins are prohibited in the Glasair Super II-S
FT. It is strongly recommend that stalls be practiced at
least 3000 ft AGL. Be familiar with standard spin
recovery procedures in the event of an inadvertent spin
entry while practicing stalls.
Remember that an airplane can stall at any airspeed and attitude (high
speed stalls) but the recovery is always the same: stick forward and add
power (unless you are inverted). The rudder is effective in keeping the
wings level throughout the stall.
Just prior to the stall, a moderate burble or airframe shake, induced by
the stall strips at the wing root, will be felt. If the stick is held back, the
shake will become more pronounced, followed by the nose dropping.
To recover, move the stick forward and apply power. Level the wings
with the rudder.
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WARNING
Do not use the ailerons to keep the wings level in a stall
as this will more easily cause a spin entry or aggravate
spin recovery.
10-11.2. Power Off Stalls
When practicing power off stalls, hold the nose up in a slight climb
attitude, gradually bringing the stick back as the airspeed bleeds off,
until the plane begins to stall. Practice power off stalls at each flap
setting to get the feel of the stall in each mode from fully retracted to
fully extended flaps.
With flaps applied, the plane feels more stabilized, the stall speed is
lowered by a few knots, the actual point of the stall is a little more
sudden, and the nose drops slightly lower. Because of the extra drag
with the flaps lowered, the stall is more pronounced and there is less
time lag between the wing root buffet and the nose dropping. The stall
with full flaps is still quite gentle and a quick recovery with minimal
altitude loss is possible. Release back pressure on the stick, apply full
power, stabilize the plane back into a climb and raise the flaps.
10-11.3. Power on Stalls
Do not practice these types of stalls lower than 5000 ft AGL. Power on
stalls are more pronounced or sudden because of the high angle of
attack, but recovery is the same as with power off stalls. Stick forward
and add power. With power applied, the torque effects of the engine
and propeller induce rolling and yawing forces during the stall. For this
reason, a wing drop is more likely to occur in a power on stall.
WARNING
Power on stalls can more easily lead to a spin entry.
Give yourself plenty of recovery room for safety in the
event of an inadvertent spin. As the power is increased
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above 1800 rpm, a spin becomes more and more likely
during power on stalls.
10-11.4. Accelerated Stalls
An airplane can stall at any airspeed and any attitude since exceeding
the acceptable angle of attack is what causes a stall. As with most
aircraft, the Glasair will stall at a progressively higher airspeed as the
angle of bank in a turn is increased.
A common means of inadvertently entering an accelerated stall is to pull
the stick back too suddenly after recovery is made from an initial stall.
This is typically done to avoid altitude loss.
In most cases, incipient stall recovery is made by simply relaxing the
back pressure or neutralizing the stick. To minimize altitude loss during
an inadvertent approach-to-landing stall or a departure stall, immediate
application of full power is necessary.
10-12.
TAXIING
The tricycle landing gear configuration makes taxiing the Glasair Super
II-S FT a simple matter. Visibility over the nose is excellent. Steering at
slow taxi speeds is by differential braking. Above about 26 knots IAS,
the rudder begins to become effective for directional control. It is best
to keep the speed well under control while taxiing and to taxi
defensively when in the vicinity of other ground traffic.
10-13.
FUEL
10-13.1. Fuel Management
WARNING
Make sure that the fuel selector valve engages the detent
for the desired tank. If the valve is positioned between
detents, fuel will feed from the header tank. When the
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header tank is empty, the engine will pull air from the
tank and quit from fuel starvation. Make sure that the
valve cannot inadvertently be bumped out of position
during flight.
10-13.2. Fuel En Route
Determine by careful experimentation what your aircraft burns in fuel
per hour at various power settings such as 55% and 75% power. Plan
your flights so that you always have an HOUR reserve on board in case
of any unexpected delays. Always keep track of how much fuel remains
in both the wing and header tanks. Make sure that for takeoff and
landing, the fuel tank selector valve is set to a full tank that has ample
fuel.
10-13.3. Fuel Filling (Thermal expansion)
When filling the wing fuel tank allow for 2 gallons of thermal expansion.
Standard useable capacity is 40 gallons. Total volume is 43 gallons. If
topped off, the expanding fuel in the wing tank will be forced overboard
through the wing vent system.
10-13.4. Fuel Filling (Grounding)
The right fuel cap and the header fuel cap have electrical conductive
chains between the fuel surface and the caps. Always ensure the
electrical potential at the fuel surface is the same as the fuel nozzle
(grounded) before and during refueling. Before unlocking and during
the opening of these fuel caps, hold the grounding cable clip to the cap
(Header or right wing as appropriate) and then clip it to the cap’s chain
during refueling. Always have a fire extinguisher nearby.
WARNING
When fueling the airplane, always ground it properly as
described above.
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WARNING
Fuel spills (caused by overfilling, fuel expansion,
improperly installed fuel vent lines, or the wings not
being level) are always a possibility when fueling the
aircraft. Be aware of the potential for spills, especially
when the airplane is parked on uneven ground. If a fuel
spill occurs, move the airplane well away from the spill
(upwind if possible), and have someone stand by with a
fire extinguisher before attempting to start the engine.
10-14.
TESTING
Because Phase I is complete, much of the information that was
contained here has been removed.
10-14.1. Study Materials
 AC 90-89A
 ASA Flight Testing Homebuilt Aircraft
10-14.2. Aerobatics
After the normal handling characteristics of the airplane have been
explored and you feel completely comfortable with the control and
operation of the airplane, aerobatics may be attempted, if desired. Log
all the aerobatic maneuvers performed. When the flight test period has
been completed, and you apply for the unlimited duration airworthiness
certificate, you can request that the operating limitations be amended to
permit those aerobatic maneuvers that you have logged. The inspector
may also request an actual flight demonstration of the maneuvers. If
you are unfamiliar with aerobatics, the operating limitations can be
amended at a later time, after you have received proper instruction and
gained some experience.
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NOTE
Consult the Limitations Section of this manual for a further
discussion of aerobatics.
10-14.3. Final Certification
The following aircraft logbook entry graduating N11HC from Phase I into
Phase II was made on January 17th 2013:
I certify that the prescribed flight test hours have been completed and
the aircraft is controllable throughout its normal range of speeds and
throughout all maneuvers to be executed, has no hazardous
characteristics or design features, and is safe for operation.
The following aircraft operating data has been demonstrated during the
flight testing (speeds are in KIAS). Vs and Vso were measured
between two GW / CG data points – 1726# / 91.48” and 2166# / 96.48”.
Vs = 63 and 67, Vso = 54 and 57 (power idle). At 65% power these
stall speeds decrease 2 to 3 KIAS). At 1726# / 91.48”, Vx and Vy are
85 and 108 KIAS. Best glide speed is also 85 KIAS.
I certify that the following aerobatic maneuvers have been test flown
and that the aircraft is controllable throughout the maneuvers’ normal
range of speeds, and is safe for operation. The flight-tested aerobatic
maneuvers are: Aileron Rolls, Slow Rolls, Barrel Rolls, Loops, Cuban
Eights, Immelmanns, Clover Leaf and Split-S.
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INTENTIONALLY LEFT BLANK
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Section 11 - Logging Changes, Updates and Inspections
Table of Contents
11-1.
GENERAL ............................................................................ 11-3
11-2.
VOR Accuracy Checks (Every 30 days) .............................. 11-3
11-3.
G3X and G430 Jeppesen NavData Update (Every 28 days)11-6
11-4.
G3X Obstacle Data Update (Every 56 days) ....................... 11-7
11-5.
G3X Terrain Data Update (As Needed) ............................... 11-8
11-6.
G3X SafeTaxi Data Update (Every 56 days) ....................... 11-8
11-7.
G3X FliteCharts Data Update (Every 28 days) .................... 11-9
11-8.
G3X AOPA Airport Data Update (Every 56 days).............. 11-10
11-9.
Pitot/Static/Transponder Checks Due: (24 Months) .......... 11-11
11-10.
Condition Inspection Due: (12 Months) ........................... 11-11
11-11.
Time-Change or Inspection Requirements ...................... 11-12
11-11.1.
Starter – every 50 hours ............................................. 11-12
11-11.2.
ELT – every year ........................................................ 11-12
11-11.2.1. Reference page 26 of Operations and Instructions for
Continued Airworthiness (ICA) Manual ..................................... 11-12
11-11.2.2. Test IAW Para 2.3 .................................................... 11-12
11-11.3.
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Propeller - 2016 .......................................................... 11-12
Section 11 – Logging Info
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11-1.
GENERAL
This section provides a central location for documenting and tracking
required updates and changes to both the POH and aircraft.
Documentation of non-applicable or one-time accomplishment of
Glasair Service Letter requirements are in a separate folder.
11-2.
VOR Accuracy Checks (Every 30 days)
The VOR accuracy must be checked and within limits and the check
documented within 30 days of an IFR flight which uses VOR
information.
IAW FAR 91.171:
(a) No person may operate a civil aircraft under IFR using the VOR system
of radio navigation unless the VOR equipment of that aircraft—
(1) Is maintained, checked, and inspected under an approved procedure; or
(2) Has been operationally checked within the preceding 30 days, and was
found to be within the limits of the permissible indicated bearing error set
forth in paragraph (b) or (c) of this section.
(b) Except as provided in paragraph (c) of this section, each person
conducting a VOR check under paragraph (a)(2) of this section shall—
(1) Use, at the airport of intended departure, an FAA-operated or approved
test signal or a test signal radiated by a certificated and appropriately rated
radio repair station or, outside the United States, a test signal operated or
approved by an appropriate authority to check the VOR equipment (the
maximum permissible indicated bearing error is plus or minus 4 degrees); or
(2) Use, at the airport of intended departure, a point on the airport surface
designated as a VOR system checkpoint by the Administrator, or, outside the
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Section 11 – Logging Info
11-3
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
United States, by an appropriate authority (the maximum permissible bearing
error is plus or minus 4 degrees);
(3) If neither a test signal nor a designated checkpoint on the surface is
available, use an airborne checkpoint designated by the Administrator or,
outside the United States, by an appropriate authority (the maximum
permissible bearing error is plus or minus 6 degrees); or
(4) If no check signal or point is available, while in flight—
(i) Select a VOR radial that lies along the centerline of an established VOR
airway;
(ii) Select a prominent ground point along the selected radial preferably more
than 20 nautical miles from the VOR ground facility and maneuver the
aircraft directly over the point at a reasonably low altitude; and
(iii) Note the VOR bearing indicated by the receiver when over the ground
point (the maximum permissible variation between the published radial and
the indicated bearing is 6 degrees).
(c) If dual system VOR (units independent of each other except for the
antenna) is installed in the aircraft, the person checking the equipment may
check one system against the other in place of the check procedures
specified in paragraph (b) of this section. Both systems shall be tuned to the
same VOR ground facility and note the indicated bearings to that station.
The maximum permissible variation between the two indicated bearings is 4
degrees.
(d) Each person making the VOR operational check, as specified in
paragraph (b) or (c) of this section, shall enter the date, place, bearing error,
and sign the aircraft log or other record. In addition, if a test signal radiated
by a repair station, as specified in paragraph (b)(1) of this section, is used,
an entry must be made in the aircraft log or other record by the repair station
certificate holder or the certificate holder's representative certifying to the
bearing transmitted by the repair station for the check and the date of
transmission.
11-4
Section 11 – Logging Info
08-22-2013
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
IAW Airport/Facility Directory, Rochester’s check is done at 3000’ MSL
over intersection of runways. And be ± 6° of the 024 radial.
Date
Where
Air
±6°
Gnd
± 4°
VOT
± 4°
Signature
KRST RW inter
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Section 11 – Logging Info
11-5
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
11-3.
No.
G3X and G430 Jeppesen NavData Update (Every 28 days)
Effective
Date Installed
1409
2014 Jul 24 – 2014 Aug 21
1410
2014 Aug 21 - 2014 Sep 18
1411
2014 Sep 18 - 2014 Oct 16
1412
2014 Oct 16 - 2014 Nov 13
1413
2014 Nov 13 - 2014 Dec 11
1501
2014 Dec 11 - 2015 Jan 08
1502
2015 Jan 08 - 2015 Feb 05
1503
2015 Feb 05 - 2015 Mar 05
1504
2015 Mar 05 - 2015 Apr 02
1505
2015 Apr 02 - 2015 Apr 30
1506
2015 Apr 30 - 2015 May 28
1507
2015 May 28 - 2015 Jun 25
1508
2015 Jun 25 - 2015 Jul 23
1509
2015 Jul 23 - 2015 Aug 20
1510
2015 Aug 20 - 2015 Sep 17
1511
2015 Sep 17 - 2015 Oct 15
1512
2015 Oct 15 - 2015 Nov 12
1513
2015 Nov 12 - 2015 Dec 10
1601
2015 Dec 10 - 2016 Jan 07
1602
2016 Jan 07 - 2016 Feb 04
1603
2016 Feb 04 - 2016 Mar 03
1604
2016 Mar 03 - 2016 Mar 31
11-6
Section 11 – Logging Info
By
08-22-2013
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
11-4.
G3X Obstacle Data Update (Every 56 days)
No
Effective
Installed
14B4
2014 Jul 24 - 2014 Sep 18
14B5
2014 Sep 18 - 2014 Nov 13
14B6
2014 Nov 13 - 2015 Jan 08
15B1
2015 Jan 08 - 2015 Mar 05
15B2
2015 Mar 05 - 2015 Apr 30
15B3
2015 Apr 30 - 2015 Jun 25
15B4
2015 Jun 25 - 2015 Aug 20
15B5
2015 Aug 20 - 2015 Oct 15
15B6
2015 Oct 15 - 2015 Dec 10
15B7
2015 Dec 10 - 2016 Feb 04
16B1
2016 Feb 04 - 2016 Mar 31
16B2
2016 Mar 31 - 2016 May 26
16B3
2016 May 26 - 2016 Jul 21
16B4
2016 Jul 21 - 2016 Sep 15
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Section 11 – Logging Info
By
11-7
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
11-5.
G3X Terrain Data Update (As Needed)
Terrain databases are updated on an "as needed" basis, and not on a regular
schedule. Terrain databases do not have effective or expiration dates.
Installed Terrain Data Base:
11-6.
No
G3X SafeTaxi Data Update (Every 56 days)
Effective
14S4
2014 Jul 24 - 2014 Sep 18
14S5
2014 Sep 18 - 2014 Nov 13
14S6
2014 Nov 13 - 2015 Jan 08
15S1
2015 Jan 08 - 2015 Mar 05
15S2
2015 Mar 05 - 2015 Apr 30
15S3
2015 Apr 30 - 2015 Jun 25
15S4
2015 Jun 25 - 2015 Aug 20
15S5
2015 Aug 20 - 2015 Oct 15
15S6
2015 Oct 15 - 2015 Dec 10
15S7
2015 Dec 10 - 2016 Feb 04
16S1
2016 Feb 04 - 2016 Mar 31
16S2
2016 Mar 31 - 2016 May 26
16S3
2016 May 26 - 2016 Jul 21
16S4
2016 Jul 21 - 2016 Sep 15
11-8
Installed
Section 11 – Logging Info
By
08-22-2013
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
11-7.
G3X FliteCharts Data Update (Every 28 days)
No
Effective
Installed
By
1408 2014 Jul 24 - 2014 Aug 21
1409 2014 Aug 21 - 2014 Sep 18
1410 2014 Sep 18 - 2014 Oct 16
1411 2014 Oct 16 - 2014 Nov 13
1412 2014 Nov 13 - 2014 Dec 11
1413 2014 Dec 11 - 2015 Jan 08
1501 2015 Jan 08 - 2015 Feb 05
1502 2015 Feb 05 - 2015 Mar 05
1503 2015 Mar 05 - 2015 Apr 02
1504 2015 Apr 02 - 2015 Apr 30
1505 2015 Apr 30 - 2015 May 28
1506 2015 May 28 - 2015 Jun 25
1507 2015 Jun 25 - 2015 Jul 23
1508 2015 Jul 23 - 2015 Aug 20
1509 2015 Aug 20 - 2015 Sep 17
1510 2015 Sep 17 - 2015 Oct 15
1511 2015 Oct 15 - 2015 Nov 12
1512 2015 Nov 12 - 2015 Dec 10
1513 2015 Dec 10 - 2016 Jan 07
1601 2016 Jan 07 - 2016 Feb 04
1602 2016 Feb 04 - 2016 Mar 03
1603 2016 Mar 03 - 2016 Mar 31
1604 2016 Mar 31 - 2016 Apr 28
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Section 11 – Logging Info
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Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
1605 2016 Apr 28 - 2016 May 26
1606 2016 May 26 - 2016 Jun 23
1607 2016 Jun 23 - 2016 Jul 21
1608 2016 Jul 21 - 2016 Aug 18
11-8.
No
G3X AOPA Airport Data Update (Every 56 days)
Effective
Installed
By
14D4 2014 Jul 24 - 2014 Sep 18
14D5 2014 Sep 18 - 2014 Nov 13
14D6 2014 Nov 13 - 2015 Jan 08
15D1 2015 Jan 08 - 2015 Mar 05
15D2 2015 Mar 05 - 2015 Apr 30
15D3 2015 Apr 30 - 2015 Jun 25
15D4 2015 Jun 25 - 2015 Aug 20
15D5 2015 Aug 20 - 2015 Oct 15
15D6 2015 Oct 15 - 2015 Dec 10
15D7 2015 Dec 10 - 2016 Feb 04
16D1 2016 Feb 04 - 2016 Mar 31
16D2 2016 Mar 31 - 2016 May 26
16D3 2016 May 26 - 2016 Jul 21
16D4 2016 Jul 21 - 2016 Sep 15
11-10
Section 11 – Logging Info
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Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
11-9.
Pitot/Static/Transponder Checks Due: (24 Months)
Date Due
11-10.
Date Accomplished
By
Condition Inspection Due: (12 Months)
Date Due
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Date Accomplished
By
Section 11 – Logging Info
11-11
Pilot’s Operating Handbook (POH) for N11HC
Glasair Super II-S FT, Slotted Flaps, IO-360, C/S Prop
11-11.
Time-Change or Inspection Requirements
11-11.1. Starter – every 50 hours
11-11.2. ELT – every year
11-11.2.1. Reference page 26 of Operations and Instructions for
Continued Airworthiness (ICA) Manual
11-11.2.2. Test IAW Para 2.3
11-11.3. Propeller - 2016
Ref: Propeller Owner’s Manual 115N. If routinely exposed to aerobatic
flight, 1000 hours, otherwise 2400 hours or 72 months whichever comes
first.
11-12
Section 11 – Logging Info
08-22-2013