PILOT’S CHECKLIST
CIRRUS SR20
With Avidyne R9
SR 20 Quick Reference Checklist
The procedures in this publication are abbreviated and derived from the
procedures in the FAA Approved Airplane Flight Manual and Pilot’s
Operating Handbook (POH) and the supplements contained therein. These
procedures do not supersede the procedures in the basic POH. In the
event of conflict, the basic POH shall take precedence.
Date
05/10/2010
03/15/2011
Change
Original
Revision 1
Record of Revision
Page(s)
W-1, Back Cover
Action
Replace
SR20 Normal Checklist
Normal Checklist
Airspeeds For Normal Operations ..........................................................N-1
Preflight Inspection ...............................................................................N-2
Before Starting Engine ...........................................................................N-5
Starting Engine ......................................................................................N-6
Definitions of Types of Starts ................................................................. N-7
Before Taxiing .......................................................................................N-8
Taxiing................................................................................................... N-8
Before Takeoff.......................................................................................N-9
Normal Takeoff ................................................................................... N-10
Short Field Takeoff .............................................................................. N-10
Climb................................................................................................... N-10
Cruise .................................................................................................. N-10
Cruise Leaning ..................................................................................... N-11
Descent ............................................................................................... N-11
Before Landing .................................................................................... N-12
Balked Landing/Go-Around ................................................................. N-12
After Landing....................................................................................... N-12
Shutdown ............................................................................................ N-12
Original
N-i
Normal Procedures
SR20 Normal Checklist
AIRSPEEDS FOR NORMAL OPERATIONS
Takeoff Rotation:
Normal, Flaps 50% ......................................................................67 KIAS
Short Field, Flaps 50% .................................................................65 KIAS
Obstacle Clearance, Flaps 50%....................................................75 KIAS
Enroute Climb, Flaps Up:
Normal, SL ................................................................................105 KIAS
Normal, 10,000’..........................................................................95 KIAS
Best Rate of Climb, SL .................................................................96 KIAS
Best Rate of Climb, 10,000’ .........................................................91 KIAS
Best Angle of Climb, SL ...............................................................81 KIAS
Best Angle of Climb, 10,000’ .......................................................85 KIAS
Landing Approach:
Normal Approach, Flaps Up ........................................................85 KIAS
Normal Approach, Flaps 50% ......................................................80 KIAS
Normal Approach, Flaps 100% ....................................................75 KIAS
Short Field, Flaps 100% ...............................................................75 KIAS
Go-Around, Flaps 50%:
Full Power ..................................................................................75 KIAS
Maximum Recommended Turbulent Air Penetration:
3000 Lb ....................................................................................131 KIAS
2600 Lb ....................................................................................122 KIAS
2200 Lb ....................................................................................111 KIAS
Maximum Demonstrated Crosswind Velocity:
Takeoff or Landing ..................................................................... 21 Knot
Original
N-1
Normal Procedures
SR20 Normal Checklist
1.
PREFLIGHT INSPECTION - CABIN
Cabin
a. Required Documents .....................................................On Board
b. Avionics Power Switch ........................................................... OFF
c. Bat 2 Master Switch ............................................................... ON
d. PFD (left IFD) ................................................................. Verify On
e. Avionics Cooling Fan ........................................................ Audible
f.
g.
Voltmeter ................................................................... 23-25 Volts
Flap Position Light ................................................................ OUT
h.
i.
Bat 1 Master Switch ............................................................... ON
Lights ................................................................ Check Operation
j.
k.
l.
m.
Stall Warning ......................................................................... Test
Fuel Quantity...................................................................... Check
Fuel Selector ...................................................Select Fullest Tank
IFD System page/Sensor tab ................. VERIFY Required systems
....................................................................................OK (green)
Flaps.......................................................... 100%, Check Light ON
Bat 1 and 2 Master Switches.................................................. OFF
n.
o.
(Continued on following page)
Original
N-2
Normal Procedures
SR20 Normal Checklist
2.
3.
4.
5.
6.
PREFLIGHT INSPECTION – (Continued)
p. Alternate Static Source .................................................. NORMAL
q. Circuit Breakers ........................................................................ IN
r. Fire Extinguisher........................................ Charged and Available
s. Emergency Egress Hammer ........................................... Available
Left Fuselage
a. COM 1 Antenna (top) ......................... Condition and Attachment
b. Wing/Fuselage Fairing ........................................................ Check
c. COM 2 Antenna (underside) ............... Condition and Attachment
d. Baggage Door .................................................. Closed and Secure
e. Static Button .................................................. Check for Blockage
f. Parachute Cover .............................................. Sealed and Secure
Empennage
a. Tiedown ..........................................................................Remove
b. Horizontal and Vertical Stabilizers ................................ Condition
c. Elevator and Tab ................................. Condition and Movement
d. Rudder .................................................... Freedom of Movement
e. Rudder Trim Tab ....................................... Condition and Security
f. Attachment hinges, bolts and cotter pins .......................... Secure
Right Fuselage
a. Static Button .................................................. Check for Blockage
b. Wing/Fuselage Fairings....................................................... Check
Right Wing Trailing Edge
a. Flap and Rub Strips (If installed)................ Condition and Security
b. Aileron and Tab ................................... Condition and Movement
c. Hinges, actuation arm, bolts, and cotter pins ..................... Secure
Right Wing Tip
a. Tip ............................................................................. Attachment
b. Strobe, Nav Light and Lens ....................... Condition and Security
c. Fuel Vent (underside) ............................................. Unobstructed
(Continued on following page)
Original
N-3
Normal Procedures
SR20 Normal Checklist
PREFLIGHT INSPECTION – (Continued)
7. Right Wing Forward and Main Gear
a. Leading Edge and Stall Strips ........................................ Condition
b. Fuel Cap ............................................ Check Quantity and Secure
c. Fuel Drains (2 underside) .................................. Drain and Sample
d. Wheel Fairings...........................Security, Accumulation of Debris
e. Tire............................................... Condition, Inflation, and Wear
f. Wheel and Brakes...............Fluid Leaks, Evidence of Overheating,
.................................................... General Condition and Security
g. Chocks and Tiedown Ropes .............................................Remove
h. Cabin Air Vent ........................................................ Unobstructed
8. Nose, Right Side
a. Cowling ........................................................ Attachments Secure
b. Exhaust Pipe ........................... Condition, Security, and Clearance
c. Transponder Ant. (underside) ............. Condition and Attachment
d. Gascolator (underside) ..................... Drain for 3 seconds, Sample
9. Nose Gear, Propeller, and Spinner
a. Tow Bar ........................................................... Remove and Stow
b. Strut ............................................................................. Condition
c. Wheel Fairing ............................Security, Accumulation of Debris
d. Wheel and Tire ............................. Condition, Inflation, and Wear
e. Propeller .............................. Condition (indentations, nicks, etc.)
f. Spinner........................................... Condition, Security, Oil Leaks
g. Air Inlets ................................................................. Unobstructed
h. Alternator Belt ......................................... Condition and Tension
10. Nose, Left Side
a. Landing Light ................................................................ Condition
b. Engine Oil ................. Check 6-8 quarts, Leaks, Cap & Door Secure
c. Cowling ........................................................ Attachments Secure
d. External Power ......................................................... Door Secure
(Continued on following page)
Original
N-4
Normal Procedures
SR20 Normal Checklist
PREFLIGHT INSPECTION – (Continued)
e. Exhaust Pipe(s) ....................... Condition, Security, and Clearance
11. Left Main Gear and Forward Wing
a. Wheel Fairing ............................Security, Accumulation of Debris
b. Tire............................................... Condition, Inflation, and Wear
c. Wheel and Brakes...............Fluid Leaks, Evidence of Overheating,
.................................................... General Condition and Security
d. Chocks and Tiedown Ropes .............................................Remove
e. Fuel Drains (2 underside) .................................. Drain and Sample
f. Cabin Air Vent ........................................................ Unobstructed
g. Fuel Cap ............................................ Check Quantity and Secure
h. Leading Edge and Stall Strips ........................................ Condition
12. Left Wing Tip
a. Fuel Vent (underside) ............................................. Unobstructed
b. Pitot Mast (underside) ...................... Cover Removed, Tube Clear
c. Strobe, Nav Light and Lens ....................... Condition and Security
d. Tip ............................................................................. Attachment
13. Left Wing Trailing Edge
a. Flap And Rub Strips (If installed) ............... Condition and Security
b. Aileron .................................................... Freedom of movement
c. Hinges, actuation arm, bolts, and cotter pins ..................... Secure
1.
2.
3.
4.
5.
6.
7.
BEFORE STARTING ENGINE
Preflight Inspection .......................................................... COMPLETED
Personal Minimums ............................................................REVIEWED
Aircraft Performance ..........................................................REVIEWED
IMSAFE Checklist................................................................. REVIEWED
Emergency Equipment ....................................................... ON BOARD
Passengers ............................................................................. BRIEFED
Seats, Seat Belts, and Harnesses ............................. ADJUST & SECURE
8.
CAPS Handle ................................................................. PIN REMOVED
Original
N-5
Normal Procedures
SR20 Normal Checklist
1.
2.
3.
4.
5.
6.
7.
8.
9.
STARTING ENGINE
External Power (If applicable) .............................................. CONNECT
Brakes........................................................................................ HOLD
Bat Master Switches ................................................. ON (Check Volts)
IFD View ................................................ VERIFY engine data displayed
Strobe Lights .................................................................................. ON
Navigation Lights ........................................................................... ON
Mixture ............................................................................... FULL RICH
Power Lever ................................................................FULL FORWARD
Fuel Pump............................................................ PRIME, then BOOST
NOTE: Minimize delay between priming and cranking to less than a
few seconds during all starting attempts. Limit starting attempts to 3
tries with no more than 10 seconds of cranking time each.
Warm Start .............................................No priming, just boost
First Start of the Day “Cool Engine” ........ 2 seconds of prime then boost
Cold Start “Cold Soaked” ........................10 seconds of prime then boost
Flooded Start ..........................................See next page for procedure
10.
11.
12.
13.
14.
15.
16.
17.
18.
19.
Propeller Area........................................................................... CLEAR
Power Lever ........................................................................ OPEN 1/4"
Ignition Switch .............................. START (Release after engine starts)
Power Lever ...................................... RETARD (to maintain 1000 RPM)
Oil Pressure .............................................................................. CHECK
Alt Master Switches ....................................................................... ON
Avionics Power Switch ................................................................... ON
Engine Parameters ...............................................................MONITOR
External Power (if applicable).......................................... DISCONNECT
Amps Volts/Indication............................................................... CHECK
Original
N-6
Normal Procedures
SR20 Normal Checklist
DEFINITIONS OF TYPES OF STARTS
Warm Start – If the aircraft has flown within the last hour or two and the
engine oil on the dipstick is warm or hot to the touch then the engine is
warm.
First Start of the Day – If the engine is cool to the touch and the oil on the
dipstick is cool to the touch then the engine will need to be primed for the
start. This would be typical of an aircraft that has just been pulled out of
the hangar for the first flight of the day.
Cold “Cold Soaked” Start (winter operations) – If the aircraft has been
sitting in temperatures of ≤ 20° F (-7° C) for a period of more than two
hours then the engine is “Cold Soaked” and will need to be primed at least
10 seconds and then boost for the start. Be sure the oil pressure comes up
within 60 seconds after start. If it doesn’t, shut down the engine and
inform maintenance. If the engine fires but fails to start and the firing
diminishes in strength, the spark plugs have most likely become frosted
and the aircraft must then be preheated to alleviate this problem.
Flooded Start – If you have primed the engine and the presence of fuel
under the aircraft is visible then you most likely have a flooded engine.
Over priming is also evident by weak firing and puffs of black smoke from
the exhaust stack. A flooded engine could possibly cause an engine fire on
start. You should review the “Engine Fire During Start” checklist before
continuing with a flooded start.
Flooded Start Procedure
1. Fuel Pump...................................................................................... Off
2. Allow fuel to drain from intake tubes .........................(10-20 seconds)
3. Mixture .............................................................................. Idle Cutoff
4. Throttle ......................................................................................... Full
5. Crank Engine to Clear Fuel
If engine fires, retard throttle and slowly advance the mixture to full
rich. As the engine begins to run advance the throttle slightly to keep
the engine running.
If engine does not start, perform “First Start of the Day” procedure.
Original
N-7
Normal Procedures
SR20 Normal Checklist
1.
2.
3.
4.
BEFORE TAXIING AND TAXIING
Flaps ....................................................................................... UP (0%)
Radios/Avionics ............................................................. AS REQUIRED
Cabin Heat/Defrost ........................................................ AS REQUIRED
Fuel Selector ................................................................. SWITCH TANK
1.
TAXIING
Parking Brake .................................................................... DISENGAGE
2.
3.
Brakes....................................................................................... CHECK
Primary Flight Information Operation ....................................... CHECK
4.
Stand-by Instruments Operation ............................................... CHECK
Original
N-8
Normal Procedures
SR20 Normal Checklist
BEFORE TAKEOFF
1.
2.
3.
4.
5.
6.
7.
8.
9.
10.
11.
12.
13.
14.
15.
16.
17.
18.
19.
20.
21.
22.
23.
24.
25.
26.
27.
Left IFD View............................................................. VERIFY PFD page
Right IFD View.................................. VERIFY ENGINE DATA DISPLAYED
Doors .................................................................................... LATCHED
CAPS Handle ......................................................... Verify Pin Removed
Seat Belts and Shoulder Harnesses.......................................... SECURE
Fuel Quantity ....................................................................... CONFIRM
Fuel Selector ................................................................. FULLEST TANK
Fuel Pump...................................................................................... ON
Flaps ........................................................................SET 50% & CHECK
Transponder .................................................................................. SET
Autopilot .................................................................................. CHECK
FMS or NAV Radios ........................................................................ SET
Cabin Heat/Defrost ........................................................ AS REQUIRED
Brakes........................................................................................ HOLD
Power Lever ........................................................................ 1700 RPM
Alternator ................................................................................. CHECK
a. Pitot Heat ............................................................................... ON
b. Navigation Lights .................................................................... ON
c. Landing Light .......................................................................... ON
d. IFD Caution/Warnings ....................................................... CHECK
Voltage ..................................................................................... CHECK
Pitot Heat ...................................................................... AS REQUIRED
Navigation Lights ........................................................... AS REQUIRED
Landing Light ................................................................. AS REQUIRED
Magnetos .......................................................... CHECK Left and Right
Verify RPM drop does not exceed 150 RPM for either magneto and
RPM differential does not exceed 75 RPM.
Engine Parameters .................................................................... CHECK
Power Lever ........................................................................ 1000 RPM
Primary Flight Information, Altimeter setting .................. CHECK & SET
Flight Controls........................................................... FREE & CORRECT
Trim .................................................................................. SET Takeoff
Autopilot ........................................................................ DISCONNECT
Original
N-9
Normal Procedures
SR20 Normal Checklist
1.
2.
3.
4.
5.
NORMAL TAKEOFF
Brakes............................................. RELEASE (Steer with Rudder Only)
Power Lever ................................................................FULL FORWARD
Engine Parameters .................................................................... CHECK
Elevator Control ................................. ROTATE Smoothly at 65-70 KIAS
At 85 KIAS, Flaps ............................................................................. UP
SHORT FIELD TAKEOFF
1.
2.
Flaps .............................................................................................50%
Brakes........................................................................................ HOLD
3.
4.
Power Lever ................................................................FULL FORWARD
Engine Parameters .................................................................... CHECK
5.
6.
7.
Brakes............................................. RELEASE (Steer with Rudder Only)
Elevator Control ...................................... ROTATE Smoothly at 65 KIAS
Airspeed at Obstacle ................................................................75 KIAS
1.
2.
3.
4.
5.
6.
CLIMB
IFD View .......................................... VERIFY ENGINE DATA DISPLAYED
Climb Power .................................................................................. SET
Flaps ..................................................................................... Verify UP
Mixture ............................................................................... FULL RICH
Engine Parameters .................................................................... CHECK
Fuel Pump..................................................................................... OFF
1.
2.
3.
4.
5.
CRUISE
Fuel Pump..................................................................................... OFF
Cruise Power.................................................................................. SET
Mixture .....................................................................LEAN as required
Engine Parameters ...............................................................MONITOR
Fuel Flow and Balance..........................................................MONITOR
Original
N - 10
Normal Procedures
SR20 Normal Checklist
CRUISE LEANING
Mixture Description
Exhaust Gas Temperature
Best Power
75 ° F Rich of Peak EGT
Best Economy
50 ° F Lean of Peak EGT
WMU recommends the use of 65% to 75% power during cruise operations.
Unless safety reasons dictate otherwise, the aircraft should be leaned to
Best Power rather than Best Economy.
1.
2.
3.
4.
5.
6.
DESCENT
Altimeter ....................................................................................... SET
Cabin Heat/Defrost ........................................................ AS REQUIRED
Landing Light ................................................................................. ON
Fuel System .............................................................................. CHECK
Mixture .......................................................................... AS REQUIRED
Brake Pressure .......................................................................... CHECK
Original
N - 11
Normal Procedures
SR20 Normal Checklist
1.
2.
3.
4.
5.
6.
BEFORE LANDING
IFD View .......................................... VERIFY ENGINE DATA DISPLAYED
Seat Belt and Shoulder Harness............................................... SECURE
Fuel Pump................................................................................ BOOST
Mixture ............................................................................... FULL RICH
Flaps .............................................................................. AS REQUIRED
Autopilot .......................................................................... DISENGAGE
1.
BALKED LANDING / GO-AROUND
Autopilot ............................................................................ Disengage
2.
3.
Power Lever ................................................................FULL FORWARD
Flaps .............................................................................................50%
4. Airspeed .............................................................................81-83 KIAS
After clear of obstacles:
5. Flaps ............................................................................................... UP
1.
2.
3.
4.
5.
6.
AFTER LANDING
Power Lever ........................................................................ 1000 RPM
Fuel Pump..................................................................................... OFF
Flaps ............................................................................................... UP
Transponder ................................................................................STBY
Lights ............................................................................. AS REQUIRED
Pitot Heat ..................................................................................... OFF
1.
2.
3.
4.
5.
6.
7.
8.
SHUTDOWN
Fuel Pump (if used) ....................................................................... OFF
Throttle ....................................................................................... IDLE
Ignition Switch ................................ CYCLE - MAG GROUNDING CHECK
Mixture ................................................................................... CUTOFF
All Switches................................................................................... OFF
Magnetos ..................................................................................... OFF
ELT .................................................................. TRANSMIT LIGHT OUT
Chocks, Tie-downs, Pitot Covers ..................................... AS REQUIRED
Original
N - 12
Normal Procedures
Intentionally
Left
Blank
WMU Practice Areas and Safety of Flight
WMU Practice Areas and Safety of Flight
BTL Taxi Diagram .................................................................................. W-1
BTL Departure Procedures .................................................................... W-2
BTL Practice Areas ................................................................................ W-3
Alpha Practice Area .............................................................................. W-4
Bravo Practice Area .............................................................................. W-5
Charlie Practice Area ............................................................................ W-6
Delta Practice Area ............................................................................... W-7
BTL Gates ............................................................................................. W-8
Arrival Gate Holding Procedures ........................................................... W-9
Lost Procedures .................................................................................. W-10
Intercept Procedures .......................................................................... W-11
Loss of Communications ..................................................................... W-13
Light Gun Signals ................................................................................ W-14
Wind Component Chart ...................................................................... W-15
Flight Plan Form ................................................................................. W-16
PIREP Form......................................................................................... W-17
WMU FOM Airfield and Runway Length Requirements ....................... W-18
Original
W-i
WMU Procedures
WMU Practice Areas and Safety of Flight
BTL TAXI DIAGRAM
FREQUENCIES
ATIS
128.325
GROUND
121.70
TWR/CTAF
126.825
AZO APP/DEP (R)
(0600-2300)
119.20
CHICAGO CENTER
(2300-0600)
127.55
VOR
109.40
UNICOM
122.95
FSS
122.20
Revision 1
CAUTION: BE ALERT TO RUNWAY CROSSING
CLEARANCES.
READBACK OF ALL
RUNWAY HOLDING INSTRUCTIONS IS
REQUIRED.
W-1
WMU Procedures
WMU Practice Areas and Safety of Flight
BTL DEPARTURE PROCEDURES
Climb to 3000’
MSL
1/2 mile and
2000’ MSL
Departure End
After takeoff when remaining in
the pattern at BTL, no turns shall
be made until the aircraft is at
least 1/2 mile past the departure
end and within 300’ of pattern
altitude unless approved otherwise
by ATC. (WMU 91.331(C))
Original
After takeoff when departing from BTL
airport, initial turns from the runway
heading should be initiated when the
aircraft is at least 1/2 mile beyond the
departure end of the runway and at
least 2000’ MSL. You should continue to
climb as you turn on course to at least
3000’ MSL (weather permitting) to
depart the airport traffic pattern to
avoid arrival traffic at lower altitudes.
(WMU91.331(D))
W-2
WMU Procedures
WMU Practice Areas and Safety of Flight
BTL PRACTICE AREAS
25 NM
D
Spartan
C
A
B
Wolverine
25 NM
Departure Directions
ALPHA – South
CHARLIE – East
Original
BRAVO – Southeast
DELTA - Northwest
W-3
WMU Procedures
WMU Practice Areas and Safety of Flight
ALPHA PRACTICE AREA
1
2
4
3
A
7
5
Wolverine
6
25 NM
Gates & Visual Reference Points
1 – East Gate
3 – Athens
5 – Union City
7 – Tekonsha
Original
2 – South Gate
4 – Turtle Lake
6 – Coldwater
W-4
WMU Procedures
WMU Practice Areas and Safety of Flight
BRAVO PRACTICE AREA
1
2
B
3
25 NM
4
5
7
6
Gates & Visual Reference Points
1 – Marshal Airport
3 – Homer
5 – Litchfield
7 – Quincy
Original
2 – Albion
4 – Tekonsha
6 – Hillsdale
W-5
WMU Procedures
WMU Practice Areas and Safety of Flight
CHARLIE PRACTICE AREA
5
4
3
C
2
25 NM
1
Gates & Visual Reference Points
1 – East Gate
3 – Olivet
5 – Charlotte
Original
2 – Duck Lake
4 – Eaton Rapids
W-6
WMU Procedures
WMU Practice Areas and Safety of Flight
DELTA PRACTICE AREA
7
25 NM
6
D
4
2
3
5
1
Gates & Visual Reference Points
1 – North Gate
2 – Gull Lake
3 – Gilmore Farms
4 – Wall Lake
5 – Dowling Noise Abatement Area
6 – Gun Lake
7 – Hastings
Original
W-7
WMU Procedures
WMU Practice Areas and Safety of Flight
BTL GATES
Spartan
D
C
B
A
Wolverine
Gate
North Gate
East Gate
South Gate
West Gate
Original
Location
Fine Lake
Exit 104 & I-94
East Leroy
Galesburg
W-8
Bearing
R-350
R-096
R-169
R-262
Distance
8.2 nm
7.7 nm
8.9 nm
7.3 nm
WMU Procedures
WMU Practice Areas and Safety of Flight
Arrival Gate
Holding
Procedures
On Company Frequency:
[South] Gate Traffic,
Western XX Entering
the Hold at the
[South] Gate
Seconds
Fly For 60
On Company Frequency
[South] Gate Traffic,
Western XX two miles
East of the [South] Gate
Switching to Tower
Turn
Left 90
Degrees
Turn
Left 90
Degrees
Fly
Until
Abeam
Gate
Turn
Left 90
Degrees
On Battle Creek Tower
Western XX, Seven [South],
inbound for pattern work
with [November].
Fly to Gat
e
~2
NM
On Company Frequency:
[South] Gate Traffic,
Western XX In the Hold,
Proceeding to the [South] Gate
Original
W-9
WMU Procedures
WMU Practice Areas and Safety of Flight
Lost Procedures
The following are basic guidelines to consider in the event of becoming
lost:
1.
Maintain Positive Aircraft control at all times.
2.
Check heading indicator with the magnetic compass. Reset heading
indicator as necessary (if applicable to aircraft).
3.
Maintain original heading, or circle present position over a prominent
landmark.
4.
If at low altitude, climb to a higher altitude.
5.
Using GPS: Navigate to nearest airport
6.
Using the sectional chart, attempt to locate and identify any
prominent landmark.
7.
Using available Navaids (VOR triangulation, GPS) to determine
position.
8.
If unable to determine position, commit to the six C’s:
1.
2.
3.
4.
5.
6.
9.
CONFESS – Admit to yourself you are lost.
CLIMB – Climb to avoid obstructions, gain better visibility and
radio reception.
CIRCLE – Pick a nearby landmark and stay in the general vicinity of
the landmark.
COMMUNICATE – Talk to ATC/FSS.
COMPLY – Follow ATC/FSS instructions.
CONSERVE – Monitor fuel available.
If unable to determine a facility frequency, or unable to establish radio
contact, transmit the situation on frequency 121.50 MHz (emergency).
Original
W - 10
WMU Procedures
WMU Practice Areas and Safety of Flight
IN-FLIGHT INTERCEPT PROCEDURES
If you are intercepted by a U.S. Military or law enforcement aircraft, immediately:
1. Follow the instructions given by the intercepting aircraft. (See chart below)
2. Notify ATC, if possible
3. Attempt to communicate with ATC on the emergency frequency 121.5 MHz, giving the identity and
position of your aircraft and the nature of the flight.
4. If equipped with a transponder, squawk 7700, unless otherwise instructed by ATC. If any instructions
received by radio from any sources conflict with those given by the intercepting aircraft by visual or
radio signals, request clarification while continuing to comply with the instructions given by the
intercepting aircraft.
I understand and
will comply.
Meaning
Rocks wings and follows.(Also, at
night, flashes navigational lights.)
I understand and
will comply.
Intercepted aircraft response
You have
been
intercepted.
Rocks Wings.
Meaning
Rock wings. After acknowledgement
initiates a slow level turn, normally
to the left, into the desired heading.
(Also, at night flashes the
navigational lights>)
You may
proceed
Intercepting aircraft signals
Performs an abrupt breakaway
maneuver consisting of a climbing 90
degree turn, or more, without
crossing the intercepted aircraft’s
flight path.
WMU Procedures
W - 11
Original
Original
W - 12
In Distress
Cannot
Comply
DAY or NIGHT-Regular switching on
and off of all available lights but in
such a manner as to be distinct from
flashing lights.
DAY or NIGHT-Irregular flashing of all
available lights.
Aerodrome
you have
designated is
inadequate
Meaning
Intercepted aircraft signals
Raises landing gear while flying over
runway between 1,000’ and 2,000’ and
continues to circle the airport. (Also,
at night, will also flash landing light.)
Lowers landing gear, follows the
intercepting aircraft and lands if
the runway is considered safe.
(Also at night shows steady
landing lights on.)
Land at this
airport
Circles airport, lowers landing gear,
and overflies runway in the direction of
landing (Also at night shows steady
landing lights on.)
Performs an abrupt breakaway
maneuver
Understood
Understood
Understood, you
may proceed
Performs an abrupt breakaway
maneuver
Performs an abrupt breakaway
maneuver
Understood,
follow me
Meaning
I understand and
will comply.
Meaning
Rock wings followed by a slow
level turn.
Intercepting aircraft response
Intercepted aircraft response
Meaning
Intercepting aircraft signals
IN-FLIGHT INTERCEPT PROCEDURES (cont.)
WMU Practice Areas and Safety of Flight
WMU Procedures
WMU Practice Areas and Safety of Flight
Loss Of Communication
Immediate Action Items
• Fly the airplane / Remain Calm
• Check the volume controls and audio panel settings
• Check for stuck microphone
• Check microphone/headset jacks and plugs
• Check circuit breakers and electrical system status
VFR Conditions: if the failure occurs in VFR conditions, or if VFR conditions are
encountered after the failure, each pilot shall remain under VFR and land as soon
as practical.
IFR Conditions: if the failure occurs in IFR conditions,
A) Route.
(1) Route ASSIGNED in the last ATC clearance received
(2) If being VECTORED, by the direct route from the point of radio
failure to the fix, route, or airway specified in the vector
clearance.
(3) In the absence of an assigned route, by the route that ATC has
advised may be EXPECTED in a further clearance.
(4) In the absence of the above, by the route FILED in the flight plan.
B) Altitude. At the highest of the following altitudes or flight levels for
the route segment being flown
(1) The MINIMUM ALTITUDE for IFR operations
(2) The altitude ATC has advised may be EXPECTED in a further
clearance.
(3) The altitude or flight level ASSIGNED in the last ATC clearance
received
C) Leave clearance limit.
(4) When the clearance limit is a fix from which an approach begins,
commence descent or descent and approach as close as possible
to the EFC time if one has been received, or if one has not been
received, as close as possible to the ETA as calculated from the
filed or amended (with ATC) estimated time en route.
(5) If the clearance limit is not a fix from which an approach begins,
leave the clearance limit at the EFC time if one has been
received, or if none has been received, upon arrival over the
clearance limit, and proceed to a fix from which an approach
begins and commence descent or descent and approach as close
as possible to the ETA as calculated from the filed or amended
(with ATC) estimated time en route.
Original
W - 13
WMU Procedures
WMU Practice Areas and Safety of Flight
Light Gun Signals
Color and type of
signal
Meaning with
respect to aircraft on
the surface
Meaning with
respect to aircraft
in flight
Steady GREEN
Cleared for
Takeoff
Cleared to land
Flashing GREEN
Cleared to taxi
Return for landing
(to be followed by
steady green at
proper time)
Steady RED
Stop
Give way to other
aircraft and
continue circling
Flashing RED
Taxi clear of
runway in use
Airport unsafe –
do not land
Flashing WHITE
Return to starting
point on airport
Not applicable
Alternating RED
and GREEN
Exercise extreme
caution
Exercise extreme
caution
Original
W - 14
WMU Procedures
WMU Practice Areas and Safety of Flight
Wind Components Chart
Original
W - 15
WMU Procedures
WMU Practice Areas and Safety of Flight
Flight Plan Form
Original
W - 16
WMU Procedures
WMU Practice Areas and Safety of Flight
Flight Watch 122.00 MHz; FSS 122.20 MHZ and as published
Original
W - 17
WMU Procedures
WMU Practice Areas and Safety of Flight
WMU FOM Airfield and Runway Length Requirements
General Limitations – Minimum Runway Length
• C-150, C-172 and Piper Cub aircraft...................................... 2,500’
• All other aircraft................................................................... 3,000’
• For all aircraft, the runway length must double the calculated A/C
performance distance
Sod Fields and Unpaved Runways
• Only those fields approved i.a.w. the FOM
Intersection departure Limitations
• Single-Engine ................. At least 4000’ remaining useable runway
• Multi-Engine ............................ Remaining Runway must be within
balanced field length for A/C
Touch and Go Limitations
• Non-Complex Aircraft ............................................... At least 3000’
• * Complex Aircraft .................................................... At least 4500’
* Complex aircraft are also limited to dual daytime operations and
only for a maximum of three consecutive pattern operations.
Stop and Go Limitations
• Single Engine..At least 4000’ remaining useable runway for takeoff
• Multi-Engine ............................ Remaining Runway must be within
balanced field length for A/C
Original
W - 18
WMU Procedures
Intentionally
Left
Blank
SR20 Abnormal Checklist
Abnormal Checklist
Brake Failure During Taxi ....................................................................... A-1
Aborted Takeoff .................................................................................... A-1
Inadvertent Icing Encounter .................................................................. A-2
Inadvertent IMC encounter ................................................................... A-2
Door Open in Flight ............................................................................... A-2
Landing with Failed Brakes .................................................................... A-3
Landing with a Flat Tire.......................................................................... A-3
Alternator Failure .................................................................................. A-4
Engine Indicating Failure........................................................................ A-4
Low MBUS or Low EBUS Alerts .............................................................. A-4
Communications Failure ........................................................................ A-5
Pitot Static Malfunction ......................................................................... A-5
Electric Trim/Autopilot Failure............................................................... A-5
Original
A-i
Abnormal Procedures
SR20 Abnormal Checklist
GROUND PROCEDURES
BRAKE FAILURE DURING TAXI
1. Engine Power ................................................................. AS REQUIRED
2. Directional Control ...................................... MAINTAIN WITH RUDDER
3. Brake Pedal(s) ............................................................................PUMP
If directional control can not be maintained:
4. Mixture ................................................................................... CUTOFF
1.
2.
ABORTED TAKEOFF
Power Lever ................................................................................. IDLE
Brakes............................................................................ AS REQUIRED
Original
A-1
Abnormal Procedures
SR20 Abnormal Checklist
IN-FLIGHT PROCEDURES
1.
2.
3.
4.
5.
INADVERTENT ICING ENCOUNTER
Pitot Heat ...................................................................................... ON
Exit icing conditions. Turn back or change altitude
Cabin Heat ......................................................................... MAXIMUM
Windshield Defrost ............................................................ FULL OPEN
Alternate Induction Air................................................................... ON
INADVERTENT IMC ENCOUNTER
1.
2.
Airplane Control.............................. Establish Straight and Level Flight
Autopilot ................................... Engage to hold Heading and Altitude
3.
Heading ............................................ Reset to initiate 180 degree turn
1.
2.
DOOR OPEN IN-FLIGHT
Airspeed ........................................................ REDUCE TO 80 - 90 KIAS
Land as soon as practical
Original
A-2
Abnormal Procedures
SR20 Abnormal Checklist
LANDING PROCEDURES
LANDING WITH FAILED BRAKES
One Brake Inoperative
1. Land on side of runway corresponding to the inop brake
2. Maintain directional control using rudder and working brake
Both Brakes Inoperative
1. Divert to the longest, widest runway with the most direct headwind
2. Land on downwind side of the runway
3. Use the rudder for obstacle avoidance
4.
Perform Emergency Engine Shutdown on Ground checklist
LANDING WITH FLAT TIRE
Flat Tire – Main Gear
1. Land on the runway side corresponding to the good tire
2. Maintain directional control with the brakes and rudder
3. Do not taxi. Stop the airplane and perform a normal engine shutdown
Flat Tire - Nose Gear
1. Land in the center of the runway
2. Hold the nosewheel off the ground as long as possible
3. Do not taxi. Stop the airplane and perform a normal engine shutdown
Original
A-3
Abnormal Procedures
SR20 Abnormal Checklist
SYSTEM MALFUNCTIONS
ALTERNATOR FAILURE
Low ALT 1 Message
1. ALT 1 Master Switch ..................................................................... OFF
2. Alternator 1 Circuit Breaker ..................................... CHECK and RESET
3. ALT 1 Master Switch ...................................................................... ON
If alternator does not reset:
4. Switch off unnecessary equipment on Main Bus 1, Main Bus 2, and the
Non-Essential Buses. Monitor voltage
5. ALT 1 Master Switch ..................................................................... OFF
6. Land as soon as practical.
Low ALT 2 Message
1. ALT 2 Master Switch ..................................................................... OFF
2. Alternator 2 Circuit Breaker ..................................... CHECK and RESET
3. ALT 2 Master Switch ...................................................................... ON
If alternator does not reset:
4. Switch off unnecessary equipment on Main Bus 1, Main Bus 2, and
Non-Essential Buses to reduce loads.
5. ALT 2 Master Switch ..................................................................... OFF
6. Land as soon as practical.
1.
2.
ENGINE INDICATING FAILURE
ANNUN / ENGINE INST Circuit Breaker ....................................... CYCLE
Land as soon as practical
1.
LOW MBUS or LOW EBUS ALERTS
Land as soon as possible
Original
A-4
Abnormal Procedures
SR20 Abnormal Checklist
1.
2.
3.
4.
5.
6.
COMMUNICATIONS FAILURE
Keyboard or IFD volume/SQ .......... VERIFY adequate volume w/ SQ off
Audio Panel ..................Verify Tel, Mute or Split comm is not selected
Frequency .............................................................................. CHANGE
Circuit Breakers......................................................................... CHECK
Headset ................................................................................. CHANGE
Hand Held Microphone ........................................................ CONNECT
1.
2.
PITOT STATIC MALFUNCTION
Pitot Heat ...................................................................................... ON
Alternate Static Source .............................................................. OPEN
ELECTRIC TRIM / AUTOPILOT FAILURE
1. Airplane Control............................................... MAINTAIN MANUALLY
2. Autopilot (if engaged) ....................................................... DISENGAGE
If problem is not corrected:
3. Circuit Breakers...................................................... PULL AS REQUIRED
a. PITCH/YAW TRIM
b. ROLL TRIM
c. AUTOPILOT
4. Power Lever ............................................. ADJUST TO CONTROL PITCH
5. Control Yoke ........................................... MANUALLY HOLD PRESSURE
6. Land as soon as practical
Original
A-5
Abnormal Procedures
SR20 Emergency Checklist
Emergency Checklist
AIRSPEEDS FOR EMERGENCY OPERATIONS ............................................ E-1
Maneuvering Speed ....................................................................... E-1
Best Glide ...................................................................................... E-1
Emergency Landing (Engine-Out) ................................................... E-1
Maximum Glide ............................................................................. E-1
GROUND EMERGENCIES ........................................................................ E-2
Engine Fire During Start ................................................................. E-2
Emergency Engine Shutdown On Ground ....................................... E-2
Emergency Ground Egress ............................................................. E-2
IN-FLIGHT EMERGENCIES ....................................................................... E-3
Engine Failure on Takeoff (Low Altitude) ........................................ E-3
Engine Failure In-Flight................................................................... E-3
Engine Airstart ............................................................................... E-3
Engine Partial Power Loss .............................................................. E-4
Low Oil Pressure ............................................................................ E-4
Propeller governor Failure ............................................................. E-4
Smoke and Fume Elimination ......................................................... E-5
Engine Fire In-Flight ....................................................................... E-5
Wing Fire in Flight .......................................................................... E-5
Cabin Fire in Flight ......................................................................... E-6
Emergency Descent ....................................................................... E-7
Inadvertent Spiral Dive During IMC Flight ....................................... E-7
Spins .............................................................................................. E-7
CAPS Deployment .......................................................................... E-7
LANDING EMERGENCIES ........................................................................ E-9
Forced Landing (Engine Out) .......................................................... E-9
Ditching ......................................................................................... E-9
Landing Without Elevator Control ................................................ E-10
SYSTEM MALFUNCTIONS ..................................................................... E-10
IFD - System Failure ..................................................................... E-10
Loss Of Air Data ........................................................................... E-10
Loss Of Attitude Data ................................................................... E-10
Power Lever Linkage Failure......................................................... E-10
Original
E-i
Emergency Procedures
SR20 Emergency Checklist
AIRSPEEDS FOR EMERGENCY OPERATIONS
MANEUVERING SPEED:
3000 LB ..................................................................................131 KIAS
2600 LB ..................................................................................122 KIAS
2200 LB ..................................................................................111 KIAS
BEST GLIDE:
3000 LB ....................................................................................96 KIAS
2500 LB ....................................................................................87 KIAS
EMERGENCY LANDING (ENGINE-OUT)
Flaps Up ...................................................................................86 KIAS
Flaps 50%.................................................................................81 KIAS
Flaps 100% ...............................................................................75 KIAS
MAXIMUM GLIDE
Glide Ratio ≈ 10.9 : 1
Note:
Checklist steps emphasized by underlining such as this:
1. Best Glide Speed ................................................................. ESTABLISH
should be memorized for accomplishment without reference to the
procedure.
Original
E-1
Emergency Procedures
SR20 Emergency Checklist
GROUND EMERGENCIES
ENGINE FIRE DURING START
1.
2.
3.
Mixture ................................................................................... CUTOFF
Fuel Pump..................................................................................... OFF
Fuel Selector ................................................................................. OFF
4.
5.
6.
Power Lever ........................................................................ FORWARD
Starter ..................................................................................... CRANK
If flames persist, perform Emergency Engine Shutdown on Ground and
Emergency Ground Egress checklists
1.
2.
3.
4.
5.
6.
EMERGENCY ENGINE SHUTDOWN ON GROUND
Power Lever ................................................................................. IDLE
Fuel Pump..................................................................................... OFF
Mixture ................................................................................... CUTOFF
Fuel Selector ................................................................................. OFF
Ignition Switch .............................................................................. OFF
Bat-Alt Master Switches ................................................................ OFF
EMERGENCY GROUND EGRESS
1.
2.
3.
Engine.............................................................................. SHUTDOWN
Seat belts ............................................................................... RELEASE
Airplane ........................................................................................EXIT
Original
E-2
Emergency Procedures
SR20 Emergency Checklist
IN-FLIGHT EMERGENCIES
ENGINE FAILURE ON TAKEOFF (LOW ALTITUDE)
1.
2.
3.
Best Glide or Landing Speed (as appropriate) ...................... ESTABLISH
Mixture ................................................................................... CUTOFF
Fuel Selector ................................................................................. OFF
4. Ignition Switch .............................................................................. OFF
5. Flaps ............................................................................. AS REQUIRED
If time permits:
6. Power Lever ................................................................................. IDLE
7. Fuel Pump..................................................................................... OFF
8. Bat-Alt Master Switches ................................................................ OFF
9. Seat Belts ................................................................ ENSURE SECURED
ENGINE FAILURE IN-FLIGHT
1.
2.
3.
4.
5.
6.
7.
Best Glide Speed ................................................................. ESTABLISH
Mixture ............................................................................... FULL RICH
Fuel Selector ................................................................ SWITCH TANKS
Fuel Pump................................................................................ BOOST
Alternate Induction Air................................................................... ON
Ignition Switch ............................................................... CHECK, BOTH
If engine does not start perform Engine Airstart or Forced Landing
checklist
ENGINE AIRSTART
1.
2.
3.
4.
5.
6.
7.
Bat Master Switches ...................................................................... ON
Power Lever ........................................................................1/2" OPEN
Mixture ....................................................................... RICH, AS REQ'D
Fuel Selector ................................................................ SWITCH TANKS
Ignition Switch ........................................................................... BOTH
Fuel Pump................................................................................ BOOST
Alternate Induction Air................................................................... ON
Original
E-3
Emergency Procedures
SR20 Emergency Checklist
8.
9.
10.
11.
12.
Alt Master Switches ...................................................................... OFF
Starter (Propeller not Windmilling) ........................................ ENGAGE
Power Lever .............................................................. slowly INCREASE
Alt Master Switches ....................................................................... ON
If engine will not start perform Forced Landing checklist
1.
2.
3.
4.
5.
6.
7.
ENGINE PARTIAL POWER LOSS
Fuel Pump................................................................................ BOOST
Fuel Selector ................................................................ SWITCH TANKS
Mixture .................................. CHECK appropriate for flight conditions
Power Lever ............................................................................. SWEEP
Alternate Induction Air................................................................... ON
Ignition Switch ............................................................ BOTH, L, then R
Land as soon as practical
1.
2.
LOW OIL PRESSURE
Power Lever .......................................................MINIMUM REQUIRED
Land as soon as possible.
1.
2.
1.
2.
3.
PROPELLER GOVERNOR FAILURE
Propeller RPM will not increase:
Oil Pressure .............................................................................. CHECK
Land as soon as practical
Propeller overspeeds or will not decrease:
Power Lever ........................................ ADJUST (to keep RPM in limits)
Airspeed ................................................................ REDUCE to 80 KIAS
Land as soon as practical
Original
E-4
Emergency Procedures
SR20 Emergency Checklist
SMOKE AND FUME ELIMINATION
1. Heater .......................................................................................... OFF
2. Air Vents .................................................................. OPEN, FULL COLD
3. Prepare to land as soon as possible
If airflow is not sufficient to clear smoke or fumes from cabin:
4. Cabin Doors .............................................................. PARTIALLY OPEN
Airspeed may need to be reduced to partially open door in flight.
1.
2.
3.
4.
5.
6.
ENGINE FIRE IN-FLIGHT
Mixture ................................................................................... CUTOFF
Fuel Pump..................................................................................... OFF
Power Lever ................................................................................. IDLE
Fuel Selector ................................................................................. OFF
Ignition Switch .............................................................................. OFF
Perform Forced Landing checklist
WING FIRE IN-FLIGHT
1.
2.
3.
4.
5.
Pitot Heat Switch .......................................................................... OFF
Navigation Light Switch ................................................................. OFF
Strobe Light Switch ....................................................................... OFF
If possible, slip to keep flames away aircraft structure
Land as soon as possible.
Original
E-5
Emergency Procedures
SR20 Emergency Checklist
CABIN FIRE IN-FLIGHT
Warning:
If in IMC conditions, turn ALT 1, ALT 2, Avionics, and BAT 1 switches OFF.
Power from battery 2 will keep the Primary Flight Display (Left IFD)
operational for about 30 minutes.
1. Bat-Alt Master Switches ................................................ OFF, AS REQ'D
2. Heater .......................................................................................... OFF
3. Air Vents ................................................................................. CLOSED
4. Fire Extinguisher .................................................................. ACTIVATE
If airflow is not sufficient to clear smoke or fumes from cabin:
5. Cabin Doors .............................................................. PARTIALLY OPEN
Airspeed may need to be reduced to partially open door in flight.
6. When fire extinguished, Air Vents ............................ OPEN, FULL COLD
7. Avionics Power Switch .................................................................. OFF
8. All other switches ......................................................................... OFF
9. Land as soon as possible
If setting master switches off eliminated source of fire or fumes and
airplane is in night, weather or IFR conditions:
10. Bat-Alt Master Switches ................................................................. ON
11. Avionics Power Switch ................................................................... ON
12. Activate required systems one at a time. Pause several seconds
between activating each system to isolate malfunctioning system.
Activate only the minimum amount of equipment necessary to
complete a safe landing.
Original
E-6
Emergency Procedures
SR20 Emergency Checklist
1.
2.
3.
EMERGENCY DESCENT
Power Lever ................................................................................. IDLE
Mixture .............................................................................As Required
Airspeed ....................................................................... V NE (200 KIAS)
INADVERTENT SPIRAL DIVE DURING IMC FLIGHT
1.
2.
Power Lever ................................................................................. IDLE
Stop the spiral dive by using coordinated aileron and rudder control
while referring to the attitude indicator and turn coordinator to level
the wings.
3.
Cautiously apply elevator back pressure to bring airplane to level flight
attitude
Trim for level flight.
Set power as required.
Use autopilot if functional otherwise keep hands off control yoke, use
rudder to hold constant heading.
Exit IMC conditions as soon as possible.
4.
5.
6.
7.
INADVERTENT SPIN ENTRY
1.
1.
2.
3.
4.
CAPS ...................................................................................... Activate
CAPS DEPLOYMENT
Airspeed ............................................................. MINIMUM POSSIBLE
The maximum demonstrated deployment speed is 135 KIAS.
Mixture (If time and altitude permit)....................................... CUTOFF
Activation Handle Cover........................................................ REMOVE
Activation Handle (Both Hands) .......................PULL STRAIGHT DOWN
Pull activation T-handle from its holder. Clasp both hands around the
handle and pull straight down in a strong, steady and continuous
motion. Maintain maximum pull force until the rocket activates. Pull
forces up to, or exceeding, 45 pounds may be required. Bending of the
handle-housing mount is to be expected.
Warning: Jerking or rapidly pulling on the activation T-handle will
greatly increase the pull forces required to activate rocket.
Original
E-7
Emergency Procedures
SR20 Emergency Checklist
5.
6.
7.
8.
9.
10.
11.
12.
13.
14.
Use a firm and steady pulling motion – a chin-up type pull
enhances successful activation.
After deployment:
Mixture ....................................................................... CHECK, CUTOFF
Fuel Selector ................................................................................. OFF
Bat- Alt Master Switches ............................................................... OFF
Ignition Switch .............................................................................. OFF
Fuel Pump..................................................................................... OFF
ELT ................................................................................................. ON
Seat Belts and Harnesses ...................................................... TIGHTEN
Loose Items ............................................................................ SECURE
Assume emergency landing body position
After the airplane comes to a complete stop, evacuate quickly and
move upwind
Original
E-8
Emergency Procedures
SR20 Emergency Checklist
LANDING EMERGENCIES
FORCED LANDING (ENGINE OUT)
1.
2.
3.
Best Glide Speed ................................................................. ESTABLISH
Radio .................................................. Transmit (121.5 MHz) MAYDAY
Transponder ................................................................ SQUAWK 7700
4.
5.
6.
7.
8.
9.
10.
11.
12.
If off airport, ELT .................................................................. ACTIVATE
Power Lever ................................................................................. IDLE
Mixture ................................................................................... CUTOFF
Fuel Selector ................................................................................. OFF
Ignition Switch .............................................................................. OFF
Fuel Pump..................................................................................... OFF
Flaps (when landing is assured) ................................................... 100%
Master Switches ........................................................................... OFF
Seat Belt(s) ........................................................................... SECURED
1.
2.
3.
4.
5.
DITCHING
Radio .................................................. Transmit (121.5 MHz) MAYDAY
Transponder ................................................................ SQUAWK 7700
CAPS .................................................................................... ACTIVATE
If available, life preservers should be donned and life raft should be
prepared for immediate evacuation upon touchdown. Consider
unlatching a door prior to assuming the emergency landing body
position in order to provide a ready escape path.
Airplane ..............................................................................EVACUATE
It may be necessary to allow some cabin flooding to equalize pressure
on the doors. If the doors cannot be opened, break out the windows
with the egress hammer and crawl through the opening.
Flotation Devices ........................ INFLATE WHEN CLEAR OF AIRPLANE
Original
E-9
Emergency Procedures
SR20 Emergency Checklist
1.
2.
3.
LANDING WITHOUT ELEVATOR CONTROL
Flaps ...................................................................................... SET 50%
Trim .................................................................................. SET 80 KIAS
Power ............................................... AS REQUIRED FOR GLIDE ANGLE
IFD - SYSTEM FAILURE
1. Stand-by instruments ................Reference to maintain aircraft control
In the unlikely event of an IFD failure, the pilot does not lose the ability to
control the autopilot through the remaining IFD controls. If this
malfunction occurs, the pilot may continue flight using remaining IFD and
operational autopilot.
2.
If attitude data is not available on the remaining IFD
a. Autopilot GPSS Mode ................................................... ACTIVATE
b. Autopilot Altitude Hold................................................. ACTIVATE
c.
If failure occurs while flying in IMC ................................ EXIT IMC
1.
2.
LOSS of AIR DATA
Standby Instruments (altitude, airspeed) .............................MONITOR
If failure occurs while flying in IMC ........................................ EXIT IMC
3.
4.
5.
6.
LOSS of ATTITUDE DATA
Standby Instruments (attitude, heading) ..............................MONITOR
Autopilot GPSS Mode ........................................................... ACTIVATE
Autopilot Altitude Hold ........................................................ ACTIVATE
If failure occurs while flying in IMC ........................................ EXIT IMC
1.
2.
POWER LEVER LINKAGE FAILURE
Power Lever Movement ............................................................VERIFY
Power ................................................................................. SET if able
3.
4.
Flaps .............................................................................. SET if needed
Mixture ............................................ AS REQUIRED (full rich to cut-off)
5. Land as soon as possible
Original
E - 10
Emergency Procedures
NOTES
NOTES
CIRCUIT BREAKER PANEL
MAIN BUS 2
NON ESSENTIAL
ESSENTIAL
10
IFD #1 (PFD)
5
FUEL PUMP
2
ANNUN/
ENGINE INST
5
SKYWATCH
2
TURN
COORD. #2
2
TURN
COORD #1
3
MLB
3
ATTITUDE #2
3
ATTITUDE #1
2
ENCODER/
XPONDER
10
IFD #2 (MFD)
10
IFD #1 (PFD)
WEATHER/
STORMSCOPE
5
ALT 1
2
STALL
WARNING
3
CABIN
LIGHTS
20
BATTERY 2
5
AUDIO PANEL
2
STARTER
RELAY
5
ALT 2
15
AVIONICS
7½
PITOT HEAT/
COOLING FAN
20
ESSENTIAL
POWER
5
FUEL QTY
3
12 VDC
OUTLET
5
AUTOPILOT
2
INST LIGHTS
5
STROBE
LIGHTS
15
AVIONICS
2
PITCH TRIM
5
NAV LIGHTS
10
IFD #2 (MFD)
2
ROLL TRIM
10
FLAPS
ICE
PROTECTION
MAIN BUS 1
Revision 1
NON ESSENTIAL
1
KEYBOARD
ESSENTIAL