Ground - Course Turbo Arrow IV
PA-28R-201T
P28R
© 2002 FSB / Basel
AFM
© 2002 FSB / Basel
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Design
10 Sections
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Section 1
Section 2
Section 3
Section 4
Section 5
Section 6
Section 7
GENERAL
LIMITATIONS
EMERGENCY PROCEDURES
NORMAL PROCEDURES
PERFORMANCE
WEIGHT and BALANCE
DESCRIPTION and
OPERATION of the
AIRPLANE and its SYSTEMS
Handling, Servicing and
Maintenance
SUPPLEMENTS
OPERATING TIPS
Section 8
Section 9
Section 10
Dimensions
© 2002 FSB / Basel
• Höhe
2.50 m
8' 3"
• Spannweite
10.78 m
35' 5"
• Länge
8.31 m
27' 4"
• Min. Wenderadius
9.45 m
31'
Engine
• Engine Manufacturer
• Model Number
• Rated Horsepower
• Rated Speed
• Max. Manifold Pressure
© 2002 FSB / Basel
Teledyne Continental
TSIO-360-FB
200 HP (3 Blad Prop)
Sea Level to 12'000 ft
DA)
2575 RPM (3 Blad Prop)
41" MP
Propeller
© 2002 FSB / Basel
• Propeller Type
Harzell F7663-2R
• Blades
3 (without Prop Heat)
Fuel
• Fuel Capacity (USG)
77
• Usable Fuel (USG)
72
AVGAS ONLY
• Minimum Grade 100 Green or 100LL
© 2002 FSB / Basel
Oil
© 2002 FSB / Basel
• Oil Capacity (QTS)
8
• Oil Specification
15W50
• Min. for FSB Use (QTS)
7
Maximun Weights
• Max. Takeoff Weight (lbs / kg)
2900 / 1315.42
• Max. Landing Weight (lbs / kg) 2900 / 1315.42
• Max. Ramp Weight (lbs / kg)
2912 / 1320.86
• Max. Weight in Bagg. Comp. (lbs / kg) 200 / 90.72
© 2002 FSB / Basel
Running Basic Empty Weight
• Weight
• CG
• Moment
© 2002 FSB / Basel
1917.0 lbs
87.36“
167‘479.4
© 2002 FSB / Basel
Air Speed Limitations (KIAS)
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© 2002 FSB / Basel
VNE
VNO
VFE
VLE
VLO
Max. Demo. X-wind
193
152
108
133
111
17 KTS
Max. Manouvering Speed
VA
Interpolation
© 2002 FSB / Basel
124 KIAS
97 KIAS
->
->
Pro 37 lbs
Pro 17 kg
2900 lbs
1893 lbs
 1 KIAS
 1 KIAS
Air Speeds for APP (KIAS)
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Initial Approach
Intermediate Approach
Final Approach
Short Final
Threshold
Based on Vso = 61 KIAS with 2900 lbs acc Figure 5-3 AFM
© 2002 FSB / Basel
100
90
80
73
67
ICAO Pattern
Throshold 1.1 - 1.2 x Vso
Initial Final 1.3 x Vso
500 ft AGL
45°
Base 1.5 x Vso
1 NM
Downwind 1.8 x Vso
1000 ft AGL
© 2002 FSB / Basel
One Mile Check
© 2002 FSB / Basel
Power Plant Limitations
© 2002 FSB / Basel
• Max. Horse Power
200
• Max. Rotation Speed
2575
• Max. Oil Temp (°F)
240
• Max. MP (in. Hg)
41.0
Maneuver Limits
No aerobatic maneuvers including spins
approved!
© 2002 FSB / Basel
Types of Operation
© 2002 FSB / Basel
• VFR Day and Night
YES
• IFR Day and Night
YES
• Icing Conditions
NO
Fuel Limitations
© 2002 FSB / Basel
• Total
77 USG
• Usable
72 USG
(36 USG each Tank)
• Filler Neck
50 USG (Usable)
(25 USG each Tank)
Altitudes
• Max. Altitude
© 2002 FSB / Basel
20'000 ft
Structure
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Fuselage
Materia
Wingtips, Fin, Stabilator
Aerobatics
Doors
Baggage Door
Storme Window
Wing Profile
© 2002 FSB / Basel
Semi-Monocoque
Alluminium
Lightweight Plastic
No
1
1
1
NACA 652-415
Engine and Engine Controls
• Type
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Rated
Max. MP
Alternate Air
Throttle
Propeller
Propeller
Mixture
• Friction
© 2002 FSB / Basel
6 Cylinder, Boxer, Aircooled
Fuel Injected, Turbo Charged
200 HP
41.0 in. Hg
Manual
Standard
Control Cable to Covernor
Hydraulic Operated
Lean to best Power
(100°F rich of Peak)
Manual
© 2002 FSB / Basel
Landing Gear
• Type
• Hydraulic Pressure
• Time
Retractable
Tricycle
Hydraulic Actuated
Electr. Powered
reversible Pump
ca. 7 sec.
Automatic Gear Extension Removed
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• Emergency Gear Down
• Type of Release Mechanism
© 2002 FSB / Basel
Free Fall
Lever Release
Landing Gear
When gear is in
transition
• Gear Unsave Light
• Gear Unsave Light and Horn
1. Gear Selector UP and Power below 14" MP
2. Gear Selector UP while on Ground
3. Gear Selector UP an Flaps 25° or more
• Tire Pressure
• Struts
© 2002 FSB / Basel
Nose
Main
Nose
Main
27 psi / 1.84 bar
30 psi / 2.05 bar
2.5“ / 5.6 cm
2.75“ / 6.9 cm
Landing Gear
© 2002 FSB / Basel
© 2002 FSB / Basel
Squat Switch
© 2002 FSB / Basel
© 2002 FSB / Basel
Brakes
© 2002 FSB / Basel
• Type
Disk
• Pedals
Left and Right Side
• Hand Brake
Normal
• Brake Cylinder
2
• Fluid Reservoir
1
Flight Controls
• System Cable
Stabilator Manual and Electr.
Rudder -> Manual spring-loaded
Auto. Disconnect Above 169 KIAS
• Trim
• Flaps
© 2002 FSB / Basel
Manually Controled
10, 25 or 40 Degrees
Fuel System
© 2002 FSB / Basel
• Capacity Total
• Capacity Usable
77 USG
72 USG
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2 (1 each Side)
3 Positions
3
Electr. / Inside
Number of Tanks
Fuel Selector
Fuel Drain
Fuel Quantity Indicator
Fuel System
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Fuel Pump
Electr. Fuel Pump
Fuel Injection Sysem
Vapor Line
Opt. Primer System
© 2002 FSB / Basel
Engine driven and Electr.
OFF / LO / HI
Continous Flow
Selected Tank
Diverter Valve / 2 Nozzels
Fuel Pump HI
Fuel System / Switch
© 2002 FSB / Basel
© 2002 FSB / Basel
Electrical System
• Battery
• Alternator Output
• Battery, Overvoltage Relay,
Masterswitch Relay, Voltage
Regulator
12 V, 25 Ah
14 V, 65 Amp
Rear Baggage
Comp.
• Electrical Switches
• Annunciator Panel OVER BST, OIL, VAC, ALT
• EMERGENCY OVERRIDE
© 2002 FSB / Basel
Emergecy Power Override
© 2002 FSB / Basel
Circuit Breaker Panel(s)
© 2002 FSB / Basel
Vacuum System
© 2002 FSB / Basel
• System
Engine Driven Pump
• Stand-By Pump
NO
• Instruments
Horizon, DG
Anti Atmospherics
• Pitot Heat
© 2002 FSB / Basel
YES
Instrument Panel
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© 2002 FSB / Basel
Slave System
DME RMT - Switch
RMI Selector
Garmin GNS 430 -> HSI-, OBS-Selector,
© 2002 FSB / Basel
Pitot and Static System
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System
Alternate Static Source
Alternate Static Source Error
Pitot and Static Drains
© 2002 FSB / Basel
Pitot ONLY
Less than 50 ft
© 2002 FSB / Basel
Pitot and Static System
© 2002 FSB / Basel
Pitot and Static System
© 2002 FSB / Basel
Cabin Features
• Intercom
© 2002 FSB / Basel
Pilot and Co-Pilot
Heating and Ventilation
System
• Heater
• Defroster
• Overhead Vent Blower
© 2002 FSB / Basel
HI / OFF / LOW
© 2002 FSB / Basel
Stall Warning
• Lift Detector
© 2002 FSB / Basel
5 - 10 KIAS above Stall Speed
Emergeny Locator Transmiter
• Position
Tail Cone Section
• Operation
ON
ARMED/NORMAL POSITION
© 2002 FSB / Basel
Emergeny Locator Transmiter
© 2002 FSB / Basel
Emergeny Locator Transmiter
© 2002 FSB / Basel
Oxygen
• Type
• Oxygen Cylinder
• Pressure
• Pressure Gauge
• Recharging
• Control Knob
• Constant Flow Mask
© 2002 FSB / Basel
Scott Aviation MK III
Portable Oxygen System
63 cubic foot / 1784.1 Lt
1850 psi / 127 bar
at 70°F / 21°C
1500 - 2000 psi
Follow Instructions in AFM
Countreclockwise ON
Clockwise OFF
Red Indicator
Oxygen
Duration in Hours at Altitude
NO SMOKING
NO Grease or Oil
© 2002 FSB / Basel
Autopilot
• Type
Century 21
Direction (HDG, NAV, APP, REV)
• Limitation
175 KIAS
OFF during T/O and Landing
Button
• Interrupt
© 2002 FSB / Basel
Weight & Balance 1
© 2002 FSB / Basel
Weight & Balance 2
© 2002 FSB / Basel
Weight & Balance 3a
© 2002 FSB / Basel
Weight & Balance 3b
© 2002 FSB / Basel
T/O Performance
Airport Elevation
QNH
OAT
T/O Weight
883 ft (LFSB)
1023 hPa
+23 °C
2900 lbs
Pressure Altitude 883 ft - ( 10 x 27 ft ) = 613 ft
Normal (Zero Flaps, VR 78 KIAS
•T/O Ground Roll
1900ft / 579m
2400ft / 732m
•T/O Distance oder 50ft Obst.
Short Field (25° Flaps, VR 66 KIAS
•T/O Ground Roll
1200ft / 366m
•T/O Distance oder 50ft Obst.
1700ft / 518m
© 2002 FSB / Basel
© 2002 FSB / Basel
© 2002 FSB / Basel
© 2002 FSB / Basel
© 2002 FSB / Basel
Landing Performance
Konfiguration
Airport Elevation
QNH
OAT
T/O Weight
Pressure Altitude
40° Flaps, VAPP 75 KIAS
883 ft (LFSB)
1023 hPa
+23 °C
2900 lbs
883 ft - ( 10 x 27 ft ) = 613 ft
LDG Distance over 50ft Obst.
LDG Ground Roll
© 2002 FSB / Basel
1590ft / 485m
680 ft / 207m
© 2002 FSB / Basel
© 2002 FSB / Basel
Happy landings !!!
© 2002 FSB / Basel