Piper Archer III / PA-28-181 / PA28

Transcription

HB-PQR
Piper Archer III / PA-28-181 / PA28
© 2004 Flugschule Basel AG
GK Archer III / HB-PQR
AFM -> Aircraft Flight Manual
•  Design
Section
Section
Section
Section
Section
Section
Section
1
2
3
4
5
6
7
Section 8
Section 9
Section 10
10 Sections
GENERAL
LIMITATIONS
EMERGENCY PROCEDURES
NORMAL PROCEDURES
PERFORMANCE
WEIGHT and BALANCE
DESCRIPTIONS and OPERATION of
the Airplane and its SYSTEMS
AIRPLANE HANDLING, SERVICING
and MAINTENANCE
SUPPLEMENTS
OPERATING TIPS
Dimensions
Höhe
2.22 m
Spannweite
10.82 m
Länge
7.32 m
Min. Wenderadius
9.14 m
Section 1 / GENERAL
Engine
Engine Manufacturer
Lycoming
Model Number
O-360-A4M
Rated Horse Power
180 HP
Take Off Power Eng. Speed
2700 RPM
Engine Type
Four Cylinder,
Direct Drive,
Horizontally
Opposed, Air
Cooled
Section 1 / GENERAL
Propeller
Propeller Manufacturer
Number of Blades
2
Propeller Type
Sensenich
Fixed Pitch
Section 1 / GENERAL
Fuel
Fuel Capacity
50 USG
Usable Fuel
48 USG
Section 1 / GENERAL
Oil
Oil Capacity
8 qts
Oil Specification
15W50
Min for FSB Use
6 qts
Section 1 / GENERAL
Maximum Weights
Maximum Ramp Weight
1160.3 kg
2558 lbs
Maximum Takeof Weight
2550 lbs
1156.7 kg
Maximum Landing Weight
2550 lbs
1156.7 kg
Maximum Weight in
Baggage Compartment
200 lbs
90.7 kg
Std Airplane Weights
Section 6 / Weight
& Balance
Section 1 / GENERAL
Air Speed Limitations (KIAS)
VNE
VNO
VA
154
125
113 / 2550 lbs
KIAS
Weight
89 / 1634 lbs
113
2550
112
110
109
108
107
105
104
103
101
100
99
97
96
95
94
92
91
90
89
2500
2450
2400
2350
2300
2250
2200
2150
2100
2050
2000
1950
1900
1850
1800
1750
1700
1650
1634
VX
VY
VCLIMB
VGLIDE
VS0
VS1
64
76
87
76
45
50
Section 2 / LIMITATIONS
Air Speeds for Circuit (KIAS)
Down Wind
55-60
Base
Final
Threshold
90
Rotate
80
70
66/53
Based on Vso with 30° Bank Angle and 0° Flaps!
Throshold 1.1 - 1.2 x Vso
Initial Final 1.3 x V so
500 ft AGL
45°
Base 1.5 x Vso
1 NM
Downwind 1.8 x Vso
1000 ft AGL
Power Plant Limitations
Max. Horse Power
180
Max. Rotation Speed
2700
Max Oil Temperature
245°F
Fuel Minimum Grade
100 or 100LL Aviation
Grade
118.3°C
Manoeuver Limits
Normal Category
All aerobatic manouvers including spins are
PROHIBITED !!!
Utility Category
Approved manouvers for bank angles
exceeding 60° !!!
Flight Load Factors
Normal
Positive Load Factor
3.8 G
Utility
4.4 G
Negative Load Factor No inverted manouvers
approved
Types of Operation
VFR Day and Night
Yes
Icing Conditions
No
Fuel Limitations
Total
50 USG
Usable
48 USG
(24 USG each Tank)
Diverse
Max. Altitude
15‘000 ft AMSL
Max. Demonstrated
X-Wind Component
17 KTS
Section 5 / PERFORMANCE
Weights
Max Takeoff Weight
kg
2550.00 lbs
Basic Empty Weight 1811.99 lbs
Useful Load
338.38 kg
1156.66
821.90 kg
746.01 lbs
Fuel (48 USG)
Pay Load
288.00 lbs
458.01 lbs
130.64 kg
207.74 kg
Fuel (34 USG) Filler Neck
Pay Load
204.00 lbs
542.01 lbs
92.53 kg
245.85 kg
Section 6 / WEIGHT & BALANCE
Structure
Fuselage
Material
Semi-Monocoque
Alluminium
Tips of Wings, Tail Fin
And Stabilator
ABS Thermoplastic
Aerobatics
NO
Doors
Baggage Door
1 plus
NACA 652-415
Wings Profile
Section 7 / SYSTEM
Engine and Propeller
Type
4 Cylinder Boxer-Motor
Rated
RPM
180 HP at 2700
Starter
70 Ampere
Alternator
28 Volt
Propeller
Fixed-Pitch
Section 7 / SYSTEM
Landing Gear
Tire Pressure
Front
18 psi
Main
24 psi
Section 7 / SYSTEM
Brakes
Type
Cylinders
Reservoir
Single-Disk
3 / Pedal- and Handbrake
1
Section 7 / SYSTEM
Flight Controls
System
Trim
Flaps
Cable
Stabilator - Manual & Electr.
Rudder - Manual
Manual – 10°, 25°, 40°
Section 7 / SYSTEM
Engine Console
Section 7 / SYSTEM
Fuel System
Section 7 / SYSTEM
Fuel System
Section 7 / SYSTEM
Electrical System
System
Battery
Alternator
NVFR Load
+2
28 Volt
24 Volt
70 Amp
32 Amp
Amp Batt.
Section 7 / SYSTEM
Electrical System
Section 7 / SYSTEM
Electrical System
Section 7 / SYSTEM
Instrument Panel
Section 7 / SYSTEM
Pitot-Static System
Section 7 / SYSTEM
Heating and Ventilation
Section 7 / SYSTEM
Air Conditioning
Switch OFF during Take-off and Landing
Section 7 / SYSTEM
Annunciator Panel
Section 7 / SYSTEM
External Power
Section 7 / SYSTEM
Emergency Locator Transmitter
Section 7 / SYSTEM
Carb Ice Detection System
& Pitot Heat
Section 7 / SYSTEM
Auxiliary Vacuum System
Section 7 / SYSTEM
Audio Panel
Section 7 / SYSTEM
Transponder & Audio
Section 7 / SYSTEM
System 55 Autopilot
Section 7 / SYSTEM
Altitude Selector / Alerter
Section 7 / SYSTEM
Download - Links
S-Tec
S-Tec Altitude Preselector / Alerter Manual
http://www.s-tec.com/pdf/st360POH.PDF
S-Tec Autopilot Manual
http://www.s-tec.com/pdf/sys55poh.PDF
Garmin
GNS 430 Pilot's Guide Rev. G, 04/03
http://www.garmin.com/manuals/GNS430_PilotsGuide.pdf
GNS 430 Quick Reference Guide Rev. C, 06/00
http://www.garmin.com/manuals/GNS430_QuickReferenceGuide.pdf
GNS 430 Sample Training Syllabus Rev. A, 09/03
http://www.garmin.com/manuals/288_SampleTrainingSyllabus.pdf
PC Simulator GNS 430
http://www.garmin.com/products/gns430/#
GMA 340 Audiopanel Manual
http://www.garmin.com/manuals/GMA340AudioPanel_PilotsGuide.pdf
ICEMAN
ICEMAN CARBURATOR ICE DETECTOR
http://www.ocflightcenter.com/uploads/documents/4173K_Ice_Detector.doc
Section 7 / SYSTEM
079 435 70 71
reto.spoerri@tiscali.ch
Section 7 / SYSTEM
Many happy landings .... ;-))
Section 7 / SYSTEM

Piper Archer III / PA-28-181 / PA28

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