Piper Archer POH Flashcards
Section 1 of POH covers:
General
Section 2 of POH covers:
Limitations
Section 3 of POH covers:
Emergency Procedures
Section 4 of POH covers:
Normal Procedures
Section 5 of POH covers:
Performance
Section 6 of POH covers:
Weight and Balance
Section 7 of POH covers:
Systems
Section 8 of POH covers:
Servicing and MX
Section 9 of the POH covers:
Supplements
Section 10 of POH covers:
Safety tips
What type of engine?
Lycoming O-360 4 cylinder Direct drive Horizontally opposed Air cooled
What is the HP of the engine?
180
What is the max RPM?
2700
Prop diameter
76 inch
Fuel capacity
Total: 50
Usable: 48
Oil capacity
8 quarts
Maximum takeoff weight and landing weight
2550 lb
Maximum baggage compartment weight
200 lb
Standard empty weight
1390 lb
Maximum useful load (difference between max takeoff weight and standard empty weight)
1160 lb
VNE
148 KTS
VNO (maximum structural cruising speed)
121 KTS
VA
108 KTS
VFE
100 KTS
VS (stall speed clean)
59 KTS
VSO (stall speed full flaps)
53 KTS
Oil pressure range
25-90 PSI
Fuel pressure range
.5 - 8 PSI
Positive load factor
3.8 G
Negative load factor limits
Not permitted
Is the airplane allowed to enter icing conditions?
No
Best glide speed:
76 KTS
VY
76 KTS
VX
64 KTS
Maximum crosswind
17 KTS
Mag check RPM
2,000
Each mag should not drop more than
175 RPM
Difference between both mags during mag check should not exceed
50 RPM
Takeoff trim setting
Slightly aft of neutral
Rotation speed
52-65 knots
Short field and soft field takeoff flap setting
25°, second notch
Short field rotation speed
41-49 KTS
Cruise climb speed
87 knots
Mixture should be leaned for operations above
5,000’
GPH for cruise
7.6, but use 10 for conservative figures