Piper PA-28-161 Maintenance Manual

PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 9
Nov 30/06
1D3
5-20-00
5. Scheduled Maintenance (continued)
Inspection
NATURE OF INSPECTION Interval (Hrs)
50 100
46. Inspect security of alternator mounting ................................................................ O O
47. Check condition and security of hydraulic line and fluid in
brake reservoir; fill as required ............................................................................. O O
48. Inspect and lubricate controls per Lubrication Chart, 12-20-00 ........................... O
49. Reinstall engine cowling ....................................................................................... O O
C. CABIN AND COCKPIT GROUP
1. Inspect cabin entrance door and windows for damage, operation
and security. (See Note 21.) ................................................................................. O
2. Inspect upholstery for tears .................................................................................. O
3. Inspect seats, seat belts, shoulder harnesses, security brackets, and bolts.
(See Restraint System - Inspection, 25-10-00.) ................................................... O
4. Inspect trim control operation ............................................................................... O
5. Inspect rudder pedals for operation and adjustment ............................................ O
6. Inspect parking brake and brake handle for operation and cylinder leaks ............ O
7. Inspect control column, pulleys and cables for condition.
(See Notes 9, 14, and 32.) .................................................................................... O
8. Inspect flap lever control cable attachment bolt for security and condition ........... O
9. Check landing, navigation, cabin and instrument lights ........................................ O O
10. Inspect instruments, lines and attachments. (See Notes 29 and 31.) ................... O
11. Inspect gyro operated instruments and electric turn and bank.
Overhaul or replace as required............................................................................ O
12. If equipped, replace filters on Attitude Gyro and Heading Indicator...................... O
13. Clean or replace vacuum regulator filter ............................................................... O
14. Inspect altimeter and transponder for installation/certification
per latest revision of AC43.13-1 and tested/inspected
per FAR’s 91.411 and 91.413, respectively........................................................... O
15. Inspect and test ELT per FAR 91.207. (See Testing ELT, 25-60-00.)..................... O
16. Inspect operation of fuel selector valve ................................................................. O
17. Inspect condition of heater controls and ducts...................................................... O
18. Inspect condition and operation of air vents.......................................................... O
19. If installed, inspect portable fire extinguisher minimum weight as specified on
nameplate ............................................................................................................ O
D. FUSELAGE AND EMPENNAGE GROUP
1. Remove inspection plates and panels................................................................... O
2. Inspect baggage door latch and hinges for operation and security....................... O
3. Inspect battery, box and cables. Flush box as required and
fill battery per instructions on box. ........................................................................ O O
4. Inspect electronic installations .............................................................................. O
5. Inspect skins, bulkheads, frames, and stringers for damage. (See Note 33.) ....... O
6. Inspect condition and security of antenna mounts and electric wiring .................. O
7. Inspect fuel lines, valve and gauges for damage and operation ........................... O
8. Inspect security of all lines .................................................................................... O

Piper PA-28-161 Specifications

General

Manufacturer	Piper Aircraft
Model	PA-28-161 Warrior II
Engine	Lycoming O-320-D3G
Horsepower	160 hp
Seating Capacity	4
Wingspan	35 ft (10.7 m)
Length	24 ft 0 in
Maximum Speed	127 knots
Cruise Speed	122 knots
Maximum Takeoff Weight	2, 325 lb (1, 055 kg)
Fuel Capacity	48 US gallons (182 L)