INSTALLATION OF WING FLAP CONTROLS. (Refer to Figure 27-25.)
1. The nap torque tube assembly may be installed by the following procedure:
A.
Install the chain sprockets with chains on the torque tube and secure with bolts, washers and nuts.
B.
Slide the tube stop fittings on their respective ends of the torque tube.
C.
Ascertain that one bearing block fitting is installed between its attachment brackets.
D.
Slide the other bearing block over its respective end of the torque tube.
E.
Position the torque tube by placing the end with the bearing block on it between the mounting
bracket and sliding the other end into the previously attached bearing block.
F.
Position the remaining bearing block and secure with bolts, washers and nuts.
G.
Push the torque tube cranks (arms) on each end of the torque tube and slide the stop fitting in
place. Align the bolt hole of the crank and stop fitting with the holes in the torque tube, and
install bolts.The holes in the stop fitting are elongated to allow the stop fitting to be pushed
against the bearing blocks thus allowing no side play of the assembly.Tighten the bolt assemblies
on the stop fittings.
H.
Install the tube support blocks on their support brackets and secure with bolts.
I.
Connect the nap return spring to the return chain and! or at the spar housing.
J.
Connect the control cable end to the tension chain and secure with bushing, clevis bolt, nut and
cotter pin.
K .
Pull the flap handle full back and connect the tension spring. Release the nap handle to the forward
position.
L .
Connect the nap control tube to the flap and/ or torque tube crank and secure.The bolt and bushing
that connects the control tube to the crank is installed through a hole in the side of the fuselage
located over the torque tube.
2. To install the nap handle with bracket, place the assembly on the floor tunnel and secure with bolts.
3. The nap control cable may be installed by the following procedure:
A.
Attach the cable and turnbuckle to the flap handle arm and secure with a new clevis bolt, nut and
cotter pin. Ascertain that the turnbuckle end is free to rotate on the arm.
B.
Route the cable through the tunnel and spar housing.
C.
Install the cable rub blocks on the aft side of the spar housing and secure with screws.
D.
Install cotter pin cable guard over pulley located just ahead of the spar housing in the forward
floor tunnel.
E.
Attach the cable end to the tension chain and secure with bushing, clevis bolt, nut and cotter pin.If
the chain is not installed because of the torque tube assembly being removed, install the assembly
as given in Step 3.
F.
Pull the flap handle full back and connect the tension spring to the cable end.
4. Install the tunnel cover and secure with screws. Also the tunnel carpet, heat deflectors, and bracket
cover.
5. Install the floor panel and seat belt attachments. Secure with screws and install seats.
RIGGING AND ADJUSTMENT OF WING FLAPS.
PPS50033
1. Place the flap handle in the full forward, flap retracted position.
2. If not previously accomplished, remove the floor panel just aft of the main spar.
3. If required, adjust the flap up stop and step lock, loosen the jam nut of the right torque tube stop screw.
located in the floor opening along the outer end of the flap torque tube, and turn the stop screw to
obtain approximately 0.60 of an inch between the stop fitting and the bearing block as measured along
the top side of the screw. (Refer to Figure 27-26.)It may be necessary to loosen the adjustment screw
of the left stop.
PIPER AIRCRAFT
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
27-50-02
Page 27-43
Revised: June 20, 1995
1L21
Summary of Contents for SEMINOLE PA-44-180
Page 38: ...CHAPTER DIMENSIONS AND AREAS 1B14...
Page 49: ...CHAPTER LIFTING AND SHORING 1C1...
Page 53: ...CHAPTER LEVELING AND WEIGHING 1C5...
Page 58: ...CHAPTER TOWING AND TAXIING 1C10...
Page 62: ...CHAPTER PARKING AND MOORING 1C14...
Page 65: ...CHAPTER REQUIRED PLACARDS 1C17...
Page 70: ...CHAPTER SERVICING 1C22...
Page 98: ...CHAPTER STANDARD PRACTICES AIRFRAME 1E2...
Page 108: ...CHAPTER ENVIRONMENTAL SYSTEM 1E12...
Page 189: ...CHAPTER AUTOFLIGHT 1H21...
Page 192: ...CHAPTER COMMUNICATIONS 1H24...
Page 202: ...CHAPTER ELECTRICAL POWER 1I10...
Page 228: ...CHAPTER EQUIPMENT FURNISHINGS 1J12...
Page 233: ...CHAPTER FIRE PROTECTION 1J17...
Page 238: ...CHAPTER FLIGHT CONTROLS 1J24...
Page 304: ...2A18 CHAPTER FUEL...
Page 325: ...2B17 CHAPTER HYDRAULIC POWER...
Page 357: ...2D1 CHAPTER ICE AND RAIN PROTECTION...
Page 414: ...CHAPTER LANDING GEAR 2F13...
Page 479: ...2I6 CHAPTER LIGHTS...
Page 488: ...2I16 CHAPTER NAVIGATION AND PITOT STATIC...
Page 503: ...2J7 CHAPTER OXYGEN...
Page 524: ...2K6 CHAPTER VACUUM...
Page 535: ...2K19 CHAPTER ELECTRICAL ELECTRONIC PANELS AND MULTIPURPOSE PARTS...
Page 546: ...INTENTIONALLY LEFT BLANK PA 44 180 180T AIRPLANE MAINTENANCE MANUAL 2L6 PIPER AIRCRAFT...
Page 547: ...2L7 CHAPTER STRUCTURES...
Page 582: ...CHAPTER DOORS 3A18...
Page 593: ...CHAPTER STABILIZERS 3B8...
Page 604: ...CHAPTER WINDOWS 3B22...
Page 611: ...CHAPTER WINGS 3C10...
Page 624: ...CHAPTER PROPELLER 3D1...
Page 643: ...CHAPTER POWER PLANT 3D21...
Page 667: ...CHAPTER ENGINE FUEL SYSTEM 3F1...
Page 681: ...CHAPTER IGNITION 3F16...
Page 712: ...CHAPTER ENGINE INDICATING 3H1...
Page 730: ...CHAPTER EXHAUST 3H19...
Page 734: ...CHAPTER OIL 3I1...
Page 743: ...CHAPTER STARTING 3I11...
Page 755: ...CHAPTER TURBINES 3J1...