F.
Remove the lower selector cover.
G.
Remove the tunnel plate just aft of the tee bar by removing enough carpet from the tunnel to
allow the plate attachment screws and plate to be removed.
H.
If the right (upper) stabilator control cable is to be removed, remove the cotter pin cable guards at
the pulley located in the forward area of the tunnel.
I.
Disconnect the cables from the lower end of the tee bar by removing cotter pin, nut, washer and
bolt.
J.
Draw the cable aft through the floor tunnel.
4. To remov either aft stabilator cable:
A.
Disconnect the assist springs from bulkhead sta. 156. (Refer to Figure 27-12.)
B.
Disconnect the cable end at the bellcrank by removing the cotter pin, nut, washer and bolt.
C.
Remove the cable guard pin at the pulley.
D.
Remove the cable from the pulley.
INSTALLATION OF STABILATOR CONTROL CABLES. (Refer to Figure 27-12.)
1. To install the forward stabilator cables
A.
Draw the control cable through the floor tunnel. Ascertain that the right (upper) cable is routed
around the pulley that is in the forward area of the forward floor tunnel.
B.
Connect the cables to the lower end of the control column tee bar with bolt, washer, nut and cotter
pin. Allow the cable to be free to rotate.
C.
If the aft control cable is not installed, install per Step 2.
D.
Connect the cable to the aft cable at the turnbuckle in the aft section of the fuselage.
E.
For the right control cable, install the cotter pin cable guard at the pulley in the forward area of
the tunnel.
F.
Within the forward area of the floor opening aft of the main spar, install the cable rub blocks to
the spar housing and secure with screws.
G.
In the aft area of the floor opening, install the cotter pin cable at the pulley cluster.
H.
Install the cable guard under the pulley cluster located in the aft area of the aft floor tunnel and
secure with screws.
I.
Set cable tension and check rigging and adjustment.
J.
Install the tunnel plate directly aft of the tee bar assembly and secure with screws.
K.
Put the floor carpet in place and secure.
L.
Install the lower and upper selector covers and secure with screws.
M. Place the fuel selector knobs on the selector torque tube and secure with set screws.
N.
Install the floor panel aft of the main spar and secure with screws. Install the seat belt attach-
ments and seats.
0.
Install the cover and carpet of the aft floor tunnel.
2. To install either aft stabilator control cable:
A.
Route the cable under pulley.
B.
Connect the cable to the stabilator bellcrank and secure with bolt, washer, nut and cotter pin.
(Tighten nut “finger tight” only.)
C.
Connect the cable to the forward cable at the turnbuckle in the aft section of the fuselage. The
upper aft cable connects to the right forward cable and the lower cable to the left cable.
D .
Connect assist springs to bulkhead sta. 156 and orient cable plates so that they align with horizontal
plate +/- 10°. (Refer to Figure 27-18.)
E.Install the cable guard pin at the pulley.
F.Set cable tension and check rigging and adjustment.
3. Install the access panels to the aft section of the fuselage.
PIPER AIRCRAFT
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
27-30-01
Page 27-32
Revised: June 20, 1995
1L10
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...