BAGGAGE DOOR LOCK ASSEMBLY.
REMOVAL OF BAGGAGE DOOR LOCK ASSEMBLY.
1. With the door open remove two screws securing the access plate, remove the access plate.
2. Remove the nut from the back of the lock assembly with the use of a special wrench. (This tool may be
fabricated from the dimensions given in Figure 52-2.)
3. Remove the lock assembly through the front of the door.
INSTALLATION OF BAGGAGE DOOR LOCK ASSEMBLY.
1. Place the lock into position for installation.
2. Install the nut on the lock assembly and tighten with the use of a special wrench.
3. Install access plate and secure with two screws.
EMERGENCY EXIT.
REMOVAL AND INSTALLATION OF EMERGENCY EXIT. (Refer to Figure 52-3.)
1. Remove the safety wire securing the lock handle and push the handle forward to unlock the exit.
2. Carefully push outward along the bottom of the door (see CAUTION next paragraph) till the door just
clears the door sill, and slowly shift the door back and forth out of the top of the fuselage skin.
3. Clean all old sealant from around the exit opening and exit assembly.
4. Inside the door frame apply lubriplate around both fore and aft latch tubes.
5. Insure that all gaps and holes between the sills and longeron are filled with PMS-C1012 sealant compound.
6. Insure that neoprene seal is securely bonded to the emergency exit assembly.
7. Cover the contacting surfaces of the assembly with vinyl film. (Refer to Chapter 91, Consumable Materials
list for suppliers.)
8. Insert the bottom edge of the exit assembly over the longeron, then push in on the top and sides until it is
properly seated. With the assembly seated push the lock handle aft to lock the assembly in place. Safety the
handle in place with tinned copper wire AWG 26, .0159 dia. wire.
9. When exit is secured in place add sealant around perimeter of door and trim any excess vinyl film from
inside and outside of the unit.
10.Test the latch mechanism, as explained in the next section, for operation prior to applying any sealant
around the door.
11.Fill all gaps around the outside of the emergency exit and fuselage with PRC5000 sealant or equivalent.
12.Check for water leaks by spraying water over the emergency exit and window assembly.
TESTING OF EMERGENCY EXIT DOOR.
1. Remove the side panel access cover to the emergency release handle.
2. Attach a calibrated spring scale 1.0 inch from the top of the handle.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
5 2 - 2 1 - 0 1
Page 52-06
Revised: May 15, 1989
3B1
PIPER AIRCRAFT
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...