B.
B u ff the area around the damage with buffing stick, Part No. 74-451-75, so that the surface is
thoroughly roughened.
C.
Apply the patch to the deicer with the stretch in the widthwise direction of the inflatable tubes, sticking
edge of patch in place, working remainder down with slight pulling action so the injury is closed. Do
not trap air between patch and deicer surface.
3. LOOSE SURFACE PLY IN DEAD AREA (NON-INFLATABLE AREA). Peel and trim the loose surface
ply to the point where the adhesion of surface ply to the deicer is good.
A.
Scrub (roughen) area in which surface ply is removed with steel wool. Scrubbing motion must be
parallel to cut edge of surface ply to prevent loosening it. Scrub with steel wool and Toluol directly
over all edges, but parallel to edges or surface ply to taper them down to the tan rubber ply.
B.
Cut a piece of surface ply material, Part No. 74451-23, to cover the damaged area and extend at least
one inch beyond in all directions.
C.
Mask off the damaged boot area 1/2 inch larger in length and width than the size of surface ply patch.
Apply one coat of cement, Part No. 74-451 - 11, to damaged area and one coat to patch. Allow cement
to set until tacky.
Roll the surface ply to the deicer with 2 inch rubber roller, Part No. 74-451-74. Roll edges with stitcher-
r o l l e r, Part No. 74-451-73. Apply just enough tension on the surface ply when rolling to prevent
wrinkling and be careful to prevent trapping air. If air blisters appear after surface ply is applied,
remove them with a hypodermic needle.
D.
Clean excess cement from deicer with solvent.
4. LOOSE SURFACE PLY IN TUBE AREA. Loose surface ply in tube area is usually an indication of the
deicer starting to flex fail. This type of failure is more easily detected in the form of a blister under the
surface ply when deicer is pressurized. If this type of damage (or void) is detected while still a small blister
(about 1/4 or 3/8 inch diameter) and patched immediately, the service life of the deicer will be appreciably
extended. Apply repair patch as outlined in Paragraph 1.
5. DAMAGE TO FABRIC BACK PLY OF DEICER DURING REMOVAL. If cement has pulled loose from
the wing skin and adhered to the back surface of the deicer, remove it with steel wool and MEK. In those
spots where the coating has pulled off the fabric, leaving bare fabric exposed, apply at least two additional
coats of cement, Part No. 74-451-24. Allow each coat to dry thoroughly.
VULCANIZED REPAIRS.
Due to the variety of boot damage possible, it is recommended that the B. F. Goodrich Company be contacted
so they can determine the extent of damage and whether it is repairable by the vulcanized method or not. The
overall condition of the deicer boot must be given careful consideration before deciding on any repairs. Damages
can vary from minor punctures which may be easily repaired, to extensive ripping of the tube or stretch areas
which may make repairs exceedingly difficult or actually impossible. The determination of just where this
division between repairable and unrepairable damage exists will depend upon the careful judgment of the
inspector. For this reason, we recommend contacting the B. F. Goodrich Company at Akron, Ohio.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
3 0 - 1 3 - 0 8
Page 30-11
Revised: May 15, 1989
2D15
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...