PREPARATION OF DEICER BOOT.
Moisten a clean cloth with MEK or Acetone and carefully clean the rough, back surface of the boot at least
twice. Change cloths frequently to avoid recontamination of the cleaned areas.
MOUNTING BOOT ON LEADING EDGE.
Thoroughly mix EC - 1403 cement before using. Apply one even brush coat to the cleaned back surface of the
boot and to the cleaned metal surface. Allow the cement to air dry for a minimum of one hour. Apply a second
coat to both surfaces and allow to air dry a minimum of one hour. Ambient temperature for installation should be
held between 40° and 110° F. However, longer drying time of the cement coats may be required as the humidity
approaches 99%. Deicer and leading edge may be cemented for a maximum of 48 hours before actual
installation, if cemented parts are covered and kept clean.
Snap a chalk line along the leading edge of the airfoil section. Intensify chalk line on leading edge and the
white reference line on the boot with a ball point pen. Most boots are made with an excess of material at the
inboard and outboard edges for final trimming after installation and some recessed boots trim on the upper and
lower edges.
Securely attach hose to deicer connections using clamps or safety wire.
1. Holding the backside of the boot close to the leading edge, fasten the end of each non-kink hose to the
corresponding air connection stem. Tinnerman or other suitable non-kink hose clamps should be used for
this purpose. Tighten each clamp with a pair of slip joint pliers but do not squeeze the clamp so tight that t
he hose is damaged.
— Note —
If non-kink hose clamps are not available, wrap each hose connection with several
turns of friction tape. Over the tape, wrap two separate bindings of safety wire, about
1/2 inch apart. Each of these bindings should consist of several turns of wire. Twist
together the ends of each binding to tighten. Press the twisted ends down against the
hose. Finally, wrap the wire with several additional turns of friction tape.
2. Push the hose connections into the leading edge grommets or seals as the case may be. Obtain sufficient
personnel to hold boot steady during installation. (Limit handling cemented side of boot with fingers.)
Continue installation by reactivating the cement along the center line leading edge surface and boot in span
wise strips approximately six inches wide. Rubber roll the deicer firmly against the wing leading edge,
being careful not to trap any air under the deicer. Always roll parallel to the inflatable tubes. Position the
deicer center line to coincide with leading edge center line. Hold boot in this position while reactivating
about three inches around connections and around corresponding holes in leading edge, using a clean, lint-
free cloth moistened with Toluol. Insert connections in leading edge holes when cement has dried to a tacky
state and rubber roll boot to leading edge in tackified area.
3. If the deicer should attach “off course,” use MEK to remove and reposition properly. Avoid twisting or
sharp bending of the deicer.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
3 0 - 1 3 - 1 2
Page 30-16
Revised: May 15, 1989
2D20
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...