SECTION 4. CABIN INTERIOR
9-60. GENERAL. Only materials that are flash-resistant should be used in cabin interiors. The requirements related to fire protection qualities of cabin interior materials are specified in CAR 3.388, fire precautions or 14 CFR part 23, section 23.853 compartment interiors.
9-61. CAR-3 AIRCRAFT INTERIOR. The requirement for an interior of a CAR-3 aircraft that is used only in 14 CFR, part 91 operations, where smoking is not permitted, is that the materials shall be flash-resistant. (Reference CAR-3.388.)
a. For compartments in CAR-3 aircraft where smoking is permitted, the wall and ceiling linings, the covering of all upholstering, floors, and furnishings shall be flame-resistant. Such compartments should be equipped with an adequate number of self-contained ash trays. All other compartments shall be placarded against smoking. (Refer to CAR-3.388.)
(1) If fabric is bought in bulk to refurbish the interior, seats, and ceiling liners for a CAR-3 aircraft used in part 91 operations, a manufacturer's statement, declaring that the material meets the American Society for Testing and Materials (ASTM) or similar national standard for either flash resistance or flame resistance, would be acceptable, but only for a CAR-3 aircraft installation. (Refer to 14 CFR part 43, section 43.13(a).) A manufacturer's statement is acceptable due to neither the Civil Aeronautics Administration (CAA) nor the Federal Aviation Administration (FAA) having published an FAA fire standard for either flash or flame resistance for interior materials for CAR-3 aircraft. Since the FAA would accept and recognize a national standard, the mechanic would reference the manufacturer's statement and the national standard that the material meets in the aircraft's maintenance records.
(2) If an annual inspection is performed on a CAR-3 aircraft with a new interior and there is no mention of a manufacturer's statement that the fabric is flash or flame resistant as applicable, the possibility exists that the fabric is an unapproved part. The mechanic should take the necessary steps to ensure that the fabric meets or exceeds the ASTM or national standards. (Refer to 14 CFR part 23, appendix F.)
(3) If an FAA-approved STC interior kit is installed in a CAR-3 aircraft, and the material and fabric in the kit are PMA or TSO approved, the mechanic should include the STC number in block 8 of FAA Form 337.
b. It is recommended that for all CAR-3 interiors to use only fabric and materials that meets the more stringent requirements of part 23, appendix F.
9-62. PART 23 AIRCRAFT INTERIOR. Materials used in part 23 aircraft interiors must meet the requirements of section 23.853, and the burn test requirements called out in part 23, appendix F.
a. If the fabric is bought in bulk to refurbish a part 23 aircraft then the fabric must meet the part 23 burn requirements. A burn test would have to be done on samples of the material and fabrics by an approved and rated FAA Repair Station. That FAA Repair Station would certify that all the material and fabrics meet part 23, appendix F requirements. The mechanic would include that repair station's statement in the aircraft's records.
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b. If STC-approved interior kit with either PMA or TSO-approved materials for a part 23 aircraft is bought, the mechanic would only have to reference the STC number on FAA Form 337 and the aircraft's records. part 23, appendix F would not be required.
c. If an annual inspection is to be performed on a part 23 aircraft in which a new interior was installed, but the aircraft's records do not reflect that a burn test was performed on the interior's materials and fabric by an FAA Approved Repair Station, or there is no mention of an STC or FAA Form 337 in the aircraft records, then a burn test that meets, part 23, appendix F must be accomplished before the aircraft is approved for return to service.
9-63. SOURCE OF INFORMATION. If information regarding the original or properly altered fire protection qualities of certain cabin interior materials is not available, requests for this information should be made to the aircraft manufacturer or the local FAA regional office, specifying the model aircraft and the aircraft manufacturer. The date the aircraft was manufactured or the serial number, and the 14 CFR part under which the aircraft is operated (i.e., CAR-3, 14 CFR part 91, or part 121, etc.).
9-64. UPHOLSTERY AND/OR BELTS. Upholstery and/or belts that have been washed may lose some or all of their fire-resistant qualities. Unless the soap is completely removed from the cloth, the strength of the material may be significantly reduced. Consult the manufacturer to determine how to maintain the fire-resistant qualities.