Check for proper condition (e.g., color of recorder case and reflective tape), security, and configuration. b. Check for the presence of a fireproof identification plate or other approved marking on each engine, as required by the referenced data. a. Verify that aircraft is equipped with oxygen equipment per part 25, §§ 25.1441 to 25.1453. b. Oxygen/fire extinguisher pressure vessel inspections must comply with 49 CFR part 180, § 180.205, DOT, or U.S. Coast Guard requirements. c. Check all portable and fixed oxygen bottles and fire bottles for hydrostatic test dates. The FAA issues regulations and prescribes standards for the training of aircraft rescue and fire fighters (ARFF) on United States airports certificated under 14 Code of Federal Regulations part 139. The compartment or container, or the item itself, must be marked as to date of last inspection. Flotation Devices (non-extended overwater operations). h. Check the condition of the fire extinguishing system components and extinguishing agent indicators. Each occupant is protected from head injury by a safety belt when there are no objects within head strike range that would cause injury. Part 121, §§ 121.173, 121.189, 121.191, 121.193, 121.195, 121.197, 121.198, 121.141; and part 121, appendix K. Minimum Equipment List. Is there documentation for each major repair and alteration, and was it accomplished in accordance with technical data approved by the FAA? For airplanes equipped with a crew rest area having separate entries from the flight deck and the passenger compartment, a door with such a locking means must be provided between the crew rest area and the passenger compartment.”, d. The following is excerpted from part 121, § 121.313(j): “Each door must meet the requirements of Sec. Also verify that the software version meets the AFM/AOM and certificate holder’s requirements. Terrain Awareness and Warning System (TAWS). b. c. There must be adequate space to allow crewmembers(s) to assist in the evacuation of passengers. f. The 10 percent of extra oxygen masks are uniformly distributed throughout the cabin. Atlantic City International Airport, NJ 08405 Verify that: a. Protective Breathing Equipment (PBE). Aircraft Inspection (with doors, compartment doors, service panels opened; flaps and slats down). Cabin Attendant Seats, Berths, Safety Belts, and Harnesses. Receive email alerts when this page is updated! Figure 1 shows FAA data for chemical heat release rate of interior cabin materials plotted versus the reciprocal of the time-to-flashover measured in full-scale aircraft cabin fire tests. Except as provided in 14 CFR part 91, § 91.715, Special Flight Operations for Foreign Civil Aircraft, there must be within the aircraft an appropriate and current airworthiness certificate. 3) Displays magnetic heading calibration readings, in not more than 45-degree increments for part 25 aircraft, or 30-degree increments for part 23 aircraft. That the required number(s) of portable oxygen bottles are onboard, and that the POBs provide oxygen flow of at least 4 liters per minute, but not less than 2 liters per minute. Repair Assessment and Survey of Pressurized Fuselages (Damage Tolerance-Based Inspections and Procedures). Verify that manufacturer-required placards are installed. The lavatory must have a sign or placard stating, “Federal Law provides for a penalty of up to $2,200 (or $2,000), as applicable, for tampering with the smoke detector installed in this lavatory.” Refer to 8900.1, Volume 6, Chapter 2, Section 4, Figure 6-17. s. Thrust reversing indicator for each engine using a thrust-reversing device, to indicate to the flightcrew when the thrust-reversing device is in the reverse thrust position (if applicable). Verify that the aircraft has been included and maintained in accordance with the certificate holder’s program and that the program included 24-month tests and inspections of the ATC transponder systems in accordance with part 43, appendix F. Tests and inspections should include altitude reporting equipment. a. Verify that the certificate holder has a current and complete (including ADs) copy of the applicable manufacturer’s FAA-approved AFM for the particular aircraft make, model, and serial number. NOTE:  Indicator may not always be located on the flight deck. d. That the oxygen pressure vessel inspections comply with DOT. At least one hand fire extinguisher in the passenger compartment must contain Halon 1211 or equivalent. Verify that the aircraft is included and maintained in accordance with the operators structural inspection program. continued_operation/ad/alt_moc/. c. Verify there is a separate approved smoke detector or fire detector system to give warning at the pilot or flight engineer station (refer to part 25, § 25.858). Are the articles tracked by nomenclature, part number, serial number, lot number, or via records the operator retains? Its placarded maximum weight of contents. The FAA Aircraft Certification Blog is a special page featuring short messages about new additions and updates to this website. Lavatory doors must be designed to ensure that no one will become trapped inside, and if equipped with a locking device, it must be capable of being unlocked from the outside without the aid of special tools. Waste Receptacle. A copy of Bridging (transfer) Document and Continuous Airworthiness Maintenance Program (CAMP) for the aircraft, including work cards and time limits, etc. FAA Certified Repair Station. Review the TCDS for specific tracking requirements. Verify that the certificate holder has an aircraft conformity or similar process documented within its manual system. Passenger or combination cargo/passenger airplanes that have a passenger seat configuration of 10–30 seats must be equipped with either: 1) TCAS I that meets TSO-C118, Traffic Alert and Collision Avoidance System (TCAS) Airborne Equipment, TCAS I, or a later version; 2) A collision avoidance system that has a TSO-C118, or a later version; or. Refer to part 25, § 25.963. There is an approved built-in fire extinguishing or suppression system controllable from the cockpit. b. Notwithstanding the above, for all aircraft, verify the installation of the equipment required by the referenced operating rules and the OpSpecs for specific operational approvals. Cockpit Check Procedures (checklist). c. Inspect the visible inlet guide vanes; and compressor and turbine blades for dents, erosion, nicks and other irregularities. AC 43-17, Methods, Techniques, and Practices Acceptable to the Administrator Governing the Installation, Removal, or Change of Identification Data and Identification Plates. Isolation. Verify that the operator’s MEL is FAA-approved, conforms to the subject aircraft, and is current with respect to the MMEL. Skin mapping (repairs) and repair assessment if applicable (part 121, § 121.370). c. The lights must be safeguarded to prevent inadvertent operation. Verify: a. When the operator’s aircraft has been modified to a cargo freighter in accordance with an STC, perform a conformity evaluation with the FAA‑approved modification data. 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