In 2010, we earned an FAA Burn Testing certification of our burn test facilities, which … continued_operation/ad/alt_moc/. Medical Kit (if located on flight deck). (Refer to part 121, § 121.153c. Fuel filter bypass indication for each turbine engine (if applicable). b. c. There must be adequate space to allow crewmembers(s) to assist in the evacuation of passengers. This level of inspection is made under normally available lighting conditions such as daylight, hangar lighting, flashlight, or drop-light. Are the articles tracked by nomenclature, part number, serial number, lot number, or via records the operator retains? Check that the installations are not partial applications of the STC. a. Verify that approved ULBs are either attached to the CVR and FDR, or installed in a location from which the ULBs are not likely to become separated from the CVR and FDR. Protective Breathing Equipment (PBE). The repair station will require submission of FAA Form 8310-3 . ATC Transponder Tests and Inspections. Perform the conformity review with this data. l. That there are no more than three seats on each side of the aisle if the aircraft has a single aisle. AC 33.28-1, Compliance Criteria for 14 CFR § 33.28, Aircraft Engines, Electrical and Electronic Engine Control Systems. b. Continuous-flow oxygen mask assemblies meet the requirements of TSO-C64b, Oxygen Mask Assembly Continuous Flow, Passenger. d. Meets all of the requirements of part 121, § 121.585(d) and (e) regarding exit row seating. More on Part 139 >>, View All Series 150 Advisory Circulars (ACs), View the Complete List of Airport CertAlerts, View More FAA Airport Safety Research Reports, View All ACRP Publications or find out more about the ACRP, Page last modified: August 28, 2020 12:01:17 PM EDT, FAA Office of Airports ... under the extreme harsh conditions of a postcrash interior fire. Ensure the aircraft baggage and cargo restraint system are properly identified to their weight or load limits, are certificated, and comply with the manufacturer’s specifications. The following is excerpted from part 121, § 121.312(e): Thermal/acoustic insulation materials. AC 20-131, Airworthiness Approval of Traffic Alert and Collision Avoidance Systems (TCAS II) and Mode S Transponders. This includes the engineering, airworthiness, production and quality systems. b. Verify the system is designed so that each light is manually operable, both from the flight deck and from a point in the passenger cabin, that is readily accessible to the flight attendant seat. a. Width of Aisle. v. Propeller position indication for each propeller of turbo propeller-powered aircraft (if applicable). The FAA Aircraft Certification Blog is a special page featuring short messages about new additions and updates to this website. Fuel Tank System Maintenance Program. Class B Baggage and Cargo Compartments. Check fire extinguishing system components and extinguishing agent indicators. g. Check composite material panels for moisture contamination and bonding, delaminating, or separation of skin-bonding. On aircraft seats that have to meet 14 CFR 25.562, flammability testing is just part of the overall f. Perform a sampling inspection of articles/components installed on the aircraft. d. A ventral or tail-cone exits must be designed and constructed so that it cannot be opened during flight. Each aircraft must have inside it an effective U.S. registration certificate issued to its owner; or for operation in the U.S., the second duplicate (pink) copy of the Aircraft Registration Application; or a registration certificate issued under the laws of an International Civil Aviation Organization (ICAO) member country. c. Ensure the PBE meets the requirements of TSO-C99A, Flight Deck (Sedentary) Crewmember Protective Breathing Equipment. Door Placard. Order 8900.1, Flight Standards Information Management System, (FSIMS), Volume 3, Chapter 32, Section 2, Approval and Acceptance of Manuals and Checklists. 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). b. c. There are means to exclude hazardous quantities of smoke, flames, or extinguishing agent from any compartment occupied by the crew or passengers. Automatic Type Emergency Locator Transmitter (ELT). Stowage Compartments. For non-part 25 aircraft, verify that the installation meets the basic requirements for at least one complete radio communications system for IFR operations. Inspect for proper condition and security, and for the proper discharger types, quantities, and locations. Ensure that the aircraft is equipped with an approved flotation means for each occupant. Verify that the certificate holder has an aircraft conformity or similar process documented within its manual system. c. Ensure that a compartment used for stowage is placarded for its weight limits. b. For communications between each airplane and the appropriate dispatch office, and between each airplane and the appropriate air traffic control unit, except as specified in part 121, § 121.351(c). Also verify that the software version meets the AFM/AOM and certificate holder’s requirements. Means must be provided to enable flight crewmembers to directly enter the passenger compartment from the pilot compartment if the flight deck door becomes jammed. Verify installation of a transponder that meets the requirements of part 91, § 91.215. b. d. If the emergency exit is located only on one side of the fuselage, check that it has a conspicuous marking on the other side. m. Engine starter indication for each turbine engine-powered part 25 aircraft (if applicable). For Type I and II emergency exits with a locking mechanism released by rotary motion of the handle, the instructions must be shown by: 1) A red arrow with a shaft at least ¾-inch wide and a head twice the width of the shaft. Inspection Program and Programs Covering Other Maintenance, Preventive Maintenance, and Alterations. k. Any projecting object that could cause injury is padded to ensure that people who are seated or moving about the airplane in normal flight will not be injured. c. Check leading edges for condition and attachment. The emergency exit configuration must be designed so that neither crewmembers nor passengers need to use that door to reach the emergency exits provided for them; and. Each occupant is protected from head injury by a safety belt when there are no objects within head strike range that would cause injury. d. Standby Horizon Additional Attitude Instrument. AC 120-28, Criteria for Approval of Category III Weather Minima for Takeoff, Landing and Rollout, AC 120-29, Criteria for Approval of Category I and Category II Weather Minima for Approach. Check that the existing cargo restraint system installation (restrain system, pallets and nets) is properly identified, certificated, and complies with manufacturer’s specifications; and has a maintenance program. Refer to 8900.1, Volume 6, Chapter 2, Section 4, Figure 6-17, and AC 25-17, Transport Airplane Cabin Interiors Crashworthiness Handbook paragraphs 621 and 626. NOTE:  Use the extinguishing agent that is most suitable for the kinds of fires that are likely to occur in the compartment. Verify the installation of an approved free air temperature indicator or an air temperature indicator that provides indications that are convertible to free air temperature. b. 8900.1, Volume 6, Chapter 2, Section 6, Conduct Spot Inspection of Operator’s Aircraft. 3) Does the operator have a system to track and report AD status and compliance? Check for condition, flaking, and evidence of corrosion at seams and fasteners; and for filliform corrosion under painted surfaces. AC 45-3, Installation, Removal, or Change of Identification Data and Identification Plates on Aircraft Engines. This report is available at the Federal Aviation Administration William J. Verify the aircraft has been included in the DTR evaluation program and is maintained in accordance with the certificate holder’s inspection program and program covering other maintenance, as applicable. c. The emergency landing conditions of part 25, § 25.561(b). c. Exterior emergency lights (if installed). Regarding training fires for ARFF in the U.S., it must be noted that most of the ARFF crews are now training at propane training facilities to complete an annual FAR 139.319 requirement for live training … d. Ensure the PBE meets the preflight requirement in the Flight Attendant Manual or Flight Operations Manual (refer to part 121, § 121.337(c)). b. AFM and company manual used in lieu of AFM, if applicable (part 121, § 121.141). Ensure a safety belt plus a cushioned rest supports the arms, shoulders, head, and spine. A placard containing the legible words “No Cigarette Disposal” must be located on or near each disposal receptacle door. Pilot aircraft operating manual (part 121, § 121.135). Review the applicability of the TCDS. c. Check that instructions for the means of opening those exits from the outside are marked on the outside of each passenger emergency exit. One exit must be provided on each side of the airplane, or a top hatch may be provided. Must be employed full-time Firefighter II at an airport, driver or relief driver with a California Class B (Firefighter) Commercial Driver’s License or equivalent. AC 20-116, Marking Aircraft Fuel Filler Openings With Color Coded Decals, AC 43-204, Visual Inspection for Aircraft. NOTE:  Depending on the TC or STC, marking and designation of the emergency exist will vary. Verify the installation of an approved directional gyro, or equivalent, at each pilot station. NOTE:  Emphasize with new or altered interiors (STC). 9. Signs that notify when seat belts should be fastened and that are installed to comply with the operating rules of this Chapter must be operable by a member of the flightcrew, and when illuminated, must be legible under all probable conditions of cabin illumination to each person seated in the cabin. b. Verify the proper incorporation of ICAs for the entertainment system or equipment added to the aircraft since manufacture. The aircraft is equipped with an approved (TSO-C72c, Individual Flotation Devices) flotation means for each occupant (includes lap children). Verify installation, security, and condition of flight deck observer seat and all required peripheral equipment. Text below is excerpted from part 121, § 121.1113(b) and (c). b. Verify installation of an approved instrument at each pilot station. 25.856 of this Chapter, effective September 2, 2003. 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. Verify that instrument lights provide enough light to make each required instrument, switch, or similar instrument, easily readable and installed so that the direct rays are shielded from flight crewmembers’ eyes and that no objectionable reflections are visible to them. a. a. c. Verify proper incorporation of ICAs for any systems or equipment added to the aircraft since manufacture. c. Verify that the actual aircraft configuration conforms to the supplements, which includes STC-derived supplements. d. For metal blades, check for general condition and leading edges for erosion, nicks and dents. b. The following is excerpted from part 121, § 121.337(b)(1): “Verify that the equipment will protect the flightcrew from the effects of smoke, carbon dioxide or other harmful gases, or an oxygen deficient environment caused by other than an airplane depressurization while on flight deck duty and must protect crewmembers from the above effects while combating fires on board the airplane.”, The following is excerpted from part 121, § 121.337(b)(9)(i), “One PBE must be on the flight deck, except that the Administrator may authorize another location for this PBE if special circumstances exist that make compliance impractical and the proposed deviation would provide an equivalent level of safety.”. Burn certifications for aircraft interior materials (14 CFR part 25, § 25.853). Aircraft Registration. For passenger compartment windows, inspect for general condition and security, visibility, scratches, crazing, and condensation. e. Check that these emergency doors and or hatches/plugs can be opened from the inside by the flightcrew, as well as from the outside of the aircraft in normal ground configuration by emergency rescue personnel. d. On aircraft with two flight deck windows that cannot be opened from the outside, the most forward left main (L1) fuselage door is designated as the required emergency exit. d. If a 9.0g barrier net is installed, check it for general condition, security, fraying, hardware integrity, and airframe attachment hardware. g. Ensure that the flight attendant, when seated, has a direct view of the cabin that they are responsible for, without compromising their proximity to the floor level exit. ATC Transponder. AC 20-74, Aircraft Position and Anticollision Light Measures. The built-in fire extinguisher must be designed to discharge automatically into each disposal receptacle upon occurrence of a fire in the receptacle.”. b. b. 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