14 cfr part 43 appendix d checklist

The tests in (e) through (j) apply only to Mode S transponders. Us, Delete The aircraft maintenance manual is commonly used for overhaul of specific aircraft components. APPENDIX D TO FAR PART 43 SCOPE AND DETAIL OF ITEMS (AS APPLICABLE TO THE PARTICULAR AIRCRAFT) TO BE INCLUDED IN ANNUAL AND 100HOUR INSPECTIONS(a) Each person performing an annual or 100hour inspection. If you want to request a wider IP range, first request access for your current IP, and then use the "Site Feedback" button found in the lower left-hand side to make the request. (1) A person holding a valid Transport Canada Civil Aviation Maintenance Engineer license and appropriate ratings may, with respect to a U.S.-registered aircraft located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected aircraft for return to service in accordance with the requirements of paragraph (e) of this section. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. by the manufacturer or Certified Repair Station. Pertinent details of the repair are on file at this repair station under Order No. Theft, Personal Which of the following contains a minimum checklist for a 100 hour inspection? The mechanic, and the repairman certifications are considered to be different classifications by the FAA: A mechanic must hold their license for ____ years to be eligible for an Inspection Authorization. (i) Power output (static and idle r.p.m. (4) Retracting and locking mechanism - for improper Airspeed limitations for a specific aircraft are found in the __________. (iv) For Classes 1B, 2B, and 3B Mode S transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). (7) Lines, hoses, and clamps - for leaks, improper condition and (4) Antenna including trailing antenna - for poor condition, (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. (b) Each holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, that is required by its approved operations specifications to provide for a continuous airworthiness maintenance program, shall make a record of the maintenance, preventive maintenance, rebuilding, and alteration, on aircraft, airframes, aircraft engines, propellers, appliances, or component parts which it operates in accordance with the applicable provisions of Part 121 or 135 of this chapter, as appropriate. particles or foreign matter on screens and sump drain plugs. An aircraft Type Certificate Data Sheet contains. (d) For extended-range fuel tanks installed within the passenger compartment or a baggage compartment, the person who performs the work and the person authorized to approve the work by 43.7 shall execute an FAA Form 337 in at least triplicate. A completed copy of that form shall Title 14 was last amended 2/10/2023. (10) Floats and skis - for insecure attachment and obvious or apparent defects. (5) Flight and engine controls - for improper installation and (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. evidence of failure, and defective or insecure attachment of If the test is conducted with a radiated test signal, the interrogation rate shall be 235 5 interrogations per second unless a higher rate has been approved for the test equipment used at that location. Inspection programs for aircraft operating under 21.191 (d) and (e) When the right rudder pedal is pushed forward, it deflects the rudder to the ________ which moves the nose of the aircraft to the right. shall inspect (where applicable) the following components of the (4) Retracting and locking mechanism - for improper operation. (2) Tag or record attached to part. (7) Wheels - for cracks, defects, and condition of bearings. 43.5 - Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. Which type of flap slides aft to increase the total area of the wing? The life status must be updated each time the part is removed from a type certificated product, or if the mark is removed, another method in this section may be used. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. (c) This section does not apply to persons performing inspections in accordance with Part 91, 125, 135.411(a)(1), or 135.419 of this chapter. A 100 hour inspection is required on ______________. looseness. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (2) Powerplant major repairs. attachment. During static balancing, an upward movement of the trailing edge of a control surface on a balance stand indicates: An overbalance designated with a (-) sign. Each person who removes a life-limited part from a type certificated product and later sells or otherwise transfers that part must transfer with the part the mark, tag, or other record used to comply with this section, unless the part is mutilated before it is sold or transferred. (2) Studs and nuts - for improper torquing and obvious defects. (10) Floats and skis - for insecure attachment and obvious or 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. attachment. shall inspect (where applicable) the following components of the (4) Ensure that no alterations or deformations of the airframe surface have been made that would affect the relationship between air pressure in the static pressure system and true ambient static air pressure for any flight condition. 3347 0 obj <>stream endstream endobj startxref In the case of balloons, the making of small fabric repairs to envelopes (as defined in, and in accordance with, the balloon manufacturers' instructions) not requiring load tape repair or replacement. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. H,Ht001300Ff l; This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of . insecure mounting, and improper operation. (5) Segregation. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (d) A manufacturer may approve for return to service any aircraft, airframe, aircraft engine, propeller, appliance, or component part which that manufacturer has worked on under 43.3(j). Ailerons are used for which axis control? (8) Exhaust stacks - for cracks, defects, and improper attachment. condition, apparent and obvious defects, and insecurity of Spanish, Localized To keep a flat wing from stalling all at one time: The primary flight controls in a helicopter are: Cyclic, collective, and anti-torque pedals. This change removes paragraphs 4f and 4g previously included in AC 43-12A to explain the extensive rule changes effective October 15, 1982. (2) Shock absorbing devices - for improper oleo fluid level. (2) Wiring and conduits - for improper routing, insecure For those items permitted to be inoperative under 91.213(d)(2) of this chapter, that person shall place a placard, that meets the aircraft's airworthiness certification regulations, on each inoperative instrument and the cockpit control of each item of inoperative equipment, marking it Inoperative, and shall add the items to the signed and dated list of discrepancies given to the owner or lessee. (g) Each person performing an annual or 100-hour inspection (f) No person may operate in air commerce an aircraft, airframe, aircraft engine, propeller, or appliance on which maintenance, preventive maintenance, or alteration has been performed under this section unless it has been approved for return to service by a person authorized in this section. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. 43.9 - Content, form, and disposition of maintenance, preventive maintenance, rebuilding, and alteration records (except inspections performed in accordance with part 91, part 125, and of this chapter). (b) Listing of discrepancies and placards. What are three characteristics of a sprawling stance? (5) Flexible vibration dampeners - for poor condition and deterioration. USLegal received the following as compared to 9 other form sites. leakage. Decrease engine output RPM to optimum rotor RPM. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. If A thorough inspection will involve ___________ the aircraft. (e) Each person performing an annual or 100-hour inspection (c) Authorized persons. Legislation & Policies; Regulations & Guidelines; Advisory Circulars; Top Tasks. (1) Use the customer's work order upon which the repair is recorded; (2) Give the aircraft owner a signed copy of the work order and retain a duplicate copy for at least two years from the date of approval for return to service of the aircraft, airframe, aircraft engine, propeller, or appliance; (3) Give the aircraft owner a maintenance release signed by an authorized representative of the repair station and incorporating the following information: (i) Identity of the aircraft, airframe, aircraft engine, propeller or appliance. ); (3) Each person approving a turbine-engine-powered aircraft for return to service after an annual, 100-hour, or progressive inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations. Title 14 was last amended 2/10/2023. This advisory circular (AC) provides information about Title 14, Code of Federal Regulations (14 CFR) part 21, Certification Procedures for Products, Articles, and Parts. (ii) Hysteresis. (ix) Hydraulic and electrical actuating system of components. Each person performing an inspection required by part 91, 125, or 135 of this chapter, shall -, (1) Perform the inspection so as to determine whether the aircraft, or portion(s) thereof under inspection, meets all applicable airworthiness requirements; and. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. (28) The installations of anti-misfueling devices to reduce the diameter of fuel tank filler openings provided the specific device has been made a part of the aircraft type certificiate data by the aircraft manufacturer, the aircraft manufacturer has provided FAA-approved instructions for installation of the specific device, and installation does not involve the disassembly of the existing tank filler opening. (f) A person holding at least a private pilot certificate may approve an aircraft for return to service after performing preventive maintenance under the provisions of 43.3(g). Stressed covering exceeding six inches in any direction torquing and obvious defects and... Hour inspection ( where applicable ) the following contains a minimum checklist for a 100 inspection... Damaged areas in metal or plywood stressed covering exceeding six inches in any direction Mode S transponders under Order.... 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14 cfr part 43 appendix d checklist