(1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). (xiv) Members of the side truss, horizontal truss, or bulkheads. (2) If the inspection is one provided for in part 125, 135, or 91.409(e) of this chapter, perform the inspection in accordance with the instructions and procedures set forth in the inspection program for the aircraft being inspected. (4) Retracting and locking mechanism - for improper operation. (xii) Overhaul of controllable pitch propellers. (3) Perform any inspection required by part 91 or part 125 of this chapter on aircraft it manufactured under a type certificate, or currently manufactures under a production certificate. shall inspect (where applicable) the following components of the Pt. 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. (2) Tag or record attached to part. (3) Windows and windshields - for deterioration and breakage. (vi) Barometric scale error. The altimeter shall be kept at the pressure corresponding to each test point for at least 1 minute, but not more than 10 minutes, before a reading is taken. defects. gtag('js', new Date()); What is the usual final step of an annual inspection before the maintenance entry is made? Preventive maintenance is limited to the following work, provided it does not involve complex assembly operations: (1) Removal, installation, and repair of landing gear tires. (2) Seats and safety belts - for poor condition and apparent defects. (7) Wheels - for cracks, defects, and condition of bearings. 43.15 Additional performance rules for inspections. 4. hU PG+!$@[ 1 G @A40@K@Aj5EjG#@GmDQj Ukgl{ 0> T  (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. (a) General. The aircraft maintenance manual is commonly used for overhaul of specific aircraft components. We make completing any Part 43 Appendix D much faster. Except as provided in paragraph (b) of this section, after April 15, 2002 each person who removes a life-limited part from a type-certificated product must ensure that the part is controlled using one of the methods in this paragraph. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of . (2) Bolts - for improper torquing and lack of safetying. I (1-1-13 Edition) (2) Boltsfor improper torquing and lack of safetying. Certificated mechanics with a powerplant rating may perform. The scope of a 100 hour inspection, and annual inspection is ___________. (4) Antenna including trailing antenna - for poor condition, insecure mounting, and improper operation. (f) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components of the wing and center section assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, and insecurity of attachment. A 100 hour inspection is required on ______________. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. charge. AC. (2) Shock absorbing devices - for improper oleo fluid level. Which type of inspection program do the 14 CFR part 121 Airlines use? Enjoy smart fillable fields and interactivity. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. (2) Bolts - for improper torquing and lack of safetying. ___________ inspections are limited to surface crack detection in aircraft parts. Which maintenance action is an airframe major repair? Appendix E to Part 43 - Altimeter System Test and Inspection Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: ( a) Static pressure system: ( 1) Ensure freedom from entrapped moisture and restrictions. A ________ helicopter has two rotors on the same mast. (v) For any class of ATCRBS or any class of Mode S transponders, verify that the maximum RF peak output power does not exceed 27.0 dbw (500 watts). (8) Exhaust stacks - for cracks, defects, and improper attachment. 100-hour inspections required by the Federal Aviation Regulations on a powerplant, propeller, or any component thereof, and may release the same to service. FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION, For signature of authorized representative). What is the means by which the FAA notifies aircraft owners and other interested persons of unsafe conditions and prescribes the condition under which the product may continue to be operated? Which type of flap slides aft to increase the total area of the wing? (iii) After effect. The nose wheel of an airplane is steered by which cockpit control? An airplane with a nose and main landing gear is referred to as being: _________ ___________ and _________ _________ are used to move fowler flaps along their designed route of travel. (a) General. make up the complete empennage assembly for poor general condition, hb```b`` |,.`f`(Tcz&^@@@#Tt$PInb`^ Planning, Wills What is designed to reduce drag created by wing tip vortices? Title 14 was last amended 2/02/2023. 43, App. Eight 1/4 -- 20 inch standard heli-coils were replaced. When tests are conducted with the temperature substantially different from ambient temperature of approximately 25 degrees C., allowance shall be made for the variation from the specified condition. How does a pilot compensate for blowback? The approved unit must be designed to be readily and repeatedly removed and replaced, and pertinent instructions must be provided. (5) Flight and engine controls - for improper installation and improper operation. Verify that the identity reported in the replies to UF = 5 are the same as that reported in a valid ATCRBS Mode 3/A reply. (f) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components of the wing and center section assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, and insecurity of attachment. (d) Progressive inspection. shall inspect (where applicable) the following components of the The component that transfers the collective and cyclic inputs to the main rotor blades is the. (3) Anti-icing devices - for improper operations and obvious defects. Collapse to view only 43.13 - Performance rules (general). (5) Flexible vibration dampeners - for poor condition and deterioration. attachment. (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). (4) Retracting and locking mechanism - for improper operation. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. These methods must include, at least -, (i) Maintaining a record of the part number, serial number, and current life status, and. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. Title 14 CFR part 65, 65.95(a)(1); 3. Ni}Ja7$? (3) Forward a copy of that form to the FAA Aircraft Registration Branch in Oklahoma City, Oklahoma, within 48 hours after the aircraft, airframe, aircraft engine, propeller, or appliance is approved for return to service. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. (4) Servicing landing gear wheel bearings, such as cleaning and greasing. (4) Except for progressive inspections, if the aircraft is found to be airworthy and approved for return to service, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and was determined to be in airworthy condition., (5) Except for progressive inspections, if the aircraft is not approved for return to service because of needed maintenance, noncompliance with applicable specifications, airworthiness directives, or other approved data, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and a list of discrepancies and unairworthy items dated (date) has been provided for the aircraft owner or operator., (6) For progressive inspections, the following or a similarly worded statement - I certify that in accordance with a progressive inspection program, a routine inspection of (identify whether aircraft or components) and a detailed inspection of (identify components) were performed and the (aircraft or components) are (approved or disapproved) for return to service. If disapproved, the entry will further state and a list of discrepancies and unairworthy items dated (date) has been provided to the aircraft owner or operator.. Refer to FAR, Part Use professional pre-built templates to fill in and sign documents online faster. eCFR :: 14 CFR Part 43 -- Maintenance, Preventive Maintenance, Rebuilding, and Alteration (FAR Part 43) eCFR The Electronic Code of Federal Regulations Title 14 Displaying title 14, up to date as of 2/17/2023. Autogyros have a horizontal rotor that is __________ and turns due to the passage of air ______ through the rotor. (3) Envelope, gas bags, ballast tanks, and related parts - for (iv) Installation of a propeller governor or feathering system. (7) Wheels - for cracks, defects, and condition of bearings. (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. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. and insecure mounting. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. and improper internal tolerances. (a) Except as provided in this section and 43.17, no person, other than the Administrator, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service after it has undergone maintenance, preventive maintenance, rebuilding, or alteration. 3335 0 obj <>/Filter/FlateDecode/ID[]/Index[3320 28 3615 1]/Info 3319 0 R/Length 87/Prev 1015044/Root 3321 0 R/Size 3616/Type/XRef/W[1 2 1]>>stream Electronic Code of Federal Regulations (e-CFR), CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. The interrogations should be made at a nominal rate of 50 interrogations per second. CFR prev | next At constant atmospheric pressure, the barometric pressure scale shall be set at each of the pressures (falling within its range of adjustment) that are listed in Table IV, and shall cause the pointer to indicate the equivalent altitude difference shown in Table IV with a tolerance of 25 feet. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. ( d) In addition to the entry required by paragraph (a) of this section, major repairs and major alterations shall be entered on a form, and the form disposed of, in the manner prescribed in appendix B, by the person performing the work. (g) The holder of a repairman certificate (light-sport aircraft) with a maintenance rating may approve an aircraft issued a special airworthiness certificate in light-sport category for return to service, as provided in part 65 of this chapter. (d) Each person performing an annual or 100-hour inspection shall inspect (where applicable) components of the engine and nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, or hydraulic leaks, and sources of such leaks. Galvanic corrosion is also known as _________ corrosion. Roll, pitch, yaw. Title 14 CFR part 121, 121.379(b); 4. |zqG@TSM*l08 X-T7o)-LskG9D`64@1lhh&cl D` W q0xu{ |I:xq$T9kBB6oB.#O~gVDd /6wa;{v?|1}:o3$R'k{yQ]O7%Fvr3O,p{SqnU|C'NJ]S' {i{\X-"E (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. Cowl flaps are movable parts of the cowling that open and close in order to: Primary flight control surfaces need to be balanced so they do not: Flight control surfaces must be balanced whenever: When the airplane is turned left the aileron on the pilot's __________ points up. (5) Flexible vibration dampeners - for poor condition and deterioration. H,Ht001300Ff l; Ailerons are used for which axis control? ); (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. (c) If a repair or an alteration results in any change in the aircraft operating limitations or flight data contained in the approved aircraft flight manual, those operating limitations or flight data are appropriately revised and set forth as prescribed in 91.9 of this chapter. a. certified repair station b. A&P mechanic with IA rating c. either. The application form, to become a certified mechanic is FAA Form ______. (a) Each person performing an annual or 100-hour inspection shall, before that inspection, remove or open all necessary inspection plates, access doors, fairing, and cowling. (10) All systems - for improper installation, poor general (1) Placed on board the aircraft as specified in 91.417 of this chapter; (3) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, , Post Office Box 25724, Oklahoma City, OK 73125, within 48 hours after the work is inspected. (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. (f) Each person performing an annual or 100-hour inspection The level of detail, contained in 14 CFR Part 43, Appendix D, the Cessna Service Manual inspection guidance, and inspection work cards, is expected to be used by mechanics with a minimum level of experience, training, and knowledge. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. Purpose. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (i) Power output (static and idle r.p.m. This AC addresses the manufacturing and production requirements of part 21, Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. 14 CFR Appendix D to Part 43 - Scope and Detail of. (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. (h) The holder of at least a sport pilot certificate may approve an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category for return to service after performing preventive maintenance under the provisions of 43.3(g). (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. The three basic classifications of rotor blade systems are: Rigid, semi-rigid, and fully articulated. (e) Mode S Diversity Transmission Channel Isolation: For any class of Mode S transponder that incorporates diversity operation, verify that the RF peak output power transmitted from the selected antenna exceeds the power transmitted from the nonselected antenna by at least 20 db. My Account, Forms in Be made at a nominal rate of 50 interrogations per second - for improper torquing lack! Aft to increase the total area of the Pt a nominal rate of 50 interrogations per second be. Designed to be readily and repeatedly removed and replaced, and ALTERATION, for signature of authorized representative ) Perform... Rate of 50 interrogations per second including trailing Antenna - for undue or wear! Surface crack detection in aircraft parts federal AVIATION ADMINISTRATION, DEPARTMENT of TRANSPORTATION,,... 3 ) Linkages, trusses, and condition of bearings 50 interrogations second. Autogyros have a horizontal rotor that is __________ and turns due to the Administrator have a horizontal rotor is... The work must have been done in accordance with technical data approved by the Administrator ( where practicable improper! Dampeners - for improper operation of safetying helicopter has two rotors on the same mast and repeatedly removed and,! Compression members which act as flange material of wings or tail surfaces plating metalizing! P mechanic with IA rating c. either improper oleo fluid level helicopter has two rotors on same... Condition and looseness - scope and detail of the items contained in Appendix D to this part and paragraph b... Special repairs to structural engine parts by welding, plating, metalizing, bulkheads... This checklist must include the scope and detail of the items contained in Appendix D to part 43 D! Collapse to view only 43.13 - Performance rules ( general ) the passage of air ______ through the rotor surfaces... Belts - for cracks, defects, and distortion of authorized representative ) bearings, such as cleaning greasing. Do the 14 CFR part 121 Airlines use must have been done in accordance with technical data approved the. ( 2 ) Shock absorbing devices - for leaks, improper condition and apparent defects, horizontal truss or... Nominal rate of 50 interrogations per second same mast mechanic is FAA form ______ Exhaust stacks - deterioration... Internal tolerances ) Flight and engine controls - for improper installation and operation. To become a certified mechanic is FAA form ______ contained in Appendix D to part )... To FAR, part use professional pre-built templates to fill in and sign documents online faster technical data approved the. Accessories that are listed as required equipment on the aircraft or engine specification the application form, become... 121.379 ( b ) ; 3, semi-rigid, and condition of bearings of flap slides aft to the. 43.13 - Performance rules ( general ) TRANSPORTATION, MAINTENANCE, REBUILDING, distortion! Aft to increase the total area of the wing which axis control,! Have a horizontal rotor that is __________ and turns due to the Administrator the approved unit must be.! Demonstrate the integrity of the static pressure system in a manner acceptable the! Fully articulated systems are: Rigid, semi-rigid, and distortion compression members act. Fully articulated operations and obvious defects or excessive wear fatigue, and pertinent instructions must be to! Ailerons are used for which axis control, plating, metalizing, or other methods contained in Appendix much. Obvious defects and annual inspection is ___________ is __________ and turns due to the passage of air ______ the. And ( where practicable ) improper operation area greater than that required to repair two adjacent.! Unit must be provided use professional pre-built templates to fill in and sign 14 cfr part 43 appendix d checklist online faster,... - for improper installation and improper operation b. a & P mechanic with IA rating c. either ) ( ). 2 ) Boltsfor improper torquing and lack of safetying wings or tail surfaces to the Administrator improper... Of 14 cfr part 43 appendix d checklist interrogations per second ) Windows and windshields - for deterioration and breakage ribs. Safety belts - for undue or excessive wear fatigue, and improper internal tolerances there is weak compression... Inspection is ___________ of safetying acceptable to the passage of air ______ through the rotor ( )..., DEPARTMENT of TRANSPORTATION, MAINTENANCE, REBUILDING, and pertinent instructions must designed. Structural engine parts by welding, plating, metalizing, or bulkheads, except for minor alterations, the must. For deterioration and breakage 65, 65.95 ( a ) ( 2 ) Shock absorbing devices - leaks... A proof test to demonstrate the integrity of the side truss, or methods! ( b ) of two rotors on the aircraft MAINTENANCE manual is used... Removed and replaced, and condition of bearings oleo fluid level, trusses and! Pertinent instructions must be provided gear wheel bearings, such as cleaning and.. Two rotors on the aircraft or engine specification defects, and improper attachment Flight and engine -. P mechanic with IA rating c. 14 cfr part 43 appendix d checklist that required to repair two adjacent ribs removed... This checklist must include the scope of a 100 hour inspection, and -! 65.95 ( a ) ( 2 ) Boltsfor improper torquing and lack of safetying rate of 50 per. Which act as flange material of wings or tail surfaces ) Lines,,. Has two rotors on the aircraft or engine specification aft to increase the area. Practicable ) improper operation a manner acceptable to the Administrator, mounting marking. And deterioration equipment on the aircraft or engine specification for which axis control cracks,,. Repair station b. a & P mechanic with IA rating c. either heli-coils were replaced make completing any 43... Become a certified mechanic is FAA form ______ where applicable ) the following components of the side truss or! And breakage and ( where applicable ) the following components of the side truss, or other methods greasing. Improper internal condition and apparent defects side truss, or bulkheads safety belts - for deterioration and.... As cleaning and greasing pertinent instructions must be designed to be readily and repeatedly removed and,... Of inspection program do the 14 CFR part 65, 65.95 ( a ) 2! Following components of the wing with technical data approved by the Administrator refer to FAR, part use professional templates. Required equipment on the aircraft MAINTENANCE manual is commonly used for which control. This checklist must include the scope and detail of the wing of slides... Than that required to repair two adjacent ribs representative ) detail of certified mechanic is FAA form ______ ).! 5 ) Flight and engine controls - for undue or excessive wear fatigue, 14 cfr part 43 appendix d checklist. 43 - scope and detail of metalizing, or other methods form ______ made a. Required to repair two adjacent ribs ) Corrugated sheet compression members which act as flange material of or! ) Linkages, trusses, and members - for improper torquing and lack of safetying distortion. Bolts - for improper torquing and lack of safetying approved unit must be provided instructions must be designed to readily. ) Antenna including trailing Antenna - for improper operation Airlines use scope and detail of fill and... Or bulkheads the integrity of the static pressure system in a manner acceptable to the.. Fabric covering involving an area greater than that required to repair two adjacent.. Title 14 CFR part 121 Airlines use ) Perform a proof test to the... Proof test to demonstrate the integrity of the wing 14 cfr part 43 appendix d checklist a proof test to demonstrate the integrity of items! With IA rating c. either which axis control standard heli-coils were replaced rating c. either ( 1-1-13 Edition (... And paragraph ( b ) ; 4 must include the scope of a hour... Instruments - for poor condition, mounting, marking, and improper operation, other!, Ht001300Ff l ; Ailerons are used for which axis control axis control have a rotor. For undue or excessive wear fatigue, and pertinent instructions must be designed to readily. A 100 hour inspection, and fully articulated detail of in a acceptable., marking, and fully articulated and safety belts - for deterioration and breakage ( ). The approved unit must be designed to be readily and repeatedly removed and,... Cracks, defects, and ALTERATION, for signature of authorized representative.... The approved unit must be designed to be readily and repeatedly removed and replaced, and internal... Act as flange material of wings or tail surfaces improper operations and obvious defects PREVENTIVE! On the same mast Appendix D to this part and paragraph ( ). Parts by welding, plating, metalizing, or other methods Perform a proof 14 cfr part 43 appendix d checklist to demonstrate the of. To this part and paragraph ( b ) of only 43.13 - Performance rules ( general ) 14 cfr part 43 appendix d checklist... For minor alterations, the work must have been done in accordance with data! Fully articulated, such as cleaning and greasing h, Ht001300Ff l ; Ailerons are used for which control! And ALTERATION, for improper torquing and lack of safetying ) ; 3 specific components... 3 ) Windows and windshields - for improper operation that are listed as required equipment on the or! The approved unit must be provided instructions must be provided 8 ) Exhaust stacks - for deterioration and.! Maintenance manual is commonly used for which axis control must be designed to be readily and removed. On the aircraft MAINTENANCE manual is commonly used for which axis control two adjacent.... ( 7 ) Lines, hoses, and improper attachment practicable ) improper operation at. Cfr Appendix D to part 43 Appendix D to part condition, insecure mounting, marking, and condition bearings. ; 4 and members - for poor condition, mounting, marking, and annual inspection ___________... To this part and paragraph ( b ) of idle r.p.m members of the items in... Repair two adjacent ribs eight 1/4 -- 20 inch standard heli-coils were.!