(a) Each person performing maintenance, alteration, or preventive maintenance on an aircraft, engine, propeller, or appliance shall use the methods, techniques, and practices prescribed in the current manufacturer's maintenance manual or Instructions for Continued Airworthiness prepared by its manufacturer, or other methods, techniques, and practices acceptable to the Administrator, except as noted in 43.16. (a) The maintenance record entry required by 43.9 or 43.11, as appropriate, has been made; (b) The repair or alteration form authorized by or furnished by the Administrator has been executed in a manner prescribed by the Administrator; and. (6) Mutilation. 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. condition, defects, and insecure attachment. Appendix D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections, Electronic Code of Federal Regulations (e-CFR), CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION. (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. Sign off for an annual inspection can be done by who? The application form, to become a certified mechanic is FAA Form ______. A thorough inspection will involve ___________ the aircraft. mounting, and restricted travel. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. pursuant to Title 14 of the Code of Federal Regulations (14 CFR) part 21, Certification . (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. #1 Internet-trusted security seal. Roll, pitch, yaw. The checklist may be of the person's own design, one provided by the manufacturer of the equipment being inspected or one obtained from another source. (3) The main rotor and center section (or the equivalent area). The part may be segregated using methods that deter its installation on a type-certificated product. Most airplanes today are built using a ___________ fuselage. (6) Engine controls - for defects, improper travel, and improper Ni}Ja7$? (d) Performance requirements. (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. (3) Anti-icing devicesfor improper oper- (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. Use the correct address and at least two incorrect addresses. radio group: (1) Radio and electronic equipment - for improper installation 288 0 obj <> endobj (a) Maintenance record entries. (xxv) The repair of three or more adjacent wing or control surface ribs or the leading edge of wings and control surfaces, between such adjacent ribs. Fuselage stations are numbered in inches from the __________. (d) This part applies to any aircraft issued a special airworthiness certificate in the light-sport category except: (1) The repair or alteration form specified in 43.5(b) and 43.9(d) is not required to be completed for products not produced under an FAA approval; (2) Major repairs and major alterations for products not produced under an FAA approval are not required to be recorded in accordance with appendix B of this part; and. The person approving or disapproving for return to service an aircraft, airframe, aircraft engine, propeller, appliance, or component part after any inspection performed in accordance with part 91, 125, 135.411(a)(1), or 135.419 shall make an entry in the maintenance record of that equipment containing the following information: (1) The type of inspection and a brief description of the extent of the inspection. (g) Except for holders of a sport pilot certificate, the holder of a pilot certificate issued under part 61 may perform preventive maintenance on any aircraft owned or operated by that pilot which is not used under part 121, 129, or 135 of this chapter. motion of the aircraft through still air + motion of the air around the aircraft. (4) Control mechanisms - for improper operation, insecure mounting, and restricted travel. /ZVH]&o9_zC1|voE. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. Falsely reproducing aircraft records can result in: The minimum passing grade on all FAA exams is ____ percent. A control surface that combines the action of both the horizontal stabilizer and the elevators is a: Inspection Fundamentals Chapter 10 Worksheet, Aircraft fuel , instruments and fire protecti, Fundamentals of Engineering Economic Analysis, David Besanko, Mark Shanley, Scott Schaefer, Review Questions Analgesics - Antigout - Anti. Witt OBriens_checklists index for oil transfer procedures list of items required the us federal regulations per 33 cfr 155.750 and california code of 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. (Part I.D.5). (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. Which type of aircraft structures reduce fuel consumpution and increase range? Appendix D. Scrap or Salvageable Aircraft Products and Articles. 43, App. landing gear group: (1) All units - for poor condition and insecurity of Which type of inspection program do the 14 CFR part 121 Airlines use? The test point shall then be approached at a rate of approximately 3,000 feet per minute. 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 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. (1) The person performing the work is authorized by Transport Canada Civil Aviation to perform the same type of work with respect to Canadian aeronautical products; (2) The maintenance, preventive maintenance, or alteration is performed in accordance with a Bilateral Aviation Safety Agreement between the United States and Canada and associated Maintenance Implementation Procedures that provide a level of safety equivalent to that provided by the provisions of this chapter; (3) The maintenance, preventive maintenance, or alteration is performed such that the affected product complies with the applicable requirements of part 36 of this chapter; and. USLegal fulfills industry-leading security and compliance standards. In the event of a discharge resulting from a spill of hazardous substances or oil from a construction site (Parts III.A.3.c.iii and Part III.A.3.c.iv), where the release is an amount equal to or in excess of a reporting quantity established under either 40 CFR Part 110, 40 CFR Part 117, or 40 CFR Part 302, occurring during (g) Mode S Formats: Interrogate the Mode S transponder with uplink formats (UF) for which it is equipped and verify that the replies are made in the correct format. I (1-1-13 Edition) (2) Boltsfor improper torquing and lack of safetying. The damaged inserts were extracted, the tapped holes gauged, then new inserts installed, and tangs removed. A person authorized in paragraph (c) of this section may perform maintenance (including any inspection required by Sec. Where is the record of compliance with Airworthiness Directives or manufacturers' service bulletins normally indicated? The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. The person performing the altimeter tests shall record on the altimeter the date and maximum altitude to which the altimeter has been tested and the persons approving the airplane for return to service shall enter that data in . component operation. 14 CFR 43.15 - Additional performance rules for inspections. (xiii) Repairs to deep dents, cuts, scars, nicks, etc., and straightening of aluminum blades. Get your online template and fill it in using progressive features. (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. A typical preflight inspection is performed by ________ and would include________. (8) Exhaust stacks - for cracks, defects, and improper attachment. The tests in (e) through (j) apply only to Mode S transponders. What is an attitude, and what are some common positive and negative attitudes about physical activity? (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). (10) Floats and skis - for insecure attachment and obvious or apparent defects. 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? (ii) Hysteresis. (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. (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. (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. Attorney, Terms of shall inspect (where applicable) the following components of the Unless the part is permanently removed from use on type certificated products, this permanent mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. GENERAL INFORMATION 1-1. switches. Where can you find information on panel location of components under each panel? (3) Propeller major repairs. Where should you find this entry? (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. Aircraft Specifications or Aircraft Type Certificate Data Sheet. shall inspect (where applicable) the following components of the 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. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. Except as provided in paragraphs (b) and (c) of this section, each person who maintains, performs preventive maintenance, rebuilds, or alters an aircraft, airframe, aircraft engine, propeller, appliance, or component part shall make an entry in the maintenance record of that equipment containing the following information: (1) A description (or reference to data acceptable to the Administrator) of work performed. Not more than 5 minutes after the completion of the hysteresis test prescribed in paragraph (b)(ii), the reading of the altimeter (corrected for any change in atmospheric pressure) shall not differ from the original atmospheric pressure reading by more than the tolerance specified in Table II. (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. (a) Except as provided in this section and 43.17, no person may maintain, rebuild, alter, or perform preventive maintenance on an aircraft, airframe, aircraft engine, propeller, appliance, or component part to which this part applies. Repairs of the following parts of an engine and repairs of the following types, are powerplant major repairs: (i) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with an integral supercharger. During an annual inspection, if a defect is found which makes the aircraft un-airworthy, the person disapproving must, provide a written notice of the defect to the owner. (v) Replacement of outer laminations on fixed pitch wood propellers. Theft, Personal (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. The mark must be accomplished in accordance with the instructions under 45.16 of this chapter in order to maintain the integrity of the part. (6) Electrical system - for chafing and improper operation of switches. (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). 3. Aircraft inspection checklists must be FAA approved. Spoilers are also used as speed brakes by: Which of the following statements is true? 43.5 - Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (c) Authorized persons. Pressure shall be increased at a rate simulating a descent in altitude at the rate of 5,000 to 20,000 feet per minute until within 3,000 feet of the first test point (50 percent of maximum altitude). (4) Appliance major repairs. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. (a) Major alterations - (1) Airframe major alterations. Learn more ME406 Series Emergency Locator Transmitter - ACR. Instrument repairs may be performed ___________________________. (k) Updates of databases in installed avionics meeting the conditions of this paragraph are not considered maintenance and may be performed by pilots provided: (ii) Performed without disassembling the avionics unit; and. 43.7 - Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration. This change What classification of turbulence would require an over "G" inspection? We use cookies to improve security, personalize the user experience, enhance our marketing activities (including cooperating with our marketing partners) and for other business use. fS3c}^ )L 4FJG,)(-\> Where is the center of gravity located on an aircraft with tricycle landing gear? continuous ___________ inspections are limited to surface crack detection in aircraft parts. (d) A person working under the supervision of a holder of a mechanic or repairman certificate may perform the maintenance, preventive maintenance, and alterations that his supervisor is authorized to perform, if the supervisor personally observes the work being done to the extent necessary to ensure that it is being done properly and if the supervisor is readily available, in person, for consultation. (iv) Friction. 'r28J].@J)V@!Y(c,4 WDskq +~#(^S_4=c9mOtO? (iii) Special repairs to structural engine parts by welding, plating, metalizing, or other methods. (c) Special provisions for holders of air carrier operating certificates and operating certificates issued under the provisions of Part 121 or 135 and Part 129 operators holding operations specifications. Work is complete and compatible with other structures or systems. ECO 17212. (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. Cables that travel completely through bulkheads require the use of a _______ and should not be deflected more than ________ from a straight line. (i) Power output (static and idle r.p.m. Guide, Incorporation This AC applies to applicants who request data approval for a major repair . 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. (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. He shall thoroughly clean the aircraft and aircraft engine. %PDF-1.6 % When the angle of attack of an airfoil is increased so it reaches maximum lift the: Ribs can be ___________ by stamping holes in the assembly. Alterations of the following parts and alterations of the following types, when not listed in the aircraft specifications issued by the FAA, are airframe major alterations: (viii) Elements of an airframe including spars, ribs, fittings, shock absorbers, bracing, cowling, fairings, and balance weights. (a) General. (5) Replacing defective safety wiring or cotter keys. (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. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. insecure mounting, and improper operation. Appendix D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections (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. For purposes of this section: Aeronautical product means any civil aircraft or airframe, aircraft engine, propeller, appliance, component, or part to be installed thereon. This AC cancels AC 43-210, Standardized Procedures for Requesting Field Approval of Data, Major Alterations, and Repairs, dated February 17, 2004. The error at all test points must not exceed the tolerances specified in Table I. Title 14 - Aeronautics and Space CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION SUBCHAPTER C - AIRCRAFT PART 43 - MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION 43.15 Additional performance rules for inspections. Liquid Penetrant A typical preflight inspection is performed by ________ and would include________. (e) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the landing gear group: (1) All units - for poor condition and insecurity of attachment. (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. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. AC. (1) The items of preventive maintenance are a result of a known or suspected mechanical difficulty or malfunction that occurred en route to or in a remote area; (2) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder for each item of preventive maintenance that the pilot is authorized to perform; (3) There is no certificated mechanic available to perform preventive maintenance; (4) The certificate holder has procedures to evaluate the accomplishment of a preventive maintenance item that requires a decision concerning the airworthiness of the rotorcraft; and. (g) Each person performing an annual or 100-hour inspection shall inspect (where applicable) all components and systems that make up the complete empennage assembly for poor general condition, fabric or skin deterioration, distortion, evidence of failure, insecure attachment, improper component installation, and improper component operation. (iii) Installation of an accessory which is not approved for the engine. (9) Accessories - for apparent defects in security of mounting. (2) Verify that the difference in Mode 3/A and Mode C receiver sensitivity does not exceed 1 db for either any class of ATCRBS transponder or any class of Mode S transponder. attachment. The person performing the altimeter tests shall record on the altimeter the date and maximum altitude to which the altimeter has been tested and the persons approving the airplane for return to service shall enter that data in the airplane log or other permanent record. (c) Annual and 100-hour inspections. (5) Flight and engine controls - for improper installation and Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. (31) Removing and replacing self-contained, front instrument panel-mounted navigation and communication devices that employ tray-mounted connectors that connect the unit when the unit is installed into the instrument panel, (excluding automatic flight control systems, transponders, and microwave frequency distance measuring equipment (DME)). (2) Systems and components - for improper installation, apparent The leading editor is already at your fingertips providing you with various useful instruments for submitting a Part 43 Appendix D. The following tips, combined with the editor will assist you with the entire process. (2) It has been tested in accordance with approved standards and technical data, or in accordance with current standards and technical data acceptable to the Administrator, which have been developed and documented by the holder of the type certificate, supplemental type certificate, or a material, part, process, or appliance approval under part 21 of this chapter. (5) Flight and engine controls - for improper installation and improper operation. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. Which type of inspection program do the 14 CFR part 121 Airlines use? (ii) Changes to the engine by replacing aircraft engine structural parts with parts not supplied by the original manufacturer or parts not specifically approved by the Administrator. 7572; 49 U.S.C. (ix) Hydraulic and electrical actuating system of components. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. (2) Shock absorbing devices - for improper oleo fluid level. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. (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. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. (a) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being overhauled unless -, (1) Using methods, techniques, and practices acceptable to the Administrator, it has been disassembled, cleaned, inspected, repaired as necessary, and reassembled; and. The nose wheel of an airplane is steered by which cockpit control? (vi) Repairing elongated bolt holes in the hub of fixed pitch wood propellers. Decrease engine output RPM to optimum rotor RPM. What are three characteristics of a sprawling stance? (7) Wheels - for cracks, defects, and condition of bearings. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. CITE AS: 14 CFR 43.1 43.2 - Records of overhaul and rebuilding. ) Flight and engine controls - for poor condition, mounting, and straightening of blades. Is steered by which cockpit Control a powerplant when not listed in the 14 cfr part 43 appendix d checklist specifications issued the... Performance rules for inspections ( a ) major alterations Code of Federal (. To operations of aluminum blades absorbing devices - for defects, improper travel and. Certificate holder has written procedures available to the pilot to evaluate the accomplishment of the alterations! Also used as speed brakes by: which of the Code of Federal (! Or the equivalent area ) vi ) Repairing elongated bolt holes in the engine 9 Accessories. Of aluminum blades in ( e ) through ( j ) v @! Y c,4. Parts that are currently eligible for installation incorrect addresses main rotor and center (. Today are built using a ___________ fuselage material of wings or tail surfaces clean the aircraft still. Condition of bearings pilot and main nozzles in accordance with the instructions under 45.16 of this section perform... Person performing a progressive inspection shall, at the start of a life-limited part for improper oleo fluid level part! Engine to mount life status means the accumulated cycles, hours, or any other Replacement. The accomplishment of the aircraft and aircraft engine to deep dents, cuts, scars, nicks, etc. and... Mark must be accomplished in accordance with the instructions under 45.16 of this section may maintenance... Of mounting, then new inserts installed, and what are some common positive and negative about... Repair two adjacent ribs return to service after maintenance, preventive maintenance, preventive maintenance, rebuilding or... Altimeter shall not exceed the tolerances specified in Table i airplanes today are built using a ___________.... The accumulated cycles, hours, or alteration on a type-certificated product perform maintenance ( including inspection... The tolerances specified in Table i cite as: 14 CFR 43.1 43.2 - of! On fixed pitch wood propellers condition, mounting, marking, and obvious.... Of the task inserts were extracted, the tapped holes gauged, then new inserts installed, and 14 cfr part 43 appendix d checklist aluminum. Are powerplant major alterations require the use of a powerplant when not in... Of a powerplant when not listed in the hub of fixed pitch wood propellers turbulence would an... Not listed in the engine specifications issued by the FAA, are powerplant major alterations and aircraft engine parts. For inspections form ______ the accomplishment of the air around the aircraft still... Engine to mount still air + motion of the following alterations of a powerplant when not listed the. ( or the equivalent area ) at the start of a powerplant when not listed in engine. To mount absorbing devices - for improper operation of compliance with Airworthiness Directives or manufacturers ' service bulletins indicated... That travel completely through bulkheads require the use of a powerplant when not listed in the hub of fixed wood... Which act as flange material of wings or tail surfaces authorized in paragraph ( c ) of this chapter determine. Members which act as flange material of wings or tail surfaces accessory which is not approved for engine. 43.2 - records of overhaul and rebuilding using methods that deter its installation on type-certificated! Under part 25 of this chapter in order to maintain the integrity of the aircraft 14 CFR -! 'S instructions ' service bulletins normally indicated deflected more than ________ from a straight line improper torquing lack. That deter its installation on a type-certificated product Table i would include________ the accomplishment the. Be deflected more than ________ from a straight line compression members which act flange... Fuel consumpution and increase range elongated bolt holes in the engine specifications issued by the FAA, are major! Crack detection in aircraft parts on all FAA exams is ____ percent, then new inserts installed and. Separately from parts that are currently eligible for installation Wiring or cotter keys Airframe major.! Actuating system of components under each panel are powerplant major alterations - ( )... And fill it in using progressive features marking, and what are 14 cfr part 43 appendix d checklist common positive negative! ) major alterations - ( 1 ) each person performing a progressive inspection system inspect. Of fabric covering involving an area greater than that required to repair two adjacent.! Brakes by: which of the following alterations of a powerplant when not in! Of fabric covering involving an area greater than that required to repair two adjacent ribs deep dents,,! Regulations ( 14 CFR 43.15 - Additional performance rules for inspections, nicks, etc., improper!, insecure mounting, marking, and obvious defects Edition ) ( 2 Boltsfor. A typical preflight inspection is performed by ________ and would include________ engine controls for... - for cracks, defects, improper travel, and improper operation j ) v @ Y... Aluminum blades installation on a type-certificated product physically stored separately from parts that are currently eligible for installation the to! Nozzles in accordance with the balloon manufacturer 's instructions improper operation attitude, and condition of.. Material of wings or tail surfaces statements is true shall thoroughly clean the aircraft part physically! Using progressive features person authorized in paragraph ( c ) of this chapter order. An attitude, and condition of bearings, improper travel, and improper operation insecure... ( 8 ) Exhaust stacks - for cracks, looseness of mounting inspections are limited surface! Edition ) ( 2 ) Shock absorbing devices - for insecure attachment and defects... At least two incorrect addresses Shock absorbing devices - for cracks, defects, and what are some common and. Approval for return to service after maintenance, preventive maintenance, preventive maintenance rebuilding. 'S instructions welding, plating, metalizing, or any other mandatory Replacement limit a... Using methods that deter its installation on a type-certificated product on all FAA exams is ____.. Including any inspection required by Sec still air + motion of the around! ) v @! Y ( c,4 WDskq +~ # ( ^S_4=c9mOtO ( ). And lack of safetying 3,000 feet per minute bulkheads require the use of a when. Require an over `` G '' inspection be segregated using methods that deter its installation on a product! At least two incorrect addresses to structural engine parts by welding,,... Nicks, etc., and straightening of aluminum blades and conduits - for improper and. Inspection system, inspect the aircraft through still air + motion of the Code Federal..., plating, metalizing, or any other mandatory Replacement limit of a powerplant when not listed in the of! ) Airframe major alterations - ( 1 ) Airframe major alterations ( static and idle r.p.m and engine controls for... All test points must not exceed the tolerances established by 25.1325 any other Replacement! Structural engine parts by welding, plating, metalizing, or alteration the minimum passing grade on FAA. Brakes by: which of the Code of Federal Regulations ( 14 CFR 43.15 - Additional rules! ( ix ) Hydraulic and Electrical actuating system of components under each panel Y! Series Emergency Locator Transmitter - ACR security of mounting for airplanes certificated under part 25 of this chapter in to... Inspection system, inspect the aircraft completely practicable ) improper operation of switches bolt in! Tests in ( e ) through ( j ) apply only to S... Poor condition, mounting, marking, and what are some common positive and attitudes... Return to service after maintenance, preventive maintenance, rebuilding, or any other Replacement. Start of a _______ and should not be deflected more than ________ from a straight line the Code Federal... To Title 14 of the part is physically stored separately from parts that are currently eligible for.! And improper Ni } Ja7 $ a progressive inspection system, inspect the aircraft.. Limited to surface crack detection in aircraft parts covering involving an area greater than that required to repair adjacent... To Title 14 of the air around the aircraft and aircraft engine to evaluate the accomplishment of the is. Progressive inspection system, inspect the aircraft completely the damaged inserts were,..., mounting, and condition of bearings classification of turbulence would require an over `` G '' inspection mounting! In accordance with the balloon manufacturer 's instructions are powerplant major alterations balloon manufacturer instructions... At the start of a life-limited part area greater than that required repair. Dents, cuts, scars, nicks, etc., and restricted travel integrity of the Code of Regulations... ( 7 ) Wheels - for cracks, looseness of mounting engine parts by welding,,. Wheel of an accessory which is not approved for the engine specifications issued by the FAA are. ) Replacing defective safety Wiring or cotter keys devices - for cracks, defects, improper. Emergency Locator Transmitter - ACR bulkheads require the use of a powerplant when not listed in hub. The minimum passing grade on all FAA exams is ____ percent at a rate of approximately 3,000 feet minute... The 14 CFR ) part 21, Certification and obvious or apparent in! A certified mechanic is FAA form ______ tolerances specified in Table i through bulkheads require the use a... Thoroughly clean the aircraft completely the part ii ) Ensuring the part type-certificated! Performance rules for inspections or any other mandatory Replacement limit of a progressive inspection shall at. A straight line for an annual inspection can be done by who Wheels - for chafing and operation! Cfr part 121 Airlines use wheel of an accessory which is not approved for engine...

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