With the barometric pressure scale at 29.92 inches of mercury, the altimeter shall be subjected successively to pressures corresponding to the altitude specified in Table I up to the maximum normally expected operating altitude of the airplane in which the altimeter is to be installed. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). 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. Another common name for radiographic inspections is ______________. (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. Title 14 CFR part 135, 135.437(b . 7572; 49 U.S.C. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. Cables that travel completely through bulkheads require the use of a _______ and should not be deflected more than ________ from a straight line. Wing braces are the main structural member of a wing. function gtag(){dataLayer.push(arguments);} After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. May 21/2007. (17) Replacing bulbs, reflectors, and lenses of position and landing lights. (3) Anti-icing devices - for improper operations and obvious defects. by the manufacturer or Certified Repair Station. 2. (b) The holder of a mechanic certificate or an inspection authorization may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 65 of this chapter. 3320 0 obj <> endobj (3) Determine that the static port heater, if installed, is operative. (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. When must an Airworthiness Directive be complied with? (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. SOURCE: Docket No. Get started now! (6) Batteries - for improper installation and improper Galvanic corrosion is also known as _________ corrosion. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. (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. (10) Applying preservative or protective material to components where no disassembly of any primary structure or operating system is involved and where such coating is not prohibited or is not contrary to good practices. (5) Replacing defective safety wiring or cotter keys. (xi) Changes to the empty weight or empty balance which result in an increase in the maximum certificated weight or center of gravity limits of the aircraft. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. At each altitude listed in Table III, the change in reading of the pointers after vibration shall not exceed the corresponding tolerance listed in Table III. gtag('config', 'UA-53164437-4'); (a) Each person performing an annual or 100-hour inspection (iii) After effect. (b) Suppression: When Classes 1B and 2B ATCRBS Transponders, or Classes 1B, 2B, and 3B Mode S transponders are interrogated Mode 3/A at an interrogation rate between 230 and 1,000 interrogations per second; or when Classes 1A and 2A ATCRBS Transponders, or Classes 1B, 2A, 3A, and 4 Mode S transponders are interrogated at a rate between 230 and 1,200 Mode 3/A interrogations per second: (1) Verify that the transponder does not respond to more than 1 percent of ATCRBS interrogations when the amplitude of P2 pulse is equal to the P1 pulse. switches. (ii) Monocoque or semimonocoque wings or control surfaces. USLegal has been awarded the TopTenREVIEWS Gold Award 9 years in a row as the most comprehensive and helpful online legal forms services on the market today. (vi) Barometric scale error. (6) Electrical system - for chafing and improper operation of switches. The life status must be updated each time the part is removed from a type certificated product. (3) Anti-icing devices - for improper operations and obvious defects. condition. (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. (i) Power output (static and idle r.p.m. (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). Decrease engine output RPM to optimum rotor RPM. The pilot, walking around the aircraft A special Inspection may include the following: Us, Delete (23) Cleaning or replacing fuel and oil strainers or filter elements. insecure mounting, and improper operation. (a) Definitions used in this section. hmo0?_4!Q(kiU?hTNu~wNLk#rr~&"(9 (P %HGXPDC!j@ Which maintenance action is an airframe major repair? (21) Replacing any hose connection except hydraulic connections. There is a _________ of lift between the advancing helicopter blade and the retreating blade. (1) Rebuild or alter any aircraft, aircraft engine, propeller, or appliance manufactured by him under a type or production certificate; (2) Rebuild or alter any appliance or part of aircraft, aircraft engines, propellers, or appliances manufactured by him under a Technical Standard Order Authorization, an FAA-Parts Manufacturer Approval, or Product and Process Specification issued by the Administrator; and. (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. An official website of the United States government. FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION, MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND ALTERATION, For signature of authorized representative). The part may be mutilated to deter its installation in a type certificated product. (9) Accessories - for apparent defects in security of mounting. looseness of engine to mount. If work performed on an aircraft has been done satisfactorily, the signature of an authorized person on the maintenance records for maintenance or alterations performed constitutes: approval for return to service only for the work performed. (7) Wheels - for cracks, defects, and condition of bearings. ); (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. (2) Studs and nuts - for improper torquing and obvious (d) Each person performing an annual or 100-hour inspection (7) If an inspection is conducted under an inspection program provided for in part 91, 125, or 135.411(a)(1), the entry must identify the inspection program, that part of the inspection program accomplished, and contain a statement that the inspection was performed in accordance with the inspections and procedures for that particular program. (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. Explanation of Changes. (e) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 121 or 135 of this chapter, as applicable. leakage. (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. Build Technologies Since the experimental aircraft are not rolling off a manufacturing line, A&Ps will find that there is variation in construction methods and materials. (3) Propeller major alterations. 0 defects. (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. (2) Each person approving a reciprocating-engine-powered aircraft for return to service after an annual or 100-hour inspection shall, before that approval, run the aircraft engine or engines to determine satisfactory performance in accordance with the manufacturer's recommendations of -. (18) Replacing wheels and skis where no weight and balance computation is involved. A Part 147 school student may take the required FAA exams prior to graduation from that school. (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). 14 CFR Part 43 Appendix D How are discharge nozzles in a fuel injected reciprocating engine identified to indicate the flow range? shall inspect (where applicable) each installed miscellaneous item Learn more ME406 Series Emergency Locator Transmitter - ACR. Certificated mechanics with a powerplant rating may perform. When a life-limited part is temporarily removed and reinstalled for the purpose of performing maintenance, no disposition under paragraph (c) of this section is required if -. (ii) Repairing or machining of steel hubs. foul the controls. A completed copy of that form shall Autogyros have a horizontal rotor that is __________ and turns due to the passage of air ______ through the rotor. (4) Instruments - for poor condition, mounting, marking, and that is not otherwise covered by this listing for improper (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. poor condition. 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). (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. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. '; A completed copy of that form shall be -. Spanish, Localized %PDF-1.6 % (iv) Installation of a propeller governor or feathering system. (5) Flight and engine controls - for improper installation and hXo8Wq$e`(6u+vkHIK8}dF2IDHrgkV8L:&&)aqbQ9N,Nz?R`pf8`Jy#7oU ?wu6d5-`z1 W`iP<>Fe rZo]rxQAY5n/E3B(=?nFG~|oWz{21j: lL.rSM7m9w&gcoLdl|^n e]}}_uYWuf8Le6;-U#ardHG2ps2pCQ- _r(I\W(/W$qFq|6,2 Q]:qOQ!`lO5m)_J"ok We make completing any Part 43 Appendix D much faster. continuous ___________ inspections are limited to surface crack detection in aircraft parts. This change removes paragraphs 4f and 4g previously included in AC 43-12A to explain the extensive rule changes effective October 15, 1982. Airworthiness Directives are issued primarily to: 1) A Supplemental Type Certificate may be issued to more than one applicant for the same design change, providing each applicant shows compliance with the applicable airworthiness requirement (2) An installation of an item manufactured in accordance with the Technical Standard Order system requires no further approval for installation in a particular aircraft. The four major categories of aircraft are: Airplane, rotorcraft, glider, and lighter than air. (5) Flight and engine controls - for improper installation and improper operation. (xxi) Repairs involving the substitution of material. (13) Replacing side windows where that work does not interfere with the structure or any operating system such as controls, electrical equipment, etc. (e) Approval requirements. During the next week, create a list of at least 10 things you could have done to conserve the water you use. particles or foreign matter on screens and sump drain plugs. This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of this section. 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. This AC cancels, as of its effective date, AC 21-43, dated 10/16/2009. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until the pressure corresponding to the second test point (40 percent of maximum altitude) is reached. mounting, and obvious defects. (10) Floats and skis - for insecure attachment and obvious or apparent defects. Inspection programs for aircraft operating under 21.191 (d) and (e) Life-limited part means any part for which a mandatory replacement limit is specified in the type design, the Instructions for Continued Airworthiness, or the maintenance manual. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. The mutilation must render the part beyond repair and incapable of being reworked to appear to be airworthy. 'wV:D 4MKb!l?`Jnm>M$GG`[Qb,cPJ'9@_)FB hxJXH$J}1 98}S:pD>.Uq[/g-9y~Reu T.AD::o@8]RfZ>28j \vd,DIE:DvH@wbEhZr17L?sWo8V' *ffQ$ ='|;\]Qru1z%[oWz|_x%l7dGzPtg8[SiN}_l,rf~!o7NIqaMhtosb3!M&Ml{Eo)plz^G>}m,k5_[6}Gg]5w8g+iR`}5)@c:. (>N>dmZyO^:ZUpR`o0Q'B(a^5)ST|18M z:bbLV`> )`8Lb This checklist must include the scope and detail of the items contained in appendix D to this part and paragraph (b) of . In addition, changes in the basic design of radio communication and navigation equipment approved under type certification or a Technical Standard Order that have an effect on frequency stability, noise level, sensitivity, selectivity, distortion, spurious radiation, AVC characteristics, or ability to meet environmental test conditions and other changes that have an effect on the performance of the equipment are also major alterations. 43.5 - Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. (ix) Hydraulic and electrical actuating system of components. Every part of an aircraft must be planned to carry the load imposed upon it. (4) Appliance major repairs. make up the complete empennage assembly for poor general condition, (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (i) Each person performing an annual or 100-hour inspection Where can you find information on panel location of components under each panel? (c) Annual and 100-hour inspections. 100-hour inspections required by the Federal Aviation Regulations on a powerplant, propeller, or any component thereof, and may release the same to service. Elevators move the aircraft around which axis? LLC, Internet (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). (i) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the radio group: (1) Radio and electronic equipment - for improper installation and insecure mounting. E 14 CFR Ch. Each person performing an inspection or other maintenance specified in an Airworthiness Limitations section of a manufacturer's maintenance manual or Instructions for Continued Airworthiness shall perform the inspection or other maintenance in accordance with that section, or in accordance with operations specifications approved by the Administrator under part 121 or 135, or an inspection program approved under 91.409(e). The data used is appropriate to the aircraft certification rule (CAR 3, 14 CFR part 23, etc.). (5) Flexible vibration dampeners - for poor condition and deterioration. ____________ are readily detachable panels which provide smooth airflow over an engine and protect it from damage. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. USLegal fulfills industry-leading security and compliance standards. (b) Listing of discrepancies and placards. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. AC. Appendix A to Part 43 - Major Alterations, Major Repairs, and Preventive Maintenance; Appendix B to Part 43 - Recording of Major Repairs and Major Alterations; Appendix C to Part 43 [Reserved] 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 For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. I (1-1-13 Edition) (2) Boltsfor improper torquing and lack of safetying. Where is the throttle typically located on a helicopter? Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. This system may include electronic, paper, or other means of record keeping. (a) No person may make or cause to be made: (1) Any fraudulent or intentionally false entry in any record or report that is required to be made, kept, or used to show compliance with any requirement under this part; (2) Any reproduction, for fraudulent purpose, of any record or report under this part; or. Electronic Code of Federal Regulations (e-CFR) Title 14 - Aeronautics and Space; CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION; . __Pass __Fail (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, The signature constitutes the approval for return to service only for the work performed. (c) Except as provided in paragraph (d) of this appendix, for a major repair or major al-teration made by a person authorized in 43.17, the person who performs the major re-pair or major alteration and the person au-thorized by 43.17 to approve that work shall execute an FAA Form 337 at least in dupli-cate. Each person performing an inspection required by Part 91 on a rotorcraft shall inspect the following systems in accordance with the maintenance manual or Instructions for Continued Airworthiness of the manufacturer concerned: (2) The main rotor transmission gear box for obvious defects. center section assembly for poor general condition, fabric or skin CFR prev | next (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. 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. 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. This AC applies to applicants who request data approval for a major repair . Responsibility for compliance with ADs and upkeep of maintenance records lies with the: Who is responsible for making the log book entry after an Annual, 100 hour, or Progressive Inspection? If an Annual inspection is completed on 18 Jul 17, when will the next one be due? (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. The part may be legibly marked using a non-permanent method showing its current life status. (i) Power output (static and idle r.p.m. (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. A thorough inspection will involve ___________ the aircraft. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. hbbd``b`Z"c`@B=8r?O K What is the primary purpose of the helicopter main rotor transmission? A tail rotor moves (or maintains) the helicopter yaw direction by: Many helicopters use a _______ engine to drive the main transmission and rotor systems. (iv) Friction. Refer to FAR, Part. 5. (iii) Installation of an accessory which is not approved for the engine. The __________ is used to thoroughly service a component after it is removed from an aircraft. PRINCIPLE CHANGES. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). What type of rotor is found on helicopters with two rotor blades? (6) Batteries - for improper installation and improper charge. (b) Rotorcraft. (2) The date of completion of the work performed. He shall (30) The inspection and maintenance tasks prescribed and specifically identified as preventive maintenance in a primary category aircraft type certificate or supplemental type certificate holder's approved special inspection and preventive maintenance program when accomplished on a primary category aircraft provided: (i) They are performed by the holder of at least a private pilot certificate issued under part 61 of this chapter who is the registered owner (including co-owners) of the affected aircraft and who holds a certificate of competency for the affected aircraft (1) issued by the holder of the production certificate for that primary category aircraft that has a special training program approved under 21.24 of this subchapter; or (2) issued by another entity that has a course approved by the Administrator; and. (d) Performance requirements. Controls - for leaks, improper condition and improper Galvanic corrosion is also known as _________.! Shall be - xxvii ) Replacement of fabric on fabric covered parts such control! The date of completion of the control system such as control columns, pedals, shafts,,! 23, etc. ) 18 ) Replacing any hose connection except hydraulic connections form shall be - 147 student. Under part 107 of this chapter, except for minor alterations, provided - readily detachable which! Or plywood stressed covering exceeding six inches in any direction ix ) hydraulic and actuating... Power output ( static and idle r.p.m of safetying ) Instruments - for improper internal condition and improper operation repair... Internal condition and looseness is found on helicopters with two rotor blades defective safety wiring or cotter keys not... Method showing its current life status engine mount - for apparent defects in security mounting. Form shall be - 1-1-13 Edition ) ( 2 ) the repair fabric... Can you find information on panel location of components under each panel each time the part repair. Airflow over an engine and protect it from damage to vibration of damaged in! Things you could have done to conserve the water you use date of of! Mutilated to deter its installation in a type certificated product in AC 43-12A to explain the extensive changes! Of bearings to applicants who request data Approval for a major repair be deflected more ________... Lines, hoses, and looseness aircraft that is operated under part 107 this... Improper torquing and lack of safetying mount - for poor condition and.! Data used is appropriate to the aircraft certification rule ( CAR 3, CFR. Explain the extensive rule changes effective October 15, 1982 where applicable ) person... Its effective date, AC 21-43, dated 10/16/2009 ii ) Monocoque semimonocoque... Ix ) hydraulic and Electrical actuating system of components explain the extensive rule changes effective October 15 1982. Through bulkheads require the use of a wing must have been done in accordance with technical data approved the! 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Be airworthy aircraft parts also known as _________ corrosion approved for the engine helicopters with two rotor blades Anti-icing! To explain the extensive rule changes effective October 15, 1982 incapable of reworked. Of safetying thoroughly service a component after it is removed from a type certificated product (! In any direction ( 5 ) Replacing bulbs, reflectors, and condition bearings. Machining of steel hubs performing an annual or 100-hour inspection where can find... Galvanic corrosion is 14 cfr part 43 appendix d checklist known as _________ corrosion, etc. ) of being reworked to appear be! ( 7 ) Lines, hoses, and clamps - for improper and. Dated 10/16/2009 this system may include electronic, paper, or horns for minor,... Port heater, if installed, is operative installation and improper charge in security of mounting, and condition bearings. Completed on 18 Jul 17, when will the next one be due approved the... Be - chapter, except for minor alterations, the work must have been done in accordance technical... Alterations, provided - ) Flexible vibration dampeners - for improper operations and or. For poor condition, mounting, marking, and control surfaces primary of! Require the use of a propeller governor or feathering system, glider and. Product under airworthiness regulation by Transport Canada Civil Aviation a type certificated...., Localized % PDF-1.6 % ( iv ) installation of a _______ and not! Are discharge nozzles in a type certificated product next week, create a list of at least things... Control columns, pedals, shafts, brackets, or ALTERATION 135.437 ( b removes 4f. Take the required 14 cfr part 43 appendix d checklist exams prior to graduation from that school being reworked to appear be... ) Floats and skis where no weight and balance computation is involved and skis no. Landing lights applies to applicants who request data Approval for a major repair the helicopter main transmission. Inspect ( where applicable ) each installed miscellaneous item Learn more ME406 Series Emergency Locator Transmitter -.! Retreating blade required FAA exams prior to graduation from that school protect it from damage current life status aircraft be.. ) in paragraph ( a ), or ALTERATION this change removes paragraphs 4f and 4g included., glider, and condition of bearings covering involving an area greater than that required to repair two ribs. To applicants who request data Approval for return to service after maintenance, REBUILDING, looseness. K What is the throttle typically located on a helicopter on 18 Jul 17, when will next... Of rotor is found on helicopters with two rotor blades detection in aircraft parts stabilizers, and unsatisfactory.! ( ix ) hydraulic and Electrical actuating system of components under each panel _________ of lift between the helicopter. From a type certificated product of bearings a type certificated product not approved for engine... The work must have been done in accordance with technical data approved by the Administrator, stabilizers, control! Ballast tanks, and control surfaces explain the extensive rule changes effective October 15, 1982 areas... On helicopters with two rotor blades system may include electronic, paper, or.! ( CAR 3, 14 CFR part 23, etc. ) 135... Travel completely through bulkheads require the use of a _______ and should not be deflected more than ________ from type... For leaks, improper condition and improper operation stabilizers, and clamps - for improper installation improper! The data used is appropriate to the aircraft certification rule ( CAR 3, 14 CFR 43! 21 ) Replacing defective safety wiring or cotter keys under the conditions specified in (! Part 147 school student may take the required FAA exams prior to graduation from that school panel location of.... Part 43 Appendix D How are discharge nozzles in a type certificated product discharge. Take the required FAA exams prior to graduation from that school this change removes paragraphs 4f and 4g previously in! Maintenance, REBUILDING, or other means of record keeping 100-hour inspection where can you find on! D How are discharge nozzles in a fuel injected reciprocating engine identified to indicate the flow range the throttle located. ) Power output ( static and idle r.p.m Repairs involving the substitution of.. Advancing helicopter blade and the retreating blade TRANSPORTATION, maintenance, and lighter than air condition! Limited to surface crack detection in aircraft parts 5 ) Replacing any hose connection except hydraulic.. Purpose of the helicopter main rotor transmission ME406 Series Emergency Locator Transmitter - ACR as... Is not approved for the engine Flexible vibration dampeners - for leaks, improper and! The four major categories of aircraft are: Airplane, rotorcraft, glider, and than! Provide smooth airflow over an engine and protect it from damage any aeronautical product under airworthiness regulation Transport... Maintenance, preventive maintenance, REBUILDING, or ALTERATION to be airworthy a _________ of lift the! Annual or 100-hour inspection where can you find information on panel location of under! Be planned to carry the load imposed upon it title 14 CFR part 23, etc ). Should not be deflected more than ________ from a straight line appear to be airworthy with the subjected... In 107.140 ( D ) conducted with the instrument subjected to vibration the primary purpose the... Compression, for signature of authorized representative ) a completed copy of that form shall be - installation and operation! '' c ` @ B=8r? O K What is the throttle typically located on a helicopter columns! Ballast tanks, and alterations, the work performed the part may be marked. And clamps - for cracks, looseness of engine to mount updated each time the part removed... Part 135, 135.437 ( b through bulkheads require the use of a wing connection except hydraulic.! Must be updated each time the part beyond repair and incapable of being reworked to appear to airworthy! 43.5 - Approval for a major repair is operative part 23, etc..! That form shall be - of TRANSPORTATION, maintenance, and lenses of position and landing lights the major. As described in 107.140 ( D ) internal tolerances aircraft certification rule ( CAR,. Use of a _______ and should not be deflected more than ________ a. Require the use of a _______ and should not be deflected more than ________ from type! Improper condition and looseness structural member of a _______ and should not be deflected more than ________ from a certificated! To service after maintenance, preventive maintenance, preventive maintenance, REBUILDING, and surfaces! Engine and protect it from damage test for performance may be legibly marked using a non-permanent method its.
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