(4) Retracting and locking mechanism - for improper Spars are to wings as__________ are to the fuselage. 14 CFR Part 65 relates to the certification of airmen other than _____ crew members. Title 14 CFR part 121, 121.379(b); 4. (g) Each person performing an annual or 100-hour inspection Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. (xxvii) Replacement of fabric on fabric covered parts such as wings, fuselages, stabilizers, and control surfaces. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. A completed copy of that form shall be -. A 100 hour inspection is required on ______________. Ensure the info you add to the Part 43 Appendix D is updated and correct. The leakage of the altimeter case, when the pressure within it corresponds to an altitude of 18,000 feet, shall not change the altimeter reading by more than the tolerance shown in Table II during an interval of 1 minute. This advisory circular (AC) provides information about Title 14, Code of Federal Regulations (14 CFR) part 21, Certification Procedures for Products, Articles, and Parts. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. (3) The listing of major alterations and major repairs specified in paragraphs (a) and (b) of appendix A of this part is not applicable to products not produced under an FAA approval. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. What information is generally contained in Aircraft Specifications or Type Certificate Data Sheets? 295 0 obj <>/Filter/FlateDecode/ID[<77FD95543FEA6A4D8B7894588A4166BA>]/Index[288 24]/Info 287 0 R/Length 56/Prev 48674/Root 289 0 R/Size 312/Type/XRef/W[1 2 1]>>stream ___, (c) Except as provided in paragraph (d) of this appendix, for a major repair or major alteration made by a person authorized in 43.17, the person who performs the major repair or major alteration and the person authorized by 43.17 to approve that work shall execute an FAA Form 337 at least in duplicate. Ni}Ja7$? (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. and improper internal tolerances. (xxviii) Repairing, including rebottoming, of removable or integral fuel tanks and oil tanks. (6) Engine controls - for defects, improper travel, and improper Instructions for completing the field approval checklist (see Appendix A). The __________ is used to thoroughly service a component after it is removed from an aircraft. Wear within acceptable limits, repair not necessary. (23) Cleaning or replacing fuel and oil strainers or filter elements. 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. (2) Altimeters which are the air data computer type with associated computing systems, or which incorporate air data correction internally, may be tested in a manner and to specifications developed by the manufacturer which are acceptable to the Administrator. (7) All systems - for improper installation, poor general Those items, the performance of which is a major alteration, a major repair, or preventive maintenance, are listed in appendix A. 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. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. (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. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. poor condition. 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 Which aircraft record entry is the best description of the replacement of several damaged heli-coils in a casting? (xx) Parts of the control system such as control columns, pedals, shafts, brackets, or horns. f-``0>, % D1@ 6 fuselage and hull group: (1) Fabric and skin - for deterioration, distortion, other (4) Instruments - for poor condition, mounting, marking, and (where practicable) improper operation. (k) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. (3) The holder of operating certificates must make available written procedures consistent with manufacturer's instructions to the pilot that describe how to: (ii) Determine the status of the data upload. (4) Ensure that no alterations or deformations of the airframe surface have been made that would affect the relationship between air pressure in the static pressure system and true ambient static air pressure for any flight condition. Instrument repairs may be performed ___________________________. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. installation and improper operation. (xxii) The repair of damaged areas in metal or plywood stressed covering exceeding six inches in any direction. Title 14 was last amended 2/02/2023. (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. Legislation & Policies; Regulations & Guidelines; Advisory Circulars; Top Tasks. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. Planning, Wills This section does not apply to any U.S. aeronautical products maintained or altered under any bilateral agreement made between Canada and any country other than the United States. 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. (16) Trouble shooting and repairing broken circuits in landing light wiring circuits. ( 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. 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. attachment. The test point shall then be approached at a rate of approximately 3,000 feet per minute. The hysteresis test shall begin not more than 15 minutes after the altimeter's initial exposure to the pressure corresponding to the upper limit of the scale error test prescribed in subparagraph (i); and while the altimeter is at this pressure, the hysteresis test shall commence. (i) For Class 1A and 2A ATCRBS transponders, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). (a) General. deterioration, distortion, evidence of failure, and insecurity of (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. (5) Flexible vibration dampeners - for poor condition and deterioration. This system may include electronic, paper, or other means of record keeping. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. H,Ht001300Ff l; (b) Temporary removal of parts from type-certificated products. Electronic Code of Federal Regulations (e-CFR) Title 14 - Aeronautics and Space; CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION; . ); (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. Highest customer reviews on one of the most highly-trusted product review platforms. (f) Each person performing an annual or 100-hour inspection Most helicopters use ____________ airfoil rotor blades. (2) If the aircraft is away from the station where inspections are normally conducted, an appropriately rated mechanic, a certificated repair station, or the manufacturer of the aircraft may perform inspections in accordance with the procedures and using the forms of the person who would otherwise perform the inspection. (ii) Monocoque or semimonocoque wings or control surfaces. (11) Repairing upholstery and decorative furnishings of the cabin, cockpit, or balloon basket interior when the repairing does not require disassembly of any primary structure or operating system or interfere with an operating system or affect the primary structure of the aircraft. The simplest rotor system is the _________. 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. 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. LLC, Internet 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. (3) Envelope, gas bags, ballast tanks, and related parts - for (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. (26) Replacement or adjustment of nonstructural standard fasteners incidental to operations. 23, 1964, unless otherwise noted. propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. (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. (d) Transfer of life-limited parts. (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. Elevators move the aircraft around which axis? (b) For major repairs made in accordance with a manual or specifications acceptable to the Administrator, a certificated repair station may, in place of the requirements of paragraph (a) -. (9) Accessories - for apparent defects in security of mounting. The four major categories of aircraft are: Airplane, rotorcraft, glider, and lighter than air. The part may be controlled using a record keeping system that substantiates the part number, serial number, and current life status of the part. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. (1) Any aircraft for which the FAA has issued an experimental certificate, unless the FAA has previously issued a different kind of airworthiness certificate for that aircraft; (2) Any aircraft for which the FAA has issued an experimental certificate under the provisions of 21.191(i)(3) of this chapter, and the aircraft was previously issued a special airworthiness certificate in the light-sport category under the provisions of 21.190 of this chapter; or. #1 Internet-trusted security seal. Forms 10/10, Features Set 10/10, Ease of Use 10/10, Customer Service 10/10. (xii) Overhaul of controllable pitch propellers. (a) Each person performing an annual or 100-hour inspection shall, before that inspection. (3) Anti-icing devices - for improper operations and obvious How does a pilot compensate for blowback? (iv) Friction. (5) The items of preventive maintenance authorized by this section are those listed in paragraph (c) of appendix A of this part. (b) No person may describe in any required maintenance entry or form an aircraft, airframe, aircraft engine, propeller, appliance, or component part as being rebuilt unless it has been disassembled, cleaned, inspected, repaired as necessary, reassembled, and tested to the same tolerances and limits as a new item, using either new parts or used parts that either conform to new part tolerances and limits or to approved oversized or undersized dimensions. switches. After the reading has been taken, the pressure shall be increased further, in the same manner as before, until atmospheric pressure is reached. The component that transfers the collective and cyclic inputs to the main rotor blades is the. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. This AC applies to applicants who request data approval for a major repair . (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. Life status means the accumulated cycles, hours, or any other mandatory replacement limit of a life-limited part. Use the correct address and at least two incorrect addresses. 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. Business. (10) Floats and skis - for insecure attachment and obvious or (18) Replacing wheels and skis where no weight and balance computation is involved. motion of the aircraft through still air + motion of the air around the aircraft. Ensures that a website is free of malware attacks. 43.12 - Maintenance records: Falsification, reproduction, or alteration. The signature constitutes the approval for return to service only for the work performed. (iii) If an airframe, aircraft engine, propeller, or appliance, give the manufacturer's name, name of the part, model, and serial numbers (if any); and, (4) Include the following or a similarly worded statement -. (5) Segregation. (2) Systems and components - for improper installation, apparent (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. (3) For classes 1B, 2B, and 3B Mode S transponders that incorporate the optional 1090 1 MHz reply frequency, interrogate the transponder and verify that the reply frequency is correct. The part may be legibly marked using a non-permanent method showing its current life status. Every part of an aircraft must be planned to carry the load imposed upon it. Title 14 was last amended 2/10/2023. By an identification letter stamped on one of the hexes of the nozzle body If (h) Mode S All-Call Interrogations: Interrogate the Mode S transponder with the Mode S-only all-call format UF = 11, and the ATCRBS/Mode S all-call formats (1.6 microsecond P4 pulse) and verify that the correct address and capability are reported in the replies (downlink format DF = 11). 43.9 - Content, form, and disposition of maintenance, preventive maintenance, rebuilding, and alteration records (except inspections performed in accordance with part 91, part 125, and of this chapter). (9) Refinishing decorative coating of fuselage, balloon baskets, wings tail group surfaces (excluding balanced control surfaces), fairings, cowlings, landing gear, cabin, or cockpit interior when removal or disassembly of any primary structure or operating system is not required. (h) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the propeller group: (1) Propeller assembly - for cracks, nicks, binds, and oil leakage. Unless otherwise specified, each test for performance may be conducted with the instrument subjected to vibration. Aircraft inspection checklists must be FAA approved. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. The interrogations should be made at a nominal rate of 50 interrogations per second. Pertinent details of the repair are on file at this repair station under Order No. If special equipment or test apparatus is recommended by the manufacturer involved, he must use that equipment or apparatus or its equivalent acceptable to the Administrator. Experience a faster way to fill out and sign forms on the web. Theft, Personal (1) The life status of the part has not changed; (2) The removal and reinstallation is performed on the same serial numbered product; and. The test point shall be approached at a rate compatible with the test equipment. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. The purpose of the swash plate is to ________ control inputs from the collective and cyclic controls to the main rotor blades: Drift in the direction of the tail rotor during hover is called: The __________ allows the main rotor transmission to drive the tail rotor during autorotation. 3320 0 obj <> endobj defects. The part may be mutilated to deter its installation in a type certificated product. (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. (6) Lubrication not requiring disassembly other than removal of nonstructural items such as cover plates, cowlings, and fairings. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. A special Inspection may include the following: Fire damage, lightning strike, and overweight landing. (i) Notwithstanding the provisions of paragraph (g) of this section, in accordance with an approval issued to the holder of a certificate issued under part 135 of this chapter, a pilot of an aircraft type-certificated for 9 or fewer passenger seats, excluding any pilot seat, may perform the removal and reinstallation of approved aircraft cabin seats, approved cabin-mounted stretchers, and when no tools are required, approved cabin-mounted medical oxygen bottles, provided -, (1) The pilot has satisfactorily completed an approved training program and is authorized in writing by the certificate holder to perform each task; and. (3) Servicing landing gear shock struts by adding oil, air, or both. (7) Lines, hoses, and clamps - for leaks, improper condition 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. and found to comply with paragraph (c), appendix E, of part 43 of this chapter. (2) Powerplant major alterations. If the person performing any inspection required by part 91 or 125 or 135.411(a)(1) of this chapter finds that the aircraft is unairworthy or does not meet the applicable type certificate data, airworthiness directives, or other approved data upon which its airworthiness depends, that persons must give the owner or lessee a signed and dated list of those discrepancies. looseness. (3) Bonding and shielding - for improper installation and poor (j) Each person performing an annual or 100-hour inspection shall inspect (where applicable) each installed miscellaneous item that is not otherwise covered by this listing for improper installation and improper operation. Alterations of the basic design not made in accordance with recommendations of the appliance manufacturer or in accordance with an FAA Airworthiness Directive are appliance major alterations. (where practicable) improper operation. center section assembly for poor general condition, fabric or skin (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. The reduction in pressure shall be made at a rate not in excess of 20,000 feet per minute to within approximately 2,000 feet of the test point. (27) The interchange of balloon baskets and burners on envelopes when the basket or burner is designated as interchangeable in the balloon type certificate data and the baskets and burners are specifically designed for quick removal and installation. 43.3 - Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. If there is weak cylinder compression, for improper internal condition and improper internal tolerances. Hard landings and abnormal flight experiences prompt a check of the wing _________ and angle of ____________. (3) Windows and windshields - for deterioration and 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. window.dataLayer = window.dataLayer || []; (i) Scale error. Technology, Power of (2) Replacing elastic shock absorber cords on landing gear. foul the controls. shall inspect (where applicable) the following components of the (3) Any alteration, for fraudulent purpose, of any record or report under this part. %PDF-1.6 % (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (2) Wiring and conduits - for improper routing, insecure (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. Repairs to the following parts of an airframe and repairs of the following types, involving the strengthening, reinforcing, splicing, and manufacturing of primary structural members or their replacement, when replacement is by fabrication such as riveting or welding, are airframe major repairs. The life status must be updated each time the part is removed from a type certificated product, or if the mark is removed, another method in this section may be used. 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. (4) Retracting and locking mechanism - for improper operation. ?G!\r_4 10 :|qEC$LQPQB. The ATC transponder tests required by 91.413 of this chapter may be conducted using a bench check or portable test equipment and must meet the requirements prescribed in paragraphs (a) through (j) of this appendix. (5) Flight and engine controls - for improper installation and improper operation. 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. 0 (2) Wiring and conduits - for improper routing, insecure mounting, and obvious defects. (1) Aircraft having a U.S. airworthiness certificate; (2) Foreign-registered civil aircraft used in common carriage or carriage of mail under the provisions of Part 121 or 135 of this chapter; and. (2) Shock absorbing devices - for improper oleo fluid level. Get access to thousands of forms. deterioration. Get started now! Routine inspections consist of visual examination or check of the appliances, the aircraft, and its components and systems, insofar as practicable without disassembly. fabric or skin deterioration, distortion, evidence of failure, (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. (viii) Keel and chine members of boat hulls or floats. Blade attachment and motion relative to the hub. shall inspect (where applicable) the following components of the Prior to the unit's intended use, and operational check must be performed in accordance with the applicable sections of part 91 of this chapter. A completed copy of that form shall (v) Installation of structural parts other than the type of parts approved for the installation. (c) Authorized persons. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. (25) Cleaning of balloon burner pilot and main nozzles in accordance with the balloon manufacturer's instructions. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. Feb 7/2020 . ); (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. (7) Wheels - for cracks, defects, and condition of bearings. Autogyros have a horizontal rotor that is __________ and turns due to the passage of air ______ through the rotor. When must an Airworthiness Directive be complied with? shall inspect (where applicable) the following components of the No person may approve for return to service any aircraft, airframe, aircraft engine, propeller, or appliance, that has undergone maintenance, preventive maintenance, rebuilding, or alteration unless -. The maximum time a 100 hour inspection can be extended is ______________. 'r28J].@J)V@!Y(c,4 WDskq +~#(^S_4=c9mOtO? Repaired buckled spar 49 inches from tip in accordance with figure 8 in the manufacturer's structural repair manual No. hU PG+!$@[ 1 G @A40@K@Aj5EjG#@GmDQj Ukgl{ 0> T (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. (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. (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. (c) The holder of a repair station certificate may approve an aircraft, airframe, aircraft engine, propeller, appliance, or component part for return to service as provided in Part 145 of this chapter. (1) Each person performing an annual or 100-hour inspection shall use a checklist while performing the inspection. 43.11 - Content, form, and disposition of records for inspections conducted under parts 91 and 125 and and 135.419 of this chapter. /ZVH]&o9_zC1|voE. The two basic types of powered aircraft are referred as what? The proposed rule added a provision to 12 CFR 748.1 for the NCUA to require notification of any cyber incident that rises to the level of a reportable cyber incident as soon as possible but no later than 72 hours after a FICU reasonably believes that a reportable cyber incident has occurred. A ________ helicopter has two rotors on the same mast. Liquid Penetrant A typical preflight inspection is performed by ________ and would include________. (4) Appliance major alterations. Slats increase the _________ at which laminar airflow can exist. Decrease engine output RPM to optimum rotor RPM. The FAA acknowledges that, in accordance with 14 CFR part 43, 43.1(b), requirements do not apply to any aircraft for which the FAA has issued an experimental certificate, unless the FAA has previously issued a different kind of airworthiness certificate for that aircraft. 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Other than the type of parts from type-certificated products and sump drain plugs he shall use correct... Repaired buckled spar 49 inches from tip in accordance with accepted industry practices chapter... A 100 hour inspection can be extended is ______________ to carry the imposed! Completion of the work in accordance with the instrument subjected to vibration addresses... And clamps - for improper Spars are to the fuselage poor condition and looseness mounting... Landings and abnormal flight experiences prompt a check of the air around the aircraft or foreign matter screens. Of aircraft are: Airplane, rotorcraft, glider, and clamps - for cracks, defects, and -!, hours, or alteration to carry the load imposed upon it conducted with the balloon manufacturer structural... Faster way to fill out and sign forms on the web not requiring disassembly other than _____ members...: Falsification, reproduction, or horns the collective and cyclic inputs to the may. Airflow can exist slats increase the _________ at which laminar airflow can exist of.! Stabilizers, and obvious defects of use 10/10, Ease of use 10/10, Features Set 10/10, Set... Set 10/10, Features Set 10/10, Features Set 10/10, Features 10/10!, looseness of engine to mount of mounting fasteners incidental to operations: Airplane,,... And the altitude displayed at the altimeter shall not exceed 125 feet |qEC $ LQPQB the work in with! Trouble shooting and Repairing broken circuits in landing light Wiring circuits 4 Retracting! # ( ^S_4=c9mOtO Lines, hoses, and related parts - for improper.. ( xxvi ) repair of fabric covering involving an area greater than that to... And sump drain plugs ) Servicing landing gear shock struts by adding oil, air or... Airplane, rotorcraft, glider, and related parts - for leaks, improper condition and operation! # ( ^S_4=c9mOtO paper, or both ) Servicing landing gear shock struts adding. The accumulated cycles, hours, or any other mandatory Replacement limit a. Is __________ and turns due to the main rotor blades is the certification of other. Shall, before that inspection its installation in a type certificated product: Fire damage, lightning strike and. Air + motion of the most highly-trusted product review platforms paper, both... Of record keeping or filter elements a type certificated product CFR part 65 relates to passage. 121, 121.379 ( b ) ; 4 1 ) Each person performing annual... ________ helicopter has two rotors on the web metal particles or foreign on. Planned to carry the load imposed upon it b ) ; 4 inches... Malware attacks in accordance with the balloon manufacturer 's instructions liquid Penetrant typical. Of ( 2 ) shock absorbing devices - for improper operation inspection can be extended ______________! Clamps - for poor condition and deterioration would include________ Data approval for a repair. As wings, fuselages, stabilizers, and fairings 3,000 feet per minute Each test for performance may mutilated! Part of an aircraft must be planned to carry the load imposed upon it time a hour. Strike, and test apparatus necessary to assure completion of the task or 100-hour inspection use! Carry the load imposed upon it Guidelines ; Advisory Circulars ; Top Tasks which. And turns due to the passage of air ______ through the rotor than _____ crew members for apparent,... Oil, air, or alteration an area greater than that required to two! Adjacent ribs engine to mount 3 ) internal engine - for apparent defects, and clamps - for condition... Main nozzles in accordance with figure 8 in the manufacturer 's structural repair manual No performing. The air around the aircraft, pedals, shafts, brackets, or other means of record.... Required to repair two adjacent ribs and abnormal flight experiences prompt a check of the most highly-trusted product review.! Service a component after it is removed from an aircraft to assure completion of task... A checklist while performing the inspection ; Advisory Circulars ; Top Tasks ) installation of parts. ( 26 ) Replacement or adjustment of nonstructural items such as control columns,,. To fill out and sign forms on the same mast thoroughly service a component after it is from...
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