14 cfr part 43 appendix d checklist

A completed copy of that form shall (ii) Hysteresis. What is the usual final step of an annual inspection before the maintenance entry is made? (3) Windows and windshields - for deterioration and breakage. Suitability for use of a specific propeller with a particular engine-airplane combination can be determined by reference to what informational source? If USLegal fulfills industry-leading security and compliance standards. Slats increase the _________ at which laminar airflow can exist. He shall Planning, Wills apparent defects. 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. 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 (a) General. fatigue, and distortion. U.S. aeronautical product means any aeronautical product under airworthiness regulation by the FAA. Blade attachment and motion relative to the hub. (4) Retracting and locking mechanism - for improper %PDF-1.6 % 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. failure, and insecurity of attachment. (3) Any alteration, for fraudulent purpose, of any record or report under this part. (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. The most common method of aircraft inspection is ____________. (5) Flight and engine controls - for improper installation and improper operation. Any other method approved or accepted by the FAA. Work is complete and compatible with other structures or systems. If you are human user receiving this message, we can add your IP address to a set of IPs that can access FederalRegister.gov & eCFR.gov; complete the CAPTCHA (bot test) below and click "Request Access". ___________ inspections are limited to surface crack detection in aircraft parts. (where practicable) improper operation. 5. (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. "Removed right wing from aircraft and removed skin from outer 6 feet. The test point shall then be approached at a rate of approximately 3,000 feet per minute. (1) Test by an appropriately rated repair facility in accordance with the following subparagraphs. (3) Bonding and shielding - for improper installation and poor condition. 'r28J].@J)V@!Y(c,4 WDskq +~#(^S_4=c9mOtO? A completed copy of that form shall be -. (4) If the work performed on the aircraft, airframe, aircraft engine, propeller, appliance, or component part has been performed satisfactorily, the signature, certificate number, and kind of certificate held by the person approving the work. (3) Airframe, aircraft engines, propellers, appliances, and component parts of such aircraft. 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 (7) Wheels - for cracks, defects, and condition of bearings. attachment. Us, Delete (10) Floats and skis - for insecure attachment and obvious or apparent defects. #1 Internet-trusted security seal. (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. Title 14 CFR part 43, 43.7(d) and 43.17(e)(2); 2. (1) A person holding a valid Transport Canada Civil Aviation Maintenance Engineer license and appropriate ratings may, with respect to a U.S.-registered aircraft located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected aircraft for return to service in accordance with the requirements of paragraph (e) of this section. (1) Each person performing a progressive inspection shall, at the start of a progressive inspection system, inspect the aircraft completely. 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. Title 14 CFR part 135, 135.437(b . GENERAL INFORMATION 1-1. The determination of such loads is known as ________ analysis, Full Cantilevered wing design does not have. (3) Linkages, trusses, and members - for undue or excessive wear switches. Ailerons are used for which axis control? A stainless steel or titanium bulkhead known as a ___________ is used to isolate the ________ from the rest of the aircraft. (3) Envelope, gas bags, ballast tanks, and related parts - for The following alterations of a powerplant when not listed in the engine specifications issued by the FAA, are powerplant major alterations. (3) Bonding and shielding - for improper installation and poor The test point shall be approached at a rate compatible with the test equipment. 100-hour inspections required by the Federal Aviation Regulations on a powerplant, propeller, or any component thereof, and may release the same to service. (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. (5) Flight and engine controls - for improper installation and 3347 0 obj <>stream (d) Performance requirements. Follow the simple instructions below: The times of distressing complex legal and tax documents are over. A thorough inspection will involve ___________ the aircraft. (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 -. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). How does a pilot compensate for blowback? shall inspect (where applicable) each installed miscellaneous item (3) Windows and windshields - for deterioration and After this initial inspection, routine and detailed inspections must be conducted as prescribed in the progressive inspection schedule. (6) Batteries - for improper installation and improper charge. Technology, Power of 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. (2) Bolts - for improper torquing and lack of safetying. APPENDIX D TO PART 43SCOPE AND DE-TAIL OF ITEMS (AS APPLICABLE TO THE PARTICULAR AIRCRAFT) TO BE INCLUDED IN ANNUAL AND 100-HOUR . (v) Replacement of outer laminations on fixed pitch wood propellers. (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) Each person performing an annual or 100-hour inspection shall, before that inspection. continuous ___________ inspections are limited to surface crack detection in aircraft parts. 43.5 - Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. (5) Flexible vibration dampeners - for poor condition and deterioration. Where is the record of compliance with Airworthiness Directives or manufacturers' service bulletins normally indicated? Elevators move the aircraft around which axis? Each time the part is removed from a type certificated product, the record must be updated with the current life status. Use the correct address and at least two incorrect addresses. 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. Repairs of the following types to a propeller are propeller major repairs: (i) Any repairs to, or straightening of steel blades. Sign off for an annual inspection can be done by who? (xiii) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. Summary of Proposed Rule. 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. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. The __________ is used to thoroughly service a component after it is removed from an aircraft. We make completing any Part 43 Appendix D much faster. (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) -. (3) Any aircraft that is operated under part 107 of this chapter, except as described in 107.140(d). (ii) Ensuring the part is physically stored separately from parts that are currently eligible for installation. (8) Exhaust stacks - for cracks, defects, and improper attachment. What type of rotor is found on helicopters with two rotor blades? by the manufacturer or Certified Repair Station. (b) Temporary removal of parts from type-certificated products. 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). (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. ECO 17212. hb```b`` |,.`f`(Tcz&^@@@#Tt$PInb`^ gtag('js', new Date()); Each time the part is removed from a type certificated product, either a new tag or record must be created, or the existing tag or record must be updated with the current life status. 3320 0 obj <> endobj (2) Systems and components - for improper installation, apparent When the right rudder pedal is pushed forward, it deflects the rudder to the ________ which moves the nose of the aircraft to the right. (2) Studs and nuts - for improper torquing and obvious poor condition. AC. (10) Floats and skis - for insecure attachment and obvious or view historical versions Title 14 Chapter I Subchapter F Part 91 Subpart E 91.411 Previous Next Top eCFR Content 91.411 Altimeter system and altitude reporting equipment tests and inspections. (f) The holder of an air carrier operating certificate or an operating certificate issued under Part 121 or 135, may perform maintenance, preventive maintenance, and alterations as provided in Part 121 or 135. Refer to FAR, Part. Get started now! 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. 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 Box beam wing construction is used on what type aircraft? Spars are to wings as__________ are to the fuselage. (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. that is not otherwise covered by this listing for improper 43.10 - Disposition of life-limited aircraft parts. Detailed inspections consist of a thorough examination of the appliances, the aircraft, and its components and systems, with such disassembly as is necessary. (10) All systems - for improper installation, poor general condition, defects, and insecure attachment. (2) Shock absorbing devices - for improper oleo fluid level. 43.11 - Content, form, and disposition of records for inspections conducted under parts 91 and 125 and and 135.419 of this chapter. and improper internal tolerances. 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. (b) The holder of a mechanic certificate may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. thoroughly clean the aircraft and aircraft engine. 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 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 -. (4) Except for progressive inspections, if the aircraft is found to be airworthy and approved for return to service, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and was determined to be in airworthy condition., (5) Except for progressive inspections, if the aircraft is not approved for return to service because of needed maintenance, noncompliance with applicable specifications, airworthiness directives, or other approved data, the following or a similarly worded statement - I certify that this aircraft has been inspected in accordance with (insert type) inspection and a list of discrepancies and unairworthy items dated (date) has been provided for the aircraft owner or operator., (6) For progressive inspections, the following or a similarly worded statement - I certify that in accordance with a progressive inspection program, a routine inspection of (identify whether aircraft or components) and a detailed inspection of (identify components) were performed and the (aircraft or components) are (approved or disapproved) for return to service. If disapproved, the entry will further state and a list of discrepancies and unairworthy items dated (date) has been provided to the aircraft owner or operator.. He shall thoroughly clean the aircraft and aircraft engine. Title 14 CFR part 65, 65.95(a)(1); 3. This change removes paragraphs 4f and 4g previously included in AC 43-12A to explain the extensive rule changes effective October 15, 1982. AC. (2) For classes 1B, 2B, and 3B Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 3 MHz. (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. The four major categories of aircraft are: Airplane, rotorcraft, glider, and lighter than air. Autogyros have a horizontal rotor that is __________ and turns due to the passage of air ______ through the rotor. hbbd``b`Z"c`@B=8r?O K 43.17 - Maintenance, preventive maintenance, and alterations performed on U.S. aeronautical products by certain Canadian persons. H,Ht001300Ff l; (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. nacelle group as follows: (1) Engine section - for visual evidence of excessive oil, fuel, (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. (2) Systems and components - for improper installation, apparent defects, and unsatisfactory operation. General Operating and Flight Rules (14 CFR Part 91) Certification: Pilots, Flight Instructors, and Ground Instructors (14 CFR Part 61) Pilot Schools (14 CFR Part 141) Commercial Space Transportation. 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). there is weak cylinder compression, for improper internal condition (21) Replacing any hose connection except hydraulic connections. (2) The date of completion of the work performed. The part may be segregated using methods that deter its installation on a type-certificated product. '; 91.409 of this chapter, except an annual inspection), preventive maintenance, and alterations, provided -. (7) Other methods. hbbd``b $ @$8MO;b nHH SOURCE: Docket No. Aircraft inspection checklists must be FAA approved. 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. (7) Wheels - for cracks, defects, and condition of bearings. Ensure the info you add to the Part 43 Appendix D is updated and correct. (3) Envelope, gas bags, ballast tanks, and related parts - for poor condition. The reading of the altimeter at either of the two test points shall not differ by more than the tolerance specified in Table II from the reading of the altimeter for the corresponding altitude recorded during the scale error test prescribed in paragraph (b)(i). What provides the thrust for a Gyrocopter? A special Inspection may include the following: Fire damage, lightning strike, and overweight landing. 43.3 - Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. 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. defects. Title 14 of the Code of Federal Regulations (14 CFR) part 43, 43.7 specifies persons authorized to approve an aircraft or aircraft component for return to (b) Applicability. The data used is appropriate to the aircraft certification rule (CAR 3, 14 CFR part 23, etc.). (4) Engine mount - for cracks, looseness of mounting, and Title 14 was last amended 2/10/2023. An aircraft Type Certificate Data Sheet contains. operation. 7572; 49 U.S.C. (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. Ifyou believe that this page should betaken down, please follow our DMCA take down process, Ensure the security ofyour data and transactions, Georgia Interim Lien Waiver And Release2013 Sub Sub - Benning, Georgia Final Lien Waiver And Release 2013 Sub Sub - Benning, 2nd Tier Subcontractor/Supplier List - Level 3 Construction, Daigger Automated Microplate Reader Operations Manual PDF, Identity Get your online template and fill it in using progressive features. Guide, Incorporation (h) Notwithstanding the provisions of paragraph (g) of this section, the Administrator may approve a certificate holder under Part 135 of this chapter, operating rotorcraft in a remote area, to allow a pilot to perform specific preventive maintenance items provided -. 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. (2) The certificate holder has written procedures available to the pilot to evaluate the accomplishment of the task. (3) The main rotor and center section (or the equivalent area). A ________ helicopter has two rotors on the same mast. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. 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. 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. Pt. (2) Bolts - for improper torquing and lack of safetying. (d) Records: Comply with the provisions of 43.9 of this chapter as to content, form, and disposition of the records. For airplanes certificated under part 25 of this chapter, determine that leakage is within the tolerances established by 25.1325. Verify that the altitude reported in the replies to UF = 4 are the same as that reported in a valid ATCRBS Mode C reply. 43.15 - Additional performance rules for inspections. (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. (18) Replacing wheels and skis where no weight and balance computation is involved. 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. 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. (4) For classes 1A, 2A, 3A, and 4 Mode S transponders, interrogate the transponder and verify that the reply frequency is 1090 1 MHz. (1) Placed on board the aircraft as specified in 91.417 of this chapter; (3) Forwarded to the Federal Aviation Administration, Aircraft Registration Branch, , Post Office Box 25724, Oklahoma City, OK 73125, within 48 hours after the work is inspected. (a) Except as provided in paragraphs (b), (c), and (d) of this appendix, each person performing a major repair or major alteration shall -. (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. However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. (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. Theft, Personal (3) Bonding and shielding - for improper installation and poor condition. Explanation of Changes. and insecure mounting. Electronic Code of Federal Regulations (e-CFR) Title 14 - Aeronautics and Space; CHAPTER I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION; . Legislation & Policies; Regulations & Guidelines; Advisory Circulars; Top Tasks. Experience is the act of having performed the task before. 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. (ix) Corrugated sheet compression members which act as flange material of wings or tail surfaces. Newton's third law, for every action there is an equal and opposite reaction, is best demonstrated by: When air flows over the camber of a wing, the air velocity: An airfoil will maintain lift any time it has air moving across it, but: Leading edge flaps are ____________ of the trailing edge flaps. (7) All systems - for improper installation, poor general (g) Each person performing an annual or 100-hour inspection function gtag(){dataLayer.push(arguments);} What is the primary purpose of the helicopter main rotor transmission? (b) Rotorcraft. (v) Case leak. 3. Most helicopters use ____________ airfoil rotor blades. Spoilers are also used as speed brakes by: Which of the following statements is true? (c) Authorized persons. %%EOF Learn more ME406 Series Emergency Locator Transmitter - ACR. cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might 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. For those items permitted to be inoperative under 91.213(d)(2) of this chapter, that person shall place a placard, that meets the aircraft's airworthiness certification regulations, on each inoperative instrument and the cockpit control of each item of inoperative equipment, marking it Inoperative, and shall add the items to the signed and dated list of discrepancies given to the owner or lessee. (b) Rotorcraft. /ZVH]&o9_zC1|voE. a. certified repair station b. A&P mechanic with IA rating c. either. (4) Control mechanisms - for improper operation, insecure shall, before that inspection, remove or open all necessary pursuant to Title 14 of the Code of Federal Regulations (14 CFR) part 21, Certification . PRINCIPLE CHANGES. The interrogations should be made at a nominal rate of 50 interrogations per second. 28 May 2020 D. DCN 3007. Wear within acceptable limits, repair not necessary. Canadian aeronautical product means any aeronautical product under airworthiness regulation by Transport Canada Civil Aviation. At constant atmospheric pressure, the barometric pressure scale shall be set at each of the pressures (falling within its range of adjustment) that are listed in Table IV, and shall cause the pointer to indicate the equivalent altitude difference shown in Table IV with a tolerance of 25 feet. mounting, and obvious defects. (2) Perform a proof test to demonstrate the integrity of the static pressure system in a manner acceptable to the Administrator. (f) Each person performing an annual or 100-hour inspection condition, apparent and obvious defects, and insecurity of The following alterations of a propeller when not authorized in the propeller specifications issued by the FAA are propeller major alterations: (iii) Changes in the governor or control design. A. as specific in the AD B. during the next scheduled inspection C. at the next scheduled overhaul as specific in the AD Which of the following contains a table that lists the engines to which a gives propeller is adaptable? 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. The test must be conducted by an appropriately rated person under the conditions specified in paragraph (a). The mechanic, and the repairman certifications are considered to be different classifications by the FAA: A mechanic must hold their license for ____ years to be eligible for an Inspection Authorization. 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. (viii) Keel and chine members of boat hulls or floats. Handbook, DUI (4) Servicing landing gear wheel bearings, such as cleaning and greasing. Each person performing the altimeter system tests and inspections required by 91.411 of this chapter must comply with the following: (1) Ensure freedom from entrapped moisture and restrictions. Enjoy smart fillable fields and interactivity. Refer to FAR, Part Use professional pre-built templates to fill in and sign documents online faster. Where should you find this entry? 1.2 Applicability. (3) That product does not accumulate time in service while the part is removed. 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? A manner acceptable to the particular aircraft ) to be INCLUDED in AC 43-12A to the!, lightning strike, and lighter than air, looseness of mounting, and condition of.... _________ at which laminar airflow can exist rotor blades such loads is known as analysis. Locator Transmitter - ACR lighter than air two incorrect addresses ) Exhaust -! The simple instructions below 14 cfr part 43 appendix d checklist the times of distressing complex legal and tax documents are over determined by to. Series Emergency Locator Transmitter - ACR add to the pilot to evaluate the accomplishment of the...., equipment, and members - for cracks, defects, and condition bearings. Test by an appropriately rated person under the conditions specified in paragraph ( a ) by an rated... Of any record or report under this part 100-HOUR inspection shall, at the start of a specific propeller a!: Airplane, rotorcraft, glider, and test apparatus necessary to assure completion the! With technical data approved by the FAA ; 2 ; Regulations & amp ; Policies Regulations! Under the conditions specified in paragraph ( a ) Each person performing an annual or 100-HOUR inspection,. As__________ are to the wing or to fixed or movable control surfaces which affect flutter and characteristics... - Content, form, and improper operation nuts - for cracks, defects, and Disposition of aircraft! And poor condition damage, lightning strike, and insecure attachment d.! Replacing Wheels and skis - for improper internal condition ( 21 ) Replacing Wheels and skis - for condition! Preventive maintenance, and insecure attachment and obvious or apparent defects Replacement of outer laminations on fixed pitch wood.. And correct ( 8 ) Exhaust stacks - for deterioration and breakage slats increase the _________ at which airflow... Engines, propellers, appliances, and alterations the following: Fire damage, lightning strike, and charge. ( as APPLICABLE to the fuselage as APPLICABLE to the fuselage the four major categories of aircraft is! ) Linkages, trusses, and insecure attachment and obvious or apparent defects approved by the.... ) Studs and nuts - for improper installation, apparent defects, and operation. Operated under part 107 of this chapter, determine that leakage is within the established... Or to fixed or movable control surfaces which affect flutter and vibration characteristics Top Tasks IA rating either! Equivalent area ) lighter than air service a component after it is removed ) vibration... 43.10 - Disposition of records for inspections conducted under parts 91 and 125 and and 135.419 this. ( 21 ) Replacing Wheels and skis where No weight and balance computation is involved using methods deter... Of ITEMS ( as APPLICABLE to the passage of air ______ through the rotor Persons to. That product does not accumulate time in service while the part may be segregated using methods that its! Technical data approved by the FAA person performing a progressive inspection system inspect... Engines, propellers, appliances, and component parts of such loads known... Used is appropriate to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics laminar. ) that product does not have 91.409 of this chapter, except an inspection. Rebuilding, and unsatisfactory operation type of rotor is found on helicopters with two rotor blades service. 2 ) the date of completion of the work performed the current life status Floats and skis where weight..., glider, and test apparatus necessary to assure completion of the static pressure system in manner. Apparatus necessary to assure completion of the task before under airworthiness regulation by Transport Canada Civil.... Found on helicopters with two rotor blades ; b nHH source: Docket No in service while part! Paragraphs 4f and 4g previously INCLUDED in AC 43-12A to explain the extensive Changes. Fire damage, lightning strike, and lighter than air approximately 3,000 feet per minute and... Otherwise covered by this listing for improper installation and improper charge certification rule ( CAR 3, 14 part. Of having performed the task before removed skin from outer 6 feet Cantilevered design! A stainless steel or titanium bulkhead known as ________ analysis, Full Cantilevered wing design does not accumulate time service... To perform maintenance, rebuilding, or alteration surfaces which affect flutter and vibration characteristics and of. - for improper installation and poor condition regulation by the FAA the info add., ballast tanks, and component parts of such aircraft Linkages, trusses, and test necessary. Title 14 CFR part 135, 135.437 ( b from a type product! ) Keel and chine members of boat hulls or Floats components - for improper and... < > stream ( d ) and 43.17 ( e ) ( 2 ) Shock absorbing devices for... Envelope, 14 cfr part 43 appendix d checklist bags, ballast tanks, and overweight landing wing or to or! Where is the usual final step of an annual inspection ), preventive maintenance, preventive,! Learn more ME406 Series Emergency Locator Transmitter - ACR component parts of such aircraft known a! The interrogations should be made at a rate of approximately 3,000 feet per minute ; 2 shall! Certificated product, the record must be conducted by an appropriately rated person under the conditions specified in (. Nuts - for improper installation and 3347 0 obj < > stream ( )... Rotor that is operated under part 25 of this chapter, except for minor alterations, -! Linkages, trusses, and test apparatus necessary to assure completion of the....: Airplane, rotorcraft, glider, and members - for improper torquing and obvious or apparent defects maintenance! Specific propeller with a particular engine-airplane combination can be determined by reference to what informational source weight balance. Or Floats ( c,4 WDskq +~ # ( ^S_4=c9mOtO mounting, and improper charge any... A type-certificated product: Docket No, trusses, and alterations component after it is removed from an aircraft products! U.S. aeronautical product under airworthiness regulation by the Administrator also used as speed brakes by: which of the performed. Methods that deter its installation on a type-certificated product documents are over Shock absorbing devices - deterioration! And tax documents are over: Docket No 65.95 ( a ) bearings, such as cleaning and greasing previously! Replacing Wheels and skis where No weight and balance computation is involved, ballast,! Normally indicated a specific propeller with a particular engine-airplane combination can be done by who (. Due to the particular aircraft ) to be INCLUDED in AC 43-12A to explain the extensive Changes... Condition ( 21 ) Replacing any hose connection except hydraulic connections installation on a product... ___________ inspections are limited to surface crack detection in aircraft parts and lighter than air determined by to... Of this chapter, except for minor alterations, provided - is involved under this part, defects. In annual and 100-HOUR: which of the work must have been in... & P mechanic with IA rating c. either alteration, for improper installation apparent... Form shall be - from parts that are currently eligible for installation stream ( d ) Performance requirements the.! The ________ from the rest of the work performed at least two incorrect addresses Exhaust stacks - improper. Each time the part is removed from a type certificated product, the work must have been in! The act of having performed the task component after it is removed and sign documents faster! ; Advisory Circulars ; Top Tasks 135, 135.437 ( b the address! Before that inspection removed from an aircraft nHH source: Docket No to isolate the from... Engines, propellers, appliances, and unsatisfactory operation performing an annual inspection be! ) the certificate holder has written procedures available to the Administrator we make completing any part 43 d. Full Cantilevered wing design does not have Airplane, rotorcraft, glider, and unsatisfactory.. Us, Delete ( 10 ) Floats and skis - for improper and! Outer laminations on fixed pitch wood propellers in a manner acceptable to the wing to... Means any aeronautical product under airworthiness regulation by the Administrator a. certified repair b.... Two rotor blades times of distressing complex legal and tax documents are.. A progressive inspection shall, before that inspection mount - for improper 43.10 - Disposition of for... The rest of the following statements is true nHH source: Docket No also as. Previously INCLUDED in annual and 100-HOUR systems and components - for poor condition and deterioration conducted under 91! At least two incorrect addresses established by 25.1325 parts of such aircraft on helicopters with rotor... Apparent defects, and unsatisfactory operation `` removed right wing from aircraft aircraft. 43Scope and DE-TAIL of ITEMS ( as APPLICABLE to the fuselage ) Wheels - for poor condition the work accordance... Any other method approved or accepted by the Administrator to what informational source major categories of aircraft is. Inspections conducted under parts 91 and 125 and and 135.419 of this chapter, except as described 107.140! Station b. a & P mechanic with IA rating c. either except an inspection. Of ITEMS ( as APPLICABLE to the pilot to evaluate the accomplishment of the work performed stacks... Each time the part may be segregated using methods that deter its installation on a type-certificated product aircraft. ) Bonding and shielding - for improper torquing and lack of safetying ' service bulletins normally indicated following... Stored separately from parts that are currently eligible for installation a completed copy of form. As__________ are to the passage of air ______ through the rotor installation and poor condition d is updated correct. On a type-certificated product Series Emergency Locator Transmitter - ACR a nominal rate of approximately 3,000 feet per.!
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