(iii) Installation of an accessory which is not approved for the engine. Disposition of life-limited aircraft parts. 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. (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. SB-115 (10/26/83) -- Deflation Panel Pull Forces . However, except for minor alterations, the work must have been done in accordance with technical data approved by the Administrator. The General Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks. 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. 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. (ii) If an aircraft, the make, model, serial number, nationality and registration marks, and location of the repaired area. 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). (6) Engine controls - for defects, improper travel, and improper safetying. 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 D to Part 43 - Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections, Appendix E to Part 43 - Altimeter System Test and Inspection, Appendix F to Part 43 - ATC Transponder Tests and Inspections, First Test Point (50 percent of maximum altitude), Second Test Point (40 percent of maximum altitude). A completed copy of that form shall be -. (c) Each person performing an annual or 100-hour inspection shall inspect (where applicable) the following components of the cabin and cockpit group: (1) Generally - for uncleanliness and loose equipment that might foul the controls. Each person who removes a life-limited part from a type certificated product and later sells or otherwise transfers that part must transfer with the part the mark, tag, or other record used to comply with this section, unless the part is mutilated before it is sold or transferred. here. (ii) Hysteresis. Before the permit is issued, an FAA inspector may personally inspect the aircraft, or require it to be inspected by an FAA certificated A&P mechanic or an appropriately certificated repair station, to determine its safety for the intended flight. (7) Lines, hoses, and clamps - for leaks, improper condition and looseness. will bring you directly to the content. 313, 314, and 601 through 610 of the Federal Aviation Act of 1958 (49 U.S.C. 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. 43-45, 77 FR 71096, Nov. 29, 2012], 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 date the work was completed. 6(c), Dept. (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. (7) All systems - for improper installation, poor general condition, apparent and obvious defects, and insecurity of attachment. 23, 1964, as amended by Amdt. (vi) Installation of parts not approved for the propeller. (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. (xiv) The repair or replacement of internal elements of blades. Aircraft Inspection and Repair - Federal Aviation . (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. (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. ); (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. 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. Repairs of the following types to appliances are appliance major repairs: (i) Calibration and repair of instruments. The difference between the automatic reporting output and the altitude displayed at the altimeter shall not exceed 125 feet. 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. (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. (3) Any alteration, for fraudulent purpose, of any record or report under this part. book to meet the regulatory requirements. Preventive maintenance is limited to the following work, provided it does not involve complex assembly operations: (1) Removal, installation, and repair of landing gear tires. 27, 2001; Amdt. This inspection will be recorded in the aircraft maintenance records. [Doc. will also bring you to search results. Search & Navigation "Published Edition". site when drafting amendatory language for Federal regulations: This applies to owner maintenance as well. (a) To be eligible for a repairman certificate a person must (1) Be at least 18 years of age; (2) Be specially qualified to perform maintenance on aircraft or components thereof, appropriate to the job for which he is employed; (3) Linkages, trusses, and members - for undue or excessive wear fatigue, and distortion. If you would like to comment on the current content, please use the 'Content Feedback' button below for instructions on contacting the issuing agency. Background and more details are available in the FAA-2000-8017, 67 FR 2110, Jan. 15, 2002, as amended by Amdt. (1) For all classes of ATCRBS transponders, interrogate the transponder and verify that the reply frequency is 1090 3 Megahertz (MHz). It is not an official legal edition of the CFR. (c) If a repair or an alteration results in any change in the aircraft operating limitations or flight data contained in the approved aircraft flight manual, those operating limitations or flight data are appropriately revised and set forth as prescribed in 91.9 of this chapter. The altimeter shall be subjected to a steady rate of decrease of pressure approximating 750 feet per minute. (2) It has been tested in accordance with approved standards and technical data, or in accordance with current standards and technical data acceptable to the Administrator, which have been developed and documented by the holder of the type certificate, supplemental type certificate, or a material, part, process, or appliance approval under part 21 of this chapter. A mechanic can be the one to solicit the ferry permit on the owner's behalf if the owner supplies a signed letter of authorization. 23. (iv) Friction. This document is available in the following developer friendly formats: Information and documentation can be found in our (a) Maintenance record entries. (2) A Transport Canada Civil Aviation Approved Maintenance Organization (AMO) holding appropriate ratings may, with respect to a U.S.-registered aircraft or other U.S. aeronautical products located in Canada, perform maintenance, preventive maintenance, and alterations in accordance with the requirements of paragraph (d) of this section and approve the affected products for return to service in accordance with the requirements of paragraph (e) of this section. For the purposes of this subparagraph, the overhaul of a component or system is considered to be a detailed inspection. (c) This part applies to all life-limited parts that are removed from a type certificated product, segregated, or controlled as provided in 43.10. Measure the automatic pressure altitude at the output of the installed ATC transponder when interrogated on Mode C at a sufficient number of test points to ensure that the altitude reporting equipment, altimeters, and ATC transponders perform their intended functions as installed in the aircraft. [Amdt. (Secs. (ii) For Class 1B and 2B ATCRBS Transponders, verify that the minimum RF peak output power is at least 18.5 dbw (70 watts). (1) Records of the maintenance, preventive maintenance, and alteration and records of the 100-hour, annual, progressive, and other required or approved inspections, as appropriate, for each aircraft (including the airframe) and each engine, propeller, rotor, and appliance of an aircraft. 43.5 Approval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. 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. 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. (b) Temporary removal of parts from type-certificated products. This is an automated process for (3) The signature, the certificate number, and kind of certificate held by the person approving or disapproving for return to service the aircraft, airframe, aircraft engine, propeller, appliance, component part, or portions thereof. No. (c) The holder of a repairman certificate may perform maintenance, preventive maintenance, and alterations as provided in part 65 of this chapter. Aircraft Maintenance Records and Airworthiness Directives for General Aviation Jun. (b) Listing of discrepancies and placards. (5) Replacing defective safety wiring or cotter keys. (12) Making small simple repairs to fairings, nonstructural cover plates, cowlings, and small patches and reinforcements not changing the contour so as to interfere with proper air flow. 43-31, 54 FR 34330, Aug. 18, 1989; Doc. (3) The main rotor and center section (or the equivalent area). 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. (19) Replacing any cowling not requiring removal of the propeller or disconnection of flight controls. The person performing the altimeter tests shall record on the altimeter the date and maximum altitude to which the altimeter has been tested and the persons approving the airplane for return to service shall enter that data in the airplane log or other permanent record. When tests are conducted with the temperature substantially different from ambient temperature of approximately 25 degrees C., allowance shall be made for the variation from the specified condition. 106(f), 106(g), 40105, 40113, 44701-44702, 44704, 44707, 44709, 44711, 44713, 44715, 45303. Use the correct address and at least two incorrect addresses. (c) Preventive maintenance. The regulations require that all maintenance be appropriately documented in the aircraft's logbooks. 101, 610, 72 Stat. Each entry must include the following information: A description of the work performed, or references to data that are acceptable to the Administrator. user convenience only and is not intended to alter agency intent The software release life cycle is the process of developing, testing, and distributing a software product. 43-51, 86 FR 4381, Jan. 15, 2021], (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. (1) Execute FAA Form 337 at least in duplicate; (2) Give a signed copy of that form to the aircraft owner; and. (iii) For Class 1A, 2A, 3A, and 4 and those Class 1B, 2B, and 3B Mode S transponders that include the optional high RF peak output power, verify that the minimum RF peak output power is at least 21.0 dbw (125 watts). Questions? (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. 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). 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 -. (xii) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurization, electrical, hydraulic, de-icing, or exhaust systems. (xxvi) Repair of fabric covering involving an area greater than that required to repair two adjacent ribs. (iv) Removal of accessories that are listed as required equipment on the aircraft or engine specification. 106(g) (Revised Pub. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 44188, Aug. 4, 2006]. 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. (d) Transfer of life-limited parts. No. Regulation Y (2) The date of completion of the work performed. 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. Note the extra lines for adding additional categories. 43-40, 71 FR 40877, July 14, 2005]. (2) Verify that the transponder replies to at least 90 percent of ATCRBS interrogations when the amplitude of the P2 pulse is 9 dB less than the P1 pulse. Logbook is built-in to the ForeFlight app, making it easy for pilots to log and share flights, track hours, review currency, record certificates and ratings, receive electronic instructor endorsements, and generate experience reports. The Code of Federal Regulations (CFR) is the official legal print publication containing the codification of the general and permanent rules published in the Federal Register by the departments and agencies of the Federal Government. (7) Making simple fabric patches not requiring rib stitching or the removal of structural parts or control surfaces. Noise emanating from trains and associated repair and maintenance equipment. (1) Persons must present their pilot certificate, medical certificate, logbook, or any other record required by this part for inspection upon a reasonable request by - (i) The Administrator; (ii) An authorized representative from the National Transportation Safety Board; or (iii) Any Federal, State, or local law enforcement officer. (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. Content, form, and disposition of maintenance, preventive maintenance, rebuilding, and alteration records (except inspections performed in accordance with part 91, part 125, 135.411(a)(1), and 135.419 of this chapter). However, those who maintain separate records for the airframe, power plant, propellers, and other components must document the 100-hour inspection, if required, in the record of each component (see 14 CFR 43.11 (a)). Each is a special inspection unto itself; they're all different. (3) Internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. . The FAA lists separate requirements to log PIC time in 61.51 (e) (1). (ii) Repairing or machining of steel hubs. 43.15 Additional performance rules for inspections. 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. 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). (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. He shall thoroughly clean the aircraft and aircraft engine. (4) Engine mount - for cracks, looseness of mounting, and looseness of engine to mount. through logbooks usually kept in the maintenance hangar. 43-37, 66 FR 21066, Apr. 43-31, 54 FR 34330, Aug. 18, 1989; 71 FR 58495, Oct. 4, 2006; Amdt. (d) Performance requirements. [Doc. These words show that the FAA intends that a logbook, or equivalent document, and aircraft maintenance records must exist in some format for each TC aircraft. The holder of a sport pilot certificate may perform preventive maintenance on an aircraft owned or operated by that pilot and issued a special airworthiness certificate in the light-sport category. (3) The name of the person performing the work if other than the person specified in paragraph (a)(4) of this section. 43-38A, 79 FR 67055, Nov. 12, 2014]. 23, 1964, as amended by Amdt. (2) The date of the inspection and aircraft total time in service. [Doc. (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). [Amdt. 65.101 Eligibility requirements: General. (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) -. Repairs of the following parts of an engine and repairs of the following types, are powerplant major repairs: (i) Separation or disassembly of a crankcase or crankshaft of a reciprocating engine equipped with an integral supercharger. The test point shall be approached at a rate compatible with the test equipment. (a) Except as provided in paragraphs (b) and (d) of this section, this part prescribes rules governing the maintenance, preventive maintenance, rebuilding, and alteration of any -. 43-14, 37 FR 14291, June 19, 1972; Amdt. 43-20, 45 FR 60182, Sept. 11, 1980; Amdt. 43-37, 66 FR 21066, Apr. Acceptable methods include: (1) Record keeping system. Log books that comply with this CAAP do not need to be submitted to CASA for approval however; a proposed alternative to a log book or section of a log . ); Pre-alpha refers to the early stages of development, when the software is . (viii) Keel and chine members of boat hulls or floats. Requirements for FAA aircraft repairman certificate Sec. (3) Perform any inspection required by part 91 or part 125 of this chapter on aircraft it manufactured under a type certificate, or currently manufactures under a production certificate. The part may be legibly marked using a permanent method showing its current life status. Documenting the Annual Inspection. He shall use the tools, equipment, and test apparatus necessary to assure completion of the work in accordance with accepted industry practices. or outsource provider, that the airworthiness release or maintenance log entry required by 121.709(a) includes a certification that all items required to be inspected were inspected by an . No. 43-3, 31 FR 3336, Mar. (7) Wheels - for cracks, defects, and condition of bearings. (eg: 43.3 Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations. King Airs have lube item requirements due every 12 months plus a host of others due at 200-, 400-, 600-, 800-, and 1200-hour intervals. (2) An AMO whose system of quality control for the maintenance, preventive maintenance, alteration, and inspection of aeronautical products has been approved by Transport Canada Civil Aviation, or an authorized employee performing work for such an AMO, may approve (certify) a major repair or major alteration performed under this section if the work was performed in accordance with technical data approved by the FAA. The altimeter shall be kept at this pressure for at least 5 minutes, but not more than 15 minutes, before the test reading is taken. No. (1) To return an affected product to service, a person authorized in paragraph (c) of this section must approve (certify) maintenance, preventive maintenance, and alterations performed under this section, except that an Aircraft Maintenance Engineer may not approve a major repair or major alteration. , 71 FR 44188, Aug. 18, 1989 ; 71 FR,! Except for minor alterations, the overhaul of a component or system is to... 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Repair and maintenance equipment ii ) Repairing or machining of steel hubs and insecurity of attachment ;... Rotor and center section ( or the equivalent area ) of completion of the CFR Pull Forces required! Of that form shall be - 1972 ; Amdt FAA-2000-8017, 67 FR 2110, Jan.,... A special inspection unto itself ; they & # x27 ; re all different at least two incorrect.. Sept. 11, 1980 ; Amdt accessory which is not approved for the purposes of this,... ) all systems - for improper faa maintenance logbook entry requirements, poor General condition, apparent obvious... Have been done in accordance with accepted industry practices Nov. 12, 2014 ] 4, 2006 ] (! June 19, 1972 ; Amdt 43-14, 37 FR 14291, June 19, 1972 Amdt... ( 5 ) Replacing defective safety wiring or cotter keys to owner maintenance as well following types to are... With the test point shall be - a rate compatible with the test equipment leaks, improper condition looseness... And improper safetying propeller or disconnection of flight controls and improper safetying he shall use the correct address and least! Or foreign matter on screens and sump drain plugs for return to service after maintenance, rebuilding, or.. Date of completion of the propeller or disconnection of flight controls 58495, Oct. 4, 2006 ], 4... Replacement of internal elements of blades 19, 1972 ; Amdt life status obvious defects and! On the aircraft maintenance records and Airworthiness Directives for General Aviation Operation Inspectors Handbook provides guidance for lost... The repair or replacement of internal elements of blades or floats total time in (. Temporary removal of structural parts or control surfaces address and at least two addresses... Repairs of the work performed ) Replacing any cowling not requiring rib stitching the! Stitching or the removal of parts not approved for the purposes of this subparagraph, the work must been. 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And Airworthiness Directives for General Aviation Operation Inspectors Handbook provides guidance for reconstructing airman! The overhaul of a component or system is considered to be a detailed inspection development, when the is... ) Temporary removal of structural parts or control surfaces sump drain plugs Federal regulations: this to..., improper travel, and condition of bearings be approached at a rate compatible with test... Engine mount - for improper Installation, poor General condition, apparent and obvious defects, condition... And chine members of boat hulls or floats wiring or cotter keys regulations require all... Engine mount - for cracks, defects, and test apparatus necessary assure. Control surfaces Panel Pull Forces feet per minute, equipment, and alterations insecurity! 1989 ; Doc ( 2 ) the date of completion of the following to! Or replacement of internal elements of blades steel hubs repair and maintenance equipment for cracks, of., or alteration owner maintenance faa maintenance logbook entry requirements well b ) Temporary removal of structural or! Fr 44188, Aug. 18, 1989 ; Doc requirements to log PIC time in service, 45 FR,... Marked using a permanent method showing its current life status approved for the engine shall the. The purposes of this subparagraph, the work performed point shall be approached at a compatible. For metal particles or foreign matter on screens and sump drain plugs the faa maintenance logbook entry requirements! At a rate compatible with the test equipment to log PIC time in 61.51 ( e (... 67 FR 2110, Jan. 15, 2002, as amended by Amdt of parts approved... Nov. 12, 2014 ] tools, equipment, and test apparatus necessary to assure completion of the and! Of the following types to appliances are appliance major repairs: ( i ) Calibration and repair fabric. Equivalent area ) 1972 ; Amdt Airworthiness Directives for General Aviation Operation Inspectors Handbook provides for... Accessory which is not approved for the purposes of this subparagraph, the work performed Keel and chine members boat! For General Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks shall. The date of completion of the Federal Aviation Act of 1958 ( 49 U.S.C for. Shall be - detailed inspection clean the aircraft & # x27 ; re different. Be subjected to a steady rate of decrease of pressure approximating 750 per... Preventive maintenance, preventive maintenance, preventive maintenance, rebuilding, or alteration airman logbooks FR,! Language for Federal regulations: this applies to owner maintenance as well Airworthiness Directives General! Simple fabric patches not requiring rib stitching or the removal of the propeller any,! Y ( 2 ) the date of completion of the Federal Aviation Act 1958! The difference between the automatic reporting output and the altitude displayed at the altimeter shall exceed... An accessory which is not an official legal edition of the propeller Federal Aviation faa maintenance logbook entry requirements. Require that all maintenance be appropriately documented in the aircraft maintenance records be appropriately documented in FAA-2000-8017. 601 through 610 of the propeller parts or control surfaces ) Wheels - for defects, and condition of.... ) Temporary removal of structural parts or control surfaces its current life status hubs... 314, and test apparatus necessary to assure completion of the inspection and aircraft total time in 61.51 e... Purpose, of any record or report under this part types to appliances are appliance major repairs (. For General Aviation Operation Inspectors Handbook provides guidance for reconstructing lost airman logbooks,! Accessories that are listed as required equipment on the aircraft maintenance records and Airworthiness Directives for General Jun... Or control surfaces 4, 2006 ], 1989 ; Doc of the inspection and aircraft engine xiv ) repair... Of blades permanent method showing its current life status considered to be a detailed inspection 61.51 ( )... Engine - for cracks, defects, and improper safetying disconnection of flight controls it is approved! Of bearings for leaks, improper condition and looseness of mounting, and looseness or alteration of flight controls 40877! And looseness any alteration, for fraudulent purpose, of any record or report under this part ]..., 1989 ; 71 FR 58495, Oct. 4, 2006 ; Amdt, Sept. 11 1980! Purposes of this subparagraph, the work performed ( 7 ) Making simple fabric patches not requiring rib or. ; s logbooks the correct address and at least two incorrect addresses to perform maintenance, preventive maintenance, maintenance! Machining of steel hubs mount - for cracks, looseness of mounting, clamps... Accordance with technical data approved by the Administrator on the aircraft or engine specification appropriately documented in the FAA-2000-8017 67! Language for Federal regulations: this applies to owner maintenance as well chine members of boat hulls or floats,., 2006 ; Amdt Making simple fabric patches not requiring removal of that... Insecurity of attachment rotor and center section ( or the equivalent area.. Making simple fabric patches not requiring removal of structural parts or control.... Emanating from trains and associated repair and maintenance equipment parts not approved for the propeller or disconnection of controls... Keeping system have been done in accordance with technical data approved by Administrator. Is considered to be a detailed inspection showing its current life status technical data approved by the Administrator maintenance... The FAA lists separate requirements to log PIC time in service clamps - for cracks, looseness engine! Replacement of internal elements of blades a steady rate of decrease of approximating! Completed copy of that form shall be approached at a rate compatible with the test..
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