Ad 98-02-08 applicability
WebLycoming AEIO-360, HIO-360, IO-360 and LIO-360 Series Engines . Issued 17 December 2024 Page 3 of 31 CAA of NZ . DCA/LYC/109A FAA AD 64-16-05 Fuel and Oil Vent Restriction – Modification Webrecurring AD 70-16-05 due to muffler applicability. Complied with AD 98-02-08, No pitting found in crankshaft. Next due 2026. Installed overhauled MA-CPA carburetor P/N-.10-5217, SIN: MSONFUOZ Drained engine Oil and serviced engine to proper level with Aeroshett 100. Operational, security, and leak checks performed at this time for the work with
Ad 98-02-08 applicability
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Web14 CFR Part 39 [63 FR 4154 NO. 18 01/28/98] [Docket No. 94-ANE-44; Amendment 39-10291; AD 98-02-08] RIN 2120-AA64 Airworthiness Directives; Certain Textron Lycoming … WebAD 98-02-08. PREVENT CRANKSHAFT FAILURE, WHICH CAN RESULT IN ENGINE FAILURE, PROPELLER SEPARATION, FORCED LANDING, AND POSSIBLE …
Web95-26-02 Textron Lycoming: Amendment 39-9460. Docket No. 95-ANE-67. Supersedes Priority . Letter AD 94-14-13, issued June 23, 1994. ... the applicability of this AD. Compliance: Required as indicated, unless accomplished previously. To prevent detonation due to low octane, which can result in severe engine damage and subsequent ... WebApr 9, 2024 · AD 98 02 08 which is where SB 505 originated starts out by saying,”O-320 engines limited to 160 HP” ... 98-02-08 Textron Lycoming: Amendment 39-10291. Docket 94-ANE-44. Applicability: Textron Lycoming 320 series limited to 160 horsepower, and 360 series, four cylinder reciprocating engines with fixed pitch propellers.
WebOct 18, 2024 · Airworthiness Directives ( AD s) are legally enforceable regulations issued by the FAA in accordance with 14 CFR part 39 to correct an unsafe condition in a product. …
WebUS-98-02-08: Issued by: United States of America: Issue date: 1998-01-28: Effective date: 1998-03-30: EASA approval number: Contributor: Federal Aviation Administration (FAA) …
WebFeb 1, 2004 · Applicability: 90, 200, and 300 series airplanes (all serial numbers) certificated in any category. Compliance: Required within the next 100 hours time-in-service after the effective date of this... i am the strongest lord in another world scanWebNov 25, 2024 · AD Requirements This AD requires inspecting the right aileron flight control cable end fittings that thread into the turnbuckle for corrosion, pitting, and cracks and replacing any damaged cable assembly. FAA's Justification and Determination of … i am the strongest lordWebMy IA is going though the logs my new to me Super Cub and it looks like in the past someone has stated that AD 98-02-08 applies. This is for the inspection of the interior … iamthestylemarshallWebNote 3: FAA Airworthiness Directive 98 -02 -08 amendment 39 -10291 refers. Compliance: Requirement 1: Engines with a time in service (TIS) since new, remanufacture or … i am the stripclub lyricsWebAug 8, 2007 · 2006-26075; Directorate Identifier 2006-CE-55-AD. Effective Date (a) This AD becomes effective on May 25, 2007. Affected ADs (b) This AD supersedes AD 72-22-01, Amendment 39-1544. Applicability (c) This AD applies to the following airplane models and serial numbers (SNs) that are certificated in any category: i am the strongest in japaneseWebActions specified by the AD are intended to continue to prevent structural failure of the V-tail, which could result in loss of control of the airplane. AD 2002-21-13: Supersedes AD 98 … mommy speech k wordsWeb(FAA AD 79-08-02 refers) Compliance: Part I - within next 10 hours TIS unless already accomplished . Part II - within next 100 hours TIS . Effective Date: DCA/PA38/6 - 9 January 1978 DCA/PA38/6A - 18 May 1979 . Note: Requirement notified to registered owners on effective date . DCA/PA38/7A Engine Mount - Inspection and Modification . Applicability: i am the student