LYCOIIIIIIIIG

If multi-engine: 0 Left 0 Right 0 Front 0 Rear TACH OR RECORDING METER TIME AT COMPLIANCE METHOD OF COMPLIANCE IS. J Amendment 39-15005. Docket No. FAA-2006-25948; Directorate Identifier 2006-NE-32-AD. Effective Date (a) This airworthiness directive (AD) becomes effective May 7, 2007. Affected ADs (b) This AD revises AD 2007-04-19. Applicability . (c) This AD applies to Superior Air Parts, Inc. (SAP), cylinder assemblies, manufactured between April 2005 and November 2005, part numbers (PINs): SA47000L-AI, SA47000L· A20P, SA47000S·AI, SA47000S- A20P, SA47000S-A2IP, SA52000-AI, SA52000-A20P, SA52000-A2IP, SA52000-A22P, SA52000-A23P, SA55000-AI, and.SA55000-A20P, installed in Teledyne Continental Motors (TCM) 470, 520, and 550 series reciprocating engines. These PIN cylinder assemblies may be installed in the TCM engine models listed in the following Table I. o Table I.-Affected Teledvne Continental Eneine Models Eneine-Model 0-470 -G ·K,·L .M, -P, -R -S ·U 10-470 -C -D -E ·F -G -R, -L.·M,·N -P -R -S ·U.·V 10-520 -A B BA,C CB D E F J K,L,M,BB MB TSIO-520 - AF. B. BB. C, CE, D. DB. E. EB. G. H. J. ]B, K, KB, L, LB. M, NJ NB, p.R TUB VB WB _.!2:.55O ·A.B.C.D E.F L These engine models are installed in, but not limited to. the aircraft models listed in the followin Table 2: Aerotecb Note: Table 2 has been moved to page 2to facilitate compilation of/his adNotem. This AD also applies to SAP. cast cylinder assemblies, PINs SL32000W·AI, SL32000W· A20P, SL32000W·A2IP, SL32000WH-AI, SL32000WH· A20P, SL32006W·Al, SL32006W· A20P, SL32006W-A2IP, SL36000TW·AI. SL36000TW·A20P, SL36000TW·A2IP, SL36000TW-A22P, SL36000W-AI, SL36000W·A20P, SL36000W-A2IP. SL36006W-AI, SL36006W·A20P, and SL36006W-A2IP, installed in Lycoming Engines (LE)'320, 360, and 540 C 2007 AeroTech Publications, Inc.. Ah rights reserved series reciprocating engines and Avco Lycoming 540 series reciprocating engines. These PIN cylinder assemblies may be installed in the LE and AL engine models listed in the following Table 3. Table 3.-Affected Lveominz Eneines and Aveo Lvcomlnz Eneine Models Eneine Model 0·320 -A, -B -C -D -E H 10·320 ·B ·D,-E LIO-320 ·B AlO·320 -A, ·B.-C AEIO-320 -D.·E 0-360 ·A -B -C ·D ·F ·G .J 10-360 -B·L ·M LQ-360 ·A AEIO-360 -B -H HO-360 -C HJO-360 ·B 0·540 -A, -B. -E -F -G ·H -J .. , 10-540 ·A,·C -D ·N ·T .y -W AEIO-540 ·D These engine models are installed m, but not limited to, the aircraft models Itsted in the followin Table 4; Aerotech Note: Table -I has been moved /0 pages 2. 3 &: -I /0 facilitate compilation of this adNotem. These engine models are known to be installed in the aircraft models listed in the following Table 5: Unsafe Condition (d) This AD results from comments from the Public on the existing AD. We are issuing this AD to prevent cylinder separation that can lead to engine failure. a possible engine compartment fire, and damage to the airplane. Compliance (e) You are responsible for having the actions required by this AD performed within the compliance times specified unless the actions have already been done. Determining Which Cylinder Assemblies Are Installed (f) If aircraft engine records do not list the PIN of the cylinder installed during engine overhaul or repair, visually inspect the cylinders. The affected SAP cylinder head barrel flanges are marked: SA47000L·AI, SA47000L-A20P, SA47000S·AI, SA47000S·A20P, SA47000S· A2IP, SA52000-AI, SA52000-A20P, SA52000-A2IP, SA52000-A22P, SA52000-A23P, SA55000-AI, or SA55000-A20P or SL32000W·AI, SL32000W· A20P, SL32000W·A2IP, SL32000WH·AI, SL32000WH·A20P, SL32006W·AI, SL32006W·A20P, SL32006W-A2IP, SL36000TW-AI, SL36000TW·A20P, SL36000TW·A2IP, SL36000TW·A22P, SL36000W·AI, SL36000W·A20P, SL36000W·A2IP, SL36006W.AI, SL36006W-A20P, or SL36006W·A2IP. Cylinder Assembly Removal (g) Remove all cylinder assemblies with a serial number of 47LE053559 through 47LF053643, or 47SE054212 through 47SF05425I; or 52D0531708 through 52H0532197, or 55E05223 through 55G05289, or 32WE059006 through 32WF059067, or 32WHE05379 through 32WHE05392, or 326WF0555 I7 through 326WF055532, or 36TWF05430 through 36TWG05453, or 36WF058058 through 36WG058124, or 366WE056944 through 366WF057061, or 366WF057150 through 366WF057232, or 366WF057259 through 366WG057534, or 366WG057556, 366WG057569, 366WG057598, 366WG057616, 366WG057621, 366WG057624, or 366WJ057770 through 366WJ057776, or 366WL058131 no later than 150 hours total time-in- service (TIS) to preclude cylinder head fatigue failure and separation at the head-to-barrel threaded interface. (h) For cylinder assemblies with more than 150 hours total TIS on the effective date of this AD, a 10 hour TIS extension is permitted for the purpose of flying the aircraft to a location where maintenance action can be done to meet the requirements of this AD. (i) After the effective date of this AD, do not install any cylinder assemblies with PINs SA47000L·AI. SA47000L·A20P, SA47000S- AI, SA47000S-A20P, SA47000S-A2IP, SAS2000-AI, SA52000-A20P, SA52000- A2IP, SA52000-A22P, SA52000-A23P, SA55000- AI, or SA55000-A20P,or SL32000W·AI, SL32000W·A20P, SL32000W·A2IP, SL32000WH· AI, SL32000WH· A20P, SL32006W·AI, SL32006W·A20P, SL32006W.A2IP, SL36000TW· AI, SL36000TW·A20P, SL36000TW·A2IP, SL36000TW·A22P, SL36000W·AI, SL36000W· A20P, SL36000W-A2IP, SL36006W·AI, SL36006W·A20P, or SL36006W·A2IP with. serial number of 47LE053559 through 47LF053643, or 47SE054212 through 47SF05425I, or 520053 I 708 through 52H0532197, or 55E05223 through 55G05289, or 32WE059006 through 32WF059067, or· 32WHE05379 through 32WHE05392, or 326WF055517 through 326WF055532, or 36TWF05430 through 36TWG05453, or 36WF058058 through 36WG058 I 24, or 366WE056944 through 366WF057061, or 366WF057150 through 366WF057232, or 366WF057259 through 366WG057534, or 39(jWG057556, 366WG057569, 366WG057598, 366WG057616, 366WG057621, 366WG057624, or 366WJ057770 through 366WJ057776, or 366WL05813 I into any engine, Alter.ative Methods of Compliaaee (j) The Manager, Special Certification Office. FAA, Rotorcraft Directorate, has the authority to approve alternative methods of compliance for this AD if requested using the procedures found in 14 CFR 39.19. Special Flight Permits (k) For aircraft with engines that have between 140 hours and 150 hours TIS only, special flight permits may be issued in accordance with Sec. Sec. 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the aircraft to a location where the requirements of this AD can be done. Special flight permits may not be issued for aircraft that have utilized the provisions of paragraph (h) of this AD. Related Information (I) Superior Air Parts, Inc. Mandatory Service Bulletin B06-01, Rev. E, dated January 24, 2007, contains information related to the subject of this AD. (m) Contact Jurgen Priester, Aerospace Engineer, Special Certification Office, FAA, Rotorcraft Directorate, Southwest Regional Headquarters, 2601 Meacham Blvd., Fort Worth, Texas 76137; e-mail: Jurgen.E.Priester@faa.gov; telephone (817) 222-5159; fax (81 7) 222·5785 for more information about this AD. Material Incorporated by Reference (n)None. Issued in Burlington, Massachusetts, on March 23,2007. Peter A. White, Acting Manager, Engine and Propeller Directorate, Aircraft Certification Service. (Over)+ ) a-J20-ElF M.B.B. Wassmer Pacific WA·S 1 0-J20-EZG Gulfstream AA5 Traveler 0-32()"'E2G Gulfstream AASA Cheetah O-32O-EJO Beechcraft BI9 Snort 0-320-EJD Pi1"ll'l'"Aircraft Cherokee 140 O-J20-H2AD Cessn, Sl'Yhawk 172 N O-32O-HlAO Parten.vi. f-66C O-J20A2C VarD', Kachina 2150 IO-32()"B2A Piner Aircraft Twin Comanche {PA-lO IO-lZO-BIC Hi 10032O-BIC Shear 10032O-BIC Win.!!! 10-32O-BI0 Ted Smith Aircraft Aerostar IO-320-DlA M.B.B. Monsun mO-209-C JO-nO-OIB M.B.B. Monsun BO-209-C rO-J20-EIA Chameioe KCAB lO-32O-EIA M.B.B. MonSUR 80-Z09-C 10-32O-EIB Bellanca Aircraft IO-J20-E2A Cham ion 7KCAB 10-32O-E2A Cham ioo Airaaft Citama :{)..32O-E28 Bellanca Aircraft 101L10-320- Piper Aircraft PAolO Comanche (2) BIA 101L10-32<>- Piper Aircraft Twin Comanche (PA-39) BIA AI0-320-BI B M.B.B. Moosun (B0-209-C AEI0-J20-0IB Slinllsbv T67MFirefl AEI0-320-02B Hindustan Aeronautics Ltd. HT-2 AEIO-12()..EIA Bellanca Aircraft AEIO-1ZO-E1A Cham ion Aircraft AEI0-320-EIB Bellanca Aircnft AEIO-J20-EIB Cham ion Aircraft -- Oecathalon 8KCAB-CS AEI0-320-E2B Bellanca Aircraft AEI0-320-E2B Cham ion Aircraft Dec:athalon 8KCAB 0-320-AIA Ril~Aircraft Rilev Twin 0-360·AIA Beechcraft Travel Air 9S. B~9S O~36(}.AIA Piner Aircraft Comanche (P A~24 0-360-AIA Intermountain MrR. Co. Call Air A-6 0-360-AIA Lake Aircraft Colonial C~2. LA •.•••4A or 4P 0-36O-AIA Doyn Aircraft Doyn-Cessna (170B, 172, 172A, I72B O-360-AIA MOOONAircraft Mark '"2OB" (M-lOB O-360-AIA Earl Horton Pawnee (Piper PA~2S 0-3';(l-AIA Oinfia Ranauel IA~SI O-J60..AlA NtI•• PD~S901 0-360-AIA Reeente IN-591 . 0-360-AIA Wassm er Su •••. 4 CWA-SOA O-360-AIA Wassm er Sancv I A-40 0-360-AIA Wassm ••. Baladou WA-40 O-360-AIA Wassm ••. Pariou A-4() 0-360-AIA Sud Gardan GY-ISO O·360-AIA Bclkow 207 0-360-AIA Partenavia Oscar (P-66 0-36(}.AIA Siai-Marchetti S-205 0-360-AlA Proca ••. Picchic ~15~A 0-360-AIA S.A.A.B. Safir 91-0 O-360-AIA Malmo vioan (M -lOB 0-360-AIA Aern Bocro AB-ISO 0-360-AIA Bea le Airedale A-I09 0-360-AIA DeHaviUand Drover ([ HA-3MKJ 0-360-AIA Kin.,srord-Smith Bushmaster JS-6 O-J60...AIA Aero En ine Service Ltd. Vieta (R·2) O-360-AIAD S.O.CAT.A. Tabaeo TB-IO O-360-AIO Pi......,. Aircraft Ccmanche rPA-24 O-360-AIO Lake Aircraft Coioniall1.A •.•••4A ~ 4P O-360-AIO Doom Aircraft Dovn-Beed11l1ccch 951 0-360-A10 Moonev Aircraft Mast er 21 CM-20E O-360-AIO Moon- Aircraft Mark 20B, 200, tM20B M20C 0-360-AI0 Mooeev Aircraft Moonev Statesman /M-2OG 0-360-A10 Oinfia Ouerandi IA""S O-J60.AID Wassmer fWA-SO 0-360-AI0 Malmo Vi an lMFI-IO 0-360-AID "Cessna Aircraft Skvhawk 0-360-AI0 Dovn Aircraft Dovn-Pioer PA-2J~I60 0-360-AIF6 Cessna Aircraft Cardinal 0-360-AIF60 Cessna Aircraft Cardinal 117 0-360-AIF60 Teal III TSC lA3 0-360-AIG6 Aero Commander 0-360-AIG60 Beech Aircraft Duchess 76 0-36O-AIH6 Piner Aircraft Seminole /'PAM O-360-AI LO W"""", Eurooa WA-S2 O-360-AIP Aviat 0-360-AIP Hu<h 0-360-A2A COller Est Aeronautiaue Reeeate R-253 0-360-A2A S.O.C.A.T.A. Rallve Commodore (Ms.89J 0-360-A2A Societe Aeronautique Mousquetaire CD- 140) Normande 0-360-A2A BoIkow Klemm n<.1 ·1 07C 0-360-A2A Partenavia OscarCP.(,6 0-360-A2A Beaele Husley ([ 5-ISO JI-I/\ O-J60-A20 Pint:rAircraft Comanche PA-24 0-360-A20 Pioer Aircraft Cherokee C PA-28-ISO 0-360-A2D Moonev Aircraft Master 21 (M-20D 0-36O-A20 Moonev Aircraft Mark 21 (M-1OE 0-360-A2E Std. Helicooter 0-360-A2F Aero Commander Lark 100 O~360-A2F Cessna AirQ"aft Cardinal 0-360-A2G Beech Aircraft SDOr1 0-360-AJA C.A.A.R.P.S.A.N. tM-23 I II O-360-AJA Societe Acronautiquc !odel (D-I4OC) Normande 0-360-A3A Robin Reeent a: R4OOIISO 0-360-A3A Robin Remcecueur ([ R400/1SOR 0-360-A3A Robin R-3170 0-360-A3A S.O.C.A.T.A. Rallvc 1800T 0-360-A3A S.O.C.A.T.A. Soortavia Soonsman fRS-ISO 0-360-A3A Norman Aeroseace Co. NAC-I Freelance 0-360-A3A NlSh Airc;raft Ltd. P ••.• 0-360-AJAD S.O.C.A.TA. TB-IO 0-360-A3AO Robin Ai Ion fR-1 ISO 0-360-A4A Pi •••••.Aircraft Cherokee "D" PA-28-180 0-360-A4D Var"a Kaehina 0-360-A4G Beech Aircraft Musketeer Custom III 0-360-A4K Grumman American Tiller 0-360-A4K Beech Aircraft Sundowncr ISO I, ) ~ 0-J60-A4M 172 (Onticmi Suocr Cub Conversion O-J60..A4M Piner Aircraft Valmet Archer II PA-18-18 PIK-2J 0-360-A4N O-J60-A4P Cessna Aircraft Penn Van Call Air A.6 O-J60..ASAD 0-360-B2C C. hoh and Co. Seabird Aviation Fu'i FA-loo SB7L Scout SGCBC-CS Star Rocket MX-7-180 O-36O-CIA Intermountain Mrll. Co. Huskv A-I O-36O-CIE O-36O-CIF Bellanca Aircraft Maule O-J6O-CIG Christen YHO-1HU Militarv 0-36O-C2B 0-36O-C20 Hu hes Tool Co. Hu hes Tool Co. t269A 269A Scout SGCBC FP 0-360-C2E Hu hes Tool Co. MX-7-ISOA SUDer Cub Conversion 0-J60-C2E Bellanca Aircraft 0-J60-C4F 0-J60-C4P Maule Penn Van Cutla5.!iRG R22 Travel-Air fB·9SA 0-360-FIA6 0-360-12A 10-J60-BIA Cessna Aircraft Robinson Beech Aircraft Travel-Air (B-9SB Dovn-Pioer PA-23·200 100J60-BIA Dovn Aircraft fA-200 10-J60-BIB 10-360-BIB Beech Aircraft I'Jnvn Aircraft See-Bee Arrow PA-28-180R 10-360-BIB 100360-B10 100360-BIE Fu'i United Consultants Pinr1' Aircraft 75 C.A.P. 10 Trainer 10-360-BIF 10-360-B2E 10-360-BIF6 Utva C.A.A.R.P. Great Lakes Soector 42 Trainer Duchess 10-360-BIG6 10-J60-B2F6 LO-360-A I G60 American Btime Great Lakes Beech Aircraft Slcyh.wk C-I72 OA-40 L0-36O-A IH6 10-J60-EIA Pint";!' Aircraft T.R Smith Aircraft Seminole CPA•.••4 Aerostar RV6, RV7, RVS 360 10-J60-L2A 10-360-MIA 10-J60-MIB 10-360-MIB Cessna Aircraft Diamond Aircraft Vans Aircraft lancair CAP-IO 5-IS AIO-360-BIB AE10-360-B I G6 Moravan Great Lakes Zim Z-S26-l SUDCl"Decathalon 8KCAB~I80 Suoer Decathalon AEI0-360-B2F AEI0-360-B4A AEI0-360-H1A AEI0-360-H1B Mundrv Pitts Bellanca Aircraft American Chamnion 269A 269A 300c HO-360-BIA H0-360-BIB H0-36O-CIA Hue:hcs Tool Co. Haehes Tool Co. Schweizer Militarv 169-A-l 1fl00360-AIA HIO-J60-AIB H10-J60-BIA Huebes Tool Co. Silven;raft Huehes Tool Co. 300 269A 269C, JOOC 300c H10-360-BIB H10-360-01A 1II0-360-0IA Huebes Tool Co. Hue:hes Tool. Co. Schweizer F2SC F2SC 1II00J60-E I AD 1II0-J60-EIBO Enstrom Helicooter Enstrom Helicooter Sentine F28F-P CB 1II0-J60-FIAO 1II0-J60-FIAD Enstrom Hellccorer Enstrom Helicooter Faicon F28F Shark 2SOFX SH-4 Heticccter SH-J Helicooter H1O-J60-FIAD 1II0-J60-GIA LIII0-360-CIA L1II0-360-C I B Enstrom Heliccorer Schweizer Silvcrcraft Silvcrcraft RF-I Comanche PA·24-150 Militarv H-2SO O-S40-AIA 0-S40-AIA5 0-S40-AIA5 Rhein-FIUllU:Ullbau Piocr Aircraft Helio YA-I Aztec PA-23-2SO 0-S40-AIA5 0-S40-AIB5 Yoeman Aviation Piocr Aircraft Comanche PA-24-250 Comanche PA-24-250 0-S40-AIB5 0-S40-AIC5 Pioc:rAircraft Pitll'!'Aircraft FBA-2C 00-2S-BI Aztec PA-1J -150 O-S40-AIO O-S40-AIO 0-540-A105 Found Bros. I>ornier Pioer Aircraft Comanche PA-24-250 Military Aztec U-I IA 0-540-AI05 O-S40-AIDS Pieer Aircraft Pioer Aircraft Twin Courier 11-500, U-S Navy Aztec PA-13-150 0-54()-AI05 0-540-A2B Domier Aero Commander 00-28 SOO ADachc PA~23-1JS Cherokee PA-24-250 Dovn-Pioc:r PA-14-1SO 0-S40-A2B 0-S40-AJD5 0-54()-BIA5 O-S4O-BIB5 0-540-BIB5 Mid-States Mfll. Co. Piner Aircraft. Piper Aircraft piner Aircraft Dovn Aircraft WA •.••1I Pawnee PA-14-23S 0-S40-BI05 0-S40-B2B5 Wassmer Piner Aircraft Cherokee PA-28-13S Aztec PA-23-1JS 0-S40-B2B5 O-S4O-B2B5 Pinf'r Aircraft PiDerAircraft 0-S40-B2B5 0-S40-B2B5 0-S4O-B2B5 Intermountain Mf . Co. Rawdon Bros. S.O.C.A. T.A. Call Air A-9 Rawdon T-I Rallv.2)sCA Carioca EMB-7l0 Rally.2J5GT 0-S40-B2C5 0-54{)..B4BS Piocr Aircraft Pieer Aircraft PawneePA-24-2JS Cherokee PA-18-23S 0-S40-B48S 0-54()-84B5 Embraer S.O.C.A.T.A. Rail e2JSC Star Racket MX-7-23S 0-54()-B4B5 0-S40-B48S S.O.C.A.T.A. Maule Super Rocket M-6-23S Sueer Std. Racket M-7-2JS Comanche PA-2~-260 0~S40-B4BS 0-540-84B5 O-S40-E4AS Maule Maule Piner Aircraft Flamingo F-1SO SF-260 SF-208 BN-l O-S40-E4AS 0-S40-E4AS O-S4Q-E4BS Aviamilano Siai-Marcbctti Britten-Norman Islander BN-2A-26 Islander BN-1A-27 0-S40-E4C5 0-S40-E4C5 Piner Aircraft Pilatus Brinen-Norman Pilatus Brinen-Norman Cherokee Six PA~31-260 Islander II BN-2B-26 Islander BN-1A-2 I Trislander BN-2A-Mark 111·2 0-S40-E4C5 Q-54{)..E4CS 0-S40-E4CS Pilatus Britten-Norman Pilatus Britten-Norman Pilatus BriUen-Norman 0-S40-FIB5 0-S40-FIB5 0-540-GIA5 BS-I201 R-44 Pawnee PA-2S-260 Omega Aircraft Robinson Piocr Aircraft O-S40-HIBSD O-S40-HZAS O-S40-HZAS 0-540-HlB50 Aero Baero Embracr Gtnosland Aero Bocro 260 Imoanema "AG" GA-200 260 0-S40-J1ASD 0-540-JlA5O Maule Maule Star Rocket MX-7-23S Super Racket M-6-2JS O~S40-JIASD 0-S40-JJA5 3 Maule Robin SUDer Std. Rocket M-7-2JS R-JOOOI235 Ballistic Recovery Systems TOTAL TIME AT COMPLIANCE METHOD OF COMPLIANCE AUTHORIZED SIGNATURE & NUMBER COMPLIANCE DATE C 2008 AeroTech Publications. Inc., All rights reserved Amendment 39-15348; Docket No. FAA-2007-29317; Directorate Identifier 2007-CE-079-AD. Effective Date (a) This AD becomes effective on February 28, 2008. Affected ADs (b) None. Applicability (c) This AD applies to the foliowing airplane models, all serial numbers, certificated in any category, that are equipped with: (1) BRS-172 Parachute System instalied via Supplemental Type Certificate (STC) No. SA01679CH, or (2) BRS-182 Parachute System installed via STC No. SA01999CH. CIssna 172 Modols CIssna 182 Modlls 172 182G 172A 182H 1728 182J 172C 182K 1720 182L '. 172E 182M 172F USAF T-41A) 182N 172G 182P - 172H USAF T-41A 1820 1721 182R 172K 182S 172L 182T 172M T182 172N T182T 172P 1720 172R 172S R172J R172K. Unsafe Condition (d) This AD results from notification by Ballistic Recovery Systems, IRC. (BRS) that the pick-up collar assembly- may prematurely move off the launch tube and adversely affect rocket trajectory during deployment. We are issuing this AD to prevent premature separation of the collar. This condition could result in the parachute failing to successfully deploy. Compliance (e) To address this problem, you must do the following, unless already done: Actions Compliance Procedures Remove and replace the pick-up collar support and Within the next 25 hours time-in-service after February (i) For Cessna 172 series airplanes follow BRS SB 07- two retaining screws. 28, 2008 (the effective date of this AD). 01, dated June 8, 2007. (ii) For Cessna182seriesairplanes,follow BRSSB 07-02, datedJune8, 2007. •• Alternative Methods of Compliance (AMOCs) (f) The Manager, Chicago Aircraft Certification Office, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATIN: Gregory Michalik, Senior Aerospace Engineer, FAA, 2300 East Devon Avenue, Des Plaines, Illinois, 60018; telephone: (847) 294-7135; fax: (847) 294-7834; e-mail: gregory.michalik@faa.gov. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. Material Incorporated by Reference (g) You must use Ballistic Recovery Systems, Inc. Service Bulletin No. 07-01, dated June 8, 2007, for Cessna 172 series airplanes; or Ballistic Recovery Systems, Inc. Service Bulletin No. 07-02, dated June 8, 2007, for Cessna 182 series airplanes; to do the actions required by this AD, unless the AD specifies otherwise. (1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact Ballistic Recovery Systems, Inc., 300 Airport Road, South Saint Paul, MN 55075- 3551; telephone: (651) 457-7491; fax: (651) 457-8651. (3) You may review copies at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Kansas City, Missouri 64106; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202- 741-6030, or go to: http://www.archives.gov/federal register/code of federal regulationslibr I ocations.html. Issued in Kansas City, Missouri, on January 16, 2008. James E. Jackson, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. () () Precision Airmotive Fuel Injectors If multi-engine: Engine Model:.:ro~ 3(00 ~LLA Serial No: L - 34/ {P(P - 51~ DATE, TACH, OR RECORDING METER TIME DATE METHOD OF COMPLIANCE TOTAL TIME AUTHORIZED SIGNATURE & NUMBER Amendment 39-15466, Docket No. FAA-2008-0420; Directorate Identifier 20 AD, Effective Date (a) This airworthiness directive (AD) becomes effective April 29, 008, to persons except those persons to whom it was made immediately emergency AD 2008-06-51, issued March 12, 2008, which contained the re of this amendment. Affected ADs (b) This AD supersedes AD 2008..06-51, Applicability (c) This AD applies to the following reciprocating engines with an in e Precision Ainmotive llC, RSA-5 or RSA-l0 series fuel injection servo, having a se plug gasket, part number (PIN) 365533, installed under the fuel injection servo plug, PI 383493: (1) lycoming Engines 10, (l)IO, TIO, (l)TIO, AEIO, AIO, IGO, IVO, and HIO series reciprocating engines, regardless of displacement, either new, rebuilt, overhauled, or repaired since August 22, 2006, andlor with an affected fuel injection servo installed either new, rebuilt, overhauled, or repaired since August 22, 2006, (2) Teledyne Continental Motors TSI0-360-RB reciprocating engines, either new, rebuilt, overhauled, or repaired since August 22, 2006, and/or with an affected fuel injection servo installed either new, rebuilt, overhauled, or repaired since August 22, 2006. (3) Superior Air Rarts, Inc. 10-360 series reciprocating engines, either new, rebuilt, overhauled, or repaired since August 22, 2006, and/or with an affected fuel injection servo installed either new, rebuilt, overhauled, or repaired since August 22, 2006. (4) This AD also applies to any other Precision Airmotive llC fuel injection servos received since August 22, 2006, or any fuel injection servos that have had the fuel injection servo plug, PIN 383493, removed during maintenance since August 22, 2006 .. Unsafe Condition (d) This AD results from eighteen reports of fuel injection servo plugs, PIN 383493, that had loosened or completely backed out of the threaded plug hole on the regulator cover of the fuel injection servo. We are issuing this AD to prevent a lean running engine, which could result in a substantial loss of engine power and subsequent loss of control of the airplane. Compliance (e) You are responsible for having the actions required by this AD perfonmed before further flight, unless the actions have already been done. The actions required by this AD must be done by an FAA-licensed mechanic. Initial Inspection (I) Inspect the fuel injection servo plug, PIN 383493, for looseness, by attempting to turn it by hand, while being careful not to damage the safety wire or seal. If the plug moves, it is loose. (g) If the plug Is not loose, go to paragraph (i) of this AD. (h) If the plug is toose, do the following: (1) Carefully cut and remove the safety wire that spans betWeen the servo plug and regutator cover onty. (2) Remove the servo plug while ensuring that the gaSket, PIN 365533, that is behind the plug, is not lost. The gasket may be slighUy stuck to the regUlator cover. Alternate Static Source Valve COMPLIANCE TOTAL TIME AT TACH OR DATE COMPLIANCE RECORDING METHOD OF COMPLIANCE AUTHORIZED SIGNATURE & NUMBER METER TIME --" -- .>:7 AT COMPLIANCE -- J 1,/drl 15', I 15./ ",IA ~y c fA! ~~~L ~ ...•.. -, / ~ ~.P..r'1 " , , , / " (.;'" Amendment 39-15508; Docket No. FAA-2008-0471; Directorate Identifier 2008-CE-025-AD. Effective Date (a) This AD becomes effective on May 12, 2008. Affected ADs (b) None. Applicability (c) This AD applies to airplanes listed in Table 1 and Table 2 of this AD that: (1) Have a part number (PIN) 2013142-18 alternate static air source selector valve installed after November 19, 2007; and (2) Are certificated in any category: ~) / Table 1.-Applicability for Airplanes That Had the Affected Part Installed at Manufacture Model Serial Nos. (SINs) 172S 172510672 through 172S10674, 172S10676, 172S10678 through 172S10680, 172S10682, 172S10683, and 172S10685. 182T 18282062 and 18282065. C 2008 AeroTech Pubhcations,loc., All nghts reserved T182T T18208822 and T18208828. I 208 20800417,20800418, and 20800419. I 208B 208B1294 throuah 208B1310. I . Note 1: Airplanes listed in Table-t may have also had the affected part installed as a replacement part. ~A'Y""/.I"/""/"'A'Y""'/"'''''''''/IYI'/.''/''''/''''/''''''''/IY .•••'/.,./I'/'/''''7.'.4M'AIY'/AI'7'/'''''''WX''''/1/ .••.ZIYIYA'?••X•••./..••./I/'Y ••../..•.1 IAerotech Note: Table 2 that was in this position in the Original FAA I Iversion of this Airworthiness Directive, has been moved to the bottom I ~of page 2 to facilitate compilation of this adNote TM. ~ 't'/.•./I/ .••./I/I/ ..••...•/lYI/I/IYIYI/I/l/I/l/I/ .••./IA••Yl/.•./I/I/.l/I/ ..••./IY.••./I/I/I/l/I/I/Ihtl/tr/I/,I/ .••./'/ •••/I,J Note 2: PIN 2013142-18 replaced PINs 2013142-9, -13, and -17. '.~ Unsafe Condition (d) This AD is the result of reports of improper installation of the part number identificatioa placard 'on the alternate static air source selector valve. We are issuing this AD to prevent erroneous indications from the altimeter, airspeed, and vertical speed indicators, which could cause the pilot to react to incorrect flight information 'and possibly result in loss of control. Compliance (e) For all affected airplanes, to address this problem, you must do the following, unless already done: Actions Compliance Procedures (1) Inspect the alternate static air source (i) For static air source selector valves installed (A) Adjust the pilot and copilot seats as far selector valve to assure that the part number before May 12, 2008 (The effective date of this aft as possible. identification placard is not obstructing the port. AD): Before further flight after May 12, 2008 (the (B) Use a flashlight and mirror to inspect the effective date of this AD), and alternate static air source selector valve to (ii) For static air source selector valves installed as assure the port on the forward end of the valve modification or replacement parts on or after May 12, is clearly visible and not covered by the part 2008 (the effective date of this AD): Before further number identification placard. flight after installation of a PIN 2013142-18 alternate static air source selector valve. Inspection of the part before, installation is acceptable. (2) If the alternate static air source selector Before further flight after any inspection required Make an entry in the aircraft records valve port is found obstructed by the part in paragraph (e)(1) of this AD where the port is showing compliance with this portion of the number identification placard during any found obstructed. AD following 14 CFR 43.9. inspection required by paragraph (e)(1) of this AD, remove the placard from the valve body, discard the placard, and assure that the port is open and unobstructed. u (f) Report the results of the inspection required by this AD where an obstruction was found to the FAA. (1) Submit this report within 10 days after the inspection or 10 days after the effective date of this AD, whichever occurs later. (2) Use the form in Figure 1 of this AD and submit it to FAA, Manufacturing Inspection District Office, Mid-Continent Airport, 1804 Airport Road, Room 101, Wichita, Kansas, 67209; or fax to (316) 946- 4189. (3) The Office of Management and Budget (OMB) approved the information collection requirements contained in this regulation under the provisions of the Paperwork Reduction Act of 1980 (44 U.S.C. 3501 et seq.) and assigned OMB Control Number 2120-0056. (Over for page 2)+ ECi Cylinders If If n L ft 0 R" hI 0 F I ORea EngineMOdel·.:x-O-~tOo -LlAserial No' L - .J><//(P(P-sIE mu r-enqrne: '-' e Ig ron r NEXT COMPL DUE AT TACH OR DATE. TACH. OR DATE TOTAL TIME RECORDING METHOD OF COMPLIANCE TOTAL RECORDING AUTHORIZED SIGNATURE & NUMBEEt AT COMPL. METER TIME TIME METER TIME .s--: ~ ATCOMPL. - I"J.•..LD "'/A A A/_'II1C ~ .••.. ~~ -;/ AdJ"1#.J.!f!I ~ l..ffi.5" 2.E9,S- NO t:.<.X ryy7 II ecs: -e: .-.. ~ , , -·("vt.iAlnlR. (' ~V(/"'~~ .::r~f" ::rN~~AUEn -- -'- ... R'/) 02008 AeroTech publications. Inc.. All nghts reserved Engine Components, Inc. (ECi): Amendment 39-15672. Docket No. FM-2008-0052; Directorate Identifier 2008-NE-01-AD. Effective Date (a) This airworthiness directive (AD) becomes effective October 20. 2008. Aff.cted ADs (b) None. Applicability (c) This AD applies to the Lycoming Engines (formerly Textron Lycoming) models 320. 360. and 540 series. "Parallel Valve". reciprocating engines listed in Table 1 of this AD. with ECi cylinder assembly. part number (PIN) AEL65102 series "Titan", and with cylinder head. PIN AEL85099. installed. (1) The applicable cylinder assembly serial numbers (SNs) are SN 1138-02 through SN 35171-22. (referred to in this AD as Group "A" cylinder assemblies); and (2) SN 35239-01 through SN 37016-28 (referred to in this AD as Group "B" cylinder assemblies). (3) Note that the cylinder assembly PIN is at the crankcase end of the cylinder assembly. and might be difficult to see. As a guide in determining if your cylinder assemblies are affected. all affected cylinder assemblies have cylinder head PIN AEL85099. The cylinder head PIN is at the top of the cylinder head. near the intake and exhaust valve springs. and is easier to locate than the cylinder assembly PIN. (4) Note that the set of numbers appearing on the cylinder. above and to the left of the SN. in the form of "123456" is not used for determining applicability. Table 1 Engine Models u --Cylinder Assembly Part Installed on Enoine Models: AEl65102-NSH3 0-3lO-J2A Number: O-S40-F1BS, JlA5D. JlBSD. JlCSD. JIDSD. J2A5D. J2BSD. J2CSD. J2DSD. AEl65102-NST04 0-320-AIB. A2B. A2C. A2D. AlA. A3B. B2B. B2C. B2D. B2E. B3B. B3C. HAS. HASD. HCSD C2B. C2C. C3B. C3C. DIA. DIAD. DIB. DIC. DID. DIF. D2A. D2B. IO-~O-ABIAS. WIAS, WIASD. W3ASD D2C. D2F. D2G. D2H. D2J. D3G. EIA. EIB. EIC. ElF. E1J. E2A. E2B. AEl65102-NST« O-Uo-L3C5D E2C. E2D. E2E. E2F. E2G. E2H. E3D. E3H AEl65102-NST07 10-320- BIA. BIB IO-J20-AIA, A2A. BIA. BIB. SIC. BID. 81E. B2A. D1A, DIAD, OIB. DIC. LlO~l20- B I A EIA. EIB. E2A. E2B AEl65102-NSTM 0-320-BIA. BIB. B2A. B2B. BlA. B3B. B3C. CIA. CIB. C2A. C2B. ClA. AEIO-320-DIB. D2B. EIA. EIB. E2A. E2B C3B. C3C. D1A, DIB D2A D2B.02C Am-nO-AlA. AIB. A2A. A2B. BIB. CIB AEl65102-NST10 0-3lo-AIA. AIC. A1D. A2A. A2E. A3A. A3D. A4A. BIA. BIB. B2A. B2B. LIO-JlO·BIA CIA. CIC. CIG. C2A. C2B. C2C. C2D. DIA. D2A. D2B AEl65102-NST05 10-320-C1A. CIB. CIF. FIA 10-36O-BIA. BIB. BIC LIO·l20-C I A HO-J60-AIA. BIA. BIB AEl65102-NST06 0-320-AIA. A2A. A2B, A2C. A3A, A3B. A3C. EIA. EIB. E2A. E2C. (also. HIO-36O-BIA. BIB an 0-320 model with no suffix) AEIO-36O-BIB 10-l20-AIA. A2A O-s.w-AIA. AlAS. AIBS. AICS. AID, AIDS, A2B, A3DS. A4AS, A4BS. AEl65102-NST07 10-320- BIA. BIB A4CS.MOl. BIAS. BIBS. BIDS. B2AS.B2BS.B2CS.B2CSD.B4AS.84BS. LlO-l20- B I A 84BSD. DIAl. EIA. E4AS.E4BS.E4Cl. FIAS. FIBS. GIAS. G2AS AEl65102-NST08 0-320-BIA. BIB. B2A. B2B. B3A. B3B. B3C. CIA. CIB. C2A. C2B. CM. 1O-5<O-CIBS.C ICS. C2C. C4BS.C4BSD.C4CS. D4Al. D4BS.NIAS. NIASD C3B. C3C. DIA. DIB. D2A. 02B. D2C AEl65102-NST12 0-3l0-AIA. AIAD. AID. AIF. A1F6. A1F6D. AIG. A1G6. A1G6D. A1H. AEl65102-NSno 0-350-AIA. AIC. AID. A2A. A2E. A3A. A3D. A4A. BIA. BIB. B2A, B2B. A1H6. AIJ. AILD. AlP. A2A. A2D. A2F. A2G. A2H. AlA. A3AD. A3D. CIA. CIC. CIG. C2A. C2B. C2C. C2D. DIA. D2A.02B A4A. A4AD. A4D. A4G. A4J. A4JD. A4K. A4M. A4N. A4P. ASAD. BIA. 10-36O-BIA. BIB. arc B2C. CIA. CIC. CIE. CIF. CIG. C2A. C2B. C2C. C2D. C2E. C4F. C4P. HO-360-AIA, BIA. BIB D2A. F1A6. G1A6 HIO~l6O-BIA, BIB HO-J60 -CIA A£10-l6O-BIB LO-J60-A I 060, A I H6 0-540-14.114.. AlAS, AIBS, AICS. AID. AIDS, A2B. 14.305, A4AS, A4B5, HI0-36O-BIA. BIB. GIA A4CS, 14.405. BIAS. BIBS. BIDS, B2AS. B2BS. B2CS. B2CSO. 8414.5. BoIBS. LTO-36O-AIA6D 84850.0114.5. EIA. E4AS. E4BS. E4C5. FIA5. FIBS. 0114.5. 0214.5 TO-J60-A I 14.60 ,O-540-CIBS. CICS. C2C, C4B5. C4B50, C4C5. 0414.5, 0485. NIAS. NIASO 10-360-BIB, BIBD. BID. BIE. BIF. BIF6. 8106. B2E. B2F. B2F6. B4A. AEl65102-NST12 0-3Go-A1A. A1AO. A10, A1F. A1F6. A1F60. A1G, A1G6. A1G60. A1H. EIA, L2A. MIA. MIB A1H6. AIJ. AllD. AlP. A2A. A2D. A2F.A2G. A2H. A3A. A3AD. A3D. AEIO-360-BIB. BID. BIE. BIF. BIF6. BIG6. BIH. B2F. B2F6. 84A. HIA. A4A. A4AD. A4D. A4G. A4J. A4JD. A4K. A4M. A4N. A4P. ASAD. B1A, HIB B2C. CIA. CIC. CIE. CIF. CIG. C2A. C2B. C2C. C2[T,'C2~r.c: ••. 0-540-14.405. B2BS. B2CS, B2CSO, 84B5, B4B5o. E4AS. E4B5, E4BSo. D2A. F1A6. GlA6 E4C5. 01A5. 0114.50. G2AS. HIA5. HIASO. HIBS. HIB5o. H2AS. H2A50. HO-36O-CIA H2BlD LO-J60-AIG6o,AIH6 10·5o.$0·C4B5. C4850. C405. C4oSD. O4A5. D4BS. D4CS. NIAS. NIA5D. HI0-36O-BIA. BIB. GIA T4ASO, T4BS. H8S0. T4C50. V4A5. V4ASO LTO-J6I1-A I 14.60 At:IO·s,w-D4AS, D4BS, D4CS. 0405 TO-36O-AIMD AEl65102-NST26 10-UO-J4A5. R1A5 10-J6II-BIB. BIBo. BID. BIE. BIF. BIF6. BI06. 82E. B2F. B2F6. 54A. TIO-S40-CIA. EIA. CIA. HIA EIA. L2A. MIA. MIB AEl65102-NST38 10-3l0-F1A AEIO-l60-BIB. BID. BIE. BIF. BIF6. BIG6. 81H. 82F. B2F6. B4A. HIA. TlO-~O-AAIAO. ABIAo. ABIBD. AFIA. AGIA. AKIA. CIA. CIAO. HIB KIAo 0-540-A40S, B2B5. B2CS. B2CSo. 84B5. B4BSO. E4AS. E485. E4BSo. LTI0-540-KIAO E4C5. GIAS. GIASo. 0214.5. HIA5. HIASO. HISS. HIBSD. H2AS. H2A5o. AEl65102-NST43 0-35O-J2A H2BSD 0-540-FIBS. JIASD. JIB50. JlCSD. 11050. 1214.50. HBSD. HC5o. H05o. IO·s,w·C4BS. C4BSD. C4D5. C4oSD. D4AS. D4BS, O4C5. NIA5, NIASo, J3AS, nA50, nCSD T4ASD. T4BS. T4BSo. T4CSO. V4AS. V4ASD m~s.w-ABIA5, WIA5. WIASO. WJASo AEIO-S40-D4AS. D4SS, 04CS. 0405 AEl651 02-NST•••• Q-UH3C5D AEL65102-NST26 I0-640-J4AS. R1AS TIO-540-CIA. EIA. GIA. HIA AEl65102-NST38 10-360-F1A For information, the Lycoming Engines (formerly Textron Lycoming) models 320 TJO-S40-AAIAD. ASIAo. ABIBD. AFIA, AGIA. AKIA. CIA. CIAO. 360, and 540 series, "Parallel Valve", reciprocating engines are installed on, bu KIAo LTIO-540·KIAD not limited to, the aircraft listed in the following Table 2: Table 2--Engines Installed On, But Not Limited To ~E~n-'a~;;n-.-M~.d-.-IS-:~----------'I-n-s,-.""II.-d-.-n-.-::s-u-' "N.-'''L-Im--:-:-it.-d:-:T:-.-: c....:.-"'--'- __ -"''--, IO·320-E1A M.B.B.: Monsun BO·209-C 0-320-AIA 251' 10-320-E2A Cham"on Aircraft:C;labna Oovn Aircraft: Oovn-Cessna 170, 170A, 170B IO-320-E2B Bellanca Aircraft Mooney Aircraft: Mark. 20A IO-320-F1A CAAR Engineering: Carr Mid et Oinfia: Ranauel 1A .•• 6 UO-320-B1A Pi er Aircraft: Twin Comanche PA-39 Simmerino-Graz Pauker: Flaminoo SGP..M-222 UO-32O-C1A Pi r Aircraft: Twin Comanche PA-39 Aviamilano: Scricciolo P-19 AIO-320-B1B M.B.a.: Monsun 80-209..(; Vos Helicooter Cc.: S fino Bok AEIO-320-D1B Slinosby: T67M Firefly Pioer Aircraft: Tri-Pacer PA-22 -150-, PA-22S. ~150 ,Aoache PA-23 AEIO-320-D28 Hundustan Aeronautics LId : HT-2 Dovo Aircraft: Do "-Cessna 170, 170A, 170B AEiO-320-E1A Bellanca Aircraft S.O.C.ATA.: Honzcn Gardan Champion Aircraft Piper Aircraft: In-Pacer (PA·22 "150·, PA-22S "1501, Agriculture (PA·l8A "1501 AE10-320-E1B Bellanca Aircraft S~ner Cub -('PA -18 "150"1, Caribbean·(PA.22 "1501, Pawnee (PA·25) Champion Aircraft: Oecathalon 8KCAB-CS Intermountain Mfa Co.: Call Air Tens A-5, A-5 AEI0-320-E2B Bellanca Aircraft Lake Aircraft: Colonial C-l Chamoion Aircraft: Decathalon 8KCAB Rawdon Bros.: Rawdon .1, T-15, T-150 0-320-A1A Riley Aircraft: Rile Twin Shinn Enaineerina: Shinn 2150-A 0-360-A1A Beech Aircraft: Travel Air 95, B-95 Dinfia: Ranauel lA .•6 Piper Aircraft: Comanche PA-24 Neiva: 1PD-5802 Intermountain Mfa. Co.: Call Air A-fJ SOO: Gardan-Honzon GV-80 Lake Aircraft: Colonial C-2, LA.~, 4A or 4P Laverda: Falco F8l Series /I, America Dovn Aircraft: Ooyn-Cessna 170B, 172, 172A. 1728 Malmo: Viean MF1-l0 Moonev Aircraft: Marte "20B" M-20B Kinosford Smith: Autocrat SCRM-153 Earl Horton: Pawnee Pioer PA·25 Aero Commander: '00 Dinfia: Ranauel 1A-51 Piper Aircraft: Tri-Pacer (PA-22 "150", PA-22S "1501. Cherokee (PA-28 "150"). Super Neiva: 'PO-5901 CublPA -'8 "'50") Regente: N-591 Aoriculture C7GCBA) Sud: Gardan GY-180 Bea Ie: PUrl 150 801kow: 207 Artic: Interstate S1B2 Partenavia: Oscar P--66 Robinson: R-22 Siai-Marchetti: S-205 Varna: Kachina 2,50A Procaer: Picchio F-,5·A Robinson: R-22 S.A.A.B.: Safir 91-0 Cicare: Cicare AG Malmo: vtcan MF-10B Bellanca Aircraft: Citabria 150 7GCAA, Citabria 150S GCBC Aero Boero: AB-'SO Piner Aircraft: Aoache PA-23 Beagle: Airedale A-109 Oovn Aircraft: Oovn-Cessna 170. 170A, 170B oeHaviliand: Drover OHA-3MK3 Corben-Fettes: Globe scecar Globe GC-1B Kingsford-Smith: Bushmaster J5-6 piner Aircraft: Ache PA-23 Aero Enaine Service LId.: Vieta R-2 Dovn Aircraft: 00 n-Cessna 170, 170A. 170B 0-36o-A1AO S.O.C.A.T.A.: Tabaoo T8-10 Teal II: TSC 1A2 0-36O-A1o Piper Aircraft: Comanche PA-2" Piper Aircraft: A ache PA·23 "160" lake Aircraft: Colonial LA. ...••, 4A or .•P Davn Aircraft: Do n-Cessna 170, 170A, 170B Dovn Aircraft: Dovn-Beech Beech 95 Malmo: Vinan rMF1-10 Mooney Aircraft: Master "21" (M-20E), Mark '"20B", "200", (M20B, M20C) , Mooney Pi r Aircraft: Ache PA-23 "160 ~~~~~~~~js!,!at~esim~a~ni CM~'-2iOG~3~1~~~~~~~~~~~~~~~~~~~~ Do n Aircraft: Davn-Cessna 170, 170A 170B [)intia: Querandi lA~5 Pi r Aircraft: Tri-Pacer PA·22 "160'" PA-22S "160"\ Wassmer: CWA-50 Pi~ r Aircraft: Tn-Pacer' PA·22 "160", PA-22S "160 Malmo: Vioan (MF,-,O Bea Ie: Airedale 05-'60 ~ii~~~~~jCle~s~sn~a~Ai~'ricr~a~ft.~. S~;k~Ylh~a~wk~~~~~~~~~~~~~~~~~~~ Fu'i--Heavv Industries: Fu'i F-200 Davn Aircraft: Dovn-Ptoer PA -23 "160 Uiranuru: Aerotec 122 0-36o-A1F6 Cessna Aircraft: Cardinal Robinson: R-22 0-360-A1F60 Cessna Aircraft: Cardinal 177 Maule: MX-7-160 Teal III: TSC 1A3 Lcon ~0~-~~~O-A~I~G~6~::=+=A~.~m~c~om~m~an~d~.r~;;~::::::::::::::::::::::::::::::::::~ Piner Aircraft: Aoache PA-23 "160· ~ 0-36o-A1G60 Beech Aircraft: Duchess 76 Oovn Aircraft: Doyn-Cessna 170, 170A, 170B 1:0!-!360-!A!1!H!6~~~:iP';I""rr!AiI·rlcrlaft!:jSi·jml;nio!,I'IPiA~"!4i!~!~~~~~~~~~~~~~ Piner Aircraft: Aoache PA·23 "160 0-36O-All0 Wassmer: Eurooa WA-52 Oov"n Aircraft: 00 n-Cessna 170. 170A, 170B 0-360-A1P Avia!: Husky Sud: Gardan GY80-160 0-360-A2A Center Est Aeronauti ue: Reoente OR-253 Pi r Aircraft: A ache PA·23 ·'60" S.O.C.A.T.A.: Rail e Commodore MS-893 Rile Aircraft: Ra 'av Aoache Societe Aeronautiaue Normande: Mousquetaire 0-140 Pio r Aircraft: A ache PA-23 "160" Bolkow: Klemm K1-107C Pio r Aircraft: A ache PA-23 "160 Partenavia: Oscar P--66 Pin r Aircraft: A ache PA·23 "160" Bea Ie: Husky 05-180 J1-U G rctrcc: Saeed Cancard Moonev Aircraft: Master "21" M-200 Mark "21"I'M-20E Grob: G115 0-360-A2E Std. Helicopter Slinosbv: T67 Fire'l 0-360·A2F Aero Commander: Lark 100 Piner Aircraft: Cherokee PA-28S "160 Cessna Aircraft: Cardinal Robin: Ma'or OR400·140B, Chevalier OR-360, R-31"0 0·360-A2G Beech Aircraft: SPCrt S.O.C.A.T.A.: Tamoico TB9 O·36o-A3A C.A.A.R.P.S.A.N.: M-23111 Slinnstw: T67C Firefl Societe Aeronauti ue Normande: Jodel ~1"OC Oaetwvler: MO-3-160 Robin: Recent DR .•001180, Remcrqueur OR400/180R . R-3170 Nash Aircraft LId.: Petrel S.O.C.A.T.A.: Rail e 180GT, Soortavia Soortsman RS-180 Aviolinht: P660 Delta Norman Aeroptace Co.: NAC-' Freelance General Avia: Pinouino Nash Aircraft Ltd.: Petrel O-~O-AlAO S.O.C.A.TA: T8-10 Robin: Aialon R·1,80 Piper Aircraft: Cherokee "0" PA-28 "'80 Var a: Kachina Beech Aircraft: Musketeer Custom III Grumman American: Tiaer Beech Aircraft: Sundowner 180 Pioer Aircraft: Archer II PA-28 '18 Valmet: PIK-23 Cessna Aircraft: 172 Optional 0-320-AI8 0-320-A2A 0-320-A28 0-320-A2C 0-320-A20 0-320-A3A 0-320-A38 0-320-81A 0-320-818 0-320-£2A 0'320-828 0-320-82C 0-320-820 " 0-320-82E ( ) 0-320-83A 0-320-838 .-/ 0-32O-CIA 0-320-CI8 0-320-ClA 0-320-C38 0-320-01A 0-320-01F 0-320-02A 0-320-028 Cessna Aircraft: Skvhawk 172 Beech Aircraft: Musketeer M-23 Pioer Aircraft: Cherokee PA-28 ",60,,\ 0-320-02J 0-320-03G 0-320-EIA Ploer Aircraft: Warrior II, Cadet PA·28-'61 Grab: G115 Piner Aircraft: Cherokee PA-28 ""0", PA-28 "150" 0-320-EIC M.B.B. lMesserschmitt-Boetkow-Blohm : Monsun BO-209-B 0-320-E1F ·M.B.B.: Monsun BO·209·B 0-320-E2A Siai-Marchetti; S-202 F.F.A.: Bravo AS-202l15 Robin: Ma'or OR-3"0, Sitar, Banheera GV-100-135 S.O.C.A.T.A.: Super Ranve MS-886, Rail e Commodore (MS·892 Partenavia: Oscar P66B ,Bucker 131 APM 0-320-E2C Beech Aircraft: Musketeer III eM -2311I Aeromot: Paulistina P-56 Pezetel: Koliber 150 M.B.B.: Monsun BO-209-B Cessna Aircraft: Cardinal 172-1, 177 0-320-E20 0-32o-E2F M.B.8.: Monsun BO-209-B . Wassmer Pacific lWA-51 0-320-E2G American Aviation Corn Traveler Hi. Shear: Wino 0-320-E30 Piper Aircraft: Cherokee 1"0 Beech Aircraft: Soort PirV!r Aircraft: Twin Comanche PA-30 10-320-82A Ted Smith Aircraft: Aerostar Ptoer Aircraft: Twin Comanche PA-30 Turbo 10-320-81C 10·320-Bl0 10-320-C1A 10-320-01A 10-320-018 M.B.B.: Monsun BO-209-C M.B.B.: Monsun BO-209-C O-~O-A4A 0-~0-A40 O-~O-A4G 0-360-A4K Penn Van: Super Cub Conversion C. Itot! and Co.: Fu'i FA -200 Seabird Aviation: SB7l Intermountain Mf . Co.: Call Air A-6 Bellanca Aircraft: Scout 8GCBC-CS Maule: Star Rocket MX-7-,80 Christen: Husky A-1 Huohes Tool cc.: 269A 0-~0-A4M 0-36O-A"N 0-360·A"P 0-~O-A5AO 0-~0-82C O-~O-CIA 0-~O-C1E 0-360-CIF O-~O-CIG 0-360-C28 0-360-C20 Hughes Tool Co.: 269A 0-~O-C2E Huohes Tool Co.: CYHO-2HU Military Bellanca Aircraft: Scout 8GCBC FP Maute: MX-7-180A Penn Van: Su r Cub Conversion Cessna Aircraft: Cutlass RG 0-360-C4F 0-~O-C4P 0-~O-F1A6 Robinson: R22 Beech Aircraft: Travet-Air B-95A Dovn Aircraft: Dcvn-Picer PA -23 "200 0·360-J2A 10-360-81A 2 .. adNote Alternate Static Source Valve COMPLIANCE DATE TOTAL TIME AT COMPLIANCE AUTHORIZED SIGNATURE & NUMBER TACH OR RECORDING METER TIME AT COMPLIANCE METHOD OF COMPLIANCE S81. Note 2: PIN 2013142-18 replaced PINs 2013142-9. -13. and -17. Amendment 39-15776; Docket No. FAA-2008-1328; Directorate Identifier 2008- CE-066-AD. Effective Date (a) This AD becomes effective on January 5, 2009. Affected ADs (b) This AD relates to AD 98-01-01, Amendment 39-10287 and AD 2008-10- 02, Amendment 39-15508. These ADs can be found on the Internet at the following Web site: http://rgl.faa.gov/. Applicability (c) This AD applies to all serial numbers (SINs) of the airplanes listed in Table 1 of this AD, certificated in any category, that: (1) Were initially delivered from the manufacturer between January 1, 1993, and March 31, 2008, unless the modificationlrework required in AD 2008-10-02 has been done and you remain in compliance with that AD; or (2) Have a part number (PIN) 2013142-18 installed as a replacement part any1ime after January 1, 1993, unless the modification/rework required in AD 2008-10-02 has been done and you remain in compliance with that AD. Note1: The affected part was shipped from Cessna Parts Distribution (CPD) between January 1,1993, and March 31, 2008. C 2008 AeroTech Publications, Inc.. All rights reserved J*'/'/'" '{J,T/A/I/.JIII;.tIfiI::.r. ••. ",.,M."*"'''·.,~ (I/I.'I~.••./..-;'AI"~""';.,r/./JII;:I./ ••. 'M,;.,j"'.In'''-''''''""r,..,.r.~/./I/" ••...• /1. ••. f. !Aerotech Note: Table 1 has been moved from this location in the Original FAA • ~ version of this Airworthiness Directive to page 3, to facilitate compilation of this " tadNoteTM. ~ ~"•••.•~..r.-W/.It':.V.•••Y•• J!I':-;.w.k.AI"/' ...,..,~/,/""IIIY,""',AI:'/I. "'~~/JIT "'I-Jr/.III'/.6'-'.# ';I/r-' ~~.;ro;;_ .'..., :6'/1-#/" " ~ Unsafe Condition (e) This AD is the result of reports of improper installation of the part number identification placard on the alternate static air source selector valve. We are issuing this AD to prevent erroneous indications from the altimeter, airspeed, and vertical speed indicators, which could cause the pilot to react to incorrect flight information and possibly result in loss of control. Compliance (e) To address this problem, you must do the following, unless already done. A person authorized to perform maintenance as specified in 14 CFR section 43.3 of the Federal Aviation Administration Regulations (14 CFR 43.3) is required to do all the actions required in this AD. Actions Compliance Procedures (1) For all affected airplanes that are not equipped for fliqht Within the next 100 hours time-in-service (TIS) after January Following the procedures in Cessna Single Engine Service under instrument flight rules (fFRl: Inspect the alternate static 5. 2009 (the effective date of this AD) or within the next 4 Bulletin air source selector valve to assure that the part number months after January 5. 2009 (the effective date of this AD). SB08-34-02. Revision I, dated October 6, 2008; Cessna Caravan identification placard is not obstructing the port. whichever occurs first. Service Bulletin CAB08·4, Revision I, dated October 6, 2008; Cessna Single Engine Service Bulletin SE808·5, dated October 13, 2008; or Cessna Multi-engine Service Bulletin MEB08-6, dated October 13.2008, as applicable (2) For all affected airplanes that are equipped for fliqht under. (A) Inspect within the next 10 days after January 5. 2009 (the Following the procedures in Cessna Single Engine Service instrument flight rules (IFR): effective date of this AD); or Bulletin (i) Inspect the alternate static air source selector valve to assure that (B) Install placards before funher flight after January 5, 2009 (the SB08-34-02, Revision 1, dated October 6, 2008; Cessna Caravan the part number identification placard is not obstructing the port, or effective date of this AD). Service Bulletin CAB08-4, Revision 1, dated October 6, 2008; Cessna Single Engine Service Bulletin SE808-5. dated October 13. 2008; or (ii) Fabricate a placard that incorporates the following words (using at Cessna least 118-inch letters) and install this placard on the instrument panel within the pilot's clear view: "IFR OPERATION IS PROHIBITED" Multi-engine Service Bulletin MEB08-6, dated October 13,2008. as and "USE OF THE ALTERNATE STATIC AJR SOURCE IS applicable PROHIBITED." (3) For all affected airplanes that are eguipped for flight under Within the next 100 hours TIS after January 5.2009 (the Following the procedures in Cessna Single Engine Service instrument flight rules (IFRl: If placards were installed in effective date of this AD) or within the next 4 months after Bulletin accordance with paragraph (e)(2)(ii) of this AD. inspect the January 5. 2009 (the effective date of this AD), whichever S808·34-02, Revision I, dated October 6, 2008; Cessna Caravan alternate static air source selector valve to assure that the part occurs first. After doing the inspection, remove the placards number identification placard is not obstructing the port. installed in accordance with paragraph (e)(2)(ii) of this AD Service Bulletin CABOS-4. Revision 1, dated October 6, 2OOS;Cessna before further flight. Single Engine Service Bulletin SEB08-5, dated October 13.2008; or Cessna Multi-engine Service Bulletin MEB08-6, dated October 13. 200S. as applicable. (4) For all affected airplanes: If the alternate static air source Before further flight after the inspection required in paragraphS Following the procedures in Cessna Single Engine Service selector valve port is found obstructed by the part number (e)(l). (e)(2)(i). and (e)(3) of this AD. Bulletin identification placard during the inspection required in SB08-34-02, Revision I, dated October 6, 2008; Cessna Caravan paragraphs (e)(1). (e)(2)(i). and (e)(3) of this AD. remove the placard from the valve body, discard the placard, and assure Service Bulletin CAB08·04, Revision I, dated October 6, 2008; that the port is open and unobstructed. Cessna Single Engine Service Bulletin SEB08-5, dated October 13, 2008, or Cessna Multi-engine Service Bulletin MEB08-6, dated October 13. 2008. as applicable (5) For ail affected airplanes: When a replacement valve is As of 10 days after January 5. 2009 (the effective date of this A person authorized to perform maintenance as specified in '4 needed. only install a PIN 2013142-18 alternate static air AD) CFR section 43.3 of the Federal Aviation Administration source selector valve that has been inspected and the port is Regulations (14 CFR 43.3) is required to do the inspection. found free from obstruction. u (Over)'* (Page 3 of Airworthiness Directive 2008-26-10) Table 1--Applicable Airplane Models Models 172 F172K 177 172A F172L 177A 1726 F172M 1776 172C F172N 177RG 1720 F172P F177RG 172E FR172E 180 172F USAF T-41A FR172F 180A 172G FR172G 180B 172H (USAF T -41A) FR172H 180C 1721 FR172J 1800 172K FR172K 180E 172L P1720 180F 172M R172E USAF T-416 USAF T -41C and 0 180G 172N R172F USAF T-41 180H 172P R172G USAF T-41C or 0) 180J 1720 R172H USAFT -410) 180K 172R R172J 182 172S R172K 182A F1720 172RG 1826 F172E 175 182C F172F 175A 1820 F172G 1756 182E F172H 175C 182F 182G A185F U2060 182H 206 U206E 182J 206H U206F 182K P206 U206G 182L P206A 207 182M P206B 207A 182N P206C T207 182P P2060 T207A 1820 P206E 208 182R T206H 208B 182S TP206A 210 182T TP206B 210A F182P TP206C 210B F1820 TP2060 210C FR182 TP206E 2100 R182 TU206A 210E T182 TU206B 210F T182T TU206C 210G TR182 TU2060 210H 185 TU206E 210J 185A TU206F 210K 185B TU206G 210L 185C U206 210M 1850 U206A 210N 185E U206B 210R A185E U206C 210-5 205 210-5A (205A) FT337F T210F M337B (USAF 02A) T210G T337B T210H T337C T210J T3370 T210K T337E T210L T337F T210M T337H T210N T337H-SP T210R T303 336 337 337 A (USAF 02B) 3378 337C 3370 337E 337F 337G 337H F337E F337F F337G F337H FT337E Precision Airmotive Fuel Injectors If multi-engine: U Left u Right :J Front U Rear Engine Model: .:/:o-Joo-L 24 Serial No: L-.l'/Iuv -$IE TACH OR RECOROING METER TIME ATCOMPL. DATE METHOD OF COMPLIANCE TOTAL TIME AT COMPL. o Amendment 39-15793. Docket No. FAA-2oo8-0420: Directorate Identifier 2008-NE-10- AD. Effective Date (a) This airworthiness directive (AD) becomes effective February 9, 2009. Affected ADs (b) This AD supersedes AD 2008-08-14, Amendment 39-15466. Applicability (c) This AD applies to the following reciprocating engines with a Precision Airmotive LLC, RSA-5 or RSA-l0 series, or Bendix, RSA-5 or RSA-l0 series, fuel injection servo, having a servo plug gasket, part number (PIN) 365533, that was installed under the fuel injection servo plug, PIN 383493, on or after August 22, 2006: (1) Lycoming Engines 10, (L)IO, TIO, (L)TIO, AEIO, AIO, IGO, IVO, and HIO series reciprocating engines. (2) Teledyne Continental Motors LTSI0-360-RB and TS10-360-RB reciprocating engines. (3) Superior Air Parts, Inc. 10-360 series reciprocating engines. (d) This AD also applies to any other Precision Airmotive LLC RSA-5 or RSA-l0 series, or Bendix, RSA-5 or RSA-l0 series, fuel injection servo: (1) That was received for installation on an engine on or after August 22, 2006 without a PIN 2577258 gasket and it does not have a letter "G" on the fuel injection servo plug, PIN 383493; or (2) Any fuel injection servo that the installation history is not known. Unsafe Condition (e) This AD results from Precision Airmotive LLC introducing the installation of a new improved servo plug gasket, PIN 2577258, to the affected Precision Airmotive LLC RSA-5 and RSA-l0 series, and Bendix, RSA-5 and RSA-l0 series, fuel injection servos. We are issuing this AD to prevent a lean running engine, which could result in a substantial loss of engine power and subsequent loss of control of the airplane. Compliance (f) You are responsible for having the actions required by this AD performed before further flight, unless the actions have already been done. Initial Inspection (g) Before further flight, inspect the fuel injection servo plug, PIN 383493, for looseness, by attempting to tum it by hand, while being careful not to damage the safety wire or seal. If the plug moves, it is loose. (h) If the plug is not loose, go to paragraph U) of this AD. (i) If the plug is loose, do the following: (1) Carefully cut and remove the safety wire that spans between the servo plug and regulator cover only. (2) Remove the servo plug and gasket, PIN 365533, that is behind the plug. The gasket may be slightly stuck to the regulator cover. (3) Examine the threads on the servo plug and regUlator cover for damage. Threads should be smooth and consistent, with no burrs or chips. The servo plug outer diameter threads should also measure within 0.7419-0. 7500-inch. (4) If the threads on either the servo plug or the regulator cover are damaged, or do not measure within the limits in paragraph (i)(3) of this AD, the servo is not eligible for any installation and must be replaced before further flight. (5) Replace the gasket, PIN 365533, with a new improved gasket, PIN 2577258. (6) While the hex plug is removed, stamp or scribe the letter "G" onto the face of the hex plug. Information on stamping or scribing can be found in Precision Airmotive LLC Mandatory Service Bulletin (MSB) No. PRS-l07 Revision 4, dated July 16, 2008. (7) When reassembling, do not install any servo plug or regulator cover that is not eligible for installation. Install a new gasket, PIN 2577258, onto the servo plug and reassemble the servo plug to the regulator cover. (8) Torque the servo plug to a new, higher torque of 90-100 in- Ibs, to maintain the proper Clamp-up force between the plug and cover. (9) Safety wire the servo plug with 0.015 thru 0.025 inch diameter wire to the reguilitor cover screws. Information on properly safety wiring the plug can be found in Precision Airmotive LLC MSB No. PRS-107, Revision 4, dated July 16, 2008. u DUE AT NEXTCOMPL DATE. TACH. OR RECORDING METER TIME TOTAL TIME AUTHORIZED SIGNATURE & NUMBER 6} 2009 AeroTeCh publications. Inc .. All rights reserved (10) Inspect all other safety wire on the servo. Replace any that are damaged. Repetitive Inspections U) For servo plugs that passed inspection with a gaSket, PIN 365533 installed, at every engine oil change or within every 50 hours of engine run time, whichever occurs first, repeat the inspection and remedial steps speclried in paragraphs (g) through (i)(10) of this AD. Mandatory Terminating Action (k) By December 31, 2009, as mandatory terminating action to the repetitive inspections required by this AD, replace all servo plug gaskets, PIN 365533 that are installed on servos affected by this AD, with gasket, PIN 2577258. (I) Use paragraphs (i)( 1) through (i)( 10) of this AD, to do the gasket replacements. Prohibition of Installing Gasket PIN 365533 (m) After the effective date of this AD, do not install gasket, PIN 365533, onto any fuel injection servo. Identification of Servo Plug Gaskets (n) Servo plug gaskets, PIN 365533, are identified as being made of either a paper or fiber material, impregnated with synthetic rubber. They are relatively flexible and have a rough surface. (0) Servo plug gaskets, PIN 2577258, are identified as being made of metal with a coating of synthetic rubber. They are relatively rigid and have a smooth surface. Special Flight Permits Prohibited (p) Under 14 CFR part 39.23, we are prohibiting special flight permits. Alternative Methods of Compliance (q) The Manager, Seattle Aircraft Certification Office, may approve altemative methods of compliance for this AD if requested using the procedures found in 14 CFR 39.19. Related Information (r) For Precision Airmotive LLC, Richard Simonson, Aerospace Engineer, Propulsion Branch, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington 98055; e-mail: Richard.simonson@faa.gov; telephone (425) 917- 6507; fax (425) 917- 6590. (s) For Lycoming Engines, Norm Perenson, Aerospace Engineer, New York Aircraft Certification Office, FAA, Engine & Propeller Directorate, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; e- mail: Norman.perenson@faa.gov; telephone (516) 228-7337; fax (516) 794-5531. (t) For Teledyne Continental Motors, Kevin Brane, Aerospace Engineer, Atlanta Aircraft Certification Office, FAA, Small Airplane Directorate, One Crown Center, 1895 Phoenix Blvd., Suite 450, Atlanta, GA 30349; e-mail: kevin.brane@faa.gov; telephone (770) 703- 6063; fax (770) 703-6097. (u) For Superior Air Parts, Inc., Tausif Butt, Aerospace Engineer, Special Certification Office, FAA, Rotorcraft Directorate, Southwest Regional Headquarters, 2601 Meacham Blvd., Fort Worth, Texas 76137; e-mail: Tausif.butt@faa.gov; telephone (817) 222-5195; fax (817) 222-5785. (v) FAA Special Airworthiness Information Bulletin NE-09-04, dated January 9, 2009, also pertains to checking servo plugs for looseness on Precision Airmotive LLC RSA-5 and RSA-l0 series, and Bendix RSA-5 and RSA-l0 series, earlier produced fuel injection servos, not affected by this AD. (w) Precision Airmotive LLC MSB No. PRS-l07, Revision 4, dated July 16, 2008, also pertains to the subject of this AD. Contact Precision Airmotive LLC, 14800 40th Avenue, NE., Marysville, WaShington 98271; telephone (360) 651-8282; http://www.precisionairmotive.com. for a copy of this MSB. Material Incorporated by Reference (x) None. Issued in Burlington, Massachusetts, on January 13, 2009. Peter A. White, Assistant Manager, Engine and Propeller Directorate, Aircraft Certification Service. Induction Air Filters If multi-engine: 0 Left 0 Right 0 Front 0 Rear NEXT COMPL DUE AT TACHOR OATE.TACH.OR DATE TOTAL TIME RECOROING METHOD OF COMPLIANCE TOTAL RECOROING AUTHORIZED SIGNATURE & NUMBER AT COMPL. METERTIME TIME METERTIME _ ~ ATCOMPL. :/' 7J"7J~ Of of - ,u;D AT Ft - .~(""y).CJ SOJ,O /~ ~ / L CA. ":;'1/ rLhq/Jo l.../<ro.~LilB.s IN:r-r4-lJV~ Nk~ "ItBri-<; "9at~t;~ "'= ~ -~;:T5~ ~h:lo'iB7./d,{J elBA.1> "")/"",.'" tJrtA tJJ1rrJ 137~.U 131£.7-; ~:...- ~ :)~V/ It;/':h<.> 13(07.'7 1.'(p7:7laIJIMA/J wh/l. 'II£() /9MJ'k7 /8/;7,/ ~---~ ':-::;-w.Rx1 ,izltho \4li7.C 1~/.t) l'&{/~,S9&Tl4tJ )SlD7.(J t~/,C) l2;1h. ~ -2(;J//~ Y' 1:iI//1b 1'S~7rJ ISC./~'1 &/ 11oQP~ !G.(.7,7 /~~7-7cJ'-v~ -k::/ ~ '3.r'it..~tA nJz//-O /~~4s /~fo.Is ?;7 /;U~ Jfl(pt{.~ 171etl, ~'/:)-9f.V'~' ~ J.c."'\~rJ?(..p ;J~11\ \/\c4:<::. '\1104,~ ~/M/&a1CIN 1~/P4-, L)f<C4-S('IJ-34--~ ff~~<9 S!t~, IW!f.t, I!::LJY,S- Y?taJfXL/J wfflJ ~) zJ~c.j,S ZJ(J'-/,S-_~ :..4IIIL/lA~1I u/J" ! U,l,.(" 13(,3·~ ~IXA<UJ1v17'U l'ItlJ ltn3,S"' U:<.oJS' 1- ~ ~/"" A.,V(1!JZlV/ Amendment 39-4966. Applies to all paper induction air· filters used in small airplanes. Compliance: Required as indicated, unless already accomplished. To prevent possible engine power loss or stoppage caused by engine ingestion of fragments of a deteriorated induction air filter, accomplish the following: Within the next one hundred hours time-in-service after the effective date of this AD or prior to the accumulation of 500 hours time-in-service on the filter, whichever occurs later, and thereafter at intervals not exceeding 500 hours time-in-service on the filter: C 1984 AeroTech publications, Inc., All nghts reserved (a) Replace the air filter with a new filter that is FAA approved for the airplane installation, (b) Within 100 hours time-in-service replace any filter on which the time-in-service cannot be determined utilizing the airplane maintenance records for this determination. NOTE: This AD does not alter current maintenance procedures which require inspection of paper induction air filters at 100 hours time-in-service and annual inspections and replacement as necessary based on filter condition. This amendment becomes effective January 29, 1985. adNote" Ignition Switch DATE METHOD OF COMPLIANCE DUE AT NEXTCOMPL DATE. TACH. OR RECORDING METER TIME TOTAL TIME AUTHORIZED SIGNATURE & NUMBER I Amendment 39-8511. Dock-et92-NM-165-AD. Applicability: ACS and Gerdes ignition switches; as installed in, but not limited to, Piper Model PA-38-112 series airplanes, Schweizer Model G-164 series (including Model G-164A, G-164B, and G-164C) airplanes, Schweizer Model 2-37 and 2-37A series airplanes, and the following Cessna airplanes; certificated in any category: ossna Model Serial Numbers 150 15074428 rouqh 15079405 150 1500389 hrough ~1500734 150 F15001024 hrouah 15001428 RA150 FRA1500212 hrouoh RA1500336 152 1527940Q hrouah 15286033 A152 ~1520735 rouah 1521049 152 15201429 hrouah F15201980 A152 A1520337 nrouQh A1520425 172 17261486 hrough 17276673 172 1722000 hrough R1723454 172RG 172RGoo01 hrouah 172RG1191 172 17201045 hrouah 17202254 R172 R17200441 rouch R17200675 177 17701890 hrouah 7702752 177RG 177RG0342 hrouoh 177RG1366 177RG 177RG0093 hrouah 177RG0177 180 18052317 hrouah 18053203 182 18261786 hrouah 18268615 R182 'l.18200001 brouah 18202041 182 182-{)137 hrough 182-{)148' 182 18200001 hrouah 18200169 fR182 R18200001 hrouah R18200070 185 18502154 hrouah 18504448 U206 J20601980 hrouah 20607020 07 0700222 hrouoh 0700788 10 1059893 hrough 1065009 210 21000001 hrouoh 21000874 u Compliance: Required as indicated, unless accomplished previously. To prevent failure of ignition switches, accomplish the following: (a) Within 100 flight hours after the effective date of this AD, or at the next annual inspection, whichever occurs first, perform an inspection of the ignition switch to detect wear and corrosion, and lubricate the switch, in accordance with ACS Service Bulletin SB92- 01, dated August 15, 1992; or Cessna Service Bulletin SEB91-5, Revision 1, June 14, 1991. If wear or corrosion is detected, prior to further flight, replace the switch in accordance with the service bulletin. Repeat this inspection and lubricate the ignition switch in accordance with the service bulletin, thereafter, at intervals not to exceed 2,000 flight hours. NOTE: ACS ignition switches that do not have a "start" position (models A-510-1 and A-510-5) or were manufactured on or after e 2004 AeroTech Publications, Inc., All rights reserved February 20, 1989, and have not accumulated 2,000 flight hours, need not' be lubricated. The manufacture date is stamped on the switch body. These switches are identifiable by red paint in the screw heads on the back of the switch. However, manufacturer lubricated switches that have a "start" position, but do not have a starter solenoid diode, must be inspected and modified. (b) Within 100 flight hours after the effective date of this AD, or at the next annual inspection, whichever occurs first, inspect the ignition switch installation to determine if a diode or other surge suppresser is' installed on the starter solenoid. If one is not installed, prior to further flight, install a starter solenoid diode in accordance with ACS Service Bulletin SB92-01, dated August 15, 1992; or Cessna Service BC:ietin SEB91-5, Revision 1, dated June 14,1991. NOTE: For operators using the Cessna service bulletin to install the diode in the starter solenoid: The procedures for installation are contained in Attachment to Service Bulletin SEB91-5R1, Revision 1, dated June 14, 1991. (c) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Los Angeles Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector', who may add comments and then send it to the Manager, Los Angeles ACO. NOTE: Information concerning the existence of approved alternative methods of compliance with this",AD, if any, may be obtained from the Los Angeles ACO. (d) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD 'can be accomplished. (e) The inspection, lubrication, replacement, and modification shall be done in accordance with ACS Service Bulletin SB92-01, dated August 15, 1992; or Cessna Service Bulletin SEB91-5, Revision 1, dated June 14, 1991, which includes Attachment to Service Bulletin SEB91-5R1, Revision 1, dated June 14, 1991. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from ACS Products Company, P.O. Box 152, 1585 Copper Drive, Lake Havasu City, Arizona 86403-0008; or Cessna Aircraft Company, Customer Services, P.O. Box 7704, Wichita, Kansas 67277. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the Los Angeles Aircraft Certification Office, 3229 East Spring Street, Long Beach, California; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. (f) This amendment becomes effective on April 29, 1993