FEDERAL AVIATION ADMINISTRATION AIRWORTHINESS DIRECTIVES SMALL AIRCRAFT, ROTORCRAFT, GLIDERS, BALLOONS, & AIRSHIPS BIWEEKLY 2004-19 This electronic copy may be printed and used in lieu of the FAA biweekly paper copy.

U.S. Department of Transportation Federal Aviation Administration Regulatory Support Division Delegation and Airworthiness Programs Branch, AIR-140 P. O. Box 26460 Oklahoma City, OK 73125-0460 FAX 405-954-4104

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SMALL AIRCRAFT, ROTORCRAFT, GLIDERS, BALLOONS, & AIRSHIPS AD No.

Information

Manufacturer

Applicability

Info: E - Emergency; COR - Correction; S - Supersedes; R - Revision; - See AD for additional information; Biweekly 2004-01 2003-23-05 2003-24-13 2003-26-04 2003-26-06 2003-26-14 2004-01-09 2004-01-10 2004-01-14 2004-01-51

COR COR

E

Titeflex Corportation Cessna Aircraft Company Agusta S.p.A. Anjou Aeronautique Kiddie Aerospace Eurocopter France Eurocopter Deutschland Eurocopter France Eurocopter France

Appliance: Titeflex hoses 172R, 172S, 182S, 182T, T182T, 206H, and T206H Rotorcraft: A109E Appliance: Safety belts and restraint systems Appliance: Hand-held halon fire extinguishers Rotorcraft: AS355E, F, F1, F2, and N Rotorcraft: MBB-BK-117 A-1, A-3, A-4, B-1, B-2, and C-1 Rotorcraft: EC130B4 Rotorcraft: AS355E, F, F1, F2, and N

Cessna Aircraft Company Raytheon Aircraft Company

441 and F406 1900, 1900C, 1900 (C-12J), and 1900D

Agusta S.p.A. Air Cruisers Company

Rotorcraft: A109E Appliance: Emergency Evacuation Slide/Raft Systems

Learjet Eurocopter France Pacific Aerospace Corporation, Ltd. The New Piper Aircraft, Inc. Pilatus Aircraft LTD.

31, 31A, 35, 35A (C-21A), 36 and 36A Rotorcraft: AS332C, L, and L1 FU24-954 and FU24A-954

45 (YT-34), A45 (T-34A, B-45), and D45 (T-34B) MU-2B, MU-2B-10, MU-2B-15, MU-2B-20, MU-2B-25, MU-2B26, MU-2B-26A, MU-2B-30, MU-2B-35, MU-2B-36, MU-2B36A, MU-2B-40, and MU-2B-60 Rotorcraft: AS355E, F, F1, F2, and N Engine: CT58-100-2, CT58-140-1, -140-2, and T58-GE-1, -3, -5, 8E, -8F, -10, -100, and -402 Turboshaft Engine: JT15D-1, -1A, and -1B Turbofan Otter DHC-3 N22B, N22S, and N24A

Biweekly 2004-02 2003-09-09 R1 2004-01-13

R S 97-22-16

Biweekly 2004-03 2004-02-03 2004-03-01

S 2003-03-11

Biweekly 2004-04 2004-03-08 2004-03-27 2004-03-29 2004-03-32 2004-04-01

COR

S 2002-01-09

PA-46-500TP PC-7, PC-12, and PC-12/45

Biweekly 2004-05 2001-13-18 R1 2003-22-07 R1

R1, COR R

Raytheon Aircraft Company Mitsubishi Heavy Industries, Ltd

2004-01-51 2004-04-06

FR

Eurocopter France General Electric Company

2004-04-09 2004-05-01 2004-05-02

Pratt & Whitney Canada Bombardier Inc. Aerospace Technologies of Australia Pty Ltd.

Biweekly 2004-06 2004-03-01

Air Cruisers Company

Appliance: Emergency Evacuation Slide/Raft System

2004-05-23

COR, S 2003-0311 S 89-21-01

Eurocopter France

2004-05-24

S 2002-23-06

Lycoming Engines

2004-05-28 2004-05-29 2004-06-51

E

2004-06-52

E

Eurocopter France Eurocopter France Boeing Defense and Space Group Robinson Helicopter Company

Rotorcraft: AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350C, AS350D, AS350D1, AS355E, AS355F, AS355F1, AS355F2, and AS355N Engine: AEIO-540, IO-540, LTIO-540, O-540, and TIO-540 Series Reciprocating Rotorcraft: AS 365 N3 Rotorcraft: EC 155B Rotorcraft: 234

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Rotorcraft: R22, R22 Alpha, R22 Beta, and R22 Mariner

SMALL AIRCRAFT, ROTORCRAFT, GLIDERS, BALLOONS, & AIRSHIPS AD No.

Information

Manufacturer

Applicability

Info: E - Emergency; COR - Correction; S - Supersedes; R - Revision; - See AD for additional information; Biweekly 2004-07 2004-06-04 2004-06-05 2004-06-09 2004-06-10

Sikorsky Aircraft Corporation Pilatus Aircraft Ltd. The Lancair Company Aerospace Technologies of Australia Pty Ltd.

Rotorcraft: S-76 A, B, and C PC-12 and PC-12/45 LC40-550FG and LC42-550FG N22B, N22S, and N24A

Eurocopter France

Rotorcraft: AS332C, L, and L1

Bombardier Inc. Engine Components Incorporated (ECi) Schempp-Hirth Flugzeugbau Gmbh Burkhardt Grob Luft-und Raumfahrt Gmbh Co & KG Glasflugel Goodrich Avionics Systems, Inc. NARCO Avionics Inc. Cessna Aircraft Company HPH s. r. o. Cessna Airplane Company

Otter DHC-3 Engine: Teledyne TSIO-520-NB, -VB, -WB, 520 and 550 Series Reciprocating Glider: Discus-2a, Discus-2b, Ventus-2a, and Ventus-2b

Biweekly 2004-08 2004-03-27

COR

Biweekly 2004-09 2004-05-01 R1 2004-08-10

R

2004-08-12 2004-08-13 2004-08-14 2004-08-15 2004-08-16 2004-08-17 2004-09-03 2004-09-05

S 2003-13-08

Glider: G103 Twin ASTIR, G103 Twin II, G103 Twin III ACRO, and G103 C Twin III SL Glider: Mosquito and Club Libelle 205 Appliance: Terrain Awareness Warning System (TAWS) Appliance: AT150 Transponders 208 amd 208B Glider: Glasflügel 304CZ, 304CZ-17, and 304C 500, 501, 550, and 551

Biweekly 2004-10 2004-08-17 2004-09-02 2004-09-07 2004-09-29

COR

2004-09-30

Cessna Aircraft Company Glasflugel-Ing. E. Hanle Raytheon Aircraft Company Honeywell International Inc.

Raytheon Aircraft Company

208 and 208B Glider: Kestrel 1900, 1900C, 1900C (C12J), and 1900D Engine: TPE331-10-501C, -10-511C, -10-501K, -10-511K, -10501M, -10-511M, -10AV-511B, -10AV-511M, -10GP-511D, 10GT-511D, -10N-511S, -10N-512S, -10N-513S, -10N-514S, 10N-515S, -10N-531S, -10N-532S, -10N-533S, -10N-534S, -10N535S, -10P-511D, -10R-501C, -10R-502C, -10R-511C, -10R512C, -10R-513C, -10T-511D, -10T-511K, -10T-511M, -10T512K, -10T-513K, -10T-515K, -10T-516K, -10T-517K, -10U501G, -10U-502G, -10U-511G, -10U-512G, -10U-503G, -10U513G, -10UA-511G, -10UF-501H, -10UF-511H, -10UF-512H,10UF-513H, -10UF-514H, -10UF-515H, -10UF-516H, -10UG513H, -10UG-514H, -10UG-515H, -10UG-516H, -10UGR-513H, -10UGR-514H, -10UGR-516H, -10UR-513H, -10UR-516H, -11U601G, -11U-602G, -11U-611G, and -11U-612G Turboprop 1900C

Goodrich Avionics Systems, Inc.

Appliance: Terrain Awareness Warning System (TAWS)

Bell Helicopter Textron Canada Alexander Schleicher GmbH & Co. Segelflugzeugbau Lycoming Engines Garmin International Inc. Eagle Aircraft (Malaysia) SDN. BHD

Rotorcraft: 407 Glider: ASH 25M

Biweekly 2004-11 2004-08-15 2004-10-07 2004-10-08 2004-10-14 2004-10-15 2004-11-04

COR S 2003-13-08 S 2002-06-52 S 91-14-22

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Engine: Direct-Drive Reciprocating Engines Appliance: Mode S transponders Eagle 150B

SMALL AIRCRAFT, ROTORCRAFT, GLIDERS, BALLOONS, & AIRSHIPS AD No.

Information

Manufacturer

Applicability

Info: E - Emergency; COR - Correction; S - Supersedes; R - Revision; - See AD for additional information; Biweekly 2004-12 2004-06-51

FR

2004-11-05 2004-11-06 2004-11-10 2004-11-12

Boeing Defense And Space Group Eurocopter France Agusta S.p.A Przedsiebiorstwo Doswiadczalno-Produkcyjne Szybownictwa ''PZL-Bielsko'' Alexander Schleicher Gmbh & Co.

Rotorcraft: 234

Agusta S.p.A. Burkhart Grob Luft-Und Raumfahrt GmbH & Co KG Cessna Airplane Company Eurocopter France Pilatus Aircraft Ltd. Dowty Aerospace Propellers

Rotorcraft: A109C, A109E, and A109K2 Glider: G103 Twin Astir, G103A Twin II Acro, G103C Twin III Acro 500, 501, 550, and 551 Rotorcraft: EC 155 B and B1 PC-12 and PC-12/45 Propeller: R321/4-82-F/8, R324/4-82-F/9, R333/4-82-F/12, and R334/4-82-F/13 Rotorcraft: MBB-BK 117 A-1, A-3, A-4, B-1, B-2, and C-1

Rotorcraft: EC 130 B4 and AS 350 B3 Rotorcraft: A109E Glider: SZD-50-3 ''Puchacz'' Glider: ASW 27

Biweekly 2004-13 2001-24-07 R1 2003-19-14 R1

R R

2004-09-05 2004-12-06 2004-12-11 2004-13-01

COR S 2002-01-28

2004-13-05

Eurocopter Deutschland

Biweekly 2004-14 95-26-05 R1 2003-13-15 R1 2004-10-14 2004-13-20 2004-13-26 2004-14-02 2004-14-12

Res. R COR, S 91-14-22

Robinson Helicopter Company Schweizer Aircraft Corporation Lycoming Engines Garmin AT Kaman Aerospace Corporation Rolls-Royce Corporation New Piper Aircraft, Inc.

Rotorcraft: R44 Rotorcraft: 269A, 269A-1, 269B, 269C, and TH-55A Engine: Direct-Drive Reciprocating Engines Appliance: Global positioning system (GPS) Rotorcraft: K-1200 Engine: 250-C28, -C28B and, -C28C Turboshaft PA-28-161, PA-28-181, PA-28R-201, PA-32R-301 (HP), PA-32R301T, PA-32R-301T, PA-32-301FT, PA-32-301XTC, PA-34220T, PA-44-180, PA-46-350P, and PA-46-500TP

The Cessna Aircraft Company

525

2004-14-21 2004-14-22

Stemme GmbH & Co. Pratt & Whitney Canada

2004-15-01

Raytheon Aircraft Company

Glider: S10-VT, S10-V, S10 Engine: PW206B, PW206C, PW206E, PW207D, and PW207E Turboshaft 390

Biweekly 2004-15 2004-14-20

COR S 2003-21-07

Biweekly 2004-16 2004-15-11 2004-15-15 2004-15-18 2004-15-19 2004-15-21 2004-15-22 2004-16-07

S 2002-19-10

Eurocopter France Air Tractor, Inc. Cessna Aircraft Company The New Piper Aircraft, Inc Agusta S.p.A. Sikorsky Aircraft Corp. General Electric Company

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Rotorcraft: EC155B and B1 AT-401, AT-401B, AT-402, AT-402A, AT-402B, AT-501, AT-502, AT-502A, AT-502B, AT-503A, AT-602, AT-802 and AT-802A 172R, 172S, 182S, 182T, T182T, 206H, T206H PA-46-500TP Rotorcraft: A109K2 Rotorcraft: S-61L, S-61N, S-61-NM, and S-61R Engine: CT7-2D1 Turboshaft

SMALL AIRCRAFT, ROTORCRAFT, GLIDERS, BALLOONS, & AIRSHIPS AD No.

Information

Manufacturer

Applicability

Info: E - Emergency; COR - Correction; S - Supersedes; R - Revision; - See AD for additional information; Biweekly 2004-17 2004-14-12 2004-16-08 2004-16-14

COR

2004-16-15 2004-17-01 2004-17-02 2004-17-03

The New Piper Aircraft, Inc. MD Helicopters Thales Avionics Eurocopter France

S 2002-22-17 S 2003-16-10

Cessna Aircraft Company Raytheon Aircraft Company Pratt & Whitney Canada

See AD Rotorcraft: MD900 Appliance: Traffic advisory/resolution advisory (TA/RA) vertical speed indicator-traffic alert and collision avoidance system (VSITCAS) indicators Rotorcraft: AS-365N2, AS 365 N3, EC 155B, EC155B1, SA365N, N1 and SA-366G1 208 and 208B See AD Engine: PW206A and PW206E

Biweekly 2004-18 2004-17-04

S 2001-26-25

2004-18-01

Grob-Werke Gmbh & Co KG Hoffmann Propeller GmbH & Co KG

Sailplane: G102 CLUB ASTIR III, G102 CLUB ASTIR IIIb, and G102 STANDARD ASTIR III Propeller: HO-V343 and HO-V343K

Biweekly 2004-19 2004-18-12 2004-19-01

S 86-26-04

DG Flugzeugbau GmbH Cessna Aircraft Company

Glider: DG-500MB See AD

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BW 2004-19 DG FLUGZEUGBAU GMBH AIRWORTHINESS DIRECTIVE SMALL AIRCRAFT, ROTORCRAFT, GLIDERS, BALLOONS, & AIRSHIPS 2004-18-12 DG Flugzeugbau GmbH: Amendment 39-13790; Docket No. 2004-CE-06-AD. When Does This AD Become Effective? (a) This AD becomes effective on October 22, 2004. What Other ADs Are Affected by This Action? (b) None. What Sailplanes Are Affected by This AD? (c) This AD affects the following sailplane models and serial numbers that are certificated in any category: DG Flugzeugbau Model DG-500MB, all serial numbers up to and including 5E220B15. What Is the Unsafe Condition Presented in This AD? (d) This AD is the result of Warner LA10 spindle drive failure. The actions specified in this AD are intended to prevent failure of the Warner LA10 spindle drive, which could result in failure of the engine pylon extension/retraction mechanism. This condition could cause an unstable engine pylon assembly during flight with consequent loss of control of the sailplane. What Must I Do To Address This Problem? (e) To address this problem, you must do the following: Actions Replace the Warner LA10 spindle drive with the Stross BSA 10 spindle drive and make any necessary electrical modifications including installation of the voltage converter for the brake of the spindle drive.

Compliance Replace and modify within 25 hours time-inservice (TIS) after October 22, 2004 (the effective date of this AD).

Procedures Follow the instructions in DG Flugzeugbau GmbH Technical Note No. 843/18 June 25, 2003.

May I Request an Alternative Method of Compliance? (f) You may request a different method of compliance or a different compliance time for this AD by following the procedures in 14 CFR 39.19. Unless FAA authorizes otherwise, send your request to your principal inspector. The principal inspector may add comments and will send your request to the Manager, Standards Office, Small Airplane Directorate, FAA. For information on any already approved alternative methods of compliance, contact Gregory Davison, Aerospace Engineer, FAA, Small Airplane Directorate, ACE-112, Room 301, 901 Locust, Kansas City, Missouri 64106; telephone: 816-329-4130; facsimile: 816-329-4090. 7

2004-18-12 2

Does This AD Incorporate Any Material by Reference? (g) You must do the actions required by this AD following the instructions in DG Flugzeugbau GmbH Technical Note No. 843/18 issue 2, dated June 25, 2003. The Director of the Federal Register approved the incorporation by reference of this service bulletin in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. You may get a copy from DG Flugzeugbau, Postbox 41 20, 76625 Bruchsal, Germany. You may review copies at FAA, Central Region, Office of the Regional Counsel, 901 Locust, Room 506, 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_regulations/ibr_locations.html. Is There Other Information That Relates to This Subject? (h) LBA airworthiness directive 2003-409, dated December 9, 2003, and Technical Note No. 843/18, issue 2, dated June 25, 2003, also address the subject of this AD. Issued in Kansas City, Missouri, on August 31, 2004. Dorenda D. Baker, Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 04-20310 Filed 9-13-04; 8:45 am] BILLING CODE 4910-13-P

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BW 2004-19 CESSNA AIRCRAFT COMPANY AIRWORTHINESS DIRECTIVE SMALL AIRCRAFT, ROTORCRAFT, GLIDERS, BALLOONS, & AIRSHIPS CORRECTION: The AD number of Amendment 39-13795 is incorrect as published in the Federal Register (FR) today, September 17, 2004. The AD number should be 2004-19-01. We will issue a correction to the FR in the near future. We have corrected this copy. 2004-19-01 Cessna Aircraft Company: Amendment 39-13795; Docket No. 2003-CE-40-AD; Supersedes AD 86-26-04, Amendment 39-5503. When Does This AD Become Effective? (a) This AD becomes effective on November 1, 2004. What Other ADs Are Affected by This Action? (b) This AD supersedes AD 86-26-04, Amendment 39-5503. What Airplanes Are Affected by This AD? (c) This AD affects the following airplane models and serial numbers that are certificated in any category and incorporate one of the Cessna accessory kits specified in paragraph (d) of this AD. Model (1) 120 (2) 140 (3) 140A (4) 150 (5) 150A (6) 150B (7) 150C (8) 150D (9) 150E (10) 150F (11) 150G (12) 150H (13) 150J (14) 150K (15) 170 (16) 170A (17) 170B (18) 172 (19) 172A (20) 172B

Serial number 8000 through 15075. 8000 through 15075. 15200 through 15724. 617, 17001 through 17999, and 59001 through 59018. 628 and 15059019 through 15059350. 15059351 through 15059700. 15059701 through 15060087. 15060088 through 15060772. 644 and 15060773 through 15061532. 15061533 through 15064532. 15064533 through 15064969 and 15064971 through 15067198. 649 and 15067199 through 15069308. 15069309 through 15071128. 15071129 through 15072003. 18000 through 18729. 18730 through 19400 and 19402 through 20266. 20267 through 20999 and 25000 through 27169. 610, 612, 615, 28000 through 29999, 36000 through 36999, and 46001 through 46754. 622, 625, and 46755 through 47746. 630 and 17247747 through 17248734. 9

2004-19-01 2

(21) 172C (22) 172D (23) 172E (24) 172F (25) 172G (26) 172H (27) 172I (28) 172K (29) P172D (30) 175 (31) 175A (32) 175B (33) 175C (34) 177 (35) 177A (36) 177B (37) 180 (38) 180A (39) 180B (40) 180C (41) 180D (42) 180E (43) 180F (44) 180G (45) 180H (46) 182 (47) 182A (48) 182B (49) 182C (50) 182D (51) 182E (52) 182F (53) 182G (54) 182H (55) 182J (56) 182K (57) 182L (58) 182M (59) 182N (60) 185 (61) 185A (62) 185B (63) 185C (64) 185D (65) 185E (66) A185E (67) 190 (68) 195

17248735 through 17249544. 17249545 through 17250572. 639 and 17250573 through 17251822. 17251823 through 17253392. 17253393 through 17254892. 638, 17254893 through 17256492, and 17256494 through 17256512. 17256513 through 17257161. 17257162 through 17258486 and 17258487 through 17259223. P17257120 through P17257188. 626, 640, 28700A, and 55001 through 56238. 619 and 56239 through 56777. 17556778 through 17557002. 17557003 through 17557119. 661, 17700001, and 17700003 through 17701164. 17701165 through 17701370. 17701371 through 17701471 and 17701473 through 17701530. 604, 614, 30000 through 32661. 32662 through 32999 and 50001 through 50355. 50356 through 50661. 624 and 50662 through 50911. 18050912 through 18051063. 18051064 through 18051183. 18051184 through 18051312. 18051313 through 18051445. 18051446 through 18052175. 613 and 33000 through 33842. 33843 through 34753, 34755 through 34999, and 51001 through 51556. 34754, 51557 through 51622, and 51624 through 52358. 631 and 52359 through 53007. 51623 and 18253008 through 18253598. 18253599 through 18254423. 18254424 through 18255058. 18255059 through 18255844. 634 and 18255846 through 18256684. 18256685 through 18257625. 18255845, 18257626 through 18257698, and 18257700 through 18258505. 18258506 through 18259305. 662, 18257699, and 18259306 through 18260055. 18260056 through 18260445. 632 and 185–0001 through 185–0237. 185–0238 through 185–0512. 185–0513 through 185–0653. 185–0654 through 185–0776. 185–0777 through 185–0967. 185–0968 through 185–1149. 185–0968 through 185–1599 and 18501600 through 18501832. 7001 through 7999 and 16000 through 16183. 7001 through 7999 and 16000 through 16183. 10

2004-19-01 3

(69) 206 (70) P206 (71) P206A (72) P206B (73) P206C (74) P206D (75) P206E (76) U206 (77) U206A (78) U206B (79) U206C (80) U206D (81) TP206A (82) TP206B (83) TP206C (84) TP206D (85) TP206E (86) TU206A (87) TU206B (88) TU206C (89) TU206D (90) 207 (91) T207 (92) 210 (93) 210–5 (205) (94) 210–5 (205A) (95) 210A (96) 210B (97) 210C (98) 210D (99) 210E (100) 210F (101) 210G (102) 210H (103) 210J (104) 210K (105) T210F (106) T210G (107) T210H (108) T210J (109) T210K (110) F150G (111) F150H (112) F150J (113) F150K

206–0001 through 206–0275. P206–0001 through P206–0160. P206–0161 through P206–0306. P206–0307 through P206–0419. P206–0420 through P206–0519. P206–0520 through P206–0603. P20600604 through P20600647. U206–0276 through U206–0437. U206–0438 through U206–0656. U206–0657 through U206–0914. U206–0915 through U206–1234. U206–1235 through U206–1444 and U20601445 through U20601587. P206–0161 through P206–0306. P206–0307 through P206–0419. P206–0420 through P206–0519. P206–0520 through P206–0603. P20600604 through P20600647. U206–0487 through U206–0656. U206–0657 through U206–0914. U206–0915 through U206–1234. U206–1235 through U206–1444 and U20601445 through U20601587. 20700001 through 20700190. 20700001 through 20700190. 618 and 57001 through 57575. 641, 648, and 205–0001 through 205–0480. 205–0481 through 205–0577. 616 and 21057576 through 21057840. 21057841 through 21058085. 21058086 through 21058139 and 21058141 through 21058220. 21058221 through 21058510. 21058511 through 21058715. 21058716 through 21058818. 21058819 through 21058936. 21058937 through 21059061. 21059062 through 21059199. 21059200 through 21059351. T210–0001 through T210–0197. T210–0198 through T210–0307. T210–0308 through T210–0392. T210–0393 through T210–0454. 21059200 through 21059351. F150–0068 through F150–0219. F150–0220 through F150–0389. F150–0390 through F150–0529. F15000530 through F15000658. 11

2004-19-01 4

(114) F172D (115) F172E (116) F172F (117) F172G (118) F172H (119) FR172E (120) FR172F (121) FR172G (122) 336 (123) 337 (124) 337A (125) 337B (126) 337C (127) 337D (128) 337E (129) T337B (130) T337C (131) T337D (132) T337E

F172–0001 through F172–0018. F172–0019 through F172–0085. F172–0086 through F172–0179. F172–0180 through F172–0319. F172–0320 through F172–0654 and F17200655 through F17200754. FR17200001 through FR17200060. FR17200061 through FR17200145. FR17200146 through FR17200225. 633, 636, and 336–0001 through 336–0195. 647 and 337–0002 through 337–0239. 337–0240 through 337–0305, 337–0307 through 337–0469, and 337–0471 through 337–0525. 656, 337–0001, 337–0470, 337–0526 through 337–0568, and 337–0570 through 337– 0755. 337–0756 through 337–0978. 337–0979 through 337–1193. 33701194 through 33701316. 337–0001, 337–0470, 337–0526 through 337–0568, and 37–0570 through 337–0755. 337–0756 through 337–0978. 337–0979 through 337–1193. 33701194 through 33701316.

What Cessna Accessory Kits Are Affected by This AD? (d) The following is a list of the affected Cessna accessory kits: CESSNA ACCESSORY KIT AK140–10 AK150–7 AK150–121 AK170–10 AK177–10 AK182–75 AK195–10 AK210–77 AK210–93 AK210–171 AK210–172 AK210–173 AK210–174 AK336–32 AK336–36 AK336–103 Note: Retainer springs, part number (P/N) 443030-401, used in Cessna service kits are not affected by this AD.

12

2004-19-01 5

What Is the Unsafe Condition Presented in This AD? (e) The actions specified in this AD are intended to prevent slippage of the pilot/co-pilot shoulder harness, which could result in failure of the shoulder harness to maintain proper belt length adjustment and tension. This failure could result in pilot/co-pilot injury. What Must I Do To Address This Problem? (f) To address this problem, you must do the following: Actions (1) Inspect only the upper shoulder harness adjuster (part number (P/N) 443030–401) for the presence of a retainer spring.

Compliance Within the next 25 hours time-in-service (TIS) after November 1, 2004 (the effective date of this AD). (2) If a retainer spring is found during Prior to further flight the inspection of the upper shoulder after the inspection harness adjuster (P/N 443030–401) required in paragraph required in paragraph (f)(1) of this AD: (f)(1) of this AD. (i) Remove the spring by cutting each side; and (ii) stamp out the –401 identification number. (3) If a retainer spring is not found Prior to further flight during the inspection of the upper after the inspection shoulder harness adjuster (P/N required in paragraph 443030–401) required in paragraph (f)(1) of this AD. (f)(1) of this AD, make an entry in the airplane log book showing compliance with this AD. (4) Only incorporate Cessna Accessory As of November 1, Kits identified in paragraph (d) of this 2004 (the effective AD that have been inspected and date of this AD). modified in accordance with paragraphs (f)(1), (f)(2), (f)(2)(i), and (f)(2)(ii) of this AD.

Procedures Follow Cessna Single Engine Service Bulletin SEB86–8, Revision 1, and Cessna Multi-engine Service Bulletin MEB86–22, Revision 1, both dated July 28, 2003. Follow Cessna Single Engine Service Bulletin SEB86–8, Revision 1, and Cessna Multi-engine Service Bulletin MEB86–22, Revision 1, both dated July 28, 2003. Follow Cessna Single Engine Service Bulletin SEB86–8, Revision 1, and Cessna Multi-engine Service Bulletin MEB86–22, Revision 1, both dated July 28, 2003. Follow Cessna Single Engine Service Bulletin SEB86–8, Revision 1, and Cessna Multi-engine Service bulletin MEB86–22, Revision 1, both dated July 28, 2003.

(g) If you did the actions of this AD using Cessna Single Engine Service Bulletin SEB86-8 and Cessna Multi-engine Service Bulletin MEB86-22, both dated November 21, 1986, no further action is required as long as you used shoulder harness adjuster, P/N 443030-401. May I Request an Alternative Method of Compliance? (h) You may request a different method of compliance or a different compliance time for this AD by following the procedures in 14 CFR 39.19. Unless FAA authorizes otherwise, send your request to your principal inspector. The principal inspector may add comments and will send your request to the Manager, Wichita Aircraft Certification Office (ACO), FAA. For information on any already approved alternative methods of compliance, contact Gary D. Park, Aerospace Engineer, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Mid-Continent Airport, Wichita, Kansas 67209; telephone: (316) 946-4123; facsimile: (316) 946-4107. 13

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Does This AD Incorporate Any Material by Reference? (i) You must do the actions required by this AD following the instructions in Cessna Single Engine Service Bulletin SEB86-8, Revision 1, and Cessna Multi-engine Service Bulletin MEB86-22, Revision 1, both dated July 28, 2003. The Director of the Federal Register approved the incorporation by reference of this service bulletin in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. You may get a copy from Cessna Aircraft Company, Product Support, P.O. Box 7706, Wichita, Kansas 67277; telephone: (316) 517-5800; facsimile: (316) 942-9006. You may review copies at FAA, Central Region, Office of the Regional Counsel, 901 Locust, Room 506, Kansas City, Missouri 64106; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. Issued in Kansas City, Missouri, on September 8, 2004. Dorenda D. Baker, Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 04-20774 Filed 9-16-04; 8:45 am] BILLING CODE 4910-13-P

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