Airworthiness Directive · Amendment 39-13795 · Cessna Aircraft Company 120, 140, 140A, 150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 206, P206, U206, TP206, TU206, 207, T207, 210, T210, 336, 337, and T337 Series Airplanes

AD 2004-19-04

Cessna Aircraft Company 120, 140, 140A, 150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 206, P206, U206, TP206, TU206, 207, T207, 210, T210, 336, 337, and T337 Series Airplanes

Airplane

Published: September 17, 2004
Effective: November 1, 2004
Maker: Cessna Aircraft Company
Supersedes: 86-26-04

Applies to

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	Serial number
(1) 120	8000 through 15075.
(2) 140	8000 through 15075.
(3) 140A	15200 through 15724.
(4) 150	617, 17001 through 17999, and 59001 through 59018.
(5) 150A	628 and 15059019 through 15059350.
(6) 150B	15059351 through 15059700.
(7) 150C	15059701 through 15060087.
(8) 150D	15060088 through 15060772.
(9) 150E	644 and 15060773 through 15061532.
(10) 150F	15061533 through 15064532.
(11) 150G	15064533 through 15064969 and 15064971 through 15067198.
(12) 150H	649 and 15067199 through 15069308.
(13) 150J	15069309 through 15071128.
(14) 150K	15071129 through 15072003.
(15) 170	18000 through 18729.
(16) 170A	18730 through 19400 and 19402 through 20266.
(17) 170B	20267 through 20999 and 25000 through 27169.
(18) 172	610, 612, 615, 28000 through 29999, 36000 through 36999, and 46001 through 46754.
(19) 172A	622, 625, and 46755 through 47746.
(20) 172B	630 and 17247747 through 17248734.
(21) 172C	17248735 through 17249544.
(22) 172D	17249545 through 17250572.
(23) 172E	639 and 17250573 through 17251822.
(24) 172F	17251823 through 17253392.
(25) 172G	17253393 through 17254892.
(26) 172H	638, 17254893 through 17256492, and 17256494 through 17256512.
(27) 172I	17256513 through 17257161.
(28) 172K	17257162 through 17258486 and 17258487 through 17259223.
(29) P172D	P17257120 through P17257188.
(30) 175	626, 640, 28700A, and 55001 through 56238.
(31) 175A	619 and 56239 through 56777.
(32) 175B	17556778 through 17557002.
(33) 175C	17557003 through 17557119.
(34) 177	661, 17700001, and 17700003 through 17701164.
(35) 177A	17701165 through 17701370.
(36) 177B	17701371 through 17701471 and 17701473 through 17701530.
(37) 180	604, 614, 30000 through 32661.
(38) 180A	32662 through 32999 and 50001 through 50355.
(39) 180B	50356 through 50661.
(40) 180C	624 and 50662 through 50911.
(41) 180D	18050912 through 18051063.
(42) 180E	18051064 through 18051183.
(43) 180F	18051184 through 18051312.
(44) 180G	18051313 through 18051445.
(45) 180H	18051446 through 18052175.
(46) 182	613 and 33000 through 33842.
(47) 182A	33843 through 34753, 34755 through 34999, and 51001 through 51556.
(48) 182B	34754, 51557 through 51622, and 51624 through 52358.
(49) 182C	631 and 52359 through 53007.
(50) 182D	51623 and 18253008 through 18253598.
(51) 182E	18253599 through 18254423.
(52) 182F	18254424 through 18255058.
(53) 182G	18255059 through 18255844.
(54) 182H	634 and 18255846 through 18256684.
(55) 182J	18256685 through 18257625.
(56) 182K	18255845, 18257626 through 18257698, and 18257700 through 18258505.
(57) 182L	18258506 through 18259305.
(58) 182M	662, 18257699, and 18259306 through 18260055.
(59) 182N	18260056 through 18260445.
(60) 185	632 and 185-0001 through 185-0237.
(61) 185A	185-0238 through 185-0512.
(62) 185B	185-0513 through 185-0653.
(63) 185C	185-0654 through 185-0776.
(64) 185D	185-0777 through 185-0967.
(65) 185E	185-0968 through 185-1149.
(66) A185E	185-0968 through 185-1599 and 18501600 through 18501832.
(67) 190	7001 through 7999 and 16000 through 16183.
(68) 195	7001 through 7999 and 16000 through 16183.
(69) 206	206-0001 through 206-0275.
(70) P206	P206-0001 through P206-0160.
(71) P206A	P206-0161 through P206-0306.
(72) P206B	P206-0307 through P206-0419.
(73) P206C	P206-0420 through P206-0519.
(74) P206D	P206-0520 through P206-0603.
(75) P206E	P20600604 through P20600647.
(76) U206	U206-0276 through U206-0437.
(77) U206A	U206-0438 through U206-0656.
(78) U206B	U206-0657 through U206-0914.
(79) U206C	U206-0915 through U206-1234.
(80) U206D	U206-1235 through U206-1444 and U20601445 through U20601587.
(81) TP206A	P206-0161 through P206-0306.
(82) TP206B	P206-0307 through P206-0419.
(83) TP206C	P206-0420 through P206-0519.
(84) TP206D	P206-0520 through P206-0603.
(85) TP206E	P20600604 through P20600647.
(86) TU206A	U206-0487 through U206-0656.
(87) TU206B	U206-0657 through U206-0914.
(88) TU206C	U206-0915 through U206-1234.
(89) TU206D	U206-1235 through U206-1444 and U20601445 through U20601587.
(90) 207	20700001 through 20700190.
(91) T207	20700001 through 20700190.
(92) 210	618 and 57001 through 57575.
(93) 210-5 (205)	641, 648, and 205-0001 through 205-0480.
(94) 210-5 (205A)	205-0481 through 205-0577.
(95) 210A	616 and 21057576 through 21057840.
(96) 210B	21057841 through 21058085.
(97) 210C	21058086 through 21058139 and 21058141 through 21058220.
(98) 210D	21058221 through 21058510.
(99) 210E	21058511 through 21058715.
(100) 210F	21058716 through 21058818.
(101) 210G	21058819 through 21058936.
(102) 210H	21058937 through 21059061.
(103) 210J	21059062 through 21059199.
(104) 210K	21059200 through 21059351.
(105) T210F	T210-0001 through T210-0197.
(106) T210G	T210-0198 through T210-0307.
(107) T210H	T210-0308 through T210-0392.
(108) T210J	T210-0393 through T210-0454.
(109) T210K	21059200 through 21059351.
(110) F150G	F150-0068 through F150-0219.
(111) F150H	F150-0220 through F150-0389.
(112) F150J	F150-0390 through F150-0529.
(113) F150K	F15000530 through F15000658.
(114) F172D	F172-0001 through F172-0018.
(115) F172E	F172-0019 through F172-0085.
(116) F172F	F172-0086 through F172-0179.
(117) F172G	F172-0180 through F172-0319.
(118) F172H	F172-0320 through F172-0654 and F17200655 through F17200754.
(119) FR172E	FR17200001 through FR17200060.
(120) FR172F	FR17200061 through FR17200145.
(121) FR172G	FR17200146 through FR17200225.
(122) 336	633, 636, and 336-0001 through 336-0195.
(123) 337	647 and 337-0002 through 337-0239.
(124) 337A	337-0240 through 337-0305, 337-0307 through 337-0469, and 337-0471 through 337-0525.
(125) 337B	656, 337-0001, 337-0470, 337-0526 through 337-0568, and 337-0570 through 337-0755.
(126) 337C	337-0756 through 337-0978.
(127) 337D	337-0979 through 337-1193.
(128) 337E	33701194 through 33701316.
(129) T337B	337-0001, 337-0470, 337-0526 through 337-0568, and 37-0570 through 337-0755.
(130) T337C	337-0756 through 337-0978.
(131) T337D	337-0979 through 337-1193.
(132) T337E	33701194 through 33701316.

The FAA's summary

The FAA adopts a new airworthiness directive (AD) that will supersede AD 86-26-04, which applies to certain Cessna Aircraft Company (Cessna) 120, 140, 140A, 150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 205, 205A, 206, P206, P206E, TP206A, TU206, TU206E, U206, U206E, 207, T207, 210, T210, 336, 337, and T337 series airplanes. AD 86-26-04 currently requires you to inspect and, if necessary, modify the pilot/co-pilot upper shoulder harness adjusters that have certain Cessna accessory kits incorporated. This AD is the result of reports that additional airplanes have the same unsafe condition and the manufacturer revised the service information to add these airplanes and correct the part number of the shoulder harness adjusters. Consequently, this AD retains the actions of 86-26-04, adds additional airplanes to the applicability section of this AD, and incorporates the revised service information. We are issuing this AD 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. Such failure could result in pilot/co- pilot injury.

What it requires

What Must I Do To Address This Problem?

To address this problem, you must do the following:

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

Filed under

The aircraft, engines and makers this AD names, by the model designations in its text. A model listed here may still be outside the AD's serial ranges.

Official sources

The Federal Register document · document 04-20774, the legal text
FAA Dynamic Regulatory System (DRS) · search 2004-19-04 for its current status and any corrections

Model

Serial number

(1) 120

8000 through 15075.

(2) 140

8000 through 15075.

(3) 140A

15200 through 15724.

(4) 150

617, 17001 through 17999, and 59001 through 59018.

(5) 150A

628 and 15059019 through 15059350.

(6) 150B

15059351 through 15059700.

(7) 150C

15059701 through 15060087.

(8) 150D

15060088 through 15060772.

(9) 150E

644 and 15060773 through 15061532.

(10) 150F

15061533 through 15064532.

(11) 150G

15064533 through 15064969 and 15064971 through 15067198.

(12) 150H

649 and 15067199 through 15069308.

(13) 150J

15069309 through 15071128.

(14) 150K

15071129 through 15072003.

(15) 170

18000 through 18729.

(16) 170A

18730 through 19400 and 19402 through 20266.

(17) 170B

20267 through 20999 and 25000 through 27169.

(18) 172

610, 612, 615, 28000 through 29999, 36000 through 36999, and 46001 through 46754.

(19) 172A

622, 625, and 46755 through 47746.

(20) 172B

630 and 17247747 through 17248734.

(21) 172C

17248735 through 17249544.

(22) 172D

17249545 through 17250572.

(23) 172E

639 and 17250573 through 17251822.

(24) 172F

17251823 through 17253392.

(25) 172G

17253393 through 17254892.

(26) 172H

638, 17254893 through 17256492, and 17256494 through 17256512.

(27) 172I

17256513 through 17257161.

(28) 172K

17257162 through 17258486 and 17258487 through 17259223.

(29) P172D

P17257120 through P17257188.

(30) 175

626, 640, 28700A, and 55001 through 56238.

(31) 175A

619 and 56239 through 56777.

(32) 175B

17556778 through 17557002.

(33) 175C

17557003 through 17557119.

(34) 177

661, 17700001, and 17700003 through 17701164.

(35) 177A

17701165 through 17701370.

(36) 177B

17701371 through 17701471 and 17701473 through 17701530.

(37) 180

604, 614, 30000 through 32661.

(38) 180A

32662 through 32999 and 50001 through 50355.

(39) 180B

50356 through 50661.

(40) 180C

624 and 50662 through 50911.

(41) 180D

18050912 through 18051063.

(42) 180E

18051064 through 18051183.

(43) 180F

18051184 through 18051312.

(44) 180G

18051313 through 18051445.

(45) 180H

18051446 through 18052175.

(46) 182

613 and 33000 through 33842.

(47) 182A

33843 through 34753, 34755 through 34999, and 51001 through 51556.

(48) 182B

34754, 51557 through 51622, and 51624 through 52358.

(49) 182C

631 and 52359 through 53007.

(50) 182D

51623 and 18253008 through 18253598.

(51) 182E

18253599 through 18254423.

(52) 182F

18254424 through 18255058.

(53) 182G

18255059 through 18255844.

(54) 182H

634 and 18255846 through 18256684.

(55) 182J

18256685 through 18257625.

(56) 182K

18255845, 18257626 through 18257698, and 18257700 through 18258505.

(57) 182L

18258506 through 18259305.

(58) 182M

662, 18257699, and 18259306 through 18260055.

(59) 182N

18260056 through 18260445.

(60) 185

632 and 185-0001 through 185-0237.

(61) 185A

185-0238 through 185-0512.

(62) 185B

185-0513 through 185-0653.

(63) 185C

185-0654 through 185-0776.

(64) 185D

185-0777 through 185-0967.

(65) 185E

185-0968 through 185-1149.

(66) A185E

185-0968 through 185-1599 and 18501600 through 18501832.

(67) 190

7001 through 7999 and 16000 through 16183.

(68) 195

7001 through 7999 and 16000 through 16183.

(69) 206

206-0001 through 206-0275.

(70) P206

P206-0001 through P206-0160.

(71) P206A

P206-0161 through P206-0306.

(72) P206B

P206-0307 through P206-0419.

(73) P206C

P206-0420 through P206-0519.

(74) P206D

P206-0520 through P206-0603.

(75) P206E

P20600604 through P20600647.

(76) U206

U206-0276 through U206-0437.

(77) U206A

U206-0438 through U206-0656.

(78) U206B

U206-0657 through U206-0914.

(79) U206C

U206-0915 through U206-1234.

(80) U206D

U206-1235 through U206-1444 and U20601445 through U20601587.

(81) TP206A

P206-0161 through P206-0306.

(82) TP206B

P206-0307 through P206-0419.

(83) TP206C

P206-0420 through P206-0519.

(84) TP206D

P206-0520 through P206-0603.

(85) TP206E

P20600604 through P20600647.

(86) TU206A

U206-0487 through U206-0656.

(87) TU206B

U206-0657 through U206-0914.

(88) TU206C

U206-0915 through U206-1234.

(89) TU206D

U206-1235 through U206-1444 and U20601445 through U20601587.

(90) 207

20700001 through 20700190.

(91) T207

20700001 through 20700190.

(92) 210

618 and 57001 through 57575.

(93) 210-5 (205)

641, 648, and 205-0001 through 205-0480.

(94) 210-5 (205A)

205-0481 through 205-0577.

(95) 210A

616 and 21057576 through 21057840.

(96) 210B

21057841 through 21058085.

(97) 210C

21058086 through 21058139 and 21058141 through 21058220.

(98) 210D

21058221 through 21058510.

(99) 210E

21058511 through 21058715.

(100) 210F

21058716 through 21058818.

(101) 210G

21058819 through 21058936.

(102) 210H

21058937 through 21059061.

(103) 210J

21059062 through 21059199.

(104) 210K

21059200 through 21059351.

(105) T210F

T210-0001 through T210-0197.

(106) T210G

T210-0198 through T210-0307.

(107) T210H

T210-0308 through T210-0392.

(108) T210J

T210-0393 through T210-0454.

(109) T210K

21059200 through 21059351.

(110) F150G

F150-0068 through F150-0219.

(111) F150H

F150-0220 through F150-0389.

(112) F150J

F150-0390 through F150-0529.

(113) F150K

F15000530 through F15000658.

(114) F172D

F172-0001 through F172-0018.

(115) F172E

F172-0019 through F172-0085.

(116) F172F

F172-0086 through F172-0179.

(117) F172G

F172-0180 through F172-0319.

(118) F172H

F172-0320 through F172-0654 and F17200655 through F17200754.

(119) FR172E

FR17200001 through FR17200060.

(120) FR172F

FR17200061 through FR17200145.

(121) FR172G

FR17200146 through FR17200225.

(122) 336

633, 636, and 336-0001 through 336-0195.

(123) 337

647 and 337-0002 through 337-0239.

(124) 337A

337-0240 through 337-0305, 337-0307 through 337-0469, and 337-0471 through 337-0525.

(125) 337B

656, 337-0001, 337-0470, 337-0526 through 337-0568, and 337-0570 through 337-0755.

(126) 337C

337-0756 through 337-0978.

(127) 337D

337-0979 through 337-1193.

(128) 337E

33701194 through 33701316.

(129) T337B

337-0001, 337-0470, 337-0526 through 337-0568, and 37-0570 through 337-0755.

(130) T337C

337-0756 through 337-0978.

(131) T337D

337-0979 through 337-1193.

(132) T337E

33701194 through 33701316.

Actions

Compliance

Procedures

(1) Inspect only the upper shoulder harness adjuster (part number (P/N) 443030-401) for the presence of a retainer spring

Within the next 25 hours time-in-service (TIS) after November 1, 2004 (the effective date of this AD)

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.

(2) If a retainer spring is found during the inspection of the upper shoulder harness adjuster (P/N 443030-401) required in paragraph (f)(1) of this AD: (i) Remove the spring by cutting each side; and (ii) stamp out the -401 identification number

Prior to further flight after the inspection required in paragraph (f)(1) of this AD

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.

(3) If a retainer spring is not found during the inspection of the upper shoulder harness adjuster (P/N 443030-401) required in paragraph (f)(1) of this AD, make an entry in the airplane log book showing compliance with this AD

Prior to further flight after the inspection required in paragraph (f)(1) of this AD

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.

(4) Only incorporate Cessna Accessory Kits identified in paragraph (d) of this AD that have been inspected and modified in accordance with paragraphs (f)(1), (f)(2), (f)(2)(i), and (f)(2)(ii) of this AD

As of November 1, 2004 (the effective date of this AD)

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.