Revision Transmittal

December 17, 2007

TO: Cessna Distributors and Single Engine Service Stations and CPC's

SUBJECT: Single Engine Service Bulletin SEB07-5 Revision 1, Pilot and Copilot Secondary Seat Stop

Installation.

REASON FOR REVISION

To remove all 188 model airplanes from the Effectivity section.

To revise the time of compliance from 200 hours of operation or 12 months to 400 hours of operation or 24

months, whichever occurs first.

To revise the copilot seat secondary stop installation compliance from mandatory to recommended.

To extend the credit expiration dates.

Miscellaneous changes as necessary.

REQUIRED ACTION

Please replace any copy of SEB07-5 with the attached copy of SEB07-5 Revision 1 which is printed in

its entirety.

NOTE: Compliance with Revision 1 is not required if in compliance with the Original Issue.

LOG OF EFFECTIVE PAGES

Page No. Date Page No. Date

1 December 17, 2007 10 December 17, 2007

2 December 17, 2007 11 December 17, 2007

3 December 17, 2007 12 December 17, 2007

4 December 17, 2007 13 December 17, 2007

5 December 17, 2007 14 December 17, 2007

6 December 17, 2007 15 December 17, 2007

7 December 17, 2007 16 December 17, 2007

8 December 17, 2007 17 December 17, 2007

9 December 17, 2007 18 December 17, 2007

*******

Page 1 of 1

To obtain satisfactory results, procedures specified in this publication must be accomplished in accordance with accepted methods and

prevailing government regulations. Cessna Aircraft Company cannot be responsible for the quality of work performed in accomplishing the

requirements of this publication.

Cessna Aircraft Company, Product Support, P.O. Box 7706, Wichita, Kansas 67277, U.S.A. (316) 517-5800, Facsimile (316) 942-9006

COPYRIGHT © 2007

Single Engine

Service Bulletin

December 17, 2007 SEB07-5

Revision 1

TITLE

PILOT AND COPILOT SECONDARY SEAT STOP INSTALLATION

EFFECTIVITY

Model Year Serial Numbers

170 1948 18000 thru 18729

170A 1949 thru 1951 18730 thru 19400

170A 1949 thru 1951 19402 thru 20266

170B 1952 thru 1956 20267 thru 20999

170B 1952 thru 1956 25000 thru 27169

170B 609, 19401

172 1956 thru 1959 28000 thru 29999

172 1956 thru 1959 36000 thru 36999

172 1956 thru 1959 46001 thru 46754

172 610, 612, 615

172A 1960 46755 thru 47746

172A 622, 625

172B 1961 17247747 thru 17248734

172B 630

172C 1962 17248735 thru 17249544

172D 1963 17249545 thru 17250572

172E 1964 17250573 thru 17251822

172E 639

172F 1965 17251823 thru 17253392

172G 1966 17253393 thru 17254892

172H 1967 17254893 thru 17256492

172H 1967 17256494 thru 17256512

172H 638

172I 1968 17256513 thru 17257161

172J 660

172K 1969 17257162 thru 17258486

Original Issue: May 14, 2007 Page 1 of 18

To obtain satisfactory results, procedures specified in this publication must be accomplished in accordance with accepted methods and

prevailing government regulations. Cessna Aircraft Company cannot be responsible for the quality of work performed in accomplishing the

requirements of this publication.

Cessna Aircraft Company, Product Support, P.O. Box 7706, Wichita, Kansas 67277, U.S.A. (316) 517-5800, Facsimile (316) 942-9006

COPYRIGHT © 2007
172K 1970 17258487 thru 17259223

172L 1971 17259224 thru 17259903

172L 1972 17259904 thru 17260758

172M 1973 17260759 thru 17261444

172M 1973 17261446 thru 17261577

172M 1973 17261579 thru 17261898

172M 17256493

172M 1974 17261899 thru 17263458

172M 1975 17263459 thru 17265684

172M 1976 17265685 thru 17267584

172N 1977 17267585 thru 17269309

172N 17261445

172N 1978 17269310 thru 17270049

172N 1978 17270051 thru 17271034

172N 17261578

172N 1979 17271035 thru 17272884

172N 1980 17272885 thru 17274009

172N 17270050

172P 1981 17274010 thru 17275034

172P 1982 17275035 thru 17275759

172P 1983 17275760 thru 17276079

172P 1984 17276080 thru 17276259

172P 1985 17276260 thru 17276516

172P 1986 17276517 thru 17276654

172Q 1983 17275869

172Q 1983 17275927 thru 17275934

172Q 1983 17275952, 17275959, 17275960

172Q 1983 17275962, 17275964, 17275965

172Q 1983 17275967, 17275968, 17275969

172Q 1983 17275971, 17275992, 17275999

172Q 1983 17276002, 17276005, 17276029

172Q 1983 17276032, 17276042, 17276045

172Q 1983 17276051, 17276052, 17276054

172Q 1984 17276101, 17276109, 17276140

172Q 1984 17276147, 17276188, 17276211

F172H 1968 F172-0432 thru F172-0435

175 1958 thru 1959 55001 thru 56238

175 28700A, 626, 640

175A 1960 56239 thru 56777

175A 619

175B 1961 17556778 thru 17557002

SEB07-5 Revision 1

Page 2 December 17, 2007
175C 1962 17557003 thru 17557119

P172D 1963 P17257120 thru P17257188

R172E (T41) 1967 thru 1968 R172-0001 thru R172-0335

R172F (T41) 1969 R172-0336 thru R172-0409

R172G (T41) 1969 thru 1970 R1720410 thru R1720444

R172H (T41) 1971 R1720445 thru R1720494

R172H (T41) 1972 R1720495 thru R1720546

R172H (T41) 1973 thru 1976 R1720547 thru R1720620

R172J 1974 P17257189

R172K 1977 R1722000 thru R1722724

R172K 1978 R1722725 thru R1722929

R172K 1979 R1722930 thru R1723199

R172K 680

R172K 1980 R1723200 thru R1723399

R172K 1981 R1723400 thru R1723454

172RG 1980 172RG0001 thru 172RG0570

172RG 1981 172RG0571 thru 172RG0890

172RG 691

172RG 1982 172RG0891 thru 172RG1099

172RG 1983 172RG1100 thru 172RG1144

172RG 1984 172RG1145 thru 172RG1177

172RG 1985 172RG1178 thru 172RG1191

177 1968 17700001

177 1968 17700003 thru 17701164

177 661

177A 1969 17701165 thru 17701370

177B 1970 17701371 thru 17701471

177B 1970 17701473 thru 17701530

177B 1971 17701531 thru 17701633

177B 17700002

177B 1972 17701634 thru 17701773

177B 1973 17701774 thru 17701973

177B 1974 17701974 thru 17702123

177B 1975 17702124 thru 17702313

177B 17701472

177B 1976 17702314 thru 17702522

177B 1977 17702523 thru 17702672

177B 1978 17702673 thru 17702752

177RG 1971 177RG0001 thru 177RG0212

177RG 1972 177RG0213 thru 177RG0282

177RG 1973 177RG0283 thru 177RG0418

SEB07-5 Revision 1

December 17, 2007 Page 3
177RG 1973 177RG0420 thru 177RG0432

177RG 1974 177RG0433 thru 177RG0592

177RG 1975 177RG0593 thru 177RG0787

177RG 1976 177RG0788 thru 177RG1051

177RG 1977 177RG1052 thru 177RG1266

177RG 1978 177RG1267 thru 177RG1366

177RG 177RG0419

180 1953 thru 1956 30000 thru 32661

180 604, 614

180A 1957 32662 thru 32999

180A 1957 thru 1958 50001 thru 50355

180B 1959 50356 thru 50661

180C 1960 50662 thru 50911

180C 624

180D 1961 18050912 thru 18051063

180E 1962 18051064 thru 18051183

180F 1963 18051184 thru 18051312

180G 1964 18051313 thru 18051445

180H 1965 thru 1972 18051446 thru 18052284

180H 645

180J 1973 thru 1976 18052285 thru 18052489

180J 1973 thru 1976 18052491 thru 18052770

180K 1977 18052771 thru 18052905

180K 1978 18052906 thru 18053000

180K 1979 18053001 thru 18053115

180K 18052490

180K 1980 18053116 thru 18053167

180K 1981 18053168 thru 18053203

182 1956 33000 thru 33842

182 613

182A 1957 33843 thru 34753

182A 1958 34755 thru 34999

182A 1958 51001 thru 51556

182B 1959 51557 thru 51622

182B 1959 51624 thru 52358

182B 34754

182C 1960 52359 thru 53007

182C 631

182D 1961 18253008 thru 18253598

182D 1961 51623

182E 1962 18253599 thru 18254423

SEB07-5 Revision 1

Page 4 December 17, 2007
182F 1963 18254424 thru 18255058

182G 1964 18255059 thru 18255844

182H 1965 18255846 thru 18256684

182H 634

182J 1966 18256685 thru 18257625

A182J 1966 A1820001 thru A1820056

A182K 1967 A1820057 thru A1820096

A182L 1968 A1820097 thru A1820116

A182N 1972 thru 1976 A1820117 thru A1820148

182K 1967 18257626 thru 18257698

182K 1967 18257700 thru 18258505

182K 1967 18255845

182L 1968 18258506 thru 18259305

182M 662

182M 1969 18259306 thru 18260055

182M 18257699

182N 1970 18260056 thru 18260445

182N 1971 18260446 thru 18260825

182P 1972 18260826 thru 18261425

182P 1973 18261426 thru 18262465

182P 1974 18262466 thru 18263475

182P 1975 18263476 thru 18263478

182P 1975 18263480 thru 18264295

182P 675

182P 1976 18264296 thru 18265175

182Q 1977 18265176 thru 18265965

182Q 1978 18265966 thru 18266590

182Q 18263479

182Q 1979 18266591 thru 18267300

182Q 1980 18267301

182Q 1980 18267303 thru 18267715

182R/T182 1981 18267716 thru 18268055

182R/T182 18267302

182R/T182 1982 18268056 thru 18268293

182R/T182 1983 18268294 thru 18268368

182R/T182 1984 18268369 thru 18268434

182R/T182 1985 18268435 thru 18268541

182R 1986 18268542 thru 18268586

R182 683

R182 1978 R18200002 thru R18200583

R182/TR182 1979 R18200584 thru R18201313

SEB07-5 Revision 1

December 17, 2007 Page 5
R182/TR182 R18200001

R182/TR182 1980 R18201314

R182/TR182 1980 R18201316 thru R18201628

R182/TR182 1981 R18201629 thru R18201798

R182/TR182 1982 R18201799 thru R18201928

R182/TR182 1983 R18201929 thru R18201973

R182/TR182 1984 R18201974 thru R18201999

R182/TR182 1985 R18202000 thru R18202031

R182/TR182 R18201315

R182/TR182 1986 R18202032 thru R18202039

185 1961 185-0001 thru 185-0237

185 632

185A 1962 185-0238 thru 185-0512

185B 1963 185-0513 thru 185-0653

185C 1964 185-0654 thru 185-0776

185D 1965 185-0777 thru 185-0967

185E 1966 185-0968 thru 185-1149

A185E 1966 185-0968 thru 185-1149

A185E 1967 185-1150 thru 185-1300

A185E 1968 185-1301 thru 185-1447

A185E 1969 185-1448 thru 185-1599

A185E 1970/1971 18501600 thru 18501934

A185E 1972 18501935 thru 18502090

A185F 1973 18502091 thru 18502299

A185F 1973 18502301 thru 18502310

A185F 652

A185F 1974 18502311 thru 18502565

A185F 1975 18502566 thru 18502838

A185F 1976 18502839 thru 18503153

A185F 1977 18503154 thru 18503458

A185F 1978 18503459 thru 18503683

A185F 1979 18503684 thru 18503938

A185F 18502300

A185F 1980 18503939 thru 18504138

A185F 1981 18504139 thru 18504328

A185F 1982 18504329 thru 18504394

A185F 1983 18504395 thru 18504415

A185F 1984 18504416 thru 18504424

A185F 1985 18504425 thru 18504448

190 1948 thru 1953 7004 thru 7999

190 1948 thru 1953 16000 thru 16183

SEB07-5 Revision 1

Page 6 December 17, 2007
195 1948 thru 1953 7004 thru 7999

195 1948 thru 1953 16000 thru 16183

195A 1948 thru 1953 7004 thru 7999

195A 1948 thru 1953 16000 thru 16183

195B 1948 thru 1953 7004 thru 7999

195B 1948 thru 1953 16000 thru 16183

210-5 (205) 1963 205-0001 thru 205-0480

210-5 (205) 641, 648

210-5 (205A) 1964 205-0481 thru 205-0577

206 1964 206-0001 thru 206-0275

U206 1965 U206-0276 thru U206-0437

U206A 1966 U206-0438 thru U206-0656

TU206A 1966 U206-0487 thru U206-0656

U206B/TU206B 1967 U206-0657 thru U206-0914

U206C/TU206C 1968 U206-0915 thru U206-1234

U206D/TU206D 1969 U206-1235 thru U206-1444

U206D/TU206D 1970 U20601445 thru U20601587

U206E/TU206E 1971 U20601588 thru U20601700

U206F/TU206F 1972 U20601701 thru U20601874

U206F/TU206F 1973 U20601875 thru U20602199

U206F/TU206F 1974 U20602200 thru U20602579

U206F/TU206F 1975 U20602580 thru U20602588

U206F/TU206F 1975 U20602590 thru U20603020

U206F/TU206F 1976 U20603021 thru U20603521

U206G/TU206G 1977 U20603522 thru U20604074

U206G/TU206G 676

U206G/TU206G 1978 U20604075 thru U20604649

U206G/TU206G 1979 U20604650 thru U20605309

U206G/TU206G U20602589

U206G/TU206G 1980 U20605310 thru U20605919

U206G/TU206G 1981 U20605920 thru U20606439

U206G/TU206G 1982 U20606440 thru U20606699

U206G/TU206G 1983 U20606700 thru U20606788

U206G/TU206G 1984 U20606789 thru U20606846

U206G/TU206G 1985 U20606847 thru U20606920

U206G/TU206G 1986 U20606921 thru U20607020

P206 1965 P206-0002 thru P206-0160

P206A 1966 P206-0161 thru P206-0306

TP206A 1966 P206-0161 thru P206-0306

P206B/TP206B 1967 P206-0307 thru P206-0419

P206C/TP206C 1968 P206-0420 thru P206-0519

SEB07-5 Revision 1

December 17, 2007 Page 7
P206D/TP206D 1969 P206-0520 thru P206-0603

P206E/TP206E 1970 P20600604 thru P20600647

P206E/TP206E P206-0001

207/T207 1969 20700001 thru 20700148

207/T207 1970 20700149 thru 20700190

207/T207 1971 20700191 thru 20700205

207/T207 1972 20700206 thru 20700215

207/T207 1973 20700216 thru 20700227

207/T207 1974 20700228 thru 20700267

207/T207 1975 20700268 thru 20700314

207/T207 1976 20700315 thru 20700362

207A/T207A 1977 20700363 thru 20700414

207A/T207A 1978 20700415 thru 20700482

207A/T207A 1979 20700483 thru 20700562

207A/T207A 1980 20700563 thru 20700654

207A/T207A 1981 20700655 thru 20700729

207A/T207A 1982 20700730 thru 20700762

207A/T207A 1983 20700763 thru 20700767

207A/T207A 1984 20700768 thru 20700788

210 1960 57001 thru 57575

210 618

210A 1961 21057576 thru 21057840

210A 616

210B 1962 21057841 thru 21058085

210C 1963 21058086 thru 21058139

210C 1963 21058141 thru 21058220

210D 1964 21058221 thru 21058510

210E 1965 21058511 thru 21058715

210F 1966 21058716 thru 21058818

210G 1967 21058819 thru 21058936

210H 1968 21058937 thru 21059061

210J 1969 21059062 thru 21059199

210K/T210K 1970 21059200 thru 21059351

210K/T210K 1971 21059352 thru 21059502

210L/T210L 1972 21059503 thru 21059719

210L/T210L 1973 21059720 thru 21060089

210L/T210L 1974 21060090 thru 21060539

210L/T210L 1975 21060540 thru 21061039

210L/T210L 1976 21061040 thru 21061041

210L/T210L 1976 21061043 thru 21061573

210M/T210M 1977 21061574 thru 21062273

SEB07-5 Revision 1

Page 8 December 17, 2007
210M/T210M 1978 21062274 thru 21062954

210M/T210M 1978 21061042

210N/T210N 1979 21062955 thru 21063640

210N/T210N 1980 21063641 thru 21064135

210N/T210N 1981 21064136 thru 21064535

210N/T210N 1982 21064536 thru 21064772

210N/T210N 1983 21064773 thru 21064822

210N/T210N 1984 21064823 thru 21064897

210R/T210R 1985 21064898 thru 21064949

210R/T210R 1986 21064950 thru 21065009

T210F 1966 T210-0001 thru T210-0197

T210G 1967 T210-0198 thru T210-0307

T210H 1968 T210-0308 thru T210-0392

T210J 1969 T210-0393 thru T210-0454

T210J 21058140

P210N 1978 P21000001 thru P21000150

P210N 1979 P21000151 thru P21000385

P210N 1980 P21000386 thru P21000590

P210N 1981 P21000591 thru P21000760

P210N 1982 P21000761 thru P21000811

P210N 1983 P21000812 thru P21000834

P210R 1985 P21000835 thru P21000866

P210R 1986 P21000867 thru P21000874

A182J 1966 A182-0001 thru A182-0056

A182K 1967 A182-0057 thru A182-0096

A182L 1968 A182-0097 thru A182-0116

A182N 1972 A182-0117 thru A182-0136

A182N 1974 A182-0137 thru A182-0146

A182N 1976 A182-0147 thru A182-0148

FP172 1963 FP172-0001 thru FP172-0003

F172D 1963 F172-0001 thru F172-0018

F172E 1964 F172-0019 thru F172-0085

F172F 1965 F172-0086 thru F172-0179

F172G 1966 F172-0180 thru F172-0319

F172H 1967 F172-0320 thru F172-0431

F172H 1967 F172-0436 thru F172-0442

F172H 1967 F172-0444 thru F172-0446

F172H 1968 F172-0432 thru F172-0435

F172H 1968 F172-0443

F172H 1968 F172-0447 thru F172-0559

F172H 1969 F172-0560 thru F172-0654

SEB07-5 Revision 1

December 17, 2007 Page 9
F172H 1970 F17200655 thru F17200754

F172K 1971 F17200755 thru F17200804

F172L 1972 F17200805 thru F17200904

F172M 1973 F17200905 thru F17201034

F172M 1974 F17201035 thru F17201234

F172M 1975 F17201235 thru F17201384

F172M 1976 F17201385 thru F17201514

F172N 1977 F17201515 thru F17201639

F172N 1978 F17201640 thru F17201749

F172N 1979 F17201750 thru F17201909

F172N 1980 F17201910 thru F17202039

F172P 1981 F17202040 thru F17202134

F172P 1982 F17202135 thru F17202194

F172P 1983 F17202195 thru F17202216

F172P 1984 F17202217 thru F17202233

F172P 1985 F17202234 thru F17202238

F172P 1986 F17202239 thru F17202254

FR172E 1968 FR17200001 thru FR17200060

FR172F 1969 FR17200061 thru FR17200145

FR172G 1970 FR17200146 thru FR17200225

FR172H 1971 FR17200226 thru FR17200275

FR172H 1972 FR17200276 thru FR17200350

FR172J 1973 FR17200351 thru FR17200440

FR172J 1974 FR17200441 thru FR17200530

FR172J 1975 FR17200531 thru FR17200559

FR172J 1976 FR17200560 thru FR17200590

FR172K 1977 FR17200591 thru FR17200620

FR172K 1978 FR17200621 thru FR17200630

FR172K 1979 FR17200631 thru FR17200655

FR172K 1980 FR17200656 thru FR17200665

FR172K 1981 FR17200666 thru FR17200675

F177RG 1971 F177RG0001 thru F177RG0042

F177RG 1972 F177RG0043 thru F177RG0062

F177RG 1973 F177RG0063 thru F177RG0092

F177RG 1974 F177RG0093 thru F177RG0122

F177RG 1975 F177RG0123 thru F177RG0138

F177RG 1976 F177RG0139 thru F177RG0160

F177RG 1977 F177RG0161 thru F177RG0177

F182P 1976 F18200001 thru F18200025

F182Q 1977 F18200026 thru F18200064

F182Q 1978 F18200065 thru F18200094

SEB07-5 Revision 1

Page 10 December 17, 2007
F182Q 1979 F18200095 thru F18200129

F182Q 1980 F18200130 thru F18200169

FR182 1978 FR18200001 thru FR18200020

FR182 1979 FR18200021 thru FR18200045

FR182 1980 FR18200046 thru FR18200070

PURPOSE

To provide a modification for installing a new design secondary seat stop for the pilot and copilot seats.

The secondary seat stop is designed to assist in providing an additional margin of safety by limiting the aft

travel of the seat in the event the primary latch pin is not properly engaged in the seat rail/track. In certain

instances, seat slippage could result in some pilots not being able to reach all the controls and/or subsequently

losing control of the airplane.

COMPLIANCE

Mandatory: Pilot seat secondary stop installation shall be accomplished within the next 400 hours of operation

or 24 months, whichever occurs first.

Recommended: Copilot seat secondary stop installation should be accomplished within the next 400 hours

of operation or 24 months, whichever occurs first.

NOTE: This Service Bulletin supersedes Service Bulletin SEB89-2: Pilot Seat Secondary Stop Installation (all

revisions).

Compliance with Revision 1 is not required if in compliance with the Original Issue.

APPROVAL

FAA approval has been obtained on technical data in this publication that affects airplane type design.

SEB07-5 Revision 1

December 17, 2007 Page 11
MAN-HOURS

The man-hours listed below are based on the work being accomplished during a scheduled 100 hour/annual

type inspection.

SK195-11: Pilot Secondary Seat Stop Installation

6.7 man-hours per airplane

SK195-12: Copilot Secondary Seat Stop Installation

Approximately 6.2 man-hours per airplane

SK210-174A: Pilot Secondary Seat Stop Installation

Installation "A": 3.5 man-hours per airplane

Installation "B": 3.4 man-hours per airplane

Installation "C": 1.5 man-hours per airplane

Installation "D": 2.9 man-hours per airplane

Installation "E": 2.2 man-hours per airplane

Installation "F": 2.0 man-hours per airplane

Installation "G": 2.4 man-hours per airplane

Installation "H": 2.4 man-hours per airplane

Installation "J": 5.4 man-hours per airplane

Installation "K": 3.6 man-hours per airplane

SK210-175: Copilot Secondary Seat Stop Installation

Installation "A": Approximately 3.0 man-hours per airplane

Installation "B": Approximately 2.9 man-hours per airplane

Installation "C": Approximately 1.0 man-hour per airplane

Installation "D": Approximately 2.4 man-hours per airplane

Installation "E": Approximately 1.7 man-hours per airplane

Installation "F": Approximately 1.5 man-hours per airplane

Installation "G": Approximately 1.9 man-hours per airplane

Installation "H": Approximately 1.9 man-hours per airplane

Installation "J": Approximately 4.9 man-hours per airplane

Installation "K": Approximately 3.1 man-hours per airplane

SEB07-5 Revision 1

Page 12 December 17, 2007
MATERIAL

The parts below are available from Cessna Parts Distribution through an appropriate Cessna Service Station

for the suggested list price shown.

NOTE: The airplane serial number must be provided when ordering the seat stop service kits.

Part Number Description Qty/Airplane Price

SK195-11 Pilot Secondary Seat

Stop Installation Kit

(Models 190/195)

1 $ 131.00 (N) ea

SK195-12 Copilot Secondary

Seat Stop Installation

Kit (Models 190/195)

1 $ 131.00 (N) ea

SK210-174A Pilot Secondary Seat

Stop Installation Kit

(Models 170-P210

except Models

190/195)

1 $ 153.11 (N) ea

SK210-175 Copilot Secondary

Seat Stop Installation

Kit (Models 170-P210

except Models

190/195)

1 $ 153.11 (N) ea

U000787S EC1300LP Adhesive

(1 Pint)

(as required) $ 29.70 (VR) ea

ALL PRICES SUBJECT TO CHANGE WITHOUT NOTICE

ACCOMPLISHMENT INSTRUCTIONS

Service Kit installation instructions are included in the following Service Kits when the kits are shipped from

Cessna Parts Distribution.

SK195-11 and SK210-174A: Pilot Secondary Seat Stop Installation; SK195-12 and SK210-175: Copilot

Secondary Seat Stop Installation.

For your convenience the typical installation of the secondary seat stop installation configurations are shown

in Figure 1.

NOTE: This information shall be considered an amendment to the Cessna Manufacturer's Service/Maintenance

Manual or Instructions for continued airworthiness and must be accomplished for ongoing airworthiness

compliance as required per 14 CFR Part 43.13.

SEB07-5 Revision 1

December 17, 2007 Page 13
CREDIT

Applicable Service Kit parts credit and applicable labor allowance credit, as listed in the Man-Hours section

of this Service Bulletin, will be provided per airplane to install Service Kits SK195-11 and SK210-174A: Pilot

Secondary Seat Stop Installation.

When applicable, freight will be credited at the most economical method unless pre-approved by Cessna. For

pre-approval contact Cessna Parts Distribution Warranty Administration at Telephone: 316-831-4296, Fax:

316-206-2746 or E-mail: cpd2claims@cessna.textron.com.

To receive credit, the work must be completed and a Warranty Claim submitted by a Cessna Single Engine

Service Station within 30 calendar days of Service Bulletin compliance before the credit expiration dates

shown below.

NOTE: A copy of the logbook entries and applicable FAA Form 8130-3, Airworthiness Approval Tag that

was shipped with the Service Kit will be required that shows installation of the applicable Service Kit

and shall be included with the Warranty Claim.

Domestic . . . . . . . . . . . . . . . . . December 17, 2009

International . . . . . . . . . . . . . . . December 17, 2009

OWNER NOTIFICATION

A. On May 14, 2007 the following Owner Advisory message was sent to applicable owners of

record in SEB07-5A.

Dear Cessna Owner:

This Owner Advisory is to inform you that SEB07-5: Pilot and Copilot Secondary Seat Stop

Installation has been issued to announce that Service Kits are available to install a new design

secondary seat stop for the pilot and copilot seats.

The secondary seat stop is designed to assist in providing an additional margin of safety by

limiting the aft travel of the seat in the event the primary latch pin is not properly engaged in the

seat rail/track. In certain instances, seat slippage could result in some pilots not being able to

reach all the controls and/or subsequently losing control of the airplane.

Compliance is mandatory: shall be accomplished within the next 200 hours of operation or

12 months, whichever occurs first.

NOTE: This Service Bulletin supersedes Service Bulletin SEB89-2: Pilot Seat Secondary Stop

Installation (all revisions).

The information contained in the referenced Cessna Service Bulletin shall be considered an

amendment to the Cessna Manufacturer's Service/Maintenance Manual or Instructions for

continued airworthiness, and must be accomplished for ongoing airworthiness compliance in

accordance with 14 CFR Part 43.13.

Applicable Service Kit parts credit and applicable labor allowance credit, as listed in the

Man-Hours section of Service Bulletin SEB07-5, will be provided per airplane to install Service

Kits SK195-11 and SK210-174: Pilot Secondary Seat Stop Installation.

To receive credit, the work must be completed and a Warranty Claim submitted by a Cessna

Single Engine Service Station within 30 calendar days of Service Bulletin compliance before the

credit expiration dates shown below.

Domestic . . . . . . . . . . . . . . . . . . . . . . May 14, 2009

International . . . . . . . . . . . . . . . . . . . . May 14, 2009

Please contact a Cessna Single Engine Service Station for detailed information and arrange to

have Cessna Service Bulletin SEB07-5 accomplished on your airplane.

SEB07-5 Revision 1

Page 14 December 17, 2007
B. On December 17, 2007 the following Owner Advisory message will be sent to applicable owners

of record in SEB07-5R1A.

Dear Cessna Owner:

This Owner Advisory is to inform you that Service Bulletin SEB07-5 Revision 1: Pilot and Copilot

Secondary Seat Stop Installation has been issued to announce that Service Kits are available to

install a new design secondary seat stop for the pilot and copilot seats.

The secondary seat stop is designed to assist in providing an additional margin of safety by

limiting the aft travel of the seat in the event the primary latch pin is not properly engaged in the

seat rail/track. In certain instances, seat slippage could result in some pilots not being able to

reach all the controls and/or subsequently losing control of the airplane.

Compliance is mandatory for the pilot seat: the secondary seat stop installation shall be

accomplished within the next 400 hours of operation or 24 months, whichever occurs first.

Compliance is recommended for the copilot seat: the secondary seat stop installation should be

accomplished within the next 400 hours of operation or 24 months, whichever occurs first.

NOTE: This Service Bulletin supersedes Service Bulletin SEB89-2: Pilot Seat Secondary Stop

Installation (all revisions).

Compliance with SEB07-5 Revision 1 is not required if in compliance with the Original

Issue of SEB07-5.

The information contained in the referenced Cessna Service Bulletin shall be considered an

amendment to the Cessna Manufacturer's Service/Maintenance Manual or Instructions for

continued airworthiness, and must be accomplished for ongoing airworthiness compliance in

accordance with 14 CFR Part 43.13.

Applicable Service Kit parts credit and applicable labor allowance credit, as listed in the

Man-Hours section of Service Bulletin SEB07-5, will be provided per airplane to install Service

Kits SK195-11 and SK210-174A: Pilot Secondary Seat Stop Installation.

To receive credit, the work must be completed and a Warranty Claim submitted by a Cessna

Multi-engine Service Station within 30 calendar days of Service Bulletin compliance before the

credit expiration dates shown below.

Domestic . . . . . . . . . . . . . . . . . December 17, 2009

International . . . . . . . . . . . . . . . December 17, 2009

Please contact a Cessna Single Engine Service Station for detailed information and arrange to

have Cessna Service Bulletin SEB07-5 Revision 1 accomplished on your airplane.

*******

SEB07-5 Revision 1

December 17, 2007 Page 15
Figure 1. Identification of Secondary Seat Stop Installation Configurations (Sheet 1)

SEB07-5 Revision 1

Page 16 December 17, 2007
Figure 1. Identification of Secondary Seat Stop Installation Configurations (Sheet 2)

SEB07-5 Revision 1

December 17, 2007 Page 17
Figure 1. Identification of Secondary Seat Stop Installation Configurations (Sheet 3)

SEB07-5 Revision 1

Page 18 December 17, 2007