# 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 fi rst. 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

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Page 1 of 1 To obtain satisfactory results, procedures speci fi ed 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 COP ILOT SECONDARY SEAT STOP INSTALLATION

**EFFECTIVIT Y**  M o d e l Y e a r S e ri a l N u m b e rs 170 1948 18000 thru 1 8729 170A 1949 thru 1951 18730 thru 19400 170A 1949 thru 1951 19402 thru 20266 170B 1952 thru 1 956 20267 thru 20999 170B 1952 thru 1956 25000 thru 27169 170B 609, 19401 172 1956 thru 1959 28000 thr u 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 172495 45 thru 17250572 172E 1964 17250573 thru 17251822 172E 639 172F 1965 17251 823 thru 17253392 172G 1966 17253393 thru 17254892 172H 1967 17254893 thru 17256492 172H 1967 1725 6494 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 speci fi ed 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 © 2007172K 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 th ru 17263458 172M 1975 17263459 thru 17265684 172M 1976 17265685 thru 17267584 172N 1977 17267585 th ru 17269309 172N 17261445 172N 1978 17269310 thru 17270049 172N 1978 17270051 t hru 17271034 172N 17261578 172N 1979 17271035 thru 17272884 172N 1980 17272885 thru 17274009 172N 17270050 172P 1981 17274010 thru 17275034 172P 1982 1727503 5 thru 17275759 172P 1983 17275760 thru 17276079 172P 1984 17276080 thru 17276259 172P 1985 172762 60 thru 17276516 172P 1986 17276517 thru 17276654 172Q 1983 17275869 172Q 1983 17275 927 thru 17275934 172Q 1983 17275952, 17275959, 17275960 172Q 1983 17275962, 17275964, 17275965 172Q 1983 17275 967, 17275968, 17275969 172Q 1983 17275971, 17275992, 17275999 172Q 1983 17276002, 17276005, 17276029 172Q 1983 1727 6032, 17276042, 17276045 172Q 1983 17276051, 17276052, 17276054 172Q 1984 17276101, 17276109, 17276140 172 Q 1984 172 76147, 17276188, 17276211 F172H 1968 F172-0432 thru F172-0435 175 1958 thru 1959 55001 thru 56238 175 28 700A, 626, 640 175A 1960 56239 thru 56777 175A 619 175B 19 61 17556778 thru 17557002

SEB07-5 Revision 1 Page 2 December 17, 2007175C 1962 17557003 thru 17557119 P172D 1963 P17257120 thr u 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 19 76 R1720547 th ru R1720620 R172J 1974 P17257189 R172K 1977 R1722000 thru R1722724 R172K 1978 R1722725 th ru R1722929 R172K 1979 R1722930 thru R1723199 R172K 680 R172K 1980 R1723200 t hru R1723399 R172K 1981 R1723400 thru R1723454 172RG 1980 172RG0001 thru 172RG0570 172RG 1981 172RG057 1 thru 172RG0890 172RG 691 172RG 1982 172RG0891 thru 172RG1099 172RG 1983 172RG11 00 thru 172RG1144 172RG 1984 172RG1145 thru 172RG1177 172RG 1985 172RG1178 thru 172RG1191 177 1968 177000 01 177 1968 17700003 thru 17701164 177 661 177A 1969 17701 165 thru 17701370 177B 1970 17701371 thru 17701471 177B 1970 17701473 thru 17701530 177B 1971 17701 531 thru 17701633 177B 17700002 177B 1972 17701634 thru 17701773 177B 1973 1770 1774 thru 17701973 177B 1974 17701974 thru 17702123 177B 1975 17702124 thru 17702313 177 B 177 01472 177B 1976 17702314 thru 17702522 177B 1977 17702523 thru 17702672 17 7B 19 78 17702673 thru 17702752 177RG 1971 177RG0001 thru 177RG0212 177RG 1972 177RG0213 thru 177RG0282 17 7RG 19 73 177RG0283 thru 177RG0418

SEB07-5 Revision 1 December 17, 2007 Page 3177RG 1973 177RG0420 thru 177RG0432 177RG 1974 177RG0433 thr u 177RG0592 177RG 1975 177RG0593 thru 177RG0787 177RG 1976 177RG0788 thru 177RG1051 177RG 1977 177RG1052 thr u 177RG1266 177RG 1978 177RG1267 thru 177RG1366 177RG 177RG0419 180 1953 thru 19 56 30000 thru 32661 180 604, 614 180A 1957 32662 thru 32999 180A 1957 thru 19 58 50001 thru 5 0355 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 180527 71 thru 18052905 180K 1978 18052906 thru 18053000 180K 1979 18053001 thru 18053115 180K 18052 490 180K 1980 18053116 thru 18053167 180K 1981 18053168 thru 18053203 182 1956 33000 thru 33842 182 613 182A 1957 33843 thru 34753 182A 1958 3475 5 thru 34999 182A 1958 51001 thru 51556 182B 1959 51557 thru 51622 182 B 195 9 51624 thru 52358 182B 34754 182C 1960 52359 thru 53007 182C 63 1 182D 1961 18253008 thru 18253598 182D 1961 51623 182E 19 62 18253599 thru 18254423

SEB07-5 Revision 1 Page 4 December 17, 2007182F 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 th ru A1820116 A182N 1972 thru 1976 A1820117 thru A1820148 182K 1967 18257626 thru 18257698 182K 1967 18257700 th ru 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 1826142 6 thru 18262465 182P 1974 18262466 thru 18263475 182P 1975 18263476 thru 18263478 182P 1975 182634 80 thru 18264295 182P 675 182P 1976 18264296 thru 18265175 182Q 1977 18265 176 thru 18265965 182Q 1978 18265966 thru 18266590 182Q 18263479 182Q 1979 18266 591 thru 18267300 182Q 1980 18267301 182Q 1980 18267303 thru 18267715 182R/T182 1981 1826 7716 thru 18268055 182R/T182 18267302 182R/T182 1982 18268056 thru 18268293 182 R/T182 198 3 182 68294 thru 18268368 182R/T182 1984 18268369 thru 18268434 182R/T182 1985 18268435 thru 18268541 18 2R 19 86 18268542 thru 18268586 R182 683 R182 1978 R18200002 thru R18200583 R1 82/TR182 19 79 R1 8200584 thru R18201313

SEB07-5 Revision 1 December 17, 2007 Page 5R182/TR182 R18200001 R182/TR182 1980 R18201314 R182/TR182 1980 R18201316 thru R18201628 R182/TR182 1981 R18201629 thru R18201798 R182/TR182 1982 R18201799 thr u R18201928 R182/TR182 1983 R18201929 thru R18201973 R182/TR182 1984 R18201974 thru R18201999 R182/TR182 1985 R18202000 t hru R18202031 R182/TR182 R18201315 R182/TR182 1986 R18202032 thru R18202039 185 1961 185-0001 th ru 185-0237 185 632 185A 1962 185-0238 thru 185-0512 185B 1963 185-0513 t hru 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 185-130 1 thru 185-1447 A185E 1969 185-1448 thru 185-1599 A185E 1970/1971 18501600 thru 18501934 A185E 1972 185019 35 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 18502 839 thru 18503153 A185F 1977 18503154 thru 18503458 A185F 1978 18503459 thru 18503683 A185 F 1979 1850 3684 thru 18503938 A185F 18502300 A185F 1980 18503939 thru 18504138 A18 5F 198 1 185 04139 thru 18504328 A185F 1982 18504329 thru 18504394 A185F 1983 18504395 thru 18504415 A1 85F 19 84 18 504416 thru 18504424 A185F 1985 18504425 thru 18504448 190 1948 thru 1953 7004 thru 7999 19 0 1948 thru 1953 16 000 thru 16183

SEB07-5 Revision 1 Page 6 December 17, 2007195 1948 thru 1953 7004 thru 7999 195 1948 thru 1953 16000 thru 161 83 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 t hru U206-0437 U206A 1966 U206-0438 thru U206-0656 TU206A 1966 U206-0487 thru U206-0656 U206B/TU2 06B 1967 U206-0657 thru U206-0914 U206C/TU206C 1968 U206-0915 thru U206-1234 U206D/TU206D 1969 U206-1235 thru U206-1444 U206D/TU 206D 1970 U20601445 thru U20601587 U206E/TU206E 1971 U20601588 thru U20601700 U206F/TU206F 1972 U20601701 thru U20601874 U206F/T U206F 1973 U206018 75 thru U20602199 U206F/TU206F 1974 U20602200 thru U20602579 U206F/TU206F 1975 U20602580 thru U20602588 U206F/ TU206F 1975 U20602 590 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 U206 G/TU206G 1982 U206 06440 thru U20606699 U206G/TU206G 1983 U20606700 thru U20606788 U206G/TU206G 1984 U20606789 thru U20606846 U20 6G/TU206G 198 5 U20 606847 thru U20606920 U206G/TU206G 1986 U20606921 thru U20607020 P206 1965 P206-0002 thru P206-0160 P2 06A 19 66 P2 06-0161 thru P206-0306 TP206A 1966 P206-0161 thru P206-0306 P206B/TP206B 1967 P206-0307 thru P206-0419 P2 06C/TP206C 19 68 P2 06-0420 thru P206-0519

SEB07-5 Revision 1 December 17, 2007 Page 7P206D/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 th ru 20700227 207/T207 1974 20700228 thru 20700267 207/T207 1975 20700268 thru 20700314 207/T207 1976 20700315 th ru 20700362 207A/T207A 1977 20700363 thru 20700414 207A/T207A 1978 20700415 thru 20700482 207A/T207A 1979 20700483 t hru 20700562 207A/T207A 1980 20700563 thru 20700654 207A/T207A 1981 20700655 thru 20700729 207A/T20 7A 1982 20700730 thru 20700762 207A/T207A 1983 20700763 thru 20700767 207A/T207A 1984 20700768 thru 20700788 210 1960 57001 th ru 57575 210 618 210A 1961 21057576 thru 21057840 210A 616 210B 1962 21057841 thru 21058085 210C 1963 21058086 thru 21058139 210C 1963 21058 141 thru 21058220 210D 1964 21058221 thru 21058510 210E 1965 21058511 thru 21058715 210F 1966 21058 716 thru 21058818 210G 1967 21058819 thru 21058936 210H 1968 21058937 thru 21059061 210J 1969 2105 9062 thru 21059199 210K/T210K 1970 21059200 thru 21059351 210K/T210K 1971 21059352 thru 21059502 210 L/T210L 1972 21059503 thru 21059719 210L/T210L 1973 21059720 thru 21060089 210L/T210L 1974 21060090 thru 21060539 21 0L/T210L 19 75 21 060540 thru 21061039 210L/T210L 1976 21061040 thru 21061041 210L/T210L 1976 21061043 thru 21061573 21 0M/T210M 19 77 21 061574 thru 21062273

SEB07-5 Revision 1 Page 8 December 17, 2007210M/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 th ru 21064897 210R/T210R 1985 21064898 thru 21064949 210R/T210R 1986 21064950 thru 21065009 T210F 1966 T210-0001 t hru 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 P2100015 1 thru P21000385 P210N 1980 P21000386 thru P21000590 P210N 1981 P21000591 thru P21000760 P210N 1982 P210007 61 thru P21000811 P210N 1983 P21000812 thru P21000834 P210R 1985 P21000835 thru P21000866 P210R 1986 P21000 867 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 F172 E 1964 F172 -0019 thru F172-0085 F172F 1965 F172-0086 thru F172-0179 F172G 1966 F172-0180 thru F172-0319 F17 2H 196 7 F172-0320 thru F172-0431 F172H 1967 F172-0436 thru F172-0442 F172H 1967 F172-0444 thru F172-0446 F1 72H 19 68 F1 72-0432 thru F172-0435 F172H 1968 F172-0443 F172H 1968 F172-0447 thru F172-0559 F1 72H 19 69 F1 72-0560 thru F172-0654

SEB07-5 Revision 1 December 17, 2007 Page 9F172H 1970 F17200655 thru F17200754 F172K 1971 F17200755 thr u F17200804 F172L 1972 F17200805 thru F17200904 F172M 1973 F17200905 thru F17201034 F172M 1974 F17201035 thr u F17201234 F172M 1975 F17201235 thru F17201384 F172M 1976 F17201385 thru F17201514 F172N 1977 F17201515 t hru F17201639 F172N 1978 F17201640 thru F17201749 F172N 1979 F17201750 thru F17201909 F172N 1980 F17201910 t hru 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 F1720223 9 thru F17202254 FR172E 1968 FR17200001 thru FR17200060 FR172F 1969 FR17200061 thru FR17200145 FR172G 1970 FR17200 146 thru FR17200225 FR172H 1971 FR17200226 thru FR17200275 FR172H 1972 FR17200276 thru FR17200350 FR172J 1973 FR1720 0351 thru FR17200440 FR172J 1974 FR17200441 thru FR17200530 FR172J 1975 FR17200531 thru FR17200559 FR172 J 1976 FR172 00560 thru FR17200590 FR172K 1977 FR17200591 thru FR17200620 FR172K 1978 FR17200621 thru FR17200630 FR172 K 1979 FR172 00631 thru FR17200655 FR172K 1980 FR17200656 thru FR17200665 FR172K 1981 FR17200666 thru FR17200675 F177 RG 1971 F177 RG0001 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 F1 77RG 19 77 F1 77RG0161 thru F177RG0177 F182P 1976 F18200001 thru F18200025 F182Q 1977 F18200026 thru F18200064 F1 82Q 19 78 F1 8200065 thru F18200094

SEB07-5 Revision 1 Page 10 December 17, 2007F182Q 1979 F18200095 thru F18200129 F182Q 1980 F18200130 thr u F18200169 FR182 1978 FR18200001 thru FR18200020 FR182 1979 FR18200021 thru FR18200045 FR182 1980 FR18200046 th ru FR18200070

**PURPOSE** To provide a m odi fi cation 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 fi rst. Recommended: Copilot seat secondary stop installation should be accomplished within the next 400 hours of operation or 24 months, whichever occurs fi rst.
**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 l isted 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

Approximatel y 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:** C opilot Secondary Seat Stop Installation

Installation "A": Approximately 3.0 man-hours per airplane Installation "B": Approximately 2.9 man-hours per airplane
Installatio n "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
Installatio n "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 se rial number must be provided when ordering the seat stop service kits.

**P a**  **r t**  **N u**  **m b** **e r**  **D e** **s c**  **r i**  **p t**  **i o**  **n Q** **t y**  **/ A**  **i r**  **p l**  **a n**  **e P**  **r i**  **c e**  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 con fi gurations 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 fi rst.
**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, 2007B. 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 Adv isory 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 i s 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 fi rst. Compliance i s 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 fi rst.
**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.

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SEB07-5 Revision 1 December 17, 2007 Page 15Figure 1. Identi fi cation of Secondary Seat Stop Installation Con fi gurations (Sheet 1)

SEB07-5 Revision 1 Page 16 December 17, 2007Figure 1. Identi fi cation of Secondary Seat Stop Installation Con fi gurations (Sheet 2)

SEB07-5 Revision 1 December 17, 2007 Page 17Figure 1. Identi fi cation of Secondary Seat Stop Installation Con fi gurations (Sheet 3)

SEB07-5 Revision 1 Page 18 December 17, 2007