here - El Paso Aero, Inc. Avionics Associates
Contents
1. Adjust the cable in accordance with the applicable SK rigging instructions b Ifyou are unable to pull more of the belt from the reel proceed to step 5 Lift the seat adjustment handle and place a 0 05 thick feeler gauge on top of the rail and then lower the seat latch pin onto it Attempt to pull more belt material from the reel a If you can pull more of the belt from the reel it must be re rigged Adjust the cable in accordance with the applicable SK rigging instructions b If you are unable to pull more of the belt from the reel proceed to step 6 Lift the seat adjustment handle and place a 0 10 thick feeler gauge on top of the rail and then lower the seat latch pin onto it Attempt to pull more belt material from the reel a If you are unable to pull more of the belt from the reel it must be re rigged Adjust the cable in accordance with the applicable SK rigging instructions b If you can pull more of the belt from the reel proceed to step 7 Sit in the seat and repeat steps 2 thru 6 while seated There should be no different functionality than when standing outside the airplane If there is adjust the reel and cable in accordance with the applicable SK installation and rigging instructions B Inspection Interval 1 2 At each 100 Hour or Annual Inspection whichever comes first perform Steps 4 A 1 thru 7 above Perform Steps 4 A 1 thru 7 any time the operator notes intermit2. F17201515 thru F17201639 F17201640 thru F17201749 F17201750 thru F17201909 F17201910 thru F17202039 F17202040 thru F17202134 F17202135 thru F17202194 F17202195 thru F17202216 F17202217 thru F17202233 F17202234 thru F17202238 F17202239 thru F17202254 FR17200001 thru FR17200060 FR17200061 thru FR17200145 FR17200146 thru FR17200225 FR17200226 thru FR17200275 FR17200276 thru FR17200350 FR17200351 thru FR17200440 FR17200441 thru FR17200530 FR17200531 thru FR17200559 FR17200560 thru FR17200590 FR17200591 thru FR17200620 FR17200621 thru FR17200630 FR17200631 thru FR17200655 FR17200656 thru FR17200665 FR17200666 thru FR17200675 F177RG0001 thru F177RG0042 F177RG0043 thru F177RG0062 F177RG0063 thru F177RG0092 F177RG0093 thru F177RG0122 F177RG0123 thru F177RG0138 F177RG0139 thru F177RG0160 F177RG0161 thru F177RG0177 F18200001 thru F18200025 F18200026 thru F18200064 F18200065 thru F18200094 F18200095 thru F18200129 SEBO7 5 Revision 6 June 11 2015 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 an additional device installed on the pilot or copilot seat that assists in preventing uncommanded rearward movement of the seat It is designed to assist in providing an additional margin of safety b
3. 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 Customer Service P O Box 7706 Wichita Kansas 67277 U S A 316 517 5800 Facsimile 316 517 7271 www cessnasupport com COPYRIGHT 2015 Single Engine 4 A Cessna A Textron Company Service Bulletin f June 11 2015 TITLE PILOT AND COPILOT SECONDARY SEAT STOP INSTALLATION EFFECTIVITY Model 170 170A 170A 170B 170B 170B 172 172 172 172 172A 172A 172B 172B 172C 172D 172E 172E 172F 172G 172H 172H Original Issue May 14 2007 Revision 1 December 17 2007 Revision 2 June 15 2010 Revision 3 December 15 2011 Revision 4 March 15 2012 Revision 5 November 11 2013 Year 1948 1949 thru 1951 1949 thru 1951 1952 thru 1956 1952 thru 1956 1956 thru 1959 1956 thru 1959 1956 thru 1959 1960 1961 1962 1963 1964 1965 1966 1967 1967 Serial Numbers 18000 thru 18729 18730 thru 19400 19402 thru 20266 20267 thru 20999 25000 thru 27169 609 19401 28000 thru 29999 36000 thru 36999 46001 thru 46754 610 612 615 46755 thru 47746 622 625 17247747 thru 17248734 630 17248735 thru 17249544 17249545 thru 17250572 17250573 thru 17251822 639 17251823 thru 17253392 17253393 thru 17254892 17254893 thru 17256492 1725649
4. 210 0307 T210 0308 thru T210 0392 T210 0393 thru T210 0454 21058140 P21000001 thru P21000150 P21000151 thru P21000385 P21000386 thru P21000590 P21000591 thru P21000760 P21000761 thru P21000811 P21000812 thru P21000834 P21000835 thru P21000866 P21000867 thru P21000874 A182 0001 thru A182 0056 A182 0057 thru A182 0096 A182 0097 thru A182 0116 A182 0117 thru A182 0136 A182 0137 thru A182 0146 A182 0147 thru A182 0148 FP172 0001 thru FP172 0003 F172 0001 thru F172 0018 F172 0019 thru F172 0085 F172 0086 thru F172 0179 F172 0180 thru F172 0319 F172 0320 thru F172 0431 F172 0436 thru F172 0442 F172 0444 thru F172 0446 F172 0432 thru F172 0435 F172 0443 F172 0447 thru F172 0559 F172 0560 thru F172 0654 F17200655 thru F17200754 Page 9 i Page 10 F172K F172L F172M F172M F172M F172M F172N F172N F172N F172N F172P F172P F172P F172P F172P F172P FR172E FR172F FR172G FR172H FR172H FR172J FR172J FR172J FR172J FR172K FR172K FR172K FR172K FR172K F177RG F177RG F177RG F177RG F177RG F177RG F177RG F182P F182Q F182Q F182Q 1971 1972 1973 1974 1975 1976 1977 1978 1979 1980 1981 1982 1983 1984 1985 1986 1968 1969 1970 1971 1972 1973 1974 1975 1976 1977 1978 1979 1980 1981 1971 1972 1973 1974 1975 1976 1977 1976 1977 1978 1979 F17200755 thru F17200804 F17200805 thru F17200904 F17200905 thru F17201034 F17201035 thru F17201234 F17201235 thru F17201384 F17201385 thru F17201514
5. 2RG0001 thru 172RG0570 172RG0571 thru 172RG0890 691 172RG0891 thru 172RG1099 172RG1100 thru 172RG1144 172RG1145 thru 172RG1177 172RG1178 thru 172RG1191 17700001 17700003 thru 17701164 661 17701165 thru 17701370 17701371 thru 17701471 17701473 thru 17701530 17701531 thru 17701633 17700002 17701634 thru 17701773 17701774 thru 17701973 17701974 thru 17702123 17702124 thru 17702313 17701472 17702314 thru 17702522 17702523 thru 17702672 17702673 thru 17702752 Page 3 j Page 4 177RG 177RG 177RG 177RG 177RG 177RG 177RG 177RG 177RG 177RG 180 180 180A 180A 180B 180C 180C 180D 180E 180F 180G 180H 180H 180J 180J 180K 180K 180K 180K 180K 180K 182 182 182A 182A 182A 182B 182B 182B 182C 182C 1971 1972 1973 1973 1974 1975 1976 1977 1978 1953 thru 1956 1957 1957 thru 1958 1959 1960 1961 1962 1963 1964 1965 thru 1972 1973 thru 1976 1973 thru 1976 1977 1978 1979 1980 1981 1956 1957 1958 1958 1959 1959 1960 177RG0001 thru 177RG0212 177RG0213 thru 177RG0282 177RG0283 thru 177RG0418 177RG0420 thru 177RG0432 177RG0433 thru 177RG0592 177RG0593 thru 177RG0787 177RG0788 thru 177RG1051 177RG1052 thru 177RG1266 177RG1267 thru 177RG1366 177RG0419 30000 thru 32661 604 614 32662 thru 32999 50001 thru 50355 50356 thru 50661 50662 thru 50911 624 18050912 thru 18051063 18051064 thru 18051183 18051184 thru 18051312 18051313 thru 18051445 18051446 thru 1805228
6. 4 4 Cessna A Textron Company Revision Transmittal June 11 2015 TO Cessna Distributors and Single Engine Authorized Service Facilities and CPC s SUBJECT Single Engine Service Bulletin SEBO7 5 Revision 6 Pilot and Copilot Secondary Seat Stop Installation REASON FOR REVISION To extend the credit expiration date Miscellaneous changes as required REQUIRED ACTION Please replace any copy of SEB07 5 Revision 5 with the attached copy of SEBO7 5 Revision 6 which is printed in its entirety NOTE Compliance with Revision 6 is not required if in compliance with the Original Issue or a previous revision However if you have not already done so you must remove and destroy the Instructions for Continued Airworthiness Attachment that is stored in the Technical Library CD ROM or Maintenance Manual for your airplane and replace it with the Instructions for Continued Airworthiness Revision A that is attached to this service bulletin LOG OF EFFECTIVE PAGES Page No Date Page No Date 4 June 11 2015 12 June 11 2015 2 June 11 2015 13 June 11 2015 3 June 11 2015 14 June 11 2015 4 June 11 2015 15 June 11 2015 5 June 11 2015 16 June 11 2015 6 June 11 2015 17 June 11 2015 7 June 11 2015 18 June 11 2015 8 June 11 2015 19 June 11 2015 9 June 11 2015 20 June 11 2015 10 June 11 2015 21 June 11 2015 11 June 11 2015 22 June 11 2015 Page 1 of 1 To obtain satisfactory results procedures specified in this publication
7. 4 645 18052285 thru 18052489 18052491 thru 18052770 18052771 thru 18052905 18052906 thru 18053000 18053001 thru 18053115 18052490 18053116 thru 18053167 18053168 thru 18053203 33000 thru 33842 613 33843 thru 34753 34755 thru 34999 51001 thru 51556 51557 thru 51622 51624 thru 52358 34754 52359 thru 53007 631 SEBO7 5 Revision 6 June 11 2015 182D 1961 18253008 thru 18253598 182D 1961 51623 182E 1962 18253599 thru 18254423 182F 1963 18254424 thru 18255058 182G 1964 18255059 thru 18255844 182H 1965 18255846 thru 18256684 182H 634 182J 1966 18256685 thru 18257625 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 R1
8. 4 thru 17256512 SEB07 5 Revision 6 Page 1 of 22 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 Customer Service P O Box 7706 Wichita Kansas 67277 U S A 316 517 5800 Facsimile 316 517 7271 www cessnasupport com COPYRIGHT 2007 j Page 2 172H 1721 172 172K 172K 172L 172L 172M 172M 172M 172M 172M 172M 172M 172N 172N 172N 172N 172N 172N 172N 172N 172P 172P 172P 172P 172P 172P 1720 1720 1720 1720 1720 1720 1720 1720 1720 1720 1720 175 175 1968 1969 1970 1971 1972 1973 1973 1973 1974 1975 1976 1977 1978 1978 1979 1980 1981 1982 1983 1984 1985 1986 1983 1983 1983 1983 1983 1983 1983 1983 1983 1984 1984 1958 thru 1959 638 17256513 thru 17257161 660 17257162 thru 17258486 17258487 thru 17259223 17259224 thru 17259903 17259904 thru 17260758 17260759 thru 17261444 17261446 thru 17261577 17261579 thru 17261898 17256493 17261899 thru 17263458 17263459 thru 17265684 17265685 thru 17267584 17267585 thru 17269309 17261445 17269310 thru 17270049 17270051 thru 17271034 17261578 17271035 thru 17272884 17272885 thru 17274009 17270050 17274010 thru 17275034 17275035 th
9. 4139 thru 18504328 18504329 thru 18504394 18504395 thru 18504415 18504416 thru 18504424 18504425 thru 18504448 7004 thru 7999 16000 thru 16183 7004 thru 7999 SEBO7 5 Revision 6 June 11 2015 195 195A 195A 195B 195B 210 5 205 210 5 205 210 5 205A 206 U206 U206A TU206A U206B TU206B U206C TU206C U206D TU206D U206D TU206D U206E TU206E U206F TU206F U206F TU206F U206F TU206F U206F TU206F U206F TU206F U206F TU206F U206G TU206G U206G TU206G U206G TU206G U206G TU206G U206G TU206G U206G TU206G U206G TU206G U206G TU206G U206G TU206G U206G TU206G U206G TU206G U206G TU206G P206 P206A TP206A P206B TP206B P206C TP206C P206D TP206D SEBO7 5 Revision 6 June 11 2015 1948 thru 1953 1948 thru 1953 1948 thru 1953 1948 thru 1953 1948 thru 1953 1963 1964 1964 1965 1966 1966 1967 1968 1969 1970 1971 1972 1973 1974 1975 1975 1976 1977 1978 1979 1980 1981 1982 1983 1984 1985 1986 1965 1966 1966 1967 1968 1969 16000 thru 16183 7004 thru 7999 16000 thru 16183 7004 thru 7999 16000 thru 16183 205 0001 thru 205 0480 641 648 205 0481 thru 205 0577 206 0001 thru 206 0275 U206 0276 thru U206 0437 U206 0438 thru U206 0656 U206 0487 thru U206 0656 U206 0657 thru U206 0914 U206 0915 thru U206 1234 U206 1235 thru U206 1444 U20601445 thru U20601587 U20601588 thru U20601700 U20601701 thru U20601874 U20601875 thru U20602199 U20602200 thru U20602579 U20602580 thru U20602
10. 5 thru 20700729 20700730 thru 20700762 20700763 thru 20700767 20700768 thru 20700788 57001 thru 57575 618 21057576 thru 21057840 616 21057841 thru 21058085 21058086 thru 21058139 21058141 thru 21058220 21058221 thru 21058510 21058511 thru 21058715 21058716 thru 21058818 21058819 thru 21058936 21058937 thru 21059061 21059062 thru 21059199 21059200 thru 21059351 21059352 thru 21059502 21059503 thru 21059719 21059720 thru 21060089 21060090 thru 21060539 21060540 thru 21061039 21061040 thru 21061041 21061043 thru 21061573 21061574 thru 21062273 21062274 thru 21062954 SEBO7 5 Revision 6 June 11 2015 210M T210M 210N T210N 210N T210N 210N T210N 210N T210N 210N T210N 210N T210N 210R T210R 210R T210R T210F T210G T210H T210J T210J P210N P210N P210N P210N P210N P210N P210R P210R A182J A182K A182L A182N A182N A182N FP172 F172D F172E F172F F172G F172H F172H F172H F172H F172H F172H F172H F172H SEBO7 5 Revision 6 June 11 2015 1978 1979 1980 1981 1982 1983 1984 1985 1986 1966 1967 1968 1969 1978 1979 1980 1981 1982 1983 1985 1986 1966 1967 1968 1972 1974 1976 1963 1963 1964 1965 1966 1967 1967 1967 1968 1968 1968 1969 1970 21061042 21062955 thru 21063640 21063641 thru 21064135 21064136 thru 21064535 21064536 thru 21064772 21064773 thru 21064822 21064823 thru 21064897 21064898 thru 21064949 21064950 thru 21065009 T210 0001 thru T210 0197 T210 0198 thru T
11. 588 U20602590 thru U20603020 U20603021 thru U20603521 U20603522 thru U20604074 676 U20604075 thru U20604649 U20604650 thru U20605309 U20602589 U20605310 thru U20605919 U20605920 thru U20606439 U20606440 thru U20606699 U20606700 thru U20606788 U20606789 thru U20606846 U20606847 thru U20606920 U20606921 thru U20607020 P206 0002 thru P206 0160 P206 0161 thru P206 0306 P206 0161 thru P206 0306 P206 0307 thru P206 0419 P206 0420 thru P206 0519 P206 0520 thru P206 0603 Page 7 i Page 8 P206E TP206E P206E TP206E 207 T207 207 T207 207 T207 207 T207 207 T207 207 T207 207 T207 207 T207 207A T207A 207A T207A 207A T207A 207A T207A 207A T207A 207A T207A 207A T207A 207A T207A 210 210 210A 210A 210B 210C 210C 210D 210E 210F 210G 210H 210J 210K T210K 210K T210K 210L T210L 210L T210L 210L T210L 210L T210L 210L T210L 210L T210L 210M T210M 210M T210M 1970 1969 1970 1971 1972 1973 1974 1975 1976 1977 1978 1979 1980 1981 1982 1983 1984 1960 1961 1962 1963 1963 1964 1965 1966 1967 1968 1969 1970 1971 1972 1973 1974 1975 1976 1976 1977 1978 P20600604 thru P20600647 P206 0001 20700001 thru 20700148 20700149 thru 20700190 20700191 thru 20700205 20700206 thru 20700215 20700216 thru 20700227 20700228 thru 20700267 20700268 thru 20700314 20700315 thru 20700362 20700363 thru 20700414 20700415 thru 20700482 20700483 thru 20700562 20700563 thru 20700654 2070065
12. 75A Copilot Secondary Seat Stop Installation For your convenience the typical installation of the secondary seat stop installation configurations are shown in Figure 1 Store the attachment that follows Airplanes Incorporating SK210 174 SK210 175 SK195 11 SK195 12 SK337 75 or SK337 76 Any ofthese SKs at any Revision level Instructions for Continued Airworthiness Revision A with the airplane maintenance manual SEBO7 5 Revision 6 June 11 2015 Page 13 AIRPLANES INCORPORATING SK210 174 SK210 175 SK195 11 SK195 12 SK337 75 or SK337 76 Any of these SKs at any Revision level INSTRUCTIONS FOR CONTINUED AIRWORTHINESS Revision A Cessna Aircraft Company P O Box 7704 Wichita Kansas 67277 Model Numbers 170 172 175 177 177RG 180 T 182 R182 TR182 185 190 195 T 206 T 207 T 210 P210 T303 336 T 337 P337 SEBO7 5 Revision 6 June 11 2015 Page 14 1 Introduction A The purpose of this Service Bulletin Attachment is to provide the maintenance technician with the information necessary to ensure the correct functionality and operation of the Secondary Seat Stop installed by accomplishment of either SK210 174 SK210 175 SK195 11 SK195 12 SK337 75 or SK337 76 on the applicable Cessna Models B This document supplements the applicable Model Maintenance Manual or Service Manual until the next revision to the Manual is accomplished C When this information is incorporate
13. 82 683 R182 1978 R18200002 thru R18200583 R182 TR182 1979 R18200584 thru R18201313 R182 TR182 R18200001 SEBO7 5 Revision 6 June 11 2015 Page 5 j Page 6 R182 TR182 R182 TR182 R182 TR182 R182 TR182 R182 TR182 R182 TR182 R182 TR182 R182 TR182 R182 TR182 185 185 185A 185B 185C 185D 185E A185E A185E A185E A185E A185E A185E A185F A185F A185F A185F A185F A185F A185F A185F A185F A185F A185F A185F A185F A185F A185F A185F 190 190 195 1980 1980 1981 1982 1983 1984 1985 1986 1961 1962 1963 1964 1965 1966 1966 1967 1968 1969 1970 1971 1972 1973 1973 1974 1975 1976 1977 1978 1979 1980 1981 1982 1983 1984 1985 1948 thru 1953 1948 thru 1953 1948 thru 1953 R18201314 R18201316 thru R18201628 R18201629 thru R18201798 R18201799 thru R18201928 R18201929 thru R18201973 R18201974 thru R18201999 R18202000 thru R18202031 R18201315 R18202032 thru R18202039 185 0001 thru 185 0237 632 185 0238 thru 185 0512 185 0513 thru 185 0653 185 0654 thru 185 0776 185 0777 thru 185 0967 185 0968 thru 185 1149 185 0968 thru 185 1149 185 1150 thru 185 1300 185 1301 thru 185 1447 185 1448 thru 185 1599 18501600 thru 18501934 18501935 thru 18502090 18502091 thru 18502299 18502301 thru 18502310 652 18502311 thru 18502565 18502566 thru 18502838 18502839 thru 18503153 18503154 thru 18503458 18503459 thru 18503683 18503684 thru 18503938 18502300 18503939 thru 18504138 1850
14. Service P O Box 7706 Wichita Kansas 67277 U S A 316 517 5800 Facsimile 316 517 7271 www cessnasupport com COPYRIGHT 2015
15. ary Seat Stop Installation Configurations Sheet 1 SEBO7 5 Revision 6 June 11 2015 Page 18 1 Reel 2 Belt 3 Control Cable Installation G Figure 1 Identification of Secondary Seat Stop Installation Configurations Sheet 2 SEBO7 5 Revision 6 Page 19 June 11 2015 B7801 Installation H Installation J 1 Reel 2 Belt 3 Control Cable Installation K 12997377 Figure 1 Identification of Secondary Seat Stop Installation Configurations Sheet 3 SEBO7 5 Revision 6 June 11 2015 Page 20 B14362 Installation M 1 Reel 2 Belt 3 Control Cable 0711041 0700531A Figure 1 Identification of Secondary Seat Stop Installation Configurations Sheet 4 SEBO7 5 Revision 6 Page 21 June 11 2015 SEBO7 5 Revision 6 June 11 2015 Page 22 4 4 Cessna A Textron Company Owner Advisory June 11 2015 SEB07 50AR6 Dear Cessna Single Engine Owner This Owner Advisory is to inform you that Service Bulletin SEBO7 5 Revision 6 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 an additional device installed on the pilot or copilot seat that assists in preventing uncommanded rearward movement of the seat It is designed to assist in providing an additional margin of safety by limiting the aft trave
16. ately 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 Installation L 2 8 man hours per airplane Installation M 2 6 man hours per airplane SEBO7 5 Revision 6 Page 12 June 11 2015 MATERIAL The parts below are available from Cessna Service Parts and Programs through an appropriate Cessna Authorized Service Facility NOTE The airplane serial number must be provided when ordering the seat stop service kits Part Number Description Qty Airplane SK195 11A Pilot Secondary Seat 1 Stop Installation Kit Models 190 195 SK195 12A Copilot Secondary 1 Seat Stop Installation Kit Models 190 195 SK210 174B Pilot Secondary Seat 1 Stop Installation Kit Models 170 P210 except Models 190 195 SK210 175A Copilot Secondary 1 Seat Stop Installation Kit Models 170 P210 except Models 190 195 U000787S EC1300LP Adhesive as required 1 Pint ACCOMPLISHMENT INSTRUCTIONS Service Kit installation instructions are included in the following Service Kits when the kits are shipped from Cessna Service Parts and Programs SK195 11A and SK210 174B Pilot Secondary Seat Stop Installation SK195 12A and SK210 1
17. d into the applicable Model Maintenance Manual the Maintenance Manual shall take precedence over this document NOTE This document must be placed with the aircraft operator s Technical Library CD ROM or Maintenance Manual and incorporated into the operator s scheduled maintenance program 2 Description and Operation A Description The Secondary Seat Stop is an additional device installed on the pilot or copilot seat that assists in preventing uncommanded rearward movement of the seat It is designed to assist in providing an additional margin of safety by limiting the aft travel of the seat should the primary seat latch pin s not be 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 The functionality of the Secondary Seat Stop should be completely transparent to the operator If operation of the seat stop is not transparent the airplane requires maintenance to correct the malfunction of the seat stop mechanism B Operation 1 The control cable of the Secondary Seat Stop is connected to the Seat Latch Pin or Seat Adjustment Handle near the Latch Pin When properly rigged the Secondary Seat Stop should be engaged preventing aft movement of the seat when the Latch Pin is in the seat rail track hole or resting atop the rail track 2 When the Latch Pin is engaged in the seat rail hole or i
18. ed per airplane to install Service Kits SK195 11A and SK210 174B Pilot Secondary Seat Stop Installation NOTE If you purchased a service kit after January 1 2015 and prior to the issuance of this revision you qualify for warranty credit and you can submit a credit claim form When applicable freight will be credited at the most economical method unless pre approved by Cessna To receive credit the work must be completed and a Warranty Claim submitted by a Cessna Authorized Service Facility within 30 calendar days of Service Bulletin compliance before the credit expiration dates shown below Domestic December 31 2016 International December 31 2016 Please contact a Cessna Authorized Service Facility for detailed information and arrange to have Cessna Service Bulletin SEBO7 5 Revision 6 accomplished on your airplane As a convenience service documents are now available online to all our customers through a simple free of charge registration process If you would like to sign up please visit the Customer Support Login link at www Cessna com to register 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 Customer
19. l of the seat should the primary seat latch pin s not be 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 The functionality of the Secondary Seat Stop should be completely transparent to the operator If operation of the seat stop is not transparent the airplane requires maintenance to correct the malfunction of the seat stop mechanism Compliance is mandatory for the pilot seat the secondary seat stop installation shall be accomplished within the next 200 hours of operation or 12 months whichever occurs first Compliance is recommended for the copilot seat the secondary seat stop installation should 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 NOTE Compliance with Revision 6 is not required if in compliance with the Original Issue or a previous revision However if you have not already done so you must remove and destroy the Instructions for Continued Airworthiness Attachment that is stored in the Technical Library CD ROM or Maintenance Manual for your airplane and replace it with the Instructions for Continued Airworthiness Revision A that is attached to service bulletin SEBO7 5 Applicable Service Kit parts credit will be provid
20. ru 17275759 17275760 thru 17276079 17276080 thru 17276259 17276260 thru 17276516 17276517 thru 17276654 17275869 17275927 thru 17275934 17275952 17275959 17275960 17275962 17275964 17275965 17275967 17275968 17275969 17275971 17275992 17275999 17276002 17276005 17276029 17276032 17276042 17276045 17276051 17276052 17276054 17276101 17276109 17276140 17276147 17276188 17276211 55001 thru 56238 287004 626 640 SEBO7 5 Revision 6 June 11 2015 175A 175A 175B 175C P172D R172E T41 R172F T41 R172G T41 R172H T41 R172H T41 R172H T41 R172J R172K R172K R172K R172K R172K R172K 172RG 172RG 172RG 172RG 172RG 172RG 172RG 177 177 177 177A 177B 177B 177B 177B 177B 177B 177B 177B 177B 177B 177B 177B SEBO7 5 Revision 6 June 11 2015 1960 1961 1962 1963 1967 thru 1968 1969 1969 thru 1970 1971 1972 1973 thru 1976 1974 1977 1978 1979 1980 1981 1980 1981 1982 1983 1984 1985 1968 1968 1969 1970 1970 1971 1972 1973 1974 1975 1976 1977 1978 56239 thru 56777 619 17556778 thru 17557002 17557003 thru 17557119 P17257120 thru P17257188 R172 0001 thru R172 0335 R172 0336 thru R172 0409 R1720410 thru R1720444 R1720445 thru R1720494 R1720495 thru R1720546 R1720547 thru R1720620 P17257189 R1722000 thru R1722724 R1722725 thru R1722929 R1722930 thru R1723199 680 R1723200 thru R1723399 R1723400 thru R1723454 17
21. s raised to no more than 0 05 inch above the seat rail track using the Seat Adjustment Handle the Secondary Seat Stop should engage thereby permitting no further aft movement of the seat C System Components 1 One of the following Cessna Service Kits at any revision level e SK210 174 e SK210 175 e SK195 11 e SK195 12 e SK337 75 e SK337 76 3 Installation and Rigging e Installation and rigging of the Secondary Seat Stop are to be done in accordance with the applicable Service Kit SK SEBO7 5 Revision 6 Page 15 June 11 2015 4 Required Maintenance A Inspection Test 1 2 7 Stand outside the airplane with the door open Check to see if the latch pin is engaged in a hole in the rail track a If it is proceed to step 3 b If it is not adjust the seat to put a pin in a hole in the seat rail track Grasp the belt about mid way between its attachment to the floor and the seat base Attempt to pull more belt material from the reel a If you can pull more of the belt from the reel it must be re rigged Adjust the cable in accordance with the applicable SK rigging instructions b Ifyou are unable to pull more of the belt from the reel proceed to step 4 Lift the seat adjustment handle and reposition the seat so that the latch pin rests atop the rail track notin a hole Attempt to pull more belt material from the reel a If you can pull more of the belt from the reel it must be re rigged
22. tent or poor functioning of the Secondary Seat Stop or is unable to move the seat aft when commanded C Troubleshooting 1 If the Secondary Seat Stop requires repeated rigging a Inspect the primary seat latch system for condition and wear b Replace worn or damaged parts c Re rig the secondary seat stop in accordance with the applicable SK SEBO7 5 Revision 6 June 11 2015 Page 16 2 If insufficient handle movement is available to release the secondary seat stop a Inspect the primary seat latch system for condition and wear b Replace worn or damaged parts c Re rig the secondary seat stop in accordance with the applicable SK 3 If intermittent or poor functioning of the Secondary Seat Stop is reported a Inspect the primary seat latch system for condition and wear b Replace worn or damaged parts c Re rig the secondary seat stop in accordance with the applicable SK 5 Airworthiness Limitations A The applicable Model Type Certificate Data Sheet and AFM contain the airframe limitations B The Secondary Seat Stop system has no mandatory replacement time or life limit associated with its installation and has no impact on the Limitations to the airframe SEBO7 5 Revision 6 Page 17 June 11 2015 Installation B Installation A Installation D 3 Control Cable 1 Reel 2 Belt Installation C NOTE All dimensions are shown in inches Figure 1 Identification of Second
23. tion that changes the airplane type design Cessna received EASA approval for the technical data in this publication that changes the airplane type design MAN HOURS NOTE The man hours listed below are provided as a guide for scheduling and planning purposes only The man hours listed below are based on the work being accomplished during a scheduled 100 hour annual type inspection SK195 11A Pilot Secondary Seat Stop Installation 6 7 man hours per airplane K195 12A Copilot Secondary Seat Stop Installation Approximately 6 2 man hours per airplane SEBO7 5 Revision 6 June 11 2015 Page 11 SK210 174B 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 Installation L 2 8 man hours per airplane Installation M 2 6 man hours per airplane SK210 175A 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 Approxim
24. y limiting the aft travel of the seat should the primary seat latch pin s not be 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 The functionality of the Secondary Seat Stop should be completely transparent to the operator If operation of the seat stop is not transparent the airplane requires maintenance to correct the malfunction of the seat stop mechanism COMPLIANCE Mandatory Pilot seat secondary stop installation shall be accomplished within the next 200 hours of operation or 12 months whichever occurs first Recommended Copilot seat secondary stop installation should 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 NOTE Compliance with Revision 6 is not required if in compliance with the Original Issue or a previous revision However if you have not already done so you must remove and destroy the Instructions for Continued Airworthiness Attachment that is stored in the Technical Library CD ROM or Maintenance Manual for your airplane and replace it with the Instructions for Continued Airworthiness Revision A that is attached to this service bulletin APPROVAL Cessna received FAA approval for the technical data in this publica
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