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10 Master Drawing List Drawing No. Rev.* Date Title E 2/27/ NC 7/9/02 APPLICABILITY LIST, CESSNA, LIGHT AIRCRAFT, MULTIPLE MODELS INSTALLATION INSTRUCTIONS, CESSNA, LIGHT AIRCRAFT, MULTIPLE MODELS CB-25 B 1/15/02 BATTERY, LEAD ACID, 12 VOLT CB-25XC NC 1/15/02 BATTERY, LEAD ACID, 12 VOLT, PLATINUM SERIES CB-35A B 1/15/02 BATTERY, LEAD ACID, 12 Volt CB-35AXC NC 1/15/02 BATTERY, LEAD ACID, 12 VOLT, PLATINUM SERIES CB24-11 B 2/5/02 BATTERY, LEAD ACID, 24 VOLT CB24-11XC NC 2/5/02 BATTERY, LEAD ACID, 24 VOLT, PLATINUM SERIES CB24-11M B 2/5/02 BATTERY, LEAD ACID, 24 VOLT CB24-11MXC NC 2/5/02 BATTERY, LEAD ACID, 24 VOLT, PLATINUM SERIES RG-25 J 11/15/99 BATTERY, VRSLA, 12 VOLT, RG-25 SERIES RG-35A B 11/17/99 BATTERY, VRSLA, 12 VOLT, RG-35 SERIES RG24-11 B 10/4/05 BATTERY, VRSLA, 24 VOLT RG24-9 A 7/19/06 BATTERY, VRSLA, 24 VOLT RG24-10 NC 2/22//07 BATTERY, VRSLA, 24 VOLT RG24-11M A 9/9/98 BATTERY, VRSLA, 24 VOLT RG24-12 NC 11/21/06 BATTERY, VRSLA, 24 VOLT RG24-15 E 10/4/05 BATTERY, VRSLA, 24 VOLT RG24-15M C 9/2/99 BATTERY, VRSLA, 24 VOLT RG24-20 B 1/25/01 BATTERY, VRSLA, 24 VOLT RG24-16 NC 1/25/06 BATTERY, VRSLA, 24 VOLT A 2/15/07 CESSNA BATTERY BOX, COVER MODIFICATION *Or later FAA approved Revision Revisions Rev. Description Date Approved A Rev , correct title & /16/02 JBT B Rev /24/04 JBT C Added RG24-16 battery 1/25/06 JBT D Updated all drawings to current revision status , , , RG24-11, RG /6/06 JBT E F Added RG24-20 battery, RG24-12 and RG24-9 Rev and Added RG24-10 Rev , /15/07 JBT 2/26/07 JBT TITLE: Master Drawing List, Cessna, Light Aircraft, Multiple Models DWG NO REV. F CAGE CODE: DRAWN: JBT 6/28/02 CHECKED AMIII 7/16/02 APPROVED JBT 7/16/02 ISSUED NS 2/27/07 SHEET: 1 OF 2

11 Drawing No. Rev.* Date Title NC 7/9/02 CB-35 SERIES AND RG-35 SERIES MODIFICATION, CESSNA MODELS 205, 206, 207, & J 2/20/07 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS, CONCORDE VALVE REGULATED MAIN BATTERY E 10/27/04 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS, CONCORDE FLOODED MAIN BATTERY TITLE: Master Drawing List, Cessna, Light Aircraft, Multiple Models DWG NO REV. F CAGE CODE: DRAWN: JBT 6/28/02 CHECKED AMIII 7/16/02 APPROVED JBT 7/16/02 ISSUED NS 2/27/07 SHEET: 2 OF 2

12 Applicability List Type Certificate Certification Basis Model No. Serial No. / Model Year Single Engine Piston Models A-768 CAR4a 140 Serial No & up 120 Serial No & up 5A2 CAR 3 CAR4a 140A Serial No Through A-799 CAR Serial No through A Serial No through except B Serial No. 609, 19401, through and through A12 CAR Serial No. 610, 612, 615, through 29999, through 36999, and through A 622, 625, through CAR 3, Part B 630, through CAR 3 172C through CAR 3, Part D through CAR 3 172E 639, through CAR 3 Part F (USAF T-41A) through CAR 3 172G through H (USAF T-41A) 638, through except I through CAR 3, Part K through (1969 Model) through (1970 Model) CAR 3 172L through (1971 Model) through (1972 Model) 172M , through (1973 Model) except and through (1974 Model) through (1975 Model) through (1976 Model) 172N , through (1977 Model) , through (1978 Model) except through (1979 Model) , through (1980 Model) 172P through (1981 Model) through (1982 Model) through (1983 Model) through (1984 Model) through (1985 Model) through (1986 Model) TITLE: Applicability List, Cessna, Light Aircraft, Multiple Models DWG. NO REV. E CAGE CODE: DRAWN: DGG 6/28/02 CHECKED JBT 6/29/02 APPROVED JBT 7/16/02 ISSUED NS 2/27/07 SHEET: 1 OF 13

13 Type Certificate Certification Basis 3A13 CAR 3 Part 23 Model No. Serial No. / Model Year Part Q through (1983 Model) through (1984 Model) 172R 172S and on 172S8001 and on and through (1956 Model) 182A through (1957 Model) through and through (1958 Model) 182B 34754, through except (1959 Model) 182C 631, through (1960 Model) 182D 51623, through (1961 Model) 182E through (1962 Model) 182F through (1963 Model) 182G through (1964 Model) 182H 634, through (1965 Model) 182J through (1966 Model) 182K , through , through (1967 Model) 182L through (1968 Model) 182M , through (1969 Model) 182N through (1970 Model) through (1971 Model) 182P through (1972 Model) through (1973 Model) through (1974 Model) 675, through except (1975 Model) through (1976 Model) 182Q through (1977 Model) , through (1978 Model) through (1979 Model) through , except (1980 Model) R182 R through R (1978 Model) R , R through R (1979 Model) TR182 R through R except R (1980 Model) R through R (1981 Model) R through R (1982 Model) R through R (1983 Model) R through R (1984 Model) R , R through R (1985 Model) R through R (1986 Model) TITLE: Applicability List, Cessna, Light Aircraft, Multiple Models DWG. NO REV. E CAGE CODE: DRAWN: DGG 6/28/02 CHECKED JBT 6/29/02 APPROVED JBT 7/16/02 ISSUED NS 2/27/07 SHEET: 2 OF 13

14 Type Certificate Certification Basis Model No. Serial No. / Model Year 182R , through (1981 Model) through (1982 Model) through (1983 Model) through (1984 Model) through (1985 Model) through (1986 Model) 182S through T T182T and On T and On A-790 CAR through through A17 CAR 3 Part through through A 7004 through through B 7004 through through A, through A 619, through B through C through P172D R172E (USAF T-41B0 (USAF T- 41C&D) R172F (USAF T-41D) R172G (USAF T-41C & T-41D) R172H (USAF T-41D) P through P R through R R through R R through R R through R (1971 Model) R through R (1972 Model) R through R (1973 through 1976) R172J P (1974 Model) R172K R through R (1977 Model) R through R (1978 Model) 680, R through R (1979 Model) R through R (1980 Model) R through R (1981 Model) TITLE: Applicability List, Cessna, Light Aircraft, Multiple Models DWG. NO REV. E CAGE CODE: DRAWN: DGG 6/28/02 CHECKED JBT 6/29/02 APPROVED JBT 7/16/02 ISSUED NS 2/27/07 SHEET: 3 OF 13

15 Type Certificate Certification Basis Model No. Serial No. / Model Year 172RG 172RG0001 through 172RG0570 (1980 Model) 691, 172RG0571 through 172RG0890 (1981 Model) 172RG0891 through 172RG1099 (1982 Model) 172RG1100 through 172RG1144 (1983 Model) 172RG1145 through 172RG1177 (1984 Model) 172RG1178 through 172RG1191 (1985 Model) A13CE Part , through except A through B through except (1970 Model) , through (1971 Model) through (1972 Model) through (1973 Model) through (1974 Model) , through (1975 Model) through (1976 Model) through (1977 Model) through (1978 Model) A20CE Part RG 177RG0001 through 177RG0212 (1971 Model) 177RG0213 through 177RG0282 (1972 Model) 177RG0283 through 177RG0432 except 177RG0419 (1973 Model) 177RG0433 through 177RG0592 (1974 Model) 177RG0593 through 177RG0787 (1975 Model) 177RG0788 through 177RG1051 (1976 Model) 177RG1052 through 177RG1266 (1977 Model) 177RG0419, 177RG1267 through 177RG1366 (1978 Model) 5A6 CAR , 614, through CAR 3 Part A through 32999, through B through C 624, through D through E through F through G through H 645, through J through except K through (1977 Model) through (1978 Model) , through (1979 Model) through (1980 Model) through (1981 Model) 3A21 CAR , through (1960 Model) 210A 616, through (1961 Model) 210B through (1962 Model) TITLE: Applicability List, Cessna, Light Aircraft, Multiple Models DWG. NO REV. E CAGE CODE: DRAWN: DGG 6/28/02 CHECKED JBT 6/29/02 APPROVED JBT 7/16/02 ISSUED NS 2/27/07 SHEET: 4 OF 13

16 Type Certificate Certification Basis Car 3 Part 23 Model No. Serial No. / Model Year 210C through and through (1963 Model) (205) 641, through (1963 Model) 210-5A (205A) through (1964 Model) 210D through (1964 Model) 210E through (1965 Model) T210F T through T (1966 Model) 210F through (1966 Model) T210G T through T (1967 Model) T210H T through T (1968 Model) 210G through (1967 Model) 210H through (1968 Model) T210J , T through T (1969 Model) 210J through (1969 Model) 210K/T210K through (1970 Model) through (1971 Model) 210L/T210L through (1972 Model) through (1973 Model) through (1974 Model) through (1975 Model) through (1976 Model) through (1976 Model) 210M/T210M through (1977 Model) , through (1978 Model) P210N P through P (1978 Model) P through P (1979 Model) P through P (1980 Model) P through P (1981 Model) P through P (1982 Model) P through P (1983 Model) 210N through (1979 Model) through (1980 Model) through (1981 Model) through (1982 Model) through (1983 Model) through (1984 Model) T210N through (1979 Model) through (1980 Model) through (1981 Model) through (1982 Model) through (1983 Model) through (1984 Model) P210R P through P (1985 Model) P through P (1986 Model) TITLE: Applicability List, Cessna, Light Aircraft, Multiple Models DWG. NO REV. E CAGE CODE: DRAWN: DGG 6/28/02 CHECKED JBT 6/29/02 APPROVED JBT 7/16/02 ISSUED NS 2/27/07 SHEET: 5 OF 13

17 Type Certificate Certification Basis 3A24 CAR 3 Part 23 Part 21 A4CE CAR 3 Part 23 Model No. Serial No. / Model Year 210R through (1985 Model) through (1986 Model) T210R through (1985 Model) through (1986 Model) , through (1961 Model) 185A through (1962 Model) 185B through (1963 Model) 185C through (1964 Model) 185D through (1965 Model) 185E through (1966 Model) A185E through (1966 Model) through (1967 Model) through (1968 Model) through (1969 Model) through (1970 &1971) through (1972 Model) A185F 652, through except (1973 Model) through (1974 Model) through (1975 Model) through (1976 Model) through (1977 Model) through (1978 Model) , through (1979 Model) through (1980 Model) through (1981 Model) through (1982 Model) through (1983 Model) through (1984 Model) through (1985 Model) through U206 U through U P206 P through P U206A U through U P206A P through P P206B P through P TU206A U through U TU206B U through U TP206A P through P TP206B P through P U206B U through U P206C/TP206C P through P P206D/TP206D P through P TITLE: Applicability List, Cessna, Light Aircraft, Multiple Models DWG. NO REV. E CAGE CODE: DRAWN: DGG 6/28/02 CHECKED JBT 6/29/02 APPROVED JBT 7/16/02 ISSUED NS 2/27/07 SHEET: 6 OF 13

18 Type Certificate Certification Basis Model No. P206E/TP206E Serial No. / Model Year P , P through P U206C/TU206C U through U U206D/TU206D U through U U206E/TU206E U through U U through U (1968 Model) (1969 Model) (1970 Model) (1971 Model) U206F/TU206F U through U (1972 Model) U through U (1973 Model) U through U (1974 Model) U206F/TU206F U through U and U through U U through U (1975 Model) (1976 Model) U206G/TU206G 676 and U through U (1977 Model) U through U (1978Model) U and U through U (1979 Model) U through U (1980 Model) U through U (1981 Model) U through U (1982 Model) U through U (1983 Model) U through U (1984 Model) U through U (1985 Model) U through U (1986 Model) 206H and On Part 23 T206H T and On A9CE Part , through A , through A188A through B through A188B 678T, through T188C T T, T T, T T, T T through T T 188A through A6CE CAR through A (USAF O2B) through except and B , , through except Part 23 T337B , through except C through T337C through D through T337D through TITLE: Applicability List, Cessna, Light Aircraft, Multiple Models DWG. NO REV. E CAGE CODE: DRAWN: DGG 6/28/02 CHECKED JBT 6/29/02 APPROVED JBT 7/16/02 ISSUED NS 2/27/07 SHEET: 7 OF 13

19 Type Certificate Certification Basis Model No. M337B (USAF O2A) 337-M0001 through 337-M IR001 through 337-IR E through T337E through Serial No. / Model Year T337F , through F through (1971 Model) , through except (1972 Model) T337G P through P (1973 Model) P through P (1974 Model) 677, P through P except P (1975 Model) P through P (1976 Model) P through P (1977 Model) 337G through (1973 Model) through (1974 Model) through (1975 Model) through (1976 Model) , through (1977 Model) 337H/T337H through except (1978 Model) through , and (1979 Model) through except and (1980 Model) P337H P through P (1978 Model) P through P and P (1979 Model) P through P (1980 Model) T337H-SP (1979 Model) through , through (1980 Model) A16CE Part /T through (1969 Model) through (1970 Model) through (1971 Model) through (1972 Model) through (1973 Model) through (1974 Model) through (1975 Model) through (1976 Model) 207A/T207A through (1977 Model) through (1978 Model) through (1979 Model) through (1980 Model) through (1981 Model) through (1982 Model) through (1983 Model) through (1984 Model) 3A14 CAR 3 305B through and and up. 305M-0001 and up. TITLE: Applicability List, Cessna, Light Aircraft, Multiple Models DWG. NO REV. E CAGE CODE: DRAWN: DGG 6/28/02 CHECKED JBT 6/29/02 APPROVED JBT 7/16/02 ISSUED NS 2/27/07 SHEET: 8 OF 13

20 Type Certificate Certification Basis Model No. 305E (Military TO-1D, O-1D, O-1F) 305M 0001 and up Serial No. / Model Year 3A19 Part , through 17999, through A 628, through B through C through D through E 644, through F through G through except H 649, through J through K through A150K A through A L through A150L A through A except A M through A150M , A through A through A , A , A through A A through A A through A A through A A through A A through A A through A A through A (1979 Model) (1980 Model) (1981 Model) (1982 Model) (1983 Model) (1984 Model) (1985 Model) Twin Engine Piston Models 3A10 CAR through A (USAF U-3A) through B 607, 35547, 35548, 35549, through C 35550, through 35999, through D through E (USAF U-3B) 35912A, 310M0001 through 310M0036 TITLE: Applicability List, Cessna, Light Aircraft, Multiple Models DWG. NO REV. E CAGE CODE: DRAWN: DGG 6/28/02 CHECKED JBT 6/29/02 APPROVED JBT 7/16/02 ISSUED NS 2/27/07 SHEET: 9 OF 13

21 Type Certificate Certification Basis Model No. 310F through Serial No. / Model Year 3A10 CAR 3 Part G 310G0001 through 310G H 310H0001 through 310H0148 E310H 310H0001 through 310H0148 E310I 310I0001 through 310I J 310J0001 through 310J J-1 310J0001 through 310J0200 E310J 310J0001 through 310J0200 E310K 310K0001 through 310K L 310L0001 through 310L N 310N0001 through 310N P 310P0001 through 310P0240 T310P 310P0001 through 310P Q 310Q0001 through 310Q1160 T310Q 310Q0001 through 310Q R 310R0001 through 310R2140 T310R 310R0001 through 310R2140 3A25 CAR through CAR 3 Part All Model 320 (Section 1) S/Ns 320A 320B 320C 320D 320E 320F 320A0001 through 320A B0001 through 320B C0001 through 320C , 320D0001 through320d E0001 through 320E , 320F0001 through 320F through (1972 Model) through (1973 Model) through (1974 Model) through (1975 Model) 340A 340A0001 through 340A0125 (1976 Model) 340A0201 through 340A0375 (1977 Model) 340A0401 through 340A0562 (1978 Model) 340A0601 through 340A0801 (1979 Model) 340A0901 through 340A1045 (1980 Model) 340A1201 through 340A1280 (1981 Model) 340A1501 through 340A1543 (1982 Model) 340A1801 through 340A1817 (1984 Model) through TITLE: Applicability List, Cessna, Light Aircraft, Multiple Models DWG. NO REV. E CAGE CODE: DRAWN: DGG 6/28/02 CHECKED JBT 6/29/02 APPROVED JBT 7/16/02 ISSUED NS 2/27/07 SHEET: 10 OF 13

22 Type Certificate Certification Basis Model No. A7CE CAR through CAR 3 Part A through through A 401B 401A0001 through 401A B0001 through 401B through A 402B 402A0001 through 402A B0001 through 402B through A 402C 414A0001 through 414A , 402C0001 through 402C1020 CAR through CAR 3 Part A 421B 421C 421A0001 through 421A B0001 through 421B C0001 through 421C1807 A25CE Part through Serial No. / Model Year A34CE Part 23 T303 T through T except T , (1982 Model) T , T , T , T , T , T , T , T , T , T , T , T , T , T , T , T , T , T , T , T , T , T , T , T , T T through T except T , (1983 Model) T , T , T , T , T , T , T , T , T , T , T , T , T , T , T , T , T , T , T , T , T , T , T , T , T T through T (1984 model) TITLE: Applicability List, Cessna, Light Aircraft, Multiple Models DWG. NO REV. E CAGE CODE: DRAWN: DGG 6/28/02 CHECKED JBT 6/29/02 APPROVED JBT 7/16/02 ISSUED NS 2/27/07 SHEET: 11 OF 13

23 The purpose of this report is to provide instructions for the replacement of the original equipment flooded lead acid battery with a Concorde Battery Corporation flooded lead acid or Valve Regulated Sealed Lead Acid (VRSLA) Battery in Cessna Aircraft Corporation aircraft. DESCRIPTION The Concorde flooded lead acid or VRSLA RG series batteries referenced here are direct replacements for the flooded lead acid batteries originally installed in these aircraft. No mechanical or electrical modifications of the aircraft are required to install the Concorde battery except for trimming the hold down tabs on Cessna 12 volt plastic battery cases per the included instructions and capping and stowing or removal of the vent tube on some 24 volt aircraft if the non manifold version of the VRSLA battery is selected. The Concorde VRSLA battery requires no venting. The Concorde batteries are compatible to all electrical specifications and operating procedures as specified in the Pilots Operating Handbooks and should be operated in exactly the same manner as the original battery. Any references to adding water can be ignored if the VRSLA battery is selected. Inspection and maintenance can be performed in any shop by reference to the latest revision of Concorde Battery Corp INSTRUCTIONS FOR CONTINUED AIRWORTHINESS (ICA). The Concorde VRSLA Battery can be safely recharged in the aircraft by following the Concorde instructions for continued airworthiness (ICA) that are part of this document. The Concorde batteries offer the operator a choice of capacities to suit the particular mission. Cessna P/N Concorde P/N Ampere-Hour (AH) Capacity at the 1 hour rate (C1) To replace the Cessna 12 volt battery P/N To replace the Cessna 12 volt battery P/N , , or To replace the Cessna 24 volt manifold battery P/N C To replace the Cessna 24 volt battery P/N C To replace the Cessna 24 volt battery P/N C To replace the Cessna 24 Volt battery P/N & REBAT P/N R2425 Concorde CB 25 Concorde CB-25XC Concorde RG-25 Concorde RG-25XC Concorde CB-35A Concorde CB-35AXC Concorde RG-35A Concorde RG-35AXC Concorde CB24-11M Concorde CB24-11MXC Concorde RG24-11M Concorde RG24-15M 20 AH 25 AH 22 AH 24 AH 29 AH 34 AH 29 AH 33 AH 10 AH 15 AH 11 AH 13.6 AH Weight (lbs.) 22 lbs lbs lbs lbs lbs lbs lbs. 32 lbs. 28 lbs. 31 lbs lbs lbs. The Concorde RG-24-11or RG can also be used as no venting is required. Cap and stow or remove the existing manifold vent line. Install NAS 43HT4-48 spacer or equivalent ¾ inch spacer on hold down bolts below heat shield if these batteries are used. Concorde RG24-9 Concorde RG24-10 Concorde CB24-11 Concorde CB24-11XC Concorde RG24-11 Concorde RG24-12 Concorde RG24-15 Concorde RG AH 8.5AH 10 AH 15 AH 11AH 11 AH 13.6 AH 13.6 AH 22lbs. 22lbs. 27 lbs. 31 lbs lbs lbs lbs lbs. Concorde RG AH 42 lbs. TITLE: Applicability List, Cessna, Light Aircraft, Multiple Models DWG. NO REV. E CAGE CODE: DRAWN: DGG 6/28/02 CHECKED JBT 6/29/02 APPROVED JBT 7/16/02 ISSUED NS 2/27/07 SHEET: 12 OF 13

24 Prepared by Donald G. Grunke, BSEE, Concorde Battery Corp., Wichita, Kansas. (316) Checked by John Newman, DER Electrical, Newman Consulting LLC, Bethany, OK (405) Revisions Rev. Description Date Approved A Add obsolete Cessna 35AH P/N s 8/16/02 JBT B Corrected S/N for 182N, 182P 3/24/04 JBT C Added R /25/06 JBT D Corrected S/N for: 172F (USAF T-41A), 172K, 172N, 172P, 182B, 182C, 182Q, 182R, 182S, 177RG, 180K, A185F P206E/TP206E, U206F/TU206F, 337F, T337H-SP, 207A/T207A, 150C, 150D, A152, 177, 337B, 337H/T337H, 305B, A150K, A152, 401B Added Model No. 310, 310A(USAF U-3A), 310B, 310C, 310D, 310E(USAF U-3B), 310F, 310G, 310H, E310H, E310I, 310J, 310J-1, E310J, E310K, 310L, 310N, 310P, T310P, 310Q, T310Q, 310R, T310R, 320, 320-1, 320A, 320B, 320C, 320D, 320E, 320F, 340, 340A, 335, 411, 411A, 401, 401A, 401B, 402, 402A, 402B, 414, 414A, 402C, 421, 421A, 421B, 421C, 404, T303, 188A, 190, 195, 195A and 195B Added RG24-20, RG24-12 and RG24-9 2/15/07 JBT E Added RG /26/07 JBT TITLE: Applicability List, Cessna, Light Aircraft, Multiple Models DWG. NO REV. E CAGE CODE: DRAWN: DGG 6/28/02 CHECKED JBT 6/29/02 APPROVED JBT 7/16/02 ISSUED NS 2/27/07 SHEET: 13 OF 13

25 CESSNA INSTALLATION INSTRUCTIONS 1.0 REMOVAL 1.1 Assure that the "Battery Master Switch" is "OFF". 1.2 Gain access to the battery compartment and loosen the battery hold downs, if not secured by the battery box lid. 1.3 Disconnect the vent tubes if installed on the battery. Cap and stow if replacement battery is not manifold type. 1.4 Disconnect the battery cables. Always disconnect the Negative cable first and reconnect it last for safety reasons. 1.5 Remove the battery and PROPERLY DISPOSE OF IT. 1.6 Clean the battery compartment and inspect the cables and connector for airworthiness. Refer to applicable service manuals instructions for cleaning, repairs and/or preventive maintenance operations on battery compartment. 2.0 INSTALLATION 2.1 Install the fully charged Concorde Battery in the battery compartment. 12 volt 205, 206, 207, & 210 installations require trimming of the battery lifting hand hold per Concorde Drawing to provide clearance in firewall recess. Engage the battery hold down if not secured by the battery box lid, tighten and safety wire. Reconnect battery cables, Negative cable last. 2.2 Close up battery compartment and secure the aircraft. 12 volt plastic battery boxes may require trimming of the lid per the Concorde Drawing Make entry into the aircraft records to show the accomplishment of this battery installation, including a change of the aircraft weight and balance if the replacement battery has a weight different from the battery being replaced. Refer to the flight manual or appropriate document to determine station number of battery location. 3.0 MAINTENANCE 3.1 The RG series battery requires no maintenance other than inspection of connections for security. This battery requires no added water. 3.2 Refer to the latest revision of Concorde Battery Corporation Instructions for Continued Airworthiness (ICA) for periodic inspection requirements and test procedures for the battery selected. The ICA is available on the Concorde battery web site at TITLE: Installation Instructions, Cessna, Light Aircraft, Multiple Models DWG NO REV. NC CAGE CODE: DRAWN: JBT 6/28/02 CHECKED: AMIII 7/8/02 APPROVED: JBT 7/9/02 ISSUED: AT 7/9/02 SHEET: 1 OF 1 1

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46 1. CESSNA MODELS 205, 206, 207, AND 210 REQUIRE THE MODIFICATION OF THE BATTERY IN ORDER TO FIT WITHIN THE BATTERY BOX IN THE AIRCRAFT. 2. THE MODIFICATION OF THE BATTERY INVOLVES THE REMOVAL OF THE HANDLE THAT IS MOLDED ON THE REAR PORTION OF THE BATTERY. THIS MAY BE ACCOMPLISHED WITH A UTILITY KNIFE, SAW, OR OTHER CUTTING INSTRUMENT. CARE MUST BE TAKEN TO AVOID CUTTING THROUGH THE TOP OF THE BATTERY COVER ITSELF. 3. FOR CB SERIES BATTERIES, COMPLETELY REMOVE THE REAR HANDLE. 4. FOR RG SERIES BATTERIES, REMOVE ONLY THAT PORTION OF THE HANDLE FROM THE OUTSIDE OF THE VENT MANIFOLD (VERTICAL PLASTIC WALL) REARWARD.

47 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS MAINTENANCE MANUAL SUPPLEMENT CONCORDE VALVE REGULATED LEAD-ACID MAIN BATTERY This document must be used in conjunction with the basic Maintenance Manual for the aircraft when the Concorde Lead-Acid Battery is installed. This Maintenance Manual Supplement modifies/augments the portions of the basic Maintenance Manual. The data/information contained herein has been reviewed and approved for general release on the basis that this document contains no export-controlled information TITLE Instructions for Continued Airworthiness, Concorde Valve Regulated Lead-Acid Main Battery DWG NO REV J CAGE CODE DRAWN JBT 6/20/02 CHECKED EFK 6/20/02 APPROVED JBT 6/20/02 ISSUED NS 2/20/07 SHEET 1 OF 11

48 RECORD OF REVISIONS Rev. No. Description Date Appd A B C D E F 1. Delete flooded batteries, 2. Revised inspection interval, 3. Add mandatory removal interval, 4. Deleted flooded battery facility requirement. 1. Revised inspection interval 8, 2. Removed 282 Charger from 8.(b). 10.b ii (1) and 13.C i (a). 1. Revised installation instructions 2. Revised note on experience rating 3. Add note on deeply discharged batteries 4. Revised servicing instructions. 5. Added non scheduled inspections 1. Revised installation and removal notes. 2. Revised torque specifications. 3. Revised battery charger types. 1. Rev cap test to C1 rate. 2. Rev cutoff voltage for conditioning procedure 3. Add warning re conditioning charge. 1. Revised format 2. Assigned Drawing Number 3. Minor text revisions 2/16/99 JBT 4/20/99 JBT 9/5/00 JBT 6/18/01 JBT 1/30/02 JBT 6/20/02 JBT G Delete reference to warranty, para 13 1/16/03 JBT H Completely revised 6/12/03 JBT J Add limitation specified in TSO-C173 Add full charge voltage to storage limitations. Add export review statement. 2/20/07 JBT TITLE Instructions for Continued Airworthiness, Concorde Valve Regulated Lead-Acid Main Battery DWG NO REV J CAGE CODE SHEET 2 OF 11

49 CONTENTS 1. Scope Purpose Application Definitions Precautions: Airworthiness Limitations Installation and Removal Inspection Requirements and Overhaul Schedule: Troubleshooting: Servicing discharged batteries: Repair / Replacement: Facilities: Storage Limitations: Disposal: TITLE Instructions for Continued Airworthiness, Concorde Valve Regulated Lead-Acid Main Battery DWG NO REV J CAGE CODE SHEET 3 OF 11

50 1. Scope: This Maintenance Manual Supplement provides the additional data required to insure satisfactory operation, maintenance, and repair of the Concorde valve regulated lead-acid battery installation. 2. Purpose: This manual sets forth the instructions for determining continued airworthiness of a Concorde valve regulated lead-acid battery. 3. Application: Concorde valve regulated aircraft batteries - RG series. 4. Definitions: a. Valve regulated battery - A lead-acid battery in which there is no free electrolyte. This battery requires no maintenance of the liquid level and recombines the gases formed on charge within the battery. The battery may be used in any attitude without danger of leakage or spilling of electrolyte. b. Rated capacity C1 - Quantity of electricity in Ampere-hours (Ah) which the cell or battery is capable of delivering in 1 h. c. End Point Voltage (EPV) - Unless otherwise stated, during discharge the battery voltage corresponding to a mean voltage per cell of 1.67 Volts for lead-acid batteries. (10 EPV for 12 volt and 20 EPV for 24 volt batteries). 5. Precautions: a. CAUTION: Aircraft batteries are certified to have certain minimum capacity for emergency operations in the event of a electrical generator system failure. Never jump start an aircraft that has a discharged or dead battery. b. WARNING: ELECTRIC SHOCK HAZARD. Do not touch uninsulated portion of the connector or the battery terminals. A possibility of serious electrical shock exists. c. WARNING: ELECTRIC SHOCK HAZARD. Do not lay tools or other metal objects on the battery as arcing or explosion could occur. Remove conductive jewelry before working around battery, charger, or test equipment. d. CAUTION: ELECTRIC BURN HAZARD. Do not wear conductive rings, belt buckles, or other jewelry when working with batteries, chargers, or test equipment. Do not lay tools or other metal objects on the battery as arcing and severe burns could occur. e. WARNING: Batteries on charge or discharge produce hydrogen gas, which can explode if ignited. Do not smoke, use an open flame, or cause sparking near a battery. Charge, service or test a battery only in a well ventilated area. The use of exhaust fans may reduce the risk of explosion. f. WARNING: Batteries contain sulfuric acid which will cause burns. DO NOT TOUCH EYES AFTER TOUCHING BATTERY. Do not get acid in your eyes, or on your skin, or clothing. In the event of acid in the eyes, flush thoroughly with clean cool water for several minutes. Get professional medical attention. Refer to battery MSDS for additional information. g. WARNING: Wear proper eye, face and hand protection at all times when TITLE Instructions for Continued Airworthiness, Concorde Valve Regulated Lead-Acid Main Battery DWG NO REV J CAGE CODE SHEET 4 OF 11

51 working with batteries. Know the location and use of emergency eyewash and shower nearest the battery charging area. h. CAUTION: To prevent damage to the connector, arc burns, or explosion, batteries should never be connected or disconnected while being charged or discharged. Batteries must be connected or disconnected only when the circuit is open. Ensure the aircraft battery switch, external power source, or the charger/analyzer is in the OFF position before connecting or disconnecting the battery. Battery terminal protectors should be installed whenever the battery is not connected in the aircraft or to the test equipment. i. CAUTION: Batteries contain hazardous materials. Know the location and proper use of emergency response materials. Refer to battery Material Safety Data Sheet (MSDS) for additional information. j. Caution / Warning: Only constant potential charging may be done on the aircraft. DO NOT constant current charge a battery on the aircraft. There may be a serious risk of injury to personnel and / or damage to the aircraft or aircraft systems due to high voltage and generation of explosive gases when charging constant current. 6. Airworthiness Limitations: a. There are no airworthiness limitations associated with the installation of a Concorde valve-regulated lead-acid battery in an aircraft. b. For batteries covered by TSO-C173 the following limitation applies: Note: The conditions and tests for this TSO approval of this battery are minimum performance standards. Those installing this battery, on or in a specific type or class of aircraft, must determine that the aircraft installation conditions are within the TSO standards. TSO articles must have separate approval for installation in an aircraft. The article may be installed only according to 14CFR part 43 or the applicable airworthiness requirements. Nickel-cadmium and lead-acid battery safety concerns include the possibility of fire and venting violently. 7. Installation and Removal: NOTE: The following instructions are generic. See airframe manufacturer s maintenance manuals or STC for instructions specific to a particular aircraft model. For removal and replacement of a nickel- cadmium battery, see airframe maintenance manual STC. a. Installation procedure: i. Removal: (1) Set Master Switch to the OFF position. (2) Disconnect any external power supply. (3) Open battery compartment access panels. (4) Disconnect battery quick disconnect plug or remove terminal bolts and disconnect battery cables from battery terminals. Always disconnect the ground cable first and install the ground cable last. TITLE Instructions for Continued Airworthiness, Concorde Valve Regulated Lead-Acid Main Battery DWG NO REV J CAGE CODE SHEET 5 OF 11

52 (5) Disconnect battery ventilation tubes, if any. (6) Unlock battery hold down clamps or remove battery hold down bars. Disengage battery. (7) Carefully remove battery. WARNING: Batteries are heavy. Use appropriate lifting devices or equipment. Use battery handles where provided. ii. Installation: (1) Inspect the battery for damage. Cracks in metal or plastic containers are not permitted. Dents in metal containers that impinge on the interior plastic container are not acceptable. (2) Set Master Switch to the OFF position. (3) Disconnect any external power supply. (4) Open battery compartment access panels. (5) Ensure the battery container or tray is clean and dry. (6) Install battery in battery container or tray. WARNING: Batteries are heavy. Use appropriate lifting devices or equipment. Use battery handles where provided. (7) Engage battery hold down hardware, torque and safety wire per airframe manufacturer maintenance manual. (8) Connect battery vent tubes to aircraft ventilation system, if any. (9) Connect battery quick disconnect plug, any auxiliary connector or for ring terminals, install with bolt and bevel lock washer provided with the battery. Torque terminal bolts as noted on the battery label. Always disconnect the ground cable first and install the ground cable last. CAUTION: Use an open end wrench on the flats of the battery terminal, where available, while torquing the terminal bolts. Failure to do so may result in the rupture of the battery seal at the terminal and premature failure of the battery. CAUTION: Use only the hardware provided with the battery. Do not use stainless steel or steel washers between the ring terminal and the battery terminal. (10) Replace electrical compartment access panel. (11) Update aircraft weight and balance data, if necessary. (12) Perform an operational test. (13) Annotate log book with battery serial number and date of installation. 8. Inspection Requirements and Overhaul Schedule: a. Scheduled inspections: NOTE: If the battery is used to satisfy the essential power requirement, it must be capacity tested. If the battery is not used for essential power, there is no requirement for periodic capacity checks. TITLE Instructions for Continued Airworthiness, Concorde Valve Regulated Lead-Acid Main Battery DWG NO REV J CAGE CODE SHEET 6 OF 11

53 i. If the battery is being used to start a turbine APU or a reciprocating engine, the battery can be operated for 24 months or 1200 hours of operation whichever occurs first before the initial capacity check. Subsequent capacity checks are due each additional 12 months or 200 hours of operation, whichever occurs first. ii. If the battery is used to start a Turbine engine, regardless of whether or not it is also being used to start a turbine APU, the initial capacity check is at 12 months or 600 hours of operation, whichever occurs first. Subsequent capacity checks are due each additional 3 months or 200 iii. hours of operation whichever occurs first. Two (2) or more batteries operated in parallel should be replaced together for maximum reliability. Replacing only one battery in a parallel string results in unequal charge acceptance as the resistance of the new battery is much different than the resistance of the older battery. NOTE: The initial recommended inspection schedule may be adjusted to coincide with the airframe or engine manufacturer s inspection interval so long as the operating time does not exceed the above limits by more than 10% or 60 hours. The inspection schedule may be adjusted after the useful battery life is established in a particular operation. After the useful life of a battery is established for a particular aircraft or operating mode, the actual useful life period in months or hours may be substituted for the above schedule. b. Non-scheduled Inspections: i. Capacity check if abnormal slow engine starting performance is noted. ii. Capacity check if abnormal high charging current is required to maintain the battery at buss voltage. c. Inspection Procedure: i. Charge the battery: (1) Special tools: (a) (b) (c) Advanced Power Products Beta D-50 Aircraft Battery Analyzer, P/N 4126, or equal. Advanced Power Products Alpha C-25 Battery Charger, P/N 4142, or equal. Advanced Power Products CA15-50 Charger/analyzer P/N 4159, or equal. Warning: Contact Concorde for determination of equal test equipment. Some brands of battery chargers will destroy the battery. (2) Depending on the type of charger available, charge the battery Constant Potential (CP). Charge at 14.1 volts for 12 volt batteries or 28.2 volts for 24 volt batteries until the charge current stabilizes for 1 hour. Caution / Warning: Only constant potential charging may be done on the aircraft. DO NOT constant current charge a battery on the aircraft. There may be a serious risk of injury to personnel and / or TITLE Instructions for Continued Airworthiness, Concorde Valve Regulated Lead-Acid Main Battery DWG NO REV J CAGE CODE SHEET 7 OF 11

54 damage to the aircraft or aircraft systems. ii. Capacity test: (1) Stabilize the battery at 15 C (59 F) or higher. The battery must be at the temperature for at least 24 hours. (2) Discharge the battery at the C1 rate on the label to an end point voltage of 10 volts for 12 volt batteries or 20 volts for 24 volt batteries, or the rate and end point voltage (EPV) specified by the airframe manufacturer for essential power. (3) Record the time to EPV. (4) The battery is acceptable for continued use if the ampere hour capacity (actual hours of discharge x ampere rate of discharge) is greater than 85% of the nominal rated capacity (C1) shown on the label (i.e. 51 minutes or more). If the battery passes the capacity test return it to service. If the battery fails the capacity test perform a conditioning procedure (13. c.). After the battery has been conditioned perform a second capacity test. If the battery passes return it to service. If the battery fails replace it. NOTE: Airframe or accessory equipment manufacturers may specify a different capacity requirement. iii. Return to service: Charge the battery as above. If the battery gets very hot (external case temperature greater than 55 C (130 F)) during charging, it should be replaced. d. Component Overhaul Schedule: No component overhaul required for this type product. 9. Troubleshooting: Symptom Probable Cause Corrective Action Low voltage / no voltage Battery does not hold charge Battery gets hot while recharging Battery partially or fully discharged Battery beyond serviceable life Battery beyond serviceable life Charge in accordance with Section 8 Replace battery Replace battery 10. Servicing discharged batteries: a. Recharging dual (parallel) batteries on the aircraft should be done individually. b. Recharging a single battery on the aircraft: i. Special tools: (1) Advanced Power Products Activator 282 Battery Charger, P/N 4105, or equal constant potential charger. (2) The Activator 282 is fully automatic. Connect to battery and initiate TITLE Instructions for Continued Airworthiness, Concorde Valve Regulated Lead-Acid Main Battery DWG NO REV J CAGE CODE SHEET 8 OF 11

55 charging. If using a constant potential charger, follow instructions below. Caution / Warning: Only constant potential charging may be done on the aircraft. Ensure the charging area is well ventilated. DO NOT constant current charge a battery on the aircraft. There may be a serious risk of injury to personnel and / or damage to the aircraft and aircraft systems. Warning: Contact Concorde for determination of equal test equipment. Some brands of battery chargers will destroy the battery. ii. Set the charger for 2.35 volts per cell (14.1 volts for a 12 volt battery, 28.2 volts for a 24 volt battery). iii. Set the current limit to the C1 rate. NOTE: If current on external power unit is not adjustable, do not charge the battery in the aircraft iv. Initiate charging and continue to charge until the charge current stabilizes for 1 hour. c. Uninstalled recharging: i. Remove the battery from the aircraft. ii. iii. Special tools: (1) Advanced Power Products Alpha C-25 Battery Charger, P/N 4142; Advanced Power Products CA15-50 Charger/analyzer P/N 4159; or equal. Warning: Contact Concorde for determination of equal test equipment. Some brands of battery chargers will destroy the battery. Depending on the type of charger available, charge the battery Constant Potential (CP). Charge at 14.1 volts for 12 volt batteries or 28.2 volts for 24 volt batteries until the charge current stabilizes for 1 hour. NOTE: Batteries that have been allowed to stand in a deeply discharged state may not accept a CP recharge. See conditioning procedure in paragraph 13.c for handling those batteries. 11. Repair / Replacement: a. Repairs should be performed only by a Concorde approved battery shop. b. Replacement may be made by removing and installing a new battery in accordance with the instructions in this supplement. c. The battery should be replaced after 3 years or 1800 hours of operation or whichever occurs first. 12. Facilities: Valve regulated batteries may be serviced in any battery facility, including nickel-cadmium service facilities. The battery is sealed to prevent cross contamination of the electrolyte. TITLE Instructions for Continued Airworthiness, Concorde Valve Regulated Lead-Acid Main Battery DWG NO REV J CAGE CODE SHEET 9 OF 11

56 13. Storage Limitations: a. Batteries are serviced and charged at the factory prior to shipment. i. For maximum battery life, boost charge when open circuit voltage is below 25.0 volts for 24 volt batteries and 12.5 volts for 12 volt batteries. The normal voltage for a fully charged battery is approximately 26 volts for 24 volt batteries and 13 volts for 12 volt batteries. ii. Batteries that have not been recharged when stored for long periods are to be conditioned (13.c) and tested (8.c) before being placed in service. b. Boost charging procedure: i. Special tools: (1) Advanced Power Products Alpha C-25 Battery Charger, P/N 4142; Advanced Power Products Activator 282 Battery Charger, P/N 4105; Advanced Power Products CA15-50 charger/analyzer, P/N 4159; or equal. ii. Depending on the type of charger available, charge the battery Constant Potential (CP). Charge at 14.1 volts for 12 volt batteries or 28.2 volts for 24 volt batteries until the charge current stabilizes for 1 hour. c. Conditioning procedure: Warning: The battery must be removed from the aircraft prior to performing a conditioning charge. i. Special tools: (1) Advanced Power Products Beta D-50 Aircraft Battery Analyzer P/N 4146 or 4159, or equal. (2) Advanced Power Products Alpha C-25 Battery Charger P/N 4142 or 4159, or equal. Warning: Contact Concorde for determination of equal test equipment. Some brands of battery chargers will destroy the battery. ii. Procedure: (1) Discharge the battery at the C1 rate to an end point voltage of 9 volts for 12 volt batteries and 18 volts for 24 volt batteries. (2) Constant current charge at the C1 /10 rate for 16 hours. WARNING: This procedure may damage the battery if performed on a repetitive basis. (3) Allow the battery to cool down for 8 hours. (4) Retest the battery following the inspection procedure (8.c). 14. Disposal: a. Batteries contain lead, sulfuric acid, and other hazardous materials. Dispose of all spent batteries in accordance with local laws and regulations. See battery Material Safety Data Sheet (MSDS) for additional information. b. Lead acid batteries are recyclable. CAUTION: Some aircraft batteries are encased in aluminum containers. These containers must be removed prior to recycling. TITLE Instructions for Continued Airworthiness, Concorde Valve Regulated Lead-Acid Main Battery DWG NO REV J CAGE CODE SHEET 10 OF 11