Page No. 1 of 6 Date: April 29, 2011 Installation Eligibility: Model. PMA NUMBER PQ2724CE Part No. Model No.
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1 PMA NUMBER No. FAA Approval Basis and Approved Design Data Eligibility: Make Page No. 1 of 6 Propeller ATG Woodward G P210452( ), , Test Report and Alexandria 17-30, 17-30A (IO-520 only) Aircraft Cont. IO-520 (2850 RPM) Edo-Aire (Bellanca) Note: For IO-550 use AT210937(A) (2700 RPM) Propeller ATM Woodward M B210460, , A Test Report and Alexandria 17-31, 17-31TC, 17-31A, 17-31ATC Aircraft Edo-Aire (Bellanca) IO-540-G1B5, E5, F5, K1A5, B5, E5 (non "A" engines) (2575 RPM) Propeller ATN Woodward N A Test Report and Alexandria 17-31, 17-31TC, 17-31A, 17-31ATC Aircraft Edo-Aire (Bellanca) IO-540-G1B5, E5, F5, K1A5, B5, E5 (non "A" engines) (2700 RPM) Propeller ATP Woodward P B210460, , A Test Report and Alexandria 17-31, 17-31TC, 17-31A, 17-31ATC Aircraft Lycoming (.947:1) Edo-Aire (Bellanca) IO-540-K1E5 and all engine serials ending with "A" (2700 RPM) Propeller ATB Woodward B None Test Report and American 8GCBC Champion Lycoming (.866:1) C1A, C1E C2A, C2E (2700 RPM) Propeller ATB Woodward B None Test Report and Computations American 8KCAB Per 14 CFR ( C ) ( 4 ) or Later FAA Approved Champion Revisions (Decathlon) AEIO-360-H1B only (2700 RPM) Propeller ATF4-4A-1 Woodward T None Test Report and Computations American 8GCBC Per 14 CFR ( C ) ( 4 ) For use with ACA P/N or Later FAA Approved Champion Control Mounting Bracket only Revisions (Scout) C1G only (2700 RPM) Propeller ATT Woodward T None Test Report and American 8GCBC Champion (Scout) C1G only (2700 RPM)
2 Page No. 2 of 6 No. Propeller ATD210688D Woodward D None Test Report and American 8KCAB Oil to decrease pitch, for Champion IO-320-E1A, B, AEIO-320-E1B, 2B counterweighted props only (Decathlon) AEIO-360-H1A only (2700 RPM) Propeller ATF Hartzell ATF None Test Report and American 8KCAB Champion (Decathlon) AEIO-360-H1B only (2700 RPM) Propeller ATF6-58 Hartzell F-6-58Z F-6-58( ) Test Report and Sky S-1T (S/N 1007 & up), S-2A (S/N International 2206 & up) (Pitts) AEIO-360-A1E (2700 RPM) Propeller ATF6-59 Hartzell F-6-59Z F-6-59( ) Test Report and Sky S-2B, C & S International Lycoming (.947:1) (Pitts) AEIO-540-D4A5 (2700 RPM) Propeller ATB Woodward B F210452, J210452, B Test Report and Cessna / R172E, F, G, H & J Reims FR172E, F, G, H & J McCauley C290D( )/T6 C290D2/T6 Cont. IO-360 (2800 RPM) Propeller ATA210760L Woodward A , , Test Report and Cessna / 180, 180A, B, C, D, E, F, G, H & J , A210452, A Reims 182, 182A, B, C, D, E, F, G, H, J McCauley C290D( )/T1 C290D2/T1 K, L, M, N & P, F182 P, Garwin ( ) 188, 188A & 188B Edo-Aire ( ) Cont. O-470 (2600 RPM) ATA210760LD Woodward , decrease pitch PCU5000 for counterweighted props only Propeller ATJ Woodward J Test Report and Cessna / 180K, 182Q, 182R & F182Q McCauley C290D( )/T14 C290D( )/T14 Reims Cont. O-470U (2400 RPM)
3 PMA NUMBER No. FAA Approval Basis and Approved Design Data Eligibility: Make Page No. 3 of 6 Propeller ATA210760H Woodward A , A Test Report and Cessna 185, 185A, B, C, D & E or Hoof McCauley C290D( )/T1 Cont. IO-470 (2625 RPM) Garwin C290D2/T1 ATA210760HD Woodward , decrease pitch PCU5000 for counterweighted props only Propeller ATG Woodward G A210462, B210419, P Test Report and Cessna A185E, F, A188, A188A, B McCauley C290D( )/T9 C290D2/T9 Cont. IO-520 (2850 RPM) Garwin Edo-Aire ATA210760HD Woodward , decrease pitch PCU5000 for counterweighted props only Propeller AT Woodward , , A210452, Test Report and 205, 205A, 210A, B & C (210452), A210680, , 210, (205), 210-5A (205A) , , FAA Approved Cont. IO-470 (2625 RPM) Propeller ATC Woodward C D210452, A Test Report and Cessna 206, U206, U206A, P206, P206A, McCauley C290D( )/T5 C290D2/T5 P206B, P206C, P206D & P206E, 210D, E, F, G, H & J Cont. IO-520, 550 (2700 RPM) Propeller AT Woodward G210452, (210462), ( ) Test Report and Cessna T188C, TP206A -E, TU206A -G, T207, T207A, P210N, P210R, McCauley C290D( )/T2 C290D2/T2, C290D4/T2 T210F - H, J - N & R C290D4/T19, C TSIO-520C, H, P, R (2700 RPM)
4 Page No. 4 of 6 No. Propeller AT Woodward (210462), L210452, A210419, Test Report and Cessna 207, 207A, 210K, L, M, N & R ( ) U206B, U206C - G, McCauley C290D( )/T4 C290D2/T4 Cont. IO-520 (2850 RPM) C290D( )/T2 Propeller ATB Woodward B F210452, B Test Report and Maule M-4-210C, S, T, M-5-210C Cont. IO-360 (2800 RPM) Propeller ATB Woodward B F210452, J210452, B Test Report and Maule M5-235, M6-235, M7-235, A, B, C MX7-235, M8-235 McCauley C290D( )/T6 C290D2/T6 Lycoming (.947:1) IO-540( ) (2400 RPM) Propeller ATE Woodward E F210452, J210452, B Test Report and Maule M5-235, M6-235, M7-235, A, B, C MX7-235, M8-235 McCauley C290D( )/T6 C290D2/T6 IO-540( ) (2575 RPM) Propeller ATH-1 Hartzell D-1, H-1 None Test Report and Mooney M20, 20A, B, C, D, E, F & G Lycoming (.866:1) O-360-A1A, A1D, A2D IO-360-A1A (2700 RPM) Propeller ATB4-2 Hartzell B-4-2 None Test Report and Piper PA O-540-A1A (2575 RPM)
5 No. Propeller ATF4-1A Hartzell F-4-1A None Test Report and Piper PA Page No. 5 of 6 O-720-A1A, A1B (2650 RPM) Propeller ATF4-4A Hartzell F-4-4A( ) F-4-4( ) Test Report and Piper PA , PA , 300, PA-32S-300 IO-540( ) (2700 RPM) Propeller ATG Woodward G None Test Report and Piper PA T, PA-28R-201T, PA28RT-201T Hartzell E-5 Cont. TSIO-360-F Cont. TSIO-360-FB (2575 RPM) Propeller ATF4-3A Hartzell F-4-3A( ) F-4-3( ) Test Report and Piper PA IO-540( ) (2575 RPM) Propeller ATF4-13 Hartzell F-4-13( ) F-4-13( ) Test Report and Piper PA Engines with serial numbers ending with " A" Lycoming Wide Deck (.947:1) IO-540( ) (2575 RPM) Propeller ATF4-21 Hartzell F-4-21( ) F-4-21( ) Test Report and Piper PA Lycoming Wide Deck (.947:1) IO-540( ) (2400 RPM) Propeller ATF2-7A Hartzell F-2-7A None Test Report and Piper PA-28R-180, -200, -201, PA-28RT-201 IO-360-B1E, -C1C, -C1C6 Lycoming (.866:1) (2700 RPM)
6 Page No. 6 of 6 No. Propeller ATF4-11B Hartzell F-4-11B( ) F-4-11( ) Test Report and Piper PA , 300, PA-32S-300, PA-32R-300, PA-32RT-300, 300T PA-32, 32R-301, 301T, Engines with serial numbers ending with " A" Lycoming Wide Deck (.947:1) IO, TSIO-540( ) (2700 RPM) Propeller ATA210760L Woodward V H, , , Test Report and Hawker H35, J35, K35, M35, A, , , Beechcraft 35-A33, 35-B33, 35-C33, E , A F33 Hartzell B4-3 Cont. O, IO-470 (2600 RPM) Garwin Note: For IO-520, 550 use ATD (2700 RPM) Propeller ATA210760H Woodward V , , , Test Report and Hawker N35, P35, G33 A Beechcraft Cont. IO-470 (2625 RPM) Note: For IO-520, 550 use ATD (2700 RPM) Propeller ATD Woodward D C210452, D Test Report and Hawker S35, V35, V35A, V35B, 35-C33A Beechcraft E33A, E33C, 36, A36, F33A, McCauley C290D( )/T23 F33C, A36TC, B36TC Cont. IO-520, 550 (2700 RPM) Cont. TSIO-520, 550 (2700 RPM) Propeller ATF Woodward F E210681, M Test Report and Socata TB20, TB21 Lycoming (.947:1) IO-540-C4D5D (2575 RPM) TIO-540-AB1AD (2575 RPM)
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