Ad/LYC/119 - ECi Cylinder Assemblies (Cth)

Case
No judgment structure available for this case.

AIRWORTHINESS DIRECTIVE

For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.001(1) of CASR 1998.  The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

Lycoming Piston Engines

AD/LYC/119 ECi Cylinder Assemblies 12/2008 DM

Applicability:

Lycoming Engines (formerly Textron Lycoming) models 320, 360, and 540 series, ''Parallel Valve'', reciprocating engines listed in Table 1 of this AD, with Engine Components, Inc (ECi) cylinder assembly, part number (P/N) AEL65102 series “Titan”, and with cylinder head, P/N AEL85099, with the following serial numbers (S/N) installed.

a.    Cylinder assembly S/N 1138-02 through SN 35171- 22, (referred to in this AD as Group ''A'' cylinder assemblies); and

b.    S/N 35239-01 through SN 37016-28 (referred to in this AD as Group ''B'' cylinder assemblies).

Note 1:  The cylinder assembly P/N is at the crankcase end of the cylinder assembly, and might be difficult to see.  As a guide in determining if your cylinder assemblies are affected, all affected cylinder assemblies have cylinder head P/N AEL85099.  The cylinder head P/N is at the top the cylinder head, near the intake and exhaust valve springs, and is easier to locate than the cylinder assembly P/N.

Note 2:  The set of numbers appearing on the cylinder, above and to the left of the SN, in the form of ''123456'' is not used for determining applicability.

This AD is not applicable to engines not overhauled or which have not had any cylinder assemblies replaced since new.

Table 1 - Engine Models

Cylinder Assembly Part Number: Installed on Engine Models:
AEL65102-NST04

O-320-A1B, A2B, A2C, A2D, A3A, A3B, B2B, B2C, B2D, B2E, B3B, B3C, C2B, C2C, C3B, C3C, D1A, D1AD, D1B, D1C, D1D, D1F, D2A, D2B, D2C, D2F, D2G, D2H, D2J, D3G, E1A, E1B, E1C, E1F, E1J, E2A, E2B, E2C, E2D, E2E, E2F, E2G, E2H, E3D, E3H

IO-320-A1A, A2A, B1A, B1B, B1C, B1D, B1E, B2A, D1A, D1AD, D1B, D1C, E1A, E1B, E2A, E2B

AEIO-320-D1B, D2B, E1A, E1B, E2A, E2B

AIO-320-A1A, A1B, A2A, A2B, B1B, C1B

LIO-320-B1A

AEL65102-NST05

IO-320-C1A, C1B, C1F, F1A

LIO-320-C1A

AEL65102-NST06

O-320-A1A, A2A, A2B, A2C, A3A, A3B, A3C, E1A, E1B, E2A, E2C, (also, an O-320 model with no suffix)

IO-320-A1A, A2A

AEL65102-NST07

IO-320-B1A, B1B

LIO-320-B1A

AEL65102-NST08 O-320-B1A, B1B, B2A, B2B, B3A, B3B, B3C, C1A, C1B, C2A, C2B, C3A, C3B, C3C, D1A, D1B, D2A, D2B, D2C
AEL65102-NST10

O-360-A1A, A1C, A1D, A2A, A2E, A3A, A3D, A4A, B1A, B1B, B2A, B2B, C1A, C1C, C1G, C2A, C2B, C2C, C2D, D1A, D2A, D2B

IO-360-B1A, B1B, B1C

HO-360-A1A, B1A, B1B

HIO-360-B1A, B1B

AEIO-360-B1B

O-540-A1A, A1A5, A1B5, A1C5, A1D, A1D5, A2B, A3D5, A4A5, A4B5, A4C5, A4D5, B1A5, B1B5, B1D5, B2A5, B2B5, B2C5, B2C5D, B4A5, B4B5, B4B5D, D1A5, E1A, E4A5, E4B5, E4C5, F1A5, F1B5, G1A5, G2A5

IO-540-C1B5, C1C5, C2C, C4B5, C4B5D, C4C5, D4A5, D4B5, N1A5, N1A5D

AEL65102-NST12

O-360-A1A, A1AD, A1D, A1F, A1F6, A1F6D, A1G, A1G6, A1G6D, A1H, A1H6, A1J, A1LD, A1P, A2A, A2D, A2F, A2G, A2H, A3A, A3AD, A3D, A4A, A4AD, A4D, A4G, A4J, A4JD, A4K, A4M, A4N, A4P, A5AD, B1A, B2C, C1A, C1C, C1E, C1F, C1G, C2A, C2B, C2C, C2D, C2E, C4F, C4P, D2A, F1A6, G1A6

HO-360-C1A

LO-360-A1G6D, A1H6

HIO-360-B1A, B1B, G1A

LTO-360-A1A6D

TO-360-A1A6D

IO-360-B1B, B1BD, B1D, B1E, B1F, B1F6, B1G6, B2E, B2F, B2F6, B4A, E1A, L2A, M1A, M1B

AEIO-360-B1B, B1D, B1E, B1F, B1F6, B1G6, B1H, B2F, B2F6, B4A, H1A, H1B

O-540-A4D5, B2B5, B2C5, B2C5D, B4B5, B4B5D, E4A5, E4B5, E4B5D, E4C5, G1A5, G1A5D, G2A5, H1A5, H1A5D, H1B5, H1B5D, H2A5, H2A5D, H2B5D

IO-540-C4B5, C4B5D, C4D5, C4D5D, D4A5, D4B5, D4C5, N1A5, N1A5D, T4A5D, T4B5, T4B5D, T4C5D, V4A5, V4A5D

AEIO-540-D4A5, D4B5, D4C5, D4D5

AEL65102-NST26

IO-540-J4A5, R1A5

TIO-540-C1A, E1A, G1A, H1A

AEL65102-NST38

IO-360-F1A

TIO-540-AA1AD, AB1AD, AB1BD, AF1A, AG1A, AK1A, C1A, C1AD, K1AD

LTIO-540-K1AD

AEL65102-NST43

O-360-J2A

O-540-F1B5, J1A5D, J1B5D, J1C5D, J1D5D, J2A5D, J2B5D, J2C5D, J2D5D, J3A5, J3A5D, J3C5D

IO-540-AB1A5, W1A5, W1A5D, W3A5D

AEL65102-NST44 O-540-L3C5D
AEL65102-NST07

IO-320-B1A, B1B

LIO-320-B1A

AEL65102-NST08 O-320-B1A, B1B, B2A, B2B, B3A, B3B, B3C, C1A, C1B, C2A, C2B, C3A, C3B, C3C, D1A, D1B, D2A, D2B, D2C
AEL65102-NST10

O-360-A1A, A1C, A1D, A2A, A2E, A3A, A3D, A4A, B1A, B1B, B2A, B2B, C1A, C1C, C1G, C2A, C2B, C2C, C2D, D1A, D2A, D2B

IO-360-B1A, B1B, B1C

B1A, B1B 

HO-360-A1A,

HIO-360-B1A, B1B

AEIO-360-B1B

O-540-A1A, A1A5, A1B5, A1C5, A1D, A1D5, A2B, A3D5, A4A5, A4B5, A4C5, A4D5, B1A5, B1B5, B1D5, B2A5, B2B5, B2C5, B2C5D, B4A5, B4B5, B4B5D, D1A5, E1A, E4A5, E4B5, E4C5, F1A5, F1B5, G1A5, G2A5

IO-540-C1B5, C1C5, C2C, C4B5, C4B5D, C4C5, D4A5, D4B5, N1A5, N1A5D

AEL65102-NST12

O-360-A1A, A1AD, A1D, A1F, A1F6, A1F6D, A1G, A1G6, A1G6D, A1H, A1H6, A1J, A1LD, A1P, A2A, A2D, A2F, A2G, A2H, A3A, A3AD, A3D, A4A, A4AD, A4D, A4G, A4J, A4JD, A4K, A4M, A4N, A4P, A5AD, B1A, B2C, C1A, C1C, C1E, C1F, C1G, C2A, C2B, C2C, C2D, C2E, C4F, C4P, D2A, F1A6, G1A6

HO-360-C1A

LO-360-A1G6D, A1H6

HIO-360-B1A, B1B, G1A

LTO-360-A1A6D

TO-360-A1A6D

IO-360-B1B, B1BD, B1D, B1E, B1F, B1F6, B1G6, B2E, B2F, B2F6, B4A, E1A, L2A, M1A, M1B

AEIO-360-B1B, B1D, B1E, B1F, B1F6, B1G6, B1H, B2F, B2F6, B4A, H1A, H1B

O-540-A4D5, B2B5, B2C5, B2C5D, B4B5, B4B5D, E4A5, E4B5, E4B5D, E4C5, G1A5, G1A5D, G2A5, H1A5, H1A5D, H1B5, H1B5D, H2A5, H2A5D, H2B5D

IO-540-C4B5, C4B5D, C4D5, C4D5D, D4A5, D4B5, D4C5, N1A5, N1A5D, T4A5D, T4B5, T4B5D, T4C5D, V4A5, V4A5D

AEIO-540-D4A5, D4B5, D4C5, D4D5

AEL65102-NST26

IO-540-J4A5, R1A5

TIO-540-C1A, E1A, G1A, H1A

AEL65102-NST38

IO-360-F1A

TIO-540-AA1AD, AB1AD, AB1BD, AF1A, AG1A, AK1A, C1A, C1AD, K1AD

LTIO-540-K1AD

AEL65102-NST43

O-360-J2A

O-540-F1B5, J1A5D, J1B5D, J1C5D, J1D5D, J2A5D, J2B5D, J2C5D, J2D5D, J3A5, J3A5D, J3C5D

IO-540-AB1A5, W1A5, W1A5D, W3A5D

AEL65102-NST44 O-540-L3C5D

For information, the Lycoming Engines (formerly Textron Lycoming) models 320, 360, and 540 series, “Parallel Valve”, reciprocating engines are installed on, but not limited to, the aircraft listed in the following Table 2:

Table 2 - Engines Installed On, But Not Limited To

Engine Models: Installed on , But Not Limited To:
O-320-A1A

Piper Aircraft: Tri-Pacer (PA-22 “150”, PA-22S “150”), Apache (PA-23), Pawnee (PA-25)

Doyn Aircraft: Doyn-Cessna (170, 170A, 170B)

Mooney Aircraft: Mark (20A)

Dinfia: Ranquel (1A-46)

Simmering-Graz Pauker: Flamingo (SGP-M-222)

Aviamilano: Scricciolo (P-19)

Vos Helicopter Co.: Spring Bok

O-320-A1B

Piper Aircraft: Tri-Pacer (PA-22 “150”, PA-22S “150”), Apache (PA-23)

Doyn Aircraft: Doyn-Cessna (170, 170A, 170B)

S.O.C.A.T.A.: Horizon (Gardan)

O-320-A2A

Piper Aircraft: Tri-Pacer (PA-22 “150”, PA-22S “150”), Agriculture (PA-18A “150”) Super Cub (PA-18 “150”), Caribbean (PA-22 “150”), Pawnee (PA-25)

Intermountain Mfg. Co.: Call Air Texas (A-5, A-5T)

Lake Aircraft: Colonial (C-1)

Rawdon Bros.: Rawdon (T-1, T-15, T-15D)

Shinn Engineering: Shinn (2150-A)

Dinfia: Ranquel (1A)46)

Neiva: (1PD-5802)

Sud: Gardan-Horizon (GY-80)

LaVerda: Falco (F8L Series II, America)

Malmo: Vipan (MF1-10)

Kingsford Smith: Autocrat (SCRM-153)

Aero Commander: 100

O-320-A2B

Piper Aircraft: Tri-Pacer (PA-22 “150”, PA-22S “150”), Cherokee (PA-28 “150”), Super Cub (PA -18 “150”)

Champion Aircraft: Challenger (7GCA, 7GCB, 7KC), Citabria (7GCAA, 7GCRC), Agriculture (7GCBA)

Beagle: Pup (150)

Artic: Interstate S1B2

Robinson: R-22

Varga: Kachina 2150A

O-320-A2C

Robinson: R-22

Cicare: Cicare AG

Bellanca Aircraft: Citabria 150 (7GCAA), Citabria 150S (7GCBC)

O-320-A2D Piper Aircraft: Apache (PA-23)
O-320-A3A

Doyn Aircraft: Doyn-Cessna (170, 170A, 170B)

Corben-Fettes: Globe Special (Globe GC-1B)

O-320-A3B

Piper Aircraft: Apache (PA-23)

Doyn Aircraft: Doyn-Cessna (170, 170A, 170B)

Teal II: TSC (1A2)

O-320-B1A

Piper Aircraft: Apache (PA-23 “160”)

Doyn Aircraft: Doyn-Cessna (170, 170A, 170B)

Malmo: Vipan (MF1-10)

O-320-B1B

Piper Aircraft: Apache (PA-23 “160”)

Doyn Aircraft: Doyn-Cessna (170, 170A, 170B)

O-320-B2A Piper Aircraft: Tri-Pacer (PA-22 “160”, PA-22S “160”)
O-320-B2B

Piper Aircraft: Tri-Pacer (PA-22 “160”, PA-22S “160”)

Beagle: Airedale (D5-160)

Fuji-Heavy Industries: Fuji (F-200)

Uirapuru: Aerotec 122

O-320-B2C Robinson: R-22
O-320-B2D Maule: MX-7-160
O-320-B2E Lycon
O-320-B3A

Piper Aircraft: Apache (PA-23 “160”)

Doyn Aircraft: Doyn-Cessna (170, 170A, 170B)

O-320-B3B

Piper Aircraft: Apache (PA-23 “160”)

Doyn Aircraft: Doyn-Cessna (170, 170A, 170B)

Sud: Gardan (GY80-160)

O-320-C1A

Piper Aircraft: Apache (PA-23 “160”)

Riley Aircraft: Rayjay (Apache)

O-320-C1B Piper Aircraft: Apache (PA-23 “160”)
O-320-C3A Piper Aircraft: Apache (PA-23 “160”)
O-320-C3B Piper Aircraft: Apache (PA-23 “160”)
O-320-D1A

Sud: Gardan (GY-80)

Gyroflug: Speed Cancard

Grob: G115

O-320-D1F Slingsby: T67 Firefly
O-320-D2A

Piper Aircraft: Cherokee (PA-28S “160”)

Robin: Major (DR400-140B), Chevalier (DR-360), (R-3140)

S.O.C.A.T.A.: Tampico TB9

Slingsby: T67C Firefly

Daetwyler: MD-3-160

Nash Aircraft Ltd.: Petrel

Aviolight: P66D Delta

General Avia: Pinguino

O-320-D2B

Beech Aircraft: Musketeer (M-23)

Piper Aircraft: Cherokee (PA-28 “160”)

O-320-D2J Cessna Aircraft: Skyhawk 172
O-320-D3G Piper Aircraft: Warrior II, Cadet (PA-28-161)
O-320-E1A Grob: G115
O-320-E1C M.B.B. (Messerschmitt-Boelkow-Blohm): Monsun
(BO-209-B)
O-320-E1F M.B.B.: Monsun (BO-209-B)
O-320-E2A

Piper Aircraft: Cherokee (PA-28 “140”, PA-28 “150”)

Robin: Major (DR-340), Sitar, Bagheera (GY-100-135)

S.O.C.A.T.A.: Super Rallye (MS-886), Rallye Commodore (MS-892)

Siai-Marchetti: (S-202)

F.F.A.: Bravo (AS-202/15)

Partenavia: Oscar (P66B), Bucker (131 APM)

Aeromot: Paulistina P-56

Pezetel: Koliber 150

O-320-E2C

Beech Aircraft: Musketeer III (M-23III)

M.B.B.: Monsun (BO-209-B)

O-320-E2D Cessna Aircraft: Cardinal (172-I, 177)
O-320-E2F M.B.B.: Monsun (BO-209-B), Wassmer Pacific (WA-51)
O-320-E2G American Aviation Corp.: Traveler
O-320-E3D

Piper Aircraft: Cherokee (140)

Beech Aircraft: Sport

IO-320-B2A Piper Aircraft: Twin Comanche (PA-30)
IO-320-B1C Hi. Shear: Wing
IO-320-B1D Ted Smith Aircraft: Aerostar
IO-320-C1A Piper Aircraft: Twin Comanche (PA-30 Turbo)
IO-320-D1A M.B.B.: Monsun (BO-209-C)
IO-320-D1B M.B.B.: Monsun (BO-209-C)
IO-320-E1A M.B.B.: Monsun (BO-209-C)
IO-320-E1B Bellanca Aircraft
IO-320-E2A Champion Aircraft: Citabria
IO-320-E2B Bellanca Aircraft
IO-320-F1A CAAR Engineering: Carr Midget
LIO-320-B1A Piper Aircraft: Twin Comanche (PA-39)
LIO-320-C1A Piper Aircraft: Twin Comanche (PA-39)
AIO-320-B1B M.B.B.: Monsun (BO-209-C)
AEIO-320-D1B Slingsby: T67M Firefly
AEIO-320-D2B Hundustan Aeronautics Ltd.: HT-2
AEIO-320-E1A

Bellanca Aircraft

Champion Aircraft

AEIO-320-E1B

Bellanca Aircraft

Champion Aircraft: Decathalon (8KCAB-CS)

AEIO-320-E2B

Bellanca Aircraft

Champion Aircraft: Decathalon (8KCAB)

O-320-A1A Riley Aircraft: Riley Twin
O-360-A1A

Beech Aircraft: Travel Air (95, B-95)

Piper Aircraft: Comanche (PA-24)

Intermountain Mfg. Co.: Call Air (A-6)

Lake Aircraft: Colonial (C-2, LA-4, 4A or 4P)

Doyn Aircraft: Doyn-Cessna (170B, 172, 172A, 172B)

Mooney Aircraft: Mark “20B” (M-20B)

Earl Horton: Pawnee (Piper PA-25)

Dinfia: Ranquel (1A-51)

Neiva: (1PD-5901)

Regente: (N-591)

Wassmer: Super 4 (WA-50A), Sancy (WA-40), Baladou (WA-40), Pariou (WA-40)

Sud: Gardan (GY-180)

Bolkow: (207)

Partenavia: Oscar (P-66)

Siai-Marchetti: (S-205)

Procaer: Picchio (F-15-A)

S.A.A.B.: Safir (91-D)

Malmo: Vipan (MF-10B)

Aero Boero: AB-180

Beagle: Airedale (A-109)

DeHavilland: Drover (DHA-3MK3)

Kingsford-Smith: Bushmaster (J5-6)

Aero Engine Service Ltd.: Victa (R-2)

O-360-A1AD S.O.C.A.T.A.: Tabago TB-10
O-360-A1D

Piper Aircraft: Comanche (PA-24)

Lake Aircraft: Colonial (LA-4, 4A or 4P)

Doyn Aircraft: Doyn-Beech (Beech 95)

Mooney Aircraft: Master “21” (M-20E), Mark “20B”, “20D”, (M20B, M20C), Mooney Statesman (M-20G)

Dinfia: Querandi (1A-45)

Wassmer: (WA-50)

Malmo: Vipan (MF1-10)

Cessna Aircraft: Skyhawk

Doyn Aircraft: Doyn-Piper (PA-23 “160”)

O-360-A1F6 Cessna Aircraft: Cardinal
O-360-A1F6D

Cessna Aircraft: Cardinal 177

Teal III: TSC (1A3)

O-360-A1G6 Aero Commander
O-360-A1G6D Beech Aircraft: Duchess 76
O-360-A1H6 Piper Aircraft: Seminole (PA-44)
O-360-A1LD Wassmer: Europa WA-52
O-360-A1P Aviat: Husky
O-360-A2A

Center Est Aeronautique: Regente (DR-253)

S.O.C.A.T.A.: Rallye Commodore (MS-893)

Societe Aeronautique Normande: Mousquetaire (D-140)

Bolkow: Klemm (K1-107C)

Partenavia: Oscar (P-66)

Beagle: Husky (D5-180) (J1-U)

O-360-A2D

Piper Aircraft: Comanche (PA-24), Cherokee “C”
(PA-28 “180”)

Mooney Aircraft: Master “21” (M-20D), Mark “21” (M-20E)

O-360-A2E Std. Helicopter
O-360-A2F

Aero Commander: Lark (100)

Cessna Aircraft: Cardinal

O-360-A2G Beech Aircraft: Sport
O-360-A3A

C.A.A.R.P.S.A.N.: (M-23III)

Societe Aeronautique Normande: Jodel (D-140C)

Robin: Regent (DR400/180), Remorqueur (DR400/180R).
R-3170

S.O.C.A.T.A.: Rallye 180GT, Sportavia Sportsman (RS-180)

Norman Aeroplace Co.: NAC-1 Freelance

Nash Aircraft Ltd.: Petrel

O-360-A3AD

S.O.C.A.T.A.: TB-10

Robin: Aiglon (R-1180T)

O-360-A4A Piper Aircraft: Cherokee “D” (PA-28 “180”)
O-360-A4D Varga: Kachina
O-360-A4G Beech Aircraft: Musketeer Custom III
O-360-A4K

Grumman American: Tiger

Beech Aircraft: Sundowner 180

O-360-A4M

Piper Aircraft: Archer II (PA-28 “18”)

Valmet: PIK-23

O-360-A4N Cessna Aircraft: 172 (Optional)
O-360-A4P Penn Yan: Super Cub Conversion
O-360-A5AD C. Itoh and Co.: Fuji FA-200
O-360-B2C Seabird Aviation: SB7L
O-360-C1A Intermountain Mfg. Co.: Call Air (A-6)
O-360-C1E Bellanca Aircraft: Scout (8GCBC-CS)
O-360-C1F Maule: Star Rocket MX-7-180
O-360-C1G Christen: Husky (A-1)
O-360-C2B Hughes Tool Co.: (269A)
O-360-C2D Hughes Tool Co.: (269A)
O-360-C2E

Hughes Tool Co.: (YHO-2HU) Military

Bellanca Aircraft: Scout (8GCBC FP)

O-360-C4F Maule: MX-7-180A
O-360-C4P Penn Yan: Super Cub Conversion
O-360-F1A6 Cessna Aircraft: Cutlass RG
O-360-J2A Robinson: R22
IO-360-B1A

Beech Aircraft: Travel-Air (B-95A)

Doyn Aircraft: Doyn-Piper (PA-23 “200”)

IO-360-B1B

Beech Aircraft: Travel-Air (B-95B)

Doyn Aircraft: Doyn-Piper (PA-23 “200”)

Fuji: (FA-200)

IO-360-B1D United Consultants: See-Bee
IO-360-B1E Piper Aircraft: Arrow (PA-28 “180R”)
IO-360-B1F Utva: 75
IO-360-B2E C.A.A.R.P. C.A.P. (10)
IO-360-B1F6 Great Lakes: Trainer
IO-360-B1G6 American Blimp: Spector 42
IO-360-B2F6 Great Lakes: Trainer
LO-360-A1G6D Beech Aircraft: Duchess
LO-360-A1H6 Piper Aircraft: Seminole (PA-44)
IO-360-E1A T.R. Smith Aircraft: Aerostar
IO-360-L2A Cessna Aircraft: Skyhawk C-172
IO-360-M1A Diamond Aircraft: DA-40
IO-360-M1B

Vans Aircraft: RV6, RV7, RV8

Lancair: 360

AEIO-360-B1F

F.F.A.: Bravo (200)

Grob: G115/Sport-Acro

AEIO-360-B1G6 Great Lakes
AEIO-360-B2F Mundry: CAP-10
AEIO-360-B4A Pitts: S-1S
AEIO-360-H1A Bellanca Aircraft: Super Decathalon (8KCAB-180)
AEIO-360-H1B American Champion: Super Decathalon
VO-360-A1A Brantly Hynes Helicopter: (B-2)
VO-360-A1B Brantly Hynes Helicopter: (B-2, B2-A). Military (YHO-3BR)
VO-360-B1A Brantly Hynes Helicopter: (B-2, B2-A)
IVO-360-A1A Brantly Hynes Helicopter: (B2-B)
HO-360-B1A Hughes Tool Co.: (269A)
HO-360-B1B Hughes Tool Co.: (269A)
HO-360-C1A Schweizer: (300C)
HIO-360-B1A Hughes Tool Co.: Military (269-A-1). (TH-55A)
HIO-360-B1B Hughes Tool Co.: (269A)
HIO-360-G1A Schweizer: (CB)
O-540-A1A Rhein-Flugzeugbau: (RF-1)
O-540-A1A5

Piper Aircraft: Comanche (PA-24 “180”)

Helio: Military (H-250)

Yoeman Aviation: (YA-1)

O-540-A1B5 Piper Aircraft: Aztec (PA-23 “250”), Comanche (PA-24 “250”)
O-540-A1C5 Piper Aircraft: Comanche (PA-24 “250”)
O-540-A1D

Found Bros.: (FBA-2C)

Dornier: (DO-28-B1)

O-540-A1D5

Piper Aircraft: Aztec (PA-23 “250”), Comanche (PA-24 “250”), Military Aztec (U-11A)

Dornier: (DO-28)

O-540-A2B

Aero Commander: (500)

Mid-States Mfg. Co.: Twin Courier (H-500), (U-5)

O-540-A3D5 Piper Aircraft: Navy Aztec (PA-23 “250”)
O-540-B1A5 Piper Aircraft: Apache (PA-23 “235”)
O-540-B1B5

Piper Aircraft: Comanche (PA-24 “250”)

Doyn Aircraft: Doyn-Piper (PA-24 “250”)

O-540-B1D5 Wassmer: (WA-421)
O-540-B2B5

Piper Aircraft: Pawnee (PA-25 “235”), Cherokee (PA-28 “235”), Aztec (PA -23 “235”)

Intermountain Mfg. Co.: Call Air (A-9)

Rawdon Bros.: Rawdon (T-1)

S.O.C.A.T.A.: Rallye 235CA

O-540-B2C5 Piper Aircraft: Pawnee (PA-25 “235”)
O-540-B4B5

Piper Aircraft: Cherokee (PA-28 “235”)

Embraer: Corioca (EMB-710)

S.O.C.A.T.A.: Rallye 235GT, Rallye 235C

Maule: Star Rocket (MX-7-235), Super Rocket (M-6-235), Super Std. Rocket (M-7-235)

O-540-E4A5

Piper Aircraft: Comanche (PA-24 “260”)

Aviamilano: Flamingo (F-250)

Siai-Marchetti: (SF-260), (SF-208)

O-540-E4B5

Britten-Norman: (BN-2)

Piper Aircraft: Cherokee Six (PA-32 “260”)

O-540-E4C5 Pilatus Britten-Norman: Islander (BN-2A-26), Islander
(BN-2A-27), Islander II (BN-2B-26), Islander (BN-2A-21), Trislander (BN-2A-Mark III-2)
O-540-F1B5

Omega Aircraft: (BS-12D1)

Robinson: (R-44)

O-540-G1A5 Piper Aircraft: Pawnee (PA-25 “260”)
O-540-H1B5D Aero Boero: 260
O-540-H2A5

Embraer: Impanema “AG”

Gippsland: GA-200

O-540-H2B5D Aero Boero: 260
O-540-J1A5D Maule: Star Rocket (MX-7-235), Super Rocket (M-6-235), Super Std. Rocket (M-7-235)
O-540-J3A5 Robin: R-3000/235
O-540-J3A5D Piper Aircraft: Dakota (PA-28-236)
O-540-J3C5D Cessna Aircraft: Skylane RG
O-540-L3C5D Cessna Aircraft: TR-182, Turbo Skylane RG
IO-540-C1B5 Piper Aircraft: Aztec B (PA-23 “250”), Comanche (PA-24 “250”)
IO-540-C1C5 Riley Aircraft: Turbo-Rocket
IO-540-C4B5

Piper Aircraft: Aztec C (PA-23 “250”), Aztec F

Wassmer: (WA4-21)

Avions Pierre Robin: (HR100/250)

Bellanca Aircraft: Aries T-250

Aerofab: Renegade 250

IO-540-C4D5 S.O.C.A.T.A.: TB-20
IO-540-C4D5D S.O.C.A.T.A.: Trinidad TB-20
IO-540-D4A5

Piper Aircraft: Comanche (PA-24 “260”)

Siai-Marchetti: (SF-260)

IO-540-D4B5 Cerva: (CE-43 Guepard)
IO-540-J4A5 Piper Aircraft: Aztec (PA-23 “250”)
IO-540-R1A5 Piper Aircraft: Comanche (PA-24)
IO-540-T4A5D General Aviation: Model 114
IO-540-T4B5 Commander: 114B
IO-540-T4B5D Rockwell: 114
IO-540-T4C5D Lake Aircraft: Seawolf
IO-540-V4A5

Maule: MT-7-260, M-7-260

Aircraft Manufacturing Factory

IO-540-V4A5D Brooklands: Scoutmaster
IO-540-W1A5 Maule: MX-7-235, MT-7-235, M7-235
IO-540-W1A5D Maule: Star Rocket (MX-7-235), Super Rocket (M-6-235), Super Std. Rocket (M-7-235)
IO-540-W3A5D Schweizer: Power Glider
AEIO-540-D4A5

Christen: Pitts (S-2S), S-2B)

Siai-Marchetti: SF-260

H.A.L.: HPT-32

Slingsby: Firefly T3A

AEIO-540-D4B5

Moravan: Zlin-50L

H.A.L.: HPT-32

AEIO-540-D4D5 Burkhart Grob: Grob G, 115T Aero
TIO-540-C1A Piper Aircraft: Turbo Aztec (PA-23-250)
TIO-540-K1AD Piper Aircraft
TIO-540-AA1AD Aerofab Inc.: Turbo Renegade (270)
TIO-540-AB1AD S.O.C.A.T.A.: Trinidad TC TB-21
TIO-540-AB1BD Schweizer
TIO-540-AF1A Mooney Aircraft: “TLS” M20M
TIO-540-AG1A Commander Aircraft: 114TC
TIO-540-AK1A Cessna Aircraft: Turbo Skylane T182T
LTIO-540-K1AD Piper Aircraft

Requirement:

1.    If the engine was overhauled or had a cylinder assembly replaced since new, do the following:

a)    Inspect the maintenance records and engine logbook to determine if the overhaul or repair facility used ECi cylinder assemblies, P/N AEL65102, with cylinder head, P/N AEL85099, with a S/N 1138-02 through SN
35171-22, or a S/N 35239-01 through S/N 37016-28, installed.

b)    If the cylinder assemblies are not ECi, P/N AEL65102, no further action is required by this AD.

c)    If the cylinder assemblies are ECi, P/N AEL65102, and if the S/N is not listed in this AD, no further action is required by this AD.

d)    If the cylinder assemblies are ECi, P/N AEL65102, and if the S/N is listed in this AD, proceed to Requirement 2 or 3 as is applicable.

Note 3:  The classification of cylinders, into Group “A” or Group “B” is detailed in the applicability section of this AD.  The classification will determine whether Requirement 2 or 3 applies.

2.    Group “A” Cylinder Assemblies

a)    Perform an initial visual inspection as specified in Requirement 4 of this AD of this AD, and an initial compression test as specified in Requirement 5 of this AD.

b)    Replace cylinder assemblies on:

Engines installed in a helicopter, if the cylinder assembly has 1,500 operating hours Time In Service (TIS) or more on the effective date of this AD; and

Engines installed in an aeroplane if the cylinder assembly has 2,000 operating hours TIS or more on the effective date of this AD.

c)    Perform repetitive visual inspections as specified in Requirement 4 of this AD, and repetitive compression tests as specified in Requirement 5 of this AD.

d)    Replace cylinder assemblies that pass the repetitive visual inspection and compression tests before exceeding:

1,500 hours TIS if the engine is installed in a helicopter; or

2,000 hours TIS if the engine is installed in an aeroplane.

3.    Group “B” Cylinder Assemblies

a)    Perform an initial visual inspection as specified in Requirement 4 of this AD, and initial compression test as specified in Requirement 5 of this AD.

b)    Replace cylinder assemblies that have more than 350 hours TIS on the effective date of this AD.

c)    Replace cylinder assemblies that pass the visual inspection and compression tests before exceeding 350 hours TIS.

4.    Visual Inspection

a)    Visually inspect around the exhaust valve side, for cracks or any signs of black or white residue of combustion leakage from cracks.

b)    Replace cracked cylinder assemblies.

Note 4:  Information on cylinder assembly visual inspection can be found in ECi Mandatory Service Bulletin (MSB) No. 08-1, Revision 3, dated August 19, 2008.

5.    Cylinder Assembly Compression Test

a)    Compression test the cylinder assembly.

b)    During the compression test, if the cylinder pressure gauge reads below 70 pounds-per-square-inch, apply a water and soap solution to the side of the leaking cylinder, near the head-to- barrel interface.

c)    Replace the cylinder assembly, if air leakage and bubbles are observed on the side of the cylinder assembly, near the head-to-barrel interface.

d)    Repair or replace the engine cylinder assembly if the cause of the low gauge reading in Requirement 5b of this AD is from leaking intake or exhaust valves, or from leaking piston rings.

Note 5:  Information on cylinder assembly compression testing can be found in ECi MSB No. 08-1, Revision 3, dated August 19, 2008.

6.    Do not install any ECi cylinder assembly, P/N AEL65102, with cylinder head,

P/N AEL85099, and with SN 1138-02 through SN 35171-22, or SN 35239-01 through SN 37016-28, onto any engine, and do not attempt to repair or reuse these ECi cylinder assemblies.

Note 6:  FAA AD 2008-19-05 Amdt 39-15672 dated 5 September 2008 refers.

Compliance:

For Requirement 1 - Before further flight after the effective date of this AD.

For Requirement 2a - If the cylinder assembly has 350 or more operating hours TIS on the effective date of this AD, but fewer than 2000 hours TIS on the effective date of this AD - Within 10 hours TIS; or

       If the cylinder has fewer than 350 hours TIS on the effective date of this AD - Before exceeding 350 hours TIS.

For Requirement 2b - Within the next 25 operating hours TIS after the effective date of this AD.

For Requirement 2c - Within every 50 operating hours TIS.

For Requirement 2d - After the effective date of this AD.

For Requirement 3a - Within an additional 10 operating hours TIS after the effective date of this AD.

For Requirement 3b - Within the next 25 operating hours TIS after the effective date of this AD.

For Requirement 3c - After the effective date of this AD.

For Requirement 4b - Before further flight.

For Requirements 5c and 5d - Before further flight.

For Requirement 6 - After the effective date of this AD.

This Airworthiness Directive becomes effective on 20 October 2008.

Background:

This AD requires initial and repetitive visual inspections and compression tests to detect cracks at the head-to-barrel interface, replacement of cylinder assemblies found cracked, and replacement of certain cylinder assemblies, at new reduced times-in-service.  This AD results from reports of 45 failures with head separations of ECi cylinder assemblies.  We are issuing this AD to prevent loss of engine power due to cracks at the head-to-barrel interface in the cylinder assemblies and possible engine failure caused by separation of a cylinder head, which could result in loss of control of the aircraft.


Charles Lenarcic
Delegate of the Civil Aviation Safety Authority

19 September 2008

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