AD 2007-04-19R1

Active

SAP cylinder assemblies

Key Information
2007-04-19R1
Active
May 07, 2007
March 23, 2007
FAA-2006-25948
39-15005
Applicability
["Appliance"]
Not specified
Lycoming Engines Superior Air Parts, Inc. Continental Motors
AEIO-320-D1B AEIO-320-D2B AEIO-320-E1A AEIO-320-E1B AEIO-320-E2A AEIO-320-E2B AEIO-360-B1B AEIO-360-B1D AEIO-360-B1F AEIO-360-B1F6 AEIO-360-B1G6 AEIO-360-B1H AEIO-360-B2F AEIO-360-B2F6 AEIO-360-B4A AEIO-360-H1A AEIO-360-H1B AEIO-540-D4A5 AEIO-540-D4B5 AEIO-540-D4C5 AEIO-540-D4D5 AIO-320-A1A AIO-320-A1B AIO-320-A2A AIO-320-A2B AIO-320-B1B AIO-320-C1B HIO-360-B1A HIO-360-B1B IO-320-B1A IO-320-B1B IO-320-B1C IO-320-B1D IO-320-B1E IO-320-B2A IO-320-D1A IO-320-D1B IO-320-D1C IO-320-E1A IO-320-E1B IO-320-E2A IO-320-E2B IO-360-B1A IO-360-B1B IO-360-B1C IO-360-B1D IO-360-B1E IO-360-B1F IO-360-B1F6 IO-360-B1G6 IO-360-B2E IO-360-B2F IO-360-B2F6 IO-360-B4A IO-360-L2A IO-360-M1A IO-360-M1B IO-540-A1A5 IO-540-AA1A5 IO-540-AA1B5 IO-540-AB1A5 IO-540-AC1A5 IO-540-AE1A5 IO-540-C1B5 IO-540-C1C5 IO-540-C2C IO-540-C4B5 IO-540-C4B5D IO-540-C4C5 IO-540-C4D5 IO-540-C4D5D IO-540-D4A5 IO-540-D4B5 IO-540-D4C5 IO-540-N1A5 IO-540-T4A5D IO-540-T4B5 IO-540-T4B5D IO-540-T4C5D IO-540-V4A5 IO-540-V4A5D IO-540-W1A5 IO-540-W1A5D IO-540-W3A5D LIO-320-B1A LO-360-A1G6D LO-360-A1H6 O-320-A1A O-320-A1B O-320-A2A O-320-A2B O-320-A2C O-320-A2D O-320-A3A O-320-A3B O-320-A3C O-320-B1A O-320-B1B O-320-B2A O-320-B2B O-320-B2C O-320-B2D O-320-B2E O-320-B3A O-320-B3B O-320-B3C O-320-C1A O-320-C1B O-320-C2A O-320-C2B O-320-C2C O-320-C3A O-320-C3B O-320-C3C O-320-D1A O-320-D1B O-320-D1C O-320-D1D O-320-D1F O-320-D2A O-320-D2B O-320-D2C O-320-D2F O-320-D2G O-320-D2H O-320-D2J O-320-D3G O-320-E1A O-320-E1B O-320-E1C O-320-E1F O-320-E1J O-320-E2A O-320-E2B O-320-E2C O-320-E2D O-320-E2F O-320-E2G O-320-E2H O-320-E3D O-320-E3H O-320-H1AD O-320-H1BD O-320-H2AD O-320-H2BD O-320-H3AD O-320-H3BD O-360-A1A O-360-A1AD O-360-A1C O-360-A1D O-360-A1F O-360-A1F6 O-360-A1F6D O-360-A1G O-360-A1G6 O-360-A1G6D O-360-A1H O-360-A1H6 O-360-A1LD O-360-A1P O-360-A2A O-360-A2D O-360-A2E O-360-A2F O-360-A2G O-360-A2H O-360-A3A O-360-A3AD O-360-A3D O-360-A4A O-360-A4AD O-360-A4D O-360-A4G O-360-A4J O-360-A4K O-360-A4M O-360-A4N O-360-A4P O-360-A5AD O-360-B1A O-360-B1B O-360-B2A O-360-B2B O-360-B2C O-360-C1A O-360-C1C O-360-C1E O-360-C1F O-360-C1G O-360-C2A O-360-C2B O-360-C2C O-360-C2D O-360-C2E O-360-C4F O-360-C4P O-360-D1A O-360-D2A O-360-D2B O-360-F1A6 O-360-G1A6 O-360-J2A O-540-A1A O-540-A1A5 O-540-A1B5 O-540-A1C5 O-540-A1D O-540-A1D5 O-540-A2B O-540-A3D5 O-540-A4A5 O-540-A4B5 O-540-A4C5 O-540-A4D5 O-540-B1A5 O-540-B1B5 O-540-B1D5 O-540-B2A5 O-540-B2B5 O-540-B2C5 O-540-B4A5 O-540-B4B5 O-540-E4A5 O-540-E4B5 O-540-E4C5 O-540-F1A5 O-540-F1B5 O-540-G1A5 O-540-G2A5 O-540-H1A5 O-540-H1A5D O-540-H1B5D O-540-H2A5 O-540-H2A5D O-540-H2B5D O-540-J1A5D O-540-J1B5D O-540-J1C5D O-540-J1D5D O-540-J2A5D O-540-J2B5D O-540-J2C5D O-540-J2D5D O-540-J3A5 O-540-J3A5D O-540-J3C5D SAP cast cylinder assemblies IO-470-C IO-470-D IO-470-E IO-470-F IO-470-G IO-470-H IO-470-L IO-470-M IO-470-N IO-470-P IO-470-R IO-470-S IO-470-U IO-470-V IO-520-A IO-520-B IO-520-BA IO-520-BB IO-520-C IO-520-CB IO-520-D IO-520-E IO-520-F IO-520-J IO-520-K IO-520-L IO-520-M IO-520-MB IO-550-A IO-550-B IO-550-C IO-550-D IO-550-E IO-550-F IO-550-L O-470-G O-470-K O-470-L O-470-M O-470-P O-470-R O-470-S O-470-U TSIO-520-AF TSIO-520-B TSIO-520-BB TSIO-520-C TSIO-520-CE TSIO-520-D TSIO-520-DB TSIO-520-E TSIO-520-EB TSIO-520-G TSIO-520-H TSIO-520-J TSIO-520-JB TSIO-520-K TSIO-520-KB TSIO-520-L TSIO-520-LB TSIO-520-M TSIO-520-N TSIO-520-NB TSIO-520-P TSIO-520-R TSIO-520-T TSIO-520-UB TSIO-520-VB TSIO-520-WB
Summary

The FAA is revising an existing airworthiness directive (AD) for certain SAP cylinder assemblies installed in Teledyne Continental Motors (TCM) 470, 520, and 550 series reciprocating engines, Lycoming Engines (LE) 320, 360, and 540 series reciprocating engines, Avco Lycoming (AL) 540 series reciprocating engines, and Superior Air Parts, Inc. (SAP) 360 series reciprocating engines. That AD currently requires removing from service certain SAP part numbered (P/N) cylinder assemblies installed in TCM, LE, and AL reciprocating engines. That AD also requires removing from service certain cylinder assemblies installed as original equipment in SAP reciprocating engines, or in certain overhauled or repaired SAP reciprocating engines.

This AD continues to require those same actions. This AD results from comments from the Public on the existing AD. We are issuing this AD to prevent cylinder separation that can lead to engine failure, a possible engine compartment fire, and damage tothe airplane.

Action Required

Final rule; request for comments.

Regulatory Text

2007-04-19R1 Superior Air Parts, Inc.: Amendment 39-15005. Docket No. FAA-2006-25948; Directorate Identifier 2006-NE-32-AD.

Effective Date

(a) This airworthiness directive (AD) becomes effective May 7, 2007.

Affected ADs

(b) This AD revises AD 2007-04-19.

Applicability

(c) This AD applies to Superior Air Parts, Inc. (SAP), cylinder assemblies, manufactured between April 2005 and November 2005, part numbers (P/Ns): SA47000L-A1, SA47000L-A20P, SA47000S-A1, SA47000S- A20P, SA47000S-A21P, SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, and SA55000-A20P, installed in Teledyne Continental Motors (TCM) 470, 520, and 550 series reciprocating engines. These P/N cylinder assemblies may be installed in the TCM engine models listed in the following Table 1.

Table 1.--Affected Teledyne Continental Engine Models

Engine Model
O-470
-G, -K, -L, -M, -P, -R, -S, -U
IO-470
-C, -D, -E, -F, -G, -H, -L, -M, -N, -P, -R, -S, -U, -VIO-520
- A, B, BA, C, CB, D, E, F, J, K, L, M, BB, MB
TSIO-520
- AF, B, BB, C, CE, D, DB, E, EB, G, H, J, JB, K, KB, L, LB, M, N, NB, P, R, T, UB, VB, WB
IO-550
- A, B, C, D, E, F, L

These engine models are installed in, but not limited to, the aircraft models listed in the following Table 2:

Table 2.--Teledyne Continental Motors-Related Aircraft Models

Engine Model
Aircraft Manufacturer
Aircraft Model Designation
IO-470-C
Beechcraft
J, K, M35
IO-470-D
Cessna
310 G & H
IO-470-D
Rockwell
200 A, B, & C
IO-470-E
Cessna
210 & A
IO-470-F
Bellanca
14-19-3
IO-470-F
Cessna
185
IO-470-H
Sierra Hotel Aero, Inc. (Navion)
Navion F &G (Rangemaster)
IO-470-L
Beechcraft
B55 Baron
IO-470-M
Gulfstream
500 A
IO-470-N
Beechcraft
N & P
IO-470-N
Beechcraft
G33
IO-470-S
Cessna
210 B & C
IO-470-S
Cessna
205
IO-470-U
Cessna
310 I & J
IO-470-V/VO
Cessna
310K, L, N, P & Q
IO-520-A
Cessna
210 D, E, F, G, & H
IO-520-A
Cessna
206
IO-520-A
Cessna
P206
IO-520-A
Rockwell
200 D
IO-520-B
Beechcraft
36 Bonanza
IO-520-B
Beechcraft
A36
IO-520-B
Sierra Hotel Aero, Inc. (Navion)
Navion H
IO-520-BA
Beechcraft
A36
IO-520-BA
Beechcraft
S & V35, V35A, V35B
IO-520-BA
Beechcraft
C33 A
IO-520-BA
Beechcraft
E33 A & C
IO-520-BA
Beechcraft
F33 A & C
IO-520-BA
Sierra Hotel Aero, Inc.
Navion G (Rangemaster)
IO-520-BA
Sierra Hotel Aero, Inc.
Navion H
IO-520-BB
Beechcraft
A36
IO-520-BB
Beechcraft
V35B
IO-520-BB
Beechcraft
F33 A
IO-520-C & CB
Beechcraft
C55 - E55 Baron
IO-520-D
Bellanca
17-30 Viking
IO-520-D
Cessna
A188-300 AG Truck
IO-520-D
Cessna
185
IO-520-E
(Cessna 310)
Exec 600
IO-520-E
(Beech Baron)
Pres 600
IO-520-F
Cessna
207
IO-520-F
Cessna
U206
IO-520-K
Bellanca
17-30A
IO-520-L
Cessna
210 K, L, M, N & R
IO-520-L
Cessna
210N II
IO-520-L
Cessna
210R
IO-520-M
Cessna
310R
IO-520-MB
Cessna
310R
IO-550-A
Cessna
310 Conversion
IO-550-B
BeechcraftA36
IO-550-B
(Beech Bonanza)
Foxstar
IO-550-C
Beechcraft
58 Baron
IO-550-D
Cessna
185/188 Conversion
IO-550-E
Cessna
310 Conversion
IO550-F
Cessna
206/207 Conversion
IO-550-L
Cessna
210 Conversion
O-470-M
Cessna
310
O-470-G
Beechcraft
H35
O-470-K
Bellanca
14-19-2
O-470-K
Cessna
180 (230 HP)
O-470-L
Cessna
182
O-470-L
Cessna
180D
O-470-M
Cessna
310 B
O-470-P
Sierra Hotel Aero, Inc. (Navion)
Navion
O-470-R
Cessna
188-230
O-470-R
Cessna
182
O-470-R
Cessna
180 E-J
O-470-S
Cessna
182
O-470-U
Cessna
182
O-470-U
Cessna
180 K
TSIO-520-AF
Cessna
P210N II
TSIO-520-B
Cessna
320D, E & F
TSIO-520-B
Cessna
T310-Q & R
TSIO-520-BB
Cessna
T310R
TSIO-520-BE
Piper
PA-46-310 Malibu
TSIO-520-C
Cessna
T210 F, G, & H
TSIO-520-C
Cessna
TU206
TSIO-520-C
Cessna
TP206
TSIO-520-C&CB
Beechcraft
58 Baron
TSIO-520-CE
Cessna
T210R
TSIO-520-CF
Cessna
P210R
TSIO-520-D
Beechcraft
V35, V35A, V35B-TC
TSIO-520-E
Cessna
402,A & B
TSIO-520-E
Cessna
401, A & B
TSIO-520-EB
Cessna
335
TSIO-520-G
Cessna
T207
TSIO-520-H
Cessna
T210 J, K & L
TSIO-520-J
Cessna
210 J
TSIO-520-J
Cessna
414
TSIO-520-J
Riley Conversions
340 Super Riley
TSIO-520-L&LB
Beechcraft
58P Baron
TSIO-520-L&LB
Beechcraft
58TC Baron
TSIO-520-M
Cessna
T207
TSIO-520-M
Cessna
TU206
TSIO-520-N
Cessna
414-II Chancellor
TSIO-520-N
Cessna
340
TSIO-520-NB
Cessna
414-II
TSIO-520-NB
Cessna
340
TSIO-520-P
Cessna
P210N
TSIO-520-R
Cessna
T210 M
TSIO-520-R
Cessna
T210N II
TSIO-520-T
Cessna
T188C AG Husky
TSIO-520-UB
Beechcraft
A36TC Bonanza
TSIO-520-UB
Beechcraft
B36TC
TSIO-520-VB
Cessna
402 C
TSIO-520-WB
Beechcraft
58P Baron
TSIO-520-WB
Beechcraft
58TC Baron

This AD also applies to SAP, cast cylinder assemblies, P/Ns SL32000W-A1, SL32000W-A20P, SL32000W-A21P, SL32000WH-A1, SL32000WH- A20P, SL32006W-A1, SL32006W-A20P, SL32006W-A21P, SL36000TW-A1, SL36000TW-A20P, SL36000TW-A21P, SL36000TW-A22P, SL36000W-A1, SL36000W-A20P, SL36000W-A21P, SL36006W-A1, SL36006W-A20P, and SL36006W-A21P, installed in Lycoming Engines (LE) 320, 360, and 540 series reciprocating engines and Avco Lycoming 540 series reciprocating engines. These P/N cylinder assemblies may be installed in the LE and AL engine models listed in the following Table 3.

Table 3.--Affected Lycoming Engines and Avco Lycoming Engine Models

Engine Model

O-320
-A, -B, -C, -D, -E, H
IO-320
-B, -D, -E
LIO-320
-B
AIO-320
-A, -B, -C
AEIO-320
-D, -E
O-360
-A, -B, -C, -D, -F, -G, -J
IO-360
- B, -L, -M
LO-360
-A
AEIO-360
-B, -H
HO-360
-C
HIO-360
-B
O-540
-A, -B, -E, -F, -G, -H, -J
IO-540
-A, -C, -D, -N, -T, -V, -W
AEIO-540
-D

These engine models are installed in, but not limited to, the aircraft models listed in the following Table 4:

Table 4.--Lycoming Engines and Avco Lycoming-Related Aircraft Models

Engine Model
Aircraft Manufacturer
Aircraft Model Designation
O-320-A
Mooney Aircraft
Mark 20A
O-320-A1A
Piper Aircraft
PA-23-150 Apache
O-320-A1A
Piper Aircraft
PA-22-150 Tri-Pacer
O-320-A1A
Piper Aircraft
PA-22S-150 Tri-Pacer
O-320-A1A
Piper Aircraft
PA-25 Pawnee
O-320-A1A
Doyne Aircraft
Doyn-Cessna 170,170A,170B
O-320-A1A
Dinfia
Ranquel 1A-46
O-320-A1A
Simmering-Graz Pauker
Flamingo SGP-M-222
O-320-A1A
Aviamilano
Scricciolo P-19
O-320-A1A
Vos Helicopter Co.
Spring Bok
O-320-A1A
Mooney Aircraft
Mark 20A
O-320-A1B
Piper Aircraft
PA-22-150 Tri-Pacer
O-320-A1B
Piper Aircraft
PA-22S-150 Tri-Pacer
O-320-A1B
Piper Aircraft
PA-23 Apache
O-320-A1B
Doyne Aircraft
Doyn-Cessna 170,170A,170B
O-320-A1B
S.O.C.A.T.A
Horizon (Gardan)
O-320-A2A
Piper Aircraft
PA-22-150
O-320-A2A
Piper Aircraft
PA-22S-150
O-320-A2A
Piper Aircraft
Agriculture PA-18A-150
O-320-A2A
Piper Aircraft
Super Cub PA-18-150
O-320-A2A
Piper Aircraft
Caribbean PA-22-150
O-320-A2A
Piper Aircraft
PA-25 Pawnee
O-320-A2ALake Aircraft
Colonial C1
O-320-A2A
Intermountain Mfg. Co.
Call Air Texas A-5, A-5T
O-320-A2A
Rawdon Bros.
Rawdon T-1, T-15, T-15D
O-320-A2A
Shinn Engineering
Shinn 2150-A
O-320-A2A
Dinfia
Ranquel 1A-46
O-320-A2A
Neiva
1PD-5802
O-320-A2A
Sud
Gardan-Horizon (GY-80)
O-320-A2A
La Verda
Falco F8L Series II, America
O-320-A2A
Malmo
Vipan MF1-10
O-320-A2A
Kingsford Smith
Autocrat SCRM-153
O-320-A2B
Aero Commander
100
O-320-A2B
Piper Aircraft
PA-22-150
O-320-A2B
Piper Aircraft
PA-22S-150
O-320-A2B
Piper Aircraft
Cherokee PA-28-150
O-320-A2B
Piper Aircraft
Super Cub PA-18-150
O-320-A2B
Champion Aircraft
Challenger 7GCA, 7GCB, 7KC
O-320-A2B
Champion Aircraft
Citabria 7GCAA, 7GCRC
O-320-A2B
Champion Aircraft
Agriculture 7GCBA
O-320-A2B
Beagle
Pup 150
O-320-A2B
Arctic
Interstate S1B2
O-320-A2B
Robinson Helicopters
R-22
O-320-A2C
Robinson Helicopters
R-22
O-320-A2C
Varga
Kachina 2150a
O-320-A2C
Cicare
Cicare AG
O-320-A2D
Bellanca Aircraft
Citabria 150 (7GCAA)
O-320-A2D
Bellanca Aircraft
Citabria 150S (7GCBC)
O-320-A2D
Bellanca
Citabria 150S (7G(.HU)
O-320-A2F
Cessna Aircraft
177A
O-320-A3A
Piper Aircraft
Apache PA-23
O-320-A3A
Doyn Aircraft
Doyn-Cessna 170, 170A, 170B
O-320-A3A
Corben-Fettes
Globe Special (Globe GC-1B)
O-320-A3B
Piper Aircraft
Apache PA-23
O-320-A3B
Doyn Aircraft
Doyn-Cessna 170, 170A, 170B
O-320-A3B
Teal II
TSC 1A2
O-320-B1A
Piper Aircraft
Apache PA-23-160
O-320-B1A
Doyn Aircraft
Doyn-Cessna 170, 170A, 170B
O-320-B1A
Malmo
Vipan MF1-10
O-320-B1B
Piper Aircraft
Apache PA-23-160
O-320-B1B
Doyn Aircraft
Doyn-Cessna 170, 170A, 170B
O-320-B2A
Piper Aircraft
PA-22-160
O-320-B2A
Piper Aircraft
PA-22S-160
O-320-B2B
Piper Aircraft
PA-22-160
O-320-B2B
Piper Aircraft
PA-22S-160
O-320-B2B
Beagle
Airedale D5-160
O-320-B2B
Fuji-Heavy Industries
Fuji F-200
O-320-B2B
Uirapuru
Aerotec 122
O-320-B2C
Robinson Helicopters
R22-HP, Alpha, Beta
O-320-B2D
Maule
MX-7-160
O-320-B2E
Lycon

O-320-B3A
Piper Aircraft
Apache PA-23-160
O-320-B3A
Doyn Aircraft
Doyn-Cessna 170, 170A, 170B
O-320-B3B
Piper Aircraft
PA-23-160 Apache
O-320-B3B
Doyn Aircraft
Doyn-Cessna 170, 170A, 170B
O-320-B3B
Sud
Gardan (GY8O-160)
O-320-C1A
Piper Aircraft
Apache PA-23-160
O-320-C1A
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 (GY80)
O-320-D1A
Gyroflug
Speed Cancard
O-320-D1A
Grob
G115
O-320-D1D
Gulfstream
GA-7
O-320-D1F
Slingsby
T67 Firefly
O-320-D2A
Piper Aircraft
Cherokee PA-28S-160
O-320-D2A
Robin
Major DR400-140B
O-320-D2A
Robin
Chevalier DR-360, R-3140
O-320-D2A
S.0.C.A.T.A.
Tampico TB9
O-320-D2A
Slingsby
T67C Firefly
O-320-D2A
Daetwyler
MD-3-160
O-320-D2A
Nash Aircraft Ltd.
Petrel
O-320-D2A
Aviolight
P66D Delta
O-320-D2A
General Avia
Pinguino
O-320-D2B
Beechcraft
Musketeer A23
O-320-D2B
Piper Aircraft
Cherokee PA-28-160
O-320-D2J
Cessna
Skyhawk 172 P
O-320-D3G
Piper Aircraft
Cadet PA-28-161
O-320-D3G
Piper Aircraft
Warrior II
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
O-320-E2A
Piper Aircraft
Cherokee PA-28-150
O-320-E2A
Robin
Major (DR-340)
O-320-E2A
Robin
Sitar
O-320-E2A
Robin
Bagheera (GY-100-135)
O-320-E2A
S.O.C.A.T.A.
Super Rallye (MS-886)
O-320-E2A
S.O.C.A.T.A.
Rallye Commodore (MS-892)
O-320-E2A
Siai-Marchetti
S-202
O-320-E2A
F.F.A.
Bravo (AS-202/15)
O-320-E2A
Partenavia
Oscar (P66B)
O-320-E2A
Partenavia
Bucker (131 APM)
O-320-E2A
Aeromot
Paulistina P-56
O-320-E2A
Pezetel
Koliber 150
O-320-E2C
Beechcraft
Musketeer (B19)
O-320-E2C
Beechcraft
Musketeer III (M-23111)
O-320-E2C
M.B.B.
Monsun (BO-209-B)
O-320-E2D
Beechcraft
B19 Sport
O-320-E2D
Cessna
177
O-320-E2D
Cessna
172 I M
O-320-E2D
Piper Aircraft
PA-28-151
O-320-E2D
Piper Aircraft
PA-28-140
O-320-E2D
Cessna
Cardinal (172.1, 177)
O-320-E2F
M.B.B.
Monsun (BO-209-B)
O-320-E2F
M.B.B.
Wassmer Pacific (WA-5 1)
O-320-E2G
Gulfstream
AA5 Traveler
O-320-E2G
Gulfstream
AA5A Cheetah
O-320-E3D
Beechcraft
B19 Sport
O-320-E3D
Piper Aircraft
Cherokee (140)
O-320-H2AD
Cessna
Skyhawk 172 N
O-320-H2AD
Partenavia
P-66C
O-320A2C
Varga
Kachina 2150
IO-320-B2A
Piper Aircraft
Twin Comanche (PA-30)
IO-320-B1C
Hi

IO-320-B1C
Shear

IO-320-B1C
Wing

IO-320-B1D
Ted Smith Aircraft
Aerostar
IO-320-D1A
M.B.B.
Monsun (BO-209-C)
IO-320-D1B
M.B.B.
Monsun (BO-209-C)
IO-320-E1A
Champion
KCAB
IO-320-E1A
M.B.B.
Monsun (BO-209-C)
IO-320-E1B
Bellanca Aircraft

IO-320-E2A
Champion
7 KCAB
IO-320-E2A
Champion Aircraft
Citabria
IO-320-E2B
Bellanca Aircraft

IO/LIO-320-B1A
Piper Aircraft
PA-30 Comanche (2)IO/LIO-320-B1A
Piper Aircraft
Twin Comanche (PA-39)
AIO-320-Bl B
M.B.B.
Monsun (BO-209-C)
AEIO-320-D1B
Slingsby
T67M Firefly
AEIO-320-D2B
Hindustan Aeronautics Ltd.
HT-2
AEIO-320-E1A
Bellanca Aircraft

AEIO-320-E1A
Champion Aircraft

AEIO-320-EIB
Bellanca Aircraft

AEIO-320-EIB
Champion Aircraft
Decathalon (8KCAB-CS)
AEIO-320-E2B
Bellanca Aircraft

AEIO-320-E2B
Champion Aircraft
Decathalon (8KCAB)
O-320-A1A
Riley Aircraft
Riley Twin
O-360-A1A
Beechcraft
Travel Air (95, B-95)
O-360-A1A
Piper Aircraft
Comanche (PA-24)
O-360-A1A
Intermountain Mfg. Co.
Call Air (A-6)
O-360-A1A
Lake Aircraft
Colonial (C-2, LA-4, 4A or 4P)
O-360-A1A
Doyn Aircraft
Doyn-Cessna (170B, 172, 172A, 172B)
O-360-A1A
Mooney Aircraft
Mark 20B (M-20B)
O-360-A1A
Earl Horton
Pawnee (Piper PA-25)
O-360-A1A
Dinfia
Ranquel (IA-51)
O-360-A1A
Neiva
(IPD-5901)
O-360-A1A
Regente
(N-591)
O-360-A1A
Wassmer
Super 4 (WA-50A)
O-360-A1A
Wassmer
Sancy (WA-40)
O-360-A1A
Wassmer
Baladou (WA-40)
O-360-A1A
Wassmer
Pariou (WA-40)
O-360-A1A
Sud
Gardan (GY-180)
O-360-A1A
Bolkow
(207)
O-360-A1A
Partenavia
Oscar (P-66)
O-360-A1A
Siai-Marchetti
(S-205)
O-360-A1A
Procaer
Picchio (F-15-A)
O-360-A1A
S.A.A.B.
Safir (91-D)
O-360-A1A
Malmo
Vipan (MF-1OB)
O-360-A1A
Aero Boero
AB-180
O-360-A1A
Beagle
Airedale (A-109)
O-360-A1A
DeHavilland
Drover (DHA-3MK3)
O-360-A1A
Kingsford-Smith
Bushmaster (J5-6)
O-360-A1A
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)
O-360-A1D
Lake Aircraft
Colonial (LA-4, 4A or 4P)
O-360-A1D
Doyn Aircraft
Doyn-Beech (Beech 95)
O-360-A1D
Mooney Aircraft
Master 21 (M-20E)
O-360-A1D
Mooney Aircraft
Mark 20B, 20D, (M2OB, M2OC)
O-360-A1D
Mooney Aircraft
Mooney Statesman (M-20G)
O-360-A1D
Dinfia
Querandi (IA-45)
O-360-A1D
Wassmer
(WA-50)
O-360-A1D
Malmo
Vipan (MFI-10)
O-360-A1D
Cessna Aircraft
Skyhawk
O-360-A1D
Doyn Aircraft
Doyn-Piper PA-23-160
O-360-AIF6
Cessna Aircraft
Cardinal
O-360-AIF6D
Cessna Aircraft
Cardinal 177
O-360-AIF6D
Teal III
TSC (1A3)
O-360-A1G6
Aero Commander

O-360-A1G6D
Beech Aircraft
Duchess 76
O-360-AIH6
Piper Aircraft
Seminole (PA-44)
O-360-Al LD
Wassmer
Europa WA-52
O-360-AIP
Aviat

O-360-AIP
Husky

O-360-A2A
Center Est Aeronautique
Regente (DR-253)
O-360-A2A
S.O.C.A.T.A.
RalIye Commodore (MS-893)
O-360-A2A
Societe Aeronautique Normande
Mousquetaire (D-140)
O-360-A2A
Bolkow
Klemm (Kl -1 07C)
O-360-A2A
Partenavia
Oscar (P-66)
O-360-A2A
Beagle
Husky (D5-180) (J1-U)
O-360-A2D
Piper Aircraft
Comanche PA-24
O-360-A2D
Piper Aircraft
Cherokee C PA-28-180
O-360-A2D
Mooney Aircraft
Master 21 (M-20D)
O-360-A2D
Mooney Aircraft
Mark 21 (M-20E)
O-360-A2E
Std. Helicopter

O-360-A2F
Aero Commander
Lark(100)
O-360-A2F
Cessna Aircraft
Cardinal
O-360-A2G
Beech Aircraft
Sport
O-360-A3A
C.A.A.R.P.S.A.N.
(M-23111)
O-360-A3A
Societe Aeronautique Normande
Jodel (D-140C)
O-360-A3A
Robin
Regent (DR400/180)
O-360-A3A
Robin
Remorqueur (DR400/180R)
O-360-A3A
Robin
R-3170
O-360-A3A
S.O.C.A.T.A.
Rallye 18OGT
O-360-A3A
S.O.C.A.T.A.
Sportavia Sportsman (RS-180)
O-360-A3A
Norman Aerospace Co.
NAC-1 Freelance
O-360-A3A
Nash Aircraft Ltd.
Petre
O-360-A3AD
S.O.C.A.T.A.
TB-l0
O-360-A3AD
Robin
Aiglon (R-l 180T)
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
O-360-A4K
Beech Aircraft
Sundowner 180
O-360-A4M
Piper Aircraft
Archer II PA-28-18
O-360-A4M
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-CIE
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

O-360-C2E
Bellanca Aircraft
Scout 8GCBC FP
O-360-C4F
Maule
MX-7-180A
O-360-C4P
Penn Van
Super Cub Conversion
O-360-F1A6
Cessna Aircraft
Cutlass RG
O-360-J2A
Robinson
R22
IO-360-B1A
Beech Aircraft
Travel-Air (B-95A)
IO-360-B1A
Doyn Aircraft
Doyn-Piper PA-23-200
IO-360-B1B
Beech Aircraft
Travel-Air (B-95B)
IO-360-B1B
Doyn Aircraft
Doyn-Piper PA-23-200
IO-360-B1B
Fuji
FA-200
IO-360-B1D
United Consultants
See-Bee
IO-360-BIE
Piper Aircraft
Arrow PA-28-180R
IO-360-BIF
Utva
75
IO-360-B2E
C.A.A.R.P.
C.A.P. (10)
IO-360-BIF6
Great Lakes
Trainer
IO-360-B1G6
American Blimp
Spector 42
IO-360-B2F6
Great Lakes
Trainer
LO-360-A1 G6D
Beech Aircraft
Duchess
LO-360-A1H6
Piper Aircraft
Seminole (PA-44)
IO-360-EIA
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
IO-360-M1B
Lancair
360
AIO-360-B1B
Moravan
Zim (Z-526-L)
AEIO-360-B1G6
Great Lakes

AEIO-360-B2F
Mundry
CAP-10
AEIO-360-B4A
Pitts
S-1S
AEIO-360-HIA
Bellanca Aircraft
Super Decathalon (8KCAB-180)
AEIO-360-HIB
American Champion
Super Decathalon
HO-360-B1A
Hughes Tool Co.
269A
HO-360-B1B
Hughes Tool Co.
269A
HO-360-C1A
Schweizer
300C
HIO-360-A1A
Hughes Tool Co.
300
H1O-360-A1B
Silvercraft

HIO-360-B1A
Hughes Tool Co.
Military 269-A-1
HlO-360-BIB
Hughes Tool Co.
269A
HIO-360-D1A
Hughes Tool Co.
269C, 300C
HIO-360-D1A
Schweizer
300C
HIO-360-E1AD
Enstrom Helicopter
F28C
HIO-360-E1BD
Enstrom Helicopter
F28C
HIO-360-F1AD
Enstrom Helicopter
Faicon F28F
HIO-360-F1AD
Enstrom Helicopter
Shark 280FX
HIO-360-F1AD
Enstrom Helicopter
Sentine F28F-P
HIO-360-G1A
Schweizer
CB
LHIO-360-C1A
Silvercraft
SH-4 Helicopter
LHIO-360-C1B
Silvercraft
SH-3 HelicopterO-540-AIA
Rhein-Flugzeugbau
RF-1
O-540-AIA5
Piper Aircraft
Comanche PA-24-150
O-540-AIA5
Helio
Military H-250
O-540-AIA5
Yoeman Aviation
YA-1
O-540-A1B5
Piper Aircraft
Aztec PA-23-250
O-540-A1B5
Piper Aircraft
Comanche PA-24-250
O-540-AIC5
Piper Aircraft
Comanche PA-24-250
O-540-A1D
Found Bros.
FBA-2C
O-540-A1D
Dornier
DO-28-B1
O-540-AID5
Piper Aircraft
Aztec PA-23 -250
O-540-AID5
Piper Aircraft
Comanche PA-24-250
O-540-AID5
Piper Aircraft
Military Aztec U-1 1A
O-540-AID5
Dornier
DO-28
O-540-A2B
Aero Commander
500
O-540-A2B
Mld-States Mfg. Co.
Twin Courier 11-500, U-5
O-540-A3D5
Piper Aircraft
Navy Aztec PA-23-250
O-540-B1A5
Piper Aircraft
Apache PA-23-235
O-540-BIB5
Piper Aircraft
Cherokee PA-24-250
O-540-BIB5
Doyn Aircraft
Doyn-Piper PA-24-250
O-540-BID5
Wassmer
WA-421
O-540-B2B5
Piper Aircraft
Pawnee PA-24-235
O-540-B2B5
Piper Aircraft
Cherokee PA-28-235
O-540-B2B5
Piper Aircraft
Aztec PA-23-235
O-540-B2B5
Intermountain Mfg. Co.
Call Air A-9
O-540-B2B5
Rawdon Bros.
Rawdon T-l
O-540-B2B5
S.O.C.A.T.A.
Rallye 235CA
O-540-B2C5
Piper Aircraft
Pawnee PA-24-235
O-540-B4B5
Piper Aircraft
Cherokee PA-28-235
O-540-B4B5
Embraer
Corioca EMB-710
O-540-B4B5
S.O.C.A.T.A.
RalIye 235GT
O-540-B4B5
S.O.C.A.T.A.
Rallye 235C
O-540-B4B5
Maule
Star Racket MX-7-235
O-540-B4B5
Maule
Super Rocket M-6-235
O-540-B4B5
Maule
Super Std. Racket M-7-235
O-540-E4A5
Piper Aircraft
Comanche PA-24-260
O-540-E4A5
Aviamilano
Flamingo F-250
O-540-E4A5
Siai-Marcbetti
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
O-540-E4C5
Pilatus Britten-Norman
Islander BN-2A-27
O-540-E4C5
Pilatus Britten-Norman
Islander II BN-2B-26
O-540-E4C5
Pilatus Britten-Norman
Islander BN-2A-2 1
O-540-E4C5
Pilatus Britten-Norman
Trislander BN-2A-Mark 111-2
O-540-F1B5
Omega Aircraft
BS-12D1
O-540-F1B5
Robinson
R-44
O-540-G1A5
Piper Aircraft
Pawnee PA-25-260
O-540-H1B5D
Aero Boero
260
O-540-H2A5
Embraer
Impanema AG
O-540-H2A5
Gippsland
GA-200
O-540-H2B5D
Aero Boero
260
O-540-J1A5D
Maule
Star Rocket MX-7-235
O-540-J1A5D
Maule
Super Rocket M-6-235
O-540-J1A5D
Maule
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
IO-540-A1A5
Doyn Aircraft
Doyn-Piper PA-23-250
IO-540-A1A5
Riley Aircraft
Rocket-Cessna 310
IO-540-A1A5
Dornier
DO-8-B 1
IO-540-A1A5
Siai-Marchetti

IO-540-C1B5
Piper Aircraft
Aztec B PA-23-250
IO-540-C1B5
Piper Aircraft
Comanche PA-24-250
IO-540-C1C5
Riley Aircraft
Turbo-Rocket
IO-540-C4B5
Piper Aircraft
Aztec C PA-23-250
IO-540-C4B5
Piper Aircraft
Aztec F
IO-540-C4B5
Wassmer
WA4-2 1
IO-540-C4B5
Avions Pierre Robin
HR 100/250
IO-540-C4B5
Bellanca Aircraft
Aries T-250
IO-540-C4B5
Aerofab
Renegade 250
IO-540-C4D5
S.O.C.A.T.A.
TB-20
IO-540-C4DSD
S.O.C.A.T.A.
Trinidad TB-20
IO-540-D4A5
Piper Aircraft
Comanche PA-24-260
IO-540-D4A5
Siai-Marchetti
SF-260
IO-540-D4B5
Cerva
CE-43 Guepard
IO-540-E1A5
Aero Commander
500-E
IO-540-EIB5
Aero Commander
500-U
IO-540-EIB5
Shrike
500-S
IO-540-EIB5
Poeschel
P-300
IO-540-GIA5
Doyn Aircraft
Doyn-Piper PA-23-250
IO-540-GIA5
Riley Aircraft
Turbo-Aztec
IO-540-GIA5
DeHavilland
Heron Conversion
IO-540-GIB5
T.R. Smith Aircraft
Aerostar 600
IO-540-GIB5
Found Bros.
Centennial 100
IO-540-G1C5
Intermountain Mfg. Co.
Call Air 1AR821
IO-540-G1DS
Intermountain Mfg. Co.
IAR-822, IAR-826, IAR-823
IO-540-G1F5
Bellanca Aircraft

IO-540-N lA5
Piper Aircraft
Comanche 260
IO-540-T4A5D
General Aviation
Model 114
IO-540-T4B5
Commander
1 14B
IO-540-T4B5D
Rockwell
114
IO-540-T4C5D
Lake Aircraft
Seawolf
IO-540-WIA5
Maule
MX-7-235, MT-7-235, M7235
IO-540-W1A5D
Maule
Star Rocket MX-7-235
IO-540-W1A5D
Maule
Super Rocket M-6-235
IO-540-W1A5D
Maule
Super Std. Rocket M-7-235
IO-540-W3A5D
Schweizer
Power Glider
IO-540-AB1A5
Cessna Aircraft
Skylane C-182
AEIO-540-D4A5
Christen
Pitts S-2S, S-2B
AEIO-540-D4A5
Siai-Marchetti
SF-260
AEIO-540-D4A5
H.A.L.
HPT-32
AEIO-540-D4A5
Slingsby
Firefly T3A
AEIO-540-D4B5
Moravan
Zlin-50L
AEIO-540-D4B5
H.A.L.
HPT-32
AEIO-540-D4D5
Burkhart Grob
Grob G, 1 15T Aero

These engine models are known to be installed in the aircraft models listed in the following Table 5:

Table 5.--Superior Air Parts, Inc.--Related Aircraft Models

Engine Model
Aircraft Manufacturer
Aircraft Model Designation
O-360-A3A2
American Champion
7GCBC & 7GCAA

Unsafe Condition

(d) This AD results from comments from the Public on the existing AD. We are issuing this AD to prevent cylinder separation that can lead to engine failure, a possible engine compartment fire, and damage to the airplane.

Compliance

(e) You are responsible for having the actions required by this AD performed within the compliance times specified unless the actions have already been done.

Determining Which Cylinder Assemblies Are Installed

(f) If aircraft engine records do not list the P/N of the cylinder installed during engine overhaul or repair, visually inspect the cylinders. The affected SAP cylinder head barrel flanges are marked: SA47000L-A1, SA47000L-A20P, SA47000S-A1, SA47000S-A20P, SA47000S-A21P, SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P or SL32000W-A1, SL32000W- A20P, SL32000W-A21P, SL32000WH-A1, SL32000WH-A20P, SL32006W-A1, SL32006W-A20P, SL32006W-A21P, SL36000TW-A1, SL36000TW-A20P, SL36000TW-A21P, SL36000TW-A22P, SL36000W-A1, SL36000W-A20P, SL36000W-A21P, SL36006W-A1, SL36006W-A20P, or SL36006W-A21P.

Cylinder Assembly Removal

(g) Remove all cylinder assemblies with a serial number of 47LE053559 through 47LF053643, or 47SE054212 through 47SF054251, or 52D0531708 through 52H0532197, or 55E05223 through 55G05289, or 32WE059006 through 32WF059067, or 32WHE05379 through 32WHE05392, or 326WF055517 through 326WF055532, or 36TWF05430 through 36TWG05453, or 36WF058058 through 36WG058124, or 366WE056944 through 366WF057061, or 366WF057150 through 366WF057232, or 366WF057259 through 366WG057534, or 366WG057556, 366WG057569, 366WG057598, 366WG057616, 366WG057621, 366WG057624, or 366WJ057770 through 366WJ057776, or 366WL058131 no later than 150 hours total time-in- service (TIS) to preclude cylinder head fatigue failure and separation at the head-to-barrel threaded interface.

(h) For cylinder assemblies with more than 150 hours total TIS on the effective date of this AD, a 10 hour TIS extension is permitted for the purpose of flying the aircraft to a location where maintenance action can be done to meet the requirements of this AD.

(i) After the effective date of this AD, do not install any cylinder assemblies with P/Ns SA47000L-A1, SA47000L-A20P, SA47000S- A1, SA47000S-A20P, SA47000S-A21P, SA52000-A1, SA52000-A20P, SA52000- A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P,or SL32000W-A1, SL32000W-A20P, SL32000W-A21P, SL32000WH-A1, SL32000WH- A20P, SL32006W-A1, SL32006W-A20P, SL32006W-A21P, SL36000TW-A1, SL36000TW-A20P, SL36000TW-A21P, SL36000TW-A22P, SL36000W-A1, SL36000W-A20P, SL36000W-A21P, SL36006W-A1, SL36006W-A20P, or SL36006W-A21P with a serial number of 47LE053559 through 47LF053643, or 47SE054212 through 47SF054251, or 52D0531708 through 52H0532197, or 55E05223 through 55G05289, or 32WE059006 through 32WF059067, or 32WHE05379 through 32WHE05392, or 326WF055517 through 326WF055532, or 36TWF05430 through 36TWG05453, or 36WF058058 through 36WG058124, or 366WE056944 through 366WF057061, or 366WF057150 through 366WF057232, or 366WF057259 through 366WG057534, or 366WG057556, 366WG057569, 366WG057598, 366WG057616, 366WG057621, 366WG057624, or 366WJ057770 through 366WJ057776, or 366WL058131 into any engine.

AlternativeMethods of Compliance

(j) The Manager, Special Certification Office, FAA, Rotorcraft Directorate, has the authority to approve alternative methods of compliance for this AD if requested using the procedures found in 14 CFR 39.19.

Special Flight Permits

(k) For aircraft with engines that have between 140 hours and 150 hours TIS only, special flight permits may be issued in accordance with Sec. Sec. 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the aircraft to a location where the requirements of this AD can be done. Special flight permits may not be issued for aircraft that have utilized the provisions of paragraph (h) of this AD.

Related Information

(l) Superior Air Parts, Inc. Mandatory Service Bulletin B06-01, Rev. E, dated January 24, 2007, contains information related to the subject of this AD.

(m) Contact Jurgen Priester, Aerospace Engineer, Special Certification Office, FAA, Rotorcraft Directorate, Southwest Regional Headquarters, 2601 Meacham Blvd., Fort Worth, Texas 76137; e-mail: Jurgen.E.Priester@faa.gov; telephone (817) 222-5159; fax (817) 222-5785 for more information about this AD.

Material Incorporated by Reference

(n) None.

Supplementary Information

On February 13, 2007, the FAA issued AD 2007-04-19, Amendment 39-14951 (72 FR 8089, February 23, 2007). That AD requires removing from service certain installed SAP cylinder assemblies, listed in that AD by P/N and serial number (SN), no later than 150 hours total time-in-service (TIS) to preclude cylinder head fatigue failure and separation at the head-to-barrel threaded interface. That AD was the result of nine separated SAP cylinder assemblies in TCM reciprocating engines and one in a LE reciprocating engine. That condition, if not corrected, could result in cylinder separation that can lead to engine failure, a possible engine compartment fire, and damage to the airplane.

Actions Since We Issued AD 2007-04-19

Since we issued AD 2007-04-19, we received comments that cause us to better define and reduce the applicability of this AD.

Comments

We provided the public the opportunity to participate in the development of this AD. We have considered the comments received.

Request To Provide a Range of Dates That SAP Manufactured the Suspect Cylinders

A number of commenters ask us to include the date range when SAP manufactured the cylinders. The commenters state that including the range of dates will help users to determine if they need to investigate further and will eliminate unnecessary time and money spent to determine if a suspect cylinder assembly is installed on their engine.

We agree. We changed the applicability to provide a date range to help narrow the applicability. Also, we clarified the SN range to narrow the applicability even further.

Minor Editorial Changes

We included some minor editorial changes in this AD to clarify some nomenclature.

Conclusion

We have carefully reviewed the available data, including the comments received, and determined that air safety and the public interest require adopting the AD with the changes described previously. We have determined that these changes will neither increase the economic burden on any operator nor increase the scope of the AD.

FAA's Determination and Requirements of This AD

The unsafe condition described previously is likely to exist or develop on other TCM 470, 520, and 550; LE 320, 360, and 540; AL 540, and SAP 360 series reciprocating engines of the same type design with certain SAP cylinder assemblies that have a part number listed in this AD. For that reason, we are issuing this AD to prevent cylinder separation which can lead to engine failure, a possible engine compartment fire, and damage to the airplane. This AD requires removing from service installed SAP cylinder assemblies listed in this AD, no later than 150 hours total TIS to preclude cylinder head fatigue failure and separation at the head-to-barrel threaded interface.

FAA's Determination for No Prior Public Notice

Since we do not anticipate adverse public interest in this action, a situation exists that allows for immediate adoption of this AD, and we have found that notice and opportunity for further public comment before issuing this AD are unnecessary.

Comments Invited

This AD is a final rule that involves requirements affecting flight safety and was not preceded by notice and an opportunity for public comment; however, we invite you to send us any written relevant data, views, or arguments regarding this AD. Send your comments to an address listed under
ADDRESSES. Include "AD Docket No. FAA-2007-25948; Directorate Identifier 2006-NE-32-AD'' in the subject line of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of the rule that might suggest a need to modify it.

We will post all comments we receive, without change, to http://dms.dot.gov , including any personal information you provide. We will also post a report summarizing each substantive verbal contact with FAA personnel concerning this AD. Using the search function of the DMS Web site, anyone can find and read the comments in any of our dockets, including the name of the individual who sent the comment (or signed the comment on behalf of an association, business, labor union, etc.). You may review the DOT's complete Privacy Act Statement in the Federal Register published on April 11, 2000 (65 FR 19477-78) or you may visit http://dms.dot.gov.

Examining the AD Docket

You may examine the docket that contains the AD, any comments received, and any final disposition in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The Docket Office (telephone (800) 647-5227) is located on the plaza level of the Department of Transportation Nassif Building at the street address stated in ADDRESSES. Comments will be available in the AD docket shortly after the DMS receives them.

Authority for This Rulemaking

Title 49 of the United States Code specifies the FAA's authority to issue rules on aviation safety. Subtitle I, Section 106, describes the authority of the FAA Administrator. Subtitle VII, Aviation Programs, describes in more detail the scope of the Agency's authority.

We are issuing this rulemaking under the authority described in Subtitle VII, Part A, Subpart III, Section 44701, "General requirements.'' Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action.

Regulatory Findings

We have determined that this AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national Government and theStates, or on the distribution of power and responsibilities among the various levels of government.

For the reasons discussed above, I certify that this AD:

1. Is not a "significant regulatory action'' under Executive Order 12866;

2. Is not a "significant rule'' under the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); and

3. Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act.

We prepared a summary of the costs to comply with this AD and placed it in the AD Docket. You may get a copy of this summary at the address listed under ADDRESSES.

List of Subjects in 14 CFR Part 39

Air transportation, Aircraft, Aviation safety, Safety.

Adoption of the Amendment

Under the authority delegated to me by the Administrator, the Federal Aviation Administration amends part 39 of the Federal Aviation Regulations (14 CFR part 39)as follows:

PART 39--AIRWORTHINESS DIRECTIVES

1. The authority citation for part 39 continues to read as follows:

Authority: 49 U.S.C. 106(g), 40113, 44701.

Sec. 39.13 [Amended]

2. The FAA amends Sec. 39.13 by removing Amendment 39-14951 (72 FR 8089, February 23, 2007), and by adding a new airworthiness directive, Amendment 39-15005, to read as follows:

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Related ADs
2007-04-19 This AD replaces the above
Contact Information

Jurgen Priester, Aerospace Engineer, Special Certification Office, FAA, Rotorcraft Directorate, Southwest Regional Headquarters, 2601 Meacham Blvd., Fort Worth, Texas 76137; e- mail: Jurgen.E. Priester@faa.gov; telephone (817) 222-5159; fax (817) 222-5785.

References
Federal Register: April 2, 2007 (Volume 72, Number 62)
--- - Part 39
Page 15603-15613
FAA Documents
ADs Superseded by This AD
AD Number Subject Effective Date Actions
2007-04-19 SAP cast cylinder assemblies 2007-03-12 View