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| Make | Model | Start S/N | End S/N | Eligibility Chart |
|---|---|---|---|---|
| Lycoming | LTO-360-E1A6D | 0 | ZZZZZZZZZZZZZZZ | 7797 |
| Lycoming | TO-360-E1A6D | 0 | ZZZZZZZZZZZZZZZ | 7797 |
| Lycoming | TEO-540-A1A | 0 | ZZZZZZZZZZZZZZZ | 7797 |
| Lycoming | TIO-540-AE2A | 0 | ZZZZZZZZZZZZZZZ | 7797 |
| Lycoming | TIO-540-AF1A | 0 | ZZZZZZZZZZZZZZZ | 7797 |
| Lycoming | TIO-540-AF1B | 0 | ZZZZZZZZZZZZZZZ | 7797 |
| Lycoming | TIO-540-AG1A | 0 | ZZZZZZZZZZZZZZZ | 7797 |
Replacement for Many Continental and Lycoming Turbo Engines
FAA-PMA approval pending. AD 2023-09-09 placed a 500-hour life limit and repetitive inspection requirements on spot-welded turbo v-band clamps. Traditional clamps suffer from spot weld cracks (primary FAA AD failure mode), rivet fatigue, corrosion, and heat fatigue in high-temp exhaust environments. AeroForce v-band clamps provide a tight, continuous seal at the exhaust-to-turbo flange and are not subject to this AD, eliminating the life-limit and inspection burden on affected aircraft.
Design has been proven through 400+ hours of engine and OEM validation testing, plus in-flight trials. The clamps use the same installation process as current clamps, with 50-hour torque check, followed by inspections aligned to engine TBO.
Key Advantages:
| Engine | Engine Model | Old P/N | AeroForce P/N | Airframe | Notes |
|---|---|---|---|---|---|
Continental |
TSIO-360-RB, LTSIO-360-RB |
670105, 646434, 653337 |
Piper PA-34-220T Seneca V |
670105 does not appear in IPC, however part noted supersedes to 670105 |
|
Continental |
TSIO-360-MB, TSIO-360-SB |
670105, 646434, 653337 |
Mooney M20K-252 |
670105 does not appear in IPC, however part noted supersedes to 670105 |
|
Continental |
TSIO-520-BE |
670105, 646434, 653337 |
Piper PA-46-310P |
670105 does not appear in IPC, however part noted supersedes to 670105 |
|
Continental |
TSIO-550-C |
670105, 646434, 653337 |
Textron LC41-550FG, T240 |
670105 does not appear in IPC, however part noted supersedes to 670105 |
|
Continental |
TSIO-550-G |
670105 |
Mooney M20TN/M20V |
||
Continental |
TSIO-550-K |
670105 |
Cirrus SR22T |
||
Lycoming |
LTO-360-E1A6D |
LW-12093-8 |
Piper PA-44-180T |
||
Lycoming |
TEO-540-A1A |
40D21162-340M |
Tecnam P2012 Traveler |
40D21162-340M does not appear in IPC |
|
Lycoming |
TIO-540-AE2A |
40D23255-340M |
Piper PA-46R-350T, |
||
Lycoming |
TIO-540-AF1A, |
40D21162-340M |
Mooney M20M |
Coupling 40D21162-340M was removed via SB M20-283A and AD2024-23-17. Aircraft will have 40D23255-340M Installed |
|
Lycoming |
TIO-540-AG1A |
40D21162-340M |
Commander 114TC |
Coupling 40D21162-340M was removed via SB 113-33A and AD2000-11-04. Aircraft will have 40D23255-340M Installed |
|
Lycoming |
TO-360-E1A6D |
LW-12093-8 |
Piper PA-44-180T |
From hose and ducting to engine baffles and seals:
Choose from elastomeric and PTFE bulk hose or SCAT, SCEET, CEET, CAT, and MIL6000D ducting. Several hose options for various applications in stock, including brake, fuel, oil, and more. Firesleeves and fittings also available.
Upgrade your baffling with Airforms FAA-PMA engine baffles for hundreds of aircraft. Improve vibration and engine cooling with premium Cowl Saver baffle seal material. Available pre-installed on baffle sets, or in rolls, sheets, and complete airframe kits.
OUR PARTS ARE ENGINEERED TO LAST LONGER WHILE SOLVING KNOWN SAFETY ISSUES
OVER 40,000 PARTS IN STOCK WITH SAME DAY SHIPPING IF ORDERED BY 3PM
OUR TEAM PROVIDES THE OLD-FASHIONED CUSTOMER SERVICE THAT YOU EXPECT
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