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490127-0001_&_490127-0000_ANGLE_FRONT_HET_V-Band_Clamp

Part Number 490127-0000

490127-0000, CLAMP, V-band

Part # 490127-0000

CLAMP, V-band


$1,538.36 Retail Price: $1,922.95
In Stock

Product Details

Specifications

Approval
FAA PMA
Condition
New
Manufacturer
Hartzell Engine Technologies
Dimensions
L: 5 x W: 5 x H: 9 in
Weight
1 lbs
Unit of Measure
Each
McFarlane Part Number
490127-0000

Product Description

Hartzell Engine Tech V-Band Clamp 490127-0000

FAA-PMA Turbo Exhaust Clamp for Lycoming TIO / TEO / LTO Series Engines

The AeroForce 490127-0000 V-Band Clamp is an FAA-PMA approved replacement for Lycoming turbocharged exhaust systems, including TIO-540, TEO-540, LTO-360, and related applications.
This clamp secures the exhaust-to-turbocharger flange connection, maintaining a tight, continuous seal in high-heat turbo environments. Proper sealing is critical to prevent exhaust leakage, carbon monoxide intrusion, turbocharger inefficiency, and potential engine power loss.
Following AD 2023-09-09, many spot-welded V-band clamps are subject to a 500-hour life limit or recurring 100-hour / 6-month inspections. The Hartzell PMA clamp is not subject to this AD, providing a long-term replacement option for Lycoming operators seeking reduced compliance burden.

Why Choose 490127-0000:

  • FAA-PMA approved for applicable Lycoming turbo engines
  • Not subject to AD 2023-09-09 life limits
  • Weld-free, rivet free construction to eliminate legacy weak points
  • Braided wire cable and a floating retainer for improved load distribution and durability
  • Integrated cable safety retention band for added security
  • Designed for high-heat turbocharger exhaust connections
  • Direct replacement for applicable OEM Lycoming part numbers

Inspection and Replacement Considerations

Replace the clamp if any of the following conditions are found:

  • Cracked or deformed T-bolt
  • Uneven band gap or clamp distortion
  • Evidence of exhaust leakage at turbo flange
  • Loss of proper torque retention

Inspect at each 100-hour, annual, or condition inspection per Hartzell Engine Technologies Service Information AF3003

Engine Engine Model Old P/N AeroForce P/N Airframe Notes

Continental

TSIO-360-RB, LTSIO-360-RB

670105, 646434, 653337

490127-0001

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

490127-0001

Mooney M20K-252

670105 does not appear in IPC, however part noted supersedes to 670105

Continental

TSIO-520-BE

670105, 646434, 653337

490127-0001

Piper PA-46-310P

670105 does not appear in IPC, however part noted supersedes to 670105

Continental

TSIO-550-C

670105, 646434, 653337

490127-0001

Textron LC41-550FG, T240

670105 does not appear in IPC, however part noted supersedes to 670105

Continental

TSIO-550-G

670105

490127-0001

Mooney M20TN/M20V

Continental

TSIO-550-K

670105

490127-0001

Cirrus SR22T

Lycoming

LTO-360-E1A6D

LW-12093-8

490127-0000

Piper PA-44-180T

Lycoming

TEO-540-A1A

40D21162-340M

490127-0000

Tecnam P2012 Traveler

40D21162-340M does not appear in IPC

Lycoming

TIO-540-AE2A

40D23255-340M

490127-0000

Piper PA-46R-350T,
Piper PA-46-350P

Lycoming

TIO-540-AF1A,
TIO-540-AF1B

40D21162-340M

490127-0000

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

490127-0000

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

490127-0000

Piper PA-44-180T


Improve Airflow and Cooling

From hose and ducting to engine baffles and seals:

Hose and Ducting

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.

Engine Baffles

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.

WARNING: Cancer and/or Reproductive Harm - California Proposition 65 Resources

Eligible Aircraft
Make Model Start S/N End S/N Eligibility Chart
Lycoming LTO-360-E1A6DLTO-360-E1A6DS/N 0 – ZZZZZZZZZZZZZZZZZZZZZZZZZZZZZZEligibility Chart 7797
Lycoming TO-360-E1A6DTO-360-E1A6DS/N 0 – ZZZZZZZZZZZZZZZZZZZZZZZZZZZZZZEligibility Chart 7797
Lycoming TEO-540-A1ATEO-540-A1AS/N 0 – ZZZZZZZZZZZZZZZZZZZZZZZZZZZZZZEligibility Chart 7797
Lycoming TIO-540-AE2ATIO-540-AE2AS/N 0 – ZZZZZZZZZZZZZZZZZZZZZZZZZZZZZZEligibility Chart 7797
Lycoming TIO-540-AF1ATIO-540-AF1AS/N 0 – ZZZZZZZZZZZZZZZZZZZZZZZZZZZZZZEligibility Chart 7797
Lycoming TIO-540-AF1BTIO-540-AF1BS/N 0 – ZZZZZZZZZZZZZZZZZZZZZZZZZZZZZZEligibility Chart 7797
Lycoming TIO-540-AG1ATIO-540-AG1AS/N 0 – ZZZZZZZZZZZZZZZZZZZZZZZZZZZZZZEligibility Chart 7797
Cross Reference

Reference only: Please verify the product is eligible for your aircraft before adding to your cart.

  • 40D21162-340M
  • 40D23255-340M
  • LW-12093-8
FAQs

What is AD 2023-09-09 and how does it affect v-band clamps?

This AD applies to spot-welded turbo v-band clamps and introduces a 500-hour life limit or repetitive 100-hour/6-month inspections due to fatigue cracking and separation risk. The AeroForce v-band clamps from McFarlane are not subject to the AD.

Are these AeroForce clamps affected by the AD?

No. These clamps are not spot-welded and are not subject to the requirements of AD 2023-09-09.

What makes these clamps different from the OEM clamps?

They use a reinforced band design with an integrated safety cable for secondary retention and are not life-limited by the AD

What does the safety cable do?

The cable provides a backup restraint to help prevent clamp separation if the primary band were to loosen or fail.

Should the exhaust gasket be replaced when installing a new v-band clamp?

Yes. Any time the exhaust or turbo flange joint is separated, the gasket or fire ring should be replaced and the mating surfaces inspected. Browse the McFarlane website to find gaskets applicable to your aircraft or engine.

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