FHE211-2 TURBINE ENGINE IGNITER
Part #: FHE211-2
| FHE2112 |
NSN 2920-00-957-9947
$774.40
International Orders: import duties, VAT/GST and customs brokerage fees are not included in our prices or shipping charges and are paid by the recipient on delivery.
Part Details
Part number FHE211-2 (Turbine Engine Igniter) is made by Champion and is listed under Champion (Igniters). Order online at the listed price, or call, text or WhatsApp +1 (954) 493-5088 for quantity pricing. Ask about certification and release documents (such as an FAA 8130-3) when you order.
| Part Number | FHE211-2 |
|---|---|
| Description | Turbine Engine Igniter |
| Manufacturer | Champion |
| Category | Champion (Igniters) |
| Ships From | Fort Lauderdale, Florida, USA, to 110+ countries and territories |
Aviation Parts Executive is an ASA-100 accredited aircraft parts distributor (FAA AC 00-56) in Fort Lauderdale, Florida, supplying aircraft parts since 1998.
Alternate Part Numbers
Part number FHE211-2 has 2 known alternate, superseded or replacement part numbers. Search any of them, or call, text or WhatsApp +1 (954) 493-5088 for availability.
| Part Number | Manufacturer | Relationship | Notes |
|---|---|---|---|
| 1-300-547-03 | Champion | Supersedes | |
| 1-300-348-03 | Champion | Replaces OEM Part | FAA-PMA eligibility: Honeywell T53-13A, -13B; basis: identicality |
Alternate and superseded part numbers are listed for reference from FAA PMA data, manufacturer cross-references and illustrated parts catalogs. Always confirm eligibility for your aircraft, engine and serial number before installation.
| Weight | .08 lbs |
|---|---|
| Dimensions | 5.25 × 1.75 × .88 in |
| Brands |
SPECIFICATIONS
• Color: Silver
• Suitable for Use With: Honeywell T53-13A-13B Series Aircraft Engine
• Domestic/Import: Domestic
FEATURES
• Silver-plated shell for protection against corrosion and seizing at mechanical interfaces
• Advanced glass and mechanical sealing features design outside the combustor case for protection against gas leakage under high temperature conditions
• Internal configuration designs that optimize heat flow away from terminations to protection sensitive ignition lead components
• Internal termination protective coating to prevent lead component seizing
• Firing end design configurations that can deliver igniter life up to 5000 flight cycles in select applications
• Use of external wear and thermal barrier coatings to protect the life limiting features from wear and thermal distress
• Option for three different semiconductor bodies for low voltage application requirements
TECHNICAL INFORMATION
• FAA-PMA Approved
APPLICATIONS
• Airline
• Business Aviation
• General Aviation
• Space and Military Aircraft Applications
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