3606110-1
OEMActive ADElevator Trim Tab Actuator Assembly
Where to Buy
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Documentation
General information based on part classification, not a certification determination. Your operator's quality manual governs.
What to ask the seller for
- FAA Form 8130-3 from the PAH or an authorized release traceable to the PAH
- Manufacturer's CofC if a Form 8130-3 was not issued
Governing reference: FAA Order 8130.21J
PMA Alternatives
No PMA alternatives found for this part. This does not mean none exist — only that none are currently in our database.
Supplemental Type Certificates
FAA-approved modifications that reference this part number
No current STCs reference this part number in their description.
Airworthiness Directives1 FAA Active
Synced 41 days ago (09/27/2026)AD 2024-15-07
Inspection of elevator trim tab actuator mounting bolts
Reports of mounting bolt loosening due to vibration. Inspection of bolt torque and condition required within 500 flight hours, with replacement of any bolts found below torque spec.
Service Difficulty Reports2 reports
Elevator trim tab actuator found with excessive play during scheduled inspection. Actuator rod end bearing worn beyond limits. Aircraft: CL-600-2B16, 12,450 flight hours.
Trim tab actuator intermittent operation reported during flight. Investigation revealed corroded electrical connector. Connector replaced, actuator tested serviceable.
Suspect-Parts Alerts (SUP/UPN)
No Suspect-Parts Alerts
This manufacturer is not named in any active FAA Suspect Unapproved Parts (SUP/UPN) notification.
NSN Cross-References
National Stock Numbers assigned to this part number by the U.S. Defense Logistics Agency
No government NSN assignment found for this part number in DLA WebFLIS PUBLOG.
Government Award Prices
U.S. government contract award prices from FPDS — unit prices for NSN purchases by DoD/DLA agencies
No government contract award price data found for this part number.
Identifiers
Manufacturer
Bombardier
Source
FAA PMA/IPCL
ATA Chapter
27
Type
OEM