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N302FD

Open the Markdown

2011 Agusta Aerospace AW139 · Pratt & Whitney Canada PT6C-67C

Open in FAA registry

© OpenStreetMap
Registered owner
Los Angeles City
Location
Van Nuys, CA
Owner type
Government
Serial number
41239
Year built
2011
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, transport
Airworthiness date
January 22, 2011
Certificate issued
February 7, 2012
Expires
February 29, 2028
Mode S code
A32741
Agusta Aerospace AW139Airframe model · 17 seats · 2 engines · 21 registeredTCDS R00002RDAirframe · Agusta Aerospace AW139TCDS E00068ENEngine · Pratt & Whitney Canada PT6C-67C

From the FAA registry file of October 22, 2026.

On this page

Airworthiness directives that may apply · 66

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

2007In forceSuperseded2026
See all 76 ADs

Information bulletins that may apply · 1

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N302FDMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Agusta Aerospace AW139 aircraft

FAA incident reports

No FAA accident or incident reports matched to N302FDMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Agusta Aerospace AW139 aircraft

Service difficulty reports

No reports matched to N302FDGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Agusta Aerospace AW139 aircraft
Reports on N302FD not matched to an aircraft · 1

They name N302FD, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

SDR 20000510SH019Fitting · crackedDURING ENGINEDECK REPLACEMENT, FOUND FUSELAGE FITTING AT LEFT FORWARD ENGINE MOUNT ATTACHMENT CRACKED. CRACKS EMANATE FROM INISDE REAR BOLT HOLE. POSSIBLE CAUSE IS HOLES NOT PROPERLY DEBURRED. SUBMITTER STATED TO PREVENT RECURRENCE, HOLES SHOULD BE DEBURREMar 2, 2000 · N302FD · Bell 412 · Fuselage, Powerplant Attach Fittings

STCs that may be installed · 77

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 77 STCs