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N212HP

Open the Markdown

1979 Bell 212 · Pratt & Whitney PT6 series

Open in FAA registry

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Registered owner
Corpat Inc
Location
Missoula, MT
Owner type
Corporation
Serial number
30951
Year built
1979
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, transport
Airworthiness date
March 21, 2001
Certificate issued
June 26, 2019
Expires
June 30, 2029
Mode S code
A1C1AD
Bell 212Airframe model · 15 seats · 2 engines · 54 registeredTCDS H4SWAirframe · Bell 212Engine modelPratt & Whitney PT6 series

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney PT6 model are included below.

On this page

Airworthiness directives that may apply · 99

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

1968In forceSuperseded2026
See all 126 ADs

Information bulletins that may apply · 10

Advisory, not mandatory.

Historical bulletins · 1
SAIB SW-05-10Issued Nov 5, 2004

NTSB investigations · 1

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

NTSB WPR09TA356Accident · 1 fatalFinal reportWillow Creek, CAThe rappeller's failure to properly latch the rappelling harness to the rappelling assembly before exiting the helicopter.Jul 21, 2009 · No damage

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Accident 20090721017989ACruise/Level Flight · Willow Creek, CA(-23) On July 21, a rappeller sustained fatal injuries from an un-arrested descent out of a helicopter from an altitude of approximately 200 feet. The accident occurred during rappel proficiency training. As the individual was moving into the rappel position…Jul 21, 2009 · No damage · 1 fatal
Reports on N212HP not matched to an aircraft · 1

They name N212HP, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

Incident 19980605021889IAmtr Velocity · Breaux Bridge, LARough engine. High temp low oil pressure. Engine siezed. Connecting rod failed.Jun 5, 1998

Service difficulty reports · 1

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR X1Y2012F00000Rod · failedSTABILIZER BAR DAMPER ROD, ROD END BEARING, PN 47-140-252-003, BECAME LOOSE IN ALUMINUM TUBE DUE TO RIVET WEAR AND LACK OF ADHESIVE ON ASSEMBLY. CONTROL ROD BEARING AND FITTNG MUST BE INSTALLED IAW SRM IAW MFG.Aug 1, 2012 · N212HP · Bell 212 · Rotorcraft Flight Control

STCs that may be installed · 414

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

See all 414 STCs