N55AG

Valid Registration

1965 PIPER PA-30

N55AG is a 1965 PIPER PA-30 registered to AIRCRAFT GUARANTY CORP TRUSTEE in OKLAHOMA CITY, OK. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 3 Airworthiness Directives may apply.

Registration Details

N-Number
N55AG
Serial Number
30-804
Manufacturer
PIPER
Model
PA-30
Year
1965
Registration Status
Valid
Airworthiness Date
2010-04-19
Owner
AIRCRAFT GUARANTY CORP TRUSTEE
Owner City
OKLAHOMA CITY
Owner State
OK

The PIPER PA-30 is registered with the FAA under N-number N55AG. This airframe was manufactured in 1965. Its manufacturer serial number is 30-804. The aircraft was issued its airworthiness certificate on 2010-04-19. The current registered owner is AIRCRAFT GUARANTY CORP TRUSTEE, based in OKLAHOMA CITY, OK. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

Fatal injuries1990-05-22

HIGHLAND, NC, USA

Accident — CESSNA 182RG (NTSB ATL90FA118)

Minor injuries1983-03-30

PALM BEACH, FL, USA

Accident — CESSNA 182 RG (NTSB MIA83LA108)

Severity reflects injuries to people involved, not damage to the aircraft. A “no injuries” accident can still involve significant aircraft damage.

N55AG has been involved in 2 NTSB accidents since 1982. Each record above includes the date, location, severity, and NTSB summary. Buyers should review the full accident narratives and verify repairs in the aircraft's logbooks before purchase.

Applicable Airworthiness Directives

3 found
AD 98-29003Effective: 1998-10-29

Airworthiness Directives; The New Piper Aircraft, Inc. PA-24, PA- 28R, PA-30, PA-32R, PA-34, and PA-39 Series Airplanes

This amendment revises AirworthinessDirective (AD) 97-01-01, which currently requires repetitively inspecting the main gear sidebrace studs for cracks on The New Piper Aircraft, Inc. (Piper)Models PA-24, PA-28R, PA-30, PA-32R, PA-34, and PA-39 series airplanes, and replacing any main gear sidebrace stud found cracked. The Federal Aviation Administration (FAA) has approved certain alternative methods of compliance (AMOC) for AD 97-01-01, and has determined that these AMOC's should be incorporated into the AD. This AD will retain all the actions of AD 97-01-01, and will incorporate certain AMOC's as a way of accomplishing the actions specified in AD 97-01-01. The actions specified by this AD are intended to prevent a main landing gear collapse caused by main gear sidebrace stud cracks, which could result in loss of control of the airplane during landing operations.

Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N55AG may be affected by 3 directives. All applicable ADs must be complied with for the aircraft to remain legally airworthy. Buyers should verify AD compliance in the aircraft's logbooks before purchase.

+2 more Airworthiness Directives found for this aircraft

Full list, with effective dates and links to the official Federal Register documents, is included in the paid report.

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Other PIPER PA-30 aircraft in our database

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Get the complete history for N55AG

Full accident narratives, all Airworthiness Directives, ownership chain, and a downloadable PDF.

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