1996 RAYTHEON AIRCRAFT COMPANY 1900D
N253GL is a 1996 RAYTHEON AIRCRAFT COMPANY 1900D registered to ALPINE AVIATION INC in PROVO, UT. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 20 Airworthiness Directives may apply.
The RAYTHEON AIRCRAFT COMPANY 1900D is registered with the FAA under N-number N253GL. This airframe was manufactured in 1996. Its manufacturer serial number is UE-253. The aircraft was issued its airworthiness certificate on 1996-11-23. The current registered owner is ALPINE AVIATION INC, based in PROVO, UT. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.
Laramie, WY, USA
Accident — Beech 1900D (NTSB DEN07LA101)
Telluride, CO, USA
Incident — Beech 1900D (NTSB DEN06IA019)
Severity reflects injuries to people involved, not damage to the aircraft. A “no injuries” accident can still involve significant aircraft damage.
N253GL 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.
Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft Company) Models 1900, 1900C, and 1900D Airplanes
We are adopting a new airworthiness directive (AD) to supersede AD 2006-24-11, which applies to certain Hawker Beechcraft Corporation (HBC) (Type Certificate previously held by Raytheon Aircraft Company) Models 1900, 1900C, and 1900D airplanes. AD 2006-24- 11 currently requires you to repetitively inspect the forward, vertical, and aft flanges of both the left and right wing rear spar lower caps for cracks, repair any cracks found, and report the inspection results to the manufacturer. Since we issued AD 2006-24-11, the manufacturer has developed a modification kit to install on the wing rear spar lower caps that will terminate the 200-hour repetitive inspection required in AD 2006-24-11. Consequently, this AD requires installing the new modification kits on the wing rear spar lower caps and terminates the repetitive inspections required in AD 2006-24-11 when the kits are installed. We are issuing this AD to prevent fatigue cracks in the wing rear spar lower caps, which could result in fatigue failure of the wing rear spar lower caps. A rear spar failure could result in complete wing failure and the wing separating from the airplane.
Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N253GL may be affected by 20 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.
+19 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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