N325NW

GATES LEARJET CORP. 35A · 1980 · Fixed-wing multi-engine · 2 engines · 10 seats · Valid Registration

Registered owner: KALITTA CHARTERS LLC, MI (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
Crow Executive Air, Inc. (DRUA)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.

4 reports on file, 2009-08-19 – 2010-02-11.

OTHER · 2010-02-11 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — BROKEN (CABIN) · corrosion level 2 · airframe 52,749 hrs · 23,599 cycles

DURING "H" CHECK FOUND FLOOR PANEL 231FF HAS BROKEN CORNERS. REPLACED FLOOR PANEL. WORK ACCOMPLISHED IAW DWG 3D25-37498.

Source: SDR DALA103463225
OTHER · 2010-02-11 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 52,749 hrs · 23,599 cycles

DURING "H" CHECK FOUND FLOOR PANEL 231CF HAS CORRODED INSERTS AND A TORN EDGE. REPLACED FLOOR PANEL. WORK ACCOMPLISHED IAW DWG 3D25-37498.

Source: SDR DALA103473225
OTHER · 2010-02-11 Matched by certificate designator
ATA 5321

Part: FLOOR PANEL — DELAMINATED (CABIN) · corrosion level 2 · airframe 52,749 hrs · 23,599 cycles

DURING "H" CHECK FOUND FLOOR PANEL 261EF DELAMINATED. REPLACED FLOOR PANEL. WORK ACCOMPLISHED IAW DWG 3D25-37498.

Source: SDR DALA103453225
OTHER · 2009-08-19 Matched by certificate designator
ATA 2910

Part: LINE — CORRODED (HYD SYSTEM) · airframe 12,554 hrs · 11,402 cycles

LINE HAD CORROSION ON 90 DEGREE BENDS ADJACENT TO FERRULES FOR B-NUTS. THE PORTION OF THE LINE AT BOTH ENDS HAD CORROSION THA WAS PRESENT WHERE THE PROTECTIVE COATING WAS REMOVED, APPARENTLY DURING MFG OF THE PART. THE CORROSION HAD EATEN THROUGH ONE END OF THIS LOCATION SUFFICIENT TO REDUCE WALL THICKNESS ALLOWING LINE TO BURST.

Source: SDR 2009FA0000766