N141DR

No registry detail on file · not in current registry

Operators of this aircraft

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

OperatorRolePeriodBasis
Martinair, Inc. (MXIA)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.

3 reports on file, 2005-02-23 – 2007-09-12.

OTHER · 2007-09-12 Matched by certificate designator
ATA 5510

Part: STRUCTURE — DAMAGED (HORIZONTAL STAB)

WHILE PERFORMING A SCHEDULED A-D INSPECTION FOUND 6 SHEARED RIVETS AND 2 LOOSE RIVETS IN THE FORWARD RIVET LINE OF THE ATTACHMENT PIVOT FITTING PN 45A21183-11 ON THE BOTTOM OF THE HORIZONTAL STABILIZER. IT IS SUSPECTED THAT THE MISSING RIVETS FAILED FROM FATIGUE. RECOMMEND INSPECTING AREA THOROUGHLY AT EACH INSPECTION, CONTACTING MFG FOR REPAIR OPTIONS. THIS IS SECOND AC THAT THE SAME DISCREPANCY HAS BEEN FOUND. (K)

Source: SDR 2007FA0000833
OTHER · 2007-09-12 Matched by certificate designator
ATA 5610

Part: WINDOW — CRACKED (COPILOT)

WHILE PERFORMING A SCHEDULED A-D INSPECTION FOUND COPILOT COCKPIT SIDE WINDOW CRACKED USING THE PRISM INSPECTION METHOD. THE D-INSPECTION REQUIRES THAT BOTH WINDSHIELDS BE INSPECTED BY REMOVING THE WINDSHIELD RETAINERS OR USING OPTICAL PRISM INSPECTION METHOD. THERE IS NO STATEMENT IN THE AC MM OR IN THE A-D INSPECTION CHECKLIST THAT REQURIES YOU TO INSPECT THE COCKPIT SIDE WINDOWS IN THE SAME MANNER AS THE WINDSHIELDS. ALL OF THE WINDOWS IN THE COCKPIT AREA ARE INSTALLED OR FASTENED IN THE SAME MANNER AS THE WINDSHIELDS. IT IS SUSPECTED THAT THE COPILOT SIDE WINDOW CRACKED FROM FATIGUE, OR TOTAL TIME INSTALLED. THE WINDOW WAS MFG MAY OF 1997. WOULD RECOMMEND THAT INSPECTION OF ALL COCKPIT WINDOWS WITH A

Source: SDR 2007FA0000832
WARNING INDICATION · 2005-02-23 Matched by certificate designator
ATA 3231

Part: SWITCH — FAILED (GEAR DOOR) · airframe 3,388 hrs

THE LANDING GEAR WOULD NOT EXTEND WITH GEAR HANDLE DOWN. GEAR WAS LOWERED USING THE MANUAL EMERGENCY EXTENSION AND THE GEAR DOORS WERE CLOSED USING THE PNEUMATIC GEAR BOTTLE. PROBABLE CAUSE WAS THE HIGH RESISTANCE IN THIS SWITCH AND THE GEAR DOOR CLOSED SWITCH. (K) (EA21200504860)

Source: SDR MXI2005F00000