Safety record in brief:1 NTSB accident (substantial damage, Apr 2018)No ADs since 1998 matched7 service difficulty reports
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The failure of the left main landing gear upper arm forging due to fatigue cracking and subsequent overstress, which resulted in the collapse of the landing gear during the landing roll.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for WPR18LA129)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
No ADs published since 1998 matched this airframe or engine model.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
HYDRAULIC REGULATOR WAS INSTALLED IN THIS AIRCRAFT AS A OVERHAULED, EXCHANGED. THIS UNIT FAILED DURING TAKEOFF, WHICH PREVENTED HYDRAULIC PRESSURE TO BUILD UP TO SYSTEM PRESSURE. UNIT WAS REMOVED AND REPLACED BY THE OWNERS ORIGINAL REGULATOR AFTER IT WAS OVERHAULED BY AN OUTSIDE VENDOR.…
From FAA Service Difficulty Reports; matched by N-number and serial number.LEFT WINDSHIELD OUTER LAYER SHATTERED AT ALTITUDE. WINDSHIELD HEAT OPERATED NORMALLY PRIOR TO INCIDENT. 500 HOURS ON WINDSHIELD.
From FAA Service Difficulty Reports; matched by N-number and serial number.ACFT RETURNED FOR FUSELAGE INSP AND FINAL REPAIRS OF THE RT WING. DURING INSP, CORROSION FND IN THE LT WING IN SAME AREA, WS 39, BOTTOM SIDE, FWD OF THE MAIN SPAR. EFFECTED PARTS, THE L/E SKIN, STR NR 6 INBD, AND 2 ANGLES FWD. EXTENT OF CORROSION REQUIRED THESE PARTS TO BE REPLACED. BOTH AREAS…
From FAA Service Difficulty Reports; matched by N-number and serial number.ACFT RETURNED FOR FUSELAGE INSP AND FINAL REPAIRS OF THE RT WING. DURING INSP, CORROSION FND IN THE LT WING IN SAME AREA, WS 39, BOTTOM SIDE, FWD OF THE MAIN SPAR. EFFECTED PARTS, THE L/E SKIN, STR NR 6 INBD, AND 2 ANGLES FWD. EXTENT OF CORROSION REQUIRED THESE PARTS TO BE REPLACED. BOTH AREAS…
From FAA Service Difficulty Reports; matched by N-number and serial number.AFTER RIGHT AFT LOWER NACELLE REMOVED TO FACILITATE MAINTENANCE, DISCOVERED THAT DURING A PREVIOUS LANDING GEAR REMOVAL, THE LEFT AND RIGHT OUTBOARD MLG TRUSS SUPPORTS WERE ACCIDENTLY DRILLED WHEN THE OUTBOARD TRUNNION PIN COVER WAS DRILLED OFF. THE LEFT TRUSS WAS REPAIRED BY BLENDING, BUT THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.THE LT AND RT ENGINE FIREWALLS FOUND TO HAVE CRACKS IN THE ALUMINUM PORTION OF FIREWALL AT THE AFT ENGINE MOUNT UPPER ATTACH FASTENERS DURING OTHER MAINTENANCE REQUIRING THE LOWER AFT NACELLES TO BE REMOVED. WITH THE NACELLES REMOVED, THE CRACKS ARE VISIBLE. ACCOMPLISHED A DER REPAIR SIMILAR TO…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A 100-HOUR INSPECTION, THE RT MLG INBOARD TRUSS ATTACH ANGLE WAS FOUND TO HAVE A 0.9 INCH RADIUS CRACK 1.0 INCH FROM AFT END. THIS CRACK WAS STOP DRILLED AND A DOUBLER AND RADIUS BLOCK WAS INSTALLED PER DER'S REPAIR SCHEME. CRACKS APPEAR TO BE ASSOCIATED WITH AIRCRAFT HAVING MORE THAN 2,000…
From FAA Service Difficulty Reports; matched by N-number and serial number.