Safety record in brief:1 NTSB accident (substantial damage, Oct 2002)No ADs since 1998 matched12 service difficulty reports
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The failure of the right main landing gear locking device to engage, which allowed the right main landing gear to collapse during taxi from landing.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC03LA012)
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.
6-8 INCH CRACK @ STA 699-704 APPX. RBL 24. REPAIR OF SKIN DAMAGE CAUSED BY CARGO LOADING/UNLOADING. REPAIR DAMAGE TO FUSELAGE SKIN @ STA 699-704 RBL 24 PER STS ENGINEERING AUTHORIZATION 81-2021-039.
From FAA Service Difficulty Reports; matched by N-number and serial number.BULKHEAD SKIN REPAIR AT F/STA 704. TO REPAIR A CORRODED SKIN SECTION ON THE REAR BULKHEAD. PERFORM BULKHEAD SKIN REPAIR PER SRM AN 01-25LA-3 TABLE 82 AND FIGURE 229 & EAC DRAWING #1930-01.
From FAA Service Difficulty Reports; matched by N-number and serial number.CRACKED FRAME AT F/STA 173.5 STRINGER 9R. TO REPAIR A CRACKED FUSELAGE FRAME. REMOVE AND SAVE MANUFACTURERS SPLICE BETWEEN STRINGER 11L & 12L. CUT DAMAGE FRAME ABOVE STRINGER 10L. MANUFACTURE AND INSTALL NEW FRAME SECTION PER SRM AN 01-25LA-3, FIGURE 69 & 70 AND DRAWING #1929-01 USING MS20470AD5…
From FAA Service Difficulty Reports; matched by N-number and serial number.LEFT WING LE REPAIR WING STATION 376 TO 412. TO REPAIR DAMAGE TO LE OF LT WING FROM WING STATION 376 TO 412. REPAIR TOP WING SKIN AFT OF LE TO STRINGER U-15. REPLACEMENT OF STRINGER U-18 & REPAIR OF WING RIB LE PORTION AT STATION 412.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING FLIGHT SHUTDOWN NR 1 ENGINE DUE TO OIL QUANTITY AND OIL PRESSURE FLUCTUATION.
From FAA Service Difficulty Reports; matched by N-number and serial number.FLIGHT CREW EXPERIENCED VOLTAGE SPIKES, TURNED OFF ALL GENERATORS, STILL HAD VOLTAGE SPIKES AND THE TURNED OFF ALL ELECTRICAL SYS.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING THE ACCOMPLISHMENT OF THE DETAILED VISUAL INSPECTION REQUIRED BY AD 58-17-02 PARA 2 TWO CRACKS WERE FOUND ON THE ELEVATOR HINGE WEB. BOTH CRACKS ARE ON THE LT HORIZONTAL STABILIZER ONE AT STA 87 HINGE AND ONE AT STA 127 HINGE. REPAIRED IAW EAC EO 1120 AND 8110-3 DATED 6/10/2011.
From FAA Service Difficulty Reports; matched by N-number and serial number.FUSELAGE FRAME 583.5 WAS FOUND BUCKLED AT STR 31 LT. REPAIRED IAW EO 1111 AND 8110-3, DATED 04-01-2011.
From FAA Service Difficulty Reports; matched by N-number and serial number.FUSELAGE SKIN FOUND DENTED FROM FUSELAGE STA 563L TO 583.5L, BETWEEN STR 31 AND 32. REPAIRED IAW EO 1111 AND 8110-3 FORM DATED 04/01/2011.
From FAA Service Difficulty Reports; matched by N-number and serial number.COMPLETE AND TOTAL LOSS OF HYDRAULIC PRESSURE AND FLUID. A/C LANDED UNEVENTFULLY REPLACED HYDRAULIC PRESSURE LINE PART NUMBER 20-575-1209 AT MAIN ACCUMULATOR DUE TO CRACK NEAR FLARED END.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 12 reports.