This N-number isn't registered right now. Below is its last known registration, canceled Oct 8, 2020.
Safety record in brief:1 NTSB accident (substantial damage, May 1991)No ADs since 1998 matched129 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
THE VAN DRIVER'S INADEQUATE VISUAL LOOKOUT AND POOR DIVISION OF ATTENTION.
From NTSB records; matched by N-number.Read NTSB report (search CAROL for ATL91FA090)
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.
DURING WALKAROUND NOTICED ELECTRICAL FUME/SMELL FROM E&E COMPARTMENT AND FWD GALLEY. FOUND BATTERY CHARGER RELAY A2 TERMINAL BURNT. REMOVED A/C BATTERIES PER AMM24-30. REMOVED BATTERY CHARGER RELAY PER AMM 24-00 GENERAL. REPLACED R2-56, R2-63 AND BATTERY CHARGER REF AMM24-30. C/W NO-GO ODI…
From FAA Service Difficulty Reports; matched by N-number and serial number.RT HOR STAB AFT SPAR UPR CHORD- INBD FASTENER HAS A 3/16 INCH CRACK AT 12:00 EXTENDING PAST HEAD. MK'D VERIFIED WITH HFEC PER NDT SPM 06-10-01.001. RT HORIZONTAL STAB SPAR CAP SPLICE REPAIR COMPLETED ON 5510-01074-16 STEP 7, ACCESS GAINED FOR REPAIR RESTORED.
From FAA Service Difficulty Reports; matched by N-number and serial number.AFT SLIDE P/N D29985-103 S/N 0980 DEFECTIVE UPPER RELEASE PIN / TIE OFF. REMOVED AND REPLACE SLIDE PER 2561-4002.
From FAA Service Difficulty Reports; matched by N-number and serial number.LT WING OB TE FLAP HAS GOUGE IN UPPER SURFACE APPROX 43 IN FROM IB EDGE. REPAIRED PER PRI 569265-14 REV 0 AND 1. COMPLIED WITH ER/A 569265-14 REV ORIGINAL.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING FORWARD GALLEY NTF REPLACEMENT, FOUND CORROSION ON FLOOR BEAM BETWEEN FLOOR PANEL 160B & 160C. REPLACED FLOOR SUPPORT REF SRM 51-01, PAGE 1 AND DWG 9936534. THIS IS CONSIDERED LEVEL 2 CORROSION.
From FAA Service Difficulty Reports; matched by N-number and serial number.TAILCONE RELEASE MECHANISM CAM FAILED TORQUE CHECK. ADJUSTED CAM MECHANISM W/REF TO AMM 53-53-02.
From FAA Service Difficulty Reports; matched by N-number and serial number.NUMEROUS CEILING EMERGENCY LIGHTS OUT. REPLACED THE BATTERY PACK B5-100, B5-102, B5-106, AND B5-107 IAW AMM 33-53-00.
From FAA Service Difficulty Reports; matched by N-number and serial number.LAVATORY SMOKE DETECTOR WILL NOT TURN OFF. REPLACED THE SMOKE DETECTOR BATTERY AND TESTED GOOD IAW AMM 26-21.
From FAA Service Difficulty Reports; matched by N-number and serial number.EMERGENCY LIGHT AT 23 DE INOPERATIVE. FOUND THE CONNECTOR DISCONNECTED. RECONNECTED.
From FAA Service Difficulty Reports; matched by N-number and serial number.OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 11 AND 15 INOP. REPLACED BATTERIES AT BATTERY PACK ROW 12 RIGHT. OPS CKS GOOD PER AMM 33-50.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 129 reports.