N381DA
Registered owner: ACLA AVIATION LLC, SC (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
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.
7 reports on file, 2000-11-02 – 2007-01-29.
Part: FLOOR SUPPORT — CORRODED (BS 950 RBL 52) · airframe 23,012 hrs · 10,062 cycles
DURING PSV 8, FOUND CORROSION WHICH WAS OUT OF LIMITS ON AFT RIGHT LAVATORY FLOOR SUPPORT AT STA 950 RBL 52. DAMAGE WAS LIMITED TO AN AREA .080 DIA AND .013 DEEP. REPAIR ACCOMPLISHED ON NR 235. PART REPLACED WAS MPN 147A5660-2.
Part: SKIN — PUNCTURED (BS 365-382) · airframe 18,936 hrs · 8,491 cycles
THE FUSELAGE SKIN WAS STRUCK BY GROUND EQUIPMENT BETWEEN FS 365 & 382, JUST ABOVE STRINGER 24R. THE DAMAGE TO THE SKIN WAS REMOVED WITH A 20 X 6 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 451256-14, REV A.
Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 16,734 hrs · 7,622 cycles
EMERGENCY LIGHTS FROM SEAT ROW 23 AFT INOP. REPLACED FUSE IN EMERGENCY BATTERY CHARGER M1672.
Part: BATTERY — MISSING (CABIN) · airframe 15,960 hrs · 7,329 cycles
CABIN ROGER UNIT SMOKED IN FLIGHT. BATTERIES REMOVED BY FLIGHT ATTENDANT. CABIN ROGER UNIT NR 1995 SER NUMBER 101433 REMOVED FROM A/C BY GATE GOURMET.
Part: LENS — CRACKED (LT OVERWING) · airframe 13,987 hrs · 6,549 cycles
LEFT OVERWING EMERGENCY EXIT PATH LIGHT LENS BROKEN WON`T STAY ON LIGHT ASSY. REPLACED LENS.
Part: TRANSMITTER — INTERMITTENT (LT WING) · airframe 13,733 hrs · 6,458 cycles
SELECTING FLAPS ON APPROACH TRAILING EDGE FLAPS STOPPED BETWEEN UP AND 1 DEG AND LEADING EDGE TRANSIT AMBER LIGHT ILLUMINATED. COMPLIED WITH ABNORMAL CK LIST AND LANDED WITH TOUCH DOWN SPEED OF 178 KTS. AUTO BRAKES SET TO 2, WT 139.5 T/S PER FIM 27-51-00-810-836. SYSTEM CHECKS GOOD. NO CURRENT FAULTS ON FSEU. DUE TO FAULT 27-52259. T/E FLAP SENSOR L ON FSEU HIST LEG 12. REPLACED LT FLAP POS IND SENSOR PER MM. ALL CKS GOOD. NOT AN RII ITEM PER TOPPS 40-30-05.
Part: SMOKE — DETECTED (CABIN) · airframe 3,615 hrs · 1,786 cycles
AFTER T/O SMOKE SMELLED IN CABIN AND COCKPIT. SMOKE SEEN IN FWD LAV. UNABLE TO DUPLICATE ON THUROUGH OPERATIONAL INSPECTION OF ENGINES AND ENVIRONMENTAL CONTROL SYSTEMS. REPLACED RECIRC AIR FILTERS AS PRECAUTION.