N761DA
Registered owner: KING AIR 76 LLC, DE (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.
14 reports on file, 1996-10-17 – 1998-05-30.
Part: SKIN — CORRODED (FS 639)
FUSELAGE SKIN, FS 639, STRG 32, REPAIR FOR CORROSION CUTOUT. THE FUSELAGE SKIN AT FS 639 AND STRG 32R WAS FOUND CORRODED. THE CORROSION WAS REMOVED BY MAKING A 8.2 BY 5.8 CUTOUT IN THE SKIN. A SECTION OF STRINGER 32 WAS ALSO CUTOUT DUE TO CORROSION. THE SKIN CUTOUT WAS REPAIRED WITH AN INTERNAL TITANIUM DOUBLER. THE STRINGER WAS REPAIRED PER THE L1011 SRM. THE REPAIR WAS DOCUMENTED PER ER/A 364916-14, REV A.
Part: ENGINE — MALFUNCTIONED (NR 3)
WHILE DES FROM FL310 TO FL290, NR 3 ENG VIBE LIGHT ILLUMINATED. VIBES ROSE RAPIIDLY TO 3.5 CONFIRMED BOTH A AND B SENSORS. SHUT DOWN ENGINE PER POM. INSPECTED INLET AND EXHAUST, REMOVED AND INSPECTED CHIP DETECTORS, NO DEFECTS. LUBED FAN BLADES AND RAN ENG TO T/O POWER, ENG RUN GOOD. RETURNED TO SERVICE.
Part: BATTERY PACK — DISCHARGED (CABIN)
EMERGENCY EXTERNAL LIGHTS AT L-2 DOOR INOP. REPLACED BATTERY PACK AT SEATS 12AB.
Earlier reports · 1996–1997 · 11 reports
1997
Part: PRESS XMITTER — LEAKING (C-HYD SYST)
WHILE IN CRUISE, LOSS C-HYD SYSTEM BOTH QUANTITY AND PRESSURE HYD PRESS LOW LIGHT NEVER CAME ON. FOUND HYD PRESS TRANSMITTER LEAKING. REPLACED TRANSMITTER, INSPECTED C-SYSTEM FILTERS, CYCLED ALL CONTROL SURFACES AND ALL CKECKS NORMAL.
Part: OVEN — OVRHEATED (MID GALLEY)
GALLEY MID AFT CENTER OVENS OVERHEATS DIRTY TRAYS CAUSE SMOKE, CLEANED OVEN AND TRAYS.
Part: SKIN — CRACKED (WS 132)
WING RT LOWER SKIN OWS 132 / S-16, REPAIR FOR SKIN CRACK AT STRINGER RUNOUT. THE LOWER WING SKIN OF THE RT WING AT OWS 132 WAS FOUND WITH A CRACK AT THE END OF STRINGER 16. THE CRACK WAS TRIMMED OUT AND REPAIR DOUBLERS INSTALLED PER ER/A 363068-14 REV A.
Part: FIRE BOTTLE — DISCHARGED (NR 3 ENGINE)
NR 3 ENG WAS REPORTED TO HAVE TAIL PIPE FIRE. CREW FIRED BOTH BOTTLES AND RETURNED TO GATE. THERE WAS NO FIRE IND IN COCKPIT. MTC INSPD ENG, NO FLUID LEAKS NOTED. REPLACED BOTH FIRE BOTTLES AND RAN ENG, HAD NORMAL START. FIRE WAS CONTAINED WITHIN THE TAIL PIPE.
Part: COUNTERBALANCE — FAILED (L 1 DOOR)
L-1 DOOR INOP ELECTRICALLY AND MANUALLY. DOOR STOPS HALF WAY UP. REPLACED COUNTERBALANCE.
Part: HYD LINE — LOOSE (NR 2 ENGINE)
ENG VIB LIGHT FOR NR 2 ENG CAME ON. VIBS SHOWED 2.8 TO 3.0 IN NORM ON BOTH A AND B CHANNELS. FOLLOWED POM AND SHUT DOWN ENG. FOUND HYDRAULIC LINE FITTING LOOSE ON BRACKET, FURTHER INSPECTION REVEALED NO OTHER DISC.
Part: LIGHT — INOPERATIVE (CABIN)
EMERGENCY FLASHLIGHT AT 2R INOP. REPLACED SAME.
Part: POWER SUPPLY — INOPERATIVE (CABIN)
EMERGENCY TRACK LIGHTING INOP. REPLACED POWER SUPPY, CKS GOOD.
1996
Part: POWER SUPPLY — INOPERATIVE (CABIN)
DURING LAYOVER INSPECTION OF EMERGENCY TRACK LIGHTING SYSTEM, TRACK LIGHTS WENT OUT AFTER 2 MINUTES. NOTICED POWER SUPPLY\CHARGING ERRATICALLY FOR A MINUTE AND THEN STOPPED ALL TOGETHER. REPLACED POWER SUPPLY ASSY AND OPERATION CHECKS NORMAL.
Part: POWER SUPPLY — INOPERATIVE (CABIN)
ON L/O, FOUND EXTERIOR EMERGENCY LIGHTS FWD PART OF A/C EXTINGUISHED AFTER 2 MINUTES OF TEST. REPLACED POWER SUPPLY, OPS CHK OK.
Part: POWER SUPPLY — INOPERATIVE (CABIN)
ON L/O, FOUND F/C EMERGENCY TRACK LIGHTING INOP. REPLACED POWER SUPPLY RT HAND SIDE, OPS CHK NORMAL.