N695DA
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.
8 reports on file, 2000-10-05 – 2006-12-13.
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 27,474 hrs · 11,612 cycles
T/E FLAP DISAGREE MSG WHEN EXTENDING FLAPS FROM 15DEG TO 20DEG USED ALT FLAPS SYS TO EXTEND FLAPS 20DEG PER QRH. FOUND LT I/B XMSSN INDICATOR POPPED. RESET INDICATOR. LUBED FLAPS INSPECTED ROLLER AND TRACKS--NTF. OPERATED FLAPS. ALL CKS NORMAL. SERVICED NR 6 AND 7 XMSNS TO FULL FLAPS OPERATED NORMAL.
Part: COFFEEMAKER — ODOR (AFT GALLEY) · airframe 22,917 hrs · 10,102 cycles
FUMES IN AIRCRAFT AT R3 AREA IN CABIN ONLY IN AFT GALLEY FL380 2 HRS INTO FLT / OPENED PANELS IN REAR GALLEY, NTF. CHECKED BEHIND C/B PANEL ALL CONNECTIONS TIGHT CHECKED CONNECTOR ON CURRENT TRANSFORMER, ALL NORMAL. CLEANED OVERHEAD VENT FILTERS. CHECKED BEHIND OVERHEAD LIGHT FIXTURE, ALL GOOD. REPLACED COFFEEMAKER AS PRECAUTIONARY.
Part: CONNECTOR — LOOSE (CABIN) · airframe 15,598 hrs · 7,388 cycles
RED EMERGENCY LIGHT ON LAV FWD OF SEAT ROW 9 INOP. SECURED CONNECTION.
Part: ENGINE — MAKING METAL (NR 2) · airframe 14,389 hrs · 6,862 cycles
RT ENGINE CSD QUIT, WENT THROUGH NORMAL DISCONNECT PROCEDURES, CSD DISCONNECTED OK. AFTER CSD DISCONNECTED GOT A RT ENGINE OIL FILTER LIGHT, OPENED UP THE QRH AND STARTED TO GO THROUGH THE PROCEDURE WHEN THE ENGINE SPOOLED DOWN ON ITS OWN. NEVER FINISHED THE PROCEDURES. DIVERTED INTO NAS. REPLACED RIGHT ENGINE.
Part: GENERATOR — INOPERATIVE (NR 1 ENGINE) · airframe 8,300 hrs · 3,925 cycles
LT GENERATOR DRIVE MESSAGE ON EICAS DURNING T/O ROLL. FOUND LEFT GENERATOR TO MCO AND PLC PER MEL 24-00-01
Part: SKIN — DELAMINATED (NR 1 SLAT) · airframe 7,476 hrs · 3,535 cycles
SLAT DELAMINATED. NUMBER ONE SLAT SEALER CRACKED AND T/E WEDGE DELAMINATED AT UPPER OUTBD T/E. REF SUPPLEMENTAL CARD ATTACHMENT A.
Part: ENGINE — FOD (NR 2) · airframe 6,597 hrs · 3,113 cycles
DURING CLIMBOUT OF MEX, NR 2 ENGINE HAD A COMPRESSOR STALL FOLLOWED BY RT ENGINE SHUT DOWN. A/C RETURNED TO MEX. REPLACED RT ENGINE.
Part: HARNESS — SHORTED (CABIN) · airframe 6,525 hrs · 3,077 cycles
DURING LAYOVER INSPECTION, THE EMERGENCY ESCAPE PATH LIGHTING WAS INOPERATIVE FROM ROW 38 TO ROW 45. FOUND FUSE F2 OPEN ON POWER SUPPLY M9102. CAUSE OF BLOWN FUSE WAS FOUND TO BE THE PATH LIGHTING HARNESS OF SEAT ROW 38 WHERE THE WIRES HAD BEEN PULLED FROM THE CONNECTOR AND SHORTED TO EACH OTHER. THE SEAT HARNESS (P/N 334202641) WAS REPLACED ALONG WITH FUSE F2.