N807DE
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.
34 reports on file, 1995-11-10 – 2003-10-19.
Part: POWER SUPPLY — BURNED (COCKPIT) · airframe 49,904 hrs · 6,414 cycles
IN FLIGHT SMOKE FROM POSER SUPPLY/ MONITOR ASSY POWER SUPPLY HAS A DISTINCT ODOR OF SMOKE. REPLACED ASSY.
Part: AMPLIFIER — ODOR (PA SYSTEM) · airframe 49,900 hrs · 6,410 cycles
PA FAILED IN FLT. PA AMP NR 1 CB PULLED AND AMP REMOVED DUE TO COMPLAINTS OF ELECTRICAL ODOR. REPLACED PA AMP.
Earlier reports · 1995–2002 · 32 reports
2002
Part: CONTROL PANEL — MALFUNCTIONED (GALLEY OVEN) · airframe 47,486 hrs · 6,032 cycles
OVEN NR 2 BURNING METAL ORDO FROM ELECTRICAL TOUCH PANEL AREA AROUND PANEL HOT C/B PULLED RESET C/B RAN OVEN TO 350 DEGREES FOR 20 MINUTES NO DEFECTS NOTED OK FOR SERVICE
Part: INDICATOR — OVERHEATED (F/O SIDE) · airframe 45,592 hrs · 5,726 cycles
AT CRUISE GOT A VERY STRONG ACRID ELEC SMELL NOTICED THAT F/O IVSI WENT BLANK AND WAS HOT TO TOUCH. PULLED CB AND DIVERTED TO SNN CA FOUND F/OS IVSI TO HAVE BURNT SMELL. WIRING AND CONNECTORINSPECTED NO TROUBLE FOUND. RPLD F/OS IVSI.
Part: MEGAPHONE — FAILED (AFT) · airframe 45,518 hrs · 5,710 cycles
AFT CABIN MEGAPHONE WILL NOT TEST. REPLACED MEGAPHONE.
2001
Part: ODOR — DETECTED (CABIN) · airframe 42,906 hrs · 5,359 cycles
ODOR OF BURNING RUBBER IN CABIN DURING CRUISE. UNABLE TO LOCATE OR DUPLICATE.
Part: CONTROL PANEL — FAILED (COCKPIT) · airframe 42,788 hrs · 5,345 cycles
AFTER T/O, A/P & A/T WOULD NOT ENGAGE. REPLACED GCP PER MM.
Part: FAN — NOISY (CABIN) · airframe 42,547 hrs · 5,318 cycles
ORIGINAL DEPARTED NGO. ELECTRICAL FUMES DETECTED ONE HOUR INTO FLIGHT. STRONGEST ODOR IN FORWARD CABIN CLOSE TO THE STAR WARS PANEL DIVERTED TO NARITA. LANDING WEIGHT 425,000LBS. PERFORMED ENTIRE CABIN INSPECTION. FOUND NR 2 RECIRCULATION FAN MAKING EXCESSIVE NOISE DEACTIVATED NR 2 RECIC-FAN AND DEACTIVATED NR 4 RECIRC-FAN DUE TO HIGH SERVICE TIME AS PRECAUTION FWD FAN TO MCO AND PLAC REF MEL 21-22-03 LANDING WEIGHT WITHIN LIMITS NO INSPECTION REQUIRED PER M/M. RMVD AND REPL 4 RECIRC FAN. REPL 2 RECIRC FAN. OPS CK GOOD
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,808 hrs · 5,228 cycles
EMERGENCY LIGHT BATTERY 2 LOW MESSAGE IN COCKPIT DURING TEST. REPLACED BATTERY PACK.
Part: CONTROL CABLE — ICED (RT SPOILER) · airframe 41,420 hrs · 5,185 cycles
ON DESCENT WHILE ATTEMPING TO DEPLOY SPOILERS NO SPOILERS DEPLOYED ON RIGHT SIDE. ALSO DID NOT GET RIGHT SPOILERS ON GROUND AND WHEN PLACING FLAPS TO 15 DEGREES GOT ROLLING MOMENT AND FLAP ASYMMTRY LIGHT D305007004. FOUND LARGE AMOUNT OF ICE BUILDUP IN RIGHT FORWARD SECTION OF THE RIGHT WHEEL WELL CAUSING SPOILER CABLE OPERATION RESTRICTION. REMOVED ALL ICE VISUALLY CHECKED AND PERFORMED SATISFACTORY OPERATIONAL CHECK OF ALL FLIGHT CONTROLS PER M/M. CLOSED OFF WATER SHUTOFF VALVE LAV M - C/W SERVICE BULLETIN MD11-53-064.
Part: COMPRESSOR — OVERHEATED (GALLEY CHILLER) · airframe 41,065 hrs · 5,128 cycles
PRIOR TO DEPARTURE FWD GALLEY CHILLER COMPRESSOR MAKING VERY LOUD NOISE AND GETTING WARM HOT / SMOKE - REPLACED CHILLER.
Part: FUEL CONTROL — FAILED (AUTOPILOT) · airframe 40,816 hrs · 5,098 cycles
ON TAKE OFF AFTER PROF SELECTED AT 1000FT AGL AUTO THROTTLES RETARDED THROTTLES 1 AND 3 - REPLACED FCC 1
Part: HANDLE — MISLOCATED (L-1 DOOR) · airframe 40,549 hrs · 5,070 cycles
L1 DOOR OPEN CONTROL HANDLE FOUND WITH INSUFFUCIENT CLEARANCE TO CREW REST MODULE. MODIFIED STRUCTURE PER ERA 388450-14.
Part: FRAME — CUT (FUSELAGE) · airframe 39,890 hrs · 5,001 cycles
THE FS 1681 FRAME WAS CUT AT LONG 47R AND THE FRAME SECTION FROM FS 47R TO THE FACTORY SPLICE AT 47L. THE FRAME SECTION WAS REMOVED TO ALLOW ACCESS TO UNDERLYING STRUCTURE. THE FRAME WAS REINSTALLED WITH THE FACTORY SPLICE AT L-47L AND AN IDENTICAL SPLICE AT L-47R. THE REPAIR WAS ACCOMPLISHED PER ER/A 379699-14, REV A.
2000
Part: BATTERY — FAILED (CABIN) · airframe 39,404 hrs · 4,954 cycles
EMERGENCY LIGHT BATTERY 1 LOW DURING TEST. REPLACED BATTERY.
Part: LATCH — FAILED (OXYGEN DOOR) · airframe 38,606 hrs · 4,875 cycles
FIRST CLASS RT CTR STU SEAT OXYGEN DOOR DID NOT OPEN ON TEST. RESET LATCH MECHANISM ON FWD CABIN RIGHT CENTER ATTENDANT SEAT OXYGEN DOOR. CHECKS GOOD PER AMM 35-21-07-5.
Part: LATCH — STUCK (OXYGEN DOOR) · airframe 38,606 hrs · 4,875 cycles
L-2 STU SEAT OXYGEN DOOR DID NOT OPEN ON TEST. REPLACED LATCH MECHANISM ON L-2 FWD FLIGHT ATTENDANT SEAT OXYGEN DOOR. CHECKS GOOD PER AMM 35-21-07-5.
Part: SWITCH — OUT OF ADJ (NR 3 ENGINE) · airframe 38,385 hrs · 4,849 cycles
NR 3 U/L ILLUMINATED AIRBORNE STAYED ON UNTIL DESCENT FOR LANDING, EXTINGUISHED LAST 15 MIN OF FLIGHT. ADJUSTED STOW SWITCHES.
Part: CONNECTOR — DAMAGED (FUEL TANK) · airframe 38,208 hrs · 4,826 cycles
AIRCRAFT ARRIVED WITH MCO NR 007341002 TAIL LEFT PUMP OFF LIGHT ILLUMINATED IN FLIGHT (TRANSFER PUMP. FOUND RECEPTACLE IN PUMP HOUSING WITH BURNED PINS AND WIRING. THE RECEPTACLE SMELLED OF FUEL BUT NO EVIDENCE OF A FUEL LEAK WAS NOTED. REPLACED HOUSING P/N 60-845-2M, COMPANY P/N 280001331, S/N OFF: 3143A, S/N ON: 5043A.
Part: ENGINE — LEAKING (NR 1) · airframe 37,719 hrs · 4,773 cycles
AIR TURNBACK, NR 1 ENG OIL QTY DROPPED TO 9 ON T/O ATL. REPLACED ENGINE FOR INTERNAL OIL LEAK.
Part: FAN — OVERHEATED (AIR DISTRIBUTION) · airframe 37,695 hrs · 4,770 cycles
ELECTRICAL SMELL IN FRONT OF TOURIST SECTION TO BUSINESS GALLEY, STRONGER ON RIGHT SIDE. SMELL DISSIPATED WHEN CABIN BUS SWTCHED OFF. INSPECTED SIDEWALL LIGHTING CEILING AREA AND GALLEY. ALSO, CHECKED CARGO COMP, ALL OK. HOWEVER AT CEILING AREA FOUND NR 2 REC, FAN OVERHEATED. REPLACED FAN.
Part: POWER SUPPLY — FAILED (CABIN) · airframe 37,513 hrs · 4,750 cycles
ON PREFLIGHT, EMERGENCY LIGHT TEST FAILED. REPLACED NR 5 POWER SUPPLY
Part: BATTERY — DISCHARGED (COCKPIT) · airframe 36,789 hrs · 4,675 cycles
EMERGENCY LIGHTS COCKPIT TEST, FAILS BATTERY 2 LOW. REPLACED U1-206 BATTERY.
1999
Part: ENGINE — FAILED (NR 3)
NR 3 ENG SURGE ON T/O ROLL. T/O ABORTED. MTC FOUND METAL EQUIP SWAP WITH ACFT 803, ACFT 807 NR 3 ENG CHANGE.
Part: DRAIN VALVE — LEAKING (POTABLE WATER)
POTABLE WATER SUPPLY DECREASE FROM FULL TO EMPTY IN 4 HOURS. FOUND RT ELECT DRAIN VALVE LEAKING INTERNALLY. CAPPED LINE AND VALVE. CLEARED WATER AND ICE OUT OF AFT STAB COMP, DEFERRED REPLACEMENT OF VALVE.
Part: BATTERY PACK — DISCHARGED (CABIN)
EMERGENCY LIGHTS TEST SHOWS BAT 2. ALL LIGHT ILLUMINATED. REMOVED AND REPLACED NR 2 BATTERY PACK. EMERGENCY LIGHTS TEST PASS. ALL LIGHTS ILLUMINATED.
Part: BATTERY — DISCHARGED (CABIN)
DURING EMERGENCY LIGHT TEST, GOT NR 2 BAT LOW MESSAGE.
1998
Part: LIGHT — INOPERATIVE (CABIN)
EMERGENCY FLASHLIGHT WOULD NOT TEST. REPLACED FLASHLIGHT.
Part: LIGHT — INOPERATIVE (CABIN)
BAT 6 LOW LIGHTS DURING EMERGENCY LIGHTS TEST AFT SECTION EMERGENCY FLOOR LIGHTS AND SIGNS INOP. FOUND LT DOOR EMERGENCY LIGHT ASSY SHORTED TO GROUND L2-531. REPLACED LIGHT ASSY, OPN NORMAL.
1997
Part: SKIN — CORRODED (FUSELAGE)
RT FUSELAGE SKIN SURROUNDING THE FWD AND AFT LAVATORY VACUUM WASTE AIR EXHAUST PORTS WAS FOUND CORRODED ON THE OUTER SURFACE AROUND THE AFT EDGES OF THE PORT CUTOUTS. THE SUBJECT SKIN IS MADE FROM 0.068 2024-T3 AL CLAD MATERIAL WITH A LOCAL 0.060 THICKNESS. REPAIR WITH 0.071 2024-T3 CLAD DOUBLER; TWO INTERNAL FINGER DOUBLERS.
Part: LIGHT — INOPERATIVE (CABIN)
FLASHLIGHT AT 4R INOP. REPLACED BATT AND STRAP, OPS OK.
1995
Part: BULB — FAILED (CABIN)
FLT ATTENDANT CREW REST AND L2 RED EMERGENCY LT INOP. REPLACED BULB, OPN OK.
Part: BULB — FAILED (CABIN)
FLOOR TRACK EELS INOP, SEAT 35 AND 42 LEFT, 45 AND 39 RT. RELAMPED, OPN CKS OK.
Part: OIL SEAL — FAILED (NR 3 ENGINE)
AIR TURNBACK, OIL SMELL IN CABIN CAUSED BY NR 3 ENG. LOCKED OUT PRESSURE REGULATOR VALVE FWD TO MC OPER MEL 36-12-01. REPLACED COALESCER BAG, REPLACED NR 3 ENG PER ROUTINE CARD DECK, OPERATION NORMAL.