N707DN
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.
27 reports on file, 2010-01-02 – 2019-04-18.
Part: LENS — CRACKED (CABIN) · airframe 51,041 hrs · 4,608 cycles
(AIRCRAFT 7107; L/P 1035671) MIDLIFE MOD- PROXIMITY EMER LT LENS ASSY FOUND CRACKED AT EXTERIOR OF OFCR AND OFAR. OFCR AND OFAR PROXIMITY LIGHT REPLACED AND OPS CHECK SA PER AMM 33-51-05 AND FOUND SATISFACTORY.
Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 50,872 hrs · 4,589 cycles
EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / INTERIOR. INSTALLED LENS OK FOR SVC.
Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 50,872 hrs · 4,589 cycles
EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / INTERIOR. INSTALLED LENS. OK FOR SVC.
Part: LENS — DAMAGED (CABIN) · airframe 50,872 hrs · 4,589 cycles
(AIRCRAFT 7107, L/P 0995030) EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. INSTALLED LENS OK FOR SVC.
Earlier reports · 2010–2018 · 23 reports
2018
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 48,353 hrs · 4,376 cycles
EMERGENCY LIGHT LENS WAS MISSING ALONG THE R1 AND GALLEY. INSTALLED THE LENS.
Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 48,247 hrs · 4,367 cycles
CABIN EMERGENCY LIGHTS INOPERATIVE ON SIDE OF SEATS 2C, 4C, 5C, 10B, AND THE CEILING EMERGENCY LIGHT AT SEAT 45G. CONNECTED LIGHT AT CEILING PANEL AT SEAT 45G. OP CHECKED GOOD.
Part: OVEN — ODOR (GALLEY) · airframe 47,075 hrs · 4,273 cycles
F/A SMELLED SOME SMOKE FROM R1 GALLEY. OVEN LOC F205 SECURED OVEN AND REMOVED FOOD. SMELL THEN DISSIPATED W/ MCC CONCURRENCE F/A'S PULLED C/B FOR THE OVEN. A/C SMOKE & FUMES QUESTIONNAIRE COMPLETED.
Part: OVEN — ODOR (GALLEY) · airframe 47,075 hrs · 4,273 cycles
FA SMELLED SMOKE FROM THE OTHER OVEN IN GALLEY 1. TURNED OVEN OFF AND PULLED CIRCUIT BREAKERS PER MAINTENANCE. THIS LOC IS 204. PRECAUTIONARY REPLACED OVEN PER AMM 25-31.
2017
Part: FAN — FAILED (RECIRCULATION) · airframe 44,492 hrs · 4,059 cycles
RECIRCULATION FAN STATUS MESSAGE. ASSOCIATED WITH SLIGHT ELECTRICAL ODOR IN CABIN. TURNED FANS OFF, ODOR WENT AWAY. REMOVED AND REPLACED THE LEFT LOWER RECIRCULATION FAN IAW AMM 21-25-07, OPS TESTED OK. OBSERVED FOR AN HOUR OF OPERATION AND FOUND NORMAL. ACFT OK FOR SERVICE.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,336 hrs · 4,041 cycles
FIRST CLASS EMERG LIGHTS INOP. FOUND BATTERY PACK INOP REPLACED IAW AMM 33-55,CK NORMAL.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 42,362 hrs · 3,872 cycles
EMERGENCY EXIT COVER DIFFUSE LENS MISSING. REPLACED EMERGENCY LIGHT LENS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,025 hrs · 3,839 cycles
EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:405. FOUND SEAT 6B FLOOR LIGHTING INOP. REPLACED BULB.
Part: COVER — UNKNOWN (CABIN) · airframe 42,025 hrs · 3,839 cycles
EMERGENCY SEAT MOUNTED LIGHTING DAMAGED/INOP, LOCATIONS:10B. INSTALLED MISSING COVER CKS OK.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,025 hrs · 3,839 cycles
EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:901. ADJUSTED BULB. OPS CHK NML. OK FOR SVC.
Part: LIGHT — OUT OF ADJUST (CABIN) · airframe 42,025 hrs · 3,839 cycles
EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:702. ADJUSTED BULB. OPS CHK NML. OK FOR SVC.
Part: RESERVOIR — DEFECTIVE (L2 DOOR) · airframe 41,014 hrs · 3,744 cycles
CABIN L2 DOOR EPAS PRESSURE GAUGE FOUND FAULTY. CABIN L2 DOOR EPAS RESERVOIR REMOVED AND REPLACED AS PER AMM 52-11-22.
Part: STIFFENER — DAMAGED (LT NACELLE) · airframe 41,014 hrs · 3,744 cycles
DURING ACCOMPLISHMENT OF CONDUCTIVITY TEST ON LT PYLON AFT FAIRING LOWER SPAR WEB AND SUPPORT STRUCTURE, FOUND THREE STIFFENERS CONDUCTIVITY VALUE NOT WITHIN ACCEPTABLE RANGE. LT PYLON AFT FAIRING LOWER TEES WERE REMOVED AND REPLACED IAW SRM 51-40-02.
Part: COVER — CHAFED (HEATSHIELD PAN) · airframe 41,014 hrs · 3,744 cycles
LEFT STRUT AFT FAIRING HEATSHIELD PAN NR 1 GAP COVER STRIP FOUND CHAFED. THE PAN COVER STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02.
Part: COVER — CHAFED (LT NACELLE) · airframe 41,014 hrs · 3,744 cycles
LEFT STRUT AFT FAIRING HEATSHIELD PAN NR 3 GAP COVER STRIP FOUND CHAFED. THE COVER STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02.
Part: COVER — CHAFED (HEATSHIELD PAN) · airframe 41,014 hrs · 3,744 cycles
LEFT STRUT AFT FAIRING HEATSHIELD PAN NR 2 GAP COVER STRIP FOUND CHAFED. THE PAN #2 GAP COVER WAS REMOVED AND REPLACED IAW SRM 51-40-02.
Part: STRUCTURE — DAMAGED (L1 DOOR) · airframe 41,014 hrs · 3,744 cycles
LOWER AFT RIGHT CORNER OF THE L1 DOOR FOUND DEFORMED AND BENT. REPAIRED IAW ER/A 552727-14 PRI REV O.
2016
Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,121 hrs · 3,660 cycles
RED EMERGENCY LIGHT BY CREW REST DOOR INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW WDM 33-51-57 AND WSPM 20-30-12.
2015
Part: RELAY — FAILED · airframe 29,757 hrs · 2,745 cycles
TURNING TO FINAL AT APPROXIMATELY 3000 FT, ACFT APPEARED TO HAVE A COMPLETE LOSS OF POWER, NO LAND 3 APPEARED, SMOKED DETECTORS SOUNDED WITH NO SMOKE AND UNABLE TO RESET. MAINTENANCE MESSAGE 24-12126 LATCHED IN THE MATERIAL. REPLACED RELAY K24201 AND CARD M24509.
2014
Part: FIRE WARNING — ACTIVATED · airframe 26,582 hrs · 2,462 cycles
DURING APPROACH, CABIN FIRE ALARMS STARTED CHIMING WITH NO INDICATIONS OF WHERE ALARM WAS COMING FROM. F/A'S REPORT FAINT ELECTRICAL ODOR. PERFORMED SMOKE IN CABIN INSPECTION WITH NO ODOR OF ELECTRICAL COMPONENTS AND NO ELECTRICAL MALFUNCTIONS NOTED.
2011
Part: SKIN — DAMAGED (FUSELAGE) · airframe 12,395 hrs · 1,103 cycles
FUSELAGE SKIN/ STA 1802, BELOW LAP JOINT AT STR 34R/ GOUGE AND DENT REF NR 2 AT PSV. REPAIRED PER PRI 488564-14 REV 4.
Part: FUSE — BLOWN (CABIN) · airframe 9,803 hrs · 871 cycles
DURING A MAINTENANCE VISIT, THE EMERGENCY LIGHTS IN SECTION AFT OF 2R AND L2 DOOR WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE FUSE BLOWN ON THE BATTERY CHARGER AND REPLACED IT. SYSTEM OPERATION WAS NORMAL AFTER THE FUSE WAS REPLACED.
2010
Part: ANTI-ICE SYSTEM — MALFUNCTIONED (NR 1 ENGINE) · airframe 3,343 hrs · 302 cycles
ANTI-ICE ENG LT- UNABLE TO RESET IAW QRH. DISCONNECTED LT EAI CONTROLLER AND RAN ENGINE. LT EAI INDICATION RETURNED. FWD TO MCO/PLAC. IAW MEL 30-21-01D. OK FOR SERVICE ETOPS CATEGORY 'E': PROBLEMS WITH SYS CRITICAL TO ETOPS.