N111DN
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
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.
13 reports on file, 1995-05-15 – 2004-08-24.
Part: FAN — UNSERVICEABLE (LEFT) · airframe 65,152 hrs · 31,188 cycles
ELECTRICAL ODOR IN COCKPIT ON 3 SEPARATE OCASSIONS, IT WAS ALSO SMELLED THROUGHOUT CABIN LASTING ONLY A FEW MINUTES THEN DISSIPATING. INSTRUCTED F/A TO TURN OFF CHILLERS AT FIRST OCCURRENCE AND IT CLEARED THEN IT RETURNED 2 MORE TIMES. FOUND LT RECIRC FAN TO BE AT FAULT (NOISY). REPLACED SAME.
Earlier reports · 1995–2001 · 12 reports
2001
Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 57,169 hrs · 27,081 cycles
LEFT AFT CEILING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY. CHECKS GOOD.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,121 hrs · 27,057 cycles
THE 2L EXTERIOR EMERGENCY LIGHT INOP. RELAMPED, CHECKS OK.
1999
Part: ACTUATOR — CRACKED (MLG)
A LOUD THUMP HEARD ON GEAR RETRACTION. AFTER GEAR WAS PUT TO THE DOWN POS THE LEFT GEAR GREEN LIGHTS WERE NOT ON AND HAD A GEAR DISAGREE AND DOORS DISAGREE LIGHTS. CREW LANDED UNEVENTFUL. MTC FOUND THE LT GEAR SIDE BRACE CRACKED AND THE BRACE BEYOND OVER CENTER. ALSO, FOUND MAIN LANDING GEAR ACTUATOR ROD SHEARED AT GEAR SIDE. REPLACED AFFECTED COMPONENTS.
1998
Part: SWITCH — FAILED (LT MLG)
LEFT MAIN GEAR INDICATED UNSAFE WHEN LOWERED. POM WAS FOLLOWED, HOWEVER GEAR STILL INDICATED UNSAFE HYD. QUANTITY AND PRESSURES WERE NORMAL. REPLACED LANDING GEAR LEVER AND SWICTHES AS PROXIMITY BOX. FAULTED SWITCH 421 AND 422. ALSO, REPLACED LEFT GEAR. INDICATOR LAMPS.
Part: BATTERY PACK — DISCHARGED (CABIN)
L1 SLIDE LIGHT INOP, ALSO BOTH LT OVERWING SLIDE LIGHTS INOP. REPLACED BOTH BATTERIES.
1997
Part: TE WEDGE — DELAMINATION (NR 8 TE SLAT)
THE NR 8 SLAT WAS FOUND TO HAVE THE TRAILING EDGE WEDGE UPPER SKIN DELAMINATED. THE DELAMINATION IS A 1 DIA CIRCLE, APPROX. 4 FROM THE AFT EDGE OF THE TRAILING EDGE WEDGE AND 3 O/B OF THE I/B END. THE TRAILING EDGE WEDGE IS MANUFACTURED WITH 0.016 5052-H38 FACE SHEETS WITH A METALLIC HONEYCOMB CORE PER BMS 4-6, TYPE 4.1-25. ACCOMPLISH A COIN TAP TEST PER FIG. 2 OF S.I. 1-65079-12AD; REPAIR DELAMINATED AREA PER THE B767-200 SRM, CHAP 57-43-02, FIG. 201.
Part: CONTROLER — FAILED (CABIN)
AIR RETURN, UNABLE TO PRESSURIZE CABIN. TROUBLE SHOOTING IN PROGRESS. REPLACED EQUIPMENT COOLING SYSTEM CONTROLLER. SYSTEM CHECKS NORMAL.
1996
Part: PRESS SYST — MALFUNCTIONED (CABIN)
AIRCRAFT WOULD NOT PRESSURIZE ON CLIMBOUT. INSPECTED AIRCRAFT ON ARRIVAL, NO DOORS OR SERVICE DOORS OPEN. FOUND EQUIPMENT COOLING VALVES OPEN, RESEQUENCED EQUIPMENT COOLING VALVES AND LOCKED OUT PER MEL 21-58-06. AIRCRAFT PRESSURIZED NORMALLY.
1995
Part: OVEN — OVERHEATED (AFT GALLEY)
UPPER RT SIDE AFT GALLEY OVEN OVERHEATED AND BEGAN TO SMOKE. FOUND THERMOSTAT FAULTY. SET UP FOR OVEN REPLACEDMENT AND FWD TO MCO.
Part: EEL POWER SUPPLY — INOPERATIVE (CABIN)
BATTERY PACK DOES NOT HOLD CHARGE FOR EMERGENCY LIGHTS. REPLACED POWER SUPPLY BATTERY, SYSTEM OPS CHECKS NORMAL. POWER SUPPLY (P/N BPS7-3)(S/N 5449), BATTERY (P/N 2013-1A) (S/N 1851).
Part: THRUST REVERSER — DELAMINATION (NR 1 ENGINE)
NUMBER ONE ENGINE LEFT THRUST REVERSER ASSEMBLY INNER WALL HAD EXISTING SRM REPAIRS AND ADDITIONAL DELAMINATION. ALSO, UPPER BEAM HAD EXISTING SRM REPAIR AND ADDITIONAL DELAMINATION. COMPONENT WAS REPAIRED PER ER/A 276777-14. REPAIR CONSISTED OF REPLACING FACE SHEETS AND REBONDING. RETURNED TO SERVICE 11-10-95.
Part: COWL — CRACKED (NR 1 ENGINE)
FOUND LWR CHANNEL, AFT END OF CORE COWL TO BE CRACKED. REPAIRED PER SRM 54-41-02 PG 217. FOUND AND REPAIRED AT SHOP INSPECTION.