N116DL

Part: SKIN — DELAMINATED (LT AILERON) · airframe 53,236 hrs · 25,884 cycles

DELAMINATED SPOT ON LEFT OUTBOARD AILERON. REPAIRED AILERON.

Part: SKIN — DEBONDED (RT WING TE FLAP) · airframe 52,530 hrs · 25,519 cycles

RIGHT INBOARD AFT FLAP DISBONDED. REPAIRED PER ER/A 418200-14.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 51,046 hrs · 24,789 cycles

CRACKS WERE FOUND IN THE LBL 10 VERTICAL STIFFENER OF THE CENTER SECTION FRONT SPAR, IN THE WEB OF THE STIFFENER AT THE OVERWING FLOORBEAM TO STIFFENER JOINT. A SPLICE REPAIR WAS ACCOMPLISHED.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 50,510 hrs · 24,550 cycles

SEAT ROW 40 AB EMERGENCY LIGHT INOP. FOUND DURING L/O CK. FOUND WIRE PULLED OUT OF CONNECTOR. REINSERTED PIN IN CONNECTOR OPS CK NML. L2 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED OPS CK GOOD.

Part: FLANGE — DELAMINATED (SPOILER) · airframe 49,929 hrs · 24,282 cycles

THE OUTBOARD SPOILER WAS FOUND WITH DELAMINATION ON THE SPAR UPPER FLANGE. REPAIR PER ER/A 411065-14.

Part: SKIN — DEBONDED (T/E FLAP) · airframe 49,929 hrs · 24,282 cycles

WING INBOARD AFT FLAP WAS FOUND WITH THE UPPER SKIN DISBONDED AT THE INBOARD END. REPAIR PER ER/A 411072-14.

Part: SKIN — DAMAGED (SPOILER) · airframe 48,799 hrs · 23,739 cycles

THE RT WING, INBOARD SPOILER UPPER AND LOWER SKINS WERE FOUND DAMAGED DURING OVERHAUL AT NORDAM. REPAIR PER ER/A 410639-14.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 48,344 hrs · 23,518 cycles

COCKPIT EMERGENCY LIGHT FAILS TO TEST. REPLACED LIGHT ASSEMBLY AND BATTERIES, EMERGENCY LIGHTS NORMAL NOW.

Part: ACTUATOR — DEFECTIVE (RT MLG) · airframe 48,097 hrs · 23,410 cycles

ON TAKEOFF AFTER GEAR HANDLE RAISED DOOR GEAR LIGHTS REMAINED ILLUMINATED EICS MESSAGE GEAR DISAGREE AND GEAR DOORS WITH HANDLE IN OFF POSITION GREEN RT MAIN LIGHT ON. MAINTENANCE IN PROGRESS. REMOVED AND REPLACED DRAG BRACE ACTUATOR ON THE RIGHT GEAR. C/W LEAK AND OPERATIONAL CK ALL OK PER MM 32-32-02--4-01.

Part: ENGINE — OVERTEMP (NR 2) · airframe 47,959 hrs · 23,349 cycles

RT ENG OVERTEMP ON T/O. EGT943 T/O DISCONTINUED AT 90K. CHECKED INLET AND EXH, RAN ENG PER PFHB MAX PWR ASSURANCE TEST. CLEARED EICAS COMPUTER, MSG 943 FOR 3 SEC OVERTEMP AREA A-MCC ADVISED.

Part: LINE — LEAKING (NR 1 ENGINE) · airframe 47,483 hrs · 23,133 cycles

LT ENG GEN DRIVE LIGHT CAME ON DURING T/O ROLL. DISCONTINUED T/O AT APPROX 90 KNOTS GROSS WGT 295000. FOUND OIL LINE FROM IDG FILTER TO OIL COOLER LEAKING. REPLACED SAME. MOTORED ENG LEAK CKS OK. RAN ENG IDG. OPERATION AND INDICATION NORMAL.

Part: HARNESS — SHORTED (ELECTRICAL) · airframe 44,580 hrs · 21,752 cycles

FIRE DAMAGE IN THE E/E FEEDER CABLES BEHIND THE P37 PANEL,SHORTED. WIRE BUNDLE W298 SHORTED AT STATION 317 DAMAGING STRINGER 317 AND SCORCHED FUSELAGE SKIN. USED DRY CHEMICAL AGENT TO EXTUNGUISH FIRE. EVENT OCCURRED AT APPROXIMATELY 2350/01. - DURING MTC - REPAIRED ALL DISCREPANT ITEMS

Part: COMPRESSOR — DAMAGED (NR 2 ENGINE)

ON ARRIVAL FLT 1814 BOS, FOUND FOD DAMAGE TO MULTIPLE FAN BLADES AND ACCOUSTICAL LINER. REPLACED FAN.

Part: FITTING — CORROSION (NR 1 PYLON)

I/B LUG OF THE NR 1 ENGINE PYLON MIDSPAR O/B FITTING FOUND WITH CORROSION AND WEAR DAMAGE. DAMAGE FOUND ON FACE OF LUG AND IN BORE, ERA 333570-14 REV A.

Part: FITTING — CORRODED (RT WING)

RT WING, I/B UNDERWING SIDE LOAD FITTING WAS FOUND WITH CORROSION DAMAGE IN THE BORE. REPAIR PER ER/A 333555-14 REV A.

Part: SKIN — DENTED (BS 465)

DENT IN FUSELAGE SKIN AT STA 465 ABOVE STRINGER 34R. STRINGER DAMAGED AT THIS LOCATION ALSO. REPAIR SKIN AND STRINGER PER ER/A 333462-14, REV A.

Part: BATTERY — DISCHARGED (CABIN)

JUST PRIOR TO DEPARTURE F/A ADVISE MTC, THE MID RT EMERGENCY FLASH LIGHT HAD LOW BATTERIES. MAINTENANCE REPLACED THE BATTERY AND BULB ASSY AND INSTALLED PLACARD, P/N257204896 BULB P/N 012211663.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY EXIT IDENTIFIER LIGHTS AT L-2 AND R-2 INOP. REPLACED POWER SUPPLY, SYSTEM OPS GOOD.

Part: SKIN — DELAMINATED (NR 2/4 LE SLAT)

THE NR 2 LEADING EDGE SLAT WAS FOUND WITH A 5 DIA DELAMINATION ON THE UPPER SKIN OF THE TRAILING EDGE WEDGE. THE NR 4 SLAT WAS FOUND WITH A 7 DIA DELAMINATION ON THE UPPER SKIN OF THE TRAILING EDGE WEDGE. BOTH DELAMINATIONS WERE REPAIRED PER THE B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364089-14AD.

Part: SKIN — DELAMINATED (NR 6 LE SLAT)

THE NR 6 SLAT TRAILING EDGE WEDGE UPPER SURFACE WAS FOUND DELAMINATED. THE DELAMINATION IS LOCATED 10 FROM THE AFT EDGE EDGE, 82 FROM THE INBOARD END AND IS APPROX 3 IN DIAMETER. THE DELAMINATED AREA WAS REPAIRED PER B767 SRM, CHAPT 51-70-10, FIGURE 9.

Part: INTERCOSTAL — CRACKED (BS 560)

DRIVE MOTOR SUPPORT/BAG BIN FLOOR SUPPORT CRACKED AT FS 560 P/N 451T2503-2. REPLACED INTERCOSTAL PER SRM 51-70-13-0-1.

Part: BY PASS VALVE — BROKEN (RT PACK)

ON CLIMBOUT, GOT A RT DUCT LEAK LIGHT AND ASSOCIATED EICAS MSG AFTER ISOLATION PROCEDURE WAS DONE, LIGHT REMAINED ON AND RT PACK STAYED ON. FOUND RT ISOLATION BYPASS VALVE BROKEN. REPLACED SAME. REPLACED SEALS ON SLIP JOINT OUTBOARD OF RT ISOLATION CHECK VALVE.

Part: COOLING FAN — FAILED (COCKPIT)

ELECTRICAL WIRING SMELL NOTICED IN COCKPIT AT 1,000 FT AGL ON APPROACH. SMELL INCREASED THROUGH LANDING. REPLACED EXHAUST RACK COOLING FAN FOR POPPING C/B, EQUIP COOLING NOW CHKS OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

NO SQUIB TEST ON EMERGENCY ESCAPE SLIDE/SPOILER. REPLACED M391 POWER SUPPLY AND BATTERY PACK OPERATION NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

NO SQUIB TEST ON EMERGENCY ESCAPE SLIDE/SPOILER. BATTERY PACK LOW VOLTS FROM MODULE 961, REPLACED SAME.

Part: ACTUATOR — FAILED (LT MLG)

FAILURE OF LEFT MLG TO RETRACT AFTER T/O. FOUND LEFT MLG DRAG BRACE ACTUATOR FAILED INTERNALLY, PISTON FELL OUT OF ACT BODY UPON REMOVAL. REPLACED ACTUATOR, OPERATION NORMAL.

Part: PITOT TUBE — CONTAMINATED (LEFT)

ABORTED TAKEOFF DUE TO NO AIRSPEED IND ON CAPTS A/S INDICATOR. AIRSPEED 105 KTS, GROSS WT 285, TEMP 60 DEGREES. BLEW DEBRIS OUT OF CAPTS PITOT TUBE. REPLACED PITOT TUBE, PRECAUTION BLEW PITOT AND STATIC LINE FROM ADC TO PITOT TUBE CONNECTORS. PUMPED A/C TO MAX AIRSPEED AND ALT - ALL CKS NORMAL.

Part: EEL LAMPS — FAILED (CABIN)

ON LAYOVER, FOUND PATH LIGHTS OUT AT SEATS 11AB, 38AB. REPLACED LAMPS, BOTH LIGHTS CK NORMAL.

Part: FAN — SHORTED (AC BAY)

DURING CRUISE, FLIGHT ATTENDANT REPORTED BURNING SMELL FROM OVERHEAD GASPER FAN VENTS. DEACTIVATED FAN, ODOR STOPPED. REPLACED GASPER FAN OPERATION NORMAL.