N103DA

Part: VALVE — INOPERATIVE (E/E BAY) · airframe 65,185 hrs · 31,789 cycles

ACFT WOULD NOT PRESSURIZE AFTER TAKEOFF. REPLACED FWD EQUIPMENT COOLING OVERBOARD EXHAUST VALVE.

Part: WIRE — CORRODED (NR 2 ENGINE) · airframe 65,081 hrs · 31,746 cycles

DURING HMV IN GSO FOUND NR 2 PYLON AND ENGINE WIRING CORRODED AT CANNON PLUGS. REPLACED WIRES AND PLUGS.

Part: WIRE — CORRODED (NR 1 ENGINE) · airframe 65,081 hrs · 31,746 cycles

DURING HMV IN GSO FOUND NR 1 PYLON AND ENGINE WIRING CORRODED AT CANNON PLUGS. REPLACED WIRING AND PLUGS.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 64,488 hrs · 31,437 cycles

MID LEFT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER, OPS GOOD.

Part: WEDGE — DEBONDED (L/E SLAT) · airframe 63,721 hrs · 31,019 cycles

RIGHT WING SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 422819-14.

Part: COUPLING — LEAKING (BLEED AIR SYS) · airframe 63,070 hrs · 30,706 cycles

LEFT DUCT LEAK ON CLIMBOUT. RESEALED COUPLING ON BODY CROSSOVER DUCT IN LEFT AC BAY. RAN TO TAKEOFF POWER PER PFHB. OK FOR SERVICE.

Part: ENGINE — FAILED (#1 ENGINE) · airframe 62,916 hrs · 30,632 cycles

LEFT ENG SURGE IN FLIGHT AND ON LANDING. ENG SHUT ITSELF DOWN ON LANDING AT 5 THOUSAND FT. ENG CHANGE IS IN WORK

Part: PANEL — UNRELIABLE (NBR 1) · airframe 61,203 hrs · 29,811 cycles

CAPTAINS VHF FREQUENCY SELECT PANEL LEFT DISPLAY 4TH DIGIT CHANGED_WITHOUT INPUT. 118.97 SWITCHED BACK AND FORTH TO 118.17 CA RPLD PANEL, OP CKS GD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 61,105 hrs · 29,751 cycles

COCKPIT PORTABLE EMERGENCY LIGHT WILL NOT ILLUM. REPLACED SAME.

Part: TARGET — OUT OF ADJ (L/E SLAT) · airframe 59,888 hrs · 29,070 cycles

ON T/O, LEADING EDGE LIGHT FLICKERED AND STICK SHAKER AFTER T/O LIGHT CAME ON STBY FLAPS WERE RETRACTED BUT STUCK BETWEEN UP AND 1 HAD ASSOCIATED L/E SLAT ASYM EICAS MSG. FOUND TARGETS ON SLATS NUMBER 2 AND 7 OUT OF ADJUSTMENT. ADJUSTED TARGETS AND PERFORMED BITE TEST OF PSEU. NO FAULTS NOTED.

Part: SKIN — DELAMINATED (SPOILER) · airframe 59,876 hrs · 29,064 cycles

DELAMINATION TO THE UPPER SKIN OF THE SPOILER. REPAIRED PER ER/A 410579-14.

Part: FUEL LINE — CRACKED (NR 2 ENGINE) · airframe 59,443 hrs · 28,819 cycles

FLUID LEAKING FROM RIGHT ENGINE ON PUSHBACK AFTER START. T/S LEAK PER M/M FOUND FUEL TUBE ON FUEL NOZZLE FEEDER MANIFOLD AT 5'OCLOCK POSITION CRACKED. REPLACED SAME, RAN ENG PERPFHB, LEAK CKS GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,376 hrs · 28,782 cycles

INSPECTION OF THE FS 1809.5 OUTER CHORDS PER AD 2001-09-13 AND BAC S/B 767-53-0078 REVEALED CRACKS EMANATING FROM TWO FASTENER HOLES IN THE RT FWD CHORD AND ONE HOLE IN THE RT AFT CHORD. THE AFT CHORD WAS COMPLETELY REPLACED AND THE UPPER SECTION OF THE FWD CHORD WAS REMOVED AND A NEW SECTION SPLICE IN PER THE S/B INSTRUCTIONS. THE REPAIRS WERE DOCUMENTED PER ER/A 381425-14AD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 58,725 hrs · 28,477 cycles

LEFT OVERWING EXTERIOR EMERGENCY LIGHTING INOP. REMOVED AND REPLACED POWER SUPPLY AND BATTERY ASSEMBLY PER M/M.

Part: BATTERY — DISCHARGED (CABIN) · airframe 58,725 hrs · 28,477 cycles

LEFT OVERWING EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY AND BATTERY ASSEMBLY PER M/M.

Part: ENGINE — LEAKING (NR 2) · airframe 57,125 hrs · 27,815 cycles

SMOKE IN CABIN SOURCE UNKNOWN SMOKE CLEARED AFTER PERFORMINGSMOKE AND FUME REMOVAL CHK LIST._HAPPENED AT FL370 DESCENDED TO FL230 ALSO SMOKE ALARM IN MID LAV WENT OFF. FLL MTC WAS SENT TO INVESTIGATE AFTER CONTRACT MTC WAS UNABLE TO DUPLICATE PROBLEM WITH RUNNING ENGS. CREW DID MAKE NOTE SMELL WAS OF OIL NATURE..FLL MTC DISCOVERED NOSE BLEED R ENG THEY ISOLATED BLEED AIR FROM R ENG AND A/C WAS MTC FERRIED TO ATL FOR ENG CHANGE

Part: SKIN — CORRODED (CENTER WING) · airframe 56,971 hrs · 27,746 cycles

CORROSION FOUND ON CENTER SECTION WING SKIN. THE DAMAGE WAS ON THE OUTER SURFACE OF THE UPPER SKIN AT STRINGER U-17 AT LBL 88. ER/A 334963-14 REPAIRED DAMAGE.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 56,971 hrs · 27,746 cycles

CORROSION FOUND ON THE RT MLG WHEEL WELL CANTED PRESSURE WEB. CORROSION LOCATED AT STA 960 BETWEEN RBL 85 AND RBL 90. ER/A 334987-14 REMOVED CORROSION.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,971 hrs · 27,746 cycles

GROUND DAMAGE AT STA 1250 STR 30R. SKIN AND STRINGER DENTED LOCALLY. SKIN AND STRINGER ARE TRIMMED OUT AND REPAIRED. ER/A 369288-14 REV A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,971 hrs · 27,746 cycles

CORROSION WAS FOUND ON THE FUSELAGE SKIN AT THE FOLLOWING LOCATIONS; FS 1175 AND S-39L, FS 1197 AND S-39L, AND FS 1197AND S-39R. THE CORROSION WAS CUT OUT AND EXTERNAL REPAIR DOUBLERS AND TRIPLERS WERE INSTALLED PER ERA 334950-14 AT MV2.

Part: SKIN — GOUGED (PAX DOOR) · airframe 56,971 hrs · 27,746 cycles

OUTER SKIN OF THE L-1 DOOR HAS BEEN GOUGED. REPAIR PER ER/A 388030-14.

Part: VALVE — MALFUNCTIONED (A/C BAY) · airframe 56,537 hrs · 27,559 cycles

AT FL350 WITH RT PACK ON GOT CABIN ALT EICAS MSG. TURNED LT PACK ON AND DID EMER DESCENT AND DIVERTED TO MEM. RT PACK TESTED GOOD. LT PACK VALVE INDICATION ON PREVIOUS DEFERRAL. REPLACED VALVE.

Part: IDG — REQUIRED SERVICE (NR 2 ENGINE)

RT GEN FIELD TRIPPED ON T/O ROLL, ABORTED T/O AT 80 KNOTS. RAN NR 2 ENG, DISCONNECTED RT IDG. VERIFIED NO VOLTS AND FREQS. SERVICED IDG WITH OIL.

Part: LIGHT — DAMAGED (CABIN)

EMERGENCY TRACK LIGHTING DAMAGED BY 2L DOOR. INSPECTED ALL EMERGENCY TRACK LIGHTING, REPAIRED DAMAGE, CKS OK.

Part: ENGINE — FAILED (NR 1)

AS POWER CAME UP FROM IDLE A BANG WAS HEARD AND LT ENG REMAINED AT IDLE PWR. NO CONTROL OF LEFT ENG FROM COCKPIT. NO ENG EXCEEDANCE NOTED AND NO INDICATIONS IN COCKPIT OF ENG FAILURE. ENG WAS NOT SHUTDOWN FOR EMERG LANDING AT JFK. FOUND METAL IN TAILPIPE. ENG REPLACED.

Part: PRESSURE DECK — CRACKED (BS 977)

THE WHEEL WELL PRESSURE DECK WAS FOUND WITH A CRACK AT 977 ON THE LEFT HAND SIDE AT LBL 35, THE CRACK IS 12 INCHES LONG. THE CRACK WAS REPAIRED PER 767-200 SRM 53-50-51 FIG 202 AND ERA 363828-14. AN EIGHT INCH CRACK WAS ALSO FOUND ON THE RIGHT HAND SIDE AT RBL 24.5. IT WAS REPAIRED PER SRM 53-50-51-2-204. REPAIRS WERE MADE ON NR CARDS 1, 2 AND 6.

Part: TE WEDGE — DELAMINATED (NR 5 TE SLAT)

THE NR 5 SLAT TRAILING EDGE WEDGE UPPER SURFACE WAS FOUND DELAMINATED ON THE AFT INBOARD CORNER. THE DELAMINATION IS APPROX 3 BY 3.5. THIS AREA WAS REPAIRED PER B767-200 SRM 51-70-10, FIGURE 9.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FWD PART OF AFT CABIN EMERGENCY PATH LIGHTING INOP DURING L/O. REPAIRED SHORTED WIRES AT SIDEWALL 35FG AND REPLACED M9009 BATTERY MODULE.

Part: BATTERY PACK — DISCHARGED (CABIN)

FOUND ON L/O, AFT THREE EXTERIOR EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY M738 AND BATTERY PACK, LIGHT OPS NORMAL.

Part: COFFEEMAKER — FAILED (AFT GALLEY)

SMOKE IN REAR GALLEY REPORTED COMING FROM AIR VENT. INSPECTED AFT GALLEY AREA AND ABOVE CEILING AREA FOR EVIDENCE OF BURNING OR SMELL, NONE FOUND AND ALL WIRING OK. REMOVED NR 3 AND NR 4 COFFEEMAKERS AND INSPECTED WIRING HARNESS FOR CONDITION, ALL OK, SLIGHT ACRID ODOR FROM COFFEEMAKERS. REPLACED NR 3 AND NR 4, ALL OK FOR SERVICE.

Part: RETRACT MECH — MALFUNCTIONED (RT MLG)

AIRCRAFT'S ATB RIGHT MLG WOULD NOT RETRACT. PRESSURE GOOD. JACKED AIRCRAFT, CYCLED GEAR SERVERAL TIMES PER MM. CHECKS NORMAL. TILTED TRUCK, TURNED ON HYDRAULIC, TRUCK TILTED NORMAL. RETURNED TO SERVICE.

Part: SPRING — BROKEN (AILERON DRUM)

ON TAXI OUT, CHECKING CONTROLS F/O SIDE AILERONS EXTREMELY STIFF, VERY DIFFICULT TO MOVE. AFTER INSPECTION FOUND SPRING (P/N 69881284-2), BROKEN ON F/O AILERON DRUM ASSY (P/N 253T1142-3).

Part: POWER SUPPLY — FAULTY (RT OVERWING)

DURING LAYOVER, RIGHT SIDE OVERWING EMERGENCY ESCAPE SLIDE SQUIB TEST 2 INOP. REPLACED RIGHT SQUIB POWER SUPPLY TEST NORMAL.