N101DA

Part: BOLT — MISINSTALLED (RT MLG) · airframe 67,674 hrs · 32,885 cycles

FOUND BY FAA INSPECTOR, RIGHT MLG WING DOOR LOWER AFT MOUNT BOLT INSTALLED INCORRECTLY. BOLT IS DAMAGED AND CENTER SHIMS ARE MISSING. INSTALLED NEW BOLT AND HARDWARE PER AMM 32-12-06 AND IPC32-12-01-05 RIGHT MLG WING DOOR LOWER AFT MOUNT INSTALLATIONS NOW CORRECT OK FOR SERVICE.

Part: LAP JOINT — CRACKED (PRESS BULKHEAD) · airframe 65,175 hrs · 31,759 cycles

DURING INSPECTION OF THE AFT P-DOME AT FS 1582 A CRACK WAS FOUND AT A FASTENER COMMON TO THE STIFFENER 5L WEB LAP JOINT. THE CRACK WAS REMOVED BY TRIMMING OUT THE LAP JOINT. THE CUTOUT WAS REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 088021-14AD.

Part: PANEL — CRACKED (PRESS BULKHEAD) · airframe 65,175 hrs · 31,759 cycles

INSPECTION OF THE AFT P-DOME GORE PANELS PER AD 88-19-03 REVEALED A CRACK AT A FASTENER LOCATION COMMON TO THE STIFFENER 13R LAP JOINT. THE CRACK WAS REMOVED WITH A CUTOUT TO THE GORE PANEL AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 088005-14AD.

Part: PANEL — GOUGED (PRESS BULKHEAD) · airframe 65,175 hrs · 31,759 cycles

THE GORE PANEL ON THE AFT P-DOME WAS FOUND WITH A GOUGE NEAR STIFFENER 11R. THE GOUGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 087997-14AD.

Part: WIRE HARNESS — CHAFED (CABIN) · airframe 64,151 hrs · 31,256 cycles

FOUND LEFT AFT CHILLER WIRE HARNESS BURNT THROUGH DUE CHAFFING ON CHILLER RACK FRAME. SECURED HARNESS ASSY AND PULLED C/B'S. VERIFIED NO POWER TO HARNESS ASSY. WILL NEED WIRE HARNESS W284 REF IPC 25-33-02-01. ALSO WILL NEED DISCONNECT D2650DPN 014206555. TMC NOTIFIED FOR POSSIBLE ENGINEERING REROUTING/REPAIR OF HARNESS. FWD TO MCO.

Part: SKIN — DENTED (FUSELAGE) · airframe 64,053 hrs · 31,208 cycles

SKIN DENT REPAIR THE FUSELAGE SKIN WAS DENTED AT FS 1263 NEAR STRINGER 37L, DUE TO CONTACT WITH GROUND EQUIPMENT. THE DENT WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER IAW ER/A 385345-14 REV B.

Part: WEDGE — DEBONDED (L/E SLAT) · airframe 63,441 hrs · 30,872 cycles

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

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 62,312 hrs · 30,302 cycles

EMERGENCY PATH LIGHT AT SEAT 31AB INOP. REPLACED UNDERSEAT HARNESS. LIGHT OPERATES NORMALLY.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 62,035 hrs · 30,163 cycles

THE 1R EXTERIOR EMERGENCY LIGHT INOP. REPLAMPED SAME.

Part: LINE — SPLIT (RT W/W) · airframe 61,541 hrs · 29,942 cycles

ON CLIMBOUT, 'C' SYS HYD QTY MSG ACTIVATED. 'C' SYS QTY CK'D AT 0.31 FOUND BROKEN LINE IN RT UPPER OUTBD W/W. RPLD SAME

Part: CONNECTOR — SHORTED (NR 2 ENGINE) · airframe 61,081 hrs · 29,689 cycles

NR 2 ENG INFLT SHUTDOWN RT OIL FILTER LIGHT CAME ON. FOUND SHORT BETWEEN D4254P AND D4258J. REPLACED PLUG D4258J. SYSTEM CHECKS NORMAL.

Part: RIB — DAMAGED (T/E FLAP) · airframe 59,729 hrs · 28,946 cycles

INBOARD AFT RT FLAP WAS FOUND WITH ELONGATED FASTENER HOLES IN THE LEADING EDGE RIBS. REPAIR PER ER/A 410559-14 AND NORDAM EWO E0034025, REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,589 hrs · 28,400 cycles

ACCOMPLISHMENT OF PERMANENT REPAIR FOR CRACKED CHORD PER SB 767-53-0078.

Part: FAN — ODOR (E/E BAY) · airframe 57,644 hrs · 28,003 cycles

AFTER ENG START ELECTRICAL ODOR IN COCKPIT AND BY L1 DOOR. FOUND EICAS MSG, FWD SUP FAN 1. SECURED C/B H18. RAN ENGS, PACKS, CKD E/E COMPARTMENT, FWD GALLEY. UNABLE TO DUPLICATE WITH FAN DEACTIVATED. FWD FAN TO MCO/PLAC 21-58-03A.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,591 hrs · 27,985 cycles

COACH CLASS SEAT MOUNTED EMERGENCY EXIT LIGHTS INOP ON BOTH LEFT AND RIGHT SIDE. REPLACED BOTH LEFT AND RIGHT BATTERY PACKS.

Part: SLIDE — MISINSTALLED (PAX DOOR) · airframe 55,748 hrs · 27,203 cycles

R1 CABIN DOOR SLIDE NOT PROPERLY ATTACHED TO DOOR. REPLACED R1 DOOR SLIDE PER M/M, OPS CHECKS NORMAL.

Part: BRACE — MISMANUFACTURED (NR 1 PYLON) · airframe 54,925 hrs · 26,841 cycles

NR 1 ENGINE DIAGIONAL BRACE REPLACED WITH NEW THREE PIECE DIAGONAL BRACE ASSY TO MEET AD 200-07-05 REQUIREMENTS. NEW DIAG BRACE ASSY 0.033 INCH TOO SHORT WITH MAXIMUM SHIMMING ALLOWANCES. FABRICATED THICKER SHIMS WITH FAA APPROVAL. CORRECTIVE ACTION: 334321-14AD.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 54,925 hrs · 26,841 cycles

CORROSION DAMAGE FOUND ON THE AFT FACE AND FLANGES OF THE REAR SPAR BULKHEAD FITTINGS. THE CORROSION IS LOCATED JUST FWD OF THE FWD EDGE OF THE MLH W/W UPPER PRESSURE WEB, AND PROCEEDS INTO THE VERTICAL RAD II OF THE MACHINED FITTINGS ON BOTH THE LT AND RT SIDES. ER/A 334204-14.

Part: MODULE — CRACKED (RT MLG WW)

ON TOUCHDOWN, LOST CTR HYD SYS AND INTERMITTENT BRAKE VLV LIGHT WITH ALT SELECTED. RES BRAKE VLV EICAS MSG. CTR HYD SYS SHOWS .09 RF. NO RES BRAKE OR OR STEERING. BRAKE SOURCE LIGHT ON. C/ MTC IN PROG. RAT MODULE REPLACED.

Part: RELAY — FAILED (E/E COMPT)

RELAY K459 SHORTED OUT IN P-33 PANEL, CAUSING ELECTRICAL SHORT. REMOVED P33 PANEL. REPLACED K459 RELAY. FOUND HEAT DAMAGE ON TB090. REPLACED ALL HIGH DENSITY BLOCKS AND RE-TERMINATED WIRING. REPLACED NUMEROUS RELAYS FOR POSSIBLE HEAT DAMAGE. PERFORMED CARGO HEAT TEST, T/E SYSTEM TEST, AFT BULK COMPARTMENT TEST, PASSENGER ENTERTAINMENT TEST AND ALL OK.

Part: ENGINE — FAILED (NR 2)

IN DESCENT RT ENGINE FAILED, OIL PRESS WENT TO ZERO. REPLACED ENGINE.

Part: WEDGE — DELAMINATED (NR 4 TE SLAT)

THE LT WING NR 4 SLAT WAS FOUND WITH A 3 INCH DIAMETER AREA OF SKIN DELAMINATION. THE DAMAGE WAS REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364149-14AD.

Part: FLOORBEAM — CORRODED (BS 287)

CORROSION FOUND ON STA 287 FLOORBEAM UPPER CHORD FROM LBL 10 TO THE RT EOP. REPAIRED PER ERA 331029-14.

Part: FLOORBEAM — CRACKED (BS 246)

FS 246 FLOORBEAM UPPER WEB FOUND WITH TYP CRACK AT RBL 20 UNDERNEATH THE RBL 20 STIFFENER. ALSO, STIFFENER CRACKED. ADDITIONALLY, CORROSION FOUND ON WEB AND MID CHORD AT APPROX RBL 30 AND RBL 40. REPAIRED ERA 331015-14.

Part: SKIN — CORRODED (BS 1140)

ADDITIONAL CORROSION DAMAGE FOUND NEAR EXISTING REPAIRED CORROSION DAMAGE (REF ERA208585-14). REPAIR IS REMOVED AND A LARGER REPAIR INSTALLED. REPAIR PER ERA 208585-14, REV B.

Part: STRINGER — CORRODED (BS 550-654)

CORROSION DAMAGE BEYOND LIMITS FOUND ON STR 34R FROM STA 550 TO STA 654. REPAIRED PER ERA 331055-14.

Part: STRINGER — CORRODED (BS 1435-1461)

STR 30R CORRODED BEYOND LIMITS BETWEEN STA 1439 AND 1461. ALSO, STR 32R CORRODED BEYOND LIMITS BETWEEN STA 1417 AND 1439. REPAIRED PER ERA 331054-14.

Part: SKIN — CORRODED (BS 1202)

THE FUSELAGE SKIN AT BS 1202, STR 39R WAS FOUND CORRODED. THE CUTOUT IS APPROX 5.5 X 1.75 IN THE SKIN. REPAIRED PER ERA 331052-14.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

TWO SECTIONS OF EMERGENCY FLOOR TRACK LIGHTS IN REAR SECTION OF AIRCRAFT INOP. REPLACED BATTERY PACKS AND RACKS M9009 AMD M9010. EMERGENCY FLOOR TRACK LIGHTS OPS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

AFT SECTION OVERHEAD AISLE EMERGENCY LIGHTS AND R-4 DOOR EXIT LIGHT INOP. REPLACED POWER SUPPLY. SYSTEM CHECKS NORMAL.

Part: SLAT — DELAMINATED (NR 9 LE SLAT)

THE NR 9 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE A 4 INCH INBOARD/OUTBOARD X 2 FWD/AFT SECTION OF THE UPPER SKIN DELAMINATED. THE DAMAGE IS LOCATED INBOARD OF THE END OF THE SLAT WEDGE. THIS AREA WAS REPAIRED PER B767 SRM 57-43-02, FIGURE 201.

Part: SKIN — CRACKED (BS 1470)

DURING A LAYOVER VISIT, SKIN WAS FOUND CRACKED AND CORRODED AT STRINGER 32R AND 34R BETWEEN FS 1461 AND FS 1480. BOTH WERE REPAIRED PER SRM.

Part: SWITCH — MALFUNCTIONED (R2 DOOR)

ALL EXTERIOR EMERGENCY LIGHTS REPORTED ON. RETURNED TO GATE. ASSOCIATED WITH RT AFT ENT DOOR LIGHT CYCLING ON AND OFF. REPLACED PROX SWITCH AT RT AFT DOOR, SYSTEM OPS CHECK GOOD.

Part: COFFEE MAKER — FAULTY (GALLEY)

THE F/C NR 2 COFFEE MAKER STARTED SMOKING WHEN BREW BUTTON WAS PRESSED. SMOKE STOPPED AFTER CIRCUIT BREAKER PULLED. REPLACED COFFEE MAKER. SYSTEM CHECK GOOD.

Part: WIRE — BROKEN (CABIN)

AFT GALLEY EMERGENCY TRACK LIGHTS ARE OUT. REPAIRED BROKEN WIRE ON TRACK, CHECKS GOOD.

Part: COFFEE MAKER — FAILED (NR 3)

SMOKE AND HOT SMELL IN AFT GALLEY. HOT WATER COMING OUT OF COLD WATER FAUCET UNDER LT SIDE COFFEE MAKERS. FOUND NR 3 COFFEE MAKER OVERHEATING. PULLED AND COLLARED C/B. FWD TO MCO AND PLAC. REPLACED COFFEE MAKER, OPERATION NORMAL.

Part: HYD LINE — CHAFED (NR 1 ENGINE)

LT HYD SYS PRES MESSAGE, HYD QTY APPEARED TO STOP DECREASING AFTER TURNING OFF LEFT HYD SYSTEM. FOUND LEFT ENG HYD LINE FROM ENG PUMP CHAFING. REPLACED HYD LINE PER M/M CHAPTER 29. RAN ENG AND OPERATED ALL FLT CONTROLS, NO FURTHER LEAKS FOUND. A/C OK FOR SERVICE.

Part: WINDOW — SHATTERED (FLT DECK)

DURING CRUISE, FIRST OFFICER'S NR 1 WINDSHIELD SHATTERED, LANDED MCO. REPLACED WINDOW AND CONTROLLER, GROUND OPERATION NORMAL.