N105DA

Part: STRUCTURE — CORRODED (T/E FLAP) · airframe 66,594 hrs · 32,114 cycles

RIGHT I/B FLAP ATTACH BOLTS HOLES CORRODED. REPAIRED PER ERA 089397-14MA REF NRC402 404 400 403 399 401.

Part: ACTUATOR — BROKEN (HORIZONTAL STAB) · airframe 64,835 hrs · 31,238 cycles

DURING A LUBE VISIT (1T188), AN AMT FOUND THE LOWER ICE SCRAPER RING FROM THE STAB TRIM ACTUATOR BALL NUT BENT AND OUT OF PLACE. IT WAS FOUND AT THE BOTTOM OF THE BALLSCREW. THE ACTUATOR PART NUMBER IS 251T4310-1. THE PART NUMBER OF THE SCRAPER IS B18834-7R. REPLACED SAME

Part: WEDGE — DEBONDED (L/E SLAT) · airframe 64,006 hrs · 30,804 cycles

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

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 62,673 hrs · 30,157 cycles

FOUND ON TRANSIT CHECK 2R DOOR FLT ATTENDANT EMERGENCY FLASHLIGHT INOP. REPLACED SAME.

Part: MODULE — FAULTY (E/E BAY) · airframe 62,231 hrs · 29,935 cycles

ABORTED TAKEOFF IN BOS FOR SPOILERS WARNING. RECYCLED SPEED BRAKE HANDLE PER BOS MTC. THROTTLED UP ON TAXIWAY WITH NO WARNING LIGHT. ATTEMPTED ANOTHER TAKEOFF. ABORTED FOR SPOILERS AGAIN. BOTH ABORTS LESS THAN 15 KNOTS. T/S PER FIM 31-51-00 FIG 108. REPLACED T/O CONFIG WARNING MODULE. PERFORMED CONFIG T/O TEST. CHECKS OK PER M/M.

Part: SOCKET — DEFECTIVE (EXTERIOR) · airframe 60,399 hrs · 28,945 cycles

LEFT OFFWING SLIDE LIGHT INOP. REPLACED LIGHT SOCKET, OPS CHECK GOOD.

Part: BULKHEAD — CRACKED (FS 1809.5) · airframe 59,881 hrs · 28,652 cycles

FUSELAGE / BULKHEAD / FS 1809.5 / RH / OUTER FWD CHORD : CRACK REPAIR INSPECTION OF THE FS 1809.5 BULKHEAD PER AD 2001-09-13 REVEALED A CRACK IN THE RH FWD OUTER CHORD TYPICAL OF THE AD AND BAC S/B 767-53-0078. THE FWD CHORD WAS CUT AND A NEW SECTION SPLICED PER THE S/B. INSPECTION OF THE LOCAL SPLICE FITTING AND SKIN IN THE AREA REVEALED A CRACK AT A FASTENER HOLE. THE HOLE WAS OVERSIZED AND BUSHED IN THE CRACKED MEMBERS. THE REPAIRS WERE PER ER/A 381714-14AD,REV A

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,784 hrs · 28,612 cycles

ON L/O FOUND EMERGENCY LIGHTS INOP AT RT OVERWING EXIT SIGN, 2L DOOR EXIT SIGN AND AFT RT LAV RED FLOOR LIGHT. RELAMPED RT OVERWING EXIT AND 2L DOOR EXIT. REPAIRED BROKEN WIRE AT 3R LAV FLOOR LIGHT.

Part: FITTING — TOOL DAMAGE (LT & RT WINGS) · airframe 56,748 hrs · 27,292 cycles

TOOLING DAMAGE OCCURRED IN THE LT AND RT WING O/B PITCH LOAD FITTINGS. THE DAMAGE WAS LOCATED ON THE THIRD FROM BOTTOM HOLE ON THE VERTICAL LEGS OF THE BACK-UP FITTINGS. REWORK CONSISTED OF OS AND RE-COLD WORKING HOLES. ER/A 334916-14.

Part: BULKHEAD — DAMAGED (NR 1 & 2 PYLONS) · airframe 56,748 hrs · 27,292 cycles

FOUR HOLES FOUND ELONGATED IN THE AFT BULKHEAD OF BOTH PYLONS. ON THE NR 1 PYLON I/B FLANGE, THE UPPER HOLE, THE SECOND FROM THE TOP, AND THE 5TH GSE FASTENER HOLE FROM THE TOP WERE DAMAGED. ON THE NR 2 PYLON, THE UPPER GSE HOLE ON THE I/B FLANGE WAS FOUND WITH DAMAGE. ER/A 334923-14.

Part: SKIN — WORN (FUSELAGE) · airframe 56,748 hrs · 27,292 cycles

PERFORMED SRM REPAIR 53-80-01-2-203. REF NR 336. REPAIR OF DAMAGE ON FUSELAGE SKIN ABOVE RT HORIZ STAB AT STA 1809.5.

Part: CONTROL CABLE — FRAYED (RUDDER) · airframe 56,748 hrs · 27,292 cycles

FOUND RUDDER CABLES RA-4 AND RB-4 FRAYED AT AFT RUDDER QUADRANT AT CENTERING MECHANISM. REPLACED CABLES.

Part: SKIN — CRACKED (BS 1255-1270)

FUSELAGE SKIN FS 1255-1270, STRINGER 38L-39L, CRACK REPAIR. WHILE ACCOMPLISHING REPETITIVE HFEC INSPECTION OF EXISTING SKIN DENTS BETWEEN FS 1255 AND 1260 AND BETWEEN S-38L AND 39L, THREE SMALL CRACKS WERE DETECTED. THE CRACKS WERE CUTOUT OF THE SKIN. AN EXSITING DOUBLER REPAIR WAS ADJACENT TO THIS LOCATION AND REMOVED. THE PREVIOUSLY REPAIRED DAMAGE CUTOUT AND THE NEW DAMAGE CUTOUTS WERE REPAIRED WITH A SINGLE ALUMINUM DOUBLER PER ER/A 368192-14.

Part: SKIN — CRACKED (BS 1270)

FUSELAGE SKIN FS 1270 STRINGER 38R, CRACK REPAIR. DURING REPETITIVE HFEC INSPECTION OF AN EXISTING DENT AT FS 1270, NEAR STRINGER 38R, A CRACK WAS FOUND. THE CRACK WAS ROUTED OUT OF THE SKIN WITH A CUTOUT. THE SKIN CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 368195-14.

Part: WEDGE — DELAMINATED (NR 9 LE SLAT)

THE TRAILING EDGE WEDGE OF THE NR 9 SLAT WAS FOUND WITH A 4 X 4 AREA OF DELAMINATION. THE DAMAGE AREA WAS CUT OUT AND REPAIRED PER THE B767 SRM 57-43-02. THE REPAIR WAS DOCUMENTED PER ER/A 367010-14AD.

Part: BATTERY — DISCHARGED (LT SERVICE DOOR)

EMERGENCY LIGHTS INOP LT AFT CEILING AND LT AFT SERVICE DOOR. REPLACED BATTERY PACK, OPS NORMAL.

Part: RVDT — INTERMITTANT (LT WING)

AFTER TAKEOFF, L/E CAUTION AND L/E SLAT ASSY EICAS MSG. RETURNED TO LAX. REPLACED M548 RVDT PER MM, ALL OPS NORMAL.

Part: BULB — MISSING (CABIN)

EMERGENCY TRACK LIGHT BULB AND LENS MISSING AT ROW 34B. INSTALLED BULB, LENS, AND O-RING AT EMERGENCY LIGHT 34B.

Part: LIGHT — MISSING (CABIN)

IRREG: 3RD WHITE EEPLS LGT MISSING F/C LT SIDE. REPLACED LGT MODULE, CKS GOOD.

Part: SKIN — CORRODED (BS 1540/1562)

THE FUSELAGE SKIN AND STRINGERS WERE FOUND CORRODED BETWEEN STA 1540 AND STA 1562, LOCATED BETWEEN STR 39R AND STR 39L. THE FUSELAGE SKIN IS CORRODED NEAR AN EXISTING DRAIN HOLE. STRINGER SECTIONS WERE SPLICED IN TO REPAIR THE DAMAGED STRINGERS. THE SKIN WAS REPAIRED WITH A DOUBLER. ADDITIONALLY, THE FRAME WEB AT STA 1562 WAS CUT AT LBL 10 AND RBL 10. THIS REPAIR SCHEME WAS APPROVED BY FAA/DER FORM 8110-3, DER DESGINATION SO889, DATED MAR 7, 1997.

Part: HYD FILTER — CRACKED (RT MLG)

ON TAXI OUT, LOSS OF CENTER HYDR QTY WENT TO ZERO AND SYS PRESS LIGHT CAME ON. FOUND C-SYS HYD MODULE AFT BLEW ELEMENT CASE CAUSING HYD FAILURE OF C-SYS. REPLACED EDP FILTERS AND MODULE.

Part: TRACK LIGHTS — DAMAGED (CABIN)

EMERGENGY FLOOR TRACK DAMAGED IN SEVERAL AREAS OF CABIN, AT SEATS 28FG, 30FG AND 13FG. REPLACED FLOOR TRACK AT SEATS 28FG, 30FG AND 13FG, TESTS GOOD.

Part: DOOR — DAMAGED (FWD CARGO COMPT)

DURING LETTER CHECK INSP, FOUND FWD CARGO DOOR HAS TWO AREAS OF DAMAGE ON SUPPORT STRUCTURE FOR LOWER HOOKS MARKED BETWEEN FWD AND MID HOOK AND BETWEEN MID AND AFT HOOK BURNISHED AND DYE CHECKED FWD AREA DYE CHECKED OK. REMOVED DAMAGE FROM AFT AREA IAW SRM 51-70-11 FABRICATED DOUBLER AND INSTALLED.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

DURING LETTER CHECK, FOUND LIGHTNING STRIKES TOP OF FUSELAGE LOCATED FWD AND AFT OF PRODUCTION SPLICE FWD OF VERTICAL STABLIZER 3 FWD AND 3 AFT, BURNISHED OUT AND REMOVED RIVETS EDDY CURRENT. CHECKED OK INSTALLED RIVETS PER SRM 53-00-01