N1613B

Part: WIRE — BROKEN (CABIN) · airframe 78,876 hrs · 9,901 cycles

EMERGENCY ESCAPE PATH MARKING LIGHT INOPERATIVE AT 38AB AND 41AB. FOUND WIRE BROKEN UNDER SEAT 38A, 41A AND REPAIRED WIRES. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — DAMAGED (CABIN) · airframe 77,416 hrs · 9,757 cycles

EMERGENCY SEAT MOUNTED LIGHTING DAMAGED AT 40F. REPLACED LIGHT SHROUD HARDWARE. SYSTEM OPERATION IS NORMAL.

Part: FAILSAFE — CRACKED (BS 955) · airframe 72,979 hrs · 9,293 cycles

UT AND BHEC INSPECTIONS ON THE RT BS 955 FAIL SAFE STRAP REVEALED A CRACK. REPAIRED THE FAIL SAFE.

Part: LIGHT — UNSECURE (CABIN) · airframe 72,471 hrs · 9,244 cycles

EMERGENCY FLOOR LIGHTING INOPERATIVE AT 22B. SECURED LIGHT ASSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: SMOKE DETECTOR — DAMAGED (LAVATORY) · airframe 71,927 hrs · 9,192 cycles

AFT LEFT LAVATORY SMOKE DETECTOR GOING OFF (ALARMING) FOR NO REASON CONFIRMED NO EVIDENCE OF SMOKE. FOUND DETECTOR DAMAGED. REPLACED LAVATORY SMOKE DETECTOR. SYSTEM OPERATION IS NORMAL.

Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT CARGO BAY) · airframe 71,927 hrs · 9,192 cycles

AFT CARGO SMOKE DETECTOR RED WARNING LIGHT COMES ON AND STAYS ON WHEN THE REST BUTTON IS PRESSED IN THE AFT CREW REST. NO EVIDENCE OF SMOKE. REPLACED VESTIBULE NR 4 DETECTOR.

Part: LIGHT — INOPERATIVE (SEAT 31F) · airframe 71,233 hrs · 9,126 cycles

SEAT 31F MOUNTED EMERGENCY LIGHT FOUND INOPERATIVE. SECURED THE LOOSE EMERGENCY LIGHT ASSEMBLY. SYSTEM OPS NORMAL.

Part: STRAP — CRACKED (FUSELAGE) · airframe 67,379 hrs · 8,647 cycles

CRACK INDICATION IN FAILSAFE STRAP DURING UT INSPECTION. REPAIRED.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,518 hrs · 7,925 cycles

EMERGENCY LIGHT AND AFT EXIT SIGN AT L2 ARE INOPERATIVE. MAINTENANCE REPLACED FUSE 4 IN CHARGER M739. SYSTEM OPERATION IS NORMAL.

Part: SKIN — CRACKED (LT WING) · airframe 58,451 hrs · 7,552 cycles

CRACKS FOUND ON THE LEFT WING LOWER SKIN, RIB 31, S 9.5. REPAIRED IAW ERA 531217-14AD REV ORIGINAL.

Part: SKIN — CRACKED (LT WING) · airframe 76,897 hrs · 9,686 cycles

LEFT WING LOWER INSPAR SKIN RIB 31 STR L-9.5 CRACKS. C/W ERA 531217-14

Part: SKIN — CRACKED (LT WING) · airframe 76,897 hrs · 9,686 cycles

LEFT WING LOWER INSPAR SKIN RIB 31 STR L-9.5 CRACKS. C/W ERA 531217-00. (LP 1732568)

Part: SLIDE — DEFECTIVE (LT OVERWING) · airframe 54,701 hrs · 7,119 cycles

LEFT OVERWING SLIDE DEFECT. LT OVERWING SLIDE DEFECT RECTIFIED IAW AMDS 2565-8101.

Part: FIRE WARNING — FALSE ACTIVATION (NR 1 ENGINE) · airframe 51,371 hrs · 6,742 cycles

RT ENGINE, NR 1 FIRE LOOP MESSAGE CAME ON FOR 2 HRS THEN WENT AWAY. PERFORMED FIRE WARNING TEST ON GROUND NO FAULTS INDICATED.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENGINE FIRE) · airframe 51,371 hrs · 6,742 cycles

RT ENGINE FIRE LP 1 STATUS MESSAGE IN EICAS IN CRUISE. INSP FIRE LOOPS AND WIRING, NO FAULTS.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,707 hrs · 6,663 cycles

EXTERIOR EMERGENCY LIGHTS WILL NOT ILLUMINATE. R & R EMERGENCY LIGHT POWER SUPPLY PACK (M733) IAW AMM 33-51 LT SIDE CHECKEDS GOOD

Part: FLOORBEAM — CORRODED (BS 946-960) · airframe 47,931 hrs · 6,354 cycles

DURING PSV, FLOORBEAM AT FS 946-960 AND RBL 11 CORRODED BEYOND LIMITS. REPAIRED PER SRM 53-00-01 FIG 201 REPAIR 3.

Part: FLOORBEAM — CORRODED (BS 946 LBL 11) · airframe 47,931 hrs · 6,354 cycles

FOUND DURING PSV, CORROSION ON FLOORBEAM AT FS 946 AT LBL 11. REPAIRED PER SRM 53-00-51 FIG 201 REPAIR 3.

Part: LIGHT — SHORTED (CABIN) · airframe 42,171 hrs · 5,579 cycles

EMERGENCY LIGHTS SEAT 1GF TO 3GF ARE INOPERATIVE. MAINTENANCE REPLACED THE SHORTED BULB AT 2FG AND THE FUSE ON THE BATTERY PACK. SYSTEM OPERATION IS NORMAL.

Part: PIN — UNSECURE (EMERGENCY EXIT) · airframe 42,031 hrs · 5,561 cycles

ON CLIMBOUT LOUD RATTLE ON LEFT AFT OVERWING ESCAPE EXIT. UPON INSP FOUND PIN FOR LEFT AFT OVERWING STEP PANEL HINGE ASSY REF IPC 52-21-01-02 ITEM 80 OUT BY 1.5 INCH FORWARD. SUSPECTED AFT SECTION OF HINGE LOOSE. RE-SECURED PIN BACK IN HINGE ASSY PER MCC ALSO INSPECTED SLAT. ADP DOOR AND FOUND ALL ITEMS TO BE IN PERFECT CONDITION. A/C OF FOR SVC. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK.

Part: STEP — UNSECURE (EMERGENCY EXIT) · airframe 38,666 hrs · 5,161 cycles

STRONG VIBRATION NOTICED IN CRUISE FROM RIGHT WING ROOT AREA. FOUND THE OVERWING ESCAPE STEP HINGE PIN NOT FULLY INSTALLED. INSTALLED THE PIN ACC AMM 52-21-01-990-208. SATISFACTORY (DL76G101765).

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,564 hrs · 4,749 cycles

INOP R1 DOOR EMERGENCY LIGHT, RELAMPED OPS CHECK GOOD.

Part: FAN — FAILED (CARGO BAY) · airframe 33,989 hrs · 4,688 cycles

BULK CARGO VENT IN CEILING BLOWING AIR THAT SMELLS LIKE BURNED PLASTIC. REMOVED AND REPLACED BULK CARGO FAN PER AMM. OPS CHKS GOOD MCO AND PLACARD REMOVED.

Part: ENGINE — FOD (NR 1) · airframe 29,735 hrs · 4,214 cycles

ON APPROACH, THE A/C FLEW THROUGH A LARGE FLOCK OF BIRDS ON THE LEFT SIDE. THE NR 1 ENG INGESTED MANY BIRDS. THE CREW ADVISED THE VIBRATION KEPT CLIMBING ON THE NR 1 ENG AND THEY SHUT THE ENG DOWN ON ROLL OUT. MTC IN PROGRESS. REMOVED AND REPLACED COMPLETE SET OF BLADES ON NR 1 ENG, PE AMM 680596PERF. TASK 71-00-00-735-267-H02 TEST 6 VIBE SURVEY ALL CHKS NML. ALSO, PERF POWER ASSURANCE CHK ALL PARAMETERS NORMAL.

Part: ENGINE — MAKING METAL (NR 1) · airframe 29,617 hrs · 4,201 cycles

BEARING MATERIAL FOUND ON MCD, C/W NUMBER 1 ENGINE CHANGE PER TRANS 1T160.

Part: SKIN — DAMAGED (FS 1373) · airframe 29,616 hrs · 4,200 cycles

DURING MTC VISIT AT GSO, THE FUSELAGE SKIN WAS FOUND TO HAVE ONE DENTED AREA OUT OF LIMITS PER B767-300 SRM 53-00-01 AT FS 1373, BETWEEN S-28R AND S-29R. THE SRM REPAIR IS NOT APPLICABLE DUE TO PROXIMITY TO THE CARGO DOOR CUTOUT. AS SUCH, BOEING WAS CONTACT FOR REPAIR APPROVAL, AND IS DOCUMENTED IN ER/A 467423-14.

Part: OVEN — SPARKS (AFT GALLEY) · airframe 29,592 hrs · 4,194 cycles

AFT GALLEY OVEN NR 3 HAD SPARKS ON TOP WHEN TURNED ON, PULLED C/B. PULLED OVEN AND INSPECTED OVEN AND AREA FOR EVIDENCE OF ELECTRICAL OR MECHANICAL DEFECT. NO TROUBLE FOUND. REACTIVATED OVER AND PERFORMED OP CK, NO DEFECT NOTED. AS PRECAUTION REPLACED OVEN, S/N670.

Part: IDG — INOPERATIVE · airframe 29,583 hrs · 4,193 cycles

90 MIN OUT OF MAN, THE CREW GOT A LT ENG IDG DRIVE LIGHT. AFTER FOLLOWING QRH 50 MIN LATER, THE APU FAILED AND WOULD NOT RESTART. LGCU SWAPPED WITH APU GCU. LEFT S/N 1195 AND APU NOW S/N 6111. IDG REPLACED. ENGINE RUN CARRIED OUT. IDG OPS NML. LEAK OK. DISCONNECT FUNCTION, OPS NML.

Part: ENGINE — POWER LOSS (NR 2) · airframe 29,350 hrs · 4,166 cycles

NR 2 ENGINE REPLACED DECLINING PERFORMANCE.

Part: TURBINE WHEEL — DAMAGED (NR 2 ENGINE) · airframe 29,341 hrs · 4,165 cycles

ON CLIMB-OUT, RT ENGINE EGT RAN AWAY AND HAD TO RETARD THROTTLE 2 KNOB WIDTH TO MAINTAIN EGT UNDER REDLINE. MTC IN PROGRESS. PERFORMED BORESCOPE OF HPC/HPT. FOUND MINOR DAMAGE ON THE 5TH AND 13TH STAGE AND IS WITHIN BLEND REPAIRABLE LIMITS PER AMM 72-00-00-206-167-H00. ENGINE IS WITHIN OPERATION LIMITS AND GOOD FOR 10 FLT CYCLES.

Part: BULB — INOPERATIVE (ROWS 3AB & 5AB) · airframe 27,915 hrs · 3,993 cycles

FOUND AISLE EMERGENCY LIGHTS AT ROWS 3AB AND 5AB INOP. RELAMPED SAME PER AMM. OPS CKS GOOD.

Part: TRANSCEIVER — INOPERATIVE (FWD E&E) · airframe 27,164 hrs · 3,904 cycles

DURING FLIGHT KNOWN WEATHER DID NOT DISPLAY ON WX RADAR SCREEN. REPLACED RADAR R/T UNIT. AN TEST, ALL GOOD.

Part: ENGINE — UNKNOWN (NR 1) · airframe 26,932 hrs · 3,871 cycles

L ENG OIL FILTER EICAS MSG, REMOVED AND REPLACED LT ENG SCAVENGE OIL FILTER ELEMENT AND REMOVED AND REPLACED LT ENG OIL FILTER DIFFERENTIAL PRESSURE SWITCH. CHECK ALL CHIP DETECT, NO DEFECT NOTED. PERFORM HIGH POWER RUN FOR 10 MIN ALL INDICATIONS NORMAL.

Part: BRAKE — LEAKING (NR 4) · airframe 25,203 hrs · 3,665 cycles

AFTER LANDING TOWER REPORTED RT MAIN GEAR EMERGENCY. CREW CAME OUT SPRAYED GEAR. REPORTED LIGHT SMOKE IND NORMAL THE WHOLE TIME. PERFORMED BRAKE FIRE INSP. REPLACED NR 4 BRAKE ASSY AND NR 4 WHEEL ASSY PER MM BRAKE MPN 2612412-1A WHEEL MPN IS 767-300ERM. FOUND BRAKE PISTON BROKEN AND LEAKING.

Part: ACTUATOR — MALFUNCTIONED (LT I/B AILERON) · airframe 24,557 hrs · 3,589 cycles

ON CLIMB-OUT WITH A/P ON NOTICED CONTROL WHEEL DEFECTED 2 DEGREES RIGHT WITH A/P OFF RUDDER TRIM PLACED 7 DEGREES RIGHT TO CENTER WHEEL. REMOVED LEFT INBD AIL PCA OUTBD PCA LT SYS OK TO INSTALL PCA S/N 3666. INSTALLED LEFT INBD AIL OUTBD PCA INSTALLATION OK. ADJ TEST OK. SAFTY AND SECURITY CHECK OK RII INSPECTIONS C/W MM 27-11-48 FOR REMOVAL AND INSTALLATION OF LT I/B AILERON PCA.

Part: PRESSURE SWITCH — MALFUNCTIONED (NR 1 ENGINE) · airframe 22,680 hrs · 3,356 cycles

DURING TAXI OUT LT ENG FUEL FILTER STATUS MSG ILLUMINATED -RTB. REPLACED DIFF PRESS SWITCH AND FUEL FILTER. ETOPS CATEGORY (E): PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: VIDEO UNIT — INOPERATIVE (CABIN) · airframe 22,051 hrs · 3,281 cycles

VIDEO EQUIPMENT INOP. RESET IFE COOLING C/B. OPS CKS GOOD.

Part: CONTROLLER — BYPASSING (RT AILERON) · airframe 20,755 hrs · 3,123 cycles

REPEAT GRIPE - RIGHT INBOARD AILERON FROZEN 1/3 UP POSITION REQUIRING 6 UNITS LEFT RUDDER TRIM IN CRUISE. REPLACED BOTH PCAS RT INBOARD AILERON AND PERFORMED AILERON RIGGING ADJ TEST. SUBSEQUENT NON-REVENUE VERIFICATION FLIGHT OK.

Part: ACTUATOR — BYPASSING (NR 7 SPOILER) · airframe 20,755 hrs · 3,123 cycles

EXCESSIVE RUDDER TRIM NEEDED FOR LEVEL FLT RT INBD AILERON DEFLECTING UP. T/S SYSTEM FOUND NR 7 SPOILER ACTUATOR BYPASSING, REMOVED NR 7 SPOILER ACT. REPLACED NR 7 SPOILER ACTUATOR SYSTEM CHECKS GOOD PER MM 27-61. RII INSPECTED INSTALL AND ADJUST OF NR 7 SPOILER ACTUATOR OK.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,348 hrs · 3,077 cycles

FOUND LT OVERWING EMERGENCY EXT LIGHT FWD ONE BULB INOP. RELAMPED CKS OK.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 19,816 hrs · 3,015 cycles

ON PDC FOUND EMERGENCY LIGHTS IN SEATS 15 THRU 20 AB INOP. FOUND WIRES CRUSHED AND BROKEN AT SEAT 15A. REPAIRED WIRES, LIGHTS OP OK.

Part: LIGHT — DAMAGED (SEAT 15 A/B) · airframe 18,024 hrs · 2,800 cycles

FWD EMERGENCY EXIT LIGHT ASSY 15 A/B DAMAGED. REP FWD EMERGENCY LIGHT ASSY AT SEAT 15 A/B, CK GOOD.

Part: ACTUATOR — LEAKING (LT AILERON) · airframe 14,763 hrs · 2,355 cycles

C-HYDRAULIC QUANTITY DECREASED IN FLIGHT. REPLACED O-RING ON NR 4 SPOILER ACTUATOR.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,437 hrs · 2,165 cycles

SEATS 2 A/B AND 2 F/G E-PATH LIGHTS INOP. RELAMPED AND REPLACED LENS, OPS CHECK OK.

Part: CIRCUIT BREAKER — POPPED (COCKPIT) · airframe 10,268 hrs · 1,710 cycles

A/C HAD NUMEROUS FAULTS AND WARNINGS AND THE CREW DECLARED AN EMERGENCY. AFTER EMERGENCY DECLARED THE CREW FOUND THE DC STBY C/B POPPED ON THE P-6 PANEL DOWN BY THE FLOOR. RESET THE C/B AND ALL SYSTEMS NORMAL. MTC DID A FUNCTIONAL CHECK OF THE STBY POWER SYSTEM. ALL SYSTEM CHECK OK.

Part: ODOR — DETECTED (CABIN) · airframe 3,593 hrs · 653 cycles

ON TAXI OUT FLIGHT ATTENDANT SMELLED A FAINT SMELL OF SMOKE IN THE FWD CABIN. A/C RTB AND TECH PERFORMED ENGINE RUN AND CHECKED PNEUMATIC SYSTEM. PERFORMED CHECK OF IFE ENTERTAINMENT SYSTEM. ALSO CHECKED MAIN E/E COMPARTMENT FOR FAULT BALLSOR LRU FAULTS. NO DISCREPANCIES NOTED. COULD NOT DUPLICATE SMELL. ALSO CHECK FWD LAV UNDER SINK AND CABINET AREA, NO FAULTS NOTED.

Part: FIRE BOTTLE — LEAKING (CABIN) · airframe 2,966 hrs · 539 cycles

FOUND WATER FIRE EXTINGUISHER IN FWD CABIN HAD LEAKED ALL OF THE WATER OUT. REPLACED BOTTLE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 292 hrs · 63 cycles

EMERGENCY LIGHTS AT SEATS 10GF - 11GF INOP. REPLACED BATTERY CHARGER M1209, OPS NORMAL.