N829MH

Part: BRACKET — BROKEN (ZONE 200) · airframe 98,703 hrs · 18,599 cycles

SEAT 33AB E PATH LIGHT ASSY MOUNTING BRACKET BROKEN OFF SEAT, NO MOUNTING "EARS". CORRECTIVE ACTION: REMOVED AND REPLACED EMERGENCY LIGHT HOUSING @PAX SEAT 33AB PER CMM 25-28. OK FOR SVC. (7928961)

Part: BRACKET — BROKEN (ZONE 200) · airframe 98,610 hrs · 18,585 cycles

SHIP 1805 SEAT MOUNTED WHITE E PATH LIGHTS MOUNTING BRACKETS HAVE 1 BROKEN EAR @ LOC 34+45 RIGHT AND 32,34,37 LEFT. CORRECTIVE ACTION: REMOVED AND REPLACED EMERGENCY PATHWAY LIGHT HOUSINGS @LOC 35,45 FG AND LOC 32,34,37 AB PER CMM 25-28. ALL OPS NML. (7928962)

Part: INTERLOCK — BROKEN (ZONE 700) · airframe 97,758 hrs · 18,458 cycles

ATB, RETURN TO JFK DUE TO GEAR DISAGREE AND GEAR DOOR MESSAGES AFTER GEAR RETRACT. C/W OW LANDING INSP. FOUND LMLG DOOR MTC ACCESS PANEL INTERLOCK MECHANISM OUT OF ADJ AND LT MAIN LANDING GEAR DOOR SAFETY PIN INSTALLED. REPAIRED AND ADJUSTED INTERLOCK MECHANISM. MLG DOORS OPS NML.(7547412)

Part: COVER — DAMAGED (ZONE 200) · airframe 96,802 hrs · 18,313 cycles

SHIP 1805 EMER OVERHEAD LIGHT COVER 3L. CORRECTIVE ACTION: REPAIRED PER ER/A 626435-14. (6389614)

Part: LINE — MALFUNCTIONED (ZONE 400) · airframe 96,802 hrs · 18,313 cycles

SHIP 1805- ATO - 10 KTS- ABORTED TAKE OFF DUE TO LEFT ENGINE APPEARED TO BE SLOW TO SPOOL. CORRECTIVE ACTION: PURGE PS3 LINE AND PERFORMED ACTUATORS CHECK. RAN ENGINE TWICE. OPS CHECK GOOD. (6648294)

Part: SKIN — DAMAGED (ZONE 100) · airframe 96,741 hrs · 18,305 cycles

SHIP 1805 FUSELAGE DAMAGE BY LT NOSE GEAR DOOR. C/W REPAIR INSTALL PER B767 400 SRM 5-00-01 (6648241)

Part: COVER — LOOSE (ZONE 200) · airframe 96,679 hrs · 18,298 cycles

SHIP 1805 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:605. REPAIRED LIGHT ASSY PER ER/A 626435-14 (0964684)

Part: INDICATOR — FAULTED (ZONE 800) · airframe 94,978 hrs · 18,055 cycles

SHIP 1805 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS: 4L. CORRECTIVE ACTION: REMOVED AND REPLACED 4L SLIDE INDICATOR ARMED LIGHT ASSEMBLY IAW B767-400 AMM 52-73. (0754382)

Part: MODULE — FAULTED (L1 DOOR SLIDE) · airframe 94,273 hrs · 17,961 cycles

SHIP 1805 1L DOOR 'SLIDE' LIGHT INOP. CORRECTIVE ACTION: MOVED AND REPLACED SLIDE LIGHT ARM MODULE PER B767-400 AMM 52-73 (6747136)

Part: LENS — UNSECURE (ARM INDICATOR) · airframe 94,229 hrs · 17,955 cycles

SHIP 1805 FLT CREW EWPORTS 1L DOOR ARM INDICATION INOP. CORRECTIVE ACTION: SECURED "ARMED" LENS ASSY REF B767 AMM 33-16. LAMP TEST OKAY (6747124)

Part: LIGHT — UNSECURE (ZONE 200) · airframe 93,714 hrs · 17,894 cycles

SHIP 1805 DURING BOARDING CREW REPORTED AT DOOR 3L DAMAGED CROSS AISLE EXIT IDENTIFIER. CORRECTIVE ACTION: RESECURED MOUNT AND LIGHT ASSEMBLY WITH 3M8681HS. ADHESIVE TAPE PER ERA 621337-14 REV ORIGINAL SEC 1. (5808196)

Part: FAN — CLOGGED (ZONE 200) · airframe 93,480 hrs · 17,863 cycles

SHIP 1805 ELECTRICAL SMELL REPORTED BY INFLIGHT CREW. SMELL REPORTED THROUGHOUT CABIN. CORRECTIVE ACTION: FOUND AFT GALLEY LAV VENT FAN NUMBER ONE NOT CREATING SUCTION.REF B767 AMM 21 26, REMOVED FAN AND FOUND INLET SCREEN CLOGGED WITH RUBBER GLOVES AND COMPACTED DUST. (5808114)

Part: SPAR — CRACKED (ZONE 400) · airframe 93,435 hrs · 17,853 cycles

SHIP 1805 REFER LOG #1503452, FOUND NO.1 PYLON I/B SIDE MID SPAR AFT WEB CRACK AT NAC 290. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER ER/A620276-14 (0541998)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 93,435 hrs · 17,853 cycles

SHIP 1805 THE SEAT TRACK FOUND CORROSION AT RBL 88 STA 1109 REF CPCP TASK NO:53-646-00. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER ERA 620452-14. (0540185)

Part: SPAR — DAMAGED (ZONE 400) · airframe 93,435 hrs · 17,853 cycles

SHIP 1805 ERA 620276-14 ISSUED FOR REPAIR TO #1 PYLON AFT MIDSPAR WEB DTE DTA IS REQUIRED. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER ER/A 00-620276 (0541019)

Part: SKIN — CRACKED (ZONE 200) · airframe 93,435 hrs · 17,853 cycles

SHIP 1805 OPEN HOLE HIGH FREQUENCY EDDY CURRENT(HFEC) INSPECTION OF ALL FASTENER HOLES(5EA.) AT THE FORWARD SERVICE DOOR CUT OUT AFT LOWER CORNER FOR ANY CRACK. FOUND CRACK AT NO.4 FASTENER HOLE. THE CRACK LOCATED AT 3 O'CLOCK. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER 620270-14AD (0540370)

Part: SKIN — DAMAGED (ZONE 200) · airframe 93,435 hrs · 17,853 cycles

SHIP 1805 ERA 620270-14AD ISSUED FOR REPAIR TO RH FORWARD DOOR CUTOUT, AFT LOWER SKIN REPAIR. FOLLOW ON ACTION IS REQUIRED. CORRECTIVE ACTION: ERA 620270-14AD ISSUED FOR REPAIR TO RH FORWARD DOOR CUTOUT, AFT LOWER SKIN REPAIR. FOLLOW ON ACTION IS REQUIRED. (0539100)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 93,435 hrs · 17,853 cycles

SHIP 1805 FWD CARGO SHEAR TIE FOUND CORROSION AT STA 654+22 BETWEEN S39L AND S39R, CORRECTIVE ACTION: THE DAMAGED SHEAR TIE REMOVED AND REPLACED AS PER B767- 400 SRM 51-40-02 (0525905)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 93,435 hrs · 17,853 cycles

SHIP 1805 FWD CARGO SHEAR TIE FOUND CORROSION AT STA 742 BETWEEN S39L AND S39R. CORRECTIVE ACTION: THE DAMAGED SHEAR TIE REMOVED AND REPLACED AS PER B767- 400 SRM 51-40-02 (0525884)

Part: WEDGE — DELAMINATED (NR 5 SLAT) · airframe 93,435 hrs · 17,853 cycles

SHIP 1805 #5 SLAT O/B SIDE T/E WEDGE FOUND DELAMINATION. CORRECTIVE ACTION: #5 SLAT O/B SIDE T/E WEDGE REPAIRED AS PER B767-400 SRM 57-43-02 (0519173)

Part: WEDGE — DELAMINATED (NR 4 SLAT) · airframe 93,435 hrs · 17,853 cycles

SHIP 1805 #4 SLAT O/B SIDE T/E WEDGE FOUND DELAMINATION. CORRECTIVE ACTION: #4 SLAT O/B SIDE T/E WEDGE REPAIRED AS PER B767-400 SRM 57-43-02 -2R-1 & SRM 51-70-10-2R-4. (0519154)

Part: STIFFENER — CRACKED (ZONE 100) · airframe 93,435 hrs · 17,853 cycles

SHIP 1805 MFEC INSPECTION FOUND 01EA CRACK APPROX. 0.750 INCH IN LENGTH ON NOSE WHEEL WELL RH VERTICAL STIFFENER FROM WL159.00 TO WL185.00 AS MARK. CORRECTIVE ACTION: ACCOMPLISHED THE VERTICAL STIFFENER REPAIR AT NOSE WHEEL WELL STA287 RBL25 REF TO J/C:5312-01186-01B (0516816)

Part: INDICATOR — UNKNOWN · airframe 93,321 hrs · 17,838 cycles

SHIP 1805 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:601. CORRECTIVE ACTION: PERFORMED BUTTON LIGHT TEST & ARMED DOOR, NTF. OK FOR SVC. (0469370)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,775 hrs · 17,768 cycles

AIRCRAFT 1805, DURING SVC CHK FOUND EMERGENCY LIGHTS ON SEATS 20-32 E, F INOP. CORRECTIVE ACTION: REPLACED BATTERY PACK. (LP 5330742)

Part: INDICATOR — UNKNOWN (R4 DOOR) · airframe 92,385 hrs · 17,714 cycles

4R ENTRY/SERVICE DOOR SLIDE ARMED INDICATING LIGHT SYSTEM. CORRECTIVE ACTION: RELAMPED 4R DOOR ARMED INDICATION IAW B767-400 AMM 33-22. OK FOR SVC. (0341186)

Part: HANDLE — BINDING (MLG) · airframe 92,222 hrs · 17,694 cycles

SHIP 1805 -GEAR- ALTERNATE GEAR EXTEND SYSTEM USED TO LOWER LANDING GEAR DUE TO JAMMED LANDING GEAR CONTROL HANDLE. CORRECTIVE ACTION: R/R LANDING GEAR HANDLE MODULE.(5631749)

Part: LIGHT — DETACHED (CABIN) · airframe 91,860 hrs · 17,648 cycles

SHIP 1805 3R EMERGENCY EXIT LIGHT FELL OFF AFTER LANDING. CORRECTIVE ACTION: RESECURED OVERHEAD EMERGENCY EXIT SIGN AS REQUIRED. ALL OPS CHKS GOOD. OK FOR CONT SVC (5338913)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 91,481 hrs · 17,600 cycles

SHIP 1805 DURING SERVICE CHK, FOUND CREW REST EMERGENCY LIGHT INOP. CORRECTIVE ACTION: R/R CREW REST EMERGENCY LIGHT BATTERY PACK IAW B767 AMM 3351. OPS CHK GOOD (5815893)

Part: SIGN — OUT OF POSITION (CABIN) · airframe 90,973 hrs · 17,534 cycles

SHIP 1805 DURING SERVICE FOUND AFT R4/L4 DOOR EMERGENCY EXIT SIGNS MISCONFIGED PER SERVICE CHK. CORRECTIVE ACTION: VERIFIED W/ ENGINEERING ONLY 1 EXIT SIGN (RUNNING MAN) ON EITHER SIDE OF 4L & 4R DOOR REF B767 - AIPC 33-21-01-04, WORKCARD 3321 -01-053-05 & BRUCE & AEROSPACE. (5493616)

Part: SIGN — INOPERATIVE (CABIN) · airframe 90,956 hrs · 17,532 cycles

SHIP 1805 DURING SERVICE FOUND COCKPIT EMERGENCY EXIT SIGN INOP. CORRECTIVE ACTION: R/R COCKPIT EMERGENCY EXIT SIGN PER B767 MM 33-51. OPS NORMAL. (5493612)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 90,956 hrs · 17,532 cycles

SHIP 1805 DURING SERVICE FOUND CREW REST EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: REPLACED LLCR BATTERY PACK PER B767-400 AMM 33-51. BATTERY PACK TESTS GOOD. CREW REST EMERGENCY LIGHTS ALL CAME ON. A/C OK FOR SVC. (5493613)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 89,307 hrs · 17,308 cycles

SHIP 1805 PERFORMED SMOKE, FIRE, + FUMES CHECKLIST DURING CRUISE DUE TO MULTIPLE REPORTED FLIGHT ATTENDANT ILLNESSES. CORRECTIVE ACTION: CREW REPORTS ON SMOKE+FUME QUESTIONAIRE NO FUMES OR ODORS ONLY MULTIPLE FA ILLNESSES. CONFERRED W/MCC ATL. NOT AN ODI. NO FURTHER T/S REQ. A/C OK FOR SERVICE (4118283)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 89,301 hrs · 17,307 cycles

SHIP 1805 SLIDE ARMED LIGHT 1L F/A PNL INOP, CORRECTIVE ACTION: UNABLE TO DUPLICATE FAULT. PERFORMED SLIDE-RAFT ARMED WARNING SYSTEM OPS TEST PER B767-400 AMM 52-73. OPS CHECK GOOD. MEL CLEARED. PLACARD REMOVED (4118279)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,885 hrs · 17,252 cycles

SHIP 1805 DOOR 1L SLIDE ARMED LIGHT INOP. CORRECTIVE ACTION: SLIDE LIGHT SWITCH RESEATED, NOW OPS OK. (4410640)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,439 hrs · 17,190 cycles

SHIP 1805 L CTR ENT DOOR EICAS MSG ILLUMINATED WITH DOOR CLOSED AND ARMED AN ENTRY DOORS LIGHT ON OVERHEAD PANEL EXTINGUISHED. CORRECTIVE ACTION: FOUND L DCU C/B OUT. RESET C/B AND CYCLED L CTR ENTRY DOOR AND OPS NML. OK FOR SVC (8956585)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,132 hrs · 17,148 cycles

AIRCRAFT 1805, DOOR 3 RIGHT EMERGENCY LIGHT INOP. CORRECTIVE ACTION: FOUND WIRING SEPERATED INSIDE OF 3R DOOR INTERIOR RUNNING MAN SIGN. RE-SOLDER WIRES PER B767-400 AMM 20-10. OPS CHECKS EXIT SIGN GOOD. (LP 9143454)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,994 hrs · 17,126 cycles

SHIP 1805 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS: 1L. CORRECTIVE ACTION: COULD NOT DUPLICATE FAULT. OPS CHECK GOOD IAW B767-4 AMM 52-73. (2783153)

Part: SENSOR — INOPERATIVE · airframe 86,098 hrs · 16,865 cycles

SHIP 1805 MAIN ENTRY/SERVICE DOOR ARMED INDICATORS 2R DOOR ARM LIGHT INOP. CORRECTIVE ACTION: NO. TROUBLE FOUND. OK FOR SVC. MEL/PLAC REMOVED. (2544651)

Part: INDICATOR — INOPERATIVE · airframe 85,893 hrs · 16,826 cycles

SHIP 1805 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:101. CORRECTIVE ACTION: PERFORMED OPS TEST OF 101 SLIDE INDICATOR LIGHT. OPS TEST GOOD REF B767-400 AMM 52-11 (2510534)

Part: SKIN — DENTED (LT NR 4 SLAT) · airframe 85,846 hrs · 16,811 cycles

SHIP 1805 FOUND DENT ON LH WING #4 SLAT UPPER SURFACE AT 23 INCHES FROM O/B EDGE AND 4 INCHES FROM UPPER EDGE. LH WING #4 SLAT UPPER SURFACE AT 23 INCHED FROM O/B EDGE AND 4 INCHES FROM UPPER EDGE REPAIRED AS PER B767-400 SRM 57-43-02-2R- 1 AND SRM 51-70-10-2R-0.

Part: SKIN — DELAMINATED (LT NR 4 SLAT) · airframe 85,846 hrs · 16,811 cycles

THE L/H WING NO.4 SLAT UPPER SURFACE FOUND DELAMINATION FROM O/B EDGE 13 INCHES UPPER T/E 5.5 INCHES. THE L/H WING NO.4 SLAT UPPER SURFACE FROM O/B EDGE 13 INCHES, UPPER T/E 5.5 INCHES REPAIRED AS PER B767-400 SRM 57-43-02-2R-1 AND SRM 51-70-10-2R-0.

Part: NONE — NONE · airframe 85,195 hrs · 16,717 cycles

SHIP 1805 FOUND ON SERVICE CHECK - EMER LIGHTS DO NOT ILLUM IN LLCR. CORRECTIVE ACTION: REPLACED LLCR'S EMER LIGHTS BATTERY (P/N 55-1988-1)AND POWER SUPPLY. EMER LIGHTS NOW TEST GOOD. (9150808)

Part: NONE — NONE · airframe 85,195 hrs · 16,717 cycles

SHIP 1805 FOUND ON SERVICE CHECK - WHITE EEPLES LENSES MISSING AT MID GALLEY LEFT-FWD, L1 CLOSET, AND 2 AT FWD GALLEY AFT. RED EEPLS LENS MISSING AT L1 CLOSET. CORRECTIVE ACTION: INSTALLED 5 WHITE EEPLS LENSES AND 1 RED LENS AT INDICATED LOCATIONS. EMERGENCY LIGHTS CHECKS GOOD. (9150806)

Part: NONE — NONE · airframe 84,957 hrs · 16,687 cycles

AIRCRAFT 1805, FOUND FLIGHT ATTENDANT LOWER LOBE CREW REST (FALLCR) FAILED/INOP DURING EMERGENCY LIGHTS OPERATIONAL TEST. CORRECTIVE ACTION: PERF OP CHK OF FALLCR PER B767 AMM 33-51. CHKS GOOD. OK FOR SVC. (9011110)

Part: PIN — LOOSE · airframe 84,810 hrs · 16,665 cycles

SHIP 1805 EMERGENCY LIGHTS IN THE FLIGHT ATTENDANT LOWER LOBE CREW REST ( FALLCR) FOUND INOP, CORRECTIVE ACTION: FOUND PIN 3 CONNECTOR R1-1617 LOOSE RESECURED REPLACED BUNK LIGHT PN BR9741-801-003-F OPS CHECK NORMAL. (7805481)

Part: BATTERY PACK — ODOR · airframe 84,270 hrs · 16,591 cycles

SHIP 1805 CREW REPORTED STRONG ELECTRICAL TYPE ODOR. ROWS 46-48 OVERHEAD CAPTS SIDE STRONGEST CONCENTRATION. SECURED IFE, DIMMED LIGHTS ODOR DECREASED SIGNF. BALANCE OF FLIGHT NO FURTHER ODORS. CORRECTIVE ACTION: R/R EMERGENCY LIGHT BATTERY PACK (M738) REF B767 AMM 33-51. OPS CHK GOOD. NO DEFECTS NOTED AT THIS TIME. R/R SEAT 47AB READING LIGHT UNIT PER B767 AMM 33-23. OPS CHK GOOD. (8766884)

Part: BATTERY PACK — INOPERATIVE · airframe 84,270 hrs · 16,591 cycles

SHIP 1805 LCR EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: R/R LLCR EMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY. REF B767 AMM 33-51. OPS CKS GOOD. (8766888)

Part: NONE — NONE · airframe 84,051 hrs · 16,557 cycles

SHIP 1805 2L DOOR ARMING BUTTON STUCK IN ARMING POSITION, CORRECTIVE ACTION: ADJUST DOOR ARMING BUTTON ON 2L DOOR PER B767-400 AMM 52-11. OPS CHK GOOD (8519680)

Part: NONE — NONE · airframe 83,994 hrs · 16,547 cycles

SHIP 1805 -DIV- TO JFK DUE TO LT HYD SYSTEM QTY DECREASING. CORRECTIVE ACTION: FOUND HYDRAULIC LEAK IN VERTICAL STABILIZER AT A MANIFOLD. REPLACED PACKINGS AND SECURED LINES. C/W LEAK CHECKS. A/C RTS.

Part: NONE — NONE · airframe 82,981 hrs · 16,355 cycles

SHIP 1805 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:601. CORRECTIVE ACTION: SLIDE LIGHT CHECKS GOOD, UNABLE TO FAULT ON GROUND. (2068068)

Part: SHUTOFF VALVE — LEAKING (FLAP/SLAT SYS) · airframe 82,611 hrs · 16,286 cycles

SHIP 1805 - MISC/DE - CENTER HYDRAULIC SYSTEM QUANTITY DECREASED DURING FLIGHT. C/W QRH AND LANDED AT DESTINATION WITHOUT ALTERNATE GEAR EXTEND AND SAFELY TAXIED TO GATE. CORRECTIVE ACTION: FOUND FLAP/SLAT SHUTOFF VALVE LEAKING. REPLACED FLAP/SLAP SHUTOFF VALVE AND SERVICED HYDRAULIC SYSTEM. (8089858)

Part: NONE — NONE · airframe 82,312 hrs · 16,233 cycles

SHIP 1805 SLIDE INDICATOR LIGHT INOP OR DAMAGED. CORRECTIVE ACTION: UNABLE TO DUPLICATE FAULT. LIGHT OPS CHK NML. (1999467)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,288 hrs · 16,023 cycles

SHIP 1805 DURING SERVICE CHECK OPERATION TEST OF EMERGENCY LIGHTS IN LOWER LOBE CREW REST, EMERGENCY LIGHTS DID NOT COME ON. CORRECTIVE ACTION: REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL. MCO/PLAC REMVOVED. (LP 7899803)

Part: SPRING — OUT OF POSITION (LIGHT SWITCH) · airframe 81,250 hrs · 16,015 cycles

SHIP 1805 EMERGENCY LIGHT SWITCH WASN'T TO SLIDE INTO ON POSITION WHEN GUARDED SWITCH DOWN. CORRECTIVE ACTION: REPOSITIONED SWITCH GUARD SPRING. SYSTEM OPERATION IS NORMAL. (LP 7546984)

Part: GUARD — DETERIORATED (EMERGENCY LIGHTS) · airframe 81,250 hrs · 16,015 cycles

SHIP 1805 - COCKPIT EMERGENCY LIGHTS WITCH GUARD REPORTED TO BE IN POOR CONDITION. CORRECTIVE ACTION: REPLACED SWITCH GUARD. SYSTEM OPERATION IS NORMAL. (LP 1894524)

Part: LOCK — OUT OF ADJUST (PAX DOOR) · airframe 81,250 hrs · 16,015 cycles

SHIP 1805 ENTRY DOOR HARD TO OPEN OR CLOSE. CORRECTIVE ACTION: LOCK MECHANISM ADJUSTED ON CREW DOOR. SYSTEM OPERATION IS NORMAL. (LP 1893171)

Part: LINE — LEAKING (HYD SYS) · airframe 81,008 hrs · 15,957 cycles

SHIP 1805 -ATB- DUE TO RMLG DOOR OPEN INDICATION WITH LANDING GEAR SELECTED "UP". CORRECTIVE ACTION: C/W OVER WEIGHT LANDING INSPECTION. FOUND HYDRAULIC LINE LEAK AT GEAR OPERATED SEQUENCE VALVE. REPLACED LINE, GEAR OPERATED AND DOOR OPERATED SEQUENCE VALVES. NO HELP. REPLACED RIGHT GEAR SAFETY VALVE. SYSTEM OPERATION IS NORMAL. (LP 7456742)

Part: LIGHT — INTERMITTENT (COCKPIT) · airframe 80,775 hrs · 15,892 cycles

SHIP 1805 COCKPIT EMERGENCY EXIT LIGHT FLASHES ON AND OFF THROUGHOUT FLIGHT DISTRACTING ESPECIALLY AT NIGHT ON LANDING. CORRECTIVE ACTION: RESET EMERGENCY LIGHT SYSTEM, OPERATION IS NORMAL. (LP 7310738)

Part: INDICATOR — OUT OF ALIGNMENT (SLIDE) · airframe 80,732 hrs · 15,881 cycles

SHIP 1805 SLIDE INDICATOR LIGHT INOPERATIVE. CORRECTIVE ACTION: MAINTENANCE FOUND LIGHT ASSEMBLY6 LOOSE AND MISALIGNED. RESET LIGHT ASSEMBLY. SYSTEM OPERATION IS NORMAL. (LP 1837193)

Part: SEAL — CRACKED (RUDDER FAIRING) · airframe 80,439 hrs · 15,809 cycles

SHIP 1805 CRACK ON RUDDER FAIRING SEAL. ON 324KL PANEL. REPAIRED PER ERA 591739-14. (LP 7380111)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,302 hrs · 15,560 cycles

CREW REST EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE INSTALLED EMERGENCY LIGHT BATTERY. MCO/PLAC REMOVED. SYSTEM OPERATION IS NORMAL.

Part: SKIN — CRACKED (BS 1654) · airframe 78,676 hrs · 15,384 cycles

DURING INSPECTION FOUND CRACK ON SKIN AT STA 1654 S-3L. CRACK REPAIRED, PER ERA 588064-14.

Part: SKIN — CRACKED (BS 1654) · airframe 78,676 hrs · 15,384 cycles

DURING INSPECTION FOUND A CRACK ON SKIN AT STA 1654 S-3R. C/W ERA 588065-14.

Part: BEAM — CORRODED (APU DOOR) · corrosion level 2 · airframe 78,676 hrs · 15,384 cycles

CORROSION LEVEL 2, DURING INSPECTION FOUND LEFT APU ACCESS DOOR FORWARD BEAM LOWER SIDE CORRODED. REPLACED BEAM.

Part: DOOR — CORRODED (APU BAY) · corrosion level 2 · airframe 78,676 hrs · 15,384 cycles

CORROSION LEVEL 2, DURING INSPECTION FOUND CORROSION ON LT APU ACCESS DOOR AT FORWARD BEAM LOWER ANGLE. ANGLE REPLACED.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 78,676 hrs · 15,384 cycles

DURING INSPECTION FOUND CORROSION ON CABIN FLOOR PANELS INSERTS AT BS 303 TO BS 355. REPLACED FLOOR PANEL.

Part: FLANGE — CRACKED (NR 2 NACELLE) · airframe 78,676 hrs · 15,384 cycles

DURING INSPECTION FOUND NR 2 PLYLON INBOARD HORIZONTAL FLANGE CRAKED AT NAC STA 230. REPAIRED, PER ERA 587941-14.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · corrosion level 2 · airframe 78,676 hrs · 15,384 cycles

DURING INSPECTION FOUND CORROSION ON CABIN FLOOR PANELS AT BS 303 TO BS 355. REPLACED FLOOR PANELS.

Part: FLANGE — CRACKED (NR 1 NACELLE) · airframe 78,676 hrs · 15,384 cycles

DURING INSPECTION FOUND NR 1 PYLON STRUT UPPER SPAR HORIZONTAL FLANGE RT SIDE ED CRACKED AT N STA 230. REPAIRED, PER ERA 587940-14.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 78,650 hrs · 15,378 cycles

DURING INSPECTION, FOUND FLIGHT DECK EMERGENCY LIGHTS INOPERATIVE. CORRECTIVE ACTION: REPLACED LIGHT ASSEMBLY, SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 78,650 hrs · 15,377 cycles

DURING INSPECTION FOUND SEVERAL CABIN EMERGENCY LIGHT SECTIONS FAILED. REPLACED BATTERY PACKS AT M1208, M6759, M7236 AND M737. SYSTEM OPERATION IS GOOD.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 78,569 hrs · 15,365 cycles

L2 DOOR EXT. EMERGENCY LIGHT INOP R767ELAMP. NO HELP. REPLACED BATT. FUSE NBR 4 CKS GOOD. REF. B767-400 AMM 33-51 (7213996)

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 77,862 hrs · 15,280 cycles

SEAT MOUNTED EMER LTS INOP FROM SEAT 6A TO L2 DOOR. C/A REP. PWR SUPPLY AND BATTERY PACK M7235 REF B767-400 M/M 33-51. LTS OPS CK GOOD (5372307)

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 77,308 hrs · 15,209 cycles

FOUND DURING SERVICE CHECK EMERGENCY LIGHTS AT SEAT 31-43AB ARE INOPERATIVE. FOUND CONNECTORS LOOSE AT SEATS 31AB AND 43AB REINSTALLED AND SECURED. SYSTEM OPEATION IS NORMAL.

Part: SEAL — BURNED (GALLEY OVEN) · airframe 74,693 hrs · 14,853 cycles

IN FLIGHT SLIGHT SMELL COMING FROM FRONT GALLEY OVEN. OVENS SHUTOFF, WARMING BINS SHUTOFF SMELL DISSIPATED. FOUND # AND #3 DOOR SEAL BURNT DAMAGE. REPLACED #1 FORWARD GALLEY OVEN.

Part: SKIN — CRACKED (BS 1654) · airframe 74,402 hrs · 14,811 cycles

SKIN STA 1654, S13AR CRACKED. C/W E/RA 567634-14.

Part: RELAY — FAILED (GROUND SERVICE) · airframe 73,971 hrs · 14,750 cycles

SHIP 1805 -FUME- WHILE AT THE GATE, APU WAS ON LINE AND THE RAMP PULLED EXTERNAL POWER. THERE WAS A BURNING ELECTRICAL SMELL IN THE COCKPIT AND FORWARD GALLEY. SEVERAL CB'S TRIPPED IN THE COCKPIT. CORRECTIVE ACTION: INSPECTION OF WIRES/ TERMINAL LUGS OK. R/R K102 GROUND SERVICE TRANSFER RELAY. SYSTEM OPERATION IS NORMAL.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,799 hrs · 14,718 cycles

THE FLOORBEAM LOWER CHORD CRACKED IN AFT CARGO AT STA 1439 LBL 28.0 AND REPAIRED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 73,799 hrs · 14,718 cycles

CARGO FLOOR STRUCTURE SPLICE ANGLE FOUND CRACK IN AFT CARGO AT STA 1087 LBL 44. C/W ERA 574872-14.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,799 hrs · 14,718 cycles

CORROSION LEVEL: 2 CABIN R1 DOOR CUTOUT LOWER EDGE FLOOR SUPPORT FOUND CORROSION AT STA 300-310. AREA REPLACED.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 73,799 hrs · 14,718 cycles

HFEC INSPECTION FOUND 01EA CRACK APPROX 0.400" IN LENGTH AT THE SPECIAL ATTENTION FASTENER ON THE VERTICAL FLANGE OF RIGHT HORIZONTAL INNER CHORD. REPAIRED PER SRM 53-80-08.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,799 hrs · 14,718 cycles

CORROSION LEVEL: 2 SEAT TRACK-CABIN SEAT TRACK AT STA 1208.5-1428 RBL 88.5 FOUND CORROSION REPLACED PER ERA 574290-14. (LP 0913450)

Part: STIFFENER — CRACKED (NLG WW) · airframe 73,799 hrs · 14,718 cycles

MFEC INSPECTION FOUND 01EA CRACK APPROK 0.350" IN LENGTH ON LT NOSE WHEEL WELL VERTICAL STIFFENER. STIFFENER REPAIRED. (LP 0913504)

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,799 hrs · 14,718 cycles

HFEC INSPECTION FOUND 01EA CRACK APPROX 0.250" IN LENGTH ON THE FUSELAGE SKIN AROUND THE 9TH STRINGER-ATTACH RIVET ALONG S-14AR, AFT OF FRAME 1629. REPAIRED PER SRM 53-80-01. (LP 0913918)

Part: SKIN — CORRODED (BS 1582) · corrosion level 2 · airframe 73,816 hrs · 14,723 cycles

DURING HCK, CORROSION WAS FOUND ON THE FUSELAGE SKIN, STA 1582, S-25L. C/W ERA 574358-14. (LP 0912182)

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,799 hrs · 14,718 cycles

CORROSION LEVEL: 2 LT FUSELAGE SKIN AT STA1582/S-25L FOUND CORROSION. REPAIRED PER ERA 574358-14. (LP 0896455)

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,799 hrs · 14,718 cycles

HFEC INSPECTION FOUND 01EA CRACK APPROX 0.450" IN LENGTH ON THE FUSELAGE SKIN AROUND THE 13TH STRINGER-ATTACH RIVET ALONG S-14AR, AFT OF FRAME 1629 REPAIRED PER SRM 53-80-01. (LP 0889834)

Part: FUSE — FAILED (EMERGENCY LIGHT) · airframe 72,184 hrs · 14,494 cycles

EMERGENCY LIGHTS AT THE L4 DOOR HEADER WAS INOPERATIVE. REPLACED THE FUSE AT M739 POWER SUPPLY. SYSTEM OPS NORMAL.

Part: BRACKET — BENT · airframe 71,182 hrs · 14,362 cycles

EMERGENCY EXIT LIGHTS CAME ON DURING TAXING OUT AND EXTINGUISHED WHEN THE ARM SWITCH WAS CYCLED. LATER IN FLIGHT, PORTIONS OF EMERGENCY LIGHTS CAME ON RANDOMLY. FOUND R1S196 RIGHT FORWARD DOOR CLOSED SENSOR BRACKET BENT AND OUT OF PROXY. REPLACED S196 BRACKET AND ADJUSTED. THE SYSTEM OPS NORMAL.

Part: STRINGER — CRACKED (BS 1654) · airframe 70,512 hrs · 14,276 cycles

DURING A CRACK INSPECTION, FOUND THE SKIN AT BS 1654, STRINGER 13AR CRACKED AND IS APPROXIMATELY 6 INCHES AND BEYOND THE 5 INCH CRACK LIMIT OF SRM 53-80-01. REPAIRED IAW SRM 53-80-01.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,495 hrs · 14,274 cycles

DURING ACCOMPLISHMENT OF WORK CARD FOUND CRACK ON STR13 LEFT SIDE APPROXIMATELY 2" LONG, STARTING AT APPROXIMATELY STA 1660 C/W SRM 53-80-01.

Part: SKIN — CRACKED (BS 1654) · airframe 74,386 hrs · 14,809 cycles

DURING A CRACK INSPECTION, FOUND A CRACK JUST AFT OF STATION 1654.5 ALONG STR 13AR. THE CRACK IS APPROXIMATELY 6 AND BEYOND THE 5 CRACK LIMIT. REPAIRED PER SRM 53-80-01 REPAIR 7

Part: STRINGER — CRACKED (FUSELAGE) · airframe 70,495 hrs · 14,274 cycles

DURING ACCOMPLISHMENT OF WORK CARD 5320-01229-01B, FOUND CRACK ON STR 13R SIDE, APPROX 6 INCHES LONG STARTING AT APPROX STA 1658. REMOVED EXISTING FASTENER AND CUTOUT DAMAGE C/W SRM 53-80-01 AND ERA 567634-14.

Part: SENSOR — MALFUNCTIONED (R1 DOOR) · airframe 69,225 hrs · 14,084 cycles

1R DOOR SHOWING NOT CLOSED AND SLIDE LIGHT FLASHING. RPLCD SENSOR S196-DOOR IND CK OK AND SLIDE IND OK, MM 52-71.

Part: CONNECTOR — DIRTY (LE SLAT) · airframe 69,164 hrs · 14,076 cycles

ATB DUE TO L/E ASYMMETRY MSG ILLUMINATED. NO FLIGHT CONTROL ISSUES. CREW DECLARED AN EMERGENCY AND LANDED APPROXIMATELY 66,000 LBS. OVER WEIGHT. BITE OF PSEU SHOWED ONLY SENSOR S277 NR 2 SLAT OB AT FAULT. NO OTHER FAULTS NOTED. PERFORMED W/C 2780-7590 FOUND S277 RESISTANCE HIGH ON ELEC BREAKOUT BOX. R&R LEADING EDGE SLAT SENSOR SWITCH S277 PER AMM 27-88 AND TARGET SENSOR PER AMM 27-88. RESISTANCE STILL HIGH. CHECKED RESISTANCE FROM D4434P TO BREAKOUT BOX 4.7 OHMS. CLEANED CONNECTORS 4434J. RESISTANCE GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 69,129 hrs · 14,068 cycles

EMERGENCY EXIT SIGNS A THE L4 & R4 DOORS ATTACHED TO THE BATTERY CHARGER M1210 WILL NOT TEST WITH THE PUSH TO TEST SWITCHES. R & R THE BATTERY CHARGER IAW AMM 33-51. HAD A GROUND ON PIN 8M CONNECTOR D10722. TROUBLESHOT IAW WDM 33-51-11, FOUND OPEN ON WIRE W836-008-22. APPROX. 3 FEET DOWN RUN. TROUBLESHOT IAW WDM 33-51-11, FOUND CONNECTOR D10722 WIRE PIN 8 BROKEN BEHIND SIDEWALL PANEL AT THE R4 DOOR & PIN 4 WIRE DAMAGED. PERFORMED ENVIRONMENTAL SPLICE ON WIRE W836-008-22 & WIRE W836-004-22 IAW SWPM 20-30. NOW EMERGENCY LIGHT TEST FUNCTIONS. OPS CHECKED GOOD IAW AMM 33-51.

Part: BATTERY — DISCHARGED (CABIN) · airframe 68,924 hrs · 14,044 cycles

EMERGENCY EXIT SIGNS AT 4 L&R ATTACHED TO BATT CHARGER M1210 WILL NOT TEST WITH PTT SWITCH. REPLACED POWER SUPPLY M1210 BATTERY REF AMM 33-51. OPS CHECK GOOD. OK FOR SVC.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 68,924 hrs · 14,044 cycles

PATH LIGHTS 38-45 F & G INOP. R&R BATT CHARGER PER AMM 33-51. OPS CK NML. OK FOR SVC.

Part: SEAL — OUT OF POSITION (R1 DOOR) · airframe 68,658 hrs · 14,010 cycles

SEAL AT THE R1 DOOR FOUND OUT OF POSITION. CORRECTLY REPOSITIONED THE SEAL.

Part: IDG — MALFUNCTIONED (NR 2) · airframe 68,383 hrs · 13,969 cycles

RECEIVED A RT GENERATOR EICAS AND RT GENERATOR DRIVE EICAS. ABOUT ONE MINUTE AFTER, NOTICED ELECTRICAL (MOTOR RUNNING HOT) ODOR. DISSIPATED AFTER 20 SECONDS. THERE WAS ALSO FO AND CAPT STATUS MESSAGES FLASHING AND A PULSING IN THE YOLK. AS THE ODOR STARTED, PRESS THE RT GENERATOR DRIVE SWITCH IAW CHECK LIST AND THE APU STARTED, EVERYTHING RETURNED TO NORMAL. TROUBLESHOT IAW FIM 24-20-02, REMOVED AND REPLACED THE NR 2 ENGINE IDG IAW AMM 24-11-01. INSPECTED THE COCKPIT, OVERHEAD AND AISLE STAND PANELS, P6 PANEL AND E / E POWER PANELS FOR SMOKE OR DAMAGE, NO DAMAGE FOUND. PERFORMED AC POWER SYS TEST IAW MM 24-22 AND INST BUSS VOLTAGE SENSING UNIT TEST IAW AMM 24-51, ALL CHECKED NORMAL. A/P HAS NO LAST LEG FAULTS, TEST 40 IAW MCDP CHECKED GOOD, RAN ENG THRU ALL POWER SETTINGS WITH ALL ACFT SYSTEMS OPERATING, NO FAULTS NOTED. R & R RT GCU IAW AMM 24-22.

Part: ELECTRICAL SYS — UNKNOWN · airframe 68,381 hrs · 13,966 cycles

RETURNED TO DEPARTURE DUE TO A SUSPECTED ELECTRICAL PROBLEM, CAUSING FLICKERING LIGHTS AND PULSATING IN THE CONTROL COLUMN. PERFORMED A STDBY POWER SYS OPS TEST WITH NTF. REPLACED THE BATTERY AND CHARGER, LEFT TRU, RELAYS K105 AND K109. RAN LEFT ENGINE WITH ALL ELECTRICAL LOAD, NTF. BITE TEST OF BPCU, TESTED OK. VERIFICATION FLIGHT GOOD.

Part: SEAL — UNSECURE (R1 DOOR) · airframe 68,002 hrs · 13,918 cycles

R1 DOOR SEAL LEAKING . REINSTALLED AND SECURED THE SEAL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 66,890 hrs · 13,775 cycles

DURING A SERVICE CHECK OF CABIN EMERGENCY LIGHTS, FOUND SEAT ROWS 30AB TO 37AB EMERGENCY LIGHTS OUT. FOUND TWO EMERGENCY LIGHT CONNECTORS DISCONNECTED UNDER SEAT 30B-RECONNECTED THE CONNECTORS AND OPS OK IAW AMM 33-50.

Part: LENS — DAMAGED (EXTERIOR LIGHT) · airframe 65,348 hrs · 13,575 cycles

FWD DOOR 2R EMERGENCY LT LENS DAMAGED (EXTERIOR). REMOVED AND REPLACED 2R DOOR EMERGENCY LIGHT LENS PER AMM 33-51.

Part: STRUCTURE — DAMAGED (NACELLE) · airframe 65,295 hrs · 13,567 cycles

HOLES ELONGATED ALONG FWD EDGE OF GENERATOR CABLE PASS THROUGH CUTOUT APPROX NACELLE STA 227 NBR 1 PYLON UPPER SURFACE. REPAIRED PER PRI 553929-14 REV 0-3. PRI 553929-14 REV 0-3 INSTRUCTIONS MATCH FINAL ERA 553929-14 REV A INSTRUCTIONS. (2844045)

Part: STRUCTURE — CRACKED (PLYON) · airframe 65,295 hrs · 13,567 cycles

PYLON CRACKED AT CUTOUT WHERE POWER FEED WIRES PASS THRU TO UPPER PYLON. REMOVED AND REINSTALLED O/B T/R ON AMDS 7831-4202. PRI 553929-14 INSTRUCTIONS REV. 0-4 MATCH FINAL ERA 553929-14 REV. A INSTRUCTIONS. (2844042)

Part: FAILSAFE — CRACKED · airframe 65,295 hrs · 13,567 cycles

BHEC IAW STEP 2 OF 5312-01170-10A-02 REVEALS A CRACK INDICATION IN LOWER HOLE OF INSPECTED AREA IN LT FAILSAFE STRAP ONLY. REPAIRED IAW AMDS CARD 5312-01170-10A-02.

Part: FAILSAFE — CRACKED · airframe 65,295 hrs · 13,567 cycles

ULTRASONIC INSPECTION IAW STEP 8 SHOWS A CRACK INDICATION IN THE FAILSAFE STRAP. REPAIRED IAW AMDS 5312-01170-10A.

Part: FASTENER — DAMAGED (FUSELAGE) · airframe 65,113 hrs · 13,537 cycles

LIGHTNING STRIKE AT STA 382, STR 29L. REMOVED DAMAGED FASTENER, PERFORMED DETAIL VISUAL INSP, TREATED AREA, INSTALLED BLIND FASTENER AND PAINTED AREA PER SRM 53-00-01, FIG 201, REPAIR 8 SECT II. NEEDS REPETITIVE INSP EVERY 1500 CYCLES AND PERM REPAIR REQUIRED AT 6000 FLT CYCLES. CATEGORY C REPAIR.

Part: FASTENER — DAMAGED (FUSELAGE) · airframe 65,113 hrs · 13,537 cycles

LIGHTNING STRIKE AT STA 385, STR 28L. REMOVED DAMAGED FASTENER, PERFORMED DETAIL VISUAL INSP, TREATED AND PAINTED AREA, INSTALLED BLIND FASTENER PER SRM 53-00-01, FIG 201, REPAIR 8, SECT II. NEEDS REPETITIVE INSP EVERY 1500 CYCLES AND PERM REPAIR REQUIRED AT 6000 FLT CYCLES. CATEGORY C REPAIR.

Part: SWITCH — STUCK (LIGHT) · airframe 64,571 hrs · 13,469 cycles

ATB DUE TO ELECTRICAL ARCING AND ELECTRICAL SMELL IN OVERHEAD PANEL. CREW NOTICED THE RIGHT TURN OFF LIGHT SWITCH IN THE OVERHEAD PANEL ARCHING, AND TRIED TO TURN IT OFF, BUT IT WAS STUCK IN THE ON POSITION. FOLLOWED THE QRH FOR OVERWEIGHT LANDING, NO EMERGENCY WAS DECLARED. DID NOT DON THE OXYGEN MASKS. FOUND RT RUNWAY TURNOFF LIGHT SWITCH STUCK IN THE ON POSITION AND ARCING WHEN YOU TRIED TO MOVE IT. PULLED C/B AND REPLACED TAXI TURNOFF LIGHT SWITCH PANEL PER B767-400 AMM 33-42. CLOSED C/B AND OPS CK OF ALL LIGHTS GOOD. INSPECTED SURROUNDING AREA WITH NO DEFECTS FOUND. CH 33-41 NBR 99 ON RI

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 59,909 hrs · 12,893 cycles

EMERGENCY LIGHT AT SEATS 16G THRU 21G INOPERATIVE. RESEATED OUTPUT PLUG AT 15G ALL OPS NORMAL.

Part: STRUT — DAMAGED (RT MLG) · airframe 58,058 hrs · 12,658 cycles

RT MLG TRUCK ASSY DAMAGED. R & R PISTON ASSY AND TRUCK ASSY IAW CMM 32-11-36, REV 21.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 57,840 hrs · 12,632 cycles

EMERGENCY LIGHTS INOPERATIVE ROWS 31-37 RT AND LT. FOUND CONNECTOR DISCONNECTED. SECURED THE CONNECTOR. CHECKED GOOD.

Part: SKIN — CRACKED (RT WING) · airframe 56,079 hrs · 12,415 cycles

DURING C-CHECK IAW AA 5724-01005, FOUND CRACK INDICATIONS AT SEVERAL FASTENER HOLES IN THE RT UPPER WING SKIN PITCH LOAD FITTING ATTACHMENTS. REPAIRED E/R A531784-14AD.

Part: SKIN — CORRODED (BS 1197) · airframe 48,911 hrs · 11,523 cycles

FOUND CORROSION HOLE 4 INCHES FWD OF BS 1197+154 AND 3 INCHES ABOVE STR 31R. REMOVED CORROSION LEAVING ABOUT 2.5 INCHES LONG BY ABOUT 1 INCH HIGH HOLE. PERFORMED HFEC IAW NDTSPM 06-01-10 PART 6 CORROSION CONTAINED, NO CRACKS NOTED FOR CUTOUT. FABRICATED DOUBLER IAW SRM 53-00-01, REPAIR 14. FINISHED SIZING HOLES. CONTOURED DOUBLER INSTALLED WET, TREATED AND PRIMED, MARKED REPAIR AS SRM 53-00-01, REPAIR 14, DATED AND PAINTED. RE-INSTALLED ACCESS IN AFT CARGO.

Part: SKIN — CORRODED (BS 955) · corrosion level 2 · airframe 48,024 hrs · 11,414 cycles

RT STA 955 UNDER REPAIR PROCESS AFTER FAIL SAFE STRAP TRIMMED OFF FUSELAGE SKIN FOUND CORROSION. TRIMMED OFF AREA FUSELAGE SKIN CORRODED AREA SPOT FACE AND BLEED MAKE DISK FILLER AND INSTALL ACCOMPLISHED IAW ER/A 511797-14AD, REV ORIG.

Part: FAILSAFE — CRACKED (BS 955) · airframe 48,024 hrs · 11,414 cycles

RT BS 955 REAR SPAR BULKHEAD FITTING AREA CRACK FOUND AT FAIL SAFE STRAP DETAIL REFER ATTACHED FIG. REPAIRED AMM 51-31-01, SRM 51-40-02, SWPM 20-10-00, AMM 32-35-10, AMM20-11-00, SRM 51-40-05, SRM51-20-01, AMM 51-21-10, AMM 51-31-06, AMM 27-11-00, AMM 05-51-24, ER/A 511797-14AD ACCOMPLISHED. ASSOCIATED ER/A 14-511797, ADDED FOR AC 1805.

Part: STIFFENER — CORRODED (BS 955) · corrosion level 2 · airframe 48,024 hrs · 11,414 cycles

RT BS 955 FAIL SAFE STRAP AREA TEE STIFFENER FOUND CORROSION. C/A TEE STIFFENER REPLACED AND INSTALLED IAW ER/A 511797-14AD REV ORIG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 48,024 hrs · 11,414 cycles

INBD MAIN FLAP OTBD L/E FAIRING FOUND DELAMINATED, REPAIRED CARRIED OUT IAW SRM 57-53-01, REPAIR FIG 201, TABLE 1.

Part: FLOORBEAM — CORRODED (BS 325) · corrosion level 2 · airframe 48,024 hrs · 11,414 cycles

BS 325, RBL 11 TO RBL 55 FLOORBEAM CORRODED. REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201.

Part: FAIRING — DELAMINATED (LT WING TE FLAP) · airframe 48,024 hrs · 11,414 cycles

LT WING OTBD FLAP INBD L/E FAIRING FOUND DELAMINATED. REPAIRED IAW SRM 57-53-01 REPAIR 1, TABLE 1 AND SRM 51-70-05, PAR 5C, FIG 2.

Part: FAIRING — DELAMINATED (TE FLAPS) · airframe 48,024 hrs · 11,414 cycles

INBD MAIN FLAP OTBD L/E FAIRING FOUND DELAMINATED. REPAIRED IAW SRM 57-53-01, REPAIR 1, TABLE 1 AND SRM 51-70-05, PAR 5A.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 47,985 hrs · 11,409 cycles

EMERGENCY EXIT SIGNS IN FWD GALLEY ILLUMINATE WITH SWITCH IN OFF POSITION. REPAIRED DAMAGED WIRES NEAR M1208, REF SPWM CH 20. OPS CK OK.

Part: FUSE — BLOWN (BATTERY CHARGER) · airframe 40,782 hrs · 10,523 cycles

MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE BETWEEN SEATS 1A AND 5A. MAINTENANCE INSPECTED AND REPLACED CHARGER FUSES PER AMM. OPERATIONAL CHECK WAS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,676 hrs · 10,254 cycles

SEAT MOUNTED EMERGENCY ESCAPE PATH MARKER IS INOPERATIVE AT SEAT 37B. MAINTENANCE RE-LAMPED. HOWEVER PROBLEM STILL PERSISTED. IT IS CURRENTLY MEL'D PER 33-51-03A.

Part: PANEL — MISSING (FUSELAGE) · airframe 38,528 hrs · 10,236 cycles

PANEL 149AL MISSING FROM AIRCRAFT, INSTALLING ERA 490445-14.

Part: CONNECTOR — LOOSE (CABIN) · airframe 37,267 hrs · 10,069 cycles

EMERGENCY PATH LIGHTS AT 37A ARE INOPERATIVE. MAINTENANCE FOUND A CONNECTOR AT 37A LOOSE AND RECONNECTED. SYSTEM OPERATION IS NORMAL. (2010-D1349) (DL764103070)

Part: WARNING SYSTEM — INOPERATIVE (DOOR L1) · airframe 34,654 hrs · 9,716 cycles

THE TAKEOFF WAS SAFELY ABORTED AT 80 KTS AFTER THE FLIGHT CREW RECEIVED AN EICAS MESSAGE THAT THE LT FWD ENTRY DOOR WAS NOT CLOSED SECURELY. THE ACFT CLEARED THE ACTIVE RUNWAY AND TAXIED BACK WHERE MX WAS ABLE TO COMPLETE A THOROUGH CHECK OF THE DOOR AND INDICATION SYS. THE DOOR WAS VERIFIED CLOSED AND THE DOOR WARNING SYS WAS PLACED ON MCO. ACFT RETURNED TO REVENUE SERVICE.

Part: OVEN — ODOR (AFT GALLEY) · airframe 33,922 hrs · 9,620 cycles

STRONG ODOR FROM NBR 4 OVEN IN AFT GALLEY. PULLED ALL CBS AS A PRECAUTION. SMELL DISAPPATED. RAN ALL OVENS FOR 2 HOURS. NO TROUBLE FOUND. ETOPS CATEGORY 'E': PROBLEMS WITH SYS CRITICAL TO ETOPS.

Part: WARNING SYSTEM — MALFUNCTIONED (BLEED AIR SYS) · airframe 32,629 hrs · 9,444 cycles

RTB DUE TO RT BLEED FAMV STATUS MESSAGE. HAPPENED DURING ENG START PWR SWAP. PERFORMED ASCTU RESET AND CYCLED C/BS. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: ISOLATION VALVE — INOPERATIVE (AC BAY) · airframe 31,727 hrs · 9,324 cycles

RIGHT ISOLATION VALVE INOP. REPLACED RIGHT ISOLATION PER M/M CHECKS OK.

Part: TRANSCEIVER — INOPERATIVE (WX RADAR) · airframe 31,585 hrs · 9,303 cycles

WX FAIL MSG ON F/OS PFD FOLLOWED BY STATUS PROMPT WITH MSGS WXR SYS AND L DPC. R & R WX RADAR TRANSCEIVER PER AMM. OPS CKS OK RESET L-PDC AND DCU BRAKERS RAN BITE TEST NO FAULTS. MSG CLEARED. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK.

Part: TRUNNION — CORRODED (FUSELAGE) · airframe 31,547 hrs · 9,297 cycles

DURING A TRIPLE GEAR CHANGE IN ATLANTA, MAINTENANCE FOUND CORROSION ON THE OTBD WALL OF THE RT NLG TRUNNION FITTING. THE MAXIMUM DEPTH OF THE CORROSION WAS .030 INCH. THE CORROSION WAS REMOVED AND REPAIRED PER ER/A 475224-14.

Part: IDG — MALFUNCTIONED (RT ENGINE) · airframe 28,836 hrs · 8,690 cycles

RT ENGINE IDG DID NOT COME ON LINE AFTER START. RESET BPCU RAN ENG CHKS OK.

Part: COMPUTER — MALFUNCTIONED (ELEVATOR FEEL) · airframe 28,755 hrs · 8,677 cycles

ELEVATOR FEEL EICAS MESSAGE DURING CLIMB-OUT. REPLACED ELEV FEEL COMPUTER PER AMM. LEAK CK OK. ADJ AND TEST CK OK PER 767-400 AMM. MFG NR 162900-100.

Part: COMPRESSOR — FAILED (NR 2 ENGINE) · airframe 25,814 hrs · 8,095 cycles

ATB DUE NR 2 ENGINE SURGE ENGINE WAS NOT SHUTDOWN C/FOUND METAL IN TAILPIPE. REPLACED NR 2 ENG. REPLACED RIGHT ENGINE.

Part: UNKNOWN — UNKNOWN · airframe 23,310 hrs · 7,578 cycles

R ENG FAN VIBRATION CYCLED CONTINUOUSLY BETWEEN 0.0 AND 5.00 ON TAXI OUT AND RTN TO GATE. NO VIB WAS FELT. ENG WAS STABILIZED AT IDLE. INSP INLET AND EXH AND CHIP DET. FWD TO MCO AND PLACARD. T/S PER FIM 77-31-00 FIG 103. PERFORMED AVM BITE PROCEDURE. ALL CHECKS NORMAL. A/C OK FOR SERVICE. MCO AND PLACARD REMOVED.

Part: PANEL — CRACKED (FUSELAGE) · airframe 23,086 hrs · 7,544 cycles

MAIN EQUIPMENT CENTER P33 STANDOFF MOUNT ATTACH POINT SKIN CRACKED (UPPER RT) MISSED ITEM ON OP 24335. REMOVED P33 IQW DELTA ERA 41526-14. REPLACED AFT SKIN PNL IAW DELTA ERA 461526-14. INSTALLED P33 IAW ERA 461526-14. PERFORMED GOOD FUNCTIONAL TEST IAW DELAT ERA 461526-14, ATTACHED RFTS #S 9 17 18 ERA 461526-14 ATTACHED JPD# 12 PG 6.

Part: COMPRESSOR — DAMAGED (NR 1 ENGINE) · airframe 22,119 hrs · 7,336 cycles

ON DESCENT, RECEIVED A BLEED HPSOV AND N2 VIBS INCREASED TO 5 UNITS. INLET AND EXHAUST OK CHECK CHIP DETECTORS OK RUN ENG AGAIN VIBS RETURNED. BOROSCOPE COMPRESSOR FOUND 6TH STAGE DAMAGE. BORO AND FOUND HPC 6TH AND 7TH STAGE DAMAGE BEYOND MM LIMITS. REMOVED BOROSCOPE PLUGS B 1-5 B 1-6 NR 1 ENG. ENG REMOVAL R REPLACED NR 1 ENG PER TRANS 1RT103.

Part: SWITCH — MALFUNCTIONED (OVERHEAD PANEL) · airframe 20,343 hrs · 6,855 cycles

CABIN TEMP UNCONTROLLABLE HOT. PERFORMED RT PACK MODULE BITE, SHOWS PACK ON ALL THE TIME. RESET RT PACK ON/OFF SWT AT P-5 OVHD PANEL, PAX OPN CKS NORMAL. MCO/PLAC REMOVED.

Part: ACM — FAILED (A/C BAY) · airframe 20,050 hrs · 6,782 cycles

AT FL250 STRONG BURNING SULFER SMELL IN C/PIT AND CABIN AT FL200 L AND R PACK MODE EICAS MSG FOLLOWED BY PACK OFF EICAS MSG TURNED PACK SW OFF AT FL120 OBL REPORTED STRONG ELECTRICAL BURNING SMELL IN FWD GALLEY NO SMOKE. DECLARED EMERGENCY AND LANDED R ACM STATUS MSG ALSO APPEARED. BITE CKD ASCTU AND RT CTC BOTH BITES R ACM FAILURE FWD TO MCO/PLAC PER MEL 21-51-07 SECURED TURBINE BYPASS VLV OPEN MEL R PACK WILL REMIAN OFF ON GND AND AT LOW ALTITUDES. REPLACED RT ACM PER M/M TEST OK NO MSG MCO AND PLAC REM.

Part: BOLT — MISSING (NR 9 SLAT INBD) · airframe 17,349 hrs · 6,190 cycles

LE SLAT ASYM MSG WHILE EXTENDING FLAPS TO 15 AFTER ENG START. FOUND SLAT 9 INBD TARGET MISSING. REPLACED SAME PER M/M. OPS CK NML.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 17,317 hrs · 6,183 cycles

DURING OPN 6803 FOUND ALL 16 BATTERY PACKS TO FAIL CHECK. PACKS ARE SUPPOSED TO LAST 15 MINUTES, LONGEST PACK LASTED 6 MINUTES. REPLACED 16 BATTERY PACKS, OPS CHECKS NORMAL. S/N'S LISTED BELOW 1) M730/12305, 2) M6756/12304, 3) M6757/12317, 4) M6758/51239, 5) M1208/9630, 6) M736/12303, 7) M7235/11706, 8) M6759/60867, 9) M732/20423, 10) M6760/9335, 11) M734/9384, 12) M1210/12980, 13) M737/17916, 14) M7236/12023, 15) M738/9417, 16) M739/9384.

Part: TARGET — BROKEN (NR 8 SLAT) · airframe 15,563 hrs · 5,760 cycles

LE SLATS WOULD NOT EXTEND. FOUND S304 NR 8 OUTBOARD SENSOR TARGET BROKEN. REPLACED BOLT OPS CK OK.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,846 hrs · 5,547 cycles

EMERGENCY TRACK LIGHTS INOP FROM 25FG TO 32 FG. FOUND BATT CHARGER BAD AT 29 FG SIDEWALL AND REPAIRED SHORTED WIRE AT ROW 25 FG SIDEWALL. OPS CK NORMAL . ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: LAMP — SHORTED (SEAT ROW 22 ABC) · airframe 13,710 hrs · 5,211 cycles

WORKING ETOPS PRE-DEPARTURE CHECK FOUND EMERGENCY EXIT LIGHTS AT SEAT ROWS 17 ABC TO 24 ABC INOP. REPLACED SHORTED TRACK LIGHT LAMP AT 22 ABC.

Part: GENERATOR — INOPERATIVE (NR 1 ENGINE) · airframe 11,864 hrs · 4,614 cycles

LEFT GEN DRIVE LIGHT CAME ON AFTER TAKEOFF AND IDG WAS SUBSEQUENTLY DISCONNECTED ACCORDING TO THE QRH. BPCU FAULTED LEFT GEN OVER FREQ CODE 24-355-01 AND 24-314-11 OVER FREQ. REPLACED LEFT GCU. RAN ENGINE, LEFT ENG GEN SYS CHECK NORMAL.

Part: POWER SUPPLY — INOPERATIVE (SLIDE LIGHT) · airframe 10,224 hrs · 4,116 cycles

DURING PRE-DEPARTURE CHECK AFTER FLIGHT 225, FOUND 2L DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOP. REBULBED, NO HELP. REPLACED POWER SUPPLY M6759. EXTERIOR EMERGENCY SLIDE LIGHT AT 2L CHECK OK.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 8,107 hrs · 3,354 cycles

SEAT MOUNTED EMERGENCY EXIT LIGHTS INOP FROM ROW 22AB TO 25AB. FOUND EMERGENCY LIGHT WIRE UNPLUGGED UNDER SEAT 22B. RECONNECTED SAME, OPS CKS GOOD.

Part: ENGINE — FAILED (NR 1) · airframe 7,578 hrs · 3,143 cycles

ON TAKEOFF ROLL, BETWEEN 30 AND 50 KTS, POWER STABILIZED AT ALTENATE 60, HEARD LOUD BANG AND CONTINUOUS RUMBLE. TAKEOFF ABORTED. ENGINE INSTRUMENTS LOOKED NORMAL. PASSENGERS REPORTED SEEING FLASH OF FLAME ON THE LEFT SIDE OF THE AIRCRAFT. FOUND METAL IN TAIL PIPE. NR 1 ENG REPLACED PER TRANS 14T1

Part: INDICATOR — FAILED (COCKPIT) · airframe 4,589 hrs · 1,899 cycles

STANDBY ATTITUDE INDICATOR WILL NOT STAY ERECT. REPLACED INDICATOR.

Part: DUCT — CRACKED (APU) · airframe 4,527 hrs · 1,856 cycles

APU PNEUMATIC T-DUCT FOUND CRACKED. FLEET PROBLEM. REMOVED AND REPLACED DUCT. LEAK CHECKS NORMAL.

Part: ACTUATOR — MALFUNCTIONED (T/E FLAP) · airframe 4,521 hrs · 1,850 cycles

AFTER T/O FLAP RETRACTION, T/E FLAP DISAGREE EICAS MSG. RAISED FLAPS USING ATLN SYS. FOUND NR 6 ROTARY ACTUATOR TRIPPED. CYCLED FLAPS SEVERAL TIMES, OPN NORMAL. REPLACED NR 6 FLAP ROTARY ACTUATOR PER AMM, CHECK NORMAL.

Part: CIRCUIT CARD — FAULTY (T/E FLAP) · airframe 4,511 hrs · 1,840 cycles

ON T/O FLL FLAP RETRACT GOT T/E FLAP DISAGREE BETWEEN 5 AND 15 DEG WITH ALT PROC FLAPS/SLATS WOULD NOT COME UP. RAN FLAPS OUT TO 20 DEG THEN AFTER 3 ATTEMPTS AND 40 MINS FLAPS RETRACTED. INSPECTED AND FOUND NO DAMAGE TO LE/TE FLAPS. REPLACED CARD M11291 ADU CONTROL. RAN FLAP/SLAT BOTH ELEC/HYD SEVERAL TIMES, NO TROUBLE FOUND. T/S PER FIM.

Part: BOLT — FAILED (L/E SLAT) · airframe 2,088 hrs · 956 cycles

LEADING EDGE SLAT TRACK BOLT FAILED ALLOWING PROX TARGET AND BEARING TO DEPART AIRCRAFT. REPLACED BOLT.

Part: OVEN — CONTAMINATED (GALLEY) · airframe 58 hrs · 65 cycles

FWD LAV SMOKE DETECTOR WENT OFF AND FWD IFE COOLING STATUS MSG. SYSTEM TURNED OFF, NO SMOKE OR FURTHER ODOR DETECTED. SYSTEM TESTS OK, NO FAULTS NOTED. IFE COOLING AND LAV DETECTION APPEAR TO HAVE PICKED UP SMELL OR SMOKE FROM NR 1 OVEN. NR 1 OVEN CLEANED.

Part: O-RING — FAILED (HYD SYSTEM) · airframe 34 hrs · 44 cycles

CREW OBSERVED THE RT HYD QTY DECREASING EN ROUTE NOTIFIED MCC 1515Z. QTY AT 1.03 DEPARTING ATL DECREASED TO .65 ON ARRIVAL FLL. FOUND RT SYS HYD LINE IN AFT BB RT FWD SIDE PALLET 20. DRIVE BAY-A- UNDER SATCOM E12 RACK AREA PANEL -O-RING FOR CK VLV DAMAGED. REPLACED O-RING, SVCD SYS PRESSURE CK NORMAL.

Part: LENS — BROKEN (ROW 20) · airframe 26 hrs · 37 cycles

EMERGENCY TRACK LIGHT LEN BROKEN OFF AT SEAT ROW 20 AB. REPLACED LIGHT AND LENS ASSY, OPS NML.