N154DL

Part: INDICATOR — DEFECTIVE (VSI) · airframe 123,372 hrs · 22,298 cycles

AFTER PARKING W/ PARKING BRAKE SET, CAPT. VSI FLICKERED AND WENT HAZY. NO EICAS, FAULT, OR CB'S NOTED. PERFORMED VISUAL INSPECT OF GALLY, COCKPIT AND CABIN LIGHTING. ALSOCHECKED RECIRCULATION FAN OPN. FOUND CAPT'S VSI INDICATOR WITH BURNT ELECT ODOR & LOOSE PARTS INSIDE. REPLACED VSI INDICATOR.

Part: QUICK DISCONNECT — DAMAGED (CABIN) · airframe 122,802 hrs · 22,206 cycles

EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT SEAT 38GF FOUND WIRE QUICK-DISCONNECT DAMAGED. CAPPED AND STOWED WIRE. FORWARD TO MEL 33-51-03A REPAIRED CONNECTOR TO LIGHT. MCO/PLAC REMOVED. SYSTEM OPERATION IS NORMAL.

Part: IDG — FAILED (LEFT) · airframe 122,692 hrs · 22,189 cycles

SHIP 1504 - DIV - TO POS AFTER LT IDG FAILED IN FLIGHT AND APU WOULD NOT START AFTER MULTIPLE ATTEMPTS. CORRECTIVE ACTION: FOUND APU INLET DOOR ACTUATOR AT FAULT. LOCKING APU DOOR IN OPEN POSITION AND WILL RUN APU INFLIGHT (LP 6677510). LT IDG PLACED ON MEL. FLIGHT TO CONTINUE TO SJU FOR CREW CHANGE AND CONTINUATION TO ATL. REPLACED APU ECB (LP 1428180), AND IDG AND IDG COOLER. LP 6677509

Part: DECODER — OVERHEATED (PSU) · airframe 122,341 hrs · 22,135 cycles

FLIGHT ATTENDANT REPORTS SMOKE IN CABIN AT 40AB. PER CREW DEBRIEF CORRECT LOCATION IS 34AB. FOUND PSU DECODER W/ INTERIOR THERMAL DAMAGE. NO ADJACENT DAMAGE. REMOVED 34AB DECODER PER ERA 583507-14 INSTALLED PSUD AT 34AB. RE-INSTALLED TERMINATION PLUG AT LAST ROW PER B767 WDM 23-34-18 AND ER/A 583507-14MULTIPLE LOCATIONS READING AND F/A CALL LIGHTS REMAIN INOP REFERENCE NEF LOG #'S 1380272 AND 1380275 FOR CORRECTIVE ACTION

Part: LAMP — ODOR (COCKPIT) · airframe 121,664 hrs · 22,038 cycles

AFTER LANDING. SLIGHT ELECTRICAL OR CHEMICAL SMELL IN COCKPIT. CONFIRMED SLIGHT SMELL FROM F/O AREA, OPENED P3,P11, PANELS, THEN GVI OF EWIS FOR BEHIND THESE PANELS, FOUND F/O'S INSTR PANEL FLOOD LIGHT ONE FLUORESCENT LAMP PIN DENT THEN RELAMPED FOR PRECAUTIONARY.

Part: SKIN — CRACKED (BS 1725) · airframe 119,441 hrs · 21,742 cycles

TAIL EXTERNAL SKIN FOUND CRACKED AT BS 1725 BUTT SPLICE S-7R CRACKED CHORD STRAP AND SKIN REPAIRED PER SRM 53-80-01. (LP 1039937)

Part: FRAME — CORRODED (BS 1197) · corrosion level 2 · airframe 119,441 hrs · 21,742 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND FRAME WEB SURFACE CORROSIONAT STA1197+66. S-38L TO S-37R. AND S-33R TO S-34R. REPLACED WEB. (LP 1039818)

Part: SHEAR TIE — CORRODED (BS 654) · corrosion level 2 · airframe 119,438 hrs · 21,741 cycles

CORROSION LEVEL: 2 -FWD CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 654+44 BETWEEN S-39R AND S-39L. REPLACED SHEAR TIE. (LP 1038420)

Part: SHEAR TIE — CORRODED (BS 764) · corrosion level 2 · airframe 119,438 hrs · 21,741 cycles

CORROSION LEVEL: 2FWD CARGO COMPARTMENT FOUND 01EA SHEAR TIE CORROSION AT STA 764 BETWEEN S-36R AND S-35R. SHEAR TIE REPLACED. (LP 1038596)

Part: SHEAR TIE — CORRODED (BS 1540) · corrosion level 2 · airframe 119,438 hrs · 21,741 cycles

CORROSION LEVEL: 2 BULK CARGO COMPARTMENT FOUND 01EA SHEAR TIE CORROSION AT STA 1540 BETWEEN S-39R AND S-38R. SHEAR TIE REPLACED. (LP 1038673)

Part: SHEAR TIE — CORRODED (BS 1219) · corrosion level 2 · airframe 119,438 hrs · 21,741 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 03EA SHEAR TIE CORROSION AT STA 1219 BETWEEN S-39R AND S-36R. REPLACED DAMAGE SHEAR TIE. (LP 1038649)

Part: SHEAR TIE — CORRODED (BS 654) · corrosion level 2 · airframe 119,438 hrs · 21,741 cycles

CORROSION LEVEL: 2FWD CARGO COMPARTMENT FOUND 04EA SHEAR TIE SURFACE CORROSION AT STA 654 BETWEEN S-39R AND S-36L . REPLACED SHEAR TIE. (LP 1038633)

Part: SHEAR TIE — CORRODED (BS 654) · corrosion level 2 · airframe 119,438 hrs · 21,741 cycles

CORROSION LEVEL: 2 FWD CARGO COMPARTMENT FOUND 02EA SHEAR TIE SURFACE CORROSION AT STA 654 BETWEEN S-38R AND S-36R. REPLACED SHEAR TIE. (LP 1038613)

Part: SHEAR TIE — CORRODED (BS 1285) · corrosion level 2 · airframe 119,438 hrs · 21,741 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 03EA SHEAR TIE CORROSION AT STA 1285 BETWEEN S-38L AND S-38R. REPLACED DAMAGED SHEAR TIE. (LP 1038658)

Part: SHEAR TIE — CORRODED (BS 1540) · corrosion level 2 · airframe 119,438 hrs · 21,741 cycles

CORROSION LEVEL: 2 BULK CARGO COMPARTMENT FOUND 01EA SHEAR TIE CORROSION AT STA 1540 BETWEEN S-39L AND S-38L. REPLACED SHEAR TIE. (LP 1038668)

Part: SHEAR TIE — CORRODED (BS 1241) · corrosion level 2 · airframe 119,438 hrs · 21,741 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 03EA SHEAR TIE CORROSION AT STA 1241 BETWEEN S-38L AND S-38R. SHEAR TIE REPLACED. (LP 1038640)

Part: SHEAR TIE — CORRODED (BS 720) · corrosion level 2 · airframe 119,438 hrs · 21,741 cycles

CORROSION LEVEL: 2 -FWD CARGO COMPARTMENT FOUND 01EA SHEAR TIE SURFACE CORROSION AT STA 720 BETWEEN S-38L AND S-37L, SHEAR TIE REPLACED. (LP 1038417)

Part: SHEAR TIE — CORRODED (BS 742) · corrosion level 2 · airframe 119,438 hrs · 21,741 cycles

CORROSION LEVEL: 2 FWD CARGO COMPARTMENT FOUND 02EA SHEAR TIE CORROSION AT STA 742 BETWEEN S-39L AND S-37L. REPLACED SHEAR TIE. (LP 1038407)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 119,438 hrs · 21,741 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE CORROSION AT STA1197+110. BETWEEN S-39R AND S-39L. SHEAR TIE REPLACED. (LP1037186)

Part: SKIN — DEBONDED (LT WING TE FLAP) · airframe 119,438 hrs · 21,741 cycles

LEFT WING O/B FLAP L/E FOUND DISBONDING AS MARK. REPAIRED PER SRM 57-53-01.

Part: SKIN — DAMAGED (RT WING) · airframe 119,438 hrs · 21,741 cycles

RH LOWER WING SKIN STRINGER L-6.5 FOUND FASTENER CODE B LOCATION NO.2 HOLE DIAMETER:0.3920" GREATER THAN 0.3185". C/W ERA 576702-14.

Part: BEAM — CRACKED (RT WING) · airframe 119,438 hrs · 21,741 cycles

FOUND RH WING L/E FRONT BEAM REPAIRED DOUBLER AT LES610 CRACK. C/W ERA 577111-14. (LP 1033977).

Part: SEAT TRACK — CORRODED (BS 1362-1518) · corrosion level 2 · airframe 119,438 hrs · 21,741 cycles

CORROSION FOUND ON SEAT TRACK RBL 11, BTW BS 1362 TO 1518. REPLACED SEAT TRACK.

Part: SHEAR TIE — CORRODED (BS 1307) · corrosion level 2 · airframe 119,438 hrs · 21,741 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 03EA SEHAR TIE CORROSION AT STA 1307. BETWEEN S-39R AND S-37L. SHEAR TIE REPLACED (LP 1037123)

Part: FITTING — CRACKED (RT WING) · airframe 119,438 hrs · 21,741 cycles

FOUND A CRACK AT RH LOWER UNDER WING LONGERON FITTING. FITTING REPLACED.

Part: SHEAR TIE — CORRODED (BS 1219) · corrosion level 2 · airframe 119,438 hrs · 21,741 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 03EA SHEAR TIE CORROSION AT STA1219. BETWEEN S-39R AND S-37L. SHEAR TIE REPLACED. (LP 1037181)

Part: SHEAR TIE — CORRODED (BS 654) · corrosion level 2 · airframe 119,438 hrs · 21,741 cycles

CORROSION LEVEL: 2FWD CARGO COMARTMENT FOUND 03EA SHEAR TIE SURFACE CORROSION AT STA654+88. BETWEEN S-38R AND S-38L. DAMAGED AREA REPLACED. (LP 1037119)

Part: SHEAR TIE — CORRODED (BS 742) · corrosion level 2 · airframe 119,438 hrs · 21,741 cycles

CORROSION LEVEL: 2 FWD CARGO COMPARTMENT FOUND 02EA SHEAR TIE CORROSION AT STA742. BETWEEN S-39R AND S-37R. REPLACED DAMAGED AREA. (LP1037171)

Part: SHEAR TIE — CORRODED (BS 1329) · corrosion level 2 · airframe 119,438 hrs · 21,741 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 02EA SHEAR TIE CORROSION AT STA1329 SHEAR TIE REPLACED. (LP 1037154)

Part: SHEAR TIE — CORRODED (BS 1307) · corrosion level 2 · airframe 119,438 hrs · 21,741 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 02EA SHEAR TIE ORROSION AT STA1307. BETWEEN S-37L AND S-35L. SHEAR TIE REPLACED. (LP 1037196)

Part: FLOORBEAM — CRACKED (BS 1395) · airframe 119,438 hrs · 21,741 cycles

AFT CARGO COMPARTMENT FOUND CABIN BEAM WEB AREA CRACK AT STA1395 BETWEEN LBL16 AND LBL19. REPAIRED PER E/RA 577045-14.

Part: BULKHEAD — CRACKED (NLG WW) · airframe 119,438 hrs · 21,741 cycles

HFEC INSPECTION CARRIED OUT.AND FOUND CRACK AT NOSE WEEL BULKHEAD CHORDS LHS. REPAIRED PER SRM 51-70-12. (LP 1025909)

Part: SEAL — DAMAGED (NR 2 ENGINE) · airframe 119,380 hrs · 21,733 cycles

A/C 1504 - ATB - RETURNED TO AMS DUE TO NR 2 ENGINE LOSS OF OIL QTY AND LOW OIL PRESSURE AFTER TAKEOFF. CONTACTED DISPATCH AND MCC, OIL PRESSURE NEVER GOT BELOW 11 PSI, REDUCED THROTTLE TO IDLE AND TO RETURN TO AMS; EMERGENCY DECLARED. CORRECTIVE ACTION: FOUND LUBE/SCAVENGE PUMP TGB SCREEN CLOGGED WITH SEAL MATERIAL. REPLACED LUBE/SCAVENGE PUMP AND FLUSHED OIL SYSTEM MULTIPLE TIMES. REMOVED BOOSTER FAN BLADES AND REPLACED NR 1 AIR/OIL SEAL AND REINSTALLED BOOSTER FAN BLADES.

Part: BRAKE — DAMAGED (MLG) · airframe 118,736 hrs · 21,643 cycles

ON TAXI OUT FOR DEPARTURE PILOT RECEIVED A BRAKE TEMP LIGHT TWO MINUTES LATER AIRCRAFT BEHIND THEM REPORTED SMOKE COMING FROM RIGHT MAIN GEAR. FIRE AND RESCUE INSPECTED SAID THERE WAS NO FIRE. WHEN TAXING BACK TO THE GATE WITH FIRE VEHICLES FOLLOWING THEY RADIOED THAT THERE WAS SMOKE COMING FROM RIGHT MAIN GEAR AND A SMALL FIRED STARTED. THE FIRE WAS EXTINGUISHED. BRAKE NR 8 DAMAGED AND REPLACED, ALONG WITH AXLE 7/8, WHEEL 7/ 8 AND NR 8 WHEEL SPEED TRANSDUCER. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — BROKEN (CABIN) · airframe 116,610 hrs · 21,358 cycles

EMERGENCY LIGHTS SWITCH IS BROKEN. REPLACED EMERGENCY LIGHT SWITCH GUARD. SYSTEM OPERATION IS NORMAL.

Part: SKIN — DELAMINATED (NR 2 NACELLE) · airframe 115,551 hrs · 21,205 cycles

DURING A SERVICE CHECK, FOUND THE NR 2 NACELLE SKIN DELAMINATED APPROXIMATELY 6 X 9 AND 6 X 3. REPAIRED IAW ERA 567774-14.

Part: STRUCTURE — DAMAGED (NR 2 NACELLE) · airframe 115,664 hrs · 21,220 cycles

NR 2 ENGINE INBD FAN COWL HAS AN AREA OF DELAMINATION ON THE UPPER AFT EDGE AND IS DENTED. REPAIRED IAW ERA 567143-14.

Part: BEZEL — DAMAGED (EMERGENCY LIGHT) · airframe 115,476 hrs · 21,194 cycles

EMERGENCY LIGHTS ABOVE THE LAVATORY DOOR IN LEFT MAIN AISLE ARE INOPERATIVE. REPLACED THE BEZEL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 115,408 hrs · 21,185 cycles

EMERGENCY LIGHTS AT SEAT 25AB ARE INOPERATIVE. SECURED AND REPLACED THE LAMPS.

Part: WIRE HARNESS — OUT OF POSITION (COCKPIT) · airframe 114,658 hrs · 21,082 cycles

WHEN CAPTAIN USED UP ELECTRIC BUTTON FOR HIS SEAT. THERE WAS A SPARK AND THE ELECTRIC USE OF THE SEAT FAILED FOR ALL AXISES. FOUND CAP SEAT CB STILL IN AT PNL P6-H15. CHECKED SEAT, FOUND ONE HARNESS CABLE PINCHED IN MECHANISM. NO DAMAGE NOTED TO SEAT STRUCTURE. MANUAL ADJUSTMENT STILL OK. C/W EAR 565163-14.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 114,296 hrs · 21,028 cycles

THE FLOOR PANEL IN TH EAFT CARGO BAY HAD A CRACKED ABOUT 10 INCHES WIDE X 1/4 INCH DEEP, BS 1197 AND 1197+132. REPAIRED IAW ERA 564601-14.

Part: STRUCTURE — BENT (NR 1 NACELLE) · airframe 114,278 hrs · 21,026 cycles

FOUND NR 1 ENGINE RT CORE COWL ON THE UPPER AFT FAIRLING SKIN HAS DAMAGED. DAMAGE CONSISTS OF A BENT FLANGE 4.5 INCH LONG FWD/AFT. THE BENT FLANGE HAS A CRACK FWD SECTION, DAMAGE LENGTH OF 1.5 INCHES UP AND DOWN. REPLACED THE COWL IAW AMM 71-11,

Part: RECEPTACLE — DEFECTIVE (CABIN) · airframe 114,119 hrs · 20,998 cycles

EMERGENCY LIGHTS AT ROW 33-41FG ARE INOPERATIVE. MAINTENANCE REPLACED M9010 BATTERY RECEPTACLE. SYSTEM OPERATION IS NORMAL

Part: CHARGER — INOPERATIVE (CABIN) · airframe 114,049 hrs · 20,990 cycles

ON SERVICE CHECK FOUND EMERGENCY LIGHT INOPERATIVE FROM ROW 14 TO 22. REPLACED EMERGENCY LIGHT CHARGER. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 113,218 hrs · 20,857 cycles

EMERGENCY LIGHTS AT CEILING PANELS POSITION 18F 20F, AND 20B ARE INOPERATIVE. REPLACED BULBS, SYSTEM OPERATION IS NORMAL.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 111,153 hrs · 20,536 cycles

CREW REPORTED PASSENGER SMOKING IN LAV 203, NO SMOKE ALARM OBSERVED. LAV SMOKE DETECTOR TEST. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 110,466 hrs · 20,424 cycles

EMERGENCY LIGHTS AT SEATS 25A, 38F WHITE LIGHTS AND SEAT 6A RED ARE INOPERATIVE. DEFERRED PER MEL33-51-03A. REPAIRED 6A EMERGENCY LIGHT, RE LAMPED AND FOUND ELECTRIC CONNECTOR LOOSE AND RECONNECTED. SYSTEM OPERATION IS NORMAL. MCO/PLAC REMOVED.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 109,762 hrs · 20,316 cycles

BOTH CREW REST EMERGENCY EXIT SIGNS ARE INOPERATIVE. MAINTENANCE RELAMPED BOTH SIGNS. SYSTEM OPERATION IS NORMAL

Part: UNKNOWN — ODOR (CABIN) · airframe 109,692 hrs · 20,307 cycles

STRONG UNUSUAL ODOR WHEN PACKS WERE SWITCHED OFF FOR TAKEOFF. ODOR NOTICEABLE IN THE COCKPIT AND CABIN. ODOR DISSIPATED VERY QUICKLY. MAINTENANCE PERFORMED APU SYSTEM CHECK. NO OIL EVIDENT NOTED IN APU BLEED DUCT. RAN BOTH PACK WITH APU BLEED NO UNUSUAL ODORS NOTICED IN CABIN. SYSTEM OPERATION IS NORMAL.

Part: PIN — DAMAGED (EMERGENCY LIGHTS) · airframe 105,833 hrs · 19,734 cycles

ON SERVICE CHECK, FOUND EXTERRIOR EMERGENCY LIGHT INOPERATIVE AT R3 DOOR. FOUND NO PIN ON D2610, PIN 11 POSITION PIN AND FOUND PIN 11 ON D2610, PIN 15, REPOSITIONED TO CORRECT POSION. SYSTEM OPERATION IS NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 118,814 hrs · 21,653 cycles

FUSELAGE SKIN AT STATION 654+86, BETWEEN S-39L AND S-38L HAS DENT AND CREASE. C/W ERA 542633-14. (LP 2293561)

Part: SHEAR TIE — DAMAGED (BS 1373) · airframe 104,560 hrs · 19,550 cycles

SHEAR TIE AT BS 1373 DAMAGED. DRILLED UP NEW SHEAR TIE AND REPLACED IAW 538982-14.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 103,384 hrs · 19,385 cycles

EMERGENCY EXIT SIGN LIGHT IS INOPERATIVE. MAINTENANCE REPLACED R4 EMERGENCY BATTERY PACK. SYSTEM OPERATION IS NROMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 102,661 hrs · 19,274 cycles

COCKPIT EMERGENCY LIGHT BATTERIES BAD. MAINTENANCE REPLACED BATTERIES. SYSTEM OPERATION IS NORMAL.

Part: SKIN — DAMAGED (BS 525) · airframe 101,669 hrs · 19,147 cycles

LIGHTNING STRIKE AT FASTENER BS 525, STRINGER 11L. REMOVED FASTENER. INSTALLED TEMPORARY BLIND FASTENER IAW SRM 53-00-01.

Part: SKIN — DAMAGED (BS 654) · airframe 101,669 hrs · 19,147 cycles

LIGHTNING STRIKE AT BS 654+104 JUST ABOVE STRINGER 36L. BLENDED THE AREA AND FOUND IT TO BE OUT OF LIMITS IAW SRM 53-00-01.

Part: SKIN — CORRODED (BS 710-718) · airframe 94,826 hrs · 18,119 cycles

FWD CARGO BS 710 TO 718, S35-36L SKIN CORRODED. CORROSION REMOVED IAW SRM 51-10-02, BS 710 - 711 NEAR S36L BLEND OUT FIG 101 LIMIT. AT OTHER AREA BLEND OUTS WITHIN ABOVE SRM LIMIT. TRIMMED OUT CORRODED SKIN AT BS 710 TO 714 S36L AREA REPAIRED IAW SRM 53-00-01. REPAIR 12, FIG 201.

Part: TEE FITTING — CRACKED (BS 955) · airframe 94,826 hrs · 18,119 cycles

RT BS 955, REAR SPAR BULKHEAD FITTING AREA, CRACKS FOUND AT TEE FITTING. REPLACED AND INSTALLED IAW ER/A 511792-14AD.

Part: FLOORBEAM — CORRODED (BS 1480) · corrosion level 2 · airframe 94,918 hrs · 18,132 cycles

BS 1480, RBL 26 TO LBL 28, FLOORBEAM SEVERAL AREAS. CORROSION REMOVED IAW SRM 51-10-02. FOUND TWO LOCATIONS OUT OF LIMITS. REPAIRED IAW ER/A 513068-14 AND ER/A 513078-14.

Part: FLOORBEAM — CORRODED (BS 654) · corrosion level 2 · airframe 94,807 hrs · 18,115 cycles

M/D BS 654+88 BL L27 FLOORBEAM UPPER TEE FOUND CORRODED. FLOORBEAM UPPER TEE REPAIRED IAW SRM 53-00-51 REPAIR 1, FIG 201.

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 94,826 hrs · 18,119 cycles

M/D BS 1439 LBL 19 - 35 FLOORBEAM LWR TEE CORRODED. REMOVED IAW SRM 51-10-02, AT LBL22" BLEND OUT DEPTH 0.031" ORG 0.090" WIDTH 0.95" LENGTH 1.2" OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1, FIG 101 LIMIT. AT OTHER AREA BLEND OUT DEPTH 0.013" ORG 0.090" WIDTH 0.95" LENGTH 1.1" WITHIN ABOVE LIMIT. REPAIRED IAW ER/A 513069-14 REV ORIG FOR LBL22 AREA.

Part: HOSE — TWISTED (ESCAPE SLIDE) · airframe 94,807 hrs · 18,115 cycles

LEFT OFF-WING SLIDE INFLATION HOSE TWISTED AND ATTACH CLIP MOUNTING INSERT DETACHED. LT OFF-WING SLIDE REPLACED.

Part: FLOORBEAM — CORRODED (BS 1439) · corrosion level 2 · airframe 94,826 hrs · 18,119 cycles

BS 1439, LBL 7 TO RBL 38, M/D FLOORBEAM LWR TEE FOUND ANCHOR NUTS HOLES AREA CORROSION. CORROSION REMOVED IAW SRM 51-10-02, AT RBL 30" BLEND OUT DEPTH 0.009", ORG 0.090", WIDTH 0.9", LENGTH 1.2" WITHIN SRM 53-00-51, ALLOWABLE DAMAGE 1 FIG 101 LIMIT, AT OTHER AREA 5, LOCATION LBL7", RBL8", RBL14", RBL21" AND RBL36 OUF OF ABOVE LIMIT. MAX DEPTH 0.032" ORG 0.090" WIDTH 0.9" LENGTH 1.3" REPAIRED THE FLOORBEAM LWR TEE IAW ER/A 513069-14 REV ORIG FOR LBL7" AND RBL8" TO RBL36" AREA.

Part: FLOORBEAM — CORRODED (BS 1480) · corrosion level 2 · airframe 94,826 hrs · 18,119 cycles

BS 1480 LBL 54 - RBL 25 FLOORBEAM LWR TEE CORRODED. BLEND OUT DEPTH MAX DEPTH 0.031" ORG 0.090" WIDTH 1.1" LENGTH 1.3" REPAIRED IAW ER/A 513071-14.

Part: FLOORBEAM — CORRODED (BS 1502) · corrosion level 2 · airframe 94,826 hrs · 18,119 cycles

BS 1502, RBL 37 - 58, FLOORBEAM LWR TEE CORROSION REMOVED IAW SRM 51-10-02 AT LBL36, RBL41, RBL50, RBL55, RBL58 TOTAL FIVE LOCATIONS OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1, FIG 101 LIMIT. THE BLEND OUT DEPTH 0.028" ORIG 0.088" WIDTH 1" LENGTH 1.2". REPAIRED IAW ER/A 513072-14 REV ORIG FOR RBL36" TO RBL58" AREA.

Part: FLOORBEAM — CORRODED (BS 1518) · corrosion level 2 · airframe 94,826 hrs · 18,119 cycles

BS 1518, LBL 2 - 52 CABIN FLOORBEAM LWR TEE ANCHOR NUTS AREA FOUND CORROSION. REPAIRED CORROSION REMOVED IAW SRM 51-10-02. AT LBL12" BLEND OUT DEPTH 0.020", ORG 0.063", WIDTH 0.95", LENGTH 1.3" OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1, FIG 101 LIMIT. AT OTHER AREA BLEND OUT DEPTH 0.008" ORG 0.063" WIDTH 0.9" LENGTH 1.2" WITHIN ABOVE LIMIT. REPAIRED IAW ER/A 513073-14 FOR LBL12" AREA.

Part: FLOORBEAM — CORRODED (BS 1518) · corrosion level 2 · airframe 94,826 hrs · 18,119 cycles

BS 1518 RBL2 TO RBL43 CABIN FLOORBEAM LWR TEE ANCHOR NUTS AREA FOUND CORROSION. BULK CARGO -STA1518, RBL2" TO RBL43" CABIN FLOORBEAM LWR CHORD CORROSION REMOVED IAW SRM 51-10-02 AT RBL25", RBL36", RBL43" BLEND OUT DEPTH 0.022" ORG 0.063" WIDTH 0.9" LENGTH 1.3" OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101, LIMIT AT OTHER AREA BLEND OUT DEPTH 0.007" ORG 0.063" WIDTH 0.9" LENGTH 1.2" WITHIN ABOVE LIMIT. REPAIRED IAW ER/A 513073-14 FOR RBL25" TO RBL43" AREA.

Part: FLOORBEAM — CORRODED (BS 1461) · corrosion level 2 · airframe 94,826 hrs · 18,119 cycles

BS 1461, LBL 67 - RBL 51 FLOORBEAM LWR TEE CORRODED CP53-251-01. CORROSION REMOVED IAW SRM 51-10-02 AT LBL8" AND LBL21" BLEND OUT DEPTH 0.027" ORG 0.090" WIDTH 0.95" LENGTH 1.3" OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1, FIG 101, LIMIT. AT OTHER AREA BLEND OUT DEPTH 0.011" ORG 0.090", WIDTH 0.9", LENGTH 1.3" WITHIN ABOVE LIMITS. REPAIRED IAW ER/A 513070-14, REV ORIG.

Part: FLOORBEAM — CORRODED (BS 1502) · corrosion level 2 · airframe 94,807 hrs · 18,115 cycles

M/D BS 1502 LBL 6 -54 FLOORBEAM CORRODED. REPAIRED THE FLOORBEAM IAW ER/A 513072-14, REV ORIG.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 94,807 hrs · 18,115 cycles

RT WING INBD T/E AFT FLAP UPPER SURFACE T/E FOUND DELAMINATED AS MARKED. RT WING INBD AFT FLAP UPPER SURFACE REPAIRED IAW SRM 51-70-01, 57-53-01, AFT FLAP REINSTALLED AND OPS TEST ACCOMPLISHED IAW AMM 27-51-00, 27-51B06.

Part: FLOORBEAM — CORRODED (BS 1562) · airframe 94,807 hrs · 18,115 cycles

AFT GALLEY BS 1562 LBL 32 FLOORBEAM UPPER TEE CORRODED. REPAIRED IAW SRM 53-00-51, REPAIR 2, FIG 201.

Part: FLOORBEAM — CORRODED (BS 654) · airframe 94,807 hrs · 18,115 cycles

MAIN DECK BS 654+110 RBL 26 - 30, FLOORBEAM UPPER TEE FOUND CORRODED. REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201.

Part: FLOORBEAM — CORRODED (BS 654) · airframe 94,807 hrs · 18,115 cycles

MAIN DECK BS 654+44, RBL 44 TO 48, FLOORBEAM FOUND CORRODED. REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 94,047 hrs · 18,006 cycles

DURING A CHECK, FOUND EMERGENCY LIGHT FROM ROW 32C-40C OUT. MX REPLACED THE CHARGER ASSY. SYS OPS IS NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 94,009 hrs · 17,997 cycles

FOUND ON DRC EMERGENCY LIGHTS AT ROWS 32-40 LT SIDE ARE INOPERATIVE. MX REPLACED THE CHARGER. SYS OPS IS NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 93,947 hrs · 17,982 cycles

OVERHEAD EMERGENCY LIGHTS FROM 19AB-30AB ARE INOPERATIVE. MX REPLACED BATTERY AND CHARGER ASSY.

Part: WIRE HARNESS — LOOSE (EMERGENCY LIGHT) · airframe 93,582 hrs · 17,935 cycles

EMERGENCY LIGHT AT SEAT 34AB ARE INOPERATIVE. MX REPLACED THE WIRE HARNESS IN THE SEAT. SYS OPS NORMAL.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 93,063 hrs · 17,873 cycles

EMERGENCY PATH LIGHTS AT SEAT 34B ARE INOPERATIVE. MX FOUND A LOOSE CONNECTOR AT SIDE WALL 34B AND RECONNECTED. SYS OPERATION IS NORMAL MCO/PLAC REMOVED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 92,975 hrs · 17,863 cycles

CABIN EMERGENCY LIGHTS TESTED ROW 15AB-19AB & DO NOT ILLUMINATE. BATTERY PACK AT SEAT 15AB WAS REPLACED. SYS OPS NORMAL.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 92,317 hrs · 17,784 cycles

SEAT 20AB EMERGENCY LIGHT INOPERATIVE. REPLACED INSEAT HARNESS. CHECKED GOOD.

Part: FRAME — CRACKED (BS 903) · airframe 91,584 hrs · 17,694 cycles

MAIN DECK FS 903 LT BETWEEN STR 20L AND 21L FRAME INNER CHORD CRACKED. THE INNER CHORD CRACK REMOVED AND REPAIRED AS PER ERA 502721-14AD REV ORG.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 90,491 hrs · 17,566 cycles

FUSELAGE SKIN FS 478 ABOVE STR 26L, FS 654+88 ABOVE STR 21L, FS 654 + 121 STR 19L LIGHTNING STRIKES ON FASTENERS REPAIR IAW ERA 492052-14.

Part: WIRE — DAMAGED (CABIN) · airframe 87,739 hrs · 17,251 cycles

EMERGENCY EXIT LIGHTS AT SEAT 25ABC ARE INOPERATIVE. MAINTENANCE INSTALLED A NEW WIRE AND LIGHT ASSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: TERMINAL — FAILED (EMERGENCY LIGHT) · airframe 86,107 hrs · 17,061 cycles

AIRCRAFT 1504, AFTER ARRIVAL OF FLIGHT 75 FROM MXP, MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT 24F INOPERATIVE. MAINTENANCE REPLACED THE FEMALE TERMINAL END. OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 84,714 hrs · 16,897 cycles

EMERGENCY ESCAPE AISLE LIGHT L782, LT SIDE IS INOPERATIVE. MX REPLACED FUSE M00737 POWER SUPPLY. SYS OPS IS NORMAL.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 84,714 hrs · 16,897 cycles

EMERGENCY ESCAPE LIGHTS AT SEATS 23AB ARE INOPERATIVE. MX REPLACED SEAT HARNESS SYS, OPS CHECKS GOOD.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 84,649 hrs · 16,890 cycles

MX FOUND ON CHECK THE EMERGENCY LIGHTS AT ROWS 21-31AB INOPERATIVE. FOUND TOP FUSE BLOWING ON AFT SEAT 22 PACK. FUSE AND CONNECTOR AT SEAT 20AB WAS REPLACED. SYS OPS IS NORMAL.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 84,129 hrs · 16,831 cycles

EMERGENCY LIGHTS ROW 20FG THROUGH 28FG ARE INOPERATIVE. MX REPLACED THE BATTERY PACK, CHARGER, AND REPAIRED A BROKEN WIRE AT SET 20FG. SYS OPS IS NORMAL.

Part: HSI — FAILED (COCKPIT) · airframe 81,587 hrs · 16,523 cycles

CAPT HSI FAILED, SWAPPED WITH LOWER EICAS DISPLAY AND FWD TO MEL 31-41-01A.

Part: LIGHT — FAULTY (GALLEY) · airframe 78,643 hrs · 16,162 cycles

ELECTRICAL SMELL IN AFT GALLEY RT SIDE. SMELL COMING FROM AFT GALLEY WORK LIGHT. REPLACED SAME PER MM MFG P/N BR9194-505-289.

Part: PROBE — INOPERATIVE (TAT) · airframe 77,945 hrs · 16,081 cycles

ATB- TAT LIGHT AND TAT PROBE EICAS AFTER TAKEOFF NOT ENGAGE. REPLACED TAT PROBE PER AMM. OPS TEST NORMAL. MFG 102LA2AG

Part: TURBINE — FAILED (APU) · airframe 77,558 hrs · 16,038 cycles

APU GENERATOR FAILED.FIELD OFF LIGHT ILLUMINATED. LONG HISTORY BIT BPCU FAULTS UNDERVOLTAGE TRIP REPLACE GCU-67. REPLACED GCU NO HELP.REPLACED BPCU AND ECU.ALL NO HELP.REINSTALLED ORIGINAL UNITS. SAME FAULT ALL THE TIME. R & R APU PER AMM. REQUIRES LEAK CHECK. INSTALLED NEW MOUNT NUTS.OPS AND LEAK CHECK GOOD. OK FOR SERVICE. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: SHUTOFF VALVE — FAILED (NR 1 ENGINE) · airframe 76,636 hrs · 15,936 cycles

LT BLEED LIGHT ILLUMINATED WHEN THROTTLE RETARDED FOR CRUISE POWER, DEACTIVATED LT HPSOV PER MM AND FWD TO MCO AND PLACARD PER M 36-11-02.

Part: PUMP — INOPERATIVE (FUEL BOOST) · airframe 74,371 hrs · 15,675 cycles

RTB DUE TO LT CTR FUEL BOOST PUMP INOP. FOUND C/B F15 ON P6 PANEL OUT. NO HIST AND CREW REPORTS IT COULD HAVE BEEN BUMPED W/CREW FLT BAG. OPS CKG GOOD OF PUMP AFTER C/B CLOSED.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 74,303 hrs · 15,668 cycles

ON TAXI OUT ELEVATOR CONTROL POSITION INDICATOR SHOWS RIGHT ELEVATOR ONLY QUARTER MOVEMENT. LEFT INDICATOR NORMAL. INDICATION BACK NORMAL AFTER ENG SHUT DOWN AND APU PWR. RESTART ENG ALL IND NORMAL.

Part: SLIDE — DEPARTED (RIGHT OVERWING) · airframe 72,366 hrs · 15,453 cycles

FLT 116 RETURNED TO ATL AFTER A REPORTED LOUD NOISE AND THE RT OVERWING ESCAPE SLIDE DOOR LIGHT INDICATION. UPON ARRIVAL IT WAS FOUND THAT THE RIGHT SIDE OFF WING ESCAPE SLIDE HAD DEPARTED THE A/C AND THE DOOR WAS OPENED AND SEVERAL COMPONENTS INSIDE THE SLIDE COMPARTMENT WERE DAMAGED.

Part: SLIDE — MISSING (RT WING) · airframe 72,366 hrs · 15,453 cycles

PASSING THRU FL210 AND LIGHT TURB GOT R WING SLIDE LIGHT. F/A AND PAX`S HEARD AIR NOISE AND ALSO SOMETHING HIT ACFT. ALL FLIGHT CONTROLS NORMAL. RETURNED TO ATL AND PERFORMED FLY-BY TO VERIFY NO SLIDE OR OTHER DAMAGE. UNEVENTFUL LDG. MTC IN PROGRESS. DAMAGE TO R INBD AFT FLAP, SLIDE COMPARTMENT AND SLIDE BOTTLE COMPARTMENT. INSTALLED PNL 196ER AND SLIDE PACK. BEGAN INST OF SLIDE BOTT AND DOOR LATCH CABLE ALSO MIDDLE AND AFT DOOR LATCH RODS. COMPLETED INSTALLATION OF SLIDE DOOR AND COMPONENTS ON RTN 7838 AD AND NRC 1-5.

Part: WARNING MESSAGE — ILLUMINATED · airframe 71,357 hrs · 15,338 cycles

LDG GEAR MONITOR STATUS MSG ON PUSH BACK.

Part: ADC — FAILED · airframe 71,193 hrs · 15,318 cycles

F/O'S ALTIMETER OFF FLAG DISPLAYED REPLACED RT ADC PER M/M. ALL TESTS PASS, FLAG CLEARED, P/N 4040800-911.

Part: ENGINE — MAKING METAL (NR 2) · airframe 69,413 hrs · 15,115 cycles

WHILE PERFORMING OPN 4050 ON NR 2 ENGINE, FOUND FERROUS MATERIAL ON MAG CHIP DETECTOR MATERIAL SENT TO SHOP FOR EVALUATION. DUE TO LAB FINDINGS, RECOMMEND ENGINE CHANGE. REPLACED NR 2 ENGINE PER TRANS 1T161.

Part: MODULE — CRACKED (HYD PUMP) · airframe 69,144 hrs · 15,085 cycles

C-2 PUMP FILTER MODULE LEAKING. FOUND C2 PUMP FILTER MODULE CRACKED. REPLACED PART.

Part: ENGINE — DAMAGED (NR 1) · airframe 68,915 hrs · 15,059 cycles

NR 1 ENG FAILED BORO ENGINE CHANGE.

Part: BRAKE — MALFUNCTIONED · airframe 68,055 hrs · 14,961 cycles

RETURNED TO GATE, PARKING BRAKE LIGHT AND EICAS MSG WHEN PARKING BRAKES ARE RELEASED. REPLACED PARKING BRAKE SWITCH S459. CHECKS GOOD.

Part: FLOORBEAM — CORRODED (BS 346) · airframe 66,860 hrs · 14,815 cycles

BS 346 RBL 38 TO 45 FLOORBEAM FOUND CORRODED AND REPAIRED AS PER DRD53-00-51D FIG 201.

Part: FLOORBEAM — CORRODED (BS 654) · airframe 66,860 hrs · 14,815 cycles

BS 654+88 RBL 28 FLOORBEAM UPPER CHORD FOUND CORRODED AND REPAIRED AS PER DRD 53-00-51D.

Part: FLOORBEAM — CORRODED (BS 1197) · airframe 66,860 hrs · 14,815 cycles

AFT CARGO COMPARTMENT STA 1197+66 FLOORBEAM AFT FACE UNDER SIDE CORRODED AND REPAIRED PER SRM53-00-07 REPAIR 4 FIG 201 DETAIL VI.

Part: FLOORBEAM — CORRODED (BS 1197) · airframe 66,860 hrs · 14,815 cycles

AFT COMPARTMENT STA 1197 RBL 23 TO 29 FLOORBEAM FWD OF AFT UNDER SIDE CORRODED AND REPAIRED PER SRM53-00--7 FIG 201 REPAIR 4 DETAIL V.

Part: FLOORBEAM — CORRODED (BS 14616) · airframe 66,860 hrs · 14,815 cycles

BS 1461 LBL 33-40 FLOORBEAM FOUND CORRODED AND REPAIRED AS PER DRD 53-00-51D FIG 201.

Part: FLOORBEAM — CORRODED (BS 1197) · airframe 66,860 hrs · 14,815 cycles

AFT CARGO COMPARTMENT STA 1197+44 RBL 22.5 FLOORBEAM AFT FACE UNDERSIDE CORRODED AND REPAIRED PER SRM 53-00-07 REPAIR 4 FIG 201 DETAIL V.

Part: FLOORBEAM — CORRODED (BS 1153) · airframe 66,860 hrs · 14,815 cycles

AFT COMARTMENT STA 1153 RBL 28 FLOORBEAM AFT FACE UNDERSIDE CORRODED AND REPAIRED PER SRM53-00-07 REPAIR 4 FIG 201 DETAIL V.

Part: FLOORBEAM — CORRODED (BS 654) · airframe 66,860 hrs · 14,815 cycles

BS 654 + 121 RBL 28 TO 55 FLOORBEAM UPPER CHORD CORRODED AND REPAIRED PER DRD53-00-51D FIG 201 ON NR CARD 51907.

Part: FLOORBEAM — CORRODED (BS 1153) · airframe 66,860 hrs · 14,815 cycles

AFT CAGRO COMPARTMENT STA 1153 RBL 29 FLOORBEAM FWD FACE UNDERSIDE CORRODED AND REPAIRED AS PER SRM 53-10-07 REPAIR 4 FIGURE 201 DETAIL 3.

Part: ACTUATOR — UNSERVICEABLE (LT MLG) · airframe 65,777 hrs · 14,669 cycles

UNABLE TO RETRACT LEFT MAIN GEAR. FOUND DRAG BRACE ACTUATOR AT FAULT. DRAG BRACE ACT REPLACED NO HELP. REPLACED LEFT TRUCK POSITIONER ACT BOTH LEFT LOCK ACT OPERATE PROPERLY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,724 hrs · 14,662 cycles

EMERGENCY LIGHTS AT R2/L2 DOOR ARE INOP. REPLACED BATTERY PACK. OP CKS GOOD.

Part: CONTROLLER — UNSERVICEABLE (NR 2 ENGINE) · airframe 64,993 hrs · 14,570 cycles

RT BLEED OFF LIGHT ILLUMINATED WITH BLEED LATCH ON. PERFORMED BITE ON ABCU FAULTED PRC AND WIRE FAULT REPLACED PRC PERFORMED BITE FAULT CLEARED RAN ENG OPS NORMAL.

Part: PANEL — MALFUNCTIONED (ATC) · airframe 64,329 hrs · 14,490 cycles

ATC FAULT EICAS MSI ATC FAIL LIGHT ON TRANSPONDER ALSO FAULT ON TCAS REPLACED BOTTOM ATC ANTENNA CHECKS GOOD IAW MM MCO AND PLACA REMOVED ETOPS CATEGORY (B): DIVERSION OR TURNBACK.

Part: ENGINE — DAMAGED (NR 2) · airframe 63,500 hrs · 14,393 cycles

NR 2 ENG FAILED OVERTEMP BORO HPC. 2 ENG OPENED UP AND BORO PLUGS REMOVED. C/W BORO INSP NR 2 S/N 695442 PER FIM. HPC FOUND DAMAGED BEYOND MTC LIMITS. ENG CHG REQUIRED QC 1513. REINSTALLED ALL BORO PLUGS THAT WERE REMOVED. NR 2 ENG CHANGE TO BE C/W BY TOC 1T160 ON R/C 1-34. NEW ENG S/N WILL BE 695376.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,735 hrs · 14,304 cycles

SEVERAL EMERGENCY LIGHTS INOP ON EXTERIOR OF A/C OVER BOTH LEFT AND RIGHT WINGS. RELAMPED 5 DIFFERENT LIGHT ASSY CKS OK.

Part: TURBINE — FAILED (APU) · airframe 58,918 hrs · 13,828 cycles

RAN APU ENTIRE FLT, AFTER LDG WHEN SWITCHED BLEEDS TO APU TO RUN PACKS SMELLED AC SMOKE. REPLACED APU.

Part: ACCESS DOOR — MISSING (FUSELAGE) · airframe 56,036 hrs · 13,441 cycles

ON ARRIVAL ACCESS DOOR FOR HYD HIGH PRESSURE CONNECT MISSING REPAIRED PER ERA 095866-14, INSTALLED PANEL, TIME LIMITED TO ONE FLIGHT. NDS PANEL P/N 145T8616-12 AND RELATED HARDWARE REF IPC 53-52-54-01 SHT 4 ITEM 100.

Part: BOLT — SHEARED (MLG WHEEL) · airframe 54,125 hrs · 13,163 cycles

NR 3 MLG WHEEL MISSING TIE BOLT. REPLACED WHEEL ASSY.

Part: BATTERY — FAILED (APU) · airframe 53,976 hrs · 13,141 cycles

CATERING REPORTED SMOKE TO F/A WENT BACK AND SMELLED SMOKE ABOUT 4 ROWS PRIOR TO THE AFT BULKHEAD. OTHER CREW MEMBERS ALSO NOTICED THE ODOR. FIRST F/A ALSO REPORTED SEEING SMOKE IN THE AFT PART OF THE AIRCRAFT. ISOLATED MAIN ODOR TO APU BATTERY OVERHEATING. REPLACED APU BATTERY AND APU BATTERY CHARGER PER MM.

Part: OVEN — BURNED (GALLEY) · airframe 50,292 hrs · 12,582 cycles

F/A REPORTS AFT GALLEY OVEN SMELLS BURNED AND HAS SCORCHED MARKS. THE 02 OVEN NR 4 SMELLS BURNED. REMOVED AND REPLACED OVEN. CHECKS GOOD MCO/PLACARD REMOVED.

Part: FAN — FAILED (RECIRCULATION) · airframe 49,939 hrs · 12,523 cycles

GOT LT RECIRCULATION FAN EICAS MSG AND ODOR OF HOT WIRES. SHUT OFF RECIRC FAN AND ODOR WENT AWAY. REPLACED FAN.

Part: SUPPORT — CORRODED (RT WING TE FLAP) · airframe 49,632 hrs · 12,475 cycles

RT WING INBOARD FLAP, INBOARD SUPPORT BEAM NR 5 HAS HOLE BORE CORROSION. CORROSION WAS FOUND IN THE 4 FLAP ATTACH FASTENER HOLES ON THE INBD SUPPORT BEAM OF THE INBD FLAP AT THE NR 5 SUPPORT LOCATION. THE HOLES WERE OVERSIZED TO REMOVE CORROSION, HFEC INSPECTED, BUSHED, AND NEW FASTENERS INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 385478-14, REV A.

Part: SUPPORT — CORRODED (LT WING TE FLAP) · airframe 49,632 hrs · 12,475 cycles

LT WING INBOARD FLAP, INBOARD SUPPORT BEAM NR 4 HAS HOLE BORE CORROSION, CORROSION WAS FOUND IN THE 4 FLAP ATTACH FASTENER HOLES IN THE INBD SUPPORT BEAM OF THE INBOARD FLAP AT THE NR 4 SUPPORT LOCATION. THE HOLES WERE OVERSIZED TO REMOVED CORROSION, HFEC INSPECTED, BUSHED, AND NEW FASTENERS INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 385477-14, REV A.

Part: SPAR — CRACKED (NR 1 NACELLE) · airframe 49,632 hrs · 12,475 cycles

PYLON, NR 1 FWD UPPER SPAR WEB, POWER FEEDER CABLE CUTOUT CRACKS. TWO CRACKS WERE FOUND IN THE UPPER SPAR WEB FROM THE POWER FEEDER CUTOUT TO THE NUTPLATE ATTACH HOLES. ERA INSTALLED REPAIR DOUBLER AND FILLER PER S/B 767-54-0090._ERA 385462-14 REVISION ORIGINAL. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: PROJECTOR — FAILED (CABIN) · airframe 48,430 hrs · 12,275 cycles

ENROUTE ATL/SCL FLT 147/06 REPORT STRONG ODOR OF BURNED PLASTIC FWD B/C SEATS FIRST 2 ROWS OF SEATS ON THE LT SIDE OF THE CABIN. CREW TURNED OFF IFE AND UTILITY BUSSES. ODOR DISSIPATED. CREW ELECTED TO CONTINUE TO SCL./C MTC FOUND THE FWD PROJECTOR INTERNALLY SHORTED. PROJECTOR DEACT AND MCO TO COVER. REF LOG C/N 328878001. REPLACED PROJECTOR. OPS NOW NORMAL. MCO AND PLACARD REMOVED.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 47,496 hrs · 12,106 cycles

COCKPIT EMERGENCY LIGHTS INOP, EXIT SIGN ABOVE COCKPIT DOOR. REPLACED LIGHT ASSY. FOUND ON LAYOVER.

Part: TOWERSHAFT — BROKEN (NR 2 ENGINE) · airframe 46,884 hrs · 11,989 cycles

AT CRUISE FL 350 RIGHT ENGINE EEC EICAS MSG AND AT SAME TIME ENG STARTED ROLLING BACK AND SHUTDOWN. FOUND GEARBOX TOWER SHAFT BROKEN. REPLACED ENGINE.

Part: WIRE HARNESS — ARCED (CABIN) · airframe 44,467 hrs · 11,572 cycles

ARCING COMING FROM UNDER SEAT 1FG. REMOVED HARNESS, INSTALLED NEW HARNESS. CHECKS GOOD, REMOVED MCO AND PLACARD.

Part: ODOR — DETECTED (CABIN) · airframe 44,022 hrs · 11,501 cycles

RAN APU FOR 10 HRS FROM MADRID. AFTER LANDING SELECTED APU BLEED TO OPERATE BOTH PACKS. CABIN FILLED WITH THIN HAZE AND FLT ATT REPORT ELECTRICAL ODOR. RAN APU PNEU SYS, RAN BOTH PACKS WITH AND WITHOUT RECIRC FAN AND NO HAZE OR ODORS FOUND. APU PNEU SYS, OPS OK.

Part: CONTROLLER — FAILED (SLDING WINDOW) · airframe 42,820 hrs · 11,313 cycles

AT DEPARTURE CAPT SLIDING SHORTED AND GOT FIRE. REPLACED SLIDING WINDOW IAW MM AND REPLACED WINDOW HEAT CONTROLLER.

Part: SKIN — CORRODED (HORIZ STAB) · airframe 41,046 hrs · 11,045 cycles

CORROSION FOUND ON THE UPPER SURFACE SKIN OF THE LT HORIZONTAL STABILIZER. DAMAGE LOCATED OVER STRINGER 3 BETWEEN RIBS 2 AND 3 APPROXIMATELY AT RT STA 2.5.

Part: BATTERY PACK — INOPERATIVE (CABIN)

EMERGENCY SEAT LIGHTS INOP 32AB TO AFT BULKHEAD. REMOVED AND REPLACED BATTERY PACK AND PWR SUPPLY LOC AT STA 1340 WL 215 BEHIND SIDEWALL.

Part: POWER SUPPLY — INOP (1R DOOR)

EMERGENCY EXIT SIGN AT 1R DOOR INOP. REPLACED POWER SUPPLY, SYSTEM CHECKS NORMAL.

Part: MECHANISM — LACK OF LUBE (1R DOOR)

DOOR 1R DOOR ARMING LEVER HARD TO OPERATE. SLIDE LIGHT INOP. RELAMPED.

Part: IDG — MALFUNCTIONED (NR 1 ENGINE)

NR 1 IDG DRIVE LIGHT EICAS MSG, NR 1 IDG DISCONNECTED. A/C RETURNED TO ATL FOR UNEVENTFUL OVERWEIGHT LANDING. REPLACED NR 1 IDG. SWAPPED TO A/C 172 TO MINIMIZE DELAY.

Part: LIGHT — OVERHEATED (MID GALLEY)

BURNING SMELL FROM AUX GALLEY AT R2 DOOR. PULLED AND COLLARED C/B FOR COUNTER LIGHTS. SUBMITTER SUSPECTS BALLAST, FWD TO MCO.

Part: STOP — MISRIGGED (LT EMER EXIT)

ON CLIMB-OUT THROUGH 15,000 FT, THE LEFT OVERWING EXIT LATCH OPENED SLIGHTLY. THE PRESSURE DIFF WAS 6 TO 8 PSID. FOUND DOOR STOPS OUT OF RIG. TWO (2) STOPS WERE NOT SAFTIED. RIGGED DOOR PER M/M AND INSTALLED SAFTIES, PRESSURIZED AIRCRAFT TO 8.5 PSID, NO LEAKS AND NO DOOR HANDLE MOVEMENT.

Part: THERMAL SHIELD — CRACKED (NR 2 ENGINE)

SHOP FINDINGS - NO FLIGHT INCIDENT. DURING OVERHAUL OF ENGINE 695373, THE HPT THERMAL SHIELD WAS FOUND TO HAVE A FLANGE TO FLANGE CRACK. THIS PART PROVIDES THE ROTATING SEAL BETWEEN THE T1 AND T2 DISK. THE THERMAL SHIELD IS NOT LIFE LIMITED. DUE TO THE CRACK, THE T1 AND T2 DISK WERE SCRAPPED BASED ON GE RECOMMENDATION.

Part: SWITCH — MALFUNCTIONED (CABIN)

PAX OXY MASKS DEPLOYED IN CLIMB AT FL 390. FOUND S119 CABIN ALTITUDE PRESSURE SWITCH AT FAULT MAKING CONTACT AT 6,300 FEET CABIN ALTITUDE INSTEAD OF 14,000 FEET CABIN ALTITUDE. REPLACED SWITCH SYSTEM CHECKS GOOD PER M/M. REPLACED USED OXY GENERATORS AND STOWED MASKS.

Part: SKIN — GOUGED (BS 610)

FUSELAGE/SKIN, FS 610 STRINGER 34L-35L, REPAIR FOR GOUGE. THE FUSELAGE SKIN WAS GOUGED AT STA 610 BETWEEN STRINGERS 34L AND 35L. THE GOUGE WAS 6 INCHES LONG BY .25 WIDE AND APPROX .065 DEEP. THE DAMAGE WAS REPAIRED WITH A SHEET METAL DOUBLER PER B767 SRM 53-00-01, FIG 201 AND DOCUMENTED PER ER/A 363563-14.

Part: WIRE — LOOSE (CABIN)

EMERGENCY TRACK LIGHTING INOP FROM ROW 26FG TO LAV AT R2 DOOR. SECURED LOOSE WIRING, SYS CKS GOOD.