N1501P

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 114,206 hrs · 21,501 cycles

THREE EMERGENCY EXIT MARKERS IN LOWER CREW REST NOT ILLUMINATING WHEN SELECTED ON. REPLACED THE LAMPS.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 112,930 hrs · 21,304 cycles

DURING CRUISE, THE MID RIGHT LAVATORY SMOKE ALARM WENT OFF WITH NO SIGNS OR EVIDENCE OF SMOKE OR FIRE. WATER PUT IN TRASH AND ALARM RESET. PERFORMED VISUAL INSPECTION OF MID RIGHT SMOKE DETECTOR AND OVERHEAT INDICATOR. NO EVIDENCE OF SMOKE. SYSTEM OPERATION IS NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 112,428 hrs · 21,222 cycles

FUSELAGE SKIN CRACK AT STA 1654, S-13AR. REPAIRED PER SRM 53-80-01 AND ERA 557850-14.

Part: WIRE — CHAFED (EMERGENCY LIGHTS) · airframe 112,228 hrs · 21,188 cycles

ROWS 31-41 LEFT, EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE FOUND A CHAFED WIRE AT AFT LEFT LAVS SHORTING. WIRE REPOSITIONED, SEAT LIGHTS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 111,351 hrs · 21,047 cycles

EMERGENCY LIGHTS ARE SEAT 1A, 2A, AND 3A ARE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY M9008. SYSTEM OPERATION IS NORMAL.

Part: FMC — FAILED (COCKPIT) · airframe 110,744 hrs · 20,952 cycles

FLIGHT CREW DIVERTED TO HND DUE TO THE LOSS OF BOTH FMC'S. AS CREW WAS RUNNING THE QRH, THE RIGHT FMC FAILED. AIRCRAFT LOST AUTOPILOT, AND ALL LNAV/VNAV FUNCTIONS. CREW PULLED, RESET CBS AND ATTEMPTED CONTACT WITH MCC VIA SATCOM, DECISION TO DIVERT TO HND. EMERGENCY DECLARED WITH ATC. CREW REPORTED THAT R FMC HAD RETURNED TO OPERATION 10-15 MINUTES AFTER CB RESET. REPLACED THE L FMC AND CROSS LOADED NAV DATA BASE AND VERIFIED SOFTWARE PER AMM 34-61.

Part: FRAME — CRACKED (BS 903) · airframe 107,043 hrs · 20,397 cycles

STA 903.5, FRAME INNER CORD CRACKED AT TRANS RADIUS AND REPAIRED.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 106,345 hrs · 20,294 cycles

EMERGENCY LIGHTS AT 31AB AND 32AB ARE INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE UNDER SEATS 31AB AND REPAIRED. SYSTEM OPS NORMAL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 106,285 hrs · 20,286 cycles

EMERGENCY LIGHTS AT ROW 20 ARE INOPERATIVE. MAINTENANCE RECONNECTED SEAT 20A CONNECTOR. SYSTEM OPS NORMAL.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 102,988 hrs · 19,813 cycles

EMERGENCY EXIT LIGHTS IN ROWS 36 & 32 ARE INOPERATIVE. MAINTENANCE FOUND CONNECTOR AT ROW 32AB LOOSE AND SECURED ALSO REPAIRED BROKEN WIRE AT ROW 36FG. SYSTEM OPERATION IS NORMAL MCO/PLAC REMOVED.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 100,450 hrs · 19,479 cycles

SEAT ROW 32AB THROUGHT 40 AB EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE FOUND SEAT 32AB WALL CONNECTOR PIN LOOSE AND POWER PACK M9010 FUSES BLOWN SECURED SEAT AT 32AB PLUG AND REPLACED BATTERY AND PACK/CHARGER AT M9010 . SYSTEM OPERATION IS NORMAL. (LP 5191755)

Part: NUT PLATE — DAMAGED (RT WING) · airframe 98,561 hrs · 19,194 cycles

RT WING T/E PANEL 661, FWD NUT PLATE FOUND DAMAGED AND REPAIRED IAW ERA 520038-14.

Part: NUT PLATE — CRACKED (RT WING) · airframe 98,561 hrs · 19,194 cycles

RT WING T/E PANEL E661, FWD NUT PLATE FOUND CRACKED, REPAIRED IAW ER/A 520038-14.

Part: STRUCTURE — CORRODED (BS 955) · corrosion level 2 · airframe 98,545 hrs · 19,192 cycles

STRUCTURE BS 955, LBL 88 TOP SURFACE CORRODED AROUND LOCK FASTENER HEADS. REPAIRED IAW ERA 14-520538.

Part: FITTING — CRACKED (FLAP TRACK) · airframe 98,545 hrs · 19,192 cycles

OTBD FLAP OTBD AUX TRACK FWD SUPPORT FITTING LOWER FOUND CRACKED REPLACED IAW ER/A 520549-14.

Part: FLOOR SUPPORT — CORRODED (BS 1545) · airframe 98,494 hrs · 19,185 cycles

BS 1545, LT OTBD FLOOR SUPPORT CORRODED REPAIRED IAW ER/A 520032-14.

Part: WEDGE — DELAMINATED (LT WING SLAT) · airframe 98,494 hrs · 19,185 cycles

LT WING SLAT UPPER WEDGE INBD AREA FOUND DELAMINATED. REPAIRED IAW SRM 57-43-02.

Part: FLOOR SUPPORT — CORRODED (BS 1545) · corrosion level 2 · airframe 98,494 hrs · 19,185 cycles

BS 1545 RT OTBD FLOOR SUPPORT CORRODED. REPAIRED IAW ERA 520032-14.

Part: SEAT TRACK — CORRODED (BS 340-423) · corrosion level 2 · airframe 98,494 hrs · 19,185 cycles

RBL 88, BS 340-423 SEAT TRACK CORRODED. REPLACED IAW SRM 51-10-02.

Part: FLOOR SUPPORT — CORRODED (BS 1545) · corrosion level 2 · airframe 98,494 hrs · 19,185 cycles

BS 1545 LT OTBD FLOOR SUPPORT CORRODED. REPAIRED IAW ERA 520032-14.

Part: FLOOR SUPPORT — CORRODED (BS 1545) · corrosion level 2 · airframe 98,494 hrs · 19,185 cycles

BS 1545, RT OTBD FLOOR SUPPORT CORRODED. REPAIRED IAW ERA 520032-14.

Part: FLOORBEAM — DAMAGED (BS 764) · airframe 98,494 hrs · 19,185 cycles

BS 764 FLOORBEAM UPPER TEE LBL 20, SCREW HOLE ELONGATED. FLOORBEAM REPAIRED IAW SRM 53-00-51.

Part: FLOORBEAM — DAMAGED (BS 654) · airframe 98,494 hrs · 19,185 cycles

MAIN DECK BS 654+22 FLOORBEAM UPPER FLANGE LBL 20 HOLES WITH SHORT EDGE MARGIN. REPAIRED IAW SRM 53-00-51.

Part: FLOORBEAM — DAMAGED (BS 654) · airframe 98,494 hrs · 19,185 cycles

CABIN BS 654+121, FLOORBEAM UPPER TEE SPLICE LBL 38 SCREW HOLE EDGE MARGIN OUT OF LIMIT. REPAIRED IAW SRM 53-00-51.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 98,494 hrs · 19,185 cycles

LT WING I/B AFT FLAP LOWER SURFACE FOUND DELAMINATED. REPAIRED IAW SRM 51-70-10, AND 57-53-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 98,403 hrs · 19,174 cycles

EMERGENCY LIGHTS ARE INOPERATIVE. MX REPLACED THE LIGHT ASSEMBLY AND BATTERY CHARGER. SYSTEM OPS NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 97,980 hrs · 19,125 cycles

EMERGENCY LIGHT INOPERATIVE. REPLACED CHARGER.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 96,962 hrs · 19,000 cycles

SQUIB TEST EMERGENCY SLIDE NR 2 LIGHT INTERMITTENT. MX REPLACED THE BATTERY PACK SYS OPS ARE NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 95,604 hrs · 18,829 cycles

EMERGENCY LIGHTS ROWS 32-40 ARE INOPERATIVE. MX REPLACED THE BATTERY AND CHARGER. SYTEM OPERATION IS NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 95,524 hrs · 18,818 cycles

EMERGENCY PATH LIGHTS AT SEAT 33FG ARE INOPERATIVE. MX R & R BATTERY CHARGER. SYS OPERATION IS NORMAL.

Part: SKIN — DAMAGED (BS 654 S28R) · airframe 94,817 hrs · 18,722 cycles

LIGHTNING STRIKE AT BS 654+116 AT STRINGER 28R. REPAIRED IAW ER/A 510176-14.

Part: SKIN — DAMAGED (BS 1542 S37R) · airframe 94,817 hrs · 18,722 cycles

LIGHTNING STRIKE DAMAGE AT BS 1542, S37L. REPAIRED IAW ER/A 510180-14.

Part: SKIN — DAMAGED (BS 697-789) · airframe 94,817 hrs · 18,722 cycles

LIGHTNING STRIKE DAMAGE FS 697 - 789 BETWEEN S35 - 36R. REPAIRED IAW ER/A 510145-14.

Part: SKIN — DAMAGED (BS 1197 S30-31R) · airframe 94,817 hrs · 18,722 cycles

LIGHTNING STRIKE AT BS 1197+88 BETWEEN S31R AND S30R. REPAIRED IAW ER/A 510147-14.

Part: SKIN — DAMAGED (BS 654 S29R) · airframe 94,817 hrs · 18,722 cycles

LIGHTNING STRIKE FASTENER AND SKIN STA 654+66 AT STR 29RCA: REPAIRED IAW ER/A 510177-14.

Part: SKIN — DAMAGED (BS 1197) · airframe 94,814 hrs · 18,721 cycles

A/C SUSTAINED LIGHTNING STRIKE AT BS 1197+88 BETWEEN STR 30 AND 31R. REPAIRED IAW ERA 510147-14. REV ORIG

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 93,737 hrs · 18,592 cycles

SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE SEATS 14AB -19A. REPLACED EMERGENCY LIGHT POWER SUPPLY AT SEAT 14AB. AMM 33-51.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 92,030 hrs · 18,383 cycles

EMERGENCY PATH LIGHTS AT SEAT 27GF ARE INOPERATIVE. THE HARNESS CONNECTOR WAS RETERMINATED. SYSTEM OPERATION IS NORMAL.

Part: PANEL — DELAMINATED (LT AILERON) · airframe 91,943 hrs · 18,369 cycles

LT WING I/B AILERON FWD LWR PNL 556AB IS DELAMINATED AND REPAIRED PER B767-300 SRM 57-60-01 REPAIR 1 AND 51-70-17 FIG 15.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 91,943 hrs · 18,369 cycles

CARGO FLOORBEAM AT FS 1480 BL-0 - LBL-14 IS CORRODED. WORKING FROM PRI.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 91,943 hrs · 18,369 cycles

CARGO FLOORBEAM AT FS 1439 AT BL 0 - RBL 43 AND LBL 22 - LBL 36 LWR FLANGE IS CORRODED. WORKING FROM PRI.

Part: BUSHING — LOOSE (NR 1 PYLON) · airframe 93,119 hrs · 13,643 cycles

NR 1 PYLON STRUT LWR SPAR FITTING AFT BUSHING IS LOOSE AND REPLACED PER B767-300 SRM 54-53-90 FIG 201 REPAIR 4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 91,943 hrs · 18,369 cycles

CARGO FLOORBEAM AT FS 1461 BL 0 - LBL 29 AND RBL 7 - RBL 59 IS CORRODED. WORKING FROM PRI.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 91,943 hrs · 18,369 cycles

CARGO FLOORBEAM AT FS 1502 LBL 2 - LBL 53 AND RBL 8 - RBL 56 LWR FLANGE IS CORRODED. WORKING FROM PRI.

Part: BOLT — SHORT (LE SLAT) · airframe 91,943 hrs · 18,369 cycles

DURING THE SLAT MAIN TRACK DOWN STOP ASSY INSP EA 01-469704-03 REV ORG ME-22 OPN 2201 THE STOP BOLTS WERE FOUND TO HAVE INCORRECT THREAD PROTRUSION AT THE NUTS. THE BOLTS AND NUTS WERE REPLACED AS PER OPN 2201 FOR THE FOLLOWING SLATS AND TRACKS. #1 I/B & O/B, #2 I/B & O/B, #3 I/B & O/B, #4 I/B & O/B, #5 I/B & O/B, #8 I/B & O/B, #9 I/B & O/B #10 I/B & O/B, #11 I/B & O/B, #12 I/B & O/B_(EA-01-469704-03).

Part: BEAM — CORRODED (FUSELAGE) · airframe 91,943 hrs · 18,369 cycles

CARGO FLOORBEAM AT FS 1417 BL-0 - RBL-22 LWR FLANGE IS CORRODED. WORKING FROM PRI.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 91,943 hrs · 18,369 cycles

CARGO FLOORBEAM AT FS 1480 AT RBL 12 - RBL 59 AND LBL 2 - LBL 53 IS CORRODED. WORKING FROM PRI.

Part: PANEL — DENTED (LT HORIZ STAB) · airframe 91,943 hrs · 18,369 cycles

LT HORIZONTAL STAB T/E PANEL 335MB IS DENTED AND REPAIRED PER B767-300 SRM 55-10-01 REPAIR 1 FIG 201 TABLE 5 AND 561-70-06 PAR 5A(1) FIG 9.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 91,943 hrs · 18,369 cycles

NR 3 SLAT T/E WEDGE I/B UPPER SURFACE IS DELAMINATED. REPAIRED PER B767-300 SRM 57-43-02 REPAIR 1 AND 51-70-10 REPAIR 4 FIG 201 SHT 1.

Part: FLOORBEAM — CORRODED (BS 1502) · airframe 91,943 hrs · 18,369 cycles

MAIN DECK BS 1502 FLOORBEAM LWR FLANGE CORRODED WL193 LBL 2 TO LBL 53 AND RBL 8 TO RBL 56 CORRODED. REPAIRED PER ERA 501557-14 REV ORIG.

Part: FLOORBEAM — CORRODED (BS 1439) · airframe 91,943 hrs · 18,369 cycles

MAIN DECK BS 1439 WL193 RBL 0 TO RBL 43 AND LBL 22 TO LBL 36, FLOORBEAM LWR FLANGE CORRODED. REPAIRED PER ERA 501559-14 REV ORIG.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 91,943 hrs · 18,369 cycles

NR 3 SLAT T/E WEDGE O/B UPPER CORNER IS DELAMINATED. REPAIRED PER B767-300 SRM 57-43-02 REPAIR 1 AND 51-70-10 REPAIR 4 FIG 202 SHT 3.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 91,943 hrs · 18,369 cycles

NR 3 SLAT T/E WEDGE I/B UPPER CORNER IS DELAMINATED. REPAIRED PER B767-300 SRM 57-43-02 REPAIR 1 AND 51-70-10 REPAIR 4 FIG 202 SHT 1.

Part: FLOORBEAM — CORRODED (BS 1417) · airframe 91,943 hrs · 18,369 cycles

MAIN DECK BS 1417 WL 193 RBL 0 TO RBL 22 FLOORBEAM LOWER FLANGE CORRODED. REPAIRED PER ERE 501555-14 REV ORIG.

Part: FLOORBEAM — CORRODED (BS 1461) · airframe 91,943 hrs · 18,369 cycles

M/DECK STA 1461 WL193 RBL7 TO RBL 59 AND LBL 0 TO LBL 29 FLOORBEAM LWR FLANGE CORRODED. REPAIRED PER ERA 501558-14 REV ORIG.

Part: FLOORBEAM — CORRODED (BS 1480) · airframe 91,943 hrs · 18,369 cycles

MAIN DECK BS 1480 WL193 RBL 12 TO RBL 59 AND LBL 2 TO LBL 53 LWR FLANGE FOUND CORRODED. REPAIRED PER ERA 501556-14 REV ORIG.

Part: FLOORBEAM — CORRODED (BS 1480) · airframe 91,943 hrs · 18,369 cycles

M/DECK FLOORBEAM STA 1480 WL193 BL 0 CORRODED. REPAIRED PER ERA 501554-14 REV ORIG.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 91,943 hrs · 18,369 cycles

FS 955 RT REAR SPAR BLKHD "T" FITTING AT FAILSAFE HAS CORROSION, WORKING FROM A PRI.

Part: TEE FITTING — CORRODED (BS 955 BULKHEAD) · airframe 91,943 hrs · 18,369 cycles

LEFT BS 955 REAR SPAR BULKHEAD TEE FITTING CORRODED. FITTING REPLACED REF ERA 501532-14AD REV ORIG.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 91,943 hrs · 18,369 cycles

FS 955 LT REAR SPAR BLKHD "T" FITTING AT FAILSAFE HAS CORROSION, WORKING FROM A PRI.

Part: TEE FITTING — CORRODED (BS 955 BULKHEAD) · airframe 91,943 hrs · 18,369 cycles

RT BS 955 REAR SPAR BULKHEAD TEE FTG FASTENER HOLES CORRODED. FITTING REPLACED REF ERA 501533-14AD REV ORIG.

Part: FLOORBEAM — CORRODED (BS 303) · airframe 91,943 hrs · 18,369 cycles

FLOORBEAM UPPER TEE CORRODED AT FS 303 LBL 40 TO LBL 46. REPAIRED AS PER SRM 53-00-57, FIGURE 201, REPAIR 1, AND SRM 51-40-05.

Part: WEB — CHAFED (NR 2 NACELLE) · airframe 91,943 hrs · 18,369 cycles

NR 2 PYLON AFT FAIRING, LOWER HORIZONTAL WEB, LT FWD UPPER SURFACE HAS DAMAGE FROM DEEP CHAFING.

Part: FLOORBEAM — CORRODED (BS 325) · airframe 91,943 hrs · 18,369 cycles

FLOORBEAM UPPER TEE CORRODED FS 325 LBL 50 TO LBL 52. REPAIRED AS PER SRM 53-00-51, FIGURE 201, REPAIR 1.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 91,943 hrs · 18,369 cycles

LT WING, O/B FLAP, LOWER SURFACE DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 57-53-01 REPAIR 1, AND SRM 51-70-06, PAR 5A(1), FIGURE 9.

Part: FAIRING — DELAMINATED (RT WING TE FLAP) · airframe 91,943 hrs · 18,369 cycles

RIGHT WING, O/B FLAP, O/B FWD FAIRING DELAMINATED. COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT AS PER SRM 57-53-01, REPAIR 1 AND SRM 51-07-05 PAR 5A(1), FIGURE 5.

Part: FLOORBEAM — CORRODED (BS 325) · airframe 91,943 hrs · 18,369 cycles

MAIN DECK FS 325 LBL 50 TO LBL 52 FLOORBEAM UPPER CHORD CORROSION.

Part: FLOORBEAM — CORRODED (BS 303) · airframe 91,943 hrs · 18,369 cycles

MAIN DECK STATION 303 LBL 40 TO LBL 46 FLOORBEAM UPPER CHORD CORROSION.

Part: FAIRING — DELAMINATED (LT WING TE FLAP) · airframe 91,943 hrs · 18,369 cycles

LEFT WING, O/B FLAP, O/B FWD FAIRING DELAMINATED. COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT AS PER SRM 57-53-01, REPAIR 1 AND SRM 51-07-05 PAR 5A(1), FIGURE 5.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 91,943 hrs · 18,369 cycles

LEFT WING, O/B FLAP LOWER SURFACE DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 57-53-01, REPAIR 1 AND SRM 51-70-06, PAR 5A(1), FIGURE 9.

Part: SKIN — DELAMINATED (NR 9 SLAT) · airframe 91,943 hrs · 18,369 cycles

RT WING NR 9 L/E SLAT UPPER SURFACE FOUND DELAMINATED. METAL HOT BOND REPAIR CARRIED OUT AT DELAMINATION AREA AS PER SRM 57-43-02 REPAIR 1 AND SRM 51-70-10 REPAIR 4, FIGURE 202, SHEET 2.

Part: SKIN — DELAMINATED (NR 10 SLAT) · airframe 91,943 hrs · 18,369 cycles

RIGHT WING NR 10 L/E SLAT UPPER O/B SURFACE DELAMINATED. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 57-43-02 REPAIR 1 AND SRM 51-70-10 REPAIR 4, SHEET 2.

Part: SKIN — DELAMINATED (NR 9 SLAT) · airframe 91,943 hrs · 18,369 cycles

RIGHT WING NR 9 L/E SLAT I/B SURFACE FOUND DELAMINATED. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 57-43-02 REPAIR 1 AND SRM 51-70-10 REPAIR 4, FIGURE 202, SHEET 3.

Part: SKIN — DELAMINATED (NR 10 SLAT) · airframe 91,943 hrs · 18,369 cycles

RIGHT WING NR 10 L/E SLAT I/B LOWER SURFACE FOUND DELAMINATED. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 57-43-02 REPAIR 1 AND SRM 51-70-10, REPAIR 4, FIGURE 203, SHEET 3.

Part: SKIN — DELAMINATED (NR 3 SLAT) · airframe 91,943 hrs · 18,369 cycles

LT WING NR 3 L/E SLAT UPPER O/B UPPER SURFACE FOUND DELAMINATED. METAL HOT BOND REPAIR CARRIED OUT AT DELAMINATED AREA AS PER SRM 57-43-02, REPAIR 1 AND SRM 51-70-10, REPAIR 4, FIGURE 202, SHEET 2.

Part: FAIRING — DELAMINATED (RT WING TE FLAP) · airframe 91,943 hrs · 18,369 cycles

RIGHT WING, I/B FLAP, O/B FWD FAIRING DELAMINATED. COMPOSITE PREPREG REPAIR CARRIED OUT AS PER SRM 57-53-01, REPAIR 1 AND SRM 51-07-05 PAR 5A(1), FIGURE 5.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 91,943 hrs · 18,369 cycles

RIGHT WING O/B FLAP UPPER SURFACE DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 57-53-01 REPAIR 1 AND SRM 51-70-06, PAR 5A(1), FIGURE 9.

Part: FAILSAFE — CRACKED (BS 955 BULKHEAD) · airframe 91,943 hrs · 18,369 cycles

CRACK FOUND AT FAILSAFE STRAP THRU THICKNESS AT LT BS 955 REAR SPAR BULKHEAD FITTING AREA. FAILSAFE STRAP REPAIRED PER ERA 501522-14AD REV ORIG.

Part: FRAME — CRACKED (BS 903 S20-21L) · airframe 91,943 hrs · 18,369 cycles

MID BS 903 S20 - 21L FRAME INNER CHORD CRACKED.

Part: FRAME — CRACKED (BS 903 S20-21L) · airframe 91,943 hrs · 18,369 cycles

BS 903 STR 20L-21L FRAME INNER CHORD CRACKED. REPAIRED PER ERA 501534-14AD REV ORIG SECT 1.

Part: FAILSAFE — CRACKED (BS 955) · airframe 91,943 hrs · 18,369 cycles

FOUND FAILSAFE CRACKED THROUGH THICKNESS AT LT BS 955 REAR SPAR BULKHEAD FITTING AREA.

Part: FAILSAFE — CRACKED (BS 955) · airframe 91,943 hrs · 18,369 cycles

FS 955 RT FAILSAFE FOUND CRACKS RUNNING FROM 5 O'CLOCK POSITION AND FROM 11 O'CLOCK POSITION.

Part: FAILSAFE — CRACKED (BS 955) · airframe 91,943 hrs · 18,369 cycles

BS 955 RT FAILSAFE STRAP FOUND CRACKED FROM 5O/C AND 11 O/C. REPAIRED PER ERA 501533-14AD REV ORIG.

Part: WIRE — DISCONNECTED (CABIN) · airframe 90,785 hrs · 18,236 cycles

SEAT 32AB PATH LIGHT INOP WIRES BROKEN AT SIDEWALL DISCONNECT. RECONNECTED WIRES AT SIDEWALL AT SEAT 32AB. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: STRUCTURE — UNKNOWN (PYLON) · airframe 90,435 hrs · 18,196 cycles

PYLON REWORKED IAW ERA 389665-14.

Part: BATTERY — DISCHARGED (CABIN) · airframe 89,655 hrs · 18,101 cycles

DURING DRC FOUND EMERGENCY PATH LIGHTS AT ROW 32FG AND AFT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND CHARGER M9010 AT ROW 38. SYSTEM OPERATION IS NORMAL.

Part: WIRE — DISCONNECTED (CABIN) · airframe 88,658 hrs · 17,984 cycles

MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT SEAT 18AB. MAINTENANCE FOUND A WIRE DISCONNECT RUNNING DOWN THE SEAT LEG TO BE BROKEN. MAINTENANCE CAPPED WIRE AND INSTALLED PLACARD. DISPATCHED PER MEL 33-51-03A.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 88,611 hrs · 17,978 cycles

EMERGENCY LIGHTS AT SEAT 5AB ARE INOPERATIVE. MAINTENANCE SECURED THE CONNECTOR. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 87,945 hrs · 17,901 cycles

MAINTENANCE FOUND EMERGENCY LIGHTS AT SEAT ROWS 32-40 ON LEFT SIDE OF CABIN INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY PACK AND BATTERY CHARGER ASSEMBLY AT ROW 38. OPERATIONAL CHECK WAS NORMAL. AIRCRAFT OK FOR SERVICE.

Part: FUSE — BLOWN (BATTERY PACK) · airframe 87,619 hrs · 17,863 cycles

EMERGENCY LIGHTS L1 CLOSET ARE INOPERATIVE. MAINTENANCE FOUND A BLOWN FUSE AT THE BATTERY PACK AND REPLACED. SYSTEM OPERATION IS NORMAL.

Part: FUSE — BLOWN (BATTERY CHARGER) · airframe 87,182 hrs · 17,814 cycles

EMERGENCY LIGHTS CABIN AFT RIGHT ARE INOPERATIVE. MAINTENANCE REPLACED THE FUSES IN THE BATTERY CHARGER ASSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 84,091 hrs · 17,453 cycles

EMERGENCY PATH LIGHT AT ROW 37FG IS INOPERATIVE. MX-TERMINATED PINS IN SOCKET. SYS OPS IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 82,549 hrs · 17,283 cycles

EMERGENCY LIGHTS RT EXTERIOR AT R1 AND R2 ALL OVER WING ARE INOPERATIVE. MX REPLACED BATTERY AND CHARGER ALSO RE-LAMPED R2. SYS OPERATION IS NORMAL.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 82,159 hrs · 17,238 cycles

CABIN ALT AUTO 2 STATUS MSG. CABIN AUTO INOP EICAS CAUTION MSG WORKED 4.0 IN MANUAL. FOUND ON BITE TEST, AC MOTOR FAULT AND LOW IN FLOW FAULT. REPLACED CABIN ALT CONTROL PANEL AND BOTH PRESSURE CONTROLLERS. OK FOR SERVICE. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 81,980 hrs · 17,217 cycles

ROW 33 FG EMERGENCY LIGHT INOP. REPAIRED BROKEN CONNECTOR. OPS NORMAL.

Part: FUSE — BLOWN (CABIN) · airframe 80,219 hrs · 16,998 cycles

FOUND DURING DRC EMERGENCY LIGHTS TEST SEATS 32F-40F INOP. FOUND BAD FUSE ON CHARGER, EQUIP NR 9010. REPLACED FUSE.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 80,104 hrs · 16,985 cycles

NR 1 ENG PYLON STRUT SKIN REPAIR, PERMANENT REPAIR COMPLIED WITH PER ERA 476516-14.

Part: FRAME — CRACKED (BS 1809.5) · airframe 80,104 hrs · 16,985 cycles

STA 1809.5 BULKHEAD FWD CHORD, CRACKED APPROX 1" IN RADIUS AT STR 5R. REPAIRED DAMAGE IAW SRM 53-80-08, REPAIR 9.

Part: SOCKET — DAMAGED (CABIN) · airframe 79,827 hrs · 16,953 cycles

ON DAILY CHECK FOUND ESCAPE LIGHTS INOP AT SEATS 21B, 32B AND 27F. REPLACED LIGHT SOCKET AT 21B, REPLACED CONNECTORS AT 32B AND 27F. OPN NORMAL.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 79,827 hrs · 16,953 cycles

ON DAILY CHECK FOUND ESCAPE LIGHTS INOP AT SEATS 21B /32B /27F. REPLACED LIGHT SOCKET AT 21B. REPLACED CONNECTORS AT 32B AND 27F. OPN NORMAL.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 79,818 hrs · 16,952 cycles

NR 1 ENG BLEED VALVE WON’T OPEN. BIT CHECK OF CONTROLLER FAULTED PRSOV. CYCLED VALVE MANUALLY. CHECKS GOOD. OK FOR SERVICE.

Part: OVEN — ODOR (AFT GALLEY) · airframe 79,693 hrs · 16,938 cycles

BURNING PLASTIC ODOR IN THE REAR GALLEY. COMPLETED SMOKE FUMES CHECK LIST. F/A NOTICED OVEN NR 5 ON AFT GALLEY SUSPECTED OF ODORS TESTED ALL OVENS TO ON AT 350F FOR 15 MIN. ALL OVENS WORKING FINE, NO BURNING PLASTIC ODORS NOTED. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: WARNING MESSAGE — ILLUMINATED (NR 2 ENGINE) · airframe 79,493 hrs · 16,916 cycles

RT IDG VALVE MSG. FWD TO MCO/PLAC PER MEL 75-21-01B DISCONNECTED AND STOWED VALVE CONNECTOR PER MEL PROCEDURES. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: THROTTLE — STUCK (NR 1 ENGINE) · airframe 77,669 hrs · 16,711 cycles

LEFT ENGINE THROTLE WILL NOT ADVANCE. REPLACED LOWER CABLE FROM PYLON TO HMU PER AMM. INSPECTED ALL OTHER AREAS. NO TROUBLE FOUND. PULL TEST NOW AT 3 POUNDS. BEFORE WAS 6 POUNDS.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 74,497 hrs · 16,353 cycles

FOUND EMERGENCY PATH LIGHTS OUT LEFT SIDE AT L1 DOOR. REPLACED CHARGER AND BATTERY PACK AND K371 RELAY AND RELAMP AT L1 DOOR. CHECKS GOOD PER AMM. CHARGER AT 1084.

Part: LINK — UNKNOWN (TE FLAP) · airframe 73,944 hrs · 16,289 cycles

O/B I/B FLAP LINK REPLACED IAW EA 01-076248-12, ME07, ME08, ME09, ME10, ME11, ME12.

Part: CONTROLLER — MALFUNCTIONED (NR 1 ENGINE) · airframe 71,038 hrs · 15,953 cycles

LEFT ENG PRV MESSAGE REMOVED AND REPLACED PRV CONTROLLER GRD, OPS CK GOOD.

Part: VALVE — UNKNOWN (HYD SYSTEM) · airframe 70,278 hrs · 15,865 cycles

AFTER PUSHBACK CTR HYD PRESS WOULD NOT RISE PAST 460 PSI. RTB, RESET HMG VALVE.

Part: ENGINE — UNKNOWN (NR 2) · airframe 70,046 hrs · 15,838 cycles

RTB - RIGHT ENGINE NR 2 ENGINE FUEL CONTROL VALVE LIGHT. NO START VALVE EXCERCISED BY OPERATING FIRE HANDLE. ENGINE GROUND RUN CARRIED OUT. NIL DEFECTS.

Part: ENGINE — INOPERATIVE (NR 2) · airframe 70,011 hrs · 15,834 cycles

R ENGINE WOULD NOT START. R ENG FUEL VLV LIGHT ON PEDESTAL ILLUM. RTB, CYCLED VALVE RAN RT ENG. CHKS GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,334 hrs · 15,754 cycles

FUSELAGE SKIN FS 437 TO FS 440. REPAIRED IAW ERA 455189-14.

Part: OVEN — ODOR (MID GALLEY) · airframe 69,107 hrs · 15,726 cycles

GALLEY MID CABIN CENTER OVEN WON`T HEAT PROPERLY GIVES OFF ELECTRICAL ODOR WHEN HEATING. CLEANED CHECKED OPS NORMAL.

Part: ISOLATION VALVE — STUCK (LEFT) · airframe 67,911 hrs · 15,581 cycles

L ISOLATION BLD VALVE EICAS MSG WITH OVERHEAD PANEL LIGHT ON. VALVE APPEARS TO BE OPEN. REPLACED L ISOLATION VALVE. VALVE WAS FROZEN IN MID POSITION RAN VLV, OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,345 hrs · 15,510 cycles

EMERGENCY LIGHT INOP EXTERIOR AT 2R. RELAMPED CKS GOOD.

Part: GUIDE VANE — MALFUNCTIONED (APU) · airframe 65,957 hrs · 15,344 cycles

FOUND APU IGVS SEIZED. REPLACED APU.

Part: PSEU — FAILED (MLG) · airframe 65,110 hrs · 15,245 cycles

ATB AT FL 3200, RECEIVED TAILSKID EICAS MSG TAIL SKID WARNING LIGHT BOTH MAIN LANDING GEAR LIGHTS W/2 BULBS, NO LANDING LIGHT W/1 BULB FOLLOWING STATUS MSGS. AIR/GND DISAGREE L REV ISLN VLV LANDING GEAR MONITOR CABIN ALT AUTO 1 NOSE A/G DISAGREE. ALSO REV ISLN WARNING LIGHT ON CENTER THROTTLE QUADRANT, ACARS LOGGED A/C ON AND TCAS STOPPED WORKING. PSEU FAULTS CARDS 11 AND 12. REPLACED PSEU.

Part: SENSOR — FAILED (TE FLAPS) · airframe 64,562 hrs · 15,183 cycles

ACFT HAS LEADING EDGE SLAT ASSY FAULT WITH SLATS LOCKED OUT PERFORMED PSEU BITE. FAULTS SENSOR 298. REPLACED SAME. ALSO ACCOMPLISHED EA 01-455226-03 ORIG ME-O2 REF ITEM 7. RAN SLATS AND FLAPS UP DOWN SEVERAL TIMES. PERFORM SENSOR CHECKOUT PER OPN 6086. ALL CHECKS GOOD.

Part: SKIN — CORRODED (BS 437-440 S36L) · airframe 64,198 hrs · 15,137 cycles

CORROSION WAS FOUND ON THE FUSELAGE SKIN AT S36L BETWEEN BS 437 AND 440. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED.

Part: FITTING — DAMAGED (NR 2 NACELLE) · airframe 64,198 hrs · 15,137 cycles

NR 2 PYLON NAC STA 253.70 FORWARD UPPER SPAR FITTING ASSY BORES WERE FOUND ELONGATED. HOLES WERE OVERSIZED AND A BUSHING INSTALLED.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 60,030 hrs · 14,610 cycles

AFTER LEVEL OFF AND UPON ADVANCING THRUST LEVERS TO INCREASE SPEED RT ENGINE BEGAN TO HAVE COMPRESSOR STALLS. REPLACED ENGINE FOR INTERNAL DAMAGE.

Part: ENGINE — UNKNOWN (NR 1) · airframe 58,296 hrs · 14,347 cycles

SHORTLY AFTER T/O WITH ALL PARAMETERS NORMAL ON BOTH ENGINES THE LEFT ENGINE FIRE WARNING ANNUNCIATED. THE CREW PULLED BACK THE THROTTLE AND THE FIRE WARNING EXTINGUISHED. THE CREW ELECTED TO SHUT DOWN THE ENGINE. NO FIRE BOTTLES WERE BLOWN. A/C DID A ATB TO ATL. THE A/C ARRIVED WITH NO EVIDENCE OF FIRE DAMAGE. ENGINE REPLACED.

Part: SENSOR — UNSERVICEABLE (RT WING SLAT) · airframe 57,791 hrs · 14,268 cycles

LE SLAT ASYM EICAS MSG AND LEADING EDGE CAUTION LIGHT WHEN FLAPS WERE SELECTED FROM 1 TO UP AFTER TO. REMOVED AND REPLACED RT NBR 12 OB SLAT PROX SWITCH S294 IAW MM OPS CH GOOD ETOPS CATEGORY (B) DIVERSION OR TURNBACK

Part: ODOR — DETECTED (FWD GALLEY) · airframe 57,661 hrs · 14,248 cycles

F/A IN FWD GALLEY REPORTED AN ELECTRICAL ODOR. LEAD F/A COULD NOT SMELL ANY UNUSUAL ODOR. ODOR STOPPED SOON AFTER INITIALLY DETECTED. F/A WHO COMPLAINED REPORTED IT MAY BE THE BUN WARMER. BUN WARMER SHOULD BE CHECKED. CHECKED FWD GALLEY AREA. NO PROBLEMS FOUND. FWD TO MCO AND PLACARD PER MEL 25-20-01B. C/B COLLARED.

Part: WIRE — CHAFED (FWD LAV OVERHEAD) · airframe 54,667 hrs · 13,804 cycles

WORKING MCO LAV 1 LIGHTING INOP. FOUND PLUG D808 IN LAV OVERHEAD SHORTED PIN 12 AFTER FURTHER TROUBLESHOOTING FOUND MANY WIRES IN WIRE BUNDLE BEING CHAFED BY THE L1 DOOR HANDLE EVERY TIME HANDLE IS ACTUATED. REPAIRED ALL.

Part: WIRE — CHAFED (LEFT ENGINE) · airframe 52,780 hrs · 13,524 cycles

REJECTED TAKEOFF DUE TO LOW OIL PRESSURE LIGHT ILLUMINATED. MAINTENANCE FOUND THE WIRING TO THE LOW OIL PRESSURE SWITCH CHAFED. REPAIRED SAME.

Part: ACTUATOR — INOPERATIVE (XFEED VALVE) · airframe 52,161 hrs · 13,421 cycles

FUEL CROSSFEED VALVE WOULD NOT OPEN IN FLIGHT. VALVE ACTUATOR REPLACED

Part: NUT — CRACKED (FUSELAGE) · airframe 51,270 hrs · 13,270 cycles

INSPECTION OF THE BARREL NUTS FOR THE VERTICAL STABILIZER TO FUSELAGE ATTACHMENT REVEALED CRACKED SEALANT AT ONE NUT LOCATION ON THE LT SIDE AT FS 1654. SINCE THIS IS INDICATIVE OF A POSSIBLE POOR TORQUE CONDITION, THE NUT AND BOLT WERE REPLACED PER ER/A 385082-14AD.

Part: OVEN — DIRTY (GALLEY) · airframe 50,676 hrs · 13,171 cycles

F/A REPORTED MINOR SMOKE IN FWD GALLEY. PULLED C/BS. SUSPECT FOOD AS CAUSE AFTER EXAMINATION. FOUND FWD GALLEY OVEN HAS LARGE AMOUNTS OF CHOCOLATE AND CARAMEL. CLEANED OVEN. NO FURTHER SIGNS OF SMOKE DURING OPS CHECK.

Part: EEC — MALFUNCTIONED (NR 2 ENGINE) · airframe 50,648 hrs · 13,167 cycles

R ENG EEC EICAS MESSAGE ON T/O ROLL. FWD TO MCO AND PLACARD PER MEL 73-21-01A. PIMU MONITOR SHOWS NO FAULTS. T/S PER FIM. RAN ENG, NO FAULTS. OK FOR SERVICE. MCO/PLAC REMOVED.

Part: COOLING FAN — MALFUNCTIONED (CARGO BAY) · airframe 50,378 hrs · 13,120 cycles

FWD EQUIP COOLING FAN STATUS MSG HAD AN ODOR IN AIR CONDITIONING AT THE SAME TIME. WENT TO STBY ON EQUIP COOLING AND ODOR DIMINISHED. REPLACED FAN.

Part: ENTERTAIN SYS — ODOR (CABIN) · airframe 49,240 hrs · 12,925 cycles

ELECTRICAL ODOR COMING FROM IFE CABINET. REPLACED PESC-V. SYS OPS CHECK OK. NO ODOR FOUND.

Part: FSEU — MALFUNCTIONED (E/E BAY) · airframe 46,835 hrs · 12,486 cycles

T/E FLAP DISAGREE LIGHT WHEN FLAPS 25 SELECTED, EICAS MSG ALSO. FLAPS DID NOT MOVE TO 25 DEGS POSITION. USED ALT FLAP PROC. INSPECTED FLAP, NO DISCREPANCIES NOTED. FSEU BITE SHOWED M603 FLAP LEVER RVDT. REPLACED FSEU PER AMM. OPS CHECKED NORMAL. NO HISTORY.

Part: ODOR — DETECTED (CABIN) · airframe 46,782 hrs · 12,476 cycles

DUE TO MISTY HYDRAULIC SMELL IN CABIN, AIRCRAFT RETURNED TO ATL. INT'L MTC RAN ENGINES TO POWER WITH PACKS ON AND OFF AND WAS UNABLE TO DUPLICATE. A/C WAS RETURNED TO SERVICE WITH NO FURTHER PROBLEMS.

Part: FAN — FAILED (EQ COOLING EXH) · airframe 46,514 hrs · 12,427 cycles

IMMEDIATLY AFTER T/O, F/AS CALLED TO REPORT SMOKE IN THE CABIN. SMOKE DETECTORS IN MID AND AFT LAVS ACTIVATED. SMOKE WAS VISIBLE WITH AN ELECTRICAL BURNING SMELL. FWD EQ EXH FAN EICAS MSG WITH STRONG ELECTRICAL SMELL IN FWD CABIN AREA. REMOVED AND REPLACED FWD EQUIP EXHAUST FAN PER M/M ETOPS CATEGORY 'B': DIVERSION OR TURNBACK

Part: ODOR — DETECTED (CABIN) · airframe 46,328 hrs · 12,393 cycles

FLIGHT ATTENDANTS REPORTED ELECTRICAL SMOKE/FIRE SMELL AT 2R DOOR. TURNED OFF 2R LIGHTS, SMELL DISSIPATED. CHECKED ELECTRICAL SYS IN AREA, CK LIGHTS AND GALLEY APPLIANCES.

Part: ENGINE — MAKING METAL (NR 2) · airframe 45,785 hrs · 12,295 cycles

METAL FOUND ON CHIP DETECTOR,-A- -C- AND -D- SUMP CHIP DETECTORS. ATL MTC REPLACING ENGINE. UPON FURTHER EVALUATION FROM ENGINE, SHOP NOW SUSPECT METAL IS CLEAN-UP MATERIAL. MTC FURTHER EVALUATING WITH T/O POWER PENALTY RUN.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,120 hrs · 11,861 cycles

INSPECTION OF THE FS 1809 BULKHEAD PER BAC SB 767-53-0078 AND AD 2001-09-13 REVEALED A CRACK IN THE LT OUTER CHORD. THE CRACKED SECTION OF CHORD WAS CUT OFF AND A NEW SECTION SPLICE IN PER THE REQUIREMENTS OF THE S/B AND PER ER/A 381053-14AD.

Part: CONTROL PANEL — OVERHEATED (COCKPIT) · airframe 42,369 hrs · 11,742 cycles

RT AUTOPILOT ENGAGE SWITCH SMOKED WHEN ENGAGED. DISCONNECTED SAME AND ENGAGED LEFT AUTOPILOT FOR REMAINDER OF FLT. REPLACED A/P MODE CONTROL PANEL AND PERFORMED OPS CKS. ALL OKAY.

Part: FLOW VALVE — FAILED (WING) · airframe 42,062 hrs · 11,690 cycles

A/C RESTRICTED FROM ETOPS OPERATIONS DUE TO REPETITIVE FUEL MIGRATION HISTORY. FOUND MOTIVE FLOW VALVE MALFUNCTION. REPLACED SAME.

Part: FAN — FAILED (SEATS 1F & 1G) · airframe 39,327 hrs · 11,237 cycles

CREW SMELL ELEC SMELL FROM VIDEO MONITOR AT SEATS 1 F AND G. COOLING FAN ON MONITOR INOP. REPLACED MONITOR.

Part: COOLING FAN — INOPERATIVE (MONITOR) · airframe 39,327 hrs · 11,237 cycles

ELECT SMELL COMING FROM MONITOR AT SEAT 1FG. TURNED OFF AND SMELL WENT AWAY. FOUND COOLING FAN ON MONITOR INOP. REMOVED AND REPLACED MONITOR AT SEAT 1FG. OPS CHECK NORMAL.

Part: THROTTLE CONTROL — MALFUNCTIONED (E/E BAY) · airframe 38,586 hrs · 11,096 cycles

LEFT THROTTLE RETARDED AGGRESSIVELY AT VNAV SELECTION AFTER T/O. RAN MCDP TESTS OF TMC AND SERVO, ALL CHECK OK.

Part: STRAP — CORRODED (FUSELAGE SKIN) · airframe 38,459 hrs · 11,077 cycles

CORROSION WAS FOUND ON THE INTERIOR SURFACE OF THE FWD CARGO OPENING BEAR STRAP. THE CORROSION WAS LOCATED BETWEEN STR 33R AND 34R AND BETWEEN APPROXIMATE STA 622 AND 631. REPAIRED PER ER/A 334435-14 REV A.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

ON WALKAROUND, FOUND GALLEY RT SIDE EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY, OPS NORMAL.

Part: SQUIB — FAILED (SLIDE)

DURING L/O CHECK, RT OVERWING SLIDE SQUIB FAILED TO TEST. DURING T/S SLIDE WAS BLOWN. A/C WAS FERRIED ON FLT 9933/24 TO REPLACE SLIDE AND WORK ON SQUIB SYS.

Part: BATTERY PACK — DISCHARGED (CABIN)

LEFT EMERGENCY ESCAPE LIGHT DID NOT TEST WITH TEST SWITCH ON P-61 PANEL. REPLACED ASSOCIATED BATTERY PACK, ALL TEST OK. LOG B537394 ITEM 002.

Part: CHILLER — OVERHEATED (GALLEY)

MID GALLEY CHILLER FAULT LIGHT ILLUMINATED, WALL BEHIND SEAT 10C SEAMED VERY HOT. TURNED OFF, WALL COOLED. CLEANED OUTLET AND VENT PORTS OF CHILLER, OPS CK OK. NO FAULT LIGHT OCCURRED.

Part: PDC BATTERY — DISCHARGED (COCKPIT)

ON PDC, FOUND RT SLIDE TEST 1 AND LEFT SPOILER TEST 2 INOP. REPLACED BATTERY PACK ON M961 AND NOW OK.

Part: POWER SUPPLY — INOPERATIVE (ROW 22-30)

OVERHEAD EMERGENCY LIGHTS DIM FROM 20 AB TO 30 AB. FOUND BAD POWER SUPPLY M737. REMOVED AND REPLACED POWER SUPPLY IAW M/M, OPS CHK GOOD.

Part: SKIN — DELAMINATED (NR 3 & 5 TE FLAP)

WING NR 3 AND NR 5 SLATS, TRAILING EDGE WEDGES, DELAMINATION REPAIR. THE UPPER SKIN OF THE TRAILING EDGE WEDGES ON THE NR 3 AND NR 5, SLATS WERE FOUND WITH A 2 BY 4 AREA OF DELAMINATION ON EACHWEDGE. THE DISBONDED AREAS WERE TRIMMED AWAY AND REPAIRED PER B767 SRM 57-43-02. THE REPAIRS WERE DOCUMENTED PER ER/A 365861-14AD.

Part: SKIN — DAMAGED (BS 620)

THE FUSELAGE SKIN AND STRINGERS BETWEEN FS 610 TO 63 AND STRINGERS 35L TO 37L WERE BADLY DENT AND TORN BY A GROUND EQUIPMENT IMPACT. THE DAMAGED SKIN AND STRINGERS WERE CUT OUT. THE STRINGERS WERE REPAIRED PER THE B767 SRM. THE SKIN WAS REPAIRED WITH AN EXTERNAL SKIN DOUBLER PER ER/A 364451-14, REV B.

Part: SKIN — DELAMINATION (NR 2 LE SLAT)

THE NR 2 LE SLAT TRAILING EDGE WEDGE WAS FOUND WITH UPPER SKIN DELAMINATION. THE SLAT HAS A DELAMINATION AREA OF 4 X 2 LOCATED ON THE I/B EDGE OF THE PART, APPROX 6 FORWARD OF THE AFT EDGE OF THE PART. THE DELAMINATION WAS REPAIRED PER B767-300 SRM 57-43-02, FIG 201. _

Part: ENGINE — FAILED (NR 2)

WHILE PERFORMING NR 1 SERVICE CHECK, FOUND METAL ON MASTER AND TRANSFER GEARBOX CHIP, A SUMP CHIP DETECTORS. REPLACING NR 2 ENGINE.