N704X

Part: GIRT BAR — FAULTY (ZONE 800) · airframe 98,741 hrs · 25,406 cycles

SHIP 6803 1L DOOR DIFFICULT TO ARM/DISARM. CORRECTIVE ACTION: REMOVED 1L DOOR SLIDE BUSTLE + INSPECTED ALL LOWER ARMING MECHANISMS. NO DEFECTS FOUND. DOOR ARMED NORMAL W/OUT EXCESSIVE FORCE MULTIPLE TIMES. CLEANED + LUBED GIRT BAR FITTINGS. R/R 1L GIRT BAR REF B757 AMM 25-66. DOOR ARMS/DISARMS W/OUT EXCESSIVE FORCE + OPS NML. REINSTALLED SLIDE BUSTLE.

Part: GIRT BAR — FOD (ZONE 800) · airframe 98,614 hrs · 25,353 cycles

SHIP 6803 1L DOOR WILL NOT ARM. CORRECTIVE ACTION: CLEARED DEBRIS AND CYCLED DOOR, OPS TEST NOW NORMAL PER B757 AMM 52-11. (6908710)

Part: ARMING LEVER — INOPERATIVE (ZONE 800) · airframe 98,394 hrs · 25,257 cycles

SHIP 6803 DOOR 1 L SLIDE ARM LEVER WILL NOT MOVE ALL THE WAY TO ARM POSITION. CORRECTIVE ACTION: OPERATED DOOR AND CLEANED DEBRIS - ARM LIGHT GOOD AND LEVER IN PROPER BAND-OK PER B757 AMM52-11-04. (4012864)

Part: GIRT BAR — FOD (ZONE 200) · airframe 98,302 hrs · 25,234 cycles

SHIP 6803 WHEN AT CRZ 1L SLIDE LIGHT WENT OUT. SOMETIME DURING DECENT FOR LANDING THE SLIDE LIGHT CAME BACK ON. F/A DISARMED 1L AS NORMAL UPON REACHING GATE. CORRECTIVE ACTION: INSPECTED, REMOVED DEBRIS FROM GRIT BAR AREA, LUBED GIRT BAR, LIGHT OPS NORMAL PER B757AMM 25-66,

Part: LANYARD — OUT OF POSITION (ZONE 800) · airframe 98,302 hrs · 25,234 cycles

SHIP 6803 1L DOOR WILL NOT ARM. CORRECTIVE ACTION: STOWED LANYARD - DOOR ARM NML (4012808)

Part: GIRT BAR — OUT OF ADJUST (ZONE 200) · airframe 97,668 hrs · 25,076 cycles

SHIP 6803 L1 DOOR SLIDE/ARM LIGHT INTERMITTENT. CORRECTIVE ACTION: T/S PER B757 FIM 52-11 TASK 813, ADJUSTED RT GIRT BAR PUSHROAD PER B757 AMM 52-11, OPS CHECK GOOD. (0509615)

Part: D-RING — OUT OF POSITION (ZONE 800) · airframe 97,599 hrs · 25,058 cycles

SHIP 6803 1L DOOR WONT ARM. CORRECTIVE ACTION: REPOSITIONED D-RING PER B757 AMM 52-11. (5704258)

Part: INDICATOR — INTERMITTENT (L1 DOOR) · airframe 97,396 hrs · 25,006 cycles

SHIP 6803 1L DOOR FAILED TO INDICATE ARMED AFTER ATTEMPT TO CLOSE AND ARM. CORRECTIVE ACTION: CYCLED L1 DOOR HANDLE ALL CHKS GOOD. INSPECTED GIRT BAR AREA. ALL CLEAN ARMED L1 DOOR ALL CHKS NML. DONE PER B757 AMM 52-11. (6027666)

Part: LIGHT — UNKNOWN (ZONE 200) · airframe 97,378 hrs · 25,000 cycles

SHIP 6803 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:32D. CORRECTIVE ACTION: EMERGENCY PATH LIGHT AT 32D & 33D OPS CK GD. (0460662)

Part: GIRT BAR — FOD (L1 DOOR) · airframe 97,267 hrs · 24,975 cycles

SHIP 6803 L1 GIRT BAR ENGAGED LIGHT WILL NOT ILLUMINATE WHEN GIRT BAR ENGAGED. CORRECTIVE ACTION: INSPECTED GIRT BAR FITTINGS, FOUND AND REMOVED DEBRIS, ENGAGED SLIDE ARMING LEVER SEVERAL TIMES, OPS CHECK GOOD. (5632292)

Part: FRAME — CRACKED (BS 1260 S3L) · airframe 96,687 hrs · 24,840 cycles

SHIP 6803 CRACK INDICATION ON FRAME 1260 @ STR 3L. HOLE COMMON TO CABLE CONTROL SUPPORT BRACKET. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 032-0001:4430-01019-01D/001 00006 ACCOMPLISHED ER/A 617548-14 REV ORIGINAL.

Part: FRAME — CRACKED (FRM 1260 S3L) · airframe 96,687 hrs · 24,840 cycles

SHIP 6803 DTE REQUIRED FOR 617548-14 REV. ORIGINAL, STA 1260 / STR 3L / FASTENER HOLE CRACK. CORRECTIVE ACTION: REF ERA 617548-14. (0315528)

Part: LIGHT — INOPERATIVE (SEAT 31D) · airframe 96,416 hrs · 24,784 cycles

SHIP 6803 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:31D. CORRECTIVE ACTION: RE-SEATED. (0254393)

Part: CONNECTOR — LOOSE (DOOR ARMING) · airframe 96,262 hrs · 24,748 cycles

2L ENTRY DOOR ARMING LIGHT DOES NOT COME ON. RESECURED LOOSE CONNECTION ON BACK OF LIGHT ASSY PER B757 WDM 25 -66-11, OPS CKS NORMAL.

Part: UNKNOWN — UNKNOWN (L1 DOOR) · airframe 96,002 hrs · 24,678 cycles

SHIP 6803 L1 DOOR SLIDE WOULD NOT ARM. CORRECTIVE ACTION: PERFORMED OPS CK OF BOTH L1 + R1 DOOR SLIDES ARM. NO TROUBLE FOUND. REF B757 AMM 25-61. (5379846)

Part: SLIDE — OUT OF ADJUST (UNKNOWN) · airframe 95,792 hrs · 24,629 cycles

SHIP 6803 4R DOOR WILL NOT ARM. CORRECTIVE ACTION: ADJUSTED SLIDE AS PER B757 AMM 52-11. NO DEFECTS. (5378756)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,875 hrs · 24,427 cycles

SHIP 6803 DOOR 4L SLIDE ARM LIGHT WILL NOT ILLUMINATE. CORRECTIVE ACTION: REMOVED DEBRIS AND PERFORMED OPS CHK PER B757 AMM 25-66. OPS CHKS GOOD. OK FOR SVC. (4424372)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,154 hrs · 24,269 cycles

SHIP 6803 ONE EMERGENCY PATH LIGHT + LENS AT SEAT 18D UNSECURED. CORRECTIVE ACTION: INSTALLED MISSING BRACKETS AND HARDWARE PER B757 CMM 25-22-57. OPS NML. (4471962)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 92,886 hrs · 23,987 cycles

SHIP 6803 F/A 'S REPORT THE RAFT MOORING LINE IS OUT OF THE POUCH AT 4L DOOR. CORRECTIVE ACTION: REPACK RAFT MOORING IN POUCH REF B757 AMM 25-66. (4034932)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 92,482 hrs · 23,902 cycles

SHIP 6803 CRACKS 2 (EA) ON WEB AT STA 1862 AND RBL 6.89 AND 14.57 AFTER ACCESORY COMPARTMENT. CORRECTIVE ACITON: SUMMARY OF NRC 00076. WEB ON STA 1862 BTW RBL 6.89 AND 14.57 OF AFTER ACCESORY COMPARTMENT WAS REPAIRED PER PRI NO.606400-14 REV 5 AND ER/A NO.606400-14, REVISION ORIGINAL, SECTION I: PERMANENT REPAIR. (2676213)

Part: UNKNOWN — UNKNOWN · airframe 92,463 hrs · 23,897 cycles

SHIP 6803 EXISTING REPAIR WAS FOUND IN THE INSPECTION AREA AT FRAME STA: 1560 BTW S-26L AND S-25L. CORRECTIVE ACTION: REF ERA 606399-14AD. (2665993)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,151 hrs · 24,485 cycles

SHIP 6803 FUSELAGE / BULKHEADS / STA 1862.7 LOWER TRANSVERSE BEAM WEB / CRACKS & CORROSION. CORRECTIVE ACTION: REF ERA 606400-14. (2666048)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,510 hrs · 24,345 cycles

SHIP 6803 FUSELAGE / MAIN FRAME / FRAME 1560, S-25L TO S-27L / EXISTING REPAIR. CORRECTIVE ACTION: REF ERA 606399-14. (2664750)

Part: NONE — NONE · airframe 92,463 hrs · 23,897 cycles

SHIP 6803 SECTION II REPAIR TO LH WING DRY BAY BARRIERS BETWEEN WSTA 231- 285 REQUIRES SECTION VI REPAIR WITHIN 24 MONTHS PER ERA 514351- 14. CORRECTIVE ACTION: REF ERA 514351-14. (2659859)

Part: NONE — NONE · airframe 92,463 hrs · 23,897 cycles

SHIP 6803 CRACK ON CHANNEL INSIDE ACCESS PANEL 117CL STA 365 BTW 0 BL. OF THE NLG WHEEL WEEL. CORRECTIVE ACTION: SUMMARY OF NRC 00164 CHANNEL INSIDE ACCESS PANEL 117CL STA 365 BTW 0 BL. OF THE NLG WHEEL WEEL.WAS REPAIRED PER B757-200 SRM. (2648038)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 92,389 hrs · 23,879 cycles

SHIP 6803 R CTR ENT DOOR ANNUNCIATED DURING LANDING ROLL. FA'S VERIFIED STILL CLOSED BUT NOTED A WINDY SOUND REMAINED LIT UNTIL ENG SHUTDOWN AT THE GATE. CORRECTIVE ACTION: PERFORMED FAST CHECK DOOR OPERATION FOR THE RT CTR DOOR IAW B757 AMM 52-11-00-206-021. DOOR OPS CHK GOOD. NO WARNING LIGHT/MSG NOTICED AT THIS TIME. (4092224)

Part: NOT ENTERED — NOT ENTERED (NOT ENTERED) · airframe 92,340 hrs · 23,868 cycles

SHIP 6803 F/A REPORTS R1 DOOR WILL NOT ARM. CORRECTIVE ACTION: FOUND LANYARD CAUGHT IN GIRT BAR LINKAGE. STOWED LANYARD DOOR NOW ARMS NORMALLY PER B757 AMM 52-11. (4092210)

Part: DOOR — UNKNOWN (R1) · airframe 91,928 hrs · 23,771 cycles

SHIP 6803 1R DOOR WOULD NOT ARM. CORRECTIVE ACTION: DOOR CLOSES & ARM PER B757 AMM 52-11 OPS CHK NML. (8581122)

Part: RATIO CHANGER — WARNING MESSAGE · airframe 91,780 hrs · 23,737 cycles

SHIP 6803 - MISC/DE - DUE TO L HYD QUANTITY LOW INDICATION CORRECTIVE ACTION: MTC FOUND LEAK COMING FROM RUDDER RATIO. REPLACED RUDDER RATIO, EDP, PTU, ACMP, AND ALL REQUIRED FILTERS. REPLACED RELAYS K105 AND K123. C/W NO GO ODI PREVENTION.

Part: NONE — NONE · airframe 91,151 hrs · 23,593 cycles

SHIP 6803 ESCAPE SLIDE ARMED CONDITION INDICATORS --L1 DOOR KNUCKLE KNOCKER INOP. CORRECTIVE ACTION: READJUSTED 1L DOOR EMERGENCY MECHANISM PER B757 AMM 52-11. OPS CK GOOD. (2412471)

Part: NONE — NONE · airframe 90,843 hrs · 23,515 cycles

SHIP 6803 DOOR OR GIRT BAR PROXIMITY SENSOR COVER DAMAGE/MISSING / LOCATIONS: 4R / ACARS TEXT: FRC5271014RSLIDE MOORING LINE OUTOF PLACE / INTERIOR. CORRECTIVE ACTION: RESECURED MOORING LINE PER B757 AMM 25-65. (2370111)

Part: NONE — NONE · airframe 90,833 hrs · 23,513 cycles

SHIP 6803 CREW REPORTS DOOR 1R WILL NOT ARM. CORRECTIVE ACTION: FOUND DEBRIS ON GIRT BAR. REMOVED DEBRIS DOOR CHECKS GOOD B757 AMM 25-66. (9023062)

Part: SKIN — DEBONDED (SLAT) · airframe 87,437 hrs · 22,730 cycles

SHIP 6803 DISBOND OF 1.800 IN. X 1.100 IN. AT OSS 305.5, LOWER SURFACE, LE SLAT 7 TRAILING EDGE WEDGE. CORRECTIVE ACTION: SUMMARY OF N.R.C. SERIAL NO.00122: LOWER SURFACE AT LE SLAT 7 ON OSS STA.305.5 OF TRAILING EDGE WEDGE WAS REPAIRED PER ERA 592987-14AD REV. ORIG. AND PER ETI-57-21-367 REV.1. (1887879)

Part: UNKNOWN — UNKNOWN · airframe 92,463 hrs · 23,897 cycles

SHIP 6803 ERA 514351-14 REV E PERFORMS AN INSPECTION OF DRY BAY AT LH WING STA 258-285, FOLLOW ON ACTION IS REQUIRED. CORRECTIVE ACTION: SUMMARY: ON DRY BAY AT LH WING WAS REPAIRED PER PRI 514351-14 REV 1. AND ER/A 514351-14 REV. F SECTION V. (1885637)

Part: STRAP — CRACKED (BS 373-377) · airframe 87,434 hrs · 22,729 cycles

SHIP 6803 CRACKED STABILIZER STRAP BTW STA 373 TO STA 377 AND LBL 24.75 AT ABOVE NLG WHEEL WELL. CORRECTIVE ACTION: REPAIRED PER SRM. (LP 1885651)

Part: NONE — NONE · airframe 92,463 hrs · 23,897 cycles

SHIP 6803 DENT ON WEDGE UPPER SURFACE, APPROX WS 258 AT SLAT NO 6. CORRECTIVE ACTION: SUMMARY OF NRC 00100: WEDGE UPPER SURFACE, APPROX WS 258 AT SLAT NO 6 WAS REPAIRED PER B757-200 SRM. (1884241)

Part: SKIN — DEBONDED (NR 6 SLAT) · airframe 87,434 hrs · 22,729 cycles

SHIP 6803 DURING INSPECTION MAINTENANCE FOUND A.A. DISBOND OF 1.100 IN. X 1.000 IN. AT ISS 137, UPPER SKIN LE SLAT 6 TRAILING EDGE WEDGE. REPAIRED PER SRM. (LP 1881248)

Part: FLOOR SUPPORT — CRACKED (BS 1320) · airframe 87,434 hrs · 22,729 cycles

SHIP 6803 CRACKED INTERCOSTALS (2 EAS) STA 1320 RBL / LBL 44 AT AFT CARGO CEILING AREA. CORRECTIVE ACTION: SUMMARY OF NRC 00129-INTERCOSTALS (2 EAS) STA 1320 RBL / LBL 44 AT AFT CARGO CEILING AREA WAS REPAIRED PER B757-200 SRM. (1878555)

Part: BOTTLE — LOW PRESSURE (R2 DOOR SLIDE) · airframe 86,468 hrs · 22,513 cycles

R2 DOOR SLIDE BOTTLE PRESSURE BELOW LIMITS. CORRECTIVE ACTION: MAINTENANCE REPLACED R2 DOOR SLIDE. SYSTEM OPERATION IS NORMAL.

Part: NONE — NONE · airframe 92,463 hrs · 23,897 cycles

SHIP 6803 DT INSPECTIONS FOR REPAIR DOUBLER AT STA 1510 BETWEEN STR 28R AND STR29 PER ER/A 569579-14. CORRECTIVE ACTION: REF ERA 569579-14. (1408669)

Part: CONNECTOR — LOOSE (CABIN) · airframe 82,000 hrs · 21,620 cycles

(AIRCRAFT 6803, L/P 6046487) SEAT-MOUNTED EMERGENCY ESCAPE PATH LIGHT AT ROW 29 INOP. FOUND CONNECTOR LOOSE. RESECURED SAME OPS CKS GOOD.

Part: SEAL — DAMAGED (APU) · airframe 81,914 hrs · 21,604 cycles

SHIP 6803- DIV - TO PDL DUE TO LT GENERATOR FAILURE FOLLOWED BY APU AUTO SHUTDOWN. CORRECTIVE ACTION: REPLACED APU OIL PER AMM 49-10. R/R APU OIL CAP SEAL AND APU STARTER SEAL REF AMM 49-20. RAN APU NO LEAKS NOTED. R/R LT IDG ASSY. OPS CK GOOD.

Part: REPAIR — GOUGED (FUSELAGE) · airframe 80,389 hrs · 21,316 cycles

SHIP 6803 EXISTING REPAIR AT STA.1280 BETWEEN STR. 9R-14R IS GOUGE. CORRECTIVE ACTION: REMOVED EXISTING REPAIR FRAME STA.1280 STR.8R-14R MAIN CABIN AND INSTALLED NEW REPAIR ON FRAME STA.1280 STR.8R-14R IAW ER/A# 576101-14AD REV. ORIGINAL. (0973819)

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 80,389 hrs · 21,316 cycles

SHIP 6803 MAIN CABIN FLOORBEAM UPPER CHORD HAS A CRACK AT RADIUS BS 700 LBL 45. CORRECTIVE ACTION: REMOVED EXISTING REPAIR FROM MAIN CABIN FLOORBEAM UPPER CHORD STA 700 LBL 45 AND INSTALLED NEW REPAIR IAW ER/A # 575613-14 REV ORIGINAL. (0970864)

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 80,389 hrs · 21,316 cycles

SHIP 6803 CRACK INDICATION NOTED ON 1 EA FASTENER HOLE STA 700 LBL 24 TOP FLOOR STIFFENER HOLE. CORRECTIVE ACTION: CUT OUT DAMAGED SECTION 1.2"X.9" AND REPAIRED STA 700 LBL 24 FLOOR STIFFENER HOLE IAW ER/A # 575613-14 REV ORIGINAL. (0970844)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,386 hrs · 21,314 cycles

SHIP 6803 FWD CABIN WET AREA FS 345 FLOORBEAM UPPER SURFACE IS CORRODED AT LBL 10. CORRECTIVE ACTION: REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS REF SRM. FABRICATED REPAIR AND INSTALLED REF SRM. (0966044)

Part: SEAT TRACK — GOUGED (BS 879) · airframe 80,386 hrs · 21,314 cycles

SHIP 6803 MAIN CABIN LH O/B SEAT TRACK STA.879 HAS GOUGE. CORRECTIVE ACTION: FOUND TO BE OUT OF LIMITS PER SRM. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW SRM. (0953300)

Part: BARRIER — DAMAGED (LT WING FUEL) · airframe 87,437 hrs · 22,730 cycles

SHIP 6803 LH WING FUEL TANK DRY BAY BARRIER-MISSING FLAME SPRAY. REPAIR PER ER/A 514351-14 REV D. CORRECTIVE ACTION: SUMMARY: DRY BAY BARRIER WAS REPAIRED PER ETI-57-21-389 REV. ORIGINAL AND ER/A 514351-14 REV. E SECTION IV. (0951439)

Part: STRINGER — CORRODED (BS 1540-1560) · corrosion level 2 · airframe 80,386 hrs · 21,314 cycles

SHIP 6803 CORROSION ON STR. 18L, BETWEEN STA 1540 TO 1560, JUST BELOW CUSP WEB. CORRECTIVE ACTION: REMOVED CORROSION AND FOUND AREA TO BE OUT OF LIMITS REF SRM. FABRICATED REPAIR AND INSTALLED IAW SRM. (0950598)

Part: FLOORBEAM — CORRODED (BS 377) · corrosion level 2 · airframe 80,386 hrs · 21,314 cycles

SHIP 6803 FWD CABIN WET AREA F.S 377.7 FLOOR BEAM UPPER SURFACE REPAIR IS CORRODED MULTIPLE PLACES BETWEEN LBL 4 AND LBL 10. CORRECTIVE ACTION: SURFACE BETWEEN LBL 4 AND LBL 10 WAS FOUND ON EXISTING REPAIR UPPER SPLICE STRAP ONLY. THIS REPAIR WAS MADE IAW B757 SRM,PERFORMED DVI INSPECTION WITH NO DEFECT NOTED, FABRICATED AND INSTALLED NEW STRAP REPAIR IAW B 757 SRM. (0942540)

Part: LIGHT — BROKEN (CABIN) · airframe 80,386 hrs · 21,314 cycles

SHIP 6803 EMERGENCY LIGHT AT LOC 31D BROKE OFF FORM THE SEAT MOUNTING. CORRECTIVE ACTION: REINSTALLED EMERGENCY LIGHT HOUSING AT 31D AS PER AMM 33-51. (3742319)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,166 hrs · 21,268 cycles

SHIP 6803 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:31D. CORRECTIVE ACTION: REINSTALLED EMERG PATH LIGHT PER AMM 33-52. (0890631)

Part: LIGHT — DAMAGED (CABIN) · airframe 80,133 hrs · 21,261 cycles

SHIP 6803 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:31D. CORRECTIVE ACTION: RESECURED 31D EMERGENCY PATH LIGHT. (0887768)

Part: BRACKET — CRACKED (R3 DOOR) · airframe 79,178 hrs · 21,071 cycles

(AIRCRAFT 6803, L/P 4835866) DURING R 3 DOOR SLIDE REPLACEMENT, FOUND UPPER AFT L BRACKET AT SLIDE PACK CRACKED. R/R DOOR 03R, UPPER AFT LT BRACKET IAW AMM 25-66. OPS CK NML. OK FOR SVC.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 77,836 hrs · 20,830 cycles

IFSD & DIV - DUE TO STATUS MESSAGES RT ENGINE SEC CONT AND RT ENGINE PRI CONT CAME ON AT FL370. DURING CLIMB TO FL390 THRUST LEVERS ADVANCED ALL ENGINE PARAMETERS RED LINED AND ENGINE UNRESPONSIVE TO THROTTLE COMMANDS A LOUD BANG AND YAW WAS EXPERIENCED, FOLLOWED QRH AND SHUT DOWN RIGHT ENGINE. REMOVED AND REPLACED THE NR 2 ENGINE REF CARDS.

Part: SKIN — CORRODED (BS 1510) · airframe 77,753 hrs · 20,815 cycles

LOWER FUSELAGE AFT OF AFT CARGO DOOR. FOUND CORROSION ON RIVETS AT ANTENNA DELETE PLATE BS 1510 BETWEEN STRINGERS 28 - 29. REMOVED THE ANTENNA BACKING DOUBLER AND DAMAGED SKIN IAW SRM 53-00-01. PERFORMED HFEC OF CUT-OUT IAW NDT PART 6 54-00-01, AND BOLT HOLE HFEC OF FASTENERS HOLES IAW NDT PART 6 51-00-01. NO ISSUES NOTED. FABRICATED A REPAIR IAW SRM 53-00-01, REPAIR 3.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 75,699 hrs · 20,398 cycles

EMERGENCY LIGHT LENS DAMAGED. REPLACED EMERGENCY LIGHT LENS.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 75,624 hrs · 20,386 cycles

(AIRCRAFT 6803, L/P 0333558) EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:607 / EMERGENCY EXIT SIGN COVER MISSING DOOR 4L / INTERIOR. INSPECTED CABIN. NO SIGN IS LOOSE OR MISSING.

Part: D-RING — UNSECURE (L2 DOOR SLIDE) · airframe 72,428 hrs · 19,789 cycles

L2 DOOR D-RING FOR SLIDE PACK FELL OUT. SECURED THE D-RING IAW AMM 52-11.

Part: SKIN — DENTED (BS 620 & 628) · airframe 71,941 hrs · 19,684 cycles

LEFT LOWER FUSELAGE HAS TWO DENTS 1 AT BS 620 STRINGER 17L THE SECOND AT BS 628 STRINER 17L. REPAIRED IAW ER/A 554321-14 REV ORIG.

Part: RECEPTACLE — CORRODED (ACTUATOR) · airframe 71,941 hrs · 19,684 cycles

THE LEFT WING SPAR ENGINE FUEL SHUTOFF VALVE ACTUATOR RECEPTICLE HAS CORROSION. REMOVED AND REPLACED THE LEFT ENGINE FUEL SHUTOFF VALVE ACTUATOR IAW 28-22-11. PERFORMED DUAL PATH WIRING CHECK AND LT ENGINE FUEL SHUTOFF VALVE ACTUATOR OPERATIONAL TEST IAW 28-22-11-404-007 AND 28-22-11-715-004. OPS CHECKED GOOD.

Part: PUSHROD — DAMAGED (DOOR GATE) · airframe 71,941 hrs · 19,684 cycles

R2 DOOR , LOWER GATE AFT PUSH ROD DAMAGED. REMOVED AND REPLACED THE R2 DOOR LOWER GATE AFT PUSH ROD IAW AMM 20-11-00-912-001 AND AMM 52-11-25-825-001. ADJUSTED AND CHECKED GOOD.

Part: SLIDER — NO TEST (GIRT BAR) · airframe 71,941 hrs · 19,684 cycles

R2 DOOR GIRT BAR AFT SLIDER FAILED MIMUM ENGAGMENT DIMENSION TEST. DOOR R-2 GIRT BAR INSTALLED.

Part: SKIN — DENTED (BS 416) · airframe 71,941 hrs · 19,684 cycles

LEFT UPPER FUSELAGE HAS ONE DENT AT BS 416 ABOVE STRINGER 13L. REPAIRED IAW ER/A 554322-14, REV ORIG.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 71,789 hrs · 19,650 cycles

R3 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED R3 DOOR EMERGENCY EXIT LIGHT LENS PER B757 AMM 33-51.

Part: BEARING — SEIZED (L4 DOOR) · airframe 71,589 hrs · 19,610 cycles

L4 DOOR WILL NOT FULLY ARM TO DETENT. FOUND BEARING ON UPPER FWD ARMING TORQUE TUBE SUPPORT SEIZED. REPLACED THE BEARING IAW CMM 52-11-25.

Part: BALLSCREW — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 67,778 hrs · 18,887 cycles

LT WING, NR 3 FLAP BALLSCREW CORRODED. BALL SCREW ASSY INSTALLED ON AMDS CARD.

Part: FRAME — GOUGED (BS 1280) · airframe 67,680 hrs · 18,863 cycles

BS 1280, FRAME GOUGED AT S-10R TO S-15R. REPAIRED BY ER/A514345-14, REV B. ERA 514345-14 UPDATED TO REV C 12 MONTH DTA TIME LIMIT IS REMOVED. LOGPAGES 1034697 AND 1863874 WILL TRACK REMAINING TIME LIMITS. CLOSED LOG AND REMOVED MONITOR INSPECTION.

Part: LIGHT — NO TEST (L3 DOOR SLIDE) · airframe 67,363 hrs · 18,795 cycles

DURING 3L DOOR SLIDE DEPLOYMENT TEST, EMERGENCY LIGHTS ON SLIDE DID NOT ILLUMINATE. ALL OTHER PARAMETERS OK. REPLACED L3 DOOR SLIDE IAW ADMS 2566-92-01-3L DOOR SLIDE INSTALLATION OK.

Part: FAN — FAILED (EQUIPMENT BAY) · airframe 65,451 hrs · 18,394 cycles

DURING APPROACH THERE WAS A PERIOD OF A BURNING ODOR SIMILAR TO KITCHEN MATCHES BURNING AT TOUCHDOWN. EQUIPMENT OVERHEAT ADVISORY MESSAGE ILLUMINATED, QRH PROCEDURE COMPLEATED MESSAGE WENT AWAY WHEN ALTERNATE SELECTED EQUIPMENT CLOG FAN STATUS MESSAGE DISPLAYED. FAN CHECKED FOR OVERHEAT, NO FAULT. FWD EQUIPMENT SUPPLY FAN 1 INOPERATIVE. CIRCUIT BREAKER SECURED, NO BURNING ODOR. R & R THE NR 1 EQUIPMENT COOLING FAN IAW MM 21-58.

Part: SKIN — DAMAGED (RT WINGLET) · airframe 65,247 hrs · 18,357 cycles

LIGHTNING STRIKE ON RT WINGLET. INSTALLED PERMANENT REPAIR TO RT WING WINGLET IAW RI 538463-14 08, AUG 15 SECTION II PERMANANT INSTRUCTIONS. CLOSED LOG AND REMOVED MON INSPECTION.

Part: SKIN — DAMAGED (LT WINGLET) · airframe 65,247 hrs · 18,357 cycles

LIGHTNING STRIKE ON LT WINGLET. INSTALLED PERMANENT REPAIR TO LT WING WINGLET IAW RI 538462-14 08 AUG 15. SECTION II PERMANENT REPAIR INSTRUCTIONS. CLOSED LOG AND REMOVED MON INSPECTIONS.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 64,957 hrs · 18,307 cycles

ELECTRIC BURNING ODOR FROM AFT GALLEY COFFEEMAKER. R & R AFT GALLEY COFFEEMAKER, LT SIDE IAW AMM 25-33-01, OPS CHECKS OK.

Part: NONE — NONE (NONE) · airframe 63,384 hrs · 18,002 cycles

FOLLOWUP TO N/R 229, LOG 1847754, ERA 514345-14AD. ACCOMPLISHED ER/A 514345-14AD, REV B SECT III ON STA R80 RT FRAME BETWEEN STR 10R & STR 14R. REF LOG PAGE 1847754

Part: REPAIR — GOUGED (FUSELAGE) · airframe 80,386 hrs · 21,314 cycles

SHIP 6803 DURING MCK THREE (3) GOUGES WERE FOUND OVER REPAIR PARTS INSTALLED PER PREVIOUS ER/A 514345-14AD, REVISION C. CORRECTIVE ACTION: REF: ERA 514345-14AD THE ERA HAS BEEN SUPERSEDED BY ERA 576101-14AD ORG. (1863874)

Part: STRUCTURE — CRACKED (RT AILERON) · airframe 63,384 hrs · 18,001 cycles

RIGHT WING AILERON AT I/B EDGE HAS A SMALL CRACK. REPAIRED IAW SRM.

Part: STRINGER — MECHANIC ERROR (BS 512) · airframe 63,384 hrs · 18,001 cycles

ER/A 522035-14, REV A, FUSELAGE, STRINGERS,S-28L, STA 512 MIS-DRILLED HOLE. REF ERA 522025-14 SECTION FOR REPAIR. 1753866

Part: FRAME — DAMAGED (BS 1280) · airframe 63,384 hrs · 18,001 cycles

SHIP 6803, REF LOG PAGE 1416739. WHILE ACCOMPLISHING SECT II OF ER/A 514345-14AD. MAINTENANCE FOUND THREE CHAFE MARKS. REMOVED -1 REPLACEMENT SECTION -2 AND -3 SPLICE, EVALUATED -2 SPICE WITH NO DAMAGE FOUND, FABRICATED -1 REPLACEMENT SECTION. PRIMED AND INSTALLED -1, -2 AND -3, REPAIR PARTS AT BS 1280 BETWEEN STR 8R TO STR 14R ALL IAW SRM. REF ERA514345-14, REV A.

Part: STRINGER — DAMAGED (BS 512) · airframe 62,775 hrs · 17,845 cycles

STRINGER 28L BS 512 DAMAGED. REPAIRED IAW ERA 522035-14, REV A.

Part: OVEN — CONTAMINATED (GALLEY) · airframe 60,621 hrs · 17,420 cycles

F/A HAD A BURNING ODOR AND SMOKE FROM REAR GALLEY WHILE HEATING MEALS. F/A PULLED CIRCUIT BREAKER AND SMOKE CLEARED. FOUND BURNED PAPER IN NR 5 OVEN. REMOVED PAPER, CLEANED OVEN, OPS CK NORMAL. AS PRECAUTIONARY, DEFERED TO NEF 25-34-02. NR 5 OVEN REPLACED ON 6-17-14.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,378 hrs · 17,376 cycles

DURING SERVICE CHECK, RED EMERGENCY LIGHT INOPERATIVE AT R2 DOOR. R & R RED EMERGENCY LIGHT ASSY IAW AMM 33-51 AND WDM. OPS CHECKED GOOD.

Part: FRAME — GOUGED (BS 1280) · airframe 63,384 hrs · 18,001 cycles

BS 1280, FRAME, S-10R TO S-15R, GOUGES INSPECTION REQUIRED TO DETERMINE FASTENER TYPES, SIZES USED, REF ERA 514345-14.

Part: SKIN — DENTED (BS 618) · airframe 59,387 hrs · 17,169 cycles

FUSELAGE, SKIN BS 618, S16L DENTED. REPAIRED IAW ERA 513922-14AD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,817 hrs · 17,050 cycles

DURING SERVICE CHECK, FOUND MULTIPLE LIGHTS INOPERATIVE. REPLACED LAMPS. OPS CHECKED GOOD.

Part: GROUND STUD — LOOSE (EMERGENCY LIGHTS) · airframe 58,751 hrs · 17,036 cycles

EMERGENCY LIGHT OVER SEAT 43CBA IS INOPERATIVE. FOUND NUT ON GROUND STUD GD491 LOOSE, TIGHTENED NUT, OPS CHECKED GOOD. OK FOR SERVICE.

Part: WEB — CORRODED (AFT CARGO DOOR) · airframe 56,122 hrs · 16,548 cycles

AFT CARGO DOOR INTERIOR STRUCTURE, FWD FRAME WEB FLANGE BOTTOM AREA CORRODED. REPAIRED IAW ERA 514352-14, REV ORIGINAL, PART 2.

Part: SEAT TRACK — CORRODED (BS 377-382) · airframe 56,122 hrs · 16,548 cycles

MAIN CABIN, BS 377 TO 382, LBL 45, SEAT TRACK HAS CORROSION. REPLACED SEAT TRACK SECTION IAW SRM 53-10-52, DETAIL 2, PG 3 AND 51-40-02, PG 7.

Part: SKIN — DAMAGED (BS 600-660) · airframe 71,941 hrs · 19,684 cycles

FUSELAGE SKIN BS 600 - 660, STRINGERS 15 - 18L DENTED AND GOUGED. REPAIRED IAW NR/A 513922-14AD REV A.

Part: GATE — CORRODED (R2 DOOR) · airframe 56,122 hrs · 16,548 cycles

R2 DOOR LWR GATE HAS CORROSION ON LWR EDGE SURFACES. R & R PART IAW CMM 52-11-15.

Part: GATE — CORRODED (L2 DOOR) · airframe 56,122 hrs · 16,548 cycles

L2 DOOR LWR GATE HAS CORROSION ON BOTH LWR EDGE SURFACES. REPLACED L2 DOOR LWR GATE IAW CMM 52-11-15.

Part: FLOORBEAM — DAMAGED (BS 1280) · airframe 56,122 hrs · 16,548 cycles

MAIN CABIN FLOORBEAM BS 1280, LBL10 HAS DOUBLE DRILLED HOLE. REPAIRED IAW SRM 53-00-51, FIG 201, REPAIR 5.

Part: SEAT TRACK — CORRODED (BS 632-636) · airframe 56,122 hrs · 16,548 cycles

SEAT TRACK BS 632-636, RBL 24-75 HAS CORRODED AND GOUGED. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 3.

Part: SEAT TRACK — CHAFED (BS 440-500) · airframe 56,122 hrs · 16,548 cycles

MAIN CABIN SEAT TRACK STA 440-500, RBL 24 HAS CHAFE/WARE MARKS IN MULTIPLE AREAS. REPAIRED IAW SRM 53-00-52, REPAIR 3.

Part: SEAT TRACK — CORRODED (BS 1320-1540) · airframe 56,122 hrs · 16,548 cycles

MAIN CABIN SEAT TRACK, BS 1320-1540, RBL 45.5 HAS CORROSION, DEEP SCRATCHES. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 3.

Part: CUSP WEB — CORRODED (BS 1380-1400) · airframe 56,122 hrs · 16,548 cycles

MAIN CABIN RT CUSP WEB BS 1380-1400, RBL 58, CORRODED. REPLACED CUSP WEB IAW SRM 51-40-02.

Part: CUSP WEB — CORRODED (BS 1360-1380) · airframe 56,122 hrs · 16,548 cycles

MAIN CABIN RT CUSP WEB BS 1360-1380, RBL 58 CORRODED. REPLACED CUSP WEB IAW SRM 51-40-02, PAGE 21.

Part: SEAT TRACK — CORRODED (BS 377-382) · airframe 56,122 hrs · 16,548 cycles

MAIN CABIN BS 377 TO 382, LBL 45, SEAT TRACK HAS CORROSION. REPLACED SEAT TRACK SECTION IAW SRM 53-10-52, DETAIL II, PG 3 AND 51-40-02, PG 7.

Part: FLOORBEAM — CORRODED (FS 700 LBL24) · airframe 56,122 hrs · 16,548 cycles

MX DISCOVERED CORROSION FUSELAGE/TRANSVERSE FLOORBEAM, FS 700, LBL24, UPPER CHORD. REPAIRED IAW ERA 481777-14.

Part: FRAME — DENTED (BS 1520 S25-26L) · airframe 56,122 hrs · 16,548 cycles

AFT CARGO LEFT FRAME DENTED BS 1520, S25-26L. REPAIRED SRM 53-00-07, FIG 201, REPAIR 5.

Part: FRAME — DENTED (BS 600 S24L) · airframe 56,122 hrs · 16,548 cycles

FWD CARGO FRAME DENTED AT BS 600 INBD & OTBD OF STR 24L. ACCOMPLISHED SRM REPAIR SRM 53-00-07, FIG 201, REPAIR 5, DET III.

Part: FRAME — DENTED (BS 580) · airframe 56,122 hrs · 16,548 cycles

FWD CARGO LT FRAME BS 580, S22-24L HAS DENTS. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 5, DETAIL 1.

Part: FRAME — DENTED (BS 1560) · airframe 56,122 hrs · 16,548 cycles

AFT CARGO LT FRAME DENTED BS 1560, S25-26L. ACCOMPLISHED REPAIRS IAW SRM 53-00-07 FIG 201, REPAIR 5.

Part: FRAME — DENTED (BS 1420) · airframe 56,122 hrs · 16,548 cycles

AFT CARGO FRAME DENTED, BS 1420, S25-26L. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 5.

Part: FRAME — DENTED (BS 1440) · airframe 56,122 hrs · 16,548 cycles

AFT CARGO FRAME DENTED STA 1440 S25-26L. REPAIRED IAW SRM 53-00-07, FIG 201 REPAIR 5.

Part: FRAME — CORRODED (CARGO DOOR) · airframe 56,122 hrs · 16,548 cycles

AFT CARGO DOOR INTERIOR STRUCTURE FWD FRAME WEB FLANGE BOTTOM AREA CORRODED. REPAIRED IAW ER/A 514352-14, REV ORIGINAL PART 2.

Part: WEB — CORRODED (AFT CARGO DOOR) · airframe 56,122 hrs · 16,548 cycles

AFT CARGO DOOR INTERIOR STRUCTURE AFT FRAME WEB FLANGE BOTTOM AREA CORRODED. REPAIRED IAW ER/A 514352-14, REV ORIGINAL.

Part: SKIN — CORRODED (BS 1510) · airframe 56,122 hrs · 16,548 cycles

CORROSION FOUND ON FUSELAGE SKIN UNDER AIRFONE ANTENNA STA 1510 BETWEEN S28-29L. REPAIRED IAW ER/A 515011-14, REV ORIGINAL.

Part: SKIN — DENTED (BS 1590 S28-29L) · airframe 56,122 hrs · 16,548 cycles

LOWER FUSELAGE EXTERNAL SKIN HAS A DENT AT BS 1590, BETWEEN S28-29L. REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 7.

Part: SKIN — DENTED (BS 1499) · airframe 56,122 hrs · 16,548 cycles

RIGHT EXTERNAL FUSELAGE SKIN HAS A PROTRUDING DENT AT BS 1499 BETWEEN S22-23R. REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 3.

Part: SKIN — DAMAGED (BS 424.5) · airframe 56,122 hrs · 16,548 cycles

RT EXTERNAL FUSELAGE SKIN HAS A CREASE AT BS 424.5, BETWEEN S21-22R. REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 3.

Part: GATE — CORRODED (R1 DOOR) · airframe 56,122 hrs · 16,548 cycles

R1 DOOR LOWER GATE HAS CORROSION ON LOWER EDGE SURFACE. REPLACED LOWER GATE IAW AMM 52-16-12.

Part: SKIN — GOUGED (BS 608-621) · airframe 56,122 hrs · 16,548 cycles

LT EXTERIOR FUSELAGE REPAIR DOUBLER, STA 608-621 BETWEEN STRINGERS 15L-17L HAS GOUGES. ACCOMPLISHED REPAIR IAW PRI 513922-14, AD REV ORIG.

Part: GATE — CORRODED (R2 DOOR) · airframe 56,122 hrs · 16,548 cycles

R2 DOOR LOWER GATE HAS CORROSION ON LWR EDGE SURFACES. R & R GATE IAW CMM 52-11-15.

Part: GATE — CORRODED (L2 DOOR) · airframe 56,122 hrs · 16,548 cycles

L2 DOOR LOWER GATE HAS CORROSION ON BOTH LOWER EDGE SURFACES. REPLACED L2 DOOR LOWER GATE IAW CMM 52-11-15.

Part: GATE — CORRODED (L1 DOOR) · airframe 56,122 hrs · 16,548 cycles

L1 DOOR LOWER GATE HAS CORROSION ON LWR EDGE SURFACES. REPLACED LOWER GATE IAW AMM 52-11-38--404-009.

Part: SLIDE — LOW PRESSURE (L3 DOOR) · airframe 54,042 hrs · 16,143 cycles

L3 EMERGENCY EXIT DOOR SLIDE LOW PRESSURE PRESSURE INDICATOR BEFORE GREEN BAND. REMOVED AND INSTALLED L3 DOOR SLIDE IAW JIC OPN 78020.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,503 hrs · 15,094 cycles

FUSELAGE STATION 1640 FLOORBEAM CORRODED MULTIPLE AREAS PSV 11 NR CARDS 44, 216, 217, 218.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,503 hrs · 15,094 cycles

FUSELAGE STATION 365 FLOORBEAM CORROSION APPROX B/L 0 THROUGH THE R1 DOOR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,503 hrs · 15,094 cycles

CORROSION DAMAGE WAS FOUND TO THE UPPER CHORD OF THE STA 324 FLOORBEAM FROM RBL 33 TO THE O/B END. THE SUBJECT CHORD WILL BE REMOVED AND A NEW SECTION WILL BE SPLICED IN. THE SUBJECT CHORD IS MADE FROM 7075-T6511 ALUMINUM EXTRUSION PER AND 10136-2409.

Part: ENGINE — FLAMED OUT (NR 2) · airframe 46,426 hrs · 14,692 cycles

DURING CRUISE FLIGHT THE NR 2 ENGINE FLAMED OUT. FLIGHT CREW DIVERTED THE AIRCRAFT TO SNN AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE. (2010-D1391) (DL75E103239)

Part: FLOORBEAM — CRACKED (STA 700 LBL 24) · airframe 43,902 hrs · 14,194 cycles

DURING PSV 10, THE CABIN FLOORBEAM AT STA 700, LBL 24 WAS FOUND TO BE CRACKED ON THE UPPER CAP. REPAIR WAS ACCOMPLISHED IAW THE SRM AND ERA 481777-14.

Part: SKIN — DENTED (STA 617 STR 15L) · airframe 43,902 hrs · 14,194 cycles

DURING PSV 10, THE FUSELAGE SKIN WAS FOUND TO BE DENTED AT STA 617 AT STRINGER 15L AND 16L. REPAIR WAS ACCOMPLISHED IAW ERA 481715-14

Part: ADC — MALFUNCTIONED (LEFT) · airframe 42,402 hrs · 13,917 cycles

REJECTED TAKEOFF AT 80 KNOTS. NO AIRSPEED INDICATION CAPTAIN SIDE ACCOMPLISHED REMOVAL AND REINSTALL OF LT ADC. CARRIED OUT L ADC TEST. OPS NOW NML. ACFT OK FOR CONTINUED SERVICE. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: ADC — INOPERATIVE (E/E BAY) · airframe 42,402 hrs · 13,917 cycles

ACFT DID A RTO AT 90 KTS DUE TO THE LT AIRSPEED INDICATOR BEING INOPERATIVE. MX FOUND BOTH THE LT AIRSPEED INDICATOR AND ALTIMETER INOP. PERFORMED ADC TEST TWICE SYS OPERATES NORMALLY. ACCOMPLISHED REMOVAL AND REINSTALL OF LT ADC. CARRIED OUT L ADC TEST. OPS NOW NORMAL. ACFT OK FOR CONTINUED SVCE. ETOPS CATEGORY 'E': PROBLEMS WITH SYS CRITICAL TO ETOPS.

Part: SWITCH — SHORTED (COCKPIT) · airframe 41,682 hrs · 13,782 cycles

A/C ABORTED TAKEOFF DUE TO TAKEOFF CONFIGURATION MTC FOUND SPEED BRAKE ARMING AND DETENT SWITCH BAD. REPLACING SAME, ALSO FOUND BROKEN WIRE IN PEDESTAL REPAIRED SAME.

Part: HYDRAULIC SYSTEM — OVERSERVICED (RIGHT SYS) · airframe 37,867 hrs · 13,060 cycles

ON TAXI OUT R HYD SYSTEM PRESSURE AND BRAKE SOURCE EICAS LIGHT ILLUMINATED AND R SYS PRESS OVERHEAD LIGHT ILLUMINATED ALL BRAKE PRESSURE INDICATE NORMAL. FOUND RT HYD SYS OVER SERVICED. DRAINED RT HYD SYS TO PROPER LEVEL. REMOVED AND REPLACED RT HYD SYS PRESSURE SWITCH S32 PER AMM LEAK CHK GOOD RT HYD PRESSURE LIGHT AND SYS NOW CHK NML.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 37,750 hrs · 13,042 cycles

L1 WINDSCREEN EXTERNAL PLY CRACKED. REMOVED AND REPLACED 1 LEFT WINDSHIELD IAW MM 56-11-01 POWER TERMINALS NEED RETORQING WITHIN 500 HOURS.

Part: LIGHT — MISSING (CABIN)

SEA - EMERGENCY PATH LIGHT AT ROWS 2 AND 3 INOPERATIVE. REPLACED MISSING LIGHT STRIP FOR EMERGENCY PATH LIGHT AT ROWS 2 AND 3. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGNECY LIGHT)

SEA - EMERGENCY ESCAPE PATH LIGHTING SYSTEM AT RIGHT AFT LAVATORY INOPERATIVE. RECONNECTED LIGHT STRIP FOR EMERGENCY ESCAPE PATH LIGHTING SYSTEM AT RIGHT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — BROKEN (EMERGENCY LIGHT)

SEA - EMERGENCY ESCAPE PATH LIGHT AT RIGHT AFT LAVATORY HAS BROKEN LENS. REPLACED BROKEN LENS FOR EMERGENCY ESCAPE PATH LIGHT AT RIGHT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — BROKEN (EMERGENCY LIGHT)

SEA - EMERGENCY ESCAPE PATH LIGHT AT ROWS 2 AND 3 HAVE BROKEN LENS. REPLACED EMERGENCY LIGHT LENS AT ROWS 2 AND 3. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LGA - EMERGENCY LIGHTS IN AFT TAIL COMPARTMENT INOPERATIVE. REPLACE BATTERY PACK AND REPAIRED BROKEN WIRE FOR EMERGENCY LIGHTS IN AFT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: GUIDE VANE — LEAKING (ENGINE)

DFW INFLIGHT T450/28OCT - AFTER TAKEOFF, RIGHT ENGINE OIL TEMPERATURE INDICATED 184 DEGREES FOLLOWED BY HEAVY SMOKE IN COCKPIT AND CABIN. SOURCE CLEARED WHILE ON APPROACH AND OIL TEMPERATURE RETURNED TO NORMAL. FOUND OIL LEAKING FROM VARIABLE GUIDE VANES ON NUMBER TWO ENGINE. REPLACED NUMBER 2 ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: A/C PACK — SMOKE (RIGHT)

MCO - INFLIGHT SHORTLY AFTER TAKEOFF HAD A STRONG OIL SMELL WITH VERY LITE SMOKE IN THE CABIN. SHUT OFF THE RIGHT PACK AND THE SMELL CLEARED. ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FMC — FAILED (COCKPIT) · airframe 16,106 hrs · 4,915 cycles

AIRCRAFT RETURNED FROM FLIGHT AT LAX TWICE WITH A DUAL FMC FAILURE. THE FIRST TIME THE RT FMC COMPUTER WAS REPLACED, (P/N 4052506-941-945). THE SECOND TIME THE AIRCRAFT WAS REMOVED FROM SERVICE. CHECK-C 11-20-99 LAX.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,504 hrs · 4,113 cycles

THE RT SIDE NR 3 CABIN DOOR EXIT LIGHT WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 11-20-99 LAX. ---CLOSED---

Part: ENGINE — FAILED (LEFT) · airframe 12,278 hrs · 3,701 cycles

JUST AFTER TAKEOFF AT 900 FT AGL, THE LEFT ENGINE SURGED. TOWER REPORTED MOMENTARY FIRE OUT THE ENGINE, THE ENGINE WAS SHUT DOWN. THERE WAS NO FIRE WARNING BUT THE CREW ELECTED TO FIRE ONE FIRE BOTTLE. FLIGHT RETURNED TO MCO. BORESCOPE REVEALED COMPRESSOR DAMAGE AND THE ENGINE WAS CHANGED. CHECK-C 11-20-99 LAX.

Part: SKIN — CORRODED (WS 300-360)

FOUND CORROSION ON LT WING SKIN SURFACE FROM FRONT TO REAR SPAR UNDER THE BLACK ICE DETECTION STRIPE, STA 300 TO 360. REMOVED BLACK ICE DETECTION STRIPE. CLEANED CORROSION FROM SURFACE OF WING SKIN AND REPLACED TWO FASTENERS DUE TO CORROSION. CLEANED HOLES FROM SAME. ALODINED AND PRIMER PAINTED WING SKIN SURFACE. REPAIRED PER 737-300 SRM 57-20-01, FIG 101 AND 102. CHECK-C 7-19-98 LAX.

Part: SKIN — CORRODED (WS 300-360)

FOUND CORROSION AROUND MANY FASTENERS AND ON RT WING SKIN SURFACE UNDER BLACK ICE DETECTION STRIPE, FRONT TO REAR SPAR, STA 300 TO 360. REMOVED BLACK ICE DETECTION STRIPE. CLEANED CORROSION FROM SURFACE OF WING SKIN. REMOVED AND REPLACED 235 FASTENERS AND CLEANED HOLES FROM SAME DUE TO CORROSION. PRIMER PAINTED WING SKIN SURFACE AND ALODINED. REPAIRED PER 737-300 SRM 57-20-01, FIG 101 AND 104. CHECK-C 7-19-98 LAX.

Part: WIRE — LOOSE (CABIN)

FOUND FIRST CLASS FLOOR EGRESS LIGHT STRIP INOPERATIVE. FOUND STRIP UNPLUGGED. SECURED CABLE. CHECK-C 7-19-98 LAX.

Part: CONNECTOR — LOOSE (CABIN)

EGRESS LIGHT INOP BY L-1 DOOR. SECURED CONNECTOR AND TRACK COVER. CHECK-C 01, 7-19-98 LAX.

Part: CONNECTOR — DAMAGED (CABIN)

EGRESS LIGHTS INOP IN FRONT OF LAV DOOR LT BEHIND FIRST CLASS. REPAIRED FLEX CABLE ASSY CONNECTORS MFG PN'S 65801-003 AND 97F9705. CHECK-C 01.

Part: LAMP — FAILED (CABIN)

EMERGENCY AISLE LIGHT INOP AT ROW 17 FED, RELAMPED. CHECK-C 01, 7-19-98 LAX.

Part: PANEL — CRACKED (LT WING)

DURING CK-C01, FOUND LT WING TOP L/E PANEL AT OTBD END OF NR 4 L/E SLAT HAS A 7 INCH CRACK. DRESSED OUT DAMAGED AREA AND INSTALLED HOT BOND REPAIR PER SRM 51-70-07 PG 40 AND SRM 57-41-01 PG 20. (X)