N702TW

Part: DOOR — FOD (ZONE 800) · airframe 97,533 hrs · 25,608 cycles

SHIP 6801 KNUCKLE KNOCKER ON L1 NOT IN CORRECT ARMED POSITION. CORRECTIVE ACTION: CLEARED DEBRI FROM DOOR OPS CK GOOD OF ARMING IAW B 757 AMM 25- 66. (5128810)

Part: INDICATOR — OUT OF POSITION (ZONE 800) · airframe 97,544 hrs · 25,610 cycles

SHIP 6801 DOOR 2R KNUCKLE KNOCKER NOT IN CORRECT POSITION WHEN ARMED. CORRECTIVE ACTION: PERFORMED ADJUSTMENT/TEST TO DOOR 2R KNUCKLE KNOCKER IAW B757 AMM 25-66. OPS CHECK NML. (5128816)

Part: INDICATOR — STUCK (ZONE 800) · airframe 97,383 hrs · 25,576 cycles

SHIP 6801 1L DOOR ARMED KNUCKLE KNOCKER STICKS. CORRECTIVE ACTION: FOUND DOOR TRIM BLOCKING KNUCKLE KNOCKER. RESECURED AND OPS NML PER B757 AMM 52-11. (5611162)

Part: GIRT BAR — FOD (R1 DOOR) · airframe 96,875 hrs · 25,461 cycles

R1 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT. REF B757 AMM 25-66. REMOVED DEBRIS FROM SLIDE GIRT BAR FITTINGS. ENGAGED SLIDE SEVERAL TIMES. NOW OPS NORMAL.

Part: INDICATOR — OBSTRUCTED (DOOR) · airframe 96,691 hrs · 25,420 cycles

DOOR ARMED KNUCKLE KNOCKER INOPERATIVE. ADJUST DOOR SHROUD AROUND THE KNUCKLE KNOCKER, OPS CHECKED NORMAL IAW AMM 25-66.

Part: ANNUNCIATOR — INOPERATIVE (L1 DOOR SLIDE) · airframe 95,814 hrs · 25,231 cycles

SHIP 6801 1L DOOR ESCAPE SLIDE ARMED CONDITION ANNUNCIATOR INOP. CORRECTIVE ACTION: COULD NOT REPLICATE FAULT. T/S PER B757 AMM 52-11. OPS CHECK NORMAL. (0266788)

Part: LIGHT — MALFUNCTIONED (L1 DOOR SLIDE) · airframe 95,675 hrs · 25,202 cycles

SHIP 6801 1L SLIDE LIGHT REMAINS DIMLY ON WHEN DOOR DISARM. CORRECTIVE ACTION: NO FAULTS FOUND. CYCLED, ARMED & DISARMED POSITION. OPS CHK NML. REF B757 AMM 52-11. (5731272)

Part: ROPE — UNSECURE (L4 DOOR SLIDE) · airframe 95,353 hrs · 25,121 cycles

SHIP 6801 L4 DOOR SLIDE PACK HAS ROPE HANGING OUT. CORRECTIVE ACTION: STOWED L4 SLIDE PACK MOORING LINE- B757 AMM 2566- SLIDE ARMS NML. (5024750)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,901 hrs · 24,997 cycles

SHIP 6801 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOPERATIVE / LOCATIONS:42D. CORRECTIVE ACTION: RESECURED LIGHT ASSY. OPS NORMAL. (0098548)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,811 hrs · 24,980 cycles

SHIP 6801 4L SLIDE LANYARD HANGING OUT AND 4R SLIDE COVER LATCH UNDONE. CORRECTIVE ACTION: FOUND 4L AND 4R COVER LATCH/STRAP LOOSE, RESECURED BOTH DOORS LATCH/STRAP PER B757 AMM 25-66. OK FOR SERVICE. (5027784)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,097 hrs · 24,829 cycles

SHIP 6801 4L DOOR WON'T TO OPEN. CORRECTIVE ACTION: ADJUSTED GUIDE ARM AND DOOR OPS NML PER B757 AMM 52-11. (4691622)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,037 hrs · 24,814 cycles

SHIP 6801 KNUCKLE KNOCKER STICKS AT 2R. CORRECTIVE ACTION: FREED KNUCKLE KNOCKER - OK FOR SRVC. (4691609)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,845 hrs · 24,771 cycles

SHIP 6801 DOOR 1L SLIDE LIGHT DOES NOT ILLUMINATE WHEN ARMED. CORRECTIVE ACTION: REMOVED DEBRIS FROM GIRT BAR SLIDER FLOOR MOUNTS. OPN 1L DOOR SLIDE LIGHT CKS NML. (4409544)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,435 hrs · 24,669 cycles

SHIP 6801 KNUCKLE KNOCKER, ON DOOR 4 L WILL NOT FULLY RETRACT WHEN DOOR IS DISARMED. CORRECTIVE ACTION: REMOVED DEBRIS BLOCKING KNOCKER. KNOCKER OPERATES NORMALLY. (4646220)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,419 hrs · 24,666 cycles

SHIP 6801 SLIDE LIGHT NOT ILLUMINATED / INTERIOR 1L. CORRECTIVE ACTION: REMOVED DEBRIS FROM GIRT BAR OPS CHK GOOD. (2801954)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 93,201 hrs · 24,619 cycles

SHIP 6801 AD - AA // DAMAGES WERE FOUND AT RH ENG DRAF FTG CLAM-UP IN HOLES 11 TO 18 AS FOLLOW: HOLE #11 CORROSION ON SKIN BETWEEN 8-9 CLOCK POSITION, HOLE #12 SCRATCHES ON SKIN AND FITTING ALL AROUND, HOLE #13 CORROSION ON SKIN BETWEEN 12-3 AND GOUGE ON FITTING EDGE AT 12 CLOCK POSITIONS, HOLE #14 CORROSION ON SKIN BETWEEN 12-3 AND FITTING BETWEEN 8-9 CLOCK POSITIONS, HOLE #15 SCRATCHES ON SKIN AND FITTIN BETWEEN 2-3 CLOCK POSITION, HOLE #16 CORROSION ON SKIN BETWEEN 10-12 AND FITTING AT 3 CLOCK POSITIONS, HOLE #17 CORROSION ON SKIN ALL AROUND, HOLE #18 CORROSION ON SKIN AT 12 AND FITTING BETWEEN 2-3 CLOCK POSITIONS IN REFERENCE TO CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00170 CORROSION LEVEL 2 HOLES #11 #12 #13 #14 #15 #16 #17 AND #18 WERE REPAIRED PER ER/A 576658-14AD REV:B; SECTION VII: PERMANENT REPAIR. (2771240)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 93,201 hrs · 24,619 cycles

SHIP 6801 A.D.//A.A. DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP & DRAG BRACE AS FOLLOW: HOLE #1 CORROSION AND SCRATCHES ON SKIN AND FITTING BTW 6 TO 12 O CLOCK POSITION. HOLE #2 CORROSION ON SKIN AND FITTING ALL AROUND HOLE. HOLE #3 CORROSION AND SCRATCHES ON SKIN AND FITTING ALL AROUND HOLE. HOLE #4 CORROSION ON SKIN AND FITTING ALL AROUND HOLE. HOLE #5 CORROSION ON SKIN AND FITTING BTW 1 TO 3; 5 TO 7; 9 TO 11 O CLOCK POSITION. HOLE #6 CORROSION ON SKIN AND FITTING BTW 5 TO 7; 11-1 O CLOCK POSITION. HOLE #7 CORROSION ON SKIN AND FITTING BTW 7 TO 1 O CLOCK POSITION. HOLE #8 CORROSION ON SKIN AND FITTING ALL AROUND HOLE. HOLE #9 CORROSION ON SKIN AND FITTING BTW 10 TO 11 O CLOCK POSITION & HOLE #10 SCRATCHES ON SKIN AND FITTING ALL AROUND HOLE. IN REF. CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00156: CORROSION LEVEL 2 HOLE #5, #9 AND #10 WERE REPAIRED PER CARD 5720-01100-04A AND HOLES #1, #2, #3, #4, #6, #7 AND #8 WERE REPAIRED PER ER/A 608123-14AD REV. ORIGINAL SECTION I: PERMANENT REPAIR. (2770852)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 93,201 hrs · 24,619 cycles

SHIP 6801 A.D.//A.A. DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP & DRAG BRACE AS FOLLOW: HOLE #11 SCRATCHES ON SKIN AND FITTING ALL AROUND HOLE AND GOUGE ON FITTING AT 11 O CLOCK POSITION. HOLE #12 SCRATCHES ON SKIN AND FITTING ALL AROUND HOLE. HOLE #13 CORROSION ON SKIN AND FITTING BTW 10 TO 11 O CLOCK POSITION AND SCRATCHES ON SKIN AND FITTING ALL AROUND HOLE. HOLE #14 CORROSION ON SKIN AND FITTING BTW 3 TO 5; 9 TO 11 O CLOCK POSITION. HOLE #15 SCRATCHES ON SKIN AND FITTING ALL AROUND HOLE. HOLE #16 SCRATCHES ON SKIN AND FITTING ALL AROUND HOLE AND CORROSION ON SKIN AND FITTING BTW 7 TO 11 O CLOCK POSITION. HOLE #17 CORROSION ON SKIN AND FITTING BTW 2 TO 5; 8 TO 10 O CLOCK POSITION & HOLE #18 CORROSION ON SKIN AND FITTING BTW 3 TO 5; 8 TO 11 O CLOCK POSITION IN REF. CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00157 HOLES #11 #12 #13 #14 #15 #16 #17 AND #18 WERE REPAIRED PER ER/A 608123-14AD REV. ORIGINAL; SECTION I: PERMANENT REPAIR AND WITH NRC 00156. (2771163)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 93,201 hrs · 24,619 cycles

SHIP 6801 AD - AA // DAMAGES WERE FOUND AT RH ENG DRAF FTG CLAM-UP IN HOLES AS FOLLOW: HOLE #1 CORROSION ON SKIN AND FITTING ALL AROUND, HOLE #2 SCRATCHES ON SKIN ALL AROUND AND ELONGATED FITTING, HOLE #3 CORROSION ON SKIN AND FITTING ALL AROUND, HOLE #4 CORROSION ON SKIN AND FITTING BETWEEN 10-1 CLOCK POSITION, HOLE #5 CORROSION ON SKIN BETWEEN 9-11 AND GOGUGE ON FITTING EDGE AT 1 CLOCK POSITIONS, HOLE #6 SCRATCHES ON FITTING BETWEEN 7-10 CLOCK POSITION, HOLE #7 CORROSION ON SKIN AND FITTING ALL AROUND, HOLE #8 CORROSION ON SKIN AND FITTING ALL AROUND, HOLE #9 CORROSION ON FITTING BETWEEN 4-9 CLOCK POSITION, HOLE #10 CORROSION ON KIN AND FITTING AT 6 CLOCK POSITION IN REFERENCE TO CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00169: HOLE #4 AND HOLE #5 WERE REPAIRED PER CARD 5720-01100-04B AND HOLE #1, #2, #3, #6, #7, #8, #9 AND #10 WERE REPAIRED PER ER/A 576658-14AD REV:B; SECTION VII: PERMANENT REPAIR. (2771040)

Part: SKIN — CRACKED (LT WING) · airframe 95,970 hrs · 25,262 cycles

SHIP 6801 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING / CRACKS / CORROSION & GOUGES. CORRECTIVE ACTION: REF ERA 608123-14AD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,186 hrs · 24,615 cycles

SHIP 6801 PROTUBERANCES (2) ON EXTERNAL FUSELAGE SKIN BTW STA 395 AND BTW S-23L - S-24L. CORRECTIVE ACTION: SUMMARY OF NRC 00009 PROTUBERANCES (2) ON EXTERNAL FUSELAGE SKIN AT STA 395 AND BTW S-23L/S-24L WERE REPAIRED PER PRI NO.607955- 14 REV.3 AND ER/A NO.607955-14 REV. ORIGINAL, SECTION I. (2759265)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,186 hrs · 24,615 cycles

SHIP 6801 DTA MONITOR INSPECTION LOG REF ERA 607955-14. CORRECTIVE ACTION: REF ERA 607955-14. (2759098)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,186 hrs · 24,615 cycles

SHIP 6801 IN REF TO AMDS 2040-0191-1R: LENGTH OF THE PIN EXTENSION ROTARY SNUBBER FLUID LEVEL ARE -0.093 IN/60 F AND THE MINIMUM LENGHT ARE 0.0 IN/70 F THEREFORE IS OUT OF LIMITS AT R1 DOOR. CORRECTIVE ACTION: SUMMARY OF NRC S/N 00103: SNUBBER AT R1 DOOR WAS REMOVED AND SERVICEABLE SNUBBER WAS INSTALLED PER B757-200 AMM 52-11. (2746674)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,186 hrs · 24,615 cycles

SHIP 6801 A. A. - A.D. DISBOND (2.200 IN X 1.100 IN) ON ISS 257 UPPER SURFACE, LE SLAT 5 TRAILING EDGE WEDGE, LH WING. CORRECTIVE ACTION: SUMMARY OF NRC: 00050 ON ISS 257 UPPER SURFACE, LE SLAT 5 TRAILING EDGE WEDGE, LH WING. WAS REPAIRED PER REPAIR PER B757- 200 S.R.M. (2730719)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 92,942 hrs · 24,565 cycles

SHIP 6801 STRONG MUSTY SOCK SMELL IN COCKPIT DURING T/O, LASTED APPROX 5 MINS. FA AT DOOR 4 ALSO REPORTED SMELL. SMOKE + FUMES QUESTIONNAIRE FILLED OUT. CORRECTIVE ACITON: C/W BLOCKS 3 AND 4 OF B757 FIM TASK 71-05-00-815-811-P00. FOUND OIL WETNESS ON NBR 2 ENG 2.5 BLEED AREA. REMOVED NBR 2 ENG BORO PLUG AP-1 PER B757 AMM 72-00. REMOVED NBR 2 ENG INLET CONE FRONT SECTION PER B757 AMM 72-31. ENGINE SHOP SUPPORT INSPECTED AREAS AND FOUND NO CURRENT RESIDUAL OIL. HIGH POWER ENG RUN REQUIRED. REINSTALLED BORO PLUG AP-1 PER B757 AMM 72-00. REINSTALLED NBR 2 ENG INLET CONE FRONT SECTION PER B757 AMM 72- 31. REMOVED #1 + #2 ENG AP 1 PLUGS PER B757 AMM 72-00. REMOVED #1 + #2 ENG SPINNER CONES PER B757 AMM 72-31. BSI OF #1 AND #2 ENG VIA AP 1 PLUG NO WETTNESS NOTED. REINSTALLED AP 1 PLUGS ON EACH ENGINE PER B757 AMM 72- 00. REMOVED #1 + #2 LPC SHAFT PLUGS AND INSPECTED FOR WETNESS. BOTH DRY. REINSTALLED PLUGS PER PW2037 EM 72-00-31. REINSTALLED #1 + #2 FWD CONES PER B757 AMM 72-31. INSPECTED 2.5 BLEED AREA ON #1 + #2 ENGINES, NO OIL WETNESS. COMPLETED B757 FIM 71-05. NO FINDINGS. C/W FIM B757 21-00-01/301. NO CONTAMINATION FOUND. HIGH POWER RUNS COMPLETED PRIOR TO SECOND SET OF INSPECTIONS. C/W NO GO ODI B757 21-72.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,589 hrs · 24,482 cycles

DURING SVC FOUND OVERHEAD EMERGENCY LIGHTS 23D, 3C, 1C INOP. REPLACED LIGHT BULBS IN ALL 3 LOCATIONS, 23D, 3C, 1C AS WELL AS CHARGING UNIT AT M730 LOCATION OP CK NORMAL.

Part: SIGN — UNSECURE (FWD GALLEY) · airframe 92,466 hrs · 24,453 cycles

SHIP 6801 FWD GALLEY EXIT SIGN MISSING. CORRECTIVE ACTION: RESECURED EXIT SIGN. (9452605)

Part: LIGHT — DAMAGED (CABIN) · airframe 91,837 hrs · 24,305 cycles

FWD GALLEY RED EMERGENCY ESCAPE PATH LIGHT DAMAGED. INSTALLED NEW LIGHT ASSY PER B757 AMM 33 - 51. (9576590)

Part: NONE — NONE · airframe 91,690 hrs · 24,265 cycles

AIRCRAFT 6801, WHILE WORKING WORK CARD 3352-01042-01B, FOUND EXIT IDENTIFIER MISSING. CORRECTIVE ACTION: REPLACED 3R EXIT IDENTIFIER PER B757 AMM 33-51. CKS OK. (LP 9576512)

Part: NONE — NONE · corrosion level 2 · airframe 89,841 hrs · 23,828 cycles

SHIP 6801 CHANNEL SUPPORT CORRODED. CORRECTIVE ACTION: REMOVED CHANNEL SUPPORT AND FABRICATED. TRIMMED TO SIZE AND DRILLED PER BOEING DWG. TREAT, PRIMED AND INSTALLED PER BOEING DWG. (2143700)

Part: NONE — NONE · airframe 89,830 hrs · 23,826 cycles

SHIP 6801 FOUND CORROSION AT MID-LAV DUMP VALVE CUT-OUT. CORRECTIVE ACTION: REMOVED MID LAV DUMP VALVE ASSY TO ACCESS CORRODED AREA PER B757 AMM 38-32 (562634). C/W COMPLETION OF STEPS 1,2,3,4,5 AND 6 IAW PRI 597635-14 REV 1. TRANSFERRED TO NON-ROUTINE #1. SUMMARY OF NON-ROUTINE #1. PERFORMED ALL STEPS OF ER/A 597635-14 REV ORIGINAL. ALL RII STEPS COMPLETE. OPERATIONAL AND LEAK CHECK OF MID LAV SYSTEM COMPLETE. (8491843)

Part: ADAPTER — CORRODED (ZONE 900) · corrosion level 2 · airframe 98,663 hrs · 25,948 cycles

SHIP 6801 ADAPTER P/N 146N3513-2 HAS GRANULAR CORROSION. CORRECTIVE ACTION: RECIEVED NEW ADAPTER P/N 146N3513-2. DRILLED HOLES TO SIZE, INSTALLED ADAPTER RING PER PRI 597635-14 REV. 3. (2142207)

Part: BUSTLE — OUT OF ADJUST (L2 DOOR SLIDE) · airframe 88,137 hrs · 23,450 cycles

SHIP 6801 L2 DOOR SLIDE LIGHT INOP AT DEPARTURE TIME. CORRECTIVE ACTION: ADJUSTED L2 DOOR BUSSLE PER B757 MM 52-11. DOOR SLIDE LIGHT NOW OPS NML. (7482520)

Part: FRAME — CRACKED (BS 1640 S14L) · airframe 88,113 hrs · 23,443 cycles

SHIP 6801 CRACK WAS FOUND 1.775 IN OF LENGTH ON FRAME STA. 1640 S-14LH AT INNER FUSELAGE STRUCTURE. CORRECTIVE ACTION: SUMMARY OF NRC 00195: THIS NRC WAS ATTENDED WITH NRC 00191 PER ER/A 593451-14AD REV. ORIGINAL SECTION I: PERMANENT REPAIR AND ETI-57-21-404-REV. 2. UNDER LOG 1918061. (1918294)

Part: FRAME — NOT REPORTED (BS 1640 S14L) · airframe 88,113 hrs · 23,443 cycles

SHIP 6801 FOUND IN FUSELAGE FRAME FASTENER HOLE AT STA 1640 STRINGER 14LH: IN LOWER INBOARD HOLE AT 10:00 AND 1:00 HRS OCLOCK POSITION. CORRECTIVE ACTION: SUMMARY OF NRC 00240: THIS NRC WAS ATTENDED WITH NRC 00191 PER ER/A 593451-14AD REV. ORIGINAL SECTION I: PERMANENT REPAIR AND ETI-57-21-404-REV. 2. UNDER LOG 1918061. (1918298)

Part: FRAME — CRACKED (BS 1640 S14L) · airframe 88,113 hrs · 23,443 cycles

SHIP 6801 CRACKED FRAME STA 1640, S-14LH AT INNER FUSELAGE STRUCTURE. CORRECTIVE ACTION: SUMMARY OF NRC 00191 : FRAME STA 1640, S-14LH AT INNER FUSELAGE STRUCTURE WAS REPAIRED PER ER/A 593451-14AD REV. ORIGINAL SECTION I: PERMANENT REPAIR AND ETI-57-21-404-REV. 2. (1918061)

Part: FRAME — DAMAGED (BS 1640 S14R) · airframe 88,095 hrs · 23,439 cycles

SHIP 6801 AD, AA, AWR IN REF AMDS 5311-01218-01AB STEP 11: UPPER HOLES INB/OUTB AND INBD LOWER WERE FOUND WITH SCRATCH, GOUGE AND CORROSION IN FUSELAGE FRAME AT STA 1640 STRINGER 14RH: IN LOWER INBD GOUGE 10:00 O?CLOCK POSITION AND UPPER HOLES INB/OUTB SCRATCHES AROUND THE HOLE. CORRECTIVE ACTION: SUMMARY ON NRC 00399: UPPER HOLES INB/OUTB AND INBD LOWER WERE FOUND WITH SCRATCH, GOUGE AND CORROSION IN FUSELAGE FRAME AT STA 1640 STRINGER 14RH: IN LOWER INBD GOUGE 10:00 OCLOCK POSITION AND UPPER HOLES INB/OUTB SCRATCHES AROUND THE HOLE WERE REPAIRED PER ETI-57-21-405 R4 AND ER/A 593541-14AD REV.ORIGINAL SECTION I. (1918033)

Part: SKIN — CORRODED (LT NACELLE) · corrosion level 2 · airframe 88,095 hrs · 23,439 cycles

SHIP 6801 CORROSION ON LH (OUTBRD) CORE COWL, 6:00 O?CLOCK POSITION (AROUND LATCHES) AT ENGINE #1. (IN REFERENCE TO NRC 00308). CORRECTIVE ACTION: SUMMARY OF NRC 00447: LH (OUTBOARD) CORE COWL OF ENG. #1 WAS REPLACED PER. B757-200 AMM 71-11. (1917818)

Part: FRAME — DAMAGED (BS 1640) · airframe 88,117 hrs · 23,445 cycles

SHIP 6801 ERA 593451-14AD ISSUED FOR REPAIR TO STATION 1640 LH FRAME. CORRECTIVE ACTION: REF ERA 593451-14AD. (1916493)

Part: FRAME — DAMAGED (BS 1640 S14R) · airframe 88,088 hrs · 23,436 cycles

SHIP 6801 ERA 593541-14AD SECTION I ISSUED FOR REPAIR TO STA 1640 FRAME RH S AT STR 14R. CORRECTIVE ACTION: REF ERA 593541-14AD. (1916312)

Part: FLOORBEAM — CRACKED (BS 377 LBL 51) · airframe 88,088 hrs · 23,436 cycles

SHIP 6801 CRACK ON BEAM UPPER CHORD AT STA 377 AND LBL 51 IN REF NRC 0205. CORRECTIVE ACTION: SUMMARY ON NRC 00276:CRACK ON BEAM UPPER CHORD AT STA 377 AND LBL 51 WAS REPAIRED PER.ETI-57-21-410 REV 1, B757-200 S.R.M. AND ER/A 593450-14 REV ORIG. (1916237)

Part: RESERVOIR — LOW PRESSURE (L2 DOOR EMER PWR) · airframe 88,088 hrs · 23,436 cycles

SHIP 6801 LOW PRESSURE ON POWER EMERGENCY RESERVOIR AT L2 DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00372: POWER EMERGENCY RESERVOIR AT L2 DOOR.WAS REPLACED. (1914588)

Part: THRUST REVERSER — CRACKED (NR 1 ENGINE) · airframe 88,088 hrs · 23,436 cycles

SHIP 6801 CRACK ON OUTBD THRUST REVERSER LOWER AREA AT ENGINE # 1. (NAC STA 156). CORRECTIVE ACTION:SUMMARY OF NRC 00309: CRACK ON OUTBD THRUST REVERSER LOWER AREA AT ENGINE # 1. (NAC STA 156). WAS REPAIRED PER ER/A 593480-14 REV. ORIGINAL SECTION I, PERMANENT REPAIR AND ETI-57-21-419 REVISION 1. (1914990)

Part: STRAP — CRACKED (BS 377 LBL 51) · airframe 88,088 hrs · 23,436 cycles

SHIP 6801 CRACKS ON FLOOR BEAM STABILIZATION STRAP AT STA 377 AND LBL 51 IN REF NRC 0346. CORRECTIVE ACTION: SUMMARY OF N.R.C. 00404: FLOOR BEAM STABILIZATION STRAP AT STA 377 AND LBL 51 WAS REPAIRED PER B-757/200 S.R.M.

Part: SUPPORT — CORRODED (BS 680) · airframe 88,088 hrs · 23,436 cycles

SHIP 6801 CORROSION ON BULKHEAD RH LATERAL SUPPORT LWR SIDE (STA 860 NEAR TO RH SIDE PLATE) AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00181, CORROSION ON BULKHEAD RH LATERAL SUPPORT LWR SIDE (STA 860 NEAR TO RH SIDE PLATE) AT FWD CARGO COMPARTMENT WAS REMOVED PER B757-200 SRM. (1910955)

Part: HARNESS — TORN (L1 DOOR SLIDE) · airframe 88,088 hrs · 23,436 cycles

SHIP 6801 TORN ON L1 SLIDE HARNESS WAS FOUND DURING OK TO INSTALL PROCESS. CORRECTIVE ACTION: SUMMARY OF NRC 00397: HARNESS ASSY ON L1 DOOR SLIDE WAS REPLACED AND INSTALLED PER B757-200 AMM 25-66. (1908124)

Part: WEDGE — DEBONDED (NR 10 SLAT) · airframe 88,088 hrs · 23,436 cycles

SHIP 6801 DISBOND ON REPAIR AREA OF THE TRAILING EDGE WEDGE (UPPER SIDE) AT SLAT # 10, OSS 786. CORRECTIVE ACTION: SUMMARY OF NRC 00019 : TRAILING EDGE WEDGE (UPPER SIDE) AT SLAT # 10, OSS 786 WAS REPAIRED PER B757-200 SRM. (1903218)

Part: SKIN — DEBONDED (NR 8 SLAT) · airframe 88,088 hrs · 23,436 cycles

SHIP 6801 ONE DISBOND OF 1) 1.125" X 0.875" (LENGHT/WIDTH) ON OSS 490.1 APPROX. UPPER SURFACE AT LE SLAT 8 TRAILING EDGE WEDGE. CORRECTIVE ACTION: SUMMARY OF NRC 00077 : LE SLAT 8 TRAILING EDGE WEDGE. WAS REPAIRED PER B-757-200 S.R.M. (1903226)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,186 hrs · 24,615 cycles

SHIP 6801 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 576658-14 REV A. CORRECTIVE ACTION: REF ERA 576658-14AD. (1595590)

Part: INDICATOR — INOPERATIVE (SLIDE ARMING) · airframe 85,257 hrs · 22,836 cycles

SHIP 6801 R1 SLIDE ARM LIGHT OUT. CORRECTIVE ACTION: REROUTED STATIC LINE AND CKED FUNCTION OF SLIDE ARM MECHANISM AND ARMED INDICATION PER B757 AMM 25-66. (1569467)

Part: GIRT BAR — DIRTY (R1 DOOR) · airframe 85,228 hrs · 22,830 cycles

DOOR R1 SLIDE ARM LIGHT OUT. R1 SLIDE WONT ARM. REMOVED SLIDE COVER FOR MAINT. CLEANED GIRT BAR AND RE LUBED. INSTALLED COVER. OPS CK GOOD.

Part: FITTING — FOD (R1 GIRT BAR) · airframe 85,200 hrs · 22,824 cycles

R1 DOOR WOULD NOT ARM AT DEPARTURE. FOUND DEBRIS IN THE GIRT BAR FITTING. REMOVED FOD, OPS CHECKED NORMAL.

Part: SLEEVE — MISSING (L1 DOOR) · airframe 84,681 hrs · 22,711 cycles

(AIRCRAFT 6801, L/P 1510878) DOOR DISARM PIN SLEEVE MISSING (B747 ONLY) / LOCATIONS: 1L / 1L DOOR DISARMD PLACARD WILL NOT EXTEND / INTERIOR. CORRECTIVE ACTION: REPLACED DOOR DISARM PIN SLEEVE PER B757 AMM 52-11.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 81,328 hrs · 22,059 cycles

(AIRCRAFT 6801, L/P 5435963) AFTER TAKEOFF, L ENG OVHT, ENG BTL1 DISCH, AFT CARGO FIRE ARM, AND #2 CARGO BTL DISCH LIGHTS ILLUMINATED. LIGHTS EXTINGUISHED @ 9000 FT. PERFORMED ENG/CARGO FIRE TEST REF B757 26-11 OPS NML. OK FOR / SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,984 hrs · 21,995 cycles

(AIRCRAFT 6801, L/P 1063778) CTR WING BOX UPPER SURFACE BENEATH CABIN FLOORBOARD HAS 8 SQ IN EXFOLIATED CORROSION UNDER RT STA 1000 SIDEWALL BEAM. DOT 127-016. CORRECTIVE ACTION: REPAIRED AREA IAW ER/A #576651-14 REV. O.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,984 hrs · 21,995 cycles

(AIRCRAFT 6801, L/P 1064072) CTR WING BOX UPPER SURFACE BENEATH CABIN FLOORBOARD HAS 4 SQ IN EXFOLIATED CORROSION UNDER LT STA 1020 SIDEWALL BEAM. DOT 127-014. REMOVED CORROSION FROM MAIN CABIN CENTER WINGBOX UPPER SURFACES LT STA 1020 HIGHEST READING .220 LOWEST READING .159 AND OUT OF LIMITS. REPAIRED AREA LT STA 1020 IAW ER/A 576650-14 REV ORIGINAL.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,984 hrs · 21,995 cycles

(AIRCRAFT 6801, L/P 1063796) CTR WING BOX UPPER SURFACE BENEATH CABIN FLOORBOARD HAS 20 SQ IN EXFOLIATED CORROSION UNDER RT STA 1020 SIDEWALL BEAM. DOT 127-017. REPAIRED AREA IAW ER/A #576651-14 REV ORIGINAL.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,984 hrs · 21,995 cycles

(AIRCRAFT 6801, L/P 1064078) CTR WING BOX UPPER SURFACE BENEATH CABIN FLOORBOARD HAS 12 SQ IN EXFOLIATED CORROSION UNDER LT STA 1000 SIDEWALL BEAM. DOT 127-015. REPAIRED AREA LT STA 1000 IAW ER/A 576650-14 REVORIGINAL.

Part: SUPPORT BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,984 hrs · 21,995 cycles

(AIRCRAFT 6801, L/P 1064092) MAIN CABIN CENTER WING BOX LT STA.980 BELOW SUPPORT BEAM HAS CORROSION. REMOVED CORROSION FROM MAIN CABIN CENTER WING BOX LT STA 980 BELOW SUPPORT BEAM THICKEST READING .180 LOWEST READING .112 AND OUT OF LIMITS REPAIRED AREA STA 980 LT IAW ER/A# 576650-14 REV ORIGINAL.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,971 hrs · 21,991 cycles

SHIP 6801 MAIN CABIN, CORROSION ON OUTBD. FLOOR PANEL SUPPORT, UPPER SIDE. CORRECTIVE ACTION: REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS REF SRM. CUT OUT DAMAGE, FABRICATED REPAIR AND INSTALLED REF SRM. (1054063)

Part: FRAME — DAMAGED (FUSELAGE) · airframe 80,971 hrs · 21,991 cycles

SHIP 6801 BS 700, STR22L, FWD CARGO PIT, LBL 45.73, FRAME IS DAMAGED BEHIND NUT PLATE. STREAMER ATTACHED, DOT#2, I-104. CORRECTIVE ACTION: REPAIRED FWD CARGO BS 700 DAMAGE FRAME AT STR 22L BY CUTTING DAMAGE AREA AND INSTALL REPAIR DOUBLER IAW SRM. (1051824)

Part: REPAIR — GOUGED (FUSELAGE) · airframe 80,971 hrs · 21,991 cycles

SHIP 6801 MAIN CABIN @ BS1280 EXISTING REPAIR HAS A GOUGE BEWTEEN S9L AND S14L. CORRECTIVE ACTION: ACCOMPLISHED REPAIR ON FRAME STA 1280 STR 10L TO STR 15L IAW ER/A# 513680-14AD REV B SECTION II PERMANENT REPAIR. (1048926)

Part: GIRT BAR — OUT OF LIMITS (L4 DOOR) · airframe 80,971 hrs · 21,991 cycles

L4 DOOR GIRT BAR OUT OF LIMITS. CORRECTIVE ACTION: REMOVED AND REPLACED L-4 DOOR GIRT BAR IAW B-757 AMDS.

Part: FITTING — DAMAGED (RT ENGINE) · airframe 80,971 hrs · 21,991 cycles

#2 R/H ENG DRAG FITTING #2 HOLE HAS 2 INDICATIONS OF DEFECTS CLOCKED AT 10 OCLOCK AND 3 OCLOCK POSITIONS IN THE UPPER SKIN. REPAIRED #2 R/H ENGINE DRAG FITTING #2 HOLE PER ER/A 576658-14AD REV ORIGINAL. (1043395)

Part: KEELBEAM — CORRODED (BS 897) · corrosion level 2 · airframe 80,971 hrs · 21,991 cycles

FWD. CARGO, CORROSION LOWER BILGE STA.897 RBL-7. CORRECTIVE ACTION: REPAIRED FWD CARGO STA 897 RBL7 CORROSION ON KEEL BEAM CHORD STRINGER PER DELTA ER/A 577291-14 REV. ORIGINAL. (1043384)

Part: REPAIR — GOUGED (FUSELAGE) · airframe 80,971 hrs · 21,991 cycles

SHIP 6801 MAIN CABIN EXISTING REPAIR HAS A GOUGE @ BS 1280 BETWEEN S9R AND S14R. CORRECTIVE ACTION: REMOVED EXISTING REPAIR FROM MAIN CABIN FRAME @ STA 1280 BETWEEN S9R AND S14R AND INSTALLED NEW REPAIR IAW ER/A# 513683-14AD REV B SECTION II PERMANENT REPAIR. (1048936)

Part: CONVERTER — CONTAMINATED (OZONE) · airframe 79,599 hrs · 21,720 cycles

(AIRCRAFT 6801, L/P 3751740) VERY STRONG WET SOCK SMELL FROM AIR CONDITIONING SYSTEM ON APPROACH. PERFORMED BSI OF THE 2.5 BLEED PORT FINDINGS TURNED OVER TO LEAK AND MCC. FOUND EVIDENCE OF OIL CONTAMINATION IN 2.5 BLEED PORT AREA R/R LT PACK OZON CONVERTER PER B757 AMM 21-51. R/R BOTH RECI/FAN FILTER PER B757 AMM 21-51. ENGINE REMOVED IAW JIC 7100-9902E-01. ENGINE INSTALLED PER B757 AMDS WORKCARD 7100-9902E-01. RII COMPLETED AND PREFLIGHT C/W PER AMDS WORKCARD 7100-9902E-01.

Part: FITTING — OUT OF ADJUST (GIRT BAR) · airframe 76,196 hrs · 21,077 cycles

SLIDE INDICATOR LIGHT INOPERATIVE. ADJUSTED THE FLOOR FITTING IAW AMM 52-11.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,117 hrs · 21,061 cycles

DURING CHECK, FOUND SEAT 3C CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED THE POWER SUPPLY IAW AMM 33-51-11.

Part: FUEL CONTROL — MALFUNCTIONED (LEFT ENGINE) · airframe 74,790 hrs · 20,800 cycles

REACHING FL390, AFTER LEVEL OFF, LEFT ENGINE EXPERIENCED TWO SEPARATE THRUST REDUCTIONS WITH ACCOMPANYING AIRCRAFT VIBRATIONS. AFTER EACH SEPARATE REDUCTION & VIBRATION, THE ENGINE RECOVERED NORMAL OPS. NO LIMIT EXCEEDED AND MC NOTIFIED. COMPLETED QRH PROCEDURE FOR ENGINE LIMIT, SURGE, & STALL. REMOVED AND REPLACED THE FUEL CONTROL AND PERFORMED ENGINE RUN, NO LEAKS AND OPS CHECK NORMAL IAW AMM 73-21. REPLACED EEC PT2/TT2 PROBE IAW AMM 73-21. AND PERFORMED HIGH POWER RUN, OPS CHECKED NORMAL.

Part: LINE — DETACHED (L4 DOOR SLIDE) · airframe 74,774 hrs · 20,797 cycles

MOORING LINE AT THE L4 DOOR DETACHED. ATTACHED THE MOORING LINE IAW AMM 25-66.

Part: LINE — DETACHED (R4 DOOR SLIDE) · airframe 74,774 hrs · 20,797 cycles

R4 DOOR UNABLE TO ARM. FOUND MOORING LINE DETACHED FROM THE SLIDE GIRT BAR IAW 06-484000-14 MA REV ORIG. LINE HAS NO EFFECT ON THE SLIDE OPERATION. VERIFIED PROPER DOOR OPERATION AFTER LINE SECURED.

Part: STRAP — CRACKED (BS 375) · airframe 72,201 hrs · 20,299 cycles

FWD ACCESSORY BAY LEFT TUNNEL STABILIZATION STRAP CRACKED AT BS 375 LBL 25. ACCOMPLISHED A PERMENENT ON THE STRAP IAW SRM.

Part: GUARD — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 72,128 hrs · 20,283 cycles

EMERGENCY LIGHTS OVERHEAD SWITCH GUARD WHEN CLOSED, CAUSES THE EMERGENCY LIGHT TO TURN OFF. ADJUSTED THE SWITCH. EMERGENCY LIGHTS OPS CHECKED GOOD IAW AMM 33-51.

Part: ROTOR — COKED (ENGINE) · airframe 70,211 hrs · 19,897 cycles

WHILE IN CRUISE, CREW REPORTED HEARING LOUD BANG, FOLLOWED BY ENGINE ROLLBACK AND SHUTDOWN. ACFT DIVERTED. CREW DECLARED AN EMERGENCY. MAINTENANCE FOUND PMA ROTOR AND STATOR COKED WITH OIL AND SCORED. PMA STATOR, ROTOR, AND CARBON SEAL WERE REPLACED. TREND DATA GOOD.

Part: SKIN — DAMAGED (BS 520) · airframe 72,446 hrs · 20,345 cycles

FOUND A DENT & GOUGE APPROXIMATELY 45 INCHES AFT OF THE E & E DOOR. ACCOMPLISHED A PERMANENT REPAIR AT BS 520 BETWEEN STRINGERS 27 & 28L IAW ERA 544898-14, REV A, SECTION III.

Part: SKIN — DENTED (NR 3 SLAT) · airframe 63,790 hrs · 18,622 cycles

LEFT WING NR 3 SLAT UPPER SURFACE T/E WEDGE HAS 2 LARGE DENTS. REPAIRED LT WING NR 3 SLAT UPPER SURFACE BY HOT BONDED NEW CORE & DOUBLER ON IAW SRM.

Part: STRAP — DAMAGED (BS 1520) · airframe 63,790 hrs · 18,622 cycles

FLOORBEAM STABILIZATION STRAP AT BS 1520, RBL 45.5 DAMAGED. DISPLACED STIFFNER, REMOVED DAMAGED STABILIZATION STRAP, FABRICATED REPAIR AND INSTALLED IN AMM AND SRM.

Part: SKIN — DENTED (BS 635) · airframe 63,790 hrs · 18,622 cycles

FUSELAGE DENT LT SIDE FORWARD OF L2 FS 635.5 . DENTS REPAIR IAW ERA 512667-14, REV O.

Part: SEAT TRACK — DAMAGED (BS 1098) · airframe 63,790 hrs · 18,622 cycles

MAIN CABIN SEAT TRACK IS CHIPPED, STA 1098, LBL 44. TRACK FOUND OUT OF LIMITS. REMOVED SEAT TRACK, FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: SKIN — CORRODED (BS 1190) · corrosion level 2 · airframe 70,667 hrs · 19,984 cycles

AFT CARGO BILGE AREA, THE SKIN HAS CORROSION AROUND LAVATORY DUMP DUCT BS 1190 STRINGER 30. REPAIRED THE SKIN IAW ER/A 532884-14 REV O.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,222 hrs · 18,070 cycles

FOUND L1 DOOR EMERGENNCY LIGHT SIGN AND R1 LOWER EMERGENCY EXIT SIGN INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51. LIGHTS OPS CHECKED GOOD. OK FOR SERVICE AT THIS TIME.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 61,046 hrs · 18,039 cycles

DURING EMERGENCY LIGHTS CHECK, FOUND ROW 38 THRU ROW 45 FLOOR LIGHTS INOPERATIVE. FOUND FAULTY SPLICE BETWEEN SEAT ROW 38 DEF AND ROW 40 DEF, REPAIRED SPLICE IAW SWPM. EMERGENCY LIGHTS CHECKED GOOD, OK FOR SERVICE.

Part: FUSE — FAILED (EMERGENCY LIGHT) · airframe 61,011 hrs · 18,032 cycles

EMERGENCY LIGHT AND SIGN INOPERATIVE. R & R FUSE ON BATTERY PACK POWER SUPPLY JUST AFT OF FWD MOST IAW AMM 33-51. OPS CHECKED GOOD.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,461 hrs · 17,932 cycles

L1 DOOR OVER HEAD EXIT SIGN INOPERATIVE. REPLACED POWER SUPPLY FUSE IAW AMM 33-51-07. OPS CHECKED GOOD.

Part: FUSE — FAILED (EMERGENCY LIGHT) · airframe 60,307 hrs · 17,900 cycles

R1 DOOR EMERGENCY LIGHTS INOPERATIVE. FOUND FUSE BAD AT POWER PACK M731 - REPLACE FUSE OK FOR SERVICE.

Part: GATE — CORRODED (L4 DOOR) · airframe 55,821 hrs · 17,030 cycles

L4 DOOR UPPER GATE HAS CORROSION AND BARE METAL IN INNER CAVATIES. REPLACED GATE IAW AMM 52-11-38-404-009.

Part: FRAME — DENTED (BS 1580 S26-27L) · airframe 55,821 hrs · 17,030 cycles

TWO DENTS ON FUSELAGE FRAME TOP FLANGE AFT CARGO BS 1580 BETWEEN S26-27L, COMPLIED WITH ERA 513899-14, REV ORIGINAL.

Part: SKIN — DENTED (BS 620-640) · airframe 55,821 hrs · 17,030 cycles

THREE DENTS IN SKIN, LT FUSELAGE BS 620-640 BETWEEN S15-16L. ACCOMPLISHED REPAIR IAW ERA 512667-14, REV ORIGINAL.

Part: FRAME — DENTED (BS 1420 S25-27L) · airframe 55,821 hrs · 17,030 cycles

SEVERAL DENTS ON FUSELAGE FRAME UPPER FLANGE IN AFT CARGO BS 1420 BETWEEN S25-27L. COMPLIED WITH ERA 513900-14, REV ORIGINAL.

Part: FRAME — DENTED (BS 1480) · airframe 55,821 hrs · 17,030 cycles

TWO DENTS ON FUSELAGE FRAME TOP FLANGE RADIUS AREA AT AFT CARGO BAY BS 1480 BETWEEN S25-26L. ACCOMPLISHED REPAIR IAW SRM 53-00-07, FIG 201, REPAIR 5, DETAIL III.

Part: SKIN — DAMAGED (NR 2 NACELLE) · airframe 55,821 hrs · 17,030 cycles

2 ELONGATED HOLES COMMON TO NR 2 PYLON LT SKIN & UPPER CHORD FOUND UPON REMOVAL OF INCOMING REPAIR PYLON STA 142.5 & 145.6. ACCOMPLISHED REPAIR IAW ER/A 512677-14, REV ORIGINAL.

Part: SKIN — DAMAGED (NR 2 PYLON) · airframe 55,821 hrs · 17,030 cycles

NR 2 PYLON INBD SIDE SUB STRUCTURE LOWER CHORD AT STA 128 HAS ONE ELONGATED FASTENER HOLE. ACCOMPLISHED ERA 512677-14, REV ORIGINAL.

Part: FRAME — DENTED (BS 640 S25R) · airframe 55,821 hrs · 17,030 cycles

FWD CARGO, RT BILGE FRAME DENTED, BS 640 S25R. CUT OUT DAMAGE SECTION OF FRAME IAW SRM 53-00-07, REPAIR 5. REPAIRED FRAME IAW SRM 53-00-07, REPAIR 5. COMPLIED WITH ERA 513687-14, REV ORIGINAL.

Part: FRAME — DENTED (BS 1440) · airframe 55,821 hrs · 17,030 cycles

DENT ON FUSELAGE FRAME TOP FLANGE AT AFT CARGO COMPARTMENT BS 1440 ABOVE S26L. ACCOMPLISHED REPAIR IAW ERA 513678-14, REV ORIG.

Part: SKIN — DENTED (BS 413 S18R) · airframe 55,821 hrs · 17,030 cycles

LOWER FUSELAGE SKIN HAS 6-7 INCH DENT AT BS 413 S18R. REPAIRED PER IAW SRM 53-00-01, FIG 201, REPAIR 2.

Part: SEAT TRACK — CORRODED (BS 1689-1715) · airframe 55,821 hrs · 17,030 cycles

CORROSION ON MAIN CABIN DECK PLATE TRACK AT BS 1689 TO 1715 BL 0. R & R TRACK ON MAIN CABIN DECK PLATE AT BS 1689 -1715, BL 0 IAW SRM 51-40-02, PG 1-3 AND PG 30.

Part: SKIN — DAMAGED (NR 2 PYLON LT) · airframe 55,821 hrs · 17,030 cycles

NR 2 PYLON INBD SIDE SUB STRUCTURE AT STA 117 LWR CHORD HAS ONE ELONGATED FASTENER HOLE. ACCOMPLISHED REPAIR IAW ERA 512677-14, REV ORIGINAL.

Part: WEB — CORRODED (BS 1677-1680) · airframe 55,821 hrs · 17,030 cycles

CORROSION ON R4 DOOR LOWER SILL WEB, BETWEEN BS 1677 - 1680. R & R WEB IAW DWG 146N1148 AND SRM 51-40-02, PG 2 AND 7.

Part: DECK PLATE — CORRODED (BS 1680-1720) · airframe 55,821 hrs · 17,030 cycles

CORROSION ON MAIN CABIN DECK PLATE BETWEEN BS 1680 AND 1720 BL 0 TO RBL 52. ACCOMPLISHED REPAIR IAW SRM 53-60-51, FIG 201, ALTERNATIVE 1, REPAIR 2.

Part: SKIN — CRACKED (R1 DOOR) · airframe 55,821 hrs · 17,030 cycles

R1 DOOR INNER SKIN LOWER SIDE LIGHTNING HOLE CRACKED. REPAIRED IAW ERA 513909-14, REV ORIG.

Part: SEAT TRACK — CORRODED (BS 640-643) · airframe 55,821 hrs · 17,030 cycles

STA 640-643 RT OTBD SEAT TRACK CORRODED. REPAIRED SEAT TRACK IAW SRM 53-00-52 AND SRM 51-40-01, PG 7 AND 6.

Part: BUSHING — MIGRATED (NR1 PYLON) · airframe 55,821 hrs · 17,030 cycles

NR 1 PYLON UPPER DIAGONAL BRACE WING FITTING (MOUNTED UNDER WING) OTBD BUSHING MIGRATED OUT OF INNER RACE REQS ENGINEERING DISPOSITION. REPAIRED IAW ERA 513675-14AD REV ORIG.

Part: FRAME — GOUGED (BS 1280 S10L) · airframe 55,821 hrs · 17,030 cycles

FRAME STA 1280, STR 10L TO 15L HAS MULTIPLE GOUGES ON INBD FLANGE AT THE EXTERNAL RADIUS. REPAIRED IAW ERA 513680-14, REV ORIG. (ERA 513680-14).

Part: FRAME — GOUGED (BS 1280 S10R) · airframe 55,821 hrs · 17,030 cycles

FRAME STA 1280 STR 10R TO 15R HAS MULTIPLE GOUGES. REPAIRED IAW ERA 512683-14, REV ORIG.

Part: CUSP WEB — CORRODED (BS 1360-1380) · airframe 55,821 hrs · 17,030 cycles

CORROSION ON MAIN CABIN RT CUSP WEB BETWEEN BS 1360 TO 1380. REPLACED CUSP WEB IAW SRM 51-40-02, PG 7 AND 21.

Part: SKIN — DENTED (R4 DOOR) · airframe 55,821 hrs · 17,030 cycles

R4 DOOR INNER SKIN DENTED 2" BOTTOM OF THE DOOR AND 5" FROM FWD END /REPAIRED IAW ERA 513689-14, REV ORIG. (ERA 513689-14)

Part: SEAT TRACK — CORRODED (BS 697-733) · airframe 55,821 hrs · 17,030 cycles

BS 697-733 RT INBD SEAT TRACK, RBL 25 CORRODED AND HAS DEEP PREVIOUS BLENDS. R & R PART IAW SRM 51-40-02 PAR 7, PG 6 AND SRM 51-40-05 FIG 2, PG 3.

Part: FRAME — DENTED (BS 580 S24L) · airframe 55,821 hrs · 17,030 cycles

FWD CARGO BILGE FRAME DENTED BS 580 AT S24L. REPAIRED IAW SRM 53-00-07, REPAIR 5, FIG 201.

Part: FRAME — DENTED (BS 1500 S25-26L) · airframe 55,821 hrs · 17,030 cycles

DENT ON FUSELAGE FRAME TOP FLANGE IN AFT CARGO BS 1500 BETWEEN S25-26L. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 5.

Part: SUPPORT FITTING — CORRODED (BS 1070) · airframe 55,821 hrs · 17,030 cycles

HINGE SUPPORT FITTING, BS 1070 BL 0 FOUND CORRODED. REPAIRED IAW ERA 513918-14, REV ORIG.

Part: PANEL — CORRODED (BS 425) · airframe 55,821 hrs · 17,030 cycles

MAIN EQUIPMENT CENTER LOWER BILGE AREA LAVATORY SERVICE PANEL CORRODED. R & R IAW SRM 51-40-02, PAGE 2 & PAGE 4.

Part: GIRT BAR — INOPERATIVE (R1 DOOR) · airframe 55,821 hrs · 17,030 cycles

R1 DOOR GIRT BAR DOES NOT SLIDE ON GIRT BAR SLIDER AT FWD END. REPLACED GIRT BAR IAW AMM 25-66-10-402-022.

Part: SKIN — DENTED (BS 1418 S28R) · airframe 55,821 hrs · 17,030 cycles

LOWER FUSELAGE DENT ON SKIN BS 1418, STR 28R. ACCOMPLISHED REPAIR IAW ERA 512666-14, REV ORIG.

Part: FLOORBEAM — CRACKED (BS 700) · airframe 54,247 hrs · 16,715 cycles

FLOORBEAM AT BS 700 CRACKED AT LBL 24.75 AND LBL 45.5. REPAIR COMPLETED IAW ER/A 507520-14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,407 hrs · 15,590 cycles

STA 377 FLOORBEAM UPPER FLANGE CORROSION DAMAGE-BL0 - LBL 23. REPAIR COMPLETED PER ERA 492668-14 REV A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,407 hrs · 15,590 cycles

CABIN FLOORBEAM STA 1640 T-CAP CORROSION. REPAIRED PER ERA 493066-14 REV ORIG.

Part: UNKNOWN — ODOR (CABIN) · airframe 43,877 hrs · 14,688 cycles

SMOKE IN CABIN AND LOSS OF LEFT AC BUSS WITH IDG RISE FAULTED ON THE BPCU. CREW DECLARED A MECHANICAL EMERGENCY AND DIVERTED. OPENED OVERHEAD CEILING PANELS AT ROWS 34-39. NO OBVIOUS ELECTICAL SHORTS. CHECKED LAVATORY HEATERS NTF. STARTED ALL OVENS AND COFFEEMAKERS IN AFT GALLEY. ALL OPS NORMAL. OPENED FWD BULKHEAD PANEL IN AFT CARGO COMPT. VISUALLY INSP AREA FOR SIGNS OF SMOKE OR ELECTICAL FUMES. CHECKS GOOD CLOSED FWD BULKHEAD PANEL. UNABLE TO DUPLICATE.

Part: IDG — FAILED (RIGHT) · airframe 42,156 hrs · 14,347 cycles

RT GEN OFF LT ILLUMINATED ON TAXI OUT ATTEMPTED ONE RESET PER QRH. FWD TO MCO IAW MEL 24-00-01 PLACARD INSTALLED. BPCU FAULTS DP TRIP. REPLACED RT IDG PER M/M. OPS AND LEAK C OK - SYS OPS NORM. ETOPS CATEGORY 'E'.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 42,082 hrs · 14,335 cycles

L ENG SEC CONT-NO OTHER MSGS OR INDICATIONS NOTED. FWD TO MCO/PLAC IAW MEL 73-21-01A. MEL PROCEDURES FOLLOWED CB PULLED AND SECURED. ETOPS CATEGORY 'E': PROBLEMS WITH SYS CRITICAL TO ETOPS.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 41,853 hrs · 14,295 cycles

RT ENG OIL SEAL STATUS MSG. REPLACED ENGINE. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: SKIN — DENTED (CARGO CUTOUT) · airframe 40,912 hrs · 14,135 cycles

FUSELAGE C-2, DOOR OPENING LOWER AFT CORNER SKIN DENTED. REPAIR IAW ERA 475920-14.

Part: WARNING LIGHT — ILLUMINATED · airframe 35,580 hrs · 12,973 cycles

AFTER PUSHBACK AND ENGINE START. RECEIVED A AUTOSPEED BRAKE MSG. FWD TO MCO PER MEL 27-62-01B. MCO AND PLAC INSTALLED.

Part: ENGINE — MAKING METAL (NR 2) · airframe 33,995 hrs · 12,461 cycles

PLEASE REPLACE THE NR 2 ENG BECAUSE OF PREVIOUS METAL FINDING FROM THE NUMBER 5 BEARING AREA. REPLACED ENGINE.

Part: SKIN — DAMAGED (WING) · airframe 33,955 hrs · 12,440 cycles

DAMAGE LED TO A 0.500" OVERSIZED WING SKIN HOLE AND A 0.310" OVERSIZED STRINGER U-9.5 HOLE AT A COMMON FASTENER LOCATION JUST INBD OF WING STATION 537 (3RD NEW FASTENER FROM RIB NR 17). REPAIR CONSISTED OF A COUNTERSUNK FREEZE PLUG AND AN OVERSIZED FASTENER. THIS REPAIR RELATES TO THE APB BLENDED WINGLET PROGRAM MODIFICATION AND INSTALLATION.

Part: LENS — DAMAGED (EMERGENCY LIGHT)

DFW - EMERGENCY PATH LIGHTS AT FIRST CLASS AND SEAT 24D LENS DAMAGED. REPLACED LENS FOR EMERGENCY PATH LIGHTS AT FIRST CLASS AND SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CAP — MISSING (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT AFT LAVATORY RIGHT HAND SIDE AND SEATS 7D, 24D, 25C, AND ROW 1AB AND ROW 6AB MISSING END CAPS. REPLACED END CAPS FOR EMERGENCY LIGHTS AT AFT LAVATORY RIGHT HAND SIDE AND SEATS 7D, 24D, 25C, AND ROW 1AB AND ROW 6AB. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PAN — CORRODED (LAVATORY)

MCI - CORROSION FOUND AROUND FORWARD LAVATORY DUMP CHUTE BETWEEN FORWARD LAVATORY SERVICE PAN AND UPPER PAN IN AREA 12 INCHES BY 12 INCHES. REPLACED FORWARD LAVATORY SERVICE PANEL UPPER PAN.

Part: SPRING — DEFORMED (GIRT BAR) · airframe 23,077 hrs · 7,956 cycles

THE EVACUATION SLIDE GIRT BAR RETENSION LEAF SPRINGS WERE ADJUSTED ACCOUNT DEFORMED ON THE L1, R1, L2, R2, L4, AND R4 CABIN DOOR.

Part: SKIN — CRACKED (PYLON) · airframe 20,903 hrs · 7,112 cycles

DURING CHECK-C MAINT FOUND CRACKS IN PYLON DURING REPAIR. FWD ACCESS HOLE NACELLE STA 116.5 EMITTING FWD APPROX 1.5 INCHES, INBD AND OTBD SIDES. ACCOMPLISHED REPAIR PER EMLR 73252 AND SB 757-54-0037.

Part: SKIN — CRACKED (NR2 PYLON) · airframe 20,903 hrs · 7,112 cycles

DURING CHECK-C MAINT CRACKS FOUND ON NUMBER 2 PYLON THE FWD ACCESS HOLE AT NACELLE STA 116.5, OTBD AND INBD OF PYLON, CRACKS 1.625 INCHES LONG AT TOP FWD SECTION OF ACCESS HOLE. CRACK IS VISIBLE ON OTBD AND INBD SIDE OF SKIN. ACCOMPLISHED BOEING SERVICE BULLETIN 757-54-0037 DIRECTED BY EMLR 73249 TO INCORPORATE REPAIR.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 20,903 hrs · 7,112 cycles

DURING CHECK-C MAINT IN THE NUMBER 2 PYLON, THE FWD ACCESS HOLE TO INTERIOR AT APPROX NAC STA 116.5, THE OTBD SIDE OF PYLON HAD CRACK 1.625 INCHES LONG. CRACK LOCATED TOP FWD SECTION OF ACCESS HOLE. CRACK IS VISIBLE ON OTBD AND INBD SIDE OF SKIN.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 20,903 hrs · 7,112 cycles

DURING CHECK-C MAINT THE NR 2 ENGINE PYLON, FWD ACCESS HOLE TO INTERIOR OF THE PYLON, APPROXIMATE NACELLE STA 162, THE OTBD SIDE HAD A CRACK 1.625 INCHES LONG. THE CRACK WAS LOCATED TOP FWD SECTION, AND VISIBLE ON OTBD TO INBD OF THE SKIN. ACCOMPLISHED BOEING SERVICE BULLETIN 757-54-0037 DIRECTED BY EMLR 73249.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 20,903 hrs · 7,112 cycles

DURING CHECK-C MAINT ON NUMBER 2 PYLON 1.5 INCH CRACKS GOING AFT WERE FOUND INBD AND OTBD FORWARD ACCESS HOLE AT NACELLE STA 120 BETWEEN STA 116.05 AND 128. ACCOMPLISHED EMLR 73249.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,684 hrs · 7,026 cycles

EGRESS LIGHTS OUT ROW 14 AND 15 DUE TO WEAR. RELAMPED AT ROW 14. OPS CHECKED NORMAL. LAST CHECK-C LAX 6/12/01.

Part: EEC — FAILED (RT ENGINE) · airframe 17,586 hrs · 5,549 cycles

IN CLIMB THE RT ENG STALLED THEN SHUT ITSELF DOWN. FLIGHT RETURNED TO STL. REPLACED THE EEC STATOR, P/N 430219, AND THE EEC ROTOR, P/N 46038. CHECK-C 6-12-01 LAX.

Part: ENGINE — LEAKING (LT ENGINE) · airframe 16,839 hrs · 5,712 cycles

THE LEFT ENGINE OIL QUANTITY DECREASED IN FLIGHT. OIL PRESSURE EVENTUALLY DECREASED TO RED LINE. ENGINE WAS SHUT DOWN, AN UNSCHEDULED LANDING MADE AT DTW. CHECK-C 10-17-99 LAX.

Part: LAMP — INOPERATIVE (COCKPIT) · airframe 15,843 hrs · 5,421 cycles

THE EGRESS SYSTEM SWITCH LIGHT WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 10-17-99 LAX.