N674DL

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 96,348 hrs · 43,298 cycles

SHIP 0674 2L DOOR LIGHT EXIT SIGN FELL OFF. REINSTALLED SIGN. (4367445)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 96,348 hrs · 43,298 cycles

SHIP 0674 2L EXIT MULTIPLE WRITE UPS FOR FALLING OFF. CORRECTIVE ACTION: INSPECTED AND SECURED LENS/COVER OK FOR SERVICE. (0062004)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 96,348 hrs · 43,298 cycles

SHIP 0674 EMERGENCY EXIT SIGN AT 2L FELL OFF. SECURED EMERGENCY EXIT SIGN @2L DOOR PER B757 AMM 33-51-01. (4367440)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 96,348 hrs · 43,298 cycles

SHIP 0674 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:603. RESECURED 603 EMERGENCY EXIT SIGN. (0059234)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 96,277 hrs · 43,257 cycles

SHIP 0674 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOPERATIVE / LOCATIONS:400 / EMERGENCY LIGHT SWITCH (ELS) REMAINS RED / INTERIOR. CORRECTIVE ACTION: RESET SWITCH EMERGENCY LIGHTS CHECK OK. (0046271)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 96,277 hrs · 43,257 cycles

SHIP 0674 L2 EXIT SIGN SECURITY. CORRECTIVE ACTION: SEEMED IDENTICAL TO R2 DOOR IN SECURITY AND APPEARANCE. REMOVED AND REPLACED LENS IAW B757 AMM 33-51. OK FOR SVC. (0042089)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 96,262 hrs · 43,247 cycles

SHIP 0674 EMERGENCY EXIT LIGHT COVER FELL OFF ONTO FLOOR. CORRECTIVE ACTION: SECURED LENS. OPS CHECK GOOD. (9490396)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 96,237 hrs · 43,227 cycles

SHIP 674 EMERGENCY EXIT SIGN OVER L2 DOOR CAME OFF. CORRECTIVE ACTION: RESECURED L2 DR EXIT SIGN. (9490368)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 96,189 hrs · 43,195 cycles

SHIP 674 STRINGER 30 CORRODED AT STA 1450. CORRECTIVE ACTION: COMPLIED WITH FUSELAGE /STRINGER 30/STA 1440 -1460 / CORROSION REPAIR - ER/A 612659-14 REV. ORIG. PRI "0", "1", "2" REPAIR INSTRUCTION STEPS. ENSURED ALL R/A 612659-14 REV. ORIG. PRI "0", "1", "2" INSTRUCTIONAL STEPS COMPLETED AND MATCHED WITH FINAL ER/A 612659-14 REV. ORIG. SECTION 1 PERMANENT REPAIR INSTRUCTIONS. (0019880)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 96,189 hrs · 43,195 cycles

SHIP 674 WING CENTER BOX / UPPER SKIN AND STRINGER 14 / BSTA 960 AND BETWEEN LBL 70.50 & LBL 45.57 / CORROSION. CORRECTIVE ACTION: REF ERA 597544-14. (2999918)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 96,104 hrs · 43,138 cycles

3L SLIDE LIGHT INOPERATIVE. T/S FOUND BAD GROUND AT LIGHT. WIRING CKS GOOD. R/R BOTH PROX SWITCHES PER B757 AMM 25-66. OPS CKS GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 96,049 hrs · 43,104 cycles

SHIP 0674 EMERGENCY EXIT DOOR 3R SLIDE ARMED LIGHT INOPERATIVE. CORRECTIVE ACTION: INSTALLED NEW SLIDE ARM LIGHT ASSY REF B757-200 AMM 33-51. OPS CKS NORMAL. OK FOR SERVICE. (4553322)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 96,031 hrs · 43,097 cycles

SHIP 0674 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:2L. CORRECTIVE ACTION: REATTACHED EXIT SIGH LENS COVER. (2957743)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 96,001 hrs · 43,081 cycles

SHIP 0674 L2 EXIT LENS CAME OFF. CORRECTIVE ACTION: INSTALLED LENS. (4553300)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,989 hrs · 43,073 cycles

SHIP 0674 AFT LEFT (L3) DOOR ARMED LIGHT DOES NOT ILLUMINATE. CORRECTIVE ACTION: REMOVED AND REPLACED SLIDE LIGHT CAP PER B757 AMM 3351. LIGHT OPS CHK NML. AC OK FOR SVC. (4473488)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,949 hrs · 43,050 cycles

SHIP 0674 HOLE IN UPPER SURFACE OF INBD FLAP ON RT WING. CORRECTIVE ACTION: REF ERA 611577-14. (4473462)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,870 hrs · 43,007 cycles

SHIP 0674 R1 DOOR ESCAPE SLIDE LITE INOPERATIVE. CORRECTIVE ACTION: REMOVED AND REPLACED GIRT BAR PER B757 AMM 25-66. VERIFIED SAFETY PIN REMOVAL FROM SLIDE AND ASSIST BOTTLE. INSTALLED THE COVER FOR THE ESCAPE SLIDE, REMOVED THE SAFETY PIN FROM THE EMERGENCY POWER RESERVOIR. DOOR NOW ARMS NORMALLY. (4473416)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,870 hrs · 43,007 cycles

SHIP 0674 DOOR 1R SLIDE LIGHT INOPERATIVE. CORRECTIVE ACTION: REPLACED CAP SLIDE LIGHT ASSY PER B757 IPC-33-51. LIGHT OPS CHECK GOOD. (4473404)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,861 hrs · 43,000 cycles

SHIP 0674 1R DOOR WILL NOT ARM. CORRECTIVE ACTION: CYCLED R1 DOOR OPEN AND CLOSED. DOOR ARMS AND DISARMS NORMALLY. REF B757 AMM 25 -66. A/C OK FOR SVC. (4473400)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,861 hrs · 43,000 cycles

SHIP 0674 IR DOOR "SLIDE" LIGHT NOT ILLUMINATED WHEN DOOR LEVER SELECTED TO ARM. CORRECTIVE ACTION: ADJUSTED THE GIRT BAR. LIGHT IS WORKING. GIRT BAR IS LOCKED IN PLACE PER B737 AMM 25-66. A/C OK FOR SVC. (4893492)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,826 hrs · 42,977 cycles

SHIP 0674 DOOR R1 GIRT BAR ENGAGEMENT LIGHT INOPERATIVE. CORRECTIVE ACTION: REMOVED AND REPLACED SLIDE ARMED INDICATOR LIGHT. REMOVED AND REPLACED BOTH PROX SWITCH IAW B757 AMM 25-66. OPS CHECKS GOOD NOW. (4893468)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,595 hrs · 42,832 cycles

SHIP 0674 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:603. CORRECTIVE ACTION: SECURED LIGHT COVER. (2851887)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,566 hrs · 42,810 cycles

SHIP 0674 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:603. CORRECTIVE ACTION: RE SECURED SIGN COVER. OK FOR SVC. (2846507)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,559 hrs · 42,804 cycles

SHIP 0674 OVERHEAD EXIT SIGN AFT OF L2 DOOR IS MISSING A COVER. CORRECTIVE ACTION: RE INSTALLED OVERHEAD EXIT SIGN PER B757 AMM 33-51. A/C OK FOR SVC. (4935810)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,475 hrs · 42,758 cycles

SHIP 674 SVC CK FOUND DOOR L2 STOP PLATE MISSING. CORRECTIVE ACTION: REPLACED STOP PLATE DOOR L-2 PER B757 AMM 52-11. (4792174)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,409 hrs · 42,716 cycles

SHIP 674 L-14 DOOR ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT INOP. CORRECTIVE ACTION: ARMED AND DISARMED L1 DOOR SLIDE MULTIPLE TIMES AND LIGHT CAME ON EVERY TIME. COULD NOIT DUPLICATE PROBLEM. (2808875)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,369 hrs · 42,683 cycles

SHIP 674 R1 DOOR INDICATOR INOP. REMOVED AND DISARMED R1 DOOR WITH SLIDE LIGHT OPERATES AS REQUIRED. (4141378)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,313 hrs · 42,644 cycles

SHIP 674 L2 DOOR EXIT LIGHT COVER CAME OFF. CORRECTIVE ACTION: INSTALLED L2 DOOR EXIT LIGHT COVER REF B757 AMM 33-51. (4141356)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 95,075 hrs · 42,501 cycles

SHIP 674 2L DOOR EMER EXIT SIGNIS HANGING LOOSE. CORRECTIVE ACTION: RE-SECURRED 2L DOOR EMER EXIT SIGN PER B757 AMM 33-51. OPS CHK NRML. (2739125)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,798 hrs · 42,343 cycles

SHIP 674 1L SLIDE LIGHT STAYS ILLUMINATED WITH DOOR IN DISARMED POSITION. CORRECTIVE ACTION: CYCLED 1L DOOR ARM/DISARM LEVER MULTIPLE TIMES WITH NORMAL INDICATION EACH TIME - CHKS OK TO CONTINUE IAW B757 AMM 52-70. (4067344)

Part: UNKNOWN — UNKNOWN · airframe 94,544 hrs · 42,184 cycles

SHIP 674 DOOR 1R SLIDE LIGHT DOES NOT ILLUMINATE WHEN DOOR IS ARMED. CORRECTIVE ACTION: ARMED AND DIS ARMED 1R SLIDE- INDICATORS CK GOOD, ARM LIGHT CKS GOOD. (4146016)

Part: TRANSMITTER — OUT OF LIMITS (LT TE FLAP) · airframe 94,188 hrs · 41,961 cycles

T/E FLAP ASYM MESSAGE. CORRECTIVE ACTION: MTC FOUND LEFT FLAP POSITION TRANSMITTER FAULT IN FSEU. TRANSMITTER WAS OFF 5 DEGREES IN EVER DETENT SETTING. REPLACED LT TRANSMITTER AND PERFORMED CHECK OUTS. C/W NO-GO PROCEDURES.

Part: CONTROLLER — ARCED · airframe 93,857 hrs · 41,745 cycles

SHIP 674 LFT FWD WINDOW ARCING AT BOTTOM WINDOW, HEATOFF AND QRL COMPLIED WITH. ACRING STOPPED. CORRECTIVE ACTION: REPLACED LT FWD COCKPIT WINDOW PER B757 AMM 56-11. REPLACED L1/ R2 WINDOW HEAT CONTROLLER, SYS TEST GOOD PER B757 AMM 30-41. (9089548)

Part: NONE — NONE · airframe 93,763 hrs · 41,668 cycles

SHIP 674 WORKING WORKCARD 3352-01042-01D. CORRECTIVE ACTION: R/R EXIT IDENTIFIERS AT 1L, 2L, AND 4L DOORS REF B757 AMM 33-51-10. (9175995)

Part: NONE — NONE · airframe 93,763 hrs · 41,668 cycles

SHIP 674 WORKING WORKCARD 3352-01042-01D. CORRECTIVE ACTION: R/R EXIT IDENTIFIERS AT 1R, 2R, AND 4R DOORS REF B757 AMM 33-51-10. (9175994)

Part: NONE — NONE · airframe 93,461 hrs · 41,428 cycles

SHIP 674 L1 DOOR SLIDE INDICATOR LIGHT DETACHED. CORRECTIVE ACTION: SECURE SLIDE LIGHT INDICATOR PER B757 AMM 25-66. (8613164)

Part: NONE — NONE · airframe 93,414 hrs · 41,392 cycles

SHIP 674 4C EMERGENCY LIGHT INOP. CORRECTIVE ACTION: REPLACED LIGHT ASSY @ SEAT 4 RIGHT REF B757 IPC 33-51 OPS CHECK GOOD. (8613126)

Part: NONE — NONE · airframe 93,408 hrs · 41,386 cycles

SHIP 674 DOOR 1 RT EMERGENCY SLIDE GIRT BAR ATTACH FITTING FOUND ON FLOOR NEXT TO SLIDE BUSTLE. CORRECTIVE ACTION: FOUND D RING VELCRO TORN OFF , REINSTALLED VELCRO AND D RING, OPS CKS GOOD REATTACHED GIRT BAR FITTING ON AFT SIDE GIRT BAR CKS GOOD IAW B757 IPC 25-66. (8613129)

Part: NONE — NONE · airframe 93,380 hrs · 41,364 cycles

SHIP 674 UNABLE TO ARM 4L DOOR. CORRECTIVE ACTION: RMVD DEBRIS OPS CKS OK PER B757MM 25-66. (9283592)

Part: NONE — NONE · airframe 93,296 hrs · 41,300 cycles

AIRCRAFT 674, RI PASSENGER DOOR GIRT BAR LOCK CAME DETACHED FROM GIRT BAR. CORRECTIVE ACTION: REINSTALLED GIRT BAR LOCK. (9283535)

Part: GIRT BAR — OUT OF ALIGNMENT · airframe 93,247 hrs · 41,263 cycles

SHIP 674 AT PUSHBACK 1R SLIDE LIGHT DID NOT ILLUMINATE. CORRECTIVE ACTION: REINSTALLED SLIDE BLOCK ON GIRT BAR VERIFIED ENGAGEMENT OPS NML LIGHT ILLUMINATES REF B757 AMM 5271. (9283506)

Part: GIRT BAR — OBSTRUCTED · airframe 93,225 hrs · 41,244 cycles

SHIP 674 AT PUSHBACK, R1 DOOR WOULD NOT ARM. CORRECTIVE ACTION: FOUND GREEN LANYARD OBSTRUCTING GIRT BAR FITTING-REPPOSITIONED LANYARD NOW OPS NML PER B 757 AMM 52-11. (8518694)

Part: GIRT BAR — DIRTY · airframe 93,079 hrs · 41,137 cycles

SHIP 674 DOOR 1R SLIDE LIGHT INOP. CORRECTIVE ACTION: REMOVED DEBRIS FROM GIRT BAR SWITCH. CKS GOOD. REF B757 AMM 25- 66-11. (8486088)

Part: INDICATOR — INOPERATIVE · airframe 92,993 hrs · 41,093 cycles

SHIP 674 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:601. CORRECTIVE ACTION: NO TROUBLE FOUND; OPS NML. (2232149)

Part: WARNING LIGHT — INTERMITTENT · airframe 92,941 hrs · 41,059 cycles

SHIP 674 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS----1 LEFT SLIDE LIGHT IS INTERMITTENT. CORRECTIVE ACTION: NSPECTED SAME PER B757 AMM 52-11. OPS CHK NML. (2224446)

Part: LIGHT — FAILED INSP · airframe 92,926 hrs · 41,046 cycles

SHIP 674 L, R EMER ESCAPE TEST SQUIB LIGHTS NOT INDICATING. CORRECTIVE ACTION: CYCLED STBY PWR SWITCH - ALL CKS GOOD. LIGHTS TEST NORMAL. (8486004)

Part: NONE — NONE · airframe 92,900 hrs · 41,023 cycles

SHIP 674 1R SLIDE LIGHT INOP. CORRECTIVE ACTION: CLEANED DEBRI FROM TARGET SENSORS AND OPS CHECKED DOOR 1R REF B757 AMM 52-11. ARMING LIGHT CHECKS OK. (7777458)

Part: NONE — NONE · airframe 92,900 hrs · 41,023 cycles

SHIP 674 1 L SLIDE LIGHT INOP. CORRECTIVE ACTION: OPS CHECKED 1 L DOOR ARMING AND SLIDE LIGHT REF B757 AMM 52-11. OPS CHECK GOOD. (7777459)

Part: NONE — NONE · airframe 92,846 hrs · 40,991 cycles

SHIP 674 1R SLIDE LIGHT WILL NOTILLUMINATE. CORRECTIVE ACTION: ADJUSTED GIRT BAR PROX SWITCH SENSOR A PER B717 AMM 25-66-11-822 -0011 OPS CHECKS GOOD. (2182774)

Part: NONE — NONE · airframe 92,789 hrs · 40,969 cycles

SHIP 674 1R SLIDE ILLUMINATION LIGHT INOP. CORRECTIVE ACTION: REPOSITIONED FWD GIRT. REINSTALLED SLIDE COVER. DOOR SLIDE LIGHT ILLUMINATES NORMAL. (7777418)

Part: NONE — NONE · airframe 92,789 hrs · 40,969 cycles

SHIP 674 DOOR 1L/1R GIRT BAR DISLODGED WHEN DOOR OPENED. CORRECTIVE ACTION: RESECURED 1L/1R GIRT BAR PER AMM 52-11-25. OPS NML. (7777412)

Part: FLOOR PANEL — CORRODED · airframe 92,749 hrs · 40,950 cycles

AHIP 674 INTERNAL FUSELAGE CENTER SECTION LH UNDER FLOOR PANEL 240-1 APPROX AT STA 960 UNDER SEALANT LINE WAS FOUND CORROSION WITH POPPED RIVET AND PROBABLY 1/4 INCH BUMP UNDER THE SKIN. CORRECTIVE ACTION: ACCOMPLISHED REPAIR ON WING CENTER BOX/ UPPER SKIN AND STR 14/BS 960 AND BTW LBL 70.50 AND LBL 45.57 IAW ER/A 597544-14 REV ORIGINAL. (2172998)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 96,189 hrs · 43,195 cycles

SHIP 0674 WING CENTER BOX / UPPER SKIN AND STRINGER 14 / BSTA 960 AND BETWEEN LBL 70.50 & LBL 45.57 / CORROSION. CORRECTIVE ACTION: REF ERA 597544-14. (2172871)

Part: SUPPORT — DAMAGED · airframe 92,750 hrs · 40,951 cycles

SHIP 674 WHILE PERFORMING HFEC INSPECTION ON R/H STA 1360 STR 26R AFT CARGO LINER SUPPORT FASTENERS. THE FRAME WHERE THE LOWER FASTNER IS CUT OUT AROUND THE FASTENER HEAD.UNABLE TO PERFORM NDT INSPECTION AS REQUIRED. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT AFT CARGO COMPT. FRAME STA 1360R STR 26R IAW ER/A 597600-14AD REV ORIGINAL. (2172794)

Part: NONE — NONE (NONE) · airframe 94,311 hrs · 42,029 cycles

DTE, ERA 597600-14 AN EXISITING REPAIR WAS FOUND ON FRAME AT BS 1360 RH AROUND STRINGER 26R. REF ERA 597600-14 REV ORG.

Part: NONE — NONE · airframe 92,749 hrs · 40,950 cycles

SHIP 674 DISBOND NOTED ON UPPER AND LOWER SURFACE OF #1 SLAT ASSY, COMMON TO DENT ON LOWER SURFACE, APPROX 4 INCHES. CORRECTIVE ACTION: ACCOMPLISHED REPAIR ON #1 SLAT ASSY T/E WEDGE UPPER AND LOWER SURFACE IAW B757-200 SRM 57-43-02-2R-1 FIG 201, NOTE D AND B757- 200 SRM 51-70-10-2R-4. (2143708)

Part: NONE — NONE · airframe 92,454 hrs · 40,770 cycles

SHIP 674 FOUND FRAME REPAIR ON FRAME 1300 COMMON THE VIASAT SHEAR TIES. CORRECTIVE ACTION: COMPLIED WITH ERA 596062-14AD REV. ORGINAL. PER TABLE 203 B757- 200 SRM. (2057046)

Part: NONE — NONE · airframe 92,242 hrs · 40,633 cycles

'SUPPLEMENTAL INFORMATION' SHIP 674 DURING SVC CHK FOUND FUSELAGE WING TO BODY FAIRING MISSING. CORRECTIVE ACTION: C/W SECTION 1 OF ER/A 531776-14MA REV ORIG. C/W ERA 561776-14MA ORIG. SECT. II PERMANENT REPAIR AT AFT WING TO BODY FAIRINGS AT 6 O'CLOCK POSITION. (8068895)

Part: CONTROL PANEL — FAULTED (EMERGENCY LIGHTS) · airframe 91,380 hrs · 40,325 cycles

SHIP 674 WHILE PUTTING A/C ON GROUND PWR EMER LIGHTS STAY ON. CORRECTIVE ACTION: R/R EMER LIGHT PANEL PER B757 AMM 33-51. OPS CHECK GOOD. (7865692)

Part: FRAME — CRACKED (BS 1640 S14R) · airframe 90,943 hrs · 40,106 cycles

SHIP 674 DURING INSPECTION MAINTENANCE FOUND THE R/H SIDE FRAME 1640 (3) FASTNERS BELOW THE INTERCOSTAL STRAP S-14 WITH INDICATIONS OF DEFECTS (CRACKS) NOTED. FASTENERS ARE MARKED IN RED SHARPIE AND INDICATIONS ARE MARKED AND MAPPED. CRACKS ARE ESTIMATED TO BE .250" IN LENGTH. FRAME REPAIRED PER ERA 591634-14AD. (LP 1813250)

Part: FRAME — CRACKED (BS 1640) · airframe 90,943 hrs · 40,106 cycles

SHIP 674 DURING INSPECTION MAITENANCE FOUND LH 1640 FRAME HAS CRACK INDICATIONS IN THE LOWER INBOARD HOLE AT APPROX 3 AND 9 O CLOCK LOOKING AFT. CRACK INDICATIONS ARE IN THE FRAME LAYER. REPAIRED LH FRAM PER ERA 592625-14AD. (LP 1812894)

Part: NONE — NONE · airframe 92,749 hrs · 40,950 cycles

SHIP 674 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 585020-14 REV A. CORRECTIVE ACTION: REF ERA 585020-14 REV A. (1781869)

Part: NONE — NONE · airframe 92,364 hrs · 40,709 cycles

SHIP 674 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 585022-14 REV A. CORRECTIVE ACTION: REF ERA 585022-14 REV A. (1781879)

Part: NONE — NONE · airframe 92,364 hrs · 40,709 cycles

SHIP 674 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 585020-14 REV A. CORRECTIVE ACTION: REF ERA 585020-14 REV A. (1781860)

Part: COVER — MISSING (L2 DOOR) · airframe 90,613 hrs · 39,983 cycles

SHIP 674 DOOR 2 LEFT MISSING DOOR PROXIMITY SENSOR COVER. CORRECTIVE ACTION: INSTALLED COVER PER B757 MM 52-71. (7398450)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 89,540 hrs · 39,627 cycles

EMERGENCY LIGHTS AT SEAT 27 THROUGH 37 ARE INOPERATIVE. CORRECTIVE ACTION: MAINTENANCE REPLACED EMERGENCY LIGHTS BATTERY SUPPLY. SYSTEM OPERATION IS NORMAL.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 89,195 hrs · 39,468 cycles

DURING INSPECTION FOUR EMERGENCY SEAT MOUNTED LIGHTS AT ROW 27-37 INOPERATIVE. CORRECTIVE ACTION: REPLACED FUSE IN POWER SUPPLY M10568. SYSTEM OPERATION IS NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 89,186 hrs · 39,465 cycles

EMERGENCY LIGHTS AT ROW 27-37 ARE INOPERATIVE. CORRECTIVE ACTION: REPLACED BATTERY PACK & CHARGER AT ROW 26E. SYSTEM OPERATION IS NORMAL.

Part: DIODE — FAILED (EMERGENCY LIGHTS) · airframe 89,158 hrs · 39,452 cycles

DURING INSPECTION FOUND EMERGENCY PATH LIGHTS AT ROWS 27-37 INOPERATIVE. CORRECTIVE ACTION: REPLACED THE DIODE AT PACK M10568. SYSTEM OPERATION IS NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 89,045 hrs · 39,397 cycles

DURING THE SERVICE CHECK, MAINTENANCE FOUND SEAT ROW 33-37 EMERGENCY PATH LIGHTING TO BE INOPERATIVE. REPLACED THE BATTERY CHARGER M11648 AND OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 88,816 hrs · 39,275 cycles

MERGENCY LIGHTS FROM SEAT 38D-42D ARE INOPERATIVE. REPLACED THE BATTERY PACK M735. SYSTEM OPERATION NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 88,810 hrs · 39,271 cycles

EMERGENCY BATTERY PACKS AT L1 AND 28 INOERATIVE. CORRECTIVE ACTION: REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL. (LP 6443853)

Part: SLIDE — INOPERATIVE (L2 DOOR) · airframe 88,810 hrs · 39,271 cycles

L2 DOOR SLIDE INOPERATIVE. REPLACED L2 SLIDE. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 88,780 hrs · 39,260 cycles

SHIP 674 EMERGENCY BATTERY POWER SUPPLY AT 27 DEF INOP. CORRECTIVE ACTION: REMOVED & REPL BATT PACK & CHARGER PER B757 AMM 33-51 ALL OPS NML. (6443828)

Part: POWERPACK — INOPERATIVE (CABIN) · airframe 88,695 hrs · 39,230 cycles

SHIP 674 SEAT ROWS 27 THRU 32 EMERGENCY LIGHTS ESCAPE PATH LIGHTING ARE OUT. CORRECTIVE ACTION: REPLACED POWER PACK M10568. (6422063)

Part: CHARGER — INOPERATIVE (CABIN) · airframe 88,661 hrs · 39,218 cycles

(AIRCRAFT 674, L/P 6422027) ON SVC CK FOUND EMERGENCY LIGHTING AT SEAT ROWS 37-32 INOP. T/S REQUIRED. CORRECTIVE ACTION: R/R BATTERY CHARGER REF B757 AMM 33-51.

Part: WIRE — DAMAGED (CABIN) · airframe 88,631 hrs · 39,206 cycles

(AIRCRAFT 0674, L/P 6422027) FOUND DURING S/C FLOOR EMERG LIGHT INOP ROW 27DEF TO 32DEF. CORRECTIVE ACTION: REF B757 WDM 33-51-22. FOUND FUSE BLOWN AT POWER SUPPLY M10568. SEAT 27F FLOOR TRACK REPAIRED WIRE INSULATION PER BOEING CH 20-10-13 PAGE 49. RPLD FUSE IAW B757 AMM 33-51-07.

Part: SKIN — CRACKED (NR 1 NACELLE) · airframe 88,501 hrs · 39,148 cycles

(AIRCRAFT 674, L/P 1499322) LH WING #1 PYLON #3 HOLE HAS 2 EA INDICATIONS IN THE CRACK INDICATION ZONE PER B757 NDTM 51-00-16 AT 3 AND 9 OCLOCK POSITION LOOKING AFT. 9 OCLOCK INDICATION ON FITTING AND 3 O CLOCK INDICATION IN UPPER SKIN. AA# 5720-01100-0101A. CORRECTIVE ACTION: REPAIRED LEFT WING I/B AND O/B DRAG FITTINGS AND UPPER SKIN IAW ER/A# 585022-14AD REV ORIGINAL C/W ALL CDCCL AND SFAR 88 REQUIREMENTS.

Part: SKIN — CRACKED (NR 1 NACELLE) · airframe 88,501 hrs · 39,148 cycles

(AIRCRAFT 674, L/P 1499333) LH WING #1 PYLON #10 HOLE HAS A CORROSION INDICATION AT 9 O CLOCK POSITION LOOKING AFT. INDICATION ON FITTING. AA# 5720-01100-0101A. CORRECTIVE ACTION: REPAIRED LEFT WING I/B AND O/B DRAG FITTINGS AND UPPER SKIN IAW ER/A# 585022-14AD REV ORIGINAL C/W ALL CDCCL AND SFAR 88 REQUIREMENTS.

Part: SKIN — CRACKED (NR 1 NACELLE) · airframe 88,501 hrs · 39,148 cycles

(AIRCRAFT 674, L/P 1499351) LH WING #1 PYLON #2 HOLE HAS A CORROSION INDICATION AT 3 O CLOCK POSITION LOOKING AFT. INDICATION ON FITTING. AA# 5720-01100-0101A. CORRECTIVE ACTION: REPAIRED I/B AND O/B DRAG FITTINGS AND UPPER SKIN ON LEFT WING IAW ER/A# 585022-14AD REV ORIGINAL C/W ALL CDCCL AND SFAR 88 REQUIREMENTS.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 88,493 hrs · 39,145 cycles

(AIRCRAFT 674, L/P 1498576) RH ENG. #2 PYLON #4 HOLE HAS A CORROSION INDICATION AT 5 OCLOCK POSITION LOOKING AFT. INDICATION IN THE TOP SKIN. CORRECTIVE ACTION: ACCOMPLISH ON ER/A 585020-14AD REV. O.

Part: SKIN — CRACKED (NR 1 NACELLE) · airframe 88,501 hrs · 39,148 cycles

(AIRCRAFT 674, L/P 1499317) LH WING #1 PYLON #4 HOLE HAS AN INDICATION IN THE CRACK INDICATION ZONE PER B757 NDTM 51-00-16 AT 3 OCLOCK POSITION LOOKING AFT. INDICATION IN FITTING. AA# 5720-01100-0101A. REPAIRED LEFT WING I/B AND O/B DRAG FITTINGS AND UPPER SKIN IAW ER/A# 585022-14AD REV ORIGINAL C/W ALL CDCCL AND SFAR 88 REQUIREMENTS.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 88,493 hrs · 39,145 cycles

(AIRCRAFT 674, L/P 1498567) RH ENG #2 PYLON #2 HOLE HAS 2EA INDICATIONS IN THE CRACK INDICATION ZONE ON THE X-Y DISPLAY PER B757 NDTM 51-00-16 AT 3 AND 9 O CLOCK POSITION LOOKING AFT. BOTH INDICATIONS IN THE TOP SKIN AA# 5720-01100-0101B. CORRECTIVE ACTION: ALL WORK ACCOMPLISHED PER ER/A 585020-14AD REV. O.

Part: SKIN — CRACKED (NR 1 NACELLE) · airframe 88,501 hrs · 39,148 cycles

(AIRCRAFT 674, L/P 1499344) LH WING #1 PYLON #5 HOLE HAS AN INDICATION IN THE CRACK INDICATION ZONE PER B757 NDTM 51-00-16 AT 9 OCLOCK POSITION LOOKING AFT. INDICATION ON FITTING. AA# 5720-01100-0101A. CORRECTIVE ACTION: REPAIRED LEFT WING I/B AND O/B DRAG FITTINGS AND UPPER SKIN IAW ER/A# 585022-14AD REV ORIGINAL C/W ALL CDCCL AND SFAR 88 REQUIREMENTS.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 88,493 hrs · 39,145 cycles

SHIP 674 LT ELEVATOR UPPER INBD SKIN HAS PREVIOUS REPAIR DELAMINATING. CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR ON LT ELEVATOR UPPER I/B SKIN IAW B757-200 SRM. (1478695)

Part: GIRT BAR — DETACHED (R1 DOOR) · airframe 88,315 hrs · 39,068 cycles

(AIRCRAFT 674, L/P 6681670) 1R GIRT BAR WOULD NOT ARM. CORRECTIVE ACTION: RE-ATTACHED PER B757 AMM 52-10.

Part: SPRING — BENT (R1 DOOR GIRT BAR) · airframe 87,638 hrs · 38,771 cycles

R1 DOOR SPRING BENT WHEN GIRT BAR DISENGAGED. CORRECTIVE ACTION: REPLACED 1R GIRT BAR PER B757 AMM 25-66.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 87,218 hrs · 38,591 cycles

AT FL350 CABIN CLIMBED AT +200 FPM (CRUISE) DURING DESCENT. CABIN CONTROL WAS ERRATIC. REPLACED CABIN OUTFLOW VALVE PER B757 AMM 21-31. C/W NO GO ODI PROCEDURE.

Part: GIRT BAR — NOT REPORTED (R1 DOOR SLIDE) · airframe 87,193 hrs · 38,578 cycles

R1 DOOR GIRT BAR WITH CABLE. R & R THE R-1 SLIDE ASSY, GIRT BAR, & BAR SLIDERS IAW AMDS WORK CARD 2566-9001-1R RII COMPLETE.

Part: DOOR SILL — DIRTY (R1 DOOR) · airframe 87,061 hrs · 38,519 cycles

UNABLE TO ARM THE R1 DOOR. CLEANED DOOR SILL FROM DEBRIS. OPS NORMAL B757 AMM 52-11.

Part: SLIDER — OUT OF POSITION (R1 DOOR GIRT BAR) · airframe 87,004 hrs · 38,496 cycles

R1 DOOR GIRT BAR HANGING OUT OF PLATE. FOUND THE FWD GIRT BAR SLIDER OUT OF PLACE. SECURED GIRT BAR SLIDER CORRECTLY IAW AMM 25-66 VERIFIED 1R DOOR SLIDE ARMS AND DISARMS NORMAL.

Part: LIGHT — MALFUNCTIONED (L1 DOOR SLIDE) · airframe 87,004 hrs · 38,496 cycles

L1 DOOR SLIDE ARM LIGHT INTERMITTENT STAYS ON WITH SLIDE DISARMED. REPLACED THE LENS CAP. OPS NORMAL.

Part: BOLT — SHEARED (L2 DOOR) · airframe 86,228 hrs · 38,160 cycles

SHIP 674 D2L GUIDE ARM ASSY FOUND DETACHED 2 BOLTS SHEARED. CORRECTIVE ACTION: REMOVED INTERNAL LOWER HINGE COVER PLATE, REPLACED BROKEN LOWER GUIDE ARM ATTACH NUT PLATES. REINSTALLED HINGE COVER PLATE. REATTACHED GUIDE ARM IAW. (5797012)

Part: PROXIMITY SWITCH — FAULTY (L3 DOOR) · airframe 85,745 hrs · 37,934 cycles

SHIP 674 3L DOOR SLIDE ARMED LIGHT INOP. CORRECTIVE ACTION: R/R AFT GIRT BAR PROX SWITCH IAW AMM 25-66 OP CHECKS GOOD. (5140444)

Part: PRESSURE SWITCH — DEFECTIVE (EVAC SLIDE) · airframe 85,503 hrs · 37,835 cycles

L OVERWING ESCAPE SLIDE BOTTLE PRESSURE SYSTEM INOP. T/S PER FIM 25-65-00-815-803 CONFIRMED BAD BOTTLE PRESSURE SWITCH. R&R LEFT OVERWING EMERGENCY ESCAPE SLIDE INFLATOR PER CARD.

Part: PLATE — MISSING (SERVICE DOOR) · airframe 85,129 hrs · 37,679 cycles

SHIP 674 DURING GIRT BAR LUBE OPERATION FOUND RT AFT SVC DOOR ONE DOOR STOP BEARING PLATE MISSING. FWD FRAME SECOND FROM TOP LOCATION. CORRECTIVE ACTION: INSTALLED NEW BEARING PLATE IAW B757 AMM 52-11. (5232683)

Part: LAMP — INOPERATIVE (SLIDE INDICATOR) · airframe 84,949 hrs · 37,582 cycles

SHIP 674 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS: 3L. CORRECTIVE ACTION: R/R LAMP CAP ASSEMBLY PER WDM 25-66. (0836960)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 84,582 hrs · 37,383 cycles

SKIN DAMAGE ON UPPER FUSELAGE AT ADSB ANTENNA.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 84,582 hrs · 37,383 cycles

DURING MAINTENANCE FOUND STR 1 DAMAGED AT STA 660 TO STA 710. REPAIRED STR1 REF SRM 53-00-03.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 84,582 hrs · 37,383 cycles

DURING MAINTENANCE FOUND STR 2L DAMAGED FROM STA 660 710. REPAIRED STR 2L REF SRM 53-00-03.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 83,648 hrs · 37,015 cycles

R1 DOOR SLIDE HANGING OUT OF THE COVER. REMOVED AND REPLACED THE SLIDE IAW WC 2566-9001-1R.

Part: FRAME — CORRODED (BS 1300) · corrosion level 2 · airframe 83,050 hrs · 36,754 cycles

AFT CARGO BAY BS 1300, FRAME UPPER SURFACE HAS CORROSION ABOVE STRINGER 30. CORROSION DAMAGE FOUND OUT OF LIMITS. REPAIRED THE FRAME IAW ER/A 556942-14AD, REV. ORIGINAL.

Part: STIFFENER — CORRODED (AFT CARGO DOOR) · corrosion level 2 · airframe 83,034 hrs · 36,747 cycles

AFT CARGO DOOR NR 3 STIFFENER FROM AFT END HAS CORROSION. REMOVED, FABRICATED, AND INSTALLED A NEW STIFFENER IAW SRM 51-40-02, DRAWINGS 146N6603, REV K, AND REV BP.

Part: FLOOR SUPPORT — BROKEN (BS 1540-1560) · corrosion level 2 · airframe 83,034 hrs · 36,747 cycles

AFT CARGO FLOOR SUPPORT UPPER ATTACH ANGLE BROKEN BS 1540 - 1560, LBL 24. FABRICATED AND INSTALLED A NEW ANGLE IAW SRM 51-40-02, AND DWG 146N5450, REV A.

Part: STIFFENER — CORRODED (AFT CARGO DOOR) · corrosion level 2 · airframe 83,034 hrs · 36,747 cycles

AFT CARGO DOOR NR 4 STIFFENER HAD CORROSION. REMOVED, FABRICATED, AND INSTALLED A NEW STIFFENER IAW SRM 51-40-02, DRAWING 146N6603 REV BP, AND REV K.

Part: STRAP — CHAFED (BS 1661-1681) · airframe 83,034 hrs · 36,747 cycles

FLOORBEAM STRAP BETWEEN BS 1661 - 1681, BL 0, CHAFED AND GOUGED.

Part: FLOOR SUPPORT — CORRODED (BS 1540-1560) · corrosion level 2 · airframe 83,034 hrs · 36,747 cycles

CORROSION FOUND ON THE FLOOR SUPPORT BETWEEN BS 1540 - 1560, LBL 24. FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 146N5434, REV.

Part: STIFFENER — CORRODED (AFT CARGO DOOR) · airframe 83,034 hrs · 36,747 cycles

AFT CARGO DOOR STIFFENER HAS A DEEP GOUGE. REMOVED, FABRICATED, AND INSTALLED A NEW STIFFENER IAW SRM 51-40-02, DRAWING 69-47423, REV B, REV H, AND 146N6603, REV K.

Part: SKIN — GOUGED · airframe 83,034 hrs · 36,747 cycles

FUSELAGE SKIN GOUGED AT FORWARD CARGO DOOR CONTROL PANEL 122AR. REPAIRED THE SKIN IAW SRM 53-00-01, REPAIR 18.

Part: SKIN — DENTED (NR 5 SLAT) · airframe 83,034 hrs · 36,747 cycles

FOUND A DENT AT THE NR 5 L/E ISS 234. REPAIRED IAW SRM 57-43-01, REPAIR 9.

Part: SKIN — GOUGED · airframe 83,034 hrs · 36,747 cycles

FUSELAGE SKIN GOUGED AT THE AFT CARGO DOOR CONTROL PANEL 154AR. REPAIRED THE SKIN IAW SRM 53-00-01, REPAIR 18.

Part: INTERCOSTAL — CORRODED (BS 1400-1420) · corrosion level 2 · airframe 83,034 hrs · 36,747 cycles

AFT CARGO, BETWEEN BS 1400 - 1420, STRINGER 30R, INTERCOSTAL CORRODED. REMOVED, FABRICATED, AND INSTALLED A NEW INTRCOSTAL IAW SRM 51-40-02, AND DRAWINGS 146N5399 REV B, AND REV F.

Part: SKIN — CORRODED (BS 750-790) · corrosion level 2 · airframe 83,034 hrs · 36,747 cycles

EXTERNAL FUSELAGE SKIN BS 750 - 790, BETWEEN STRINGERS 18R AND 22R, HAD CORROSION. REPAIRED THE SKIN IAW ER/A 556487-14AD, REV ORIGINAL.

Part: GATE — GOUGED (R1 DOOR) · airframe 83,034 hrs · 36,747 cycles

R1 DOOR HAS A GOUGE AT THE LOWER AFT CORNER. REMOVED AND REPLACED THE GATE IAW AMM 52-11-38.

Part: SKIN — DENTED (NR 5 SLAT) · airframe 83,034 hrs · 36,747 cycles

DENT ON THE NR 5 SLAT L/E ISS 234. FOUND OUT OF LIMITS. ACCOMPLISHED A PERMANENT REPAIR IAW SRM 57-43-01, REPAIR 9.

Part: FLOORBEAM — CORRODED (BS 1680) · corrosion level 2 · airframe 83,034 hrs · 36,747 cycles

CORROSION ON THE AFT CARGO BS 1680 FLOORBEAM BL 0 TO BL 44 AND AROUND NUTPLATES AND ATTACH CLIPS. CORROSION FOUND OUT OF LIMITS. REPAIRED IAW ER/A 556488-14, REV ORIGINAL.

Part: SHEAR TIE — CORRODED (BS 1620) · corrosion level 2 · airframe 83,034 hrs · 36,747 cycles

AFT CARGO BAY BS 1620 SHEAR TIE IS CORRODED BETWEEN STRINGERS 29L & 30L. FOUND TO BE OUT OF LIMITS. REMOVED, FABRICATED, AND INSTALLED A NEW SHEAR TIE IAW SRM 51-40-02, 51-40-05, AND DWG 146N1022, REV C, AND REV EU.

Part: ACTUATOR — CORRODED · airframe 83,034 hrs · 36,747 cycles

BARE METAL AND CORROSION ON HOUSING OF LINEAR ACTUATOR MOUNTED UPPER FWD ON ELEVATOR MIXING CONTROL ON AFT ACCESSORY BAY ON TOP AND AFT OF HORIZONTAL STAB CENTER BOX. REMOVED AND REPLACED THE ASSYMETRY LIMITER ACTUATOR IAW AMM 27-31-03.

Part: CUSP WEB — CORRODED (BS 921) · corrosion level 2 · airframe 83,034 hrs · 36,747 cycles

BS 921, LBL 67, STRINGER 17L, EXFOILIATING CORROSION ON THE CUSP WEB. CORROSION DAMAGE FOUND OUT OF LIMITS. REMOVED AND REPLACED THE CUSP WEB IAW SRM 51-40-02, AND DRAWING 144N5140, REV D.

Part: FITTING — CORRODED (BS 1680) · corrosion level 2 · airframe 83,034 hrs · 36,747 cycles

CORROSION FOUND ON THE AFT SCUFF PLATE ATTACHMENT FITTING AT THE L4 DOOR, BS 1680. THE CORROSION WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE FITTING IAW SRM 51-40-02, AND DRAWING 146N8722, REV N.

Part: ANGLE — CORRODED (BS 1720) · corrosion level 2 · airframe 83,034 hrs · 36,747 cycles

CORROSION UNDER PRESSURE DECK IN THE AFT CARGO, BS 1720, LBL 40, ON THE NUT PLATES, L ANGLE, AND THE PRESSURE DECK. ALL THREE SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED THE L ANGLE IAW SRM 51-40-02, 53-00-51, AND DWG #146N5300 REV C.

Part: FLOOR SUPPORT — DAMAGED (BS 398) · airframe 83,034 hrs · 36,747 cycles

MAIN CABIN, BS 398, RBL 60, FLOOR SUPPORT HAS ELONGATED HOLES. REMOVED, FABRICATED, AND INSTALLED A NEW MAIN CABIN FLOOR SUPPORT IAW SRM 51-40-02, 51-40-05, DRAWINGS 141N5162, REV-, REV.A, 141N5161, REV C, REV AG.

Part: BRACKET — CORRODED (BS 1715) · corrosion level 2 · airframe 83,034 hrs · 36,747 cycles

CORROSION BEHIND NUTPLATE BRACKET, BOTTOM SIDE OF PRESSURE DECK BS 1715, LBL 24. CORROSION DAMAGE FOUND TO BE OUT OF LIMITS DUE TO 100% MAT. LOSS, IAW SRM 53-00-51. REMOVED, FABRICATED, AND INSTALLED A NEW BRACKET IAW 51-40-02, DRAWINGS 146N5300, REV C, 146N5240, REV C, AND REV.H.

Part: SEAL DEPRESSOR — CHAFED (R4 DOOR) · airframe 83,034 hrs · 36,747 cycles

R4 DOOR CUTOUT UPPER LANDING CHAFED. FOUND SEAL DEPRESSOR TO BE OUT OF LIMITS IAW SRM 53-61-15. REMOVED AND INSTALLED A NEW SEAL DEPRESSOR IAW SRM 51-40-02, AND DWG 146N6104 REV A.

Part: GIRT BAR — DIRTY (R2 DOOR) · airframe 82,624 hrs · 36,605 cycles

(AIRCRAFT 674, L/P 3676744) F/A REPORTS 2R DOOR "ARMED" LITE STILL ILLUMINATED WHEN IT SHOULD BE DISARMED. CLEARED DEBRIS FROM GIRT BAR BRACKET.

Part: GIRT BAR — DIRTY (L4 DOOR) · airframe 82,197 hrs · 36,452 cycles

AT PUSH BACK, FA REPORTED THEY WERE UNABLE TO ARM THE L4 DOOR. FOUND DEBRIS BLOCKING THE GIRT BAR FROM ENGAGING. CLEANED DEBRIS FROM THE ARMING MECHANISM, WORKS OK. GOOD FOR SERVICE.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 82,171 hrs · 36,444 cycles

R1 DOOR SLIDE LIGHT WILL NOT INDICATE. INSTALLED NEW SLIDE LIGHT ASSEMBLY AT THE R1 DOOR IAW WDM 25-66. OPS NORMAL.

Part: INLET — DAMAGED (ENGINE) · airframe 80,432 hrs · 35,878 cycles

FAN INLET DAMAGED AT THE 5 AND 7 O`CLOCK POSITIONS. INSTALLED A REPAIR IAW ERA 480335-14MA, REV B, SECTION 1.

Part: ACOUSTIC LINER — DAMAGED (ENGINE) · airframe 80,432 hrs · 35,878 cycles

NOSE COWL ACOUSTICAL LINER DAMAGED IN 6 PLACES. INSTALLED PERMANENT REPAIR PER ERA363449-14MA.

Part: FLOORBEAM — DAMAGED (BS 1500) · airframe 79,974 hrs · 35,730 cycles

DURING INSTALLATION OF E7 RACK, WHEN REMOVING PREVIOUS RACK, FOUND DAMAGE TO THE FLOORBEAM BS 1500, RBL 45.50. REPAIRED IAW ERA 554986-14 REV ORIG.

Part: FLOORBEAM — DAMAGED (BS 1520) · airframe 79,974 hrs · 35,730 cycles

DURING INSTALLATION OF E7 RACK , WHEN REMOVING PREVIOUS RACK, FOUND DAMAGE TO THE FLOORBEAM AT BS 1520, RBL 45.5, REPAIRED IAW ERA 554987-14 REV ORIG.

Part: BEARING — CORRODED (NR 2 SLAT) · airframe 77,088 hrs · 34,526 cycles

BEARING RUSTED, NR 2 SLAT OTBD, INBD SUPPORT BEARING HAS RUST COMING OUT OF IT. SUMMARY NR FOR ADDITIONAL INFORMATION 001-0258:2020-2339/008. CLEANED AND LUBED BEARING IAW PS 900-2-1001-0258:2020-2339/008.

Part: FLAP TRACK — CORRODED (NR 2 FLAP) · airframe 77,088 hrs · 34,526 cycles

NR 2 FLAP TRACK HAS RUST COMING OUT BETWEEN FLAP TRACK AND WING LOWER SURFACE AT AFT INBD CORNER ATTACH AREA. REPAIRED FLAP TRACK CORROSION IAW CMM 27-51-82. CORROSION IS LEVEL 1. REPAIRED ON NR 85. REMOVED/INSTALLED ON NR 275.

Part: SKIN — DENTED (BS 520-550) · airframe 77,088 hrs · 34,526 cycles

ERA383903-14AD, REV E FS 520 TO FS 550/S14L TO S16L, LT SKIN DENTS & FS 540 FRAME SHEAR TIE CRACKED AD2001-20-12 - RESTRICTION 2. ERA INI CYC ACTL/2110 CONVERTED TO SCEPTRE ON 09OCT13 03:51 UTC AD NR FROM ACTL 2001-20-12, ENG ACTL AD NR DOES NOT HAVE ASSOCIATED ACTL EA NR, ENG, AD TO AA CONVERSION NOT COMPLETED, ENG, AA 5100-01787 IN AD-AA CONVERSION LIST NOT IN SCEPTRE IMD FOR AD NR ERA ISSUE DATE 29SEP02 WAS AFTER LAST DEFERED DATE 24MAR92. USED LAST DEFERED DATE AS THE LOG REPORTED BY DATE. REDEFERRED LOG TO QC, ESTAB MONITOR INSPECTIONS; 10-0553-8-0410, SN 674 INI SEC II, 10-0553-8-0411, SN 674, REP SEC II. C/W LFEC OF PERIMETER ROW OF FASTENERS IAW NDT MANUAL, PT 6 53-00-06, NO DEFECTS.

Part: SEAL — TORN (LIFE RAFT) · airframe 77,076 hrs · 34,516 cycles

F/A OBSERVE TORN SEAL ON LIFE RAFT LOCATED IN AFT MIN CABIN. PERFORMED GVI ON ALL LIFE RAFTS, ALL SEALS INTACT. OPS CHECK GOOD. OK FOR SERVICE.

Part: SKIN — DAMAGED (BS 574) · airframe 77,088 hrs · 34,526 cycles

ERA369014-14, REV C, FS 574, STR 27L/LIGHTNING STRIKE DAMAGE TIME LIMITED. ERA REP CYC ACTL/2100 CONVERTED TO SCEPTRE ON 09OCT13 03:51 UTC, REDEFERRED LOG TO QC, ESTAB MONITOR INSPECTION; 10-0553-8-0406, SN 674, REP SEC II. OPENED FWD CARGO FLOOR PANEL FOR INSPECTION ACCESS. C/W INSPECTION IAW MON 56 REP, 1129533, INSP, EC, ERA 369014C-11, FUS, 674. CLOSED FWD CARGO FLOOR PANEL. C/W HFEC INSPECTION IAW ERA 369014-14, REV C SECTION 2 REP INSPECTION. NO CRACKS. COMPLETED INSTALLATION OF FLOOR PANEL THAT WAS PARTIALLY REMOVED IN PRIOR STEP.

Part: LIGHT — INOPERATIVE (SEAT 2C) · airframe 76,610 hrs · 34,342 cycles

SEAT 2C EMERGENCY LIGHT INOPERATIVE AND NEEDS DIFFUSER LENS. REMOVED LIGHT ASSY. REPLACED LENS, CHECKS NORMAL.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 74,728 hrs · 33,553 cycles

EMERGENCY LIGHTS AT MAIN CABIN ROWS 1 AND 32 INOPERATIVE. FOUND BROKEN WIRES AT MAIN CABIN SEAT ROW 1 AMD 32 SPLICED WIRES AT BROKEN LOCATION IAW SWPM 20-30-12.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 73,347 hrs · 32,948 cycles

DURING A SERVICE CHECK, FOUND EMERGENCY LIGHT ON SEAT 1CD INOPERATIVE. REPAIRED BROKEN SPLICE ON SEAT WIRING HARNESS, IAW BSWPM 20-30. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (SEAT 21D) · airframe 72,000 hrs · 32,377 cycles

EMERGENCY LIGHT ON SEAT 21D INOPERATIVE. R & R EMERGENCY LIGHT ASSY.

Part: SKIN — DAMAGED (BS 215) · airframe 70,971 hrs · 31,952 cycles

SKIN AT BS 215.25, S20R, DENTED. REPAIRED IAW ERA 502852-14, REV B.

Part: FAIRING — CRACKED (LT WING TE FLAP) · airframe 70,935 hrs · 31,937 cycles

DENT IN LEFT INBD MAIN FLAP 18, OTBD OF CANOE FAIRING. REPAIRED IAW ERA 452274-14.

Part: SKIN — DENTED (BS 215) · airframe 71,280 hrs · 32,077 cycles

DENT IN LT FUSELAGE SKIN AT BS 215 S26L. DENT WAS CUT OUT AND DOUBLER INSTALLED IAW SECTION I OF ERA 523592-14, REV ORIG.

Part: CARRIAGE — CHAFED (RT WING TE FLAP) · airframe 70,824 hrs · 31,894 cycles

WINGS / ATTACH FITTINGS / RH INBD MAIN FLAP OUTBD CARRIAGE ASSEMBLY / OUTBD SIDE CHAFFED REPAIRED IAW ERA 489932-14 LOG PAGE 1129541 / 

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 70,736 hrs · 31,863 cycles

EMERGENCY LIGHTS INOPERATIVE 3CD / 5AB. REPAIRED WIRES IAW SWPM 20-10. CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 70,699 hrs · 31,849 cycles

SEAT 27DEF AFT SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. REPAIRED BROKEN WIRE IAW ESPM 20. CHECKED OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,961 hrs · 31,547 cycles

FIRST CLASS EMERGENCY LIGHT INOPERATIVE. REPLACED PACK BATTERY AND FUSE IAW WDM 33-51. EMERGENCY LIGHTS OPS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,868 hrs · 31,505 cycles

ENTIRE FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY M9101 AND BATTERY. OPS NORMAL IAW AMM 33-51.

Part: UNKNOWN — ODOR (CABIN) · airframe 69,694 hrs · 31,431 cycles

ODOR REPORTED MID CABIN, INFLT, NEAR ROW 27-28. DROPPED PAX SERVICE UNITS BY ROW 27-28 AND 29DEF. REMOVED BOTH RT SIDE O/W EXIT HATCHES AND INSPECTED AREA / RAN PACKS, NO ODOR NOTED. ALL IAW AMM 52-22-01. ACFT SMOKE AND FUME QUESTIONAIRE FWD IAW INSTRUCTIONS. ACFT OK IAW SVC.

Part: SKIN — DAMAGED (BS 328 S10L) · airframe 69,429 hrs · 31,329 cycles

FUSELAGE SKIN BS 328 S10L HAS A LIGHTNING STRIKE, BLIND FASTENER REPAIR. REMOVED FASTENER AND INSPECTED, NO CRACKS C/W PERM REPAIR OF ERA 507383-14, REV ORG.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,767 hrs · 31,094 cycles

DURING SERVICE CHECK, FOUND SIX EMERGENCY LIGHTS OUT. R & R BATTEY PACK CHARGER IAW AMM 33-51. OPS CHECKED OK.

Part: FEEDER CABLE — BROKEN (EMERGENCY LIGHTS) · airframe 68,433 hrs · 30,971 cycles

SEAT 24D EMERGENCY PATH LIGHT INOPERATIVE. FOUND LAMP TO FLOOR CABLE BROKE. REPLACED IAW 20 . OPS GOOD.

Part: SKIN — DAMAGED (BS 215.25 S20) · airframe 68,293 hrs · 30,905 cycles

DENT AND SCRATCHES ON FUSELAGE SKIN. REMOVED SCRATCHES. ALODINED, PRIMED AND PAINTED AFFECTED AREA, IAW SRM 51-20-01.

Part: SKIN — DENTED (BS 215.25 S20R) · airframe 68,063 hrs · 30,799 cycles

DURING LAYOVER INSPECTION, MX FOUND A SKIN DENT AT BS 215.25 AND ABOVE S20R AT WL 198. REPAIR PERFORMED IAW ERA 502852-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 67,718 hrs · 30,654 cycles

FOUND A SCATCH, A SLIGHT DENT ON BELLEY 15", FWD 17" LT OF CENTER OF FWD WI-FI ANTENNA. CLEANED UP SCRATCH PAINT AREA. DAMAGE LESS THAN LIMIT IAW SRM 53-00-01.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,034 hrs · 30,379 cycles

ON SERVICE CHECK FOUND ROW 2CD, 5CD AND 6CD EMERGENCY PATH LIGHTS INOPERATIVE. LAMPED 5CD AND 6CD SEAT ROW LIGHTS CHECKED OK. NO HELP ON SEAT 2CD FOUND BAD CONNECTION. ALSO, DURING FINAL OPS CK ALL FIRST CLASS LIGHTS WENT INOPERATIVE. R & R BATTERY CHARGER AND BATTERYPACK IAW AMM 33-51-07. REPAIRED WIRING IAW SWPM 20-30. OPS CHECK NORMAL. ACFT OK FOR SVC.

Part: SOCKET — UNSECURE (EMERGENCY LIGHT) · airframe 66,604 hrs · 30,185 cycles

MX DISCOVERED THE EMERGENCY LIGHT ABOVE SEAT 23D INOPERATIVE. SECURED BULB SOCKET. OPS OK.

Part: SKIN — DAMAGED (BS 1500 S5L) · airframe 66,383 hrs · 30,091 cycles

MX DISCOVERED A LIGHTNING STRIKE AT BS 1500, STR 5L. REPAIRED IAW SRM 53-00-01, REPAIR 2, FIG 201, TABLE V INSPECTION.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 66,062 hrs · 29,941 cycles

SHIP 674, MAINTENANCE DISCOVERED 1ST CLASS SEAT EMERGENCY LIGHT AT 1C HAS A BROKEN WIRE. REPAIRED SPLICE PER B757 SWPM 20-10. LIGHT STILL INOP. REPLACED CHARGER AND BATTERY PER B757 AMM 33-51. EMERGENCY LIGHTS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 64,657 hrs · 29,322 cycles

EXTERIOR EMERGENCY LIGHT AT DOOR 2R INOP. TROUBLESHOT AND REPAIRED 2R EXT EMERGENCY LIGHT IAW B757 WDM 31-51-13, OPS CHECKED GOOD IAW B757 AMM 33-51-06.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 64,657 hrs · 29,322 cycles

EXTERIOR EMERGENCY LIGHT AT DOOR 1R INOP. TROUBLESHOT AND REPAIRED EMERGENCY EXIT LIGHT IAW B757 WDM 33-51-13, OPS CHECKS GOOD IAW B757 AMM 33-51-06.

Part: DOOR FRAME — CRACKED (L2 DOOR) · airframe 64,657 hrs · 29,322 cycles

L-2 DOOR JAMB UPPER HINGE CUTOUT CRACKED IN RADIUS. REPAIRED IAW B757-200 SRM 52-10-02 REPAIR 1.

Part: DOOR FRAME — CRACKED (R2 DOOR) · airframe 64,657 hrs · 29,322 cycles

R-2 DOOR JAMB UPPER HINGE CUTOUT CRACKED IN RADIUS REPAIRED IAW B757-200 SRM 51-10-02 REPAIR 4.

Part: FRAME — DAMAGED (BS 1300 STR 1L) · airframe 64,657 hrs · 29,322 cycles

MAIN CABIN FRAME AT BS 1300 STRINGER 1L HAS MISDRILLED HOLES. REPAIRED IAW SRM 53-00-07 REPAIR 1.

Part: SKIN — DENTED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

EXTERNAL FUSELAGE SKIN TWO DENTS NEAR JUST FWD AND ABOVE OF REPAIR AT BS 1580. ACCOMPLISHED REPAIR PER ERA 489933-14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

MAIN CABIN FLOORBEAM HAS CORROSION BS 324, RBL. REPAIRED PER B757 SRM 53-00-51, REPAIR 3, FIG 201.

Part: INTERCOSTAL — DAMAGED (BS1500-1520) · airframe 64,657 hrs · 29,322 cycles

INTERCOSTAL FROM BS 1500 TO 1520 CORRODED AND FOUND CORRODED AND CRACKED. FABRICATED NEW INTERCOSTAL IAW DWG 146N5432 INSTALLED PER SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

INTERCOSTAL FROM 1500-1520 BL 5L CORRODED AND FOUND TO BE CRACKED. REPLACED PER B757-200 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

FLOORBEAM CORRODED STA 338 RBL 23-RBL 44. REPAIRED PER B757 SRM 53-00-51 ON N/R 42955, THIS REPAIR IS RE-WRITTEN FROM ORIGINAL N/R 43191.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

AFT PIT, LT SLOPE AT STA 1440 FRAME DENTED. REPAIRED STA 1440 FRAME, BETWEEN STRINGERS 26L AND 27L PER B757 SRM 53-00-07, REPAIR NR 5, DETAIL I.

Part: SKIN — DAMAGED (TE FLAP) · airframe 64,657 hrs · 29,322 cycles

RT INBD FLAP HAS A HOLE 1X1.5 ON THE LOWER SURFACE IN THE CENTER 3FT FROM INBD EDGE. TEMP REPAIRED. POST CURE INSPECTION FOUND DELAM AREA REQUIRING REPAIR. REF NR 502021-42019. REF C/N U10120210. REPAIRED RW I/B AFT FLAP I/B LOWER SURFACE BY BONDING SEPTUM CORE FILLER AND GRAPHITE PREPREG IAW B757 SRM 57-52-01 AND 51-70-05, FIG 2.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

KEEL BEAM AREA LEFT SIDE PANEL ATTACH STRUCTURE STA 960 TO STA 1000 HAS CORROSION AROUND FASTENER HOLES. CORROSION FOUND TO BE OUT OF LIMITS. REPLACED TEE IAW B757 SRM 51-40-02.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

AFT PIT RT SLOPE AT STA 1340 FRAME DENTED. REPAIRED STA 1340 FRAME BETWEEN STRINGERS S26R AND 27R PER B757 SRM 53-00-07 REPAIR NR 5, DETAIL I.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

AFT PIT, LEFT SLOPE AT STA 1480 FRAME DENTED. REPAIRED AFT PIT FRAME AT FS 1480 IAW B757 SRM 53-00-07 FIG 201.

Part: SUPPORT — WORN (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

RIGHT ESC BAY STA 900 BL12 TO BL40, STRUCTURE HAS AREAS OF BARE METAL. REPAIRED PER B757 SRM 51-40-02 AND SRM 51-70-12.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

AFT PIT LT SLOPE AREA AT STA 1500, FRAME DENTED. REPAIRED AFT PIT FRAME AT FS 1500 IAW B757 ARM 53-00-07, FIG 201.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

AFT PIT, LEFT SLOPE AT STA 1420 FRAME DENTED. REPAIRED AFT PIT FRAME AT FS 1420 IAW B757 SRM 53-00-07, FIG 201.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

MAIN CABIN FLOORBEAM HAS CORROSION NUMEROUS SPOTS BS 365, RBL1 - RBL 64. CORROSION OUT OF LIMITS. REPAIRED PER B757 SRM 53-00-51, FIG 201, REPAIR 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

MAIN CABIN FLOORBEAM CORROSION OUT OF LIMITS AS DOCUMENTED ON N/R 42955. REPAIRED ON N/R 43191 PER B757 SRM 53-00-51.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

AFT PIT LT SLOPE AREA AT STA 1520, FRAME DENTED. REPAIRED AFT PIT FRAME AT STATION 1520 IAW B757 SRM 53-00-07 FIG 201, 51-20-01 AND DETAIL I, REPAIR 5 OF SRM 53-00-07, FIG 201.

Part: SKIN — CRACKED (RT WING) · airframe 64,657 hrs · 29,322 cycles

CRACK INDICATION FOUND IN THE RIGHT LOWER WING SKIN AT THE DRAG FITTING AT WSTA 210.3 O/B HOLE COMMON TO THE LOWER CHORD OF THE REAR SPAR REF: NTM PART 4 57-25-01.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

DURING MAINTENANCE VISIT AN EXISTING SKIN REPAIR AT BS 550 STR 14-16 LT WAS FOUND TO HAVE FASTENER HOLES INTERSECTING A CHEM-MILLED STEP. REPAIRED BY EA 383903-14AD CLASSIFIED AS MAJOR REPAIR.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

DURING MAINTENANCE VISIT, AN EXISTING SKIN REPAIR AT BS 550 BETWEEN STR 14-16 LT WAS FOUND TO HAVE FASTENER HOLES INTERSECTING A CHEM-MIL STEP. REPAIRED PER ERA 383903-14 REV F.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

DURING MAINTENANCE VISIT AN EXISTING SKIN REPAIR AT BS 1360-1380 BETWEEN STR 21-23 LT WAS FOUND TO HAVE FASTENER HOLES INTERSECTING A CHEM-MIL STEP. REPAIRED PER ERA 493526-14 REV A.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

DURING MAINTENANCE VISIT AN EXISTING SKIN REPAIR AT BS 1360-1380 BETWEEN STR 21-23 LT WAS FOUND TO HAVE FASTENERS INTERSECTING A CHEM MILLED STEP. TO BE REPAIRED BY ERA 493526-14. AND N/R43141 ERA CLASSIFIED AS MAJOR REPAIR.

Part: FITTING — DAMAGED (NR 2 PYLON) · airframe 64,657 hrs · 29,322 cycles

NR 2 PYLON FWD SPAR TENSION CLIP P/N 012N8886-2 HOLE NR 1 JOB CARD 06-070332-03 0228 PANEL 2 STEP 6 REQUIRES SPOTFACE .8125 HOLE HAS MINIMUM EDGE DISTANCE. ITEM ADDRESSED ON N/R 43117 AND ER/A 489934-14.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

DISCOVERY - KEEL BEAM AREA LEFT SIDE PANEL ATTACH STRUCTURE STA 960 TO STA 1000 HAS CORROSION AROUND FASTENER HOLES. FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-40-12.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

DISCOVERY - FLOORBEAM AT STATIOIN 338 RBL 23 - RBL 44 CORRODED OUT OF LIMITS. TO BE REPAIRED IAW B757 SRM 53-00-51.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

DISCOVERY - WING TO BODY FAIRING SUPPORT ANGLE FS 900 RBL 10 TO LBL 16 CORRODED OUT OF LIMITS IAW B757 SRM 53-00-71 FIG 101 DETAIL IX. SUPPORT ANGLE WILL BE REPAIRED IAW B757-200 SRM 51-70-12 FIG 2 GENERAL-TYPICAL EXTRUDED SECTION REPAIR.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

DISCOVERY - INTERCOSTAL FROM STA 1500 TO 1520 BL5L CORRODED AND FOUND TO BE CRACKED. TO BE REPLACED IAW B757-200 SRM 51-40-02.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

DURING MAINTENANCE VISIT FRAME AT BS 1520 BETWEEN STRINGERS 26-27 LT WAS FOUND TO BE DENTED. (DAMAGE EXCEEDS ALLOWABLE LIMITS. IAW B757-200 SRM 53-00-07 FIG 101- NO DENTS ALLOWED IN FRAME FLANGE.) FRAME TO BE REPAIRED IAW B757-200 SRM 53-00-07 FIG 201 DETAIL I. CAUSE OF DEFECT WAS UNDETERMINED. DOCUMENTED ON NON-ROUTINE 42815.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

DURING MAINTENANCE VISIT FRAME AT BS 1420 BETWEEN STRINGERS 25 AND 27 LT WAS FOUND TO BE DENTED. (DAMAGE EXCEEDS ALLOWABLE LIMITS IAW B757-200 SRM 53-00-01 FIG 101. - NO DENTS ALLOWED IN FRAME FLANGE). FRAME TO BE REPAIRED IAW B757-200SRM 53-00-07 FIG 20A DETAIL III. CAUSE OF DEFECT WAS UNDETERMINED. DOCUMENTED ON NON-ROUTINE 42809.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

DURING MAINTENANCE VISIT FRAME AT BS 1440 BETWEEN STRINGERS 26 AND 27 LT WAS FOUND TO BE DENTED. (DAMAGE EXCEEDS ALLOWABLE LIMITS IAW B757-200 SRM 53-00-07 FIG 101. - NO DENTS ALLOWED IN FRAME FLANGE.) FRAME TO BE REPAIRED IAW B757-200 SRM 53-00-01 FIG 201 DETAIL I. CAUSE OF DEFECT WAS UNDETERMINED. DOCUMENTED ON N/R 42810.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

DURING MAINTENANCE VISIT FRAME AT BS 1480 BETWEEN STRINGERS S5-27 LT WAS FOUND TO BE DENTED. (DAMAGE EXCEEDS ALLOWABLE LIMITS IAW B757-200 SRM 53-00-07 FIG 101. NO DENTS ALLOWED IN FRAME FLANGE) FRAME TO BE REPAIRED IAW B757-200 SRM FIG 201 DETAIL I. CAUSE OF DEFECT WAS UNDETERMINED. DOCUMENTED ON N/R 42811.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

DURING MAINTENANCE VISIT FRAME AT BS 1340 BETWEEN STRINGERS 26R AND S7R WAS FOUND TO BE DENTED. DAMAGE EXCEEDS ALLOWABLE LIMITS IAW B757-200 SRM 53-00-07 FIG 101 - NO DENTS ALLOWED IN FRAME FLANGE. FRAME TO BE REPAIRED IAW B757 SRM 53-00-01 FIGURE 201 DETAIL I. CAUSE OF DEFECT WAS UNDETERMINED. DOCUMENTED ON NON-ROUTINE 42806. 53-00-07 FIG 101.

Part: FRAME — DENTED (FUSELAGE) · airframe 64,657 hrs · 29,322 cycles

DURING MAINTENANCE VISIT FRAME AT BS 1500 BETWEEN STRINGERS 26 AND 27 LT WAS FOUND TO BE DENTED. DAMAGE EXCEEDS ALLOWABLE LIMITS IAW B757 SRM 53-00-07 FIG 101. NO DENTS ALLOWED IN FRAME FLANGE. FRAME TO BE REPAIRED IAW B757-200 SRM 53-00-07 FIGURE 201 DETAIL I. CAUSE OF DEFECT WAS UNDETERMINED. DOCUMENTED ON NON-ROUTINE 42814.

Part: WIRE — DAMAGED (CABIN) · airframe 63,663 hrs · 28,911 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY PATHLIGHTS AT SEATS 29, 31, AND 34 INOPERATIVE. MAINTENANCE REPAIRED THE WIRING AT EACH LOCATION. OPERATIONAL CHECKS WERE GOOD.

Part: TIRE — BLOWN (NR 6) · airframe 62,745 hrs · 28,592 cycles

IN LAX FOUND NR 6 TIRE BLOWN CAUSING DENT TO FUSELAGE AT STA 1365 BETWEEN STR 23L AND 24L. DAMAGE WAS REPAIRED PER ERA 493526-14. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,573 hrs · 28,080 cycles

DURING A LAYOVER CHECK, MX FOUND THE FIRST CLASS EMERGENCY PATH LIGHTS INOPERATIVE. MX REPLACED THE BATTERY CHARGER FUSE. OPS CHECK WAS GOOD.

Part: LIGHT — INOPERATIVE (SEAT 33D) · airframe 59,629 hrs · 27,169 cycles

DURING LAYOVER CHECK, MX FOUND EMERGENCY PATH LIGHTS AT 33D AND THE AFT RT LAV INOPERATIVE. MX REPLACED THE LIGHT ASSY AT 33D AND REPAIRED THE WIRING AT THE AFT RT LAV. OPS CHECK WAS GOOD.

Part: FAN — INOPERATIVE (NR 1) · airframe 52,516 hrs · 23,746 cycles

RECIEVED EQUIP OVERHEAT EICAS MSG IN FLT SMELLED SMOKE HEARD EQUIP FAN C/B POP. FOUND FAN 1 INOP REPLACED NR 1 FWD EQUIPMENT COOLING SUPPLY, CLEARED MSG CKS GOOD.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 52,380 hrs · 23,670 cycles

LT ELEVATOR UPPER AND LOWER SKIN TRAILING EDGE REPAIRED IAW ERA 452271-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 52,380 hrs · 23,670 cycles

FUSELAGE SKIN FS 600 STR 16L REPAIRED IAW ERA 452191-14.

Part: SPAR — CRACKED (NR 2 PYLON) · airframe 52,380 hrs · 23,670 cycles

NR 2 PYLON FWD UPPER SPAR CHORD CRACK REPAIRED IAW ERA 452272-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 52,380 hrs · 23,670 cycles

FUSELAGE SKIN STA 199-223.5, RBL & LBL 14.10 REPAIRED IAW ERA 452570-14.

Part: SKIN — UNKNOWN (FUSELAGE) · airframe 52,380 hrs · 23,670 cycles

FUSELAGE SKIN STA 1350 REMOVAL OF SKY RADIO ANTENNA IAW ERA 452276-14.

Part: TRANSMITTER — FAULTED (NR 2 ENGINE) · airframe 50,463 hrs · 22,781 cycles

THE RT ENG HAD LOW OIL PRESSURE AND FOLLOWED THE THROTTLE MOVEMENT. ENG T/S TEAM FOUND THE NR 2 ENG OIL PRESS TRANSMITTER TO BE AT FAULT. REPLACED SAME.

Part: ENGINE — FAILED (NR 1) · airframe 49,625 hrs · 22,486 cycles

WINDING UP FOR T/O HEARD AUDIBLE ENGINE SURGE/STALL PASSENGERS OBSERVED FLAMES COMING FROM LEFT ENGINE. A/C RETURNED TO GATE. MTC INSPECTED TAIL PIPE FOUND BB SIZED DEBRIS. WILL NEED ENGINE CHANGE. REPLACED NR 1 ENG PER ROUTINE CARD DECK TRANS 6T103.

Part: COFFEEMAKER — ODOR (MID GALLEY) · airframe 49,094 hrs · 22,242 cycles

FLT ATT COMPLAIN OF BURNING SMELL FROM MID GALLEY COFFEE POTS. TURNED ON COFFEE MAKERS AND OVENS FOR 30 MIN. NO SIGNS OF BURNING SMELL OK FOR SERVICE.

Part: ODOR — DETECTED (CABIN) · airframe 46,068 hrs · 21,191 cycles

BRIEF ELECTRICAL BURNING SMELL NOTED BY FLT ATTENDANT AND PASSENGERS APPROX ROWS 28-32. DURING FLIGHT SMELL DISSIPATED THEN RETURNED ON DESCENT. MTC IN SJO OPENED AND CHECKED ALL PSU FROM ROW 20-39, FOUND NORMAL CONDITIONS. OPERATED BOTH A/C PACKS AND RECIRCULATION FANS WITH DOORS CLOSED FOR ONE HOUR, NO SMELL DETECTED. RAN BOTH ENGINES AND OPERATED ALL CABIN ELECTRICAL SYSTEMS COULD NOT DUPLICATE SMELL.

Part: SLIDE — FAULTY (R1 DOOR) · airframe 39,853 hrs · 18,978 cycles

THE 1R DOOR SLIDE LIGHT REMAINS ILLUMINATED AFTER SLIDE IS IN DISARMED POSITION. SLIDE DID NOT DEPLOY PROPERLY. REPLACED SLIDE, ASSIST BOTTLE, FWD PROX SWITCH AND FWD GIRT BAR FOOT.

Part: INVERTER — UNSERVICEABLE (FWD E/E) · airframe 38,858 hrs · 18,565 cycles

ELECTICAL TYPE FUMES AND HAZE THROUGHOUT CABIN AFTER TAKE OFF. REMOVED STATIC INVERTER (2 CB PULLED 6D10 6L11) RESET CB'S AND REPLACED STATIC INVERTER PERFORMED EQ. COOLING BITE TEST, ALL INDICATIONS NORMAL.

Part: SKIN — DENTED (FS 540, S-15L) · airframe 36,219 hrs · 17,416 cycles

FUSELAGE / SKIN ASSY / FS 520-550 / STRG. 14L-16L : GROUND DAMAGE REPAIR THE FUSELAGE WAS STRUCK BY GROUND EQUIPMENT RESULTING IN A LARGE DENTED AREA BETWEEN FS 520 & 550 FROM STRINGER 14L TO 16L. THE SKIN DAMAGE WAS REMOVED WITH A 30" X 10" CUTOUT. THE UNDERLYING STRINGERS WERE REPAIRED PER THE B757 SRM. THE SKIN CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 383903-14, REV A.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 35,023 hrs · 16,824 cycles

ON LAYOVER FOUND AFT EMERGENCY LIGHTS INOP. REPLACED BATTERY CHARGER AND BATTERY OPS CHECK GOOD.

Part: FITTING — BROKEN (RT MLG) · airframe 31,045 hrs · 14,883 cycles

LOST LEFT HYDRAULIC SYSTEM ON LANDING. FOUND PRESSURE LINE ON TOP OF RT MLG RETRACT CYL FITTING BROKEN OFF. REPLACED FITTING AND REINSTALLED HYD LINE, LEAK CHECKS GOOD. REPLACED LT ACMP CASE DRAIN AND LT EDP CASE DRAIN FILTERS, LEAK CHECKS GOOD.

Part: SMOKE — DETECTED (CABIN) · airframe 28,162 hrs · 13,571 cycles

ELECTRICAL SMOKE BURNING SMELL AROUND ROWS 20 TO 23. PER FLT CREW REQUEST CHECKED ALL OVENS, COFFEEMAKERS, OVERHEAD PANELS AND LIGHT BALLASTS IN ROWS 20 - 26. OPERATED VIDEO SYS, RAN PACKS RAN BOTH ENGINES. CHECKED FWD CARGO AND A/C DISTRIBUTION AREA. NO DISCREPANCIES NOTED. UNABLE TO DUPLICATE.

Part: RIB — DAMAGED (LE SLAT)

DURING B757 L/E SLAT T/E WEDGE CHANGE PER EO 6-74595-3AD, THE NR 10 L/E SLAT I/B END RIB HAD ONE HOLE OVERSIZED IN THE I/B END RIB AT OSS 707. PER ER/A 387211-14AD THE SUBJECT PART WAS REPAIRED BY OVERSIZING THE DISCREPANT HOLE TO ACCOMODATE A .25 DIA BLIND BOLT.

Part: OIL LINE — CRACKED (NR 2 ENGINE)

THE MAIN OIL BEARING MANIFOLD SCAVENGE LINE CRACKED AT AN ELBOW WHERE IT GOES INTO THE TOWER SHAFT, MFG NR 1A821101. REPLACED LINE.

Part: BULB — FAILED (CABIN)

EMERGENCY TRACK LIGHT AT ROW 34 INOP DURING MAINTENANCE TEST. RELAMPED AND INSTALLED A NEW LENS, OPERATION NOW NORMAL.

Part: BULB — FAILED (CABIN)

EMERGENCY TRACK LIGHT AT ROW 39 INOP DURING MAINTENANCE TEST. RELAMPED AND OPERATIONAL CHECK NORMAL.

Part: COFFEE MAKER — SMOKING (CABIN)

ELECTRICAL SMOKE CAME OUT OF NR 1 F/C COFFEE MAKER. C/B PULLED TO STOP SMOKE. REPLACED DISPENSER, OPN NML.

Part: RADOME — DAMAGED (FWD FUS)

UPON INSPECTION RADOME (DL 13) WAS FOUND TO EXCEED MOISTURE LIMITS AT TOP AND RIGHT SIDES CONTAINING AN AREA OF 20 PERCENT OF RADOME SURFACE. ACCOMPLISHED REPAIRS PER SRM 53-10-72.