N543US

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,158 hrs · 31,724 cycles

SHIP 5643 DENT ON RIGHT WING PANEL 611DB. CORRECTIVE ACTION: REF ERA 614118-14. (5086408)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,565 hrs · 31,437 cycles

SHIP 5643 -MISC/DE- CREW DECLARED EMERGENCY DUE TO TE FLAP ASYM ON APPROACH. CORRECTIVE ACTION: SECURED LOOSE CONNECTOR ON FLAP POWER DRIVE UNIT.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,514 hrs · 31,412 cycles

SHIP 5643 EXIT SING AT DOOR L2 FELL OFF. CORRECTIVE ACTION: RE SECURED EMERGENCY EXIT LIGHT COVER PER B757 AMM 33-51. NO FAULTS NOTED AT THIS TIME. (4906888)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,501 hrs · 31,405 cycles

SHIP 5643 AFTER INSPECTION OF L-1 DOOR, ROTARY SNUBBER FOUND TO BE OUT OF LIMITS. CORRECTIVE ACTION: SUMMARY OF NRC:00056- REMOVED AND REPLACED L1 DOOR SNUBBER IAW B757 AMM 52-11-10. (2954289)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,501 hrs · 31,405 cycles

SHIP 5643 RH ENG DRAG FTG CLAMP-UP HOLE #12 HAS GOUGES AND CORROSION NOTED IN SKIN LOCATED AT 7 AND 9 O'CLOCK POSITION. CORRECTIVE ACTION: REAMED HOLE #12 IN THE SKIN CONCENTRICALLY UP TO 0.06557" AND C/ W HFEC OPEN HOLE INSPECTION NO DEFECTS NOTED, ASSET#'S 21511,17459,23968, FABRICATED INSTALLED, REAMED FREEZE PLUG AND INSTALLED NEW FASTENER AT HOLE IAW ER/A 582596-14AD REV C. (2946345)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,501 hrs · 31,405 cycles

SHIP 5643 R-4 PASSENGER DOOR, ROTARY SNUBBER FOUND TO BE OUT OF LIMITS. CORRECTIVE ACTION: REMOVED AND INSTALLED R4 DOOR ROTARY SNUBBER IAW B757 AMM 52-11. (2923005)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,374 hrs · 31,340 cycles

SHIP 5643 -SMKE/FUME- CREW REPORTED BRIEF AND QUICKLY DISSIPATING SMOKE AND ELECTRICAL ODOR IN FLIGHT DECK AFTER LANDING. CREW OXYGEN MASKS DONNED. NO ODOR OR VISIBLE ACCUMULATION IN PASSENGER CABIN. CORRECTIVE ACTION: T/S NO SMOKE SMELL PRESENT, MTC C/W MCC NO GO LOG. DOOR 2 HEATER DEFERRED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,883 hrs · 31,106 cycles

SHIP 5643 R1 DOOR DIFFICULT TO CLOSE FROM THE OUTSIDE OF THE A/C. CORRECTIVE ACTION: FOUND DOOR TO NOT BE SITTING FLUSH WITH A/C. REMAINS CRACKED OPEN. PER MCC REQUEST, INSPECT DOOR LINKAGES, SEALS ETC. REF B757 AMM 52- 11. REMOVED ESCAPE SLIDE RAFT COVER PER B757 AMM 52-11. ADJUSTED DOOR, R1, AS PER B757 AMM 52-11, OPS CK GOOD. STOWED SLIDE PIN AND INSTALLED SLIDE COVER PER B757 AMM 52-11. (2747115)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,883 hrs · 31,106 cycles

SHIP 5643 1 RIGHT DOOR IS BROKEN AND WOULD NOT CLOSE. CORRECTIVE ACTION: PERFORMED OPS CHECK OF 1R DOOR. CHECK OK.REF B757 AMM 52-11. (4193226)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,696 hrs · 31,006 cycles

SHIP 5643 -DIV- TO JFK DUE TO WEATHER RADAR WITH STORMY WEATHER ENROUTE. CORRECTIVE ACTION: R/R WEATHER RADAR ANTENNA DRIVE UNIT AND TRANSCEIVER.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,646 hrs · 30,989 cycles

SHIP 5643 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS****L3 SLIDE LIGHT INOP. CORRECTIVE ACTION: EXAMINED GIRT BAR LOCK PER B757 AMM 25-66. LIGHT OPS NML. (2676529)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,638 hrs · 30,985 cycles

SHIP 5643 DOOR 4L UPPER FORWARD CM FOLLOWER BEARING BROKEN. CORRECTIVE ACTION: REMOVE AND REPLACE THE FWD UPPER LATCH CAM ROLLER B757 AMM 52-11 -00. ADJ. AND OPS CH. GD. (9462370)

Part: NONE — NONE · airframe 82,439 hrs · 30,878 cycles

SHIP 5643 R FWD ENTRY DOOR WOULD NOT ARM OR CLOSE COMPLETELY. CORRECTIVE ACTION: OPENED & RE-CLOSED R1 DOOR ARMED & OPS CHECK GOOD REF B757 AMM 52-00. (9558990)

Part: UNKNOWN — UNKNOWN · airframe 82,365 hrs · 30,846 cycles

SHIP 5643 DURING SVC FOUND MULTIPLE EMERGENCY LIGHTS INOP - EPATH SEATS 43 -45 DEF, 3R UPPER INTERIOR SIGN, 3L LOWER INTERIOR SIGN, 3R EXTERIOR EMER. LIGHT. CORRECTIVE ACTION: T/S PER B757-200 SSM 33-51. FOUND ALL LIGHTS ASSOCIATED WITH BATTERY PACK M736 INOP, INSTALLED POWER SUPPLY PER B757 AMM 33-51. TEST OK. (9558943)

Part: NONE — NONE (NONE) · airframe 82,006 hrs · 30,660 cycles

COMPLY WITH ERA 604561-14AD REV. ORIGINAL. COMPLIED WITH ERA 604561-14AD REV ORIGINAL.

Part: NONE — NONE · airframe 81,483 hrs · 30,437 cycles

SHIP 5643 1R DOOR DOES NOT CLOSE PROPERLY. CORRECTIVE ACTOIN: CYCLED 1R DOOR, DOOR OPS NML. (9171718)

Part: COVER — BROKEN · airframe 80,544 hrs · 30,107 cycles

SHIP 5643 EMERGENCY EXIT COVER KNOCKED OFF BY PAX BAG. CORRECTIVE ACTION: REATTACHED COVER. CHECKS OK. (2290539)

Part: HANDLE — OUT OF ADJUST · airframe 80,412 hrs · 30,071 cycles

SHIP 5643 2L DOOR NOT CLOSING PROPERLY & GUST LOCK RELEASE NOT LATCHING. CORRECTIVE ACTION: FOUND EXTERIOR HANDLE OUT OF SEQUENCE. CYCLED & ALL CKS WELL. EXERCISED GUST LOCK & NOW OPS NORMAL ALSO. OK FOR CONT. SVC. REF B757 AMM 52-11. (9279732)

Part: NONE — NONE · airframe 80,204 hrs · 30,016 cycles

SHIP 5643 DURING SVC CHK FOUND LAMP INOP AT 16D CEILING PANEL. CORRECTIVE ACTION: REMOVED AND REPLACED EMERGENCY LIGHT CAP ASSY BY SEAT 16C/D PER B757 AMM 33-51. CHECKS GOOD. (8768633)

Part: NONE — NONE · airframe 78,123 hrs · 29,436 cycles

SHIP 5643 ON WAKE UP FOUND - SQUIB TEST 2 - EMERGENCY ESCAPE LEFT BOTTLE PRESS TEST FAIL. CORRECTIVE ACTION: T/S PER FIM TASK 25-65. R/R RELAY K10486 AND NO HELP ALSO SWAPPED SQUIB TEST PANEL - REINSTALLED OLD TEST PANEL. R/R OVER WING EMERGENCY ESCAPE SLIDE INFLATOR PER AMDS CARD# OPS CHECK GOOD LEFT OFF WING SLIDE BOTTLE INSTALLED PER JIC. (7830070)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,959 hrs · 29,385 cycles

SHIP 5643 ROW 23-26 EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: R/R BATTERY PACK M10507 IAW B757 AMM 33-51. OPS CHK NML. (7830001)

Part: WEDGE — DEBONDED (NR 3 SLAT) · airframe 77,909 hrs · 29,366 cycles

SHIP 5643 HE #3 SLAT T/E WEDGE LWR SURFACE HAS AN AREA THAT HAS AN INDICATION OF DISBOND NOTED. CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR ON #3 SLAT T/E WEDGE IAW BOEING S.B. 757-57-0066, B757-200 SRM. SLAT REMOVED AND INSTALLED ON AMDS W/C. (1933049)

Part: UNKNOWN — UNKNOWN · airframe 81,106 hrs · 30,316 cycles

SHIP 5643 DTA MONITOR INSPECTION LOG REF ERA 593624-14 REV. B. CORRECTIVE ACTION: REF ERA 593624-14 REV B. (1932962)

Part: SKIN — DENTED (FUSELAGE) · airframe 77,909 hrs · 29,366 cycles

SHIP 5643 DTA MONITOR INSPECTION LOG REF ERA 593633-14 REV. B. , SEVERAL DENTS (5EA) WERE FOUND ON EXTERNAL SKIN. CORRECTIVE ACTION: REF ERA 593633-14 REV B AND REF 593560-14. (1932028)

Part: FRAME — CRACKED (BS 1640 S14R) · airframe 77,909 hrs · 29,366 cycles

SHIP 5643 BS 1640 FUSELAGE FRAME R/H SIDE LOWER I/B FASTENER HOLE AT S-14R HAS CRACK INDICATION AT THE 3 OCLOCK POSITION (I/B SIDE OF FASTENER HOLE VIEWED FROM THE FWD SIDE OF FRAME LOOKING AFT) LAYERS NEED TO BE SEPARATED (INTERCOSTAL TEE CLIP FRAME WEB & LOWER HINGE FITTING FOR FURTHER NDT EVALUATION. CORRECTIVE ACTION: REPAIRED STA 1640 R/H FRAME LOWER I/B HOLE @ S-14R IAW ERA 593495-14AD REV ORIG. (1930783)

Part: SKIN — DENTED (BS 760-780 S4L-R) · airframe 77,909 hrs · 29,366 cycles

SHIP 5643 FUSELAGE SKIN UPPER CROWN HAS 5 EACH LOCATIONS WITH DENTS AND REQUIRES REPAIRS STA 760-780 S-4R TO S-4L. CORRECTIVE ACTION: REPAIRED UPPER FUSELAGE SKIN FROM STA 760 TO 780 STR 4L TO STR 4R IAW ERA # 593633-14 REV ORIGINAL. (1929442)

Part: SKIN — DENTED (BS 740-760 S4-6R) · airframe 77,909 hrs · 29,366 cycles

SHIP 5643 DENT FOUND AT STA 740-760 S-4R TO S-6R AND REQUIRES REPAIR. CORRECTIVE ACTION: REPAIRED UPPER FUSELAGE SKIN FROM STA 740 - 780 STR 4 R TO STR 6R IAW ERA # 593624-14 REV A. (1929431)

Part: SKIN — DENTED (BS 740-760 S4-6L) · airframe 77,909 hrs · 29,366 cycles

SHIP 5643 DENT FOUND AT STA 740-760 S-4L TO S6L AND REQUIRES REPAIR. CORRECTIVE ACTION: REPAIRED UPPER FUSELAGE SKIN STA 740-760 S-4L TO S5L IAW ERA # 593626-14 REV A. (1929545)

Part: NONE — NONE · airframe 79,113 hrs · 29,720 cycles

SHIP 5643 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 582596-14 REV A. CORRECTIVE ACTION: REF ERA 582596-14AD REV A. (1754150)

Part: SKIN — DAMAGED (RT WING) · airframe 77,909 hrs · 29,366 cycles

SHIP 5643 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 582596-14 REV A. CORRECTIVE ACTION: REF ERA 582596-14AD REV B. (1754160)

Part: COUPLING — DISCONNECTED (ADC) · airframe 73,911 hrs · 28,318 cycles

SHIP 5643 -ATB- ON TAKE OFF F/O SIDE AIRSPEED SLOWLY WENT TO ZERO ALTIMETER FROZE AT ABOUT 1100', WENT THROUGH QRH PROCEDURE AND BROUGHT BACK F/O A/S & ALT W/ AIR DATA SWITCH. SEVERAL EICAS MSGS MACH/SPD TRIM AND RUDDER RATIO DID NOT CLEAR. CORRECTIVE ACTION: FOUND RIGHT ADC STATIC LINE COUPLING DISCONNECTED, REINSTALLED PERFORMED ADC TEST PER AMM SYSTEMS CHECKS GOOD.

Part: D-RING — OUT OF POSITION (EVAC SLIDE) · airframe 73,935 hrs · 28,324 cycles

SHIP 5643 ON SVC CHK R1 SLIDE D-RING NOT VISIBLE FOR SURVIVAL KIT. CORRECTIVE ACTION:REMOVED SLIDE COVER AND PINNED R-1 SLIDE. FOUND D-RING INCORRECT ROUTING. AS A PRECAUTION REMOVED AND REPLACED R-1 SLIDE PER AMDS WORK CARD. (7192774)

Part: DOOR — CONTAMINATED (R1) · airframe 73,646 hrs · 28,250 cycles

(AIRCRAFT 5643, L/P 6381424) DOOR 1R WILL NOT ARM. CORRECTIVE ACTION: OPENED DOOR AND CK FOR DEBRIS. NOTED WATER DRAINING FROM DOOR. CLOSED AND ARMED SLIDE. OPS NORMAL.

Part: TRACK — FOD (PAX DOOR) · airframe 73,360 hrs · 28,179 cycles

RT FWD ENTRY DOOR WILL NOT DISARM. DISARM LEVER NOT FULLY TO LEFT. CLEANED DEBRI FROM TRACK AREA.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 72,838 hrs · 28,039 cycles

(AIRCRAFT 5643, L/P 6157781) 2L EMERGENCY EXIT SIGN FELL OFF WHEN DOOR OPENED. CORRECTIVE ACTION: REINSTALLED EXIT ROW SIGN.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,803 hrs · 28,028 cycles

EMERGENCY EXIT SIGNS INOPERATIVE, REPLACED THE EXIT SIGN IAW 33-51. OK FOR SERVICE.

Part: WINDSHIELD — ARCED (LEFT) · airframe 72,795 hrs · 28,026 cycles

ENROUTE NOTICED A BRIGHT ORANGE ELECTRICAL ARC IN CAPTAINS LOWER RIGHT FWD WINDOW. ACCOMPLISHED NNC TURNED L FWD HEAT OFF. R & R 1 LEFT WINDSHIED IAW AMM 56-11-01. THIRD TORQUE COMPLETED.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 72,795 hrs · 28,026 cycles

(AIRCRAFT 5643, L/P 6157756) EMERGENCY EXIT LIGHT LENSE OVER L2 DOOR CAME OFF. CORRECTIVE ACTION: RESECURED LENSE.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 72,795 hrs · 28,026 cycles

EMERGENCY SIGN OVER THE L2 DOOR FELL DOWN. ADJUSTED EMERGENCY EXIT SIGN AND RESECURED.

Part: SENSOR — OUT OF ADJUST (AFT PAX DOOR) · airframe 72,787 hrs · 28,024 cycles

LEFT AFT ENTRY DOOR LIGHT ILLUMINATED ON THE GROUND. ADJUSTED LEFT AFT ENTRY DOOR SENSOR, PERFORMED OPERATIONAL CHECK, OPS CHECKED GOOD.

Part: FRAME — DAMAGED (BS 395 BULKHEAD) · airframe 72,776 hrs · 28,018 cycles

SHIP 5643 HARD LANDING STA 395 BULKHEAD L/H CHORD REPAIR ESR 006. CORRECTIVE ACTION: REPAIRED L/H CHORD STA 395 IAW DELTA ER/A 582392-14 REV. 0 MONITOR INSPECTION LOG 1371499. (1379032)

Part: FUEL SYS — LEAKING (LT WING) · airframe 72,776 hrs · 28,018 cycles

(AIRCRAFT 5643, L/P 1379019) LEFT WING INTERNAL DRY BAY IS LEAKING FUEL OUT OF "WEEP" HOLE. CORRECTIVE ACTION: REPAIRED IAW ERA 583350-14.

Part: FUEL CELL — LEAKING (RT WING) · airframe 72,776 hrs · 28,018 cycles

SHIP 5643 RIGHT WING HAS FUEL LEAKING OUT OF DRY BAY "WEEP" HOLE. CORRECTIVE ACTION: REPAIRED R/W DRY BAY BETWEEN STA 285 & 313 IAW ER/A 583355-14 REV. ORIG. (1379026)

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 72,776 hrs · 28,018 cycles

EMERGENCY TRACK LIGHTING INOPERATIVE, BS 388 TO 680 L&R. CONNECTED THE CONNECTORS IAW AMDS CARD 2525-0062.

Part: BARRIER — DAMAGED (RT WING) · airframe 77,909 hrs · 29,366 cycles

SHIP 5643 SECTION I REPAIR TO RH WING DRY BAY FUEL BARRIER REQUIRES SECTION II REPAIR WITHIN 24 MONTHS. CORRECTIVE ACTION: REF ERA 583355 REV A. (1377981)

Part: BARRIER — DAMAGED (LT WING) · airframe 77,909 hrs · 29,366 cycles

SHIP 5643 SECTION I REPAIR ERA 583350-14 REV ORIG TO LH WING DRY BAY FUEL BARRIER REQUIRES SECTION II REPAIR. CORRECTIVE ACTION: REF ERA 583350-14. (1377990)

Part: FRAME — DAMAGED (BS 395 BULKHEAD) · airframe 72,773 hrs · 28,014 cycles

(AIRCRAFT 5643, L/P 1377015) HARD LANDING STA 395 BULKHEAD R/H CHORD REPAIR. CORRECTIVE ACTION: REPAIRED STA 395 BULKHEAD R/H CHORD IAW ERA 582391-14 REV ORIGINAL.

Part: STRINGER SPLICE — CRACKED (BS 1620) · airframe 72,776 hrs · 28,018 cycles

AFT CARGO STRINGER 20R SPLICE AT BS 1620 IS CRACKED. CORRECTIVE ACTION: REMOVED, FABRICATED AND INSTALLED NEW AFT CARGO BS 1620 STRINGER 20R SPLICE IAW SRM 51-40-02 AND DWG 146N3821 REV P.

Part: TUNNEL WALL — CRACKED (BS 1620) · corrosion level 2 · airframe 72,776 hrs · 28,018 cycles

AFT CARGO RT SIDE TUNNEL POSSIBLE CRACK AND HAS CORROSION UNDER STRINGER STA 1620 S20R. CORRECTIVE ACTION: CUT OUT DAMAGED SECTION OF STR 20R AND REPAIRED STRINGER SECTION IAW SRM 53-00-03-2R PROCEDURE 1 REPAIR 1.

Part: SHEAR TIE — CORRODED (BS 720) · corrosion level 2 · airframe 72,773 hrs · 28,014 cycles

(AIRCRAFT 5643, L/P 1371985) FWD CARGO BS720 SHEAR TIE CORRODED INB OF S-27L UNDER TRANSITION PANEL. CORRECTIVE ACTION: REMOVED CORROSION AT FWD CARGO BS 770 SHEAR TIE STR 27L IAW B757 SRM 51-10-02. REMOVED, FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: SKIN — NOT REPORTED (BS 395) · airframe 72,773 hrs · 28,014 cycles

(AIRCRAFT 5643, L/P 1371379) FUSELAGE SKIN STA 395 STR 18R TO 17R PERMANENT REPAIR. CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR AT FUSELAGE SKIN STA 395 STR CUT OUT IAW DELTA ERA 582140-14 REV ORIGINAL SECTION 1.

Part: SKIN — CRACKED (RT WING) · airframe 72,773 hrs · 28,014 cycles

(AIRCRAFT 5643, L/P 1371509) FASTENER #2 HAS CRACK INDICATIONS IN UPPER SKIN 4 OCLOCK AND 10 OCLOCK POSITIONS LOOKING AFT. CORRECTIVE ACTION: REPAIRED RIGHT WING FWD DRAG FITTING #2 HOLE IAW ER/A # 582596-14 AD.

Part: SKIN — DAMAGED (BS 1520-1540) · airframe 72,773 hrs · 28,014 cycles

(AIRCRAFT 5643, L/P 1371258) 2 DEEP BLEND OUTS AROUND FASTENERS ON EXTERNAL FUSELAGE SKIN BTWN STA 1520-1540 ON STR 27R. CORRECTIVE ACTION: REPAIRED AREA IAW B757 SRM 53-00-01 REPAIR 28 INSPECTION THRESHOLD 25,000 FLIGHT CYCLES. REPEAT INTERVALS 6,000 FLIGHT CYCLES HFEC AND EXTERNAL DETAILED VISUAL NDT PT6 51-00-01.

Part: SKIN — DENTED (BS 460) · airframe 72,773 hrs · 28,014 cycles

(AIRCRAFT 5643, L/P 1369948) LOCATED DENT AT FUSELAGE SKIN STA 460, STR 22R - 23R. CORRECTIVE ACTION: DENT OUT OF LIMITS PER B757 SRM 53-00-01. REMOVED DAMAGE, FABRICATED FILLER , DOUBLER, TRIPLER, ALODINED AND REPAIR PARTS. INSTALLED REPAIR PARTS. SEALED AFFECTED AREAS, ALL IAW B757-SRM-53-00-01 REPAIR 29, SRM 51-20-01 AND SRM 51-20-05.

Part: SKIN — DENTED (BS 690) · airframe 72,773 hrs · 28,014 cycles

(AIRCRAFT 5643, L/P 1368823) LOCATED DENT AT FUSELAGE SKIN STA 690 STR 23L-24L. CORRECTIVE ACTION: CUT OUT DAMAGED AREA AND REPAIRED AREA IAW B757 SRM 53-00-01 REPAIR 28 FIGURE 201 THIS IS A CATEGORY B REPAIR AND REQUIRES SUPPLEMENTAL INSPECTIONS AS GIVEN IN B757 SRM 53-00-01 REPAIR 28 TABLE 206 STARTING AT 37,500 FLIGHT CYCLES AND EVERY 6,000 CYCLES THEREAFTER BY HFEC AND DETAILED VISUAL INSPECTION.

Part: SKIN — DENTED (BS 1600-1620) · airframe 72,773 hrs · 28,014 cycles

(AIRCRAFT 5643, L/P 1368752) LOCATED 3 DENTS ON EXTERNAL SKIN REPAIR BTWN STA 1600-1620 APPROX STR 17L. CORRECTIVE ACTION: REMOVED DAMAGED FUSELAGE SKIN REPAIR DOUBLER STA 1600 TO 1620 STR 17L IAW B757 SRM 51-40-02. FABRICATED AND INSTALLED NEW REPAIR DOUBLER IAW EA 582946-14 REV O.

Part: SEAT TRACK — GOUGED (BS 1358-1512) · airframe 72,773 hrs · 28,014 cycles

(AIRCRAFT 5643, L/P 1368391) MAIN CABIN L/H OUTBOARD SEAT TRACK IS GOUGED OUT OF LIMITS AT STA 1358 AND STA 1512. CORRECTIVE ACTION: REMOVED FLOOR PNLS IN MAIN CABIN L/H SIDE, O/B SEAT TRACK, I/B AND O/B SIDE BTWN STA 1320-1540 FOR ACCESS TO PERFORM A REPAIR, REMOVED MAIN CABIN L/H SIDE O/B SEAT TRACK, PERFORMED A MATERIAL VERIFICATION FOR REPAIR, FABRICATED NEW PARTS, CUT OUT DAMAGED SEAT TRACK FOR NEW PARTS, LOCATED AND DRILLED NEW PARTS, TREATED AND PRIMED NEW PARTS, APPLIED TOP COAT ON NEW PARTS, INSTALLED PARTS, AND NEW ANGLES, REINSTALLED FLOOR PNLS IN MAIN CABIN L/H SIDE, O/B SEAT TRACK, I/B AND O/B SIDE BTWN STA 1320-1540, IAW B757 SRM 51-40-02 SRM 53-00-52 REPAIR 1, SRM 51-20-01 AND AMM 51-21-00.

Part: SHEAR TIE — DAMAGED (BS 377) · airframe 72,773 hrs · 28,014 cycles

(AIRCRAFT 5643, L/P 1363263) HARD LANDING DAMAGE FRAME AND SHEAR TIE STA 377 STR 23L. CORRECTIVE ACTION: REMOVED, FABRICATED AND INSTALLED NEW FRAME SECTION AT STA 377 L/H IAW DRW# 141N1220 REV - AND SHEAR TIE AT STA 377 STR 23L IAW DRW# 141N1220 REV - . PARTS HEAT TREATED IAW AMS 2770.

Part: SEAT TRACK — CORRODED (BS 680-730) · corrosion level 2 · airframe 72,773 hrs · 28,014 cycles

(AIRCRAFT 5643, L/P 1363071) THERE IS CORROSION IN MID CABIN AREA STARTING AT STA 680 ON L/H SIDE OF RBL 24 SEAT TRACK ENDING AT STA 730. CORRECTIVE ACTION: REMOVED FABRICATED AND INSTALLED NEW SEAT TRACK IAW B757 SRM 51-40-05 AND B757 SRM 51-40-02.

Part: SKIN — DENTED (BS 500) · airframe 72,773 hrs · 28,014 cycles

(AIRCRAFT 5643, L/P 1358130) LOCATED DENT AT FUSELAGE SKIN STA 500, STR 23R-24R. CORRECTIVE ACTION: FABRICATED REPAIR DOUBLER AND FILLER IAW B757 SRM 53-00-01, REPAIR 29 & NDTM PT 6 51-00-16, INSTALLED ID TAG IAW DPS 900-5-1 NO:04, PERFORM A DECAL CONDITION INSPECTION EVERY C CHECK PER TOPP MANUAL 30-10-70 PAR 1, PAGE 14.

Part: SKIN — DENTED (BS 1320-1340) · airframe 72,773 hrs · 28,014 cycles

(AIRCRAFT 5643, L/P 1358095) DENT ON EXTERNAL FUSELAGE SKIN BTWN STA 1320-1340, BTWN STR 29L-30. CORRECTIVE ACTION: FABRICATED REPAIR PARTS. LOCATED, DRILLED, TRIMMED AND INSTALLED REPAIR PARTS AS REQ IAW B757 SRM 53-00-01 R.29, SRM 51-40-02, 51-40-05, 51-40-08, INSTALLED ID TAG IAW DPS 900-5-1 NO:04, PERFORM A DECAL CONDITION INSPECTION EVERY C CHECK PER TOPP MANUAL 30-10-70 PAR1 PAGE 14.

Part: CREASE BEAM — CORRODED (BS 1175) · corrosion level 2 · airframe 72,773 hrs · 28,014 cycles

(AIRCRAFT 5643, L/P 1358057) MAIN CABIN STA 1175 RH SIDE CREASE BEAM CORRODED. CORRECTIVE ACTION: REMOVED CORROSION AS REQ AT MAIN CABIN STA 1175 R/H INNER CHORD CUSP WEB. FABRICATED, LOCATED, DRILLED AND TRIMMED 3 EA REPAIR PARTS (1) EA STRAP. INSTALLED REPAIR PARTS IAW B757 SRM 53-00-13 REPAIR 2.

Part: SEAT TRACK — GOUGED (BS 1295) · airframe 72,773 hrs · 28,014 cycles

(AIRCRAFT 5643, L/P 1356001) MAIN CABIN R/H INBOARD SEAT TRACK IS GOUGED OUT OF LIMITS AT STA 1295. CORRECTIVE ACTION: REMOVED, FABRICATED AND INSTALLED NEW MAIN CABIN R/H INBOARD SEAT TRACK STA 1295 USING BAC 1520-792 7178 IAW B757 SRM 53-60-52 AND B 757 SRM 51-40-02 BETWEEN STA 1140 TO 1320.

Part: SEAT TRACK — GOUGED (BS 1325) · airframe 72,773 hrs · 28,014 cycles

(AIRCRAFT 5643, L/P 1355990) MAIN CABIN R/H OUTBOARD SEAT TRACK IS GOUGED OUT OF LIMITS AT STA 1325. CORRECTIVE ACTION: CUT OUT DAMAGED SECTION ON MAIN CABIN R/H OUT BOARD SEAT TRACK BETWEEN STA 1510 TO 1560 RBL 54 IAW B757 SRM 53-00-52 REP 1. FABRICATED AND INSTALLED REPAIR PARTS IAW B 757 SRM 53-00-52, REP 1 AND B 757 SRM 51-40-02.

Part: SEAT TRACK — GOUGED (BS 1510) · airframe 72,773 hrs · 28,014 cycles

(AIRCRAFT 5643, L/P 1355999) MAIN CABIN L/H INBOARD SEAT TRACK IS GOUGED OUT OF LIMITS AT STA 1510. CORRECTIVE ACTION: CUT OUT DAMAGED SECTION OF SEAT TRACK ON MAIN CABIN L/H INBOARD SEAT TRACK BETWEEN STA 1510 TO 1560 IAW B 757 SRM 53-00-52, FABRICATED AND INSTALLED REPAIR PARTS IAW B 757 SRM 53-00-52 REP 7 AND B 757 SRM 51-40-02.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,773 hrs · 28,014 cycles

(AIRCRAFT 5643, L/P 1339494) AFT CABIN FLOOR STRUCTURE HAS CORROSION ON UPPER SURFACE FROM STA 1681-1718 BL 0 - LBL 54. CORRECTIVE ACTION: REMOVED CORROSION AT FLOOR STRUCTURE AFT DECK FROM STA 1681 - 1718 BL 0 TO LBL 17 AND LBL 25 TO LBL 54 IAW B757 SRM 51-10-02, AREA WITH ORIGINAL THICKNESS .071 MATT LOSS .005 MATT REMAINING .066 TO BE WITHIN LIMITS IAW B757 SRM 53-00-51. AREA BETWEEN STA 1681 - 1718 LBL 18 TO LBL 24 WITH MATT REMAINING .060 TO BE OUT OF LIMITS IAW B757 SRM 53-00-51 CUT OUT DAMAGED AREA FABRICATED AND INSTALLED REPAIR PARTS IAW B757 SRM 53-60-51 REP 17.

Part: SKIN — DAMAGED (BS 550-661) · airframe 72,773 hrs · 28,014 cycles

CROWN SKIN DAMAGED BS 550 - 661 STR 10L TO 10R. COMPLIED WITH ERA 581456-14, COMPARED ERA 581456-14 REV ORIGINAL WITH PRI 581456-14 REV 0 THUR 4, BOTH MATCH.

Part: STRUCTURE — DAMAGED · airframe 73,423 hrs · 28,198 cycles

(AIRCRAFT 5643, L/P 5894078) HARD LANDING ON NOSE WHEEL AFTER MAINS TOUCHED DOWN. CORRECTIVE ACTION: WHILE PERFORMING HARD LANDING PHASE I INSPECTION FOUND EXTENSIVE DAMAGE. REQUIRES PHASE II INSP. PER B757 AMM 05-51. REF. L/P 1251252 FOR PHASE II INSPECTION COMPLIED WITH. PERFORMED REPAIRS PER ER/A 580761-14 REV A AND ER/A 580760-14 REV A . REQUIRED INSPECTION COMPLIED WITH. REF LOG PAGE 5894099.

Part: STRINGER — DAMAGED (NOT REPORTED) · airframe 72,773 hrs · 28,014 cycles

DAMAGED STRINGERS. COMPLIED WITH ERA 581455-14, COMPARE ERA 581455-14 REF ORIGINAL WITH PRI 581455-14 REV 0 THUR 5.

Part: FRAME — CRACKED (BS 1681) · airframe 72,773 hrs · 28,014 cycles

DURING ACCOMPLISHMENT OF OPEN HOLE EDDY CURRENT PER AA5311-01207-01B STEP 13, FOUND INBOARD HOLE HAS CRACK INDICATION AT APPROXIMATELY 3 O'CLOCK POSITION AS VIEWED FROM REAR. INDICATION IS IN THE STA 1681 FRAME, NOT THE CLIP ON AFT SIDE OF FRAME. CANNOT DETERMINE LENGTH OF CRACK WITH INSTALLATION STACK UP. COMPLIED WITH ER/A 581570-14AD REV ORIGINAL.

Part: FRAME — CRACKED (BS 1640) · airframe 72,773 hrs · 28,014 cycles

CRACK IN FRAME BS 1640 UNDER STRAP AT STRINGER 14L. UNABLE TO DETERMINE LENGTH. REPAIR MUST BE COMPLETED PRIOR TO FURTHER FLIGHT. COMPLIED WITH ER/A 581573-14AD REV ORIGINAL.

Part: SKIN — DAMAGED (CROWN) · airframe 74,705 hrs · 28,531 cycles

DURING PERMANENT REPAIR OF CROWN SKIN DAMAGE PER ER/A 581456-14, DAMAGE REMOVAL REQUIRED THE REMOVAL ON GPS ANTENNAS AND / MOUNTING STRUCTURE REF ERA 581683-14. CORRECTIVE ACTION: REF ERA 581683-14 REV A.

Part: STRAP — UNSECURE (R1 DOOR) · airframe 71,567 hrs · 27,705 cycles

(AIRCRAFT 5643, L/P 5491190) STRAP HANGING FROM 1R DOOR NEAR BOTTOM OF DOOR SLIDE. RESECURED DITCHING STRAP TO SLIDE BUSSEL PER AMM 52-11.

Part: HANDLE — OBSTRUCTED (L3 DOOR) · airframe 70,525 hrs · 27,422 cycles

(AIRCRAFT 5643, L/P 5340812) 3L DOOR SLIDE LIGHT WON'T COME ON & ARM HANDLE WILL NOT "ARM". CLEARED OBSTRUCTION - OPS CHECK GOOD. OK SERVICE - REF B757 AMM 25-66.

Part: PROXIMITY SWITCH — OUT OF ADJUST (L4 DOOR) · airframe 70,429 hrs · 27,395 cycles

SHIP 5643 ON TAKEOFF "L AFT ENT DOOR" EICAS MSG CAME ON FOR A FEW SECONDS AND THEN EXTINGUISHED SEVERAL TIMES. CORRECTIVE ACTION: PSEU BITE SHOWS NO FAULTS AND TARGET POSITION INDICATES NORMAL. CLEANED AND INSPECTED PROX SWITCH AT DOOR 4L. ADJUSTED PROX SWITCH PLUNGER OUT SLIGHTLY TO ELIMINATE NUISANCE INDICATION. (5365382)

Part: TRANSMITTER — MALFUNCTIONED (HYD SYSTEM IND) · airframe 69,933 hrs · 27,261 cycles

(AIRCRAFT 5643, L/P 4216116) DURING DESCENT GOT C HYD SYS PRESS EICAS MSG, COMPLIED W/ QRH AFTER LANDING DURING TAXI LOST R HYD SYSTEM. STOPPED A/C AND TOWED TO GATE. AFTER LANDING DURING TAXI LOST R HYD SYSTEM TRANSFER TO LOG #4216117. TROUBLESHOT CENTER HYD PRESS INDICATION PER B757 FIM 29-11-00-815-831. NO FAULTS FOUND. PERFORMED ENG RUN, TO RUN BOTH CENTER PUMPS. NO FAULTS. R&R CENTER PRESS X-MITTER M342 & C SYSTEM PRESSURE SWITCH S10002 AS PRECAUTION. REF B757 AMM 29-31-01 AND B757 AMM 29-11-19. OPS CHECKS GOOD. CONTACTED MC. OK FOR SVC.

Part: LANYARD — UNSECURE (R1 DOOR) · airframe 69,830 hrs · 27,232 cycles

SHIP 5643 DOOR 1R WILL NOT ARM. CORRECTIVE ACTION: RESECURED DOOR LAYNARD. (4396058)

Part: LANYARD — UNSECURE (R1 DOOR) · airframe 69,691 hrs · 27,189 cycles

SHIP 5643 1R DOOR WILL NOT ARM. CORRECTIVE ACTION: FOUND SECURITY LANYARD LOOSE, RECONNECTED LANYARD REF B757 AMM 52-11. (4396012)

Part: DOOR — OBSTRUCTED (R1) · airframe 69,360 hrs · 27,093 cycles

AT DEP, 1R DOOR WONT ARM. REMOVED DEBRIS. SATIS.

Part: PLUNGER — FAILED (L4 DOOR WARNING) · airframe 68,212 hrs · 26,767 cycles

DURING A ROUTINE GIRT BAR TEST. THE L4 DOOR SHOWED CLOSED ALL THE TIME. EICAS DOES NOT SEE L4 DOOR OPEN. REPLACED THE DOOR WARNING SENSOR PLUNGER ROD IAW AMM 52-71-00. CHECKED GOOD.

Part: GIRT BAR — FOD (R1 DOOR) · airframe 68,194 hrs · 26,762 cycles

R1 DOOR WONT ARM. INSPECTED THE GIRT BAR FOR SLIDE, CLEARED DEBRIS, CLOSED AND ARMED DOOR. OK FOR SERVICE.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 68,218 hrs · 26,770 cycles

PASSENGER SEATS, TRIPLE SEAT Y/C ROW 40 RIGHT FWD INBOARD SEAT TRACK DAMAGED. COMPLIED WITH ERA 569526-14 REV ORIG SEC II PERMANENT REPAIR, INSTRUCTIONS AND ERA 569675-14 REV ORIGINAL.

Part: ROPE — UNSECURE (R1 DOOR) · airframe 68,110 hrs · 26,742 cycles

DOOR 1R HAS WIRE HANGING OUT OF THE BOTTOM. SECURED SURVIVAL ROPE CHK GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 68,064 hrs · 26,732 cycles

EMERGENCY LIGHT LENS AT SEAT 27A WAS MISSING. INSTALLED A NEW LENS IAW AMM 33-51.

Part: ACM — SEIZED (LEFT) · airframe 67,913 hrs · 26,693 cycles

AIR TURNBACK DUE TO THE CREW REPORTED DURING CLIMB, THERE WAS A HAZE AND ODOR IN THE COCKPIT WITH AN ASSOCIATED EQUIPMENT COOLING FAN OVERHEAT WARNING. REPLACED A SEIZED LEFT ACM. REPLACED LT LOW LIMIT VALVE AND REHEATER AS PRECAUTION. PERFORMED WATER SPRAY NOZZLE CHECK FOR LT PACK, CHECKED GOOD. INSP 2.5 BLEED RING FOR OIL LEAKS, NONE NOTED. PERFORMED SINGLE PACK CONFIDENCE CHECK, ALL WITHIN LIMITS. REPLACED RT TEMP CONTROL VALVE DUE FAULT, LOG 4387226.

Part: FITTING — DIRTY (L1 GIRT BAR) · airframe 67,371 hrs · 26,570 cycles

DUE TO REPORTS OF R1 DOOR MECHANISM BEING STICKY AND HARD TO ARM. CLEANED, LUBED, AND INSPECTED THE R1 GIRT BAR ATTACH FITTINGS. MANUALLY ENGAGED GIRT BARS AND VERIFIED SLIDE LIGHT AND GIRT BAR ATTACHMENT.

Part: PROXIMITY SENSOR — FAILED (L2 GIRT BAR) · airframe 67,377 hrs · 26,571 cycles

SLIDE INDICATOR LIGHT INOPERATIVE. REMOVED AND REPLACED THE L2 GIRT BAR PROXIMITY SENSOR IAW AMM 25-66.

Part: MECHANISM — OBSTRUCTED (R1 DOOR SLIDE) · airframe 67,231 hrs · 26,534 cycles

R1 DOOR NOT ARMING. REPACKED A LOOSE STRING SO AS TO NOT INTERFERE WITH SLIDE MECHANISM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 66,880 hrs · 26,438 cycles

ROW 26DEF HAS ONE RED EMERGENCY LIGHT LENS BROKEN. REPLACED THE LENS, OPS CHECKED NORMAL.

Part: UNKNOWN — ODOR (CABIN) · airframe 66,682 hrs · 26,384 cycles

HOT ODOR REPORTED BY FLIGHT ATTENDANT COMING FROM VENTS EITHER SIDE OF THE L3 DOOR. VENTS WERE WARM. HOT ODOR. LASTED ABOUT 10 MINUTES. EXAMINED AREA ABOVE AND BELOW L3 DOOR NO SIGNERS OF BURNING OR HOT ODOR. PERFORMED CHECK OF AND EXAMINED COFFEEMAKER AT THE L3 DOOR. COFFEEMAKER INOPERATIVE. PERFORMED DOOR HEATER CHECK IAW AMM 21-45, OPS CHECKED GOOD. PERFORMED NOGO ODI PREVENTION CHECK LIST, NO OTHER CAUSES WERE FOUND.

Part: THRESHOLD — DIRTY (R1 DOOR) · airframe 65,894 hrs · 26,179 cycles

R1 DOOR SLIDE WOULD NOT ARM. REMOVED DEBRIS FROM THE THRESHOLD. OPS CHECKED GOOD.

Part: ANGLE — GOUGED · airframe 65,756 hrs · 26,134 cycles

ANGLE HAS A DEEP GOUGE, BOTTOM OF VERTICAL LEFT SIDE LOWER FWD ATTACH ANGLE. COMPLIED WITH ERA 562481-14 REV ORIGINAL.

Part: ATTACH ANGLE — GOUGED (VERTICAL STAB) · airframe 65,756 hrs · 26,134 cycles

DEEP GOUGE AT BOTTOM OF VERTICAL STAB LT SIDE LOWER FWD ATTACH ANGLE. REPAIRED THE ATTACH ANGLE IAW ERA 562481-14, REV 0.

Part: SLIDE — DAMAGED (L4 DOOR) · airframe 65,756 hrs · 26,134 cycles

L4 DOOR SLIDE PACK BULGED AT CORNERS. SLIDE REPLACED.

Part: BEARING — WORN (HORIZONTAL STAB) · airframe 65,756 hrs · 26,134 cycles

RIGHT HORIZONTAL STAB, RIGHT SYSTEM ACTUATOR, MOST OUTBOARD UNIT BEARING WORN OUT, CLEVIS LINK SLOPPY, MOVES WHEN SHAKEN BY HAND. VISIBLE FROM BOTTOM, LOOKING UP, HEAVY RUST AROUND WORN BEARING. REPLACED PCU ON CARD 2900-4202-01.

Part: MECHANISM — OUT OF ADJUST (L1 DOOR) · airframe 65,756 hrs · 26,134 cycles

L1 DOOR EMERGENCY POWER TRIGGER MECHANISM DID NOT MEET CABLE TRAVEL MEASUREMENT. THE MECHANISM WAS ADJUSTED IAW AMM 52-11-32.

Part: SKIN — CORRODED (FUSELAGE) · airframe 65,756 hrs · 26,134 cycles

CORROSION IN THE SKIN JOINT AT THE 6 O CLOCK POSITION ON THE FUSELAGE JUST BELOW THE AFT CARGO DOOR AND JUST IN FRONT OF THE ANTENNA ON THE BELLY. REPAIRED PER SRM 53-00-01 AND RESTORED FINISH PER SRM 51-20-01.

Part: BRACKET — WORN (WING DUCT) · airframe 65,756 hrs · 26,134 cycles

PNEUMATIC DUCT SUPPORT WORN IN WING L/E AT THE NR 6 SLAT. R & R THE SUPPORT BRACKET IAW AMM 36-11-01.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 65,590 hrs · 26,084 cycles

DIV TO OKC DUE TO CREW OXYGEN SLOWLY DECREASING AND DOWN TO 240 PSI. MTC FOUND OBS SEAT O2 MASK IN EMERGENCY, REPLACED OBS O2 STORAGE BOX. FOUND F/O O2 MASK LEAKING AT STORAGE BOX, REPLACED MASK AND STORAGE BOX. REPLACED O2 BOTTLE LEAK CHECKS GOOD.

Part: HANDLE — OUT OF ADJUST (L2 DOOR) · airframe 65,233 hrs · 25,984 cycles

L2 DOOR EXTERIOR HANDLE NOT SEATED FLUSH AFTER DOOR CLOSURE. ADJUSTED EXTERIOR DOOR HANDLE CATCH IAW AMM 52-11. DOOR HANDLE LATCHED & SECURED FLUSH AFTER CLOSURE. OK FOR SERVICE.

Part: GIRT BAR — OBSTRUCTED (L3 DOOR) · airframe 63,190 hrs · 25,447 cycles

DOOR 3L DOOR ARMING HANDLE JAMMED WON'T MOVE. REMOVED DEBRIS FROM GIRT BAR, PERFORMED OPS CHK PER AMM 52-11, OPS CHKS GOOD. OK FOR SVC.

Part: LANYARD — OUT OF POSITION (R1 DOOR SLIDE) · airframe 63,182 hrs · 25,445 cycles

R1 DOOR SLIDE WILL NOT ARM.FOUND SURVIVAL STRAP ATTACH CHORD CAUGHT IN GIRT BAR MECHANISM. REPOSTIONED CHORD. DOOR SLIDE ARMS AND DISARMS. REF. B757 AMM 25-66.

Part: COVER PLATE — UNSECURE (R2 DOOR) · airframe 62,309 hrs · 25,200 cycles

2R ARM LEVER PART MISSING. SECURED COVERPLATE FOR DOOR HANDLE ATTACH.

Part: LANYARD — UNSECURE (R1 DOOR SLIDE) · airframe 62,249 hrs · 25,185 cycles

R1 MAIN DOOR WOULDN'T ARM. SECURED THE R1 DOOR SLIDE LANYARD. GROUND CHECKED GOOD.

Part: SIGN — DISLODGED (EMERGENCY LIGHT) · airframe 60,502 hrs · 24,699 cycles

EXIT SIGN OVER 2L DOOR COVER FELL OFF. RESECURED EXIT SIGN.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 60,546 hrs · 24,711 cycles

DOOR 2R EXIT LENS COSMETICALLY DAMAGED. REPLACED LENS ACFT OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 60,201 hrs · 24,597 cycles

WHILE CONDUNTING AN OPS CHECK OF THE INTERIOR EMERGENCY LIGHTS DURING THE SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE IN MULTIPLE SECTIONS. FOUND BATTERIES DEPLETED AND UNABLE TO HOLD CHARGE AT BATTERY PACK CHARGERS M730, M732, M10568, M10699 AND M736. R & R DEFECTIVE UNITS IAW AMM 33-51. OPS CHECK GOOD.

Part: RETAINER — DAMAGED (EMERGENCY LIGHT) · airframe 60,044 hrs · 24,561 cycles

EXIT SIGNS ON L2 DOOR FALL OFF. FOUND LENS 2 EA RETAINING LEAF SPRINGS BENT. REPOSITIONED SPRINGS. INSTALLED LENS IAW AMM 33-51-10. CKS GOOD. MCC ADVISED. OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,920 hrs · 24,527 cycles

ON TAKEOFF AND ENROUTE CABIN EMERGENCY LIGHTS WOULD ILLUMINATE WITH COCKPIT SWITCH IN ARMED POSITION. FOUND FORWARD EMERGENCY LIGHTS ON WITH COCKPIT SWITCH IN ARMED POSITION. R & R EMERGENCY LIGHT BATTERY CHARGER, M731 AND BATTERY IAW AMM 33-51. INSPECTED NLG EMERGENCY LIGHT TEST SWITCH WIRING. NO FAULTS FOUND. R & R EMERGENCY LIGHT POWER TRANSFER RELAY K10570. SYS OPS CHECKS NORMAL IAW AMM 33-51.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 59,824 hrs · 24,500 cycles

THE EMERGENCY LIGHTS FLICKERED ON AND OFF DURING TAKEOFF AND REMAINED ILLUMINATED UNTIL MID CLIMB. DOORS 1 AND 3 LIGHTS STAYED ILLUMINATED UNTIL CRUIZE. MAINTENANCE FOUND AND REPLACED TWO BAD BATTERY PACKS, 1 IN THE FWD GALLEY AND ONE IN THE AFT GALLEY. BOTH CHARGERS WERE ALSO REPLACED. LIGHTS CHECKED OK.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 59,824 hrs · 24,500 cycles

THE CABIN EMERGENCY LIGHTS ILLUMINATED ON TAKEOFF AND CLIMB OUT AND WERE UNCONTROLLABLE FROM THE F/F PANEL. MAINTENANCE TROUBLESHOT THE EMERGENCY LIGHT SYS AND COULD NOT FIND A PROBLEM. THE ACFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,652 hrs · 24,454 cycles

EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED EMERGENCY EXIT SIGN ABOVE L2 DOOR IAW AMM 25-60.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,984 hrs · 24,262 cycles

EMERGENCY LIGHT AT M731 INOPERATIVE. REPLACED CHARGER ASSY IAW AMM 33-50, CHECKED OK FOR SERVICE.

Part: FUSE — FAILED (EMERGENCY LIGHT) · airframe 58,917 hrs · 24,242 cycles

DURING SERVICE CHECK, FOUND LT OUTSIDE EMERGENCY LIGHT OUT. REPLACED THE FUSE. FOUND BETWEEN PIN NR 9, D7764 AND GROUND, 100 OHM MORE. RESEQURED GD2994-DC TERMINAL AND CKS NORMAL IAW MM33-51, WDM 33-51-13.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,895 hrs · 24,235 cycles

EXTERIOR EMERGENCY LIGHT AT DOOR 1 RT & EMERGENCY LIGHT AT ROW 1 THRU 3 INOPERATIVE. ISOL & T/S BATTERY PACK INOPERATIVE. REPLACED THE BATTERY PACK AND CHECKED OK.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 58,318 hrs · 24,092 cycles

L2 DOOR EMERGENCY EXIT OVERHEAD SIGN FALLS OFF WHEN DOOR IS CLOSED OR OPENED. REPLACED OVERHEAD EXIT SIGN.

Part: SNUBBER — FAILED (L4 DOOR) · airframe 58,278 hrs · 24,071 cycles

L4 DOOR SNUBBER FAILED CHECK ON WC 521-2102-4L, STEP 2. REPLACED L4 DOOR SNUBBER REF N/R CARD 00273.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,528 hrs · 23,634 cycles

MSP MAINTENANCE FOUND EMERGENCY EXIT LIGHTING INOPERATIVE ROWS 24-28. EMERGENCY LIGHTS POWER SUPPLY ABOVE ROW 23 DEF WAS REPLACED. LP1941441.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 56,423 hrs · 22,997 cycles

EMERGENCY AISLE SEAT LIGHTS INOPERATIVE FROM ROW 20 TO ROW 28. TROUBLESHOT & REPAIRED WIRING IAW WDM 33-51-22 AND EMERGENCY LIGHTS INSTALLATION DWG 5B33-41158.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,420 hrs · 22,995 cycles

DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE ON SEATS ROWS 20 TO 28. R & R EMERGENCY POWER SUPPLY ON ROW 23. OPS CHECKED NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,374 hrs · 22,961 cycles

ROW 24ABC TO 28ABC SEAT EMERGENCY LIGHTS OUT. R & R BATTERY PACK CHARGER IAW AMM 33-51.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 55,846 hrs · 22,656 cycles

ON S/C FOUND 34C EMERGENCY ESCAPE LIGHT INOPERATIVE. REPLACED SPLICE CONNECTION AT 34C.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,060 hrs · 22,162 cycles

AFT AISLE EXIT SIGN AND R4 DOOR EXIT SIGN INOPERATIVE DURING EMERGENCY LIGHT TEST. REPLACED POWER SUPPLY M00737 AND BATTERY PACK IAW AMM 33-51-07. EMERGENCY LIGHT CK OK.

Part: SKIN — DAMAGED (BS 570-660) · airframe 53,928 hrs · 21,433 cycles

FUSELAGE SKIN BS 570 - 660, S14-19L DAMAGED. SKIN REPLACED IAW ER/A 520601-14AD.

Part: SPRING — FAILED (GIRT BAR) · airframe 53,928 hrs · 21,433 cycles

L4 DOOR GIRT BAR LOCK SPRING CHECK FAILED. R & R L4 DOOR GIRT BAR ASSY IAW AMM 25-66-10-402-022, OPS CHECKED GOOD.

Part: FLOOR PANEL — CORRODED (BS 1681) · corrosion level 2 · airframe 53,928 hrs · 21,433 cycles

AFT CABIN FLOOR LOWER SURFACE BS 1681, LBL 3, 39 AND 46 IS CORRODED. BLENDED OUT CORROSION FOUND OUT OF LIMIT. ACCOMPLISHED PERMANENT REPAIR IAW REF SRM 53-60-51 REPAIR.

Part: ANGLE — CORRODED (BS 1360-1380) · corrosion level 2 · airframe 53,928 hrs · 21,433 cycles

DURING REMOVAL OF RT TRANSITION PANEL, DISCOVERED CORROSION ON AFT CARGO LOWER SILL ANGLE BS 1360-1380. R & R SILL ANGLE IAW SRM 51-40-02. PG 1-10.

Part: CREASE BEAM — CORRODED (BS 1180-1200) · corrosion level 2 · airframe 53,928 hrs · 21,433 cycles

MAIN CABIN CREASE BEAM HAS CORROSION AT STRINGER 17R, BS 1180-1200. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13, PG 102, FIG 101. INSTALLED PERMANENT REPAIR IAW ER/A 520606-14.

Part: FRAME — DENTED (BS 540) · airframe 53,928 hrs · 21,433 cycles

FUSELAGE FRAME BS 540, S23-25L, DENTED IN TWO PLACES. FRAME TRIMMED AND REPAIRED IAW ER/A 520603-14.

Part: STRINGER — DENTED (BS 590-660) · airframe 53,928 hrs · 21,433 cycles

ON REMOVAL OF FUSELAGE SKIN, LT BS 590-660 DISCOVERED STR 16L DENTED ON LOWER FLANGE AT STA 598-605. DENT ON STR 16L LWR FLANGE STA 598-605 MEASURED A=1.0", Y=.050" A/Y=20. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03, ALLOWABLE DAMAGE 1, PG 2, FIGURE 101, DETAIL III. REPAIRED STR 16L FROM STA 570-612 IAW SRM 53-00-03, REPAIR 1, FIG 201 AS PERMANENT.

Part: STRINGER — CORRODED (BS 594) · airframe 53,928 hrs · 21,433 cycles

ON REMOVAL OF SKIN, DISCOVERED STRINGER 18L DENTED ON LOWER FLANGE AT BS 594. REPAIRED IAW SRM 53-00-03, FIG 201, REPAIR 1.

Part: ANGLE — CORRODED (BS 560-620) · corrosion level 2 · airframe 53,928 hrs · 21,433 cycles

ON REMOVAL OF NUT PLATE STRIP ON FORWARD CARGO DOOR SILL, LOWER ANGLE FOUND CORRODED BS 560 TO 620 ON UPPER SURFACE OF OTBD FLANGE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15, FIG 101. R & R IAW SRM 51-40-05 & SRM 51-40-02.

Part: CREASE BEAM — CORRODED (BS 780) · corrosion level 2 · airframe 53,928 hrs · 21,433 cycles

MID CABIN RT INBD CREASEBEAM ANGLE HAS CORROSION BS 780, RBL 62. R & R ANGLE IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 53,928 hrs · 21,433 cycles

FORWARD CABIN, FLOORBEAM HAS CORROSION, PREVIOUS BLEND, AT BS 365, RBL 5-20. REMOVED CORROSION TO FOUND OUT OF LIMITS. INSTALLED PERMANENT REPAIR IAW SRM 53-00-51.

Part: CREASE BEAM — CORRODED (BS 860-900) · corrosion level 2 · airframe 53,928 hrs · 21,433 cycles

MAIN CABIN CREASEBEAM INNER ANGLE HAS AREAS OF CORROSION BETWEEN BS 860 AND 900. REMOVED CORROSION IAW SRM 53-30-13, FIG 101, DETAIL VIII ALLOWABLE DAMAGE-I, PAGE 105. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, FIG 101, DET VIII ALLOWABLE DAMAGE -I, PAGE 105. REMOVED DAMAGE CREASEBEAM AND REPLACED IAW SRM 51-40-02.

Part: FRAME — DENTED (BS 1480) · airframe 53,928 hrs · 21,433 cycles

AFT CARGO BAY, FRAME DENTED AT BS 1480, LBL 28. CUT OUT DAMAGE IAW SRM 53-00-07, REPAIR 5, FIG 2, STEP 1. FABRICATED, REPAIR J SECTION. INSTALLED REPAIR SECTION IAW SRM 51-40-02, PARA 7D AND SRM 53-00-07, REPAIR 5, FIG 201, DETAIL 1.

Part: FLOORBEAM — CORRODED (BS 377) · corrosion level 2 · airframe 53,928 hrs · 21,433 cycles

FORWARD CABIN, FLOORBEAM HAS CORROSION ON UPPER AND LOWER SURFACES BS 377, LBL 12-RBL 8. REMOVED CORROSION TO FOUND OUT OF LIMITS IAW SRM 53-00-51. ALLOWABLE DAMAGE, 1 DETAIL III. INSTALLED PERMANENT REPAIR IN REF SRM 53-00-51, REPAIR 10.

Part: STRINGER — CORRODED (BS 633-637) · airframe 53,928 hrs · 21,433 cycles

ON REMOVAL OF SKIN, DISCOVERED STRINGER 15L DENTED ON LOWER FLANGE BS 633-637. REPAIRED IAW SRM 53-00-03 REPAIR I, FIG 201.

Part: FRAME — DENTED (BS 1340) · airframe 53,928 hrs · 21,433 cycles

AFT CARGO BAY, BILGE FRAME DENTED AT BS 1340, RBL 28. REPAIRED FRAME IAW SRM 53-00-07, REPAIR 5, FIG 201.

Part: CREASE BEAM — CORRODED (BS 1020-1040) · corrosion level 2 · airframe 53,928 hrs · 21,433 cycles

MAIN CABIN RT CREASEBEAM HAS AREAS OF CORROSION BETWEEN BS 1020 AND 1040, REMOVED CORROSION & FOUND OUT OF LIMITS. R & R CREASEBEAM ANGLE IAW SRM 51-10-02.

Part: FRAME — DENTED (BS 1520) · airframe 53,928 hrs · 21,433 cycles

AFT CARGO, LT BILGE FRAME HAS DENT AT BS 1520, LBL 27. TRIMMED OUT DAMAGE ON FRAME AND REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 5.

Part: FRAME — DENTED (BS 660) · airframe 53,928 hrs · 21,433 cycles

FWD CARGO FRAME DENTED AT BS 660, LONGERON 24L. ACCOMPLISHED PERMANENT REPAIR IAW SRM 53-00-07, FIG 201, REPAIR 5.

Part: FRAME — DENTED (BS 1500) · airframe 53,928 hrs · 21,433 cycles

AFT CARGO BILGE FRAME DENTED AT BS 1500, RBL 24, REPAIRED IAW SRM 53-00-07, REPAIR 5, FIG 201.

Part: FRAME SPLICE — GOUGED (BS 1480) · airframe 53,928 hrs · 21,433 cycles

AFT CARGO, RT FRAME SPLICE HAS GOUGES BS 1480, STRINGER 23- 25R. R & R FRAME SPLICE IAW SRM 51-40-02.

Part: STRAP — BROKEN (BS 365-377) · airframe 53,928 hrs · 21,433 cycles

BROKEN STABILIZER STRAP BETWEEN CABIN FLOORBEAMS AT BS 365 AND 377, LBL 24. R & R BROKEN STABILIZER STRAP IAW ER/A 384483-14MA, REV D.

Part: CONNECTOR — LOOSE (CABIN) · airframe 4,368 hrs · 1,580 cycles

DURING LINE CHECK MAINTENANCE FOUND EXIT SIGN AT 3R INOP. MAINTENANCE RECONNECTED LOSE CONNECTOR. EXIT SIGN NOW WORKS OK PER AMM 33-51.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 4,354 hrs · 1,576 cycles

DURING LINE CHECK MAINTENANCE FOUND DOOR EMERGENCY SLIDE AT DOOR R2 INOP. MAINTENANCE REPLACED BATTERY PACK M736. CHECK OF LIGHT NOW OK PER AMM 33-51.

Part: FRAME — CORRODED (BS 1380) · corrosion level 2 · airframe 53,929 hrs · 21,434 cycles

DURING CHECK, CORROSION WAS FOUND COMMON TO BS 1380 FRAME WEB AT STRINGER 25R. CORRODED FRAME WEB WAS REPAIRED IAW SECTION I OF ER/A 499039-14.

Part: HOUSING — BROKEN (EMERGENCY LIGHT) · airframe 2,330 hrs · 836 cycles

MX FOUND EMERGENCY LIGHT HSG AT 2L BROKEN. REPLACED EMERGENCY LIGHT ASSY. OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,102 hrs · 18,007 cycles

DURING A LINE CHECK, MX FOUND THE EMERGENCY PATH LIGHTS AT 1-4AB INOPERATIVE. MX REPLACED THE LIGHTS. OPS CHECK WAS GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 43,820 hrs · 16,857 cycles

DOOR 1 LEFT, EMERGENCY SLIDE LIGHTS INOP. REPLACED M731 POWER SUPPLY, OPS OK.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 43,813 hrs · 16,855 cycles

FIRST CLASS EMERGENCY EGRESS SEAT MOUNTED LIGHTS INOP (LOG PAGES 0161082, 0161883). REPLACED POWER SUPPLIES M730 AND M732, TESTS OK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,715 hrs · 16,822 cycles

DOOR 1L AND L629 EXIT LIGHT INOPERATIVE. REPLACED M731 BATTERY PACK. LIGHT CHECKED OK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 43,660 hrs · 26,490 cycles

DURING LINE CHECK FOUND SEAT-MOUNTED EMERGENCY LIGHTS AT ROWS 34-38 AND OVERHEAD EMERGENCY AISLE LIGHTS AT ROWS 27-37 INOPERATIVE. MAINTENANCE REPLACED BATTERY ON M735 POWER SUPPLY.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,912 hrs · 14,399 cycles

DURING OVERNIGHT LINE CHECK, FOUND DOOR 2 RIGHT EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED DOOR 2 RIGHT POWER SUPPLY, REF FIM NR 33-51-00, FIG NR 103. OPS CHECK NORMAL. AIRCRAFT OK FOR SERVICE.

Part: TORQUE BOX — CRACKED · airframe 21,117 hrs · 8,350 cycles

During "H" check found crack in outboard side of pylon lower torque box upper aft corner at access panel 433AL. Repaired per EA 56-189401.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED CHECK, MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY WITH A SERVICEABLE UNIT, OPERATIONAL CHECK WAS SATISFACTORY.