N6703D

Part: FSEU — FAULTED (FLAP SYSTEM) · airframe 71,863 hrs · 27,420 cycles

SHIP 6703 -FCNT/DE- DUE TO TRAILING EDGE FLAP DISAGREE DUE TO FLAP HANDLE OVERSHOOT. CORRECTIVE ACTION: PERFORMED FSEU BITE PER FIM AND RAN FLAPS WITH NORMAL OPERATION.

Part: GIRT BAR — FOD (ZONE 800) · airframe 71,691 hrs · 27,344 cycles

SHIP 6703 1R DOOR WILL NOT ARM. CORRECTIVE ACTION: FOUND DEBRIS PREVENTING GIRT BAR ENGAGMENT, RMVD DEBRIS. DOOR/ GIRT BART ARMS NML, REF B757 AMM 52-11. (6979994)

Part: FRAME — CRACKED (AFT CARGO L/H SI) · airframe 70,802 hrs · 26,872 cycles

SHIP 6703 AFT CARGO L/H SIDE FUSELAGE FRAME HAS EXISTING REPAIR AT FRAME STA 1460 S26L. APPROX 12" IN LENGTH. REF AD TASK CARD 5311-01227 -01A. STEP # 2. CORRECTIVE ACTION: SUMMARY OF NR-00205- REMOVED, FABRICATED AND INSTALLED FRAME REPAIR AT STA 1460 FRAME BTW STR-26L AND STR-28L TO ACCOMPLISH NDT INSPECTIONS PER WORK CARD 5311-01227-01A IAW ER/A 621867-14AD REV ORIG. REFERENCE LOG PAGES 0679921 AND 0679923 FOR FOLLOW ON INSPECTIONS.

Part: LIGHT — INOPERATIVE (MULTIPLE SEATS) · airframe 70,802 hrs · 26,872 cycles

SHIP 6703 MULTIPLE SEATS EEPLS LIGHT ASSEMBLIES DAMAGED. CORRECTIVE ACTION: REMOVED AND REPLACED MULTIPLE SEATS EEPLS LIGHT ASSEMBLIES AND PERFORMED SATISFACTORY EEPLS LIGHT OPS CHECKS IAW B757 AMM 33-51 -11. (0681162)

Part: FRAME — ABNORMAL (CARGO FRAME) · airframe 70,802 hrs · 26,872 cycles

SHIP 6703 DTA MONITOR INSPECTION LOG REF ERA 621867-14AD FUSELAGE / AFT CARGO FRAME / AT STA 1460 / S-26L & S-28L / EXISTING REPAIR. CORRECTIVE ACTION: REF ERA 621867-14. (0679921)

Part: ELEC CONNECTOR — DAMAGED (ZONE 200) · airframe 70,802 hrs · 26,872 cycles

SHIP 6703 MAIN CABIN RH EEPLS CONNECTOR AT BS 520 MISSING DOT 14/126. CORRECTIVE ACTION: REPLACED RH MAIN CABIN EEPLS CONNECTOR AT BS520 IAW B757 SWPM 20 -64-17. OP CHECK TO BE PERFORMED ON NR 00022. (0654894)

Part: LENS — BROKEN (ZONE 200) · airframe 70,802 hrs · 26,872 cycles

SHIP 6703 FWD GALLEY CLEAR EEPLS LIGHT LENS BROKEN. CORRECTIVE ACTION: REMOVED AND REPLACED FWD GALLEY CLEAR EEPLS LIGHT LENS IAW B757 AMM 33-51-11. FULL EEPLS LIGHTS OPS CHECKS TO BE PERFORMED ON NR -00022. (0654904)

Part: ELEC CONNECTOR — DAMAGED (ZONE 200) · airframe 70,802 hrs · 26,872 cycles

SHIP 6703 MAIN CABIN RH EEPLS CONNECTOR DAMAGED AT BS480 DOT 13/126. CORRECTIVE ACTION: REPLACED RH MAIN CABIN EEPLS CONNECTOR AT BS480 IAW B757 SWPM 20 -64-17. OP CHECK TO BE PERFORMED ON NR 00022. (0654888)

Part: ELEC CONNECTOR — MISSING (ZONE 200) · airframe 70,802 hrs · 26,872 cycles

SHIP 6703 MAIN CABIN RH EEPLS CONNECTOR MISSING AT BS1420 DOT 15/126. CORRECTIVE ACTION: REPLACED RH MAIN CABIN EEPLS CONNECTOR AT BS1420 IAW B757 SWPM 20-64-17. OP CHECK TO BE PERFORMED ON NR 00022. (0654898)

Part: LENS — BROKEN (ZONE 200) · airframe 70,802 hrs · 26,872 cycles

SHIP 6703 AFT R/H LAVATORY HAS 1EA RED AND 1EA CLEAR EEPLS LIGHTS LENS BROKEN. CORRECTIVE ACTION: REMOVED AND REPLACED AFT R/H LAVATORY 1EA RED AND 1EA CLEAR EEPLS LIGHTS LENS IAW B757 AMM 33-51-11. FULL EEPLS LIGHTS OPS CHECKS TO BE PERFORMED ON NR-00022. (0654911)

Part: SNUBBER — OUT OF TOLERANCE (ZONE 800) · airframe 70,802 hrs · 26,872 cycles

SHIP 6703 R-1 DOOR ROTARY SNUBBER FAILER INSPECTION CHECK, PIN EXTENSION LOWER THAN REQUIRED LENGTH. CORRECTIVE ACTION: SUMMARY OF NRC: 00314 - REMOVED AND REPLACED R-1 DOOR ROTARY SNUBBER IAW B757 AMM 52-11-10. (0655182)

Part: SNUBBER — LEAKING (L1 DOOR) · airframe 70,802 hrs · 26,872 cycles

SHIP 6703 L-1 PASSENGER DOOR ROTARY SNUBBER LEAKING FROM RETAINING NUT. CORRECTIVE ACTION: SUMMARY OF NRC: 00713 - REMOVED AND REPLACED L-1 DOOR ROTARY SNUBBER IAW B757 AMM 52-11-10. (0650713)

Part: WINDSHIELD — ARCED (ZONE 200) · airframe 70,802 hrs · 26,872 cycles

SHIP 6703 R1 WINDOW HAS SIGNS OF ARCING ALONG UPPER BUS BAR. CORRECTIVE ACTION: REMOVED AND REPLACED R/H CO-PILOT #1 WINDSHIELD IAW B757 AMM 56- 11-01. LEAK AND OPERATIONAL CHECKS. (0646948)

Part: TRACK — FOD (ZONE 800) · airframe 70,408 hrs · 26,642 cycles

SHIP 6703 1R DOOR WOULD NOT ARM. CORRECTIVE ACTION: OPENED DOOR AND FOUND DEBRIS ON DOOR TRACK. REMOVED DEBRIS, 1R DOOR ARMS AND DISARMS SUCCESSFULLY. (6022328)

Part: RESERVOIR — EMPTY (R1) · airframe 70,360 hrs · 26,619 cycles

SHIP 6703 R1 DOOR EMERGENCY POWER RESERVOIR FOUND EMPTY. CORRECTIVE ACTION: R/R R1 DOOR EMERGENCY POWER RESERVOIR PER B757 AMM 52-11-30. (6207892)

Part: LIGHT — DAMAGED (CABIN) · airframe 69,925 hrs · 26,390 cycles

SHIP 6703 FOUND DURING SRV CHECK - WHT EMER LIGHT ON LAV 202 IS DAMAGED AND MISSING LENS. REPLACED WHITE EMERGENCY LIGHT ASSEMBLY MOUNTED ON LAV 202. FOR SVC. REF B757 AMM 33-51-11. (5926998)

Part: WARNING MESSAGE — FALSE ACTIVATION (R2 DOOR SLIDE) · airframe 69,464 hrs · 26,118 cycles

SHIP 6703 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT/S. 2R SLIDE LIGHT INOP. CORRECTIVE ACTION: OPS CHECKED 2R DOOR SLIDE PER B757 AMM 25-66 COULD NOT DUPLICATE FAULT. OPS CHK OK

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 68,043 hrs · 25,401 cycles

2R SLIDE LIGHT INOPERATIVE/BROKEN (REMAINS ILLUMINATED). T/S PER SSM 25-66-01 FOUND LIGHT SWITCH INOP. R/R PER B757 SSM 25-66 OPS CHECK NML.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 67,776 hrs · 25,251 cycles

SHIP 6703 R1 DOOR WOULD NOT ARM FOR PUSHBACK. CORRECTIVE ACTION: CLEARED DEBRIS FROM GIRT BAR SLIDER. NOW OPS NORMAL. REF B757 AMM 52-71. (4427180)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 67,579 hrs · 25,142 cycles

SHIP 6703 MAIN CABIN FLOOR BEAM HAS A CRACK IN THE UPPER CHORD AT RADIUS BS.700 APROX RBL.25.5 (VIEW FROM FWD CARGO CEILING). CORRECTIVE ACTION: REPAIRED THE MAIN CABIN FLOOR BEAM AT STA 700 RBL 24 TO 26 IAW DELTA ERA 610023-14. (2868904)

Part: FRAME — UNKNOWN (BS 620 S3-4L) · airframe 70,064 hrs · 26,462 cycles

SHIP 6703 DTE, ERA 563827-14AD REVISION B, FUSELAGE / FRAME / FS620 / STR 3L - 4L / GROUND STUD FASTENER INTERFERENCE. CORRECTIVE ACTION: REF ERA 563827-14. (2850925)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 68,427 hrs · 25,601 cycles

SHIP 6703 FUSELAGE / FRAME / FS620 / STR 2L & 3R / OVERSIZE HOLES. CORRECTIVE ACTION: REF ERA 609749-14AD. (2843063)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 67,575 hrs · 25,141 cycles

SHIP 6703 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 573570-14 REV A. CORRECTIVE ACTION: REF ERA 573570-14AD. (1580140)

Part: SKIN — DAMAGED (RT WING) · airframe 67,575 hrs · 25,141 cycles

RIGHT OUTER WING UPPER SURFACE SKIN OTBD FWD DRAG FITTING, HOLE NR 5 FREEZE PLUG & OVERSIZED FASTENER. C/W ERA 573570-14.

Part: HOLDER — BROKEN (EXIT LIGHT) · airframe 67,402 hrs · 25,091 cycles

(AIRCRAFT 6703, L/P 6739326) SEAT 23D EXIT LIGHTING HOLDER BROKEN. CORRECTIVE ACTION: RESECURED AS REQUIRED.

Part: SENSOR — INTERMITTENT (L3 DOOR) · airframe 66,879 hrs · 24,905 cycles

3L SLIDE LIGHT ILLUMINATION IS INTERMITTENT. CORRECTIVE ACTION: R/R SENSOR IAW AMM 25-66-11. VERIFIED SLIDE BOTTLE PIN REMOVED AND DOOR ASSIST BOTTLE PIN REMOVED.

Part: SENSOR — OBSTRUCTED (L3 DOOR) · airframe 65,838 hrs · 24,487 cycles

(AIRCRAFT 6703, L/P 6025855) SLIDE LIGHT 3L INOP. T/S PER SSM 25-66-01. FOUND DEBRIS ON GIRT BAR SENSORS ON 3L DOOR. CLEANED SENSORS.

Part: PILOT VALVE — FAILED (LEFT BLEED SYS) · airframe 65,734 hrs · 24,441 cycles

DIVERTED DUE TO LT BLEED TRIP. CREW OPENED UP THE ISOLATION VALVE PER QRH AND THE RT BLEED TRIPPED FOLLOWED BY LOSS OF PRESSURIZATION. R & R 14TH STG PILOT VALVE PER B757 AMM 36-11 AND ENGINE BLEED TRIP ODI REMOVED FAN AIR VALVE PER B757 AMM 36-11. REMOVED FAN AIR TEMP SENSOR PER B757 AMM 36-11. R/R LT ENGINE HS PILOT VALVE CONTROL PER B757 AMM: 36-11. REPLACED FAN AIR VALVE PER B757 36-11 AMM. R/R REVERSE FLOW CONTROLLER PER B757 36-11 AMM. R/R #1 ENG HP VALVE PER B757 36-11 AMM. C/W AMDS CARD 3611-2010 PNEUMATIC SYSTEM ENGINE RUN DATA LEFT ENGINE BLEED CKS NML RT ENGINE FAILED. R/R RT ENGINE 14TH STG PILOT VALVE CONTROL AND 14TH STAGE BLEED VALVE PER B757 AMM 36-11. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (L4 DOOR SLIDE) · airframe 65,694 hrs · 24,427 cycles

L4 DOOR SLIDE LIGHT INOPERATIVE WITH DOOR ARMED.

Part: LENS — MISSING (EXIT SIGN) · airframe 64,196 hrs · 23,846 cycles

SHIP 6703 R2 DOOR EMERGENCY LIGHT EXIT SIGN OVER DOOR MISSING LENS. CORRECTIVE ACTION: REPLACED LIGHT LENS ASSY. (5063853)

Part: COVER — DETACHED (R3 DOOR SENSOR) · airframe 63,991 hrs · 23,753 cycles

SHIP 6703 3R DOOR WOULD NOT ARM FOR PUSHBACK. REATTACHED PROX SENSOR COVER.

Part: SIGN — LOOSE (CABIN) · airframe 63,968 hrs · 23,739 cycles

SHIP 6703 EMERGENCY EXIT SIGNS INOPERATIVE / LOCATIONS:02R. CORRECTIVE ACTION: FOUND EXIT SIGN LOOSE RESECURED SAME. (0951188)

Part: PANEL — DELAMINATED (CABIN) · airframe 63,642 hrs · 23,630 cycles

SHIP 6703 R2 DOOR UPPER EXIT LIGHT PANEL DISLODGED, DELAMINATED FROM FRAME. CORRECTIVE ACTION: INSTALLED NEW EXIT PANEL. (4865262)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 67,582 hrs · 25,145 cycles

AIRCRAFT 6703, DURING THE RADOME INTERCOSTAL INSTALLATION PER GOGO DRAWING D18470 / 22207 REV. C (REFERENCE AMDS WORKCARD 2330-01349-01D) AT STA 620 BETWEEN STR 2R AND 3R, MTC REPORTED SIX (6) EXISTING FASTENER HOLES IN THE FRAME WHERE THE INTERCOSTAL T-CLIP (P/N P31839-001) IS TO BE INSTALLED. THE HOLES FINAL DIAMETER AFTER CLEAN UP RANGES BETWEEN 0.198/0.335. CORRECTIVE ACTION: INSTALLED REPAIR DOUBLER AND REPAIRED PER ERA 563816-14. (LP 0878808)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 67,582 hrs · 25,145 cycles

AIRCRAFT 6703, MTC REPORTED SIX (6) EXISTING FASTENER HOLES IN THE FRAME THAT WERE IMPROPERLY INSTALLED BY A PREVIOUS MOD AT STA 620 BETWEEN STR 2L AND 3L. CORRCTIVE ACTION: INSTALL DOUBLER AND REPAIRED PER ERA 563815-14). (LP 0873499)

Part: SKIN — UNKNOWN (RT WING) · airframe 63,503 hrs · 23,579 cycles

(AIRCRAFT 6703, L/P 0863578) AA/AD: BROKEN PAINT AROUND THE FASTENER HEAD # 1 TO 10 (MOT 2). SUMMARY OF NRC 00371: RH OUTER WING UPPER SURFACE SKIN HOLE # 5 WAS REPAIRED PER ETI-57-18-040 REV. 7 AND ER/A 573570-14AD REV. ORIG. SECTION I. REPETITIVE INSPECTIONS (TBD) MUST BE MONITORED WITH LOG 0863227 PER ERA 573570-14 AD REV ORIGINAL SEC II ASSOCIATED AA 5720-01100 ADDED FOR AC 6703.

Part: SKIN — CRACKED (RT WING) · airframe 63,497 hrs · 23,577 cycles

(AIRCRAFT 6703, L/P 0863649) THIS NRC IS ISSUED INSTEAD OF NRC.00605 DUE TO WRONG DESCRIPTION : AWR: TO MAINTENANCE FACILITIES, REMOVE AND INSTALL PARTS AS REQUIRED OF THE REPAIR ON CRACK AT UPPER SKIN HOLE #5 RH WING IN REF. NRC 00371 AND CARD 5720-01100-0101B STEP 26. (RH-MOT 2). CORRECTIVE ACTION: SUMMARY: OF NRC 00606 PARTS WERE REMOVED AND INSTALL PER B 757-200 AMM 28-11-08-004-015, 28-11-01-004-001, 27-81-20-024-001, 26-11-01-024-001, 26-11-01-424-036 AND 28-11-01-404-014.

Part: BUSHING — CORRODED (RT NACELLE) · airframe 63,492 hrs · 23,574 cycles

(AIRCRAFT 6703, L/P 0863620) RII: CORROSION ON RH PYLON UPPER LINK BUSHING AMDS 2021-2718-2 (MOT2). REPLACED PER B757-200 AMM 54-51-01.

Part: BALLSCREW — CORRODED (RT WING TE FLAP) · airframe 63,492 hrs · 23,574 cycles

(AIRCRAFT 6703, L/P 0862121) RII: CORROSION ON OUTBD BUSHING BALL NUT ON OUTBD BALLSCREW OF RH WING INBD FLAP. OUTBD BUSHING BALL NUT ON OUTBD BALLSCREW OF RH WING INBD FLAP WAS REPLACED AND TESTED PER B 757-200 AMM 27-51-21.

Part: PAN — CRACKED (BS 1380) · airframe 63,492 hrs · 23,574 cycles

(AIRCRAFT 6703, L/P 0856741) INITIAL INSPECTION: CRAKED FWD LWR CORNER PAN STA 1380 AT AFT CARGO COMPARTMENT DOOR (PTAS). SUMMARY OF NRC 00060; (TWO CRACKS OF 1.500" AND 2.500" OF LENGTH) FWD LWR CORNER PAN STA 1380 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ETI-57-18-038 REV. 5 AND ER/A 573387-14 REV. ORIGINAL. MAINTENANCE REQUERIMENTS WERE VERIFIED AND FOLLOWINGS ACTIONS ARE NEEDED: IDENTIFY REPAIR PER DAL PROCESS STANDARD 900-5-1, NO 04. PER ER/A NO 573387-14 REV ORIGINAL SECTION I. PERMANENT REPAIR STEP 25.

Part: DOUBLER — CORRODED (LAV SERVICE AREA) · corrosion level 2 · airframe 63,492 hrs · 23,574 cycles

(AIRCRAFT 6703, L/P 0854699) INITIAL INSPECTION: CORROSION ON DOUBLER OF INTERNAL SKIN AT LAVATORY SERVICE PANEL.E&E. SUMMARY: IN REF NRC 00500 (CORROSION LEVEL 2) DOUBLER OF INTERNAL SKIN AT LAVATORY SERVICE PANEL.E&E WAS REPLACED PER B757-200 DWG 141N8631 REV: AF, SRM 51-40-02 PAR. 4 AND 7, AMM 30-71-04-404-006 AND AMM 38-32-16-404-074.

Part: BUSHING — WORN (LT NACELLE) · airframe 63,492 hrs · 23,574 cycles

(AIRCRAFT 6703, L/P 0852103) AWR. DUE TO THE REMOVAL OF LH ENGINE PYLON STRUT. WORN BUSHINGS INBD/OUTBD ON UPPER LUGS NAC STA: 162 AT LH ENGINE PYLON STRUT. (IN REF. CARD 2021-2718-1). SUMMARY: IN ACCORDANCE OF NRC # 546 LH PYLON STRUT WAS REPAIRED PER B757-200 SRM 54-51-90 REPAIR 3 PAG.201 AND NEW BUSHINGS WERE REPLACED ON LH PYLON STRUT PER B757-200 SRM 54-51-90 REPAIR 3 PAG. 203.

Part: STRUT — CHAFED (RT PYLON) · airframe 63,492 hrs · 23,574 cycles

(AIRCRAFT 6703, L/P 0852106) RII: CORROSION ON RH PYLON NACELLE STRUT BUSHING AMDS 2021-2718-2 (MOT2). SUMMARY: IN ACCORDANCE OF NRC # 368 RH PYLON STRUT WAS REPAIRED PER B757-200 SRM 54-51-90 REPAIR 3 PAG.201 AND NEW BUSHINGS WERE REPLACED ON RH PYLON STRUT PER B757-200 SRM 54-51-90 REPAIR 3 PAG. 203.

Part: ARM — CORRODED (RT SPIN BRAKE) · corrosion level 2 · airframe 63,492 hrs · 23,574 cycles

(AIRCRAFT 6703, L/P 0850693) AWR. HIDDEN CORROSION. CORROSION ON SETTLEMENT AREA OF LWR SPIN BRAKE BAR AT NLG WHEEL WELL RH BRAKE SPRING. (IN REF NRC 304) (FYT). SUMMARY: IN REF NRC00601 (CORROSION LEVEL 2)RH SPIN BRAKE ARM AT NLG WHEEL WELL AREA WAS REPLACED PER B757-200 AMM 32-45-05-402-008. (UT) MEASUREMENT THICKNESS WAS ACCOMPLISHED B757 NDT MANUAL PART. 4 51-00-10 AND AREAS ARE OUT OF LIMITS. PER. DWG 141N0091 REV A . EQUIP. PANAMETRICS 38DL PLUS N/C:1788, EXP 22/ FEB/19, S/N: 171455802, TRANSDUCER V260-SM N/S:1120097.

Part: ACTUATOR — MALFUNCTIONED (EVAC SLIDE) · airframe 63,492 hrs · 23,574 cycles

DURING OVERWING SLIDE PNEUMATIC DEPLOYMENT CHECK, THE OVERWING SLIDE COMP. DOOR DOESN'T DEPLOY WHEN APPLY THE MAXIMUM NITROGEN PRESSURE. REMOVED AND INSTALLED PNEUMATIC ACTUATOR ASSY PER AMM 25-65.

Part: PLATE — CORRODED (BS 1531-1570) · corrosion level 2 · airframe 63,492 hrs · 23,574 cycles

(AIRCRAFT 6703, L/P 0844235) AWR: IN REF. NRC 00126 CORROSION OUT LIMITS ON LH SIDE PLATE FROM STA 1531 TO 1570 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 0561: CORROSION LEVEL 2; LH SIDE PANEL FROM STA .1531 TO 1570 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM 53-00-53 REPAIR 3 FIG 201.

Part: STRINGER — CORRODED (BS 1460-1480) · corrosion level 2 · airframe 63,492 hrs · 23,574 cycles

(AIRCRAFT 6703, L/P 0842691) HIDDEN DAMAGE: CORROSION WAS FOUND, DURING RUSTED HARDWARE REMOVED ON STRIGER LBL 2.90 BTW. STA 1460 TO 1480 AT AFT CARGO COMPARTMENT (C2). CORROSION LEVEL 2, STRINGER WAS REPAIRED PER B757-200 SRM 53-00-53 REP.1 FIG 201 DETAIL X.

Part: FRAME — DAMAGED (BS 1500) · airframe 63,492 hrs · 23,574 cycles

SHIP 6703 INITIAL INSPECTION: BENDED FRAME STA 1500 BTW S-26L AND S-27L AT AFT CARGO COMPARTMENT (C2). CORRECTIVE ACTION: REF NRC 00122 REMOVED DAMAGE PER B757 SRM, INSPECTED AND NO CRACKS WER FOUND. REPAIRED PER B757 SRM. (0841539)

Part: FRAME — DAMAGED (BS 1500) · airframe 63,492 hrs · 23,574 cycles

SHIP 6703 INITIAL INSPECTION: BENDED FRAME STA 1500 BTW S-26L AND S-27L AT AFT CARGO COMPARTMENT (C2). CORRECTIVE ACTION: REF NRC 00122 DAMAGE AREA WAS REMOVED REF B757 SRM, INSPECTED AND NO CRACKS WERE FOUND. AREA WAS REPAIRED PER B757 SRM. (0841551)

Part: SPLICE — CRACKED (BS 1681) · airframe 63,492 hrs · 23,574 cycles

(AIRCRAFT 6703, L/P 0840572) INITIAL INSPECTION: CRACK ON SPLICE OF RH STATION 1681 FRAME BTW S-17 AND S-18 AT AFT CARGO COMPARTMENT. (C2). SUMMARY: IN REF NRC 00522 (ONE CRACK OF 0.875" LENGTH) SPLICE OF RH STATION 1681 FRAME BTW S-17 AND S-18 WAS REPLACED PER B757 DWG 146N8712 REV: BC.

Part: SUPPORT — CORRODED (BS 1640) · corrosion level 2 · airframe 63,492 hrs · 23,574 cycles

(AIRCRAFT 6703, L/P 0840562) INITIAL INSPECTION. CORROSION ON GALLEY SUPPORT OF FS STA: 1640 AND LBL 45 AT PAX CABIN FLOOR STRUCTURE W4 AREA. (CPAX). CORROSION LEVEL 2 GALLEY SUPPORT WAS REPLACED PER B757-200 SRM 51-40-02 PAR 7.

Part: FLOOR PANEL — DELAMINATED · airframe 63,492 hrs · 23,574 cycles

(AIRCRAFT 6703, L/P 0839517) DELAMINATED FLOOR PANEL NBR: 1020C AT WINGBOX AREA (CPAX) IN REF AMDS 2500-0177. SUMMARY: OF NRC 00584: FLOOR PANEL NBR. 1020C WAS FABRICATED, REPLACED AND IDENTIFIED PER. B-757 A.M.M. 53-01-01-201.

Part: SKATE ANGLE — CORRODED (BS 1661-1681) · corrosion level 2 · airframe 63,492 hrs · 23,574 cycles

SHIP 6703 SKATE ANGLE BTW FS STA: 1661-1681 AND LBL 54 AT PAX CABIN FLOOR STRUCTURE W4 AREA. CORRECTIVE ACTION: IN REFERENCE NRC 542 SUMMARY: CORROSION LEVEL II SUPPORT (SKATE ANGLE) WAS REPLACED PER B757-200 SRM. (0836046)

Part: FLOOR SUPPORT — CRACKED (BS 680-700) · airframe 63,492 hrs · 23,574 cycles

SHIP 6703 CRACK ON FASTENER HOLE OF INTERCOSTAL BTW FS STA: 680-700 AND RBL 45 AT PAX CABIN. CORRECTIVE ACTION: IN REFERENCE NRC 00568 INTERCOSTAL ANGLE BTW FS STA: 680-700 AND RBL 45 AT PAX CABIN. WAS REPLACED PER B757-200 SRM. (0835202)

Part: FLOOR SUPPORT — CRACKED (BS 1320-1340) · airframe 63,492 hrs · 23,574 cycles

SHIP 6703 CRACKED INTERCOSTAL ON CEILING AREA BL 0 BTW STA 1320 AND 1340 AT AFT CARGO COMPARTMENT (C2). CORRECTIVE ACTION: SUMMARY IN REF NRC 00135 ANGLE OF THE INTERCOSTAL AREA BL 0 BTW STA 1320 AND 1340 AT AFT CARGO COMPARTMENT (C2) WAS REPLACED PER B757-200 SRM. (0832499)

Part: FLOOR SUPPORT — CRACKED (BS 405) · airframe 63,492 hrs · 23,574 cycles

SHIP 6703 INITIAL INSPECTION. CRACK ON INTERCOSTAL UPPER SIDE FS STA: 405 AND BL 0 AT PAX CABIN. CORRECTIVE ACTION: NRC 329: INTERCOSTAL WAS REPAIRED PER B757-200 SRM, (ET) (HFEC) INSPECTION WAS ACCOMPLISHED ON INTERCOSTAL UPPER SIDE FS STA: 405 AND BL 0 AT PAX CABIN. NO CRACKS WERE FOUND AFTER CUT OUT PER B757 NDTM. (0832190)

Part: FLOOR SUPPORT — CRACKED (BS 678) · airframe 63,492 hrs · 23,574 cycles

SHIP 6703 INITIAL INSPECTION: CRACK ON STRINGER RBL 16.10 AND STA 678 ALSO MISSING FASTENERS ON STRINGER SUPPORT AT FWD CARGO COMPARTMENT (C1). CORRECTIVE ACTION: IN REFERENCE NRC S/N 00261 STRINGER RBL 16.10 AND STA 678 WAS REPLACED PER B757-200 SRM. (0830036)

Part: LENS — DAMAGED (SLIDE INDICATOR) · airframe 63,472 hrs · 23,566 cycles

SLIDE INDICATOR LIGHT WAS DAMAGED. REPLACED THE LENS, CHECKED GOOD.

Part: SPRING — DEFECTIVE (SLIDE LIGHT) · airframe 63,297 hrs · 23,481 cycles

SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:112 / INTERIOR. REPLACED TORSION SPRING REF CMM 25-24, OPS NML.

Part: BUSTLE — DETACHED (EVAC SLIDE) · airframe 63,034 hrs · 23,343 cycles

R1 DOOR WILL NOT ARM. FOUND BUSTLE FALLEN OFF, RE-ATTACHED R1 BUSTLE AND PERFORMED OPS CHK PER AMM 25-66. OPS CHKS NORMAL. CLEANED GIRT BAR ASSY. OK FOR SVC.

Part: DOOR — OBSTRUCTED (R1) · airframe 62,947 hrs · 23,307 cycles

(AIRCRAFT 6703, L/P 3913404) DOOR R1 WILL NOT ARM. REMOVED DEBRIS. OPS CKS NML.

Part: FITTING — OBSTRUCTED (GIRT BAR) · airframe 62,580 hrs · 23,190 cycles

DOOR 1 RIGHT WILL NOT ARM. REMOVED DEBRIS FROM GIRT BAR FITTING OK FOR SERVICE.

Part: VALVE — MALFUNCTIONED (SLIDE BOTTLE) · airframe 60,920 hrs · 22,600 cycles

RT OVERWING SLIDE FAILED A DEPLOYMENT TEST. FOUND THE BOTTLE VALVE TO HAVE MALFUNCTIONED. REPLACED THE BOTTLE AND SLIDE IAW SPC 56-2560-9-0002, AND SPC 55-2560-9-0016.

Part: FRAME — GOUGED (BS 620) · airframe 63,617 hrs · 23,623 cycles

SHIP 6703 WHILE IN FOR THE 2KU WIFI MOD AND DURING THE RADOME INTERCOSTAL INSTALLATION PER GOGO DRAWING REV. C (REFERENCE AMDS WORKCARD) AT STA 620 BETWEEN STR 2R AND 3R, MTC REPORTED SIX (6) EXISTING FASTENER HOLES IN THE FRAME WHERE THE INTERCOSTAL T-CLIP IS TO BE INSTALLED. ADDITIONALLY, SEVERAL GOUGES WERE REPORTED ON THE FRAME WEB AND THE UPPER FLANGE. CORRECTIVE ACTION: REF ERA563816-14 REV A. (0320887)

Part: STRUCTURE — DAMAGED (BS 680) · airframe 63,773 hrs · 23,669 cycles

WHILE IN FOR THE 2KU WIFI MODIFICATION AND DURING THE RADOME INSTALLATION PER GOGO DRAWING REV. C (REFERENCE AMDS WORKCARD) AT FS 680 AT STR 3R, MTC REPORTED SIX (6) EXISTING OVERSIZED FASTENER HOLES. REF ERA 563820-14 REV A.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 57,705 hrs · 21,541 cycles

EMERGENCY LIGHT AT SEAT 30D IS INOPERATIVE. RECONNECTED ELECTRICAL CONNECTOR FOR THE LIGHTAT 30D. EMERGENCY LIGHT TESTED SATISFACTORY.

Part: COVER — BROKEN (R2 DOOR) · airframe 57,473 hrs · 21,457 cycles

R2 DOOR ARM - DISARM HINGE COVER BROKEN. REMOVED AND REPLACED THE HINGE COVER AND SPRING IAW AMM 52-11. OPS CHECKED GOOD. OK FOR SERVICE.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 56,979 hrs · 21,288 cycles

1R DOOR WILL NOT DISARM. RMVD PLASTIC STICK FROM UNDER GIRT BAR. ARMS/DISARMS OK.

Part: SHAFT — UNDERSIZE (MOUNT) · airframe 57,908 hrs · 21,612 cycles

DURING THE ACCOMPLISHMENT OF CMM 310N3020 (71-21-15) REPAIR 1-2, THE SHAFT END JOURNAL OF THE FORWARD ENGINE MOUNT BEAM REQUIRED MACHINING BELOW THE REPAIRABLE LIMIT IN ORDER TO COMPLETELY REMOVE PREVIOUS CHROME PLATING. THE SHAFT END JOURNAL OF THE PART MEASURES 1.965 INCHES AFTER REMOVAL OF ALL CHROME PLATE. AS A RESULT, THE SHAFT END JOURNAL BELOW THE MINIMUM REPAIRABLE LIMITS IAW SRM, REPAIR 1 AND BELOW THE MINIMUM REPAIRABLE LIMITS IAW CMM 71-21-15, REPAIR 1-2. EA AUTHORIZES THE ACCEPTANCE OF THE UNDERSIZE SHAFT END JOURNAL DIAMETER AND APPLICATION OF A NICKEL-CHROME REPAIR IN ORDER TO RETURN THE ENGINE MOUNT BEAM TO ROUTINE SERVICE AND MAINTENANCE. ERA 556209-14.

Part: GROUND STUD — UNSECURE (EMERGENCY LIGHTS) · airframe 53,343 hrs · 19,934 cycles

EMERGENCY LIGHTS ON WITH COCKPIT SWITCH IN OFF POSITION AND ALSO ILLUMINATED WITH SIDEWALL LIGHT FROM FWD ATTEND SEAT. R & R FWD ATTEND PANEL ALSO REPLACED BATTERY PACK 2, M730, M731, M732 , M733, M736, M737 BATTERIES. FOUND EMERGENCY AFT TEST SW S10295 DISCONNECTED. RECONNECTED SWITCH. FOUND BAD GROUND ON GD3402-DC. SECURED STUD AND LUG IAW SPWM CHAPT 20 AND WDM 33-51. OPS CK GOOD. OK FOR SERVICE.

Part: FUSE — OPEN (EMERGENCY LIGHT) · airframe 53,337 hrs · 19,929 cycles

EMERGENCY SEAT LIGHTS BETWEEN ROWS 23-26 DO NOT COME ON. FOUND TWO FUSES TO BE OPEN. R & R 2 EACH FUSES AT POWER SUPPLY M10567 IN REF TO AMM.

Part: STRAP — CRACKED (BS 377) · airframe 53,337 hrs · 19,929 cycles

ON OK TO CLOSE FLOOR PANELS IN FWD CABIN, FOUND STABILIZATION STRAP CRACKED AND SEVERED AT BS 377, LBL-45. REMOVED DAMAGE AREA AT BS 377, LBL 45 IAW SRM 53-00-51, REPAIR 12. CUT OUT LENGTH, L=1.88" FINAL, ACCOMPLISHED HFEC AND OPEN HOLE INSP. NO DAMAGE NOTED, FABRICATED REPAIR PARTS IAW SRM 53-00-51, REP 12. TABLE 201, TREATED AND PRIMED REPAIR PARTS IAW SRM 51-20-01, PAGE 6 AND 26N, AND INSTALLED REPAIR PARTS AT BS 377, LBL 45 IAW SRM 53-00-51, REPAIR 12 INSTALLED ID TAG IAW TOPP 30-10-70, PG 13.

Part: SEAL — CRACKED (NR 1 NACELLE) · airframe 52,984 hrs · 19,811 cycles

NR 1 PYLON AFT FIRE SEAL CRACKED. REMOVED AND DRILLED NEW FIRE SEAL IAW DWG. BEGAN INSTALLING NEW FIRE SEAL IAW DWG VERTICAL FASTENERS NEED INSTALLED, COMPLETED INSTALLATION IAW DWG.

Part: WARNING MESSAGE — ILLUMINATED (SPOILERS) · airframe 52,379 hrs · 19,592 cycles

PERFORMED A REJECTED TAKEOFF AT LESS THAN 10 KNOTS DUE TO A SPOILER EICAS MESSAGE. PCA FAULT ON SCM 1R WILL NOT RESET.

Part: SKIN — DENTED (BS 620) · airframe 57,655 hrs · 21,524 cycles

FUSELAGE SKIN BS 620 STRINGER 16L DENTED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,061 hrs · 18,382 cycles

EMERGENCY EXIT SIGN AT R2 DOOR FAILED TO ILLUMINATE DURING TEST. REPLACED BATTERY PACK AND POWER SUPPLY IAW AMM 33-51. TESTED GOOD.

Part: SKIN — DENTED (BS 620) · airframe 49,974 hrs · 18,718 cycles

RAMP REPORTED A DENT AT BS 620 S16L. COMPLIED WITH REPAIR INSTRUCTIONS IAW RI 525762-14. DVI OF DENT AND STRINGERS PERFORMED. NO FURTHER DAMAGE NOTED. PERFORMED HFEC SURFACE SCAN INSPECTION OF DAMAGE IAW REPAIR INSTRUCTIONS 525762-14. NO CRACK INDICATORS EXIST. REPAIRED IAW ERA 525762-14, REV B,

Part: FUSE — FAILED (EMERGENCY LIGHT) · airframe 48,759 hrs · 18,264 cycles

RT WING EMERGENCY LIGHT INOPERATIVE. REPLACED FUSE IN BATTERY PACK ASSY. OPS CHECKED GOOD. OK FOR SERVICE.

Part: SKIN — DAMAGED (BS 526) · airframe 51,104 hrs · 19,126 cycles

LIGHTNING STRIKE AT BS 526, .7500" BELOW S23R. REMOVED BLIND FASTENER IAW SRM. REPAIRED IAW SRM.

Part: GROUND WIRE — BROKEN (EMERGENCY LIGHT) · airframe 45,240 hrs · 17,061 cycles

FLT CREW REPORTS LEFT WING FWD EMERGENCY OVERWING EXIT LOWER LIGHTS OUT. FOUND EXIT LIGHT ASSY MISSING AND GROUND WIRE BROKEN. REPLACED GROUND WIRE AND LIGHT ASSY. OPS NORMAL.

Part: FRAME — DENTED (BS 540 S25-26L) · airframe 44,463 hrs · 16,783 cycles

FWD CARGO BS 540, BETWEEN STR 25L-26L TOP OF FRAME IS DENTED. ACCOMPLISHED ERA 510128-14 REV ORIG, (TO 115).

Part: FLOORBEAM — CORRODED (BS 365 RBL 45) · airframe 44,463 hrs · 16,783 cycles

FLOORBEAM CORRODED ON UPPER SURFACE BS 365, RBL 45. REPAIRED ERA 510970-14 REV ORIG.

Part: SKIN — DENTED (BS 1450 S28-29R) · airframe 44,463 hrs · 16,783 cycles

RT AFT EXTERIOR FUSELAGE SKIN HAS THREE DENTS BETWEEN BS 1450 TO 1460 S28-29R. REPAIRED IAW ERA 510135-14, REV ORIG.

Part: BULKHEAD — GOUGED (BS 1885 RBL 8) · airframe 44,463 hrs · 16,783 cycles

APU COMPARTMENT FWD BULKHEAD BS 1885, RBL 8. REPAIRED IAW SRM 53-80-08.

Part: SKIN — PUNCTURED (RT WING TE FLAP) · airframe 44,463 hrs · 16,783 cycles

RT WING INBD MAIN FLAP LOWER SURFACE HAS A PUNCTURE. ACCOMPLISHED ERA 510954-14, ORIG.

Part: TEE FITTING — CRACKED (BS 1681.8) · airframe 44,463 hrs · 16,783 cycles

TEE FITTING CRACKED, REPLACED TEE FITTING IAW EA 06-465922-03.

Part: FRAME — DENTED (BS 1460 S26L) · airframe 44,463 hrs · 16,783 cycles

FRAME IN AFT CARGO IS DENTED AT BS 1460 ABOVE STR 26L AT UPPER FLANGE. REPAIRED IAW REPAIR 5, PG 204.

Part: FRAME — DENTED (BS 1460 S26L) · airframe 44,463 hrs · 16,783 cycles

FRAME IN AFT CARGO DENTED AT STA 1460 ABOVE STR 26L AT UPPER FLANGE. ACCOMPLISHED SRM 53-00-07, FIG 201, REPAIR 5.

Part: FRAME — DENTED (BS 1400 S26L) · airframe 44,463 hrs · 16,783 cycles

FRAME IN AFT CARGO IS DENTED AT STA 1400, ABOVE STR 26L AT UPPER FLANGE. REPAIR ACCOMPLISHED IAW SRM 53-00-07, FIG 201, REPAIR 5.

Part: FRAME — DENTED (BS 1480 S26L) · airframe 44,463 hrs · 16,783 cycles

FRAME IN AFT CARGO IS DENTED AT 1480 ABOVE STR 26L UPPER FLANGE. ACCOMPLISHED REPAIR IAW SRM 53-00-01, REPAIR 5.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,379 hrs · 16,741 cycles

EMERGENCY LIGHTS FROM ROW 38D TO 45D WOULD NOT TEST. MX REPLACED BATTERY PACK M11649 IAW AMM 35-51. OPS OF LIGHTS CHECKED OK.

Part: BOTTLE — EMPTY (L4 DOOR ASSIST) · airframe 42,569 hrs · 16,025 cycles

DURING CABIN SERVICE THE LEFT SLIDE FELL OUT FROM STOWAGE AND THE DOOR ASSIST BOTTLE WAS DISCOVERED TO BE AT ZERO PSI. REMOVED AND REPLACED THE L4 DOOR SLIDE AND REMOVED AND REPLACED THE L4 DOOR EMERGENCY POWER RESERVOIR.

Part: SKIN — DAMAGED (BS 520) · airframe 42,549 hrs · 16,016 cycles

DURING INSPECTION MAINTENANCE DISCOVERED A BURN MARK AT BS 520 BETWEEN STR 6 AND 7. MAINTENANCE REMOVED THE DAMAGE, INSPECTED. NO FAULTS NOTED AND INSTALLED BLIND FASTENERS.

Part: SKIN — DAMAGED (BS 268) · airframe 42,549 hrs · 16,016 cycles

MAINTENANCE DISCOVERED A BURNED LOCK FASTENER AT BS 268 JUST FWD OF NLG DOORS. REMOVED DAMAGED LOCK FASTENER AND INSPECTED, NO DAMAGE FOUND. REPLACED FASTENER REFERENCE SRM 53-00-01.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 42,549 hrs · 16,016 cycles

MAINTENANCE PERFORMED INSPECTION, DUE TO LIGHTNING STRIKE ON THE GROUND. MAINTENANCE DISCOVERED AND REPAIRED DAMAGE PER SRM 53-00-01.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,773 hrs · 15,720 cycles

LINE MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE AT SEAT 32C AND 34D. REPLACED BATTERY PACK AND CHARGER, ALL LIGHTS OPERATION NORMAL.

Part: BALLAST — OVERHEATED (CABIN LIGHTS) · airframe 37,793 hrs · 14,240 cycles

WHILE ON APPROACH A STRONG ELECTRICAL/BURNED PLASTIC SMELL WAS REPORTED. CREW TURNED OFF THE RECIRCULATION FANS AND THE SMELL DISSIPATED SOON AFTER THE ACFT LANDED. MX FOUND A LIGHT BALLAST INOPERATIVE AND MEL'D THE SAME. REPLACED BALLAST. LIGHTS OPERATE NORMALLY.

Part: SKIN — DENTED (FS 710-740) · airframe 34,757 hrs · 13,290 cycles

C/W ERA 472193-14 REV B CODE 6-53-31-20 ACTL2200. REWORKED DENTS AT SKIN FS 710-740 S24R IAW SRM 51-70-01 WITHIN LIMITS IAW SRM 53-00-01. REMOVED DAMAGE AT 2 LOCATIONS IAW PRI 472193-14 REV 0 MADE CUTOUTS IAW SRM 53-00-01 REPAIR 2. REPAIRED IAW PRI 472193-14 REV 1. ERA 472193-14 REV C MATCHES PRI 472193-14 REV 1.

Part: FLOOR SUPPORT — TOOL DAMAGE (BS 594)

FLOOR SUPPORT STRINGER HAS DRILL BIT DAMAGE BS 594 LBL 11 FWD CARGO COMPT. CUT OUT DRILLED SECTION OF FLOOR SUPPORT, FABRICATED AND INSTALLED 2 ANGLES 9" BY 1" BY 1" FROM 7075-T6 .050" AND 2 ANGLES 10" BY 1" BY 1" FROM 2024-T3 .040" IAW B757 SRM 51-70-12, FIG 1.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 18,219 hrs · 8,045 cycles

SEAT 18 RT EMERGENCY PATH LIGHT INOP. REPAIRED BROKEN WIRE IN SIDEWALL.

Part: FUEL CONTROL — MALFUNCTIONED (NR 2 ENGINE) · airframe 16,188 hrs · 7,248 cycles

AT FL 370 ENG INSTRUMENTS APPEARED FROZEN ENG WOULD NOT ACCELERATE ABOVE 65 PERCENT, N1 ENG WOULD IDLE DOWN. DIVERTED TO CVG. REPLACED FUEL CONTROL AND FUEL PUMP. LEAK CKS OK, ENG TEST OK PER PFHB AND M/M.

Part: WIRE — CHAFED (NR 2 ENGINE) · airframe 15,998 hrs · 7,177 cycles

NR 2 ENG ROLLED BACK TO APPROX 63 PERCENT N1 AT FL 410, WOULD NOT ACCELERATE NORMALLY AFTER THROTTLE RETARDED AND THE ADVANCED ENGINE STAYED ROLLED BACK UNTIL DESENDING BELOW 10,000 FT MSL AND THEN OPERATED NORMALLY FOR THE REST OF THE FLIGHT THROUGH LANDING. REPAIRED CHAFED WIRING AND REPLACED PDIU.

Part: WIRE HARNESS — DISCONNECTED (CABIN) · airframe 12,534 hrs · 5,864 cycles

FOUND ON INSPECTION SEAT 34D EMERGENCY TRACK LIGHTING INOP. FOUND SEAT HARNESS DISCONNECTED. RECONNECTED HARNESS LIGHT, OPS GOOD.

Part: LIFE RAFT — DEPLOYED (CABIN) · airframe 11,227 hrs · 5,362 cycles

FORWARD CABIN LIFE RAFT PARTIALLY INFLATED DURING FLIGHT, CAUSING SOME SHEET METAL DAMAGE TO THE LIFE RAFT COMPARTMENT. REPAIRED COMPARTMENT AND REPLACED RAFT.