N668DN

Part: SEQUENCE VALVE — INOPERATIVE (ZONE 700) · airframe 96,183 hrs · 45,415 cycles

SHIP 0668 -ATB- DUE TO LEFT MAIN LANDING GEAR WOULD NOT RETRACT. CORRECTIVE ACTION: ADJ LH MLG DOOR ACTUATOR, REMOVED AND REPLACED LT MLG DOOR, REMOVED AND INSTALLED SEQUENCE VALVE FOR MLG, REMOVED AND REPLACED LINKAGE, AND C/W GEAR DOOR ADJ. EXT/RETRACTION GOOD.

Part: PRESSURE DECK — CORRODED (ZONE 100) · corrosion level 2 · airframe 95,904 hrs · 45,222 cycles

SHIP 668 FUSELAGE / MAIN FRAME / LH LANDING GEAR / PRESSURE DECK WEB, STA 1080 TO 1180 & LBL 8.20 TO LBL 70 / CORROSION. ER/A 498884-14 REV C REQUIRES SECTION II. CORRECTIVE ACTION: ER/A 498884-14.

Part: PANEL — ODOR (ZONE 200) · airframe 95,869 hrs · 45,200 cycles

SHIP 668 ELECTRICAL BURNING SMELL DETECTED IN THE COCKPIT. SMELL IS NOTICED NEAR THE ENTRANCE OF THE COCKPIT BY MULTIPLE CREW MEMBERS. CORRECTIVE ACTION: FOUND OVERHEAD AUX ANNUNCIATOR PANEL TO HAVE SMELL. R&R'D PANEL I/A W B-757 AMM 33-16-71. OPS CK GOOD. (5889412)

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 95,466 hrs · 44,918 cycles

SHIP 668 1R DOOR WILL NOT FULLY ARM. ARM LVR DOES NOT MOVE TO THE FULL ARM POSITION. SLIDE LIGHT DOES NOT ILLUMINATE. CORRECTIVE ACTION: ADJUSTED GIRT BAR MECHANISM PER B757 AMM 52-11. OPS CHK GOOD. (5606784)

Part: GIRT BAR — INTERFERENCE (R1 DOOR) · airframe 95,466 hrs · 44,918 cycles

SHIP 668 R1 DOOR RESISTANCE ENGAGING SLIDE. CORRECTIVE ACTION: PERFORMED GVI. FOUND GIRT BAR STRAP INTERFERENCE. POSITIONED STRAP. OPS CHECK GOOD PER B757 AMM 25-66. (5606782)

Part: PROXIMITY SWITCH — FAULTED (R1 GIRT BAR) · airframe 95,417 hrs · 44,896 cycles

SHIP 668 1R GIRT BAR ARMED LIGHT INOP. CORRECTIVE ACTION: R/R FWD AND AFT R1 GIRT BAR PROX SWITCH. ADJUSTED GIRT BAR CATCH PER B757 AMM 25-66. OPS CKS GOOD. (5606722)

Part: HANDLE — LACK OF LUBE (PARKING BRAKE) · airframe 95,144 hrs · 44,723 cycles

SHIP 0668 -ATO- T/O CONFIG WARNING FOR PARKING BRAKE. CORRECTIVE ACTION: CLEANED AND LUBED PARKING BRAKE HANDLE. (LP 5384868)

Part: DOOR — UNKNOWN (R1) · airframe 94,876 hrs · 44,560 cycles

SHIP 668 UNABLE TO DISARM THE 1R DOOR. CORRECTIVE ACTION: CYCLED DISARMED LEVER SEVERAL TIMES. OPS CHKS NML. (5835388)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 94,876 hrs · 44,560 cycles

SHIP 668 FOUND AFT LEFT SECTION OF EMERGENCY LTS INOP. CORRECTIVE ACTION: REPLACED M736 AFT LEFT EMER LT BATTERY PACK AND CHARGER PER B757 AMM 33-51. NOW OPS CK GOOD. (5835380)

Part: LIGHT — INOPERATIVE (R1 DOOR SLIDE) · airframe 94,605 hrs · 44,388 cycles

SHIP 668 1R SLIDE LIGHT WILL NOT ILLUMINATE. CORRECTIVE ACTION: VERIFIED GIRT BAR ENGAGEMENT-OK IAW B757 AMM 33-22. OPS CHL GOOD INDICATIONS NML. (5598814)

Part: CONTROL UNIT — ODOR (CABIN) · airframe 94,566 hrs · 44,359 cycles

SHIP 668 WHILE AT CRUISE ABOUT 20 MINUTES AFTER T/O PAX IN 1L SAID HE SMELLED SMOKE. AT THE SAME TIME ALL LEFT SIDE IFE/ TV MONITOR WENT BLANK. FA DIDNT SMELL THE SMOKE. THE PAX DIDNT SMELL IT EITHER ANYMORE. WE TURNED OFF IFE FROM FA STATION. CORRECTIVE ACTION: R/R AMCU AND SPM. UPON IFE ACTIVATION NO SMELL, ARCING OR SMOKE IAW B757 AMM 23-82 OPS CK NML. (5083692)

Part: GIRT BAR — FOD (R2 DOOR) · airframe 94,469 hrs · 44,302 cycles

SHIP 668 2R DOOR WILL NOT DISARM. CORRCTIVE ACTION: INSPECTED THE 2R GIRT BAR SENSORS AND FOUND DEBRIS INCLUDING METAL. CLEANED SENSORS PER B757 AMM 52-71-00 AND DOOR SLIDE INDICATION NOW OPS CHECKS GOOD. (5083628)

Part: GIRT BAR — FOD (DOOR SLIDE) · airframe 94,451 hrs · 44,287 cycles

SHIP 668 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:602. CORRECTIVE ACTION: REMOVED DEBRIS FROM GIRT BAR AREA. SLIDE LIGHT NOW CKS NORMAL. (0158919)

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 94,434 hrs · 44,280 cycles

SHIP 668 R1 DOOR SLIDE LIGHT NOT ILLUMINATED WHEN DOOR ARMED. CORRECTIVE ACTION: FOUND GIRTBAR LOOSE, RE ATTACHED PER B757 AMM 25-66. OP CHECKED GOOD (5083614)

Part: INDICATOR — OUT OF ADJUST (R4 DOOR) · airframe 94,434 hrs · 44,280 cycles

SHIP 668 DR4 609 DOOR ARMED KNUCKLE KNOCKER INOP. CORRECTIVE ACTION: ADJUSTED DOOR TRIM AND OPS NOW NORMAL. (5083617)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,047 hrs · 44,017 cycles

SHIP 0668 4R DOOR SLIDE ARM/DISARM HANDLE HARD TO OPERATE. CORRECTIVE ACTION: THE GIRT BAR MECHANISM ON DOOR R4 WAS ADJUSTED PER B757-200 AMM 52-11. HANDLE OPERATE CORRECTLY. (4915688)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,047 hrs · 44,017 cycles

SHIP 0668 2L DOOR SLIDE LIGHT DOES NOT TURN ON WITH DOOR ARMED. CORRECTIVE ACTION: GIRT BAR PROXIMITY SENSOR AT 2L DOOR WAS REPLACED PER B757-200 AMM 25-66. SLIDE LIGHT DOES TURN ON WITH DOOR ARMED TEST OK. (4915687)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,043 hrs · 44,015 cycles

SHIP 0668 FUSELAGE / AFT CARGO FRAME / AT STA 1300 / S-24L & S-26L / EXISTING REPAIR. CORRECTIVE ACTION: SUMMARY OF NRC 00112: AFT CARGO FRAME AT STA 1300 BTW S-24L AND S-26L WAS REPAIRED PER ER/A 612100-14AD REV. ORIGINAL SECTION I. (0025922)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,043 hrs · 44,015 cycles

SHIP 0668 FUSELAGE / AFT CARGO FRAME / STA 1300 / S-24L & S-26L / EXISTING REPAIR. CORRECTIVE ACTION: REF ERA 61200-14. (0025665)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,043 hrs · 44,015 cycles

SHIP 0668 FUSELAGE / EXTERNAL SKIN / BTW STA 760 & STA 780 / BTW S18R & S19R / CORROSION. CORRECTIVE ACTION: REF ERA 612228-14. (0023603)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 94,043 hrs · 44,015 cycles

SHIP 0668 IN REF TO: NRC 00210: AFTER REMOVE CORROSION AREA WAS FOUND AREA OUT LIMITS, STA 760 AND 780 BTW S-19R AND S-18R OF FUSELAGE SKIN. CORRECTIVE ACTION: SUMMARY OF NRC 00502: EXTERNAL FUSELAGE SKIN ON STA 760/780 BTW S-19R AND S-18R WAS REPAIRED PER ER/A 612228-14AD. (0024019)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,043 hrs · 44,015 cycles

SHIP 0668 DTE, 612228-14AD FUSELAGE SKIN CORROSION. CORRECTIVE ACTION: REF ERA 612228-14AD. (0023592)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,043 hrs · 44,015 cycles

SHIP 668 A.D.//A.A. DAMAGES WERE FOUND ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #11 CORROSION ON SKIN AND FITTING BTW 2 TO 4 O CLOCK POSITION, HOLE #12 CORROSION ON SKIN AND FITTING BTW 2 TO 4 O CLOCK POSITION, HOLE #13 CORROSION ON SKIN AND FITTING BTW 9 TO 11 O CLOCK POSITION, HOLE #14 CORROSION ON SKIN AND FITTING BTW 10 TO 11 O CLOCK POSITION, HOLE #16 CORROSION ON SKIN AND FITTING BTW 10 TO 12 O CLOCK POSITION, HOLE #17 CORROSION ON FITTING BTW 12 TO 1 O CLOCK POSITION, HOLE #18 CORROSION ON SKIN AND FITTING BTW 9 TO 11 O CLOCK POSITION, IN REF. CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00187:[ A.D.//A.A] RH ENG DRAG FTG CLAMP-UP HOLES , #12, #13, #14, #16, #17 WERE REPAIRED PER CARD 5720-01100-05B AND HOLES #11 AND #18 WERE REPAIRED PER PRI 612008-14 REV. 1 AND ERA 612008-14AD REV. ORIGINAL SECTION I. (0012774)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,043 hrs · 44,015 cycles

SHIP 668 A.D.//A.A. DAMAGES WERE FOUND ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #1 CORROSION ON SKIN AND FITTING BTW 5 TO 7 O CLOCK POSITION, HOLE #3 CORROSION ON SKIN AND FITTING BTW 1 TO 5 O CLOCK POSITION, HOLE #6 CORROSION ON SKIN AND FITTING BTW 8 TO 10 O CLOCK POSITION, HOLE #7 SCRATCH ON FITTING BTW 4 TO 7 O CLOCK POSITION, HOLE #10 CORROSION ON SKIN AND FITTING BTW 7 TO 8 O CLOCK POSITION, IN REF. CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00188: [ A.D.//A.A] RH ENG DRAG FTG CLAMP-UP HOLES #1, #3, #6, #7 AND #10 WERE REPAIRED PER CARD 5720-01100- 04B AND FASTENERS WERE INSTALLED PER PRI 612008-14 REV. 1 AND ERA 612008-14AD REV. ORIGINAL SECTION I. (0012931)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,043 hrs · 44,015 cycles

SHIP 668 DTA MONITOR INSPECTION LOG REF ERA 612253-14 CORROSION WAS FOUND AFFECTING THE EXTERNAL SKIN PANEL BETWEEN STA 740 & STA 760, AND BETWEEN S-20R & S-21R. CORRECTIVE ACTION: REF ERA 612253-14. (0011038)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 94,043 hrs · 44,015 cycles

SHIP 0668 CORROSION AREA WAS FOUND AREA OUT LIMITS, STA 760 TO 740, BTW S-21R TO S-20R OF FUSELAGE SKIN. CORRECTIVE ACTION SUMMARY OF NRC 00503, FUSELAGE SKIN AT STA 760 TO 740, BTW S-21R TO S-20R WAS REPAIRED PER ER/A 612253-14. (0011325)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,043 hrs · 44,015 cycles

SHIP 0668 NICK ON EXTERNAL FUSELAGE SKIN BTW STA 520- 540 LONGERON 28-29LH, STA 540-550 LONGERON 28-29LH. CORRECTIVE ACTION SUMMARY OF NRC 00047: EXTERNAL FUSELAGE SKIN BTW STA 520-540 LONGERON 28-29LH WAS REPAIRED PER ERA 612199-14. (0003288)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,043 hrs · 44,015 cycles

SHIP 0668 757/ FUSELAGE / STA 620 - STA 640/ S-14L AND S-19L / DENTS AND REPAIR. CORRECTIVE ACTION REF ERA 498881-14. (0003269)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,043 hrs · 44,015 cycles

SHIP 0668 B757-200 / FUSELAGE / SKIN / STA 520-540, S- 27L TO S-28L / NICKS. CORRECTIVE ACTION REF ERA 612199-14. (0001220)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,043 hrs · 44,015 cycles

SHIP 0668 WINGS / OUTER WING / RHS UPPER SKIN AND DRAG FITTINGS / CORROSION. CORRECTIVE ACTION REF ERA 612008-14. (0001384)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,043 hrs · 44,015 cycles

SHIP 0668 NRC 00210, AFTER REMOVE CORROSION AREA WAS FOUND AREA OUT LIMITS, STA 760 TO 780 BTW S-28R TO S-29R OF FUSELAGE SKIN. CORRECTIVE ACTION SUMMARY OF NRC 00504: FUSELAGE SKIN AT STA 760 TO 780 BTW S-28R TO S-29R WAS REPAIRED PER ER/A 612274-14. (0000619)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,043 hrs · 44,015 cycles

SHIP 0668 FUSELAGE / STA 620- STA 640 / S-14L AND S19L / DENTS AND REPAIR. CORRECTIVE ACTION REF ERA 498881-14AD. (0001378)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,043 hrs · 44,015 cycles

SHIP 0668 FUSELAGE / SKIN / STA 760 TO 780 & S-27R TO 28R / CORROSION. CORRECTIVE ACTION REF ERA 612274-14. (2999640)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,043 hrs · 44,015 cycles

SHIP 0668 AD, AA - 01 DISBOND OF 6.25IN LENGTH AND 3.5IN WIDTH AT OSS 305.5 WAS FOUND ON LOWER SKIN OF SLAT 7 TRAILING EDGE WEDGE IN REFERENCE TO JOB 126-0001/CARD 5740-01145-05G. CORRECTIVE ACTION: SUMMARY OF NRC 00019: LOWER SKIN OF SLAT 7 TRAILING EDGE WEDGE WAS REINSPECTED AND NO DISBONDS WERE FOUND PER B757 NDT MANUAL 51-00-01. (2996625)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,043 hrs · 44,015 cycles

SHIP 0668 AD//AA - DISBOND WAS FOUND ON UPPER SKIN OF SLAT 7 TRAILING EDGE WEDGE: DISBOND 7.5IN LENGTH AND 3.75IN WIDTH AT OSS 305.5 (IN REFERENCE TO JOB 126-0001/CARD 5740-01145-05G). CORRECTIVE ACTION: SUMMARY OF NRC 00018: UPPER SKIN OF SLAT 7 TRAILING EDGE WEDGE WAS REPAIRED PER B757-200 SRM 57-43 AND B757-200 SRM 51-70. (2994797)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 94,043 hrs · 44,015 cycles

SHIP 0668 CORROSION ON FLOOR STRUCTURE BTW STA 319 TO STA 322 RBL 4 ITS OUT OF LIMITS. CORRECTIVE ACTION SUMMARY OF NRC 00555: FLOOR STRUCTURE BTW STA 319 TO STA 322 RBL 4 WAS FABRICATED PER B757 DWG 141N5160, BAC 1508-238 AND INSTALLED PER B757-200 SRM 51-40-02. (2991439)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 94,043 hrs · 44,015 cycles

SHIP 0668 CORROSION ON MEMBRANE FROM STA 680 TO STA 700, LBL 63 AND RBL 63 ALSO FROM STA 720 TO STA 740 RBL 63 AT PASSENGER CABIN FLOOR STRUCTURE (W2). CORRECTIVE ACTION SUMMARY OF NRC 00398: MEMBRANE FROM STA 680 TO STA 700, LBL 63 AND RBL 63 ALSO FROM STA 720 TO STA 740 RBL 63 AT PASSENGER CABIN FLOOR STRUCTURE (W2) WERE FABRICATED PER DWG 143N5413, DWG 143N5209 AND INSTALLED PER B757-200 SRM 51-40-02. (2991455)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 94,043 hrs · 44,015 cycles

SHIP 0668 CORROSION ON ANGLE (SILL) UPPER SURFACE BTW STA 730-690 LBL 65 AT L2 AT PAX CABIN. CORRECTIVE ACTION SUMMARY OF NRC 00352: ANGLE (SILL) BTW STA 660 TO STA 755 LBL 65 AT L2 AT PAX CABIN WAS REPLACED PER B757-200 SRM 51-40-02. (2989939)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,043 hrs · 44,015 cycles

SHIP 0668 IN REFERENCE TO NRC. 00430 PREVIOUS REPAIR WAS FOUND ON FLOOR BEAM STA 1640 BTW RBL 15 TO LBL 41 AT W4 AREA (CPAX). CORRECTIVE ACTION: SUMMARY OF NRC 00540: FLOOR BEAM STA 1640 BTW RBL 15 TO LBL 41 AT W4 AREA (CPAX) WAS REPAIRED PER B757-200 SRM. (2983089)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,043 hrs · 44,015 cycles

SHIP 0668 CRACK ON STIFFENER BWT STA 560 LBL 45 AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00411: STIFFENER BWT STA 560 LBL 45 WAS REAPIRED PER B757-200 SRM 53-00-51. (2984177)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,043 hrs · 44,015 cycles

SHIP 0668 LOW PRESSURE ON R1 DOOR EMERGENCY RESEVOIR AT PAX CABIN. CORRECTIVE ACTION SUMMARY OF NRC 00229: LOW PRESSURE R1 DOOR EMERGENCY RESERVOIR WAS REPLACED BY SERVICEABLE DOOR EMERGENCY RESERVOIR PER B-757 IPC 52-11-40-51A ITEM - 001 AND MUST BE INSTALLED PER JOB CARD 5211-3001-1R. (2982120)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 94,043 hrs · 44,015 cycles

SHIP 0668 DAMAGES WERE FOUND ON OPEN HOLE AT LH ENG DRAG FTG CLAMP-UP & DRAG BRACE AS FOLLOW: HOLE NO.3 CORROSION AND SCRATCHES ON SKIN AND FITTING BTW 1 TO 5 O CLOCK POSITION. CORRECTIVE ACTION SUMMARY OF NRC 00178: HOLE # 3 WAS REAMED TO DIAMETER 0.5780" PER CARD 5720-01100-04A. (2980624)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,043 hrs · 44,015 cycles

LENGTH OUT OF LIMITS (PIN EXTENSION) OF ROTARY SNUBBER AT 1R DOOR. CORRECTIVE ACTION: THE ROTARY SNUBBER AT R1 DOOR WAS REMOVED PER B757-200 AMM 52-11. SUMMARY OF NRC 00065, THE ROTARY SNUBBER AT 1R DOOR WAS REPLACED PER B757 AMM 52-11.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,043 hrs · 44,015 cycles

SHIP 668 LENGTH OUT OF LIMITS (PIN EXTENSION) OF ROTARY SNUBBER AT 4R DOOR. (IN REF AMDS). CORRECTIVE ACTION: SUMMARY OF NRC 00063: ROTARY SNUBBER AT 4R DOOR WAS REPLACED PER B757-200 AMM 52-11. (2977897)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,043 hrs · 44,015 cycles

SHIP 0668 PREVIOUSLY REPAIR ON FUSELAGE SKIN FROM BSTA 440 TO BSTA 550 BTW S13 & S15 LH, SEVERAL RIVETS WRONG INSTALLED INTERNAL SIDE. CORRECTIVE ACTION: REF ERA 498897.14. (2976344)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,016 hrs · 43,994 cycles

SHIP 0668 R1 DOOR SLIDE LIGHT WAS NOT LIT. CORRECTIVE ACTION: REMOVED DEBRIS FROM SLIDE LT SENSOR, SLIDE OPS NORM. AS PER B- 757 AMM 52-02. A/C OK FOR SVC. (4915646)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,932 hrs · 43,948 cycles

SHIP 0668 #9 SLAT HAS DISBOND AT T/E I/B SIDE AT PREVIOUS REPAIR PER AMDS 57-40-01145-05L. CORRECTIVE ACTION: REMOVED DOUBLER WHICH HAD DELAMINATION NOTE DURING NDT INSPECTION. CLEANED AREA. READY TO INSTALL NEW DOUBLER PER B757 SRM 57-43-02. (4850194)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 93,387 hrs · 43,620 cycles

SHIP 668 L2 DOOR SLIDE ARM LIGHT INOP. CORRECTIVE ACTION: L2 SLIDE ARM GIRT BAR PROX SW FAULTY. REMOVED AND REPLACED RT HAND PROX SW IN REF W/ B757 AMM 25-66. OPS NML. (4745408)

Part: SKIN — DAMAGED · airframe 92,649 hrs · 43,100 cycles

SHIP 668 L2 DOOR (SKIN DAMAGE) LOWER LEFT CORNER OF DOOR, CATCHES ON DOOR FRAME WHILE OPENING/CLOSING. REMOVED TEMP REPAIR, STEPPED UP HOLES, RPLCD L2 DOOR ASSY ON LOG 9940826 REF AMDS CARD. (9872592)

Part: CONTROLLER — FAULTED (WINDOW HEAT) · airframe 92,054 hrs · 42,742 cycles

RT FWD WINDSCREEN ARC AT LOWER LEFT SIDE. RAN QRH. CRACKED OBSERVED. R/R WINDDOW HEAT CONTROLLER PER B757 AMM 30-41, OPS CK GOOD. R/R RI WINDOW PER B757 56-11 AND SEALANT APPLIED. COMPLETED FINAL TORQUE OF WINDOW. INSTALLATION COMPLETE PER B757 AMM 56-11.

Part: LIGHT — BROKEN · airframe 91,543 hrs · 42,396 cycles

SHIP 668 FOUND ON CABIN WALK THROUGH- SEAT 43DEF HAS A BROKEN EPL ASSEMBLY. CORRECTIVE ACTION: REPLACED BROKEN EPL ASSEMBLY. SWAPPED EMER LIGHT FROM OLD ASSY TO NEW. EMER LIGHTS STILL TEST OK. REPLACED PER CMM. (8969224)

Part: LIGHT — INOPERATIVE · airframe 91,260 hrs · 42,174 cycles

SHIP 668 ON EMERG LIGHTS CHECK FOUND LT OVERWING EMERG AND RT OVERWING EMERG EXIT 1 LIGHT OUT ON EA. SIDE. CORRECTIVE ACTION: RELAMPED LT OVERWING EMERG LITE AND REPLACED FUSE F4 ON M736, OPS CK OK. REF B757 AMM 33-51. (8599354)

Part: TIRE — BLEW OUT · airframe 91,250 hrs · 42,166 cycles

SHIP 668 #5 TIRE BLEW AT GATE DUE TO PARKING BRAKES REMAINING SET AT GATE. CORRECTIVE ACTION: TIRE BLEW DUE TO PARKING BRAKES REMAING SET AND NOT ALLOWING SUFFICIENT COOLING. R/R WHEEL ASSY PER 757 AMM 32-42. (8599342)

Part: PRESSURE SWITCH — LEAKING · airframe 91,195 hrs · 42,144 cycles

SHIP 668 - ATB - DUE TO THE LOSS OF HYD PRESSURE ON THE RT ENG. CORRECTIVE ACTION: INSPECTED FOR ANY LEAKS AND CHECKED THE RIGHT HYD QUANTITY. REPLACED RT HYD SYSTEM PRESSURE SWITCH.

Part: NONE — NONE · airframe 91,172 hrs · 42,125 cycles

SHIP 668 1R SLIDE INDICATOR LIGHT INOP. CORRECTIVE ACTION: SECURED 1R DOOR BUSTLE OPS NML. REF B757 AMM 52-11. (8240570)

Part: GIRT BAR — DIRTY · airframe 91,113 hrs · 42,085 cycles

SHIP 668 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS, 1 R SLIDE LIGHT INOP. CORRECTIVE ACTION: PERFORMED DOOR OP'S CK AFTER AFTER REMOVAL OF DEBRI FROM GIRT BAR MECH. OP'S NML. NO FURTHER FAULTS. (2232022)

Part: NONE — NONE · airframe 90,991 hrs · 42,009 cycles

SHIP 668 ER/A 590828-14 / SECTION II REPEAT INSPECTION. CORRECTIVE ACTION:UPDATE TO REFLECT ER/A IS NOW AT REV C. ACCOMPLISH ER/A 590828- 14AD REV C SECTION II. (2174117)

Part: NONE — NONE · airframe 90,417 hrs · 41,671 cycles

SHIP 668 FLT ATTENDANTS REPORT L2 DOOR EXIT SIGN FELL. CORRECTIVE ACTION: SECURED EXIT SIGN TO LIGHT ASSY. (7893013)

Part: NONE — NONE · airframe 90,417 hrs · 41,671 cycles

SHIP 668 SEAT 42D AISLE EMERG. LIGHT INOP. CORRECTIVE ACTION: FOUND PUSH BACK PIN AT 42D UNDER THE SEAT. RESECURE PIN TO CONNECTOR IAW P.S. 900-9-2 NO.11. OP CHK OK. (7893011)

Part: NONE — NONE · airframe 90,279 hrs · 41,614 cycles

SHIP 668 L EMERGENCY ESCAPE LIGHT ON P61 PANEL WILL NOT LIGHT IN TEST 1. CORRECTIVE ACTION: T/S REF B757 WDM 25-65-11. R/R RELAY K10486 L SLIDE TEST RELAY. OPS CKS GOOD REF B757 AMM 25-65. (7894351)

Part: NONE — NONE · airframe 90,214 hrs · 41,586 cycles

SHIP 668 EMERGENCY EXIT LEFT SQUIB TEST 1 FAILED. CORRECTIVE ACTION: T/S PER B757 WDM 25-65-11 AND B757 FIM 25-65. FOUND RELAY K10537 TO BE STICKING. REMOVED AND REPLACED K10537 PER WDM 25-65-11. OPS CHK GOOD. (7894322)

Part: NONE — NONE · airframe 90,202 hrs · 41,580 cycles

SHIP 668 L EMERGENCY ESCAPE SQUID WILL NOT ILLUMINATE ON TEST 1. CORRECTIVE ACTION: OPS CHK NML AT THIS TIME. (7894317)

Part: NONE — NONE · airframe 90,172 hrs · 41,569 cycles

SHIP 668 FOUND DURING A CHECK JOBCARD#0591-0301 NLG CONTROL PANEL EMERG LIGHT TEST SWITCH INOP. CORRECTIVE ACTION: REPLACED EXTERNAL EMERG LIGHT TEST SW S10035 IAW BOEING SWPM CH 20-83. REF B757 WDM 33-51-11. CONN D40488P FOUND PIN "C " RECESSED. PULLED OUT PIN AND LOCK IN CONNECTOR. AND CHECKS GOOD. SECURED CONNECTOR D40488P. EMERG LIGHT TEST CHECKS GOOD. (8335185)

Part: ENGINE — CONTAMINATED (NR 1) · airframe 90,074 hrs · 41,508 cycles

SHIP 668 STRONG OLD SWEAT SOCK SMELL DURING T.O. INITIAL CLIMB. DISSIPATED SLOWLY AFTER CLB PWR SELECTED. COCKPIT ONLY. NO SMELL IN CABIN. CRUISE WAS OK BUT STRONG SMELL APPEARED PERIODICALLY DURING DESCENT AND APPROACH. CORRECTIVE ACTION: WKG NO GO ODI ATA 2172. T/S PER FIM 21-00-01/301. FOUND OIL IN THE 1 ENG SPINNER AREA. C/W NO GO ODI RAN RT ENG NO SMELL IN L OR R PACK. PNUE CK CKS NORMAL. (8335132)

Part: NONE — NONE · airframe 90,037 hrs · 41,474 cycles

SHIP 668 PLASTIC EMERG LIGHT HOUSING BROKEN AT SEAT 29D. CORRECTIVE ACTION: R&R PLASTIC EMERG LIGHT HOUSING AT SEAT 29D. (8079481)

Part: NONE — NONE · airframe 89,826 hrs · 41,349 cycles

SHIP 668 LT WING SLIDE LIGHT ILLUMINATES ON TAXI OUT. CORRECTIVE ACTION: FOUND LT WING SLIDE DOOR LATCH OUT OF ADJUSTMENT. RERIGGED LT WING DOOR IAW 25-65-09. LATCH LOCKING PROPERLY AND DOOR FLUSHNESS GOOD. NO SLIDE LIGHT ILLUMINATED. RII INSPECTED COMPLIED WITH FAS 75. (8018444)

Part: NONE — NONE · airframe 89,826 hrs · 41,349 cycles

SHIP 668 LT WING SLIDE LIGHT ILLUMINATED. CORRECTIVE ACTION: FOUND LT OVERWING SLIDE DOOR OPENED. HANDLE AND DOOR RESET AND SECURED IAW AMM B757 25-65. (8018442)

Part: NONE — NONE · airframe 89,792 hrs · 41,329 cycles

SHIP 668 CRACK INDICATIONS NOTED ON THE RH 1640 FRAME UPPER I/B HOLE AT APPROX THE 3 AND 9 OCLOCK POSITIONS LOOKING AFT. INDICATIONS APPEAR TO BE IN THE AFT SIDE OF FRAME, NEED LAYER SEPARATION TO CONFIRM, APPROX .030" IN LENGTH EACH. CORRECTIVE ACTION: ACCOMPLISHED FRAME REPAIR ON STA 1640 RH FRAME FOR UPPER I/B HOLE CRACK IAW ER/A 593897-14AD REV ORIGINAL. (1956542)

Part: NONE — NONE · airframe 89,792 hrs · 41,329 cycles

SHIP 668 CRACK INDICATIONS NOTED ON THE RH 1640 FRAME LOWER I/B HOLE AT APPROX THE 3 AND 9 OCLOCK POSITIONS LOOKING AFT. INDICATIONS APPEAR TO BE IN THE AFT SIDE OF FRAME, NEED LAYER SEPARATION TO CONFIRM. CRACK INDICATIONS ARE BOTH GREATER THAN .030" IN LENGTH. CORRECTIVE ACTION: ACCOMPLISHED REPAIR ON STA 1640 RH FRAME FOR LOWER I/B HOLE CRACK IAW ER/A 593897-14AD REV ORIGINAL. (1956525)

Part: NONE — NONE · airframe 89,792 hrs · 41,329 cycles

SHIP 668 #2 PYLON UPPER LINK ATTACH POINT ON PYLON HAS BOTH BUSHING WITH SOME FORM OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED #2 PYLON UPPER FWD SPAR FITTING, I/B AND O/B BUSHING IAW B757 SRM. (1953206)

Part: SNUBBER — OUT OF LIMITS (L4 DOOR) · airframe 89,792 hrs · 41,329 cycles

SHIP 668 L-4 PASSENGER DOOR SNUBBER OUT OF LIMITS PER T/C: 2040-0191-4L. CORRECTIVE ACTION: REMOVED AND REPLACED L-4 PASSENGER DOOR SNUBBER IAW B757 AMM 52-11. (1947720)

Part: MECHANISM — LACK OF LUBE (R1 DOOR) · airframe 89,449 hrs · 41,172 cycles

SHIP 668 FLIGHT ATTENDANT REPORTS 1R DOOR IS DIFFICULT TO ARM. CORRECTIVE ACTION: LUBED MECHANISM - CKS GOOD. (7851070)

Part: TEST PANEL — FAULTED (SQUIB) · airframe 88,877 hrs · 40,921 cycles

SHIP 668 ON WAKE UP CK FOUND SQUIB TEST 1-LEFT EMERG ESCAPE LIGHT NOT WORKING. LIGHT TEST OK. CORRECTIVE ACTION: RPLD SQUIB TEST PANEL PER B757 M/M 26-21.

Part: NONE — NONE · airframe 90,991 hrs · 42,009 cycles

SHIP 668 AMOC REQUIRED (AD 2019-07-04) - TRACKING - ER/A 590828-14AD REV A. CORRECTIVE ACTION: REF ERA 590828-14AD. (1803464)

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 88,383 hrs · 40,712 cycles

EMERGENCY LIGHT DIFFUSER LENS WAS DAMAGED. REPLACED THE LENS.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 88,074 hrs · 40,593 cycles

AIR TURNBACK DUE TO CAPTAIN'S SHATTERED WINDSHIELD. REPLACED NR 1 WINDOW PER AMM.

Part: GIRT BAR — MALFUNCTIONED (R1 DOOR SLIDE) · airframe 87,740 hrs · 40,417 cycles

(AIRCRAFT 668, L/P 6190504) F/A REPORTS 1R GIRT BAR NOT WORKING. CORRECTIVE ACTION: INSTALLED GIRT BAR FITTING PER B757 MM REF 25-66, CK'D DOOR ARMING PER B757 MM REF 25-11. ALL CKS OK. AIRCRAFT OK FOR SVC. VERIFIED SLIDE PIN REMOVED AND VERIFIED DOOR ASSIST BOTTLE PINS REMOVED.

Part: GIRT BAR — DIRTY (R1 DOOR) · airframe 87,585 hrs · 40,353 cycles

SHIP 668 R1 ENTRY DOOR WILL NOT ARM. CORRECTIVE ACTION: TROUBLESHOT IAW BOEING 757 AMM 25-66-11 NO TROUBLE FOUND. CLEARED AND LUBE GIRT BAR FITTINGS. DOOR OPS CHECK GOOD. (6190504)

Part: SKIN — INDICATION (BS 1573) · airframe 87,528 hrs · 40,329 cycles

(AIRCRAFT 668, L/P 1320302) EXTERNAL DFEC INSPECTION OF STR 14R SHOWS INDICATION AT STA 1573 MARKED. CORRECTIVE ACTION: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. CORRECTIVE ACTION: COMPLIED WITH PRI 581984-14AD REV 0 THRU 4 WHICH MATCHES COMPLIED WITH ERA 581984-14AD REV. 0.

Part: NONE — NONE · airframe 87,528 hrs · 40,329 cycles

(AIRCRAFT 668, L/P 1320475) DUE TO REPAIRS INSTALLED ON L/H SIDE OF A/C, UNABLE TO COMPLY WITH INSPECTION OF FUSELAGE SKIN LAP PER CARD 5331-01282-03. REPAIRS LOCATED: STA. 445-564, (ERA 498897-14) STA 588-596. CORRECTIVE ACTION: C/W PRI 498897-14 REV 2 RECEIVED ERA 498897-14AD REV D , PRI 498897-14 REV 2 MATCHES ERA 498897-14 REV. D.

Part: SKIN — INDICATION (BS 1581) · airframe 87,528 hrs · 40,329 cycles

(AIRCRAFT 668, L/P 1320300) EXTERNAL DFEC INSPECTION OF STR 14R SHOWS INDICATION AT STA 1581 MARKED. CORRECTIVE ACTION: COMPLIED WITH PRI 581984-14AD REV 0 THRU 4 WHICH MATCHES COMPLIED WITH ERA 581984-14AD REV. 0.

Part: SKIN — INDICATION (BS 1562) · airframe 87,528 hrs · 40,329 cycles

(AIRCRAFT 668, L/P 1320305) EXTERNAL DFEC INSPECTION OF STR 14R SHOWS INDICATION AT STA 1562 MARKED. CORRECTIVE ACTION: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. COMPLIED WITH PRI 581984-14AD REV 0 THRU 4 WHICH MATCHES COMPLIED WITH ERA 581984-14AD REV. 0.

Part: SKIN — INDICATION (BS 1565) · airframe 87,528 hrs · 40,329 cycles

(AIRCRAFT 668, L/P 1320303) EXTERNAL DFEC INSPECTION OF STR 14R SHOWS INDICATION AT STA 1565 MARKED. CORRECTIVE ACTION: COMPLIED WITH PRI 581984-14AD REV 0 THRU 4 WHICH MATCHES COMPLIED WITH ERA 581984-14AD REV. 0.

Part: SKIN — INDICATION (BS 1581) · airframe 87,528 hrs · 40,329 cycles

(AIRCRAFT 668, L/P 1320301) EXTERNAL DFEC INSPECTION OF STR 14R SHOWS INDICATION AT STA 1581 MARKED. CORRECTIVE ACTION: COMPLIED WITH PRI 581984-14AD REV 0 THRU 4 WHICH MATCHES COMPLIED WITH ERA 581984-14AD REV. 0.

Part: STRINGER — CRACKED (BS 579) · airframe 87,513 hrs · 40,325 cycles

SHIP 668 CRACK AT STR 14L STA 579 DURING DFEC INSPECTION PER AMDS. CORRECTIVE ACTION: SUMMARY SEE NR 113-0001:5331-01282-03/023 00307 COMPLIED WITH ERA 581625-14AD REV. 0. (1320069)

Part: STRINGER — CRACKED (BS 518) · airframe 87,513 hrs · 40,325 cycles

SHIP 668 CRACK INDICATION AT STR 14R STA 518 DURING DFEC INSPECTION PER AMDS, STANDARD NDT 1087-3. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 113-0001:5331-01282-03/019 00303 COMPLIED WITH PRI/ERA 581625-14AD REVISION REV ORIG. (1318886)

Part: STRINGER — INDICATION (BS 1351) · airframe 87,513 hrs · 40,325 cycles

SHIP 668 CRACK INDICATION FOUND (MARKED) AT STR 14L STA 1351.5 DURING DFEC INSPECTION PER AMDS STANDARD NDT 1087-12. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 113-0001:5331-01282-03/016 00299 COMPLIED WITH REPAIR INSTRUCTIONS PER ERA 581983-14AD REV. ORIG. (1318805)

Part: STRINGER — CRACKED (BS 577) · airframe 87,513 hrs · 40,325 cycles

SHIP 668 CRACK AT STR 14L STA 577 DURING DFEC INSPECTION PER AMDS. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 113-0001:5331-01282-03 /021 00305 COMPLIED WITH ERA 581625-14AD REV. 0. (1320058)

Part: STRINGER — CRACKED (BS 444) · airframe 87,513 hrs · 40,325 cycles

SHIP 668 CRACK INDICATION AT STR 14R STA 444 DURING DFEC INSPECTION PER AMDS 5331-01282-03 STANDARD NDT 1087-3. CORRECTIVE ACTION: SUMMARY SEE NR 113-0001:5331-01282-03/017 00301 COMPLIED WITH PRI/ERA 581625-14AD REV ORIG. (1318882)

Part: STRINGER — CRACKED (BS 1563) · airframe 87,513 hrs · 40,325 cycles

SHIP 668 STA. 1563 STR. 14R CRACK INDICATIONS CORRECTIVE ACTION: SEE NR FOR ADDITIONAL INFORMATION 113-0001:5331-01282-03/025 00349 COMPLIED WITH ERA 581984-14AD REV. 0. (1320243)

Part: STRINGER — INDICATION (BS 1600) · airframe 87,490 hrs · 40,313 cycles

SHIP 668 EXTERNAL DFEC INSPECTION OF STR 14RT SHOWS INDICATION AT STA 1600 RT. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 113-0001:5331-01282-03/003 00279 COMPLIED WITH ERA 581625-14 REV 0. (1320051)

Part: STRINGER — CRACKED (BS 580) · airframe 87,513 hrs · 40,325 cycles

SHIP 668 CRACK INDICATION AT STR 14L STA 580 DURING DFEC INSPECTION PER AMDS 5331-01282-03 STANDARD NDT 1087-3. CORRECTIVE ACTION: SEE NR FOR ADDITIONAL INFORMATION 113-0001:5331-01282-03/024 00308 COMPLIED WITH ERA 581625-14AD REV. 0. (1320072)

Part: STRINGER — INDICATION (BS 1339) · airframe 87,513 hrs · 40,325 cycles

SHIP 668 EXTERNAL DFEC INSPECTION OF STR 14LEFT SHOWS INDICATION AT STA 1339.5. CORRECTIVE ACTION: SEE NR FOR 113-0001:5331-01282-03/014 00290 COMPLIED WITH REPAIR INSTRUCTIONS PER ERA 581983-14AD REV. ORIG. (1318801)

Part: STRINGER — INDICATION (BS 1345) · airframe 87,490 hrs · 40,313 cycles

SHIP 668 EXTERNAL DFEC INSPECTION OF STR 14LEFT SHOWS INDICATION AT STA 1345. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 113-0001:5331-01282-03/015 00291 COMPLIED WITH REPAIR INSTRUCTIONS PER ERA 581983-14AD REV. ORIG. (1318803)

Part: REPAIR — NONE · airframe 87,513 hrs · 40,325 cycles

SHIP 668 REMOVE R/H WIFI DOUBLER NEAR F.S. 1533 TO FACILITATE REPAIR, MULTIPLE CRACK INDICATION FINDINGS WERE REPORTED. CORRECTIVE ACTION: SEE NR FOR ADDITIONAL INFORMATION 113-0001:5331-01282-03/036 00425 COMPLIED WITH ERA 582231-14 REV A. (1320002)

Part: STRINGER — INDICATION (BS 1542) · airframe 87,513 hrs · 40,325 cycles

SHIP 668 EXTERNAL DFEC INSPECTION OF STR 14R SHOWS INDICATION AT STA 1542. CORRECTIVE ACTION: SEE NR FOR ADDITIONAL INFORMATION 113-0001:5331-01282-03/010 00286 COMPLIED WITH REPAIR INSTRUCTIONS OF ERA 582107-14AD REV. ORIGINAL. (1319921)

Part: STRINGER — CRACKED (BS 578) · airframe 87,513 hrs · 40,325 cycles

SHIP 668 CRACK INDICATION AT STR 14L STA 578 DURING DFEC INSPECTION PER AMDS STANDARD NDT 1087-3. CORRECTIVE ACTION: SEE NR FOR ADDITIONAL INFORMATION 113-0001:5331-01282-03/022 00306 COMPLIED WITH ERA 581625-14AD REV. 0. (1320063)

Part: STRINGER — INDICATION (BS 1338) · airframe 87,490 hrs · 40,313 cycles

SHIP 668 EXTERNAL DFEC INSPECTION OF STR 14LEFT SHOWS INDICATION AT STA 1338. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 113-0001:5331-01282-03/013 00289 COMPLIED WITH REPAIR INSTRUCTIONS PER ERA 581983-14AD REV. ORIG. (1318810)

Part: STRINGER — CRACKED (BS 1597) · airframe 87,513 hrs · 40,325 cycles

SHIP 668 EXTERNAL DFEC INSPECTION OF STR 14R SHOWS INDICATION AT STA 1597. CORRECTIVE ACTION: SEE NR FOR ADDITIONAL INFORMATION 113-0001:5331-01282-03/004 00280 COMPLIED WITH ERA 581625-14AD REV. 0. (1320054)

Part: STRINGER — INDICATION (BS 1495) · airframe 87,513 hrs · 40,325 cycles

SHIP 668 EXTERNAL DFEC INSPECTION OF STR 14LEFT SHOWS INDICATION AT STA 1495. CORRECTIVE ACTION: SEE NR FOR ADDITIONAL INFORMATION 113-0001:5331-01282-03/011 00287 COMPLIED WITH REPAIR INSTRUCTIONS PER ERA 581982-14AD REV ORIG. (1320192)

Part: SKIN — CRACKED (BS 481) · airframe 87,490 hrs · 40,313 cycles

SHIP 668 CRACK INDICATION FOUND (MARKED) AT STR 14R STA 481 DURING DFEC INSPECTION PER AMDS STANDARD NDT 1087-3. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 113-0001:5331-01282-03/018 00302 COMPLIED WITH PRI/ERA 581625-14AD LATEST REVISION REV ORIG. (1318883)

Part: STRINGER — INDICATION (BS 1486) · airframe 87,513 hrs · 40,325 cycles

SHIP 668 EXTERNAL DFEC INSPECTION OF STR 14LEFT SHOWS INDICATION AT STA 1486. CORRECTIVE ACTION: SEE NR FOR ADDITIONAL INFORMATION 113-0001:5331-01282-03/012 00288 COMPLIED WITH REPAIR INSTRUCTIONS PER ERA 581982-14AD REV ORIG. (1320193)

Part: SKIN — CRACKED (WING) · airframe 87,490 hrs · 40,313 cycles

BHEC INSPECTION PER AMDS 5331-01232-02G STEP 2 REVEALS CRACK INDICATIONS AT TWO HOLES. HOLE NR 1 LOCATED AT BS 349.57 3.51 INCHES ABOVE S-7L. HOLE NR 2 LOCATED AT EDGE OF DOOR CUTOUT 7.19 INCHES FWD OF STA. 349.57. REPAIRED IAW ERA. 581643-14AD REV. O. P.R.I. AND FINAL MATCH.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 94,043 hrs · 44,015 cycles

SHIP 668 SHIP 668 - ER/A 581643-14AD - FUSELAGE / DOOR SURROUND STRUCTURE / L1 DOOR / FWD UPPER CORNER / CRACK IN BEARSTRAP. CORRECTIVE ACTION: REF ERA 581643-14AD. (1310552)

Part: PCA — NOT REPORTED (SPOILER) · airframe 87,490 hrs · 40,313 cycles

(AIRCRAFT 668, L/P 1283715) REPLACE #9 SPOILER PCA PER CARD 2762-01021-01B DUE TO P/N. CORRECTIVE ACTION: REPLACED #9 SPOILER PCA PER CARD 2762-01021-01B.

Part: SENSOR — FAULTY (EMERGENCY EXIT) · airframe 87,447 hrs · 40,290 cycles

(AIRCRAFT 668, L/P 5900720) "L AFT EMER DOOR" EICAS CAUTION MESSAGE. PERFORMED BITE CHECK OF PSEU PER AMM 32-09-06. PSEU FAULTS LEFT AFT EMER EXIT SENSOR CODE 376. REMOVED AND REPLACED LEFT AFT EMER EXIT DOOR LOCKED SENSOR. ADJUSTED PER AMM 52-71-00. PSEU BITE TESTS GOOD PER AMM 32-09-06.

Part: PSEU — FAULTY (LANDING GEAR) · airframe 87,484 hrs · 40,308 cycles

SHIP 668 UPON LANDING, L AFT EMER DOOR EICAS MESSAGE AND EMER DOOR OVERHEAD LIGHT ILLUMINATED. CORRECTIVE ACTION: NO FAULTS / EICAS MSGS UPON ARRIVAL. R/R PSEU IAW AMM 32-09-04. OPS CKS GOOD. (5900730)

Part: TARGET — OUT OF ADJUST (EMERGENCY EXIT) · airframe 87,447 hrs · 40,290 cycles

(AIRCRAFT 668, L/P 6189980) L AFT EMER DOOR MESSAGE. CORRECTIVE ACTION: DISARMED LEFT OVERWING HATCH OVERWING ESCAPE SYSTEM PER AMM 25-65-00 AND 52-22-01. REMOVED LT AFT HATCH AND MEASURED PROX SW TARGET DIMENSION. ADJUSTED PER 52-71-00. PERFORMED PSEU VERIFY, NO FAULTS. CHECKED NEAR AND FAR, OPS OK. REACTIVATED LEFT OVERWING SLIDE SYSTEM PER AMM 25-65-00. BOTTLE PIN REMOVAL IS RII.

Part: PSEU — MALFUNCTIONED (EMERGENCY EXIT) · airframe 87,337 hrs · 40,233 cycles

LEFT AFT EMERGENCY DOOR CAUTION MESSAGE PRIOR TO PUSHBACK. REMOVED AND REPLACED PSEU IAW AMM 32-09-04. SYSTEM CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (R3 DOOR) · airframe 85,755 hrs · 39,532 cycles

SHIP 668 DOOR 3R WILL NOT ARM. CORRECTIVE ACTION: EXERCISED DOOR 3R. DOOR ARMS AND DISARMS NORMALLY. (5825720)

Part: SEAL — DAMAGED (THRUST REVERSER) · airframe 84,396 hrs · 38,914 cycles

NR 2 PYLON O/B T/R, FWD UPPER SEAL AND SEAL RETAINER WORN/DAMAGED. REPL O/B T/R.

Part: ATTACH FITTING — WORN (PRECOOLER) · airframe 84,396 hrs · 38,914 cycles

FWD PRE-COOLER ATTCH FITTING I/B I/D WORN ON NR 2 PYLON. REAMED HOLE TO REMOVE DAMAGE TO 1.192 (514869). R&R FWD PRE-COOLER ATTACH FITTING PER DWG 311N3000.

Part: SKIN — DAMAGED (RT HORIZ STAB) · airframe 84,396 hrs · 38,914 cycles

RT HORIZ STAB L/E DAMAGED. BLENDED RT HORIZ STAB L/E DAMAGE PER SRM 55-10-01, ALLOWABLE DAMAGE 1, FIG 101. FOUND 20 EA. LOCATIONS BEYOND LIMITS PER SRM 55-10-01, ALLOWABLE DAMAGE1 FIG 101. C/W RI 571438-14 SEC I, STEP 3 UT INSPECTION, NO DEFECTS NOTED. C/W THRU STEP 4 OF RI 571438-14 SEC I C/W RI 571438-14 DATED 08SEP18/1640E.

Part: FITTING — DAMAGED (BLEED AIR SYS) · airframe 84,396 hrs · 38,914 cycles

NR 2 PYLON PRE COOLER HAS DEBRIS IN INLET AND OUTLET. FOUND INBD AFT BUSHING AND FITTING DAMAGED. REPLACED INBD AFT BUSHING & FITTING ASSY PER BAC DWG 311N3654. INSTALLED SERVICEABLE PRE-COOLER AND REINSTALLED FAN AIR VALVE PER AMM 36-11.

Part: ISOLATOR — WORN (THRUST REVERSER) · airframe 84,396 hrs · 38,914 cycles

RT PYLON THRUST REV ISOLATORS WORN, INBD AFT, OUT BD MID AND FWD. REMOVED AND REPLACED WORN ISOLATORS PER AMM 78-31-17.

Part: DOOR — DAMAGED (RT MLG) · airframe 84,396 hrs · 38,914 cycles

RT MLG FLYING DOOR DAMAGED AT 2 SPOTS FWD LEADING EDGE AND CENTER OF THE DOOR. NO COMPOSITE DAMAGE FOUND IN CENTER SPOT OF RT MLG DOOR. DAMAGE CONFINED TO EXTERIOR FINISH ONLY. REFINISHED PER SRM 52-80-02. APPLIED PERMANENT REPAIR TO LEADING EDGE OF RT MLG DOOR PER SRM 52-80-02.

Part: THRUST REVERSER — DAMAGED (NR 2 ENGINE) · airframe 84,396 hrs · 38,914 cycles

NR 2 ENG O/B T/R DAMAGED IN MULTIPLE AREAS. REMOVED NR 2 ENG O/B T/R PER W/C 7800-4467.

Part: ENGINE — SEIZED (NR 2) · airframe 84,396 hrs · 38,914 cycles

DUE TO NR 2 ENGINE FOUND SEIZED FROM IFSD. PERFORM PYLON INSPECTION PER AMM 05-51-10-212-001. NO FURTHER DAMAGE FOUND.

Part: ENGINE — FAILED (NR 2) · airframe 84,396 hrs · 38,914 cycles

RT SIDE OF A/C REQUIRES A VISUAL INSP DUE TO NR 2 ENG UNCONTAINED FAILURE. PERFORMED DETAILED VISUAL INSP OF RT SIDE OF A/C PER AMM 05-41.

Part: ANGLE — CRACKED · airframe 84,396 hrs · 38,914 cycles

HYD ACCESS BAY FWD UPPER ANGLE CRACKED AT I/B END. REPLACED ANGLE PER DWG 313N3052.

Part: THRUST REVERSER — DAMAGED (NR 2 ENGINE) · airframe 84,396 hrs · 38,914 cycles

NR 2 ENG I/B T/R DAMAGED IN MULTIPLE AREAS. REMOVED NR 2 ENG I/B THR/REV PER W/C 7800-4467.

Part: ANTENNA — DEFECTIVE (WEATHER RADAR) · airframe 84,018 hrs · 38,757 cycles

DIV TO MEM DUE TO WEATHER RADAR C/B TRIPPED. REPLACED RADAR ANTENNA & TRANSCEIVER PER AMM 34-43. C/W NO GO ODI STEPS 1-3. ALL CHECKS OK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,490 hrs · 40,313 cycles

(AIRCRAFT 668, L/P 0660166) MTC FOUND CORROSION AT FS1460 FRAME AND SHEAR TIE (PN 146N1029-11 AND 140N2002-344, RESPECTIVELY). THE CORRODED SHEAR TIE WILL BE REMOVED AND DISCARDED. THE FRAME ATTACH FLANGE COMMON TO THE REMOVED SHEAR TIE WAS ALSO CORRODED, AND HAD TO BE REMOVED ALTOGETHER. THE ER/A ASSOCIATED WITH THIS LOG PAGE AUTHORIZES THE FABRICATION AND INSTALLATION OF A MODIFIED SHEAR TIE. CORRECTIVE ACTION: THE DTE SECTION, REFERENCING LOG 0660166, HAS A RUN OUT IN JULY 22, 2020. THE DTE IS ENGINEERING RELATED ONLY WITHOUT ANY MTC. WORK NEEDED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,007 hrs · 38,752 cycles

FRAME LOWER LEG STA 1460 CORRODED BETWEEN STR 29R AND STR 30R. COMPLIED WITH ERA 570260-14 REV ORIG SECTION I PERMANENT REPAIR.

Part: CONTROL PANEL — DEFECTIVE (EVAC SLIDE) · airframe 83,990 hrs · 38,746 cycles

LT EMERGENCY ESCAPE SLIDE BULB INOP ON SQUIB TEST PANEL. R&R SQUIB CONTROL TEST PANEL PER AMM 26-21.

Part: PROXIMITY SENSOR — DEFECTIVE (L2 DOOR) · airframe 83,682 hrs · 38,627 cycles

2L DOOR DISARMED/ARMED LIGHT REMAINED ILLUMINATED. OPS CKD PER AMM 52-71-00. OPS CK GOOD. DUE TO HISTORY REPLACED PROX SW S10219 PER AMM 25-66-11.

Part: SWITCH — DEFECTIVE (L2 DOOR) · airframe 83,489 hrs · 38,548 cycles

2L SLIDE DOOR LIGHT ILLUMINATED WITH DOOR DISARMED. REMOVED AND REPLACED SLIDE ARM KORRY SWITCH ASSY PER AMM 25-66.

Part: SWITCH — MALFUNCTIONED (L2 DOOR SLIDE) · airframe 83,476 hrs · 38,544 cycles

L2 DOOR SLIDE LIGHT REMAINED ILLUMINATED WITH DOOR DISARMED. REMOVED THE BUSTLE AND INSPECTED THE GIRT BAR FITTINGS, AND MECHANISM , NO DEFECTS. REPLACED THE LAMPS AND DOOR INDICATION SWITCH.

Part: CIRCUIT BREAKER — FAULTY · airframe 83,293 hrs · 38,468 cycles

THE DOOR GIRT BAR C/B C4183 IS POPPING. P11-4 PANEL, WDM 25-66-11. REPLACED SWITCH AND REPAIRED PER WDM 25-66-11.

Part: PIN — BACKED OUT (CABIN) · airframe 82,778 hrs · 38,240 cycles

EMERGENCY LIGHT AT ROW 16 INOP. LIGHT AT 16D VERIFIED ASSY WORKED POSSIBLE WIRE DISCONNECT ON SEAT, FOUND PIN PUSHED BACK ON CONNECTION UNDER SEAT.

Part: SENSOR — ICED (PAX DOOR) · airframe 82,732 hrs · 38,224 cycles

ENTRY DOOR LIGHT ON OVERHEAD PANEL FAILED TO ILLUMINATE WHEN ENTRY DOOR WAS OPEN. FOUND ICE AND DEBRIS IN THE DOOR SENSOR, REMOVED THE ICE AND DEBRIS, OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (ROW 16 ABC) · airframe 82,720 hrs · 38,220 cycles

EMERGENCY LIGHT, CEILING AT ROW 16 ABC INOPERATIVE. R & R THE LIGHT ASSY IAW AMM 33-51.

Part: SENSOR — DIRTY (L2 DOOR) · airframe 82,720 hrs · 38,220 cycles

ENTRY DOOR SENSOR NOT SHOWING L2 DOOR OPEN. NO ENTRY DOOR ANNUNCIATOR OR ACARS IN TIME. CLEANED THE SENSOR, OPS CHECKED GOOD DOOR ANNUNCIATION GOOD.

Part: SKIN — DENTED (CARGO DOOR) · airframe 82,149 hrs · 38,007 cycles

FWD CARGO DOOR EXTERNAL SKIN FOUND DENTED, 10 INCHES DOWN FROM TOP EDGE, 22 INCHES AFT OF FWD EDGE. REMOVED THE CARGO DOOR IAW AMM 52-34-01-004. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 52-30-01, REPAIR 4. INSTALLED THE CARGO DOOR IAW AMM 52-34-01-404-014.

Part: ROD END — DIRTY (HORIZONTAL STAB) · airframe 82,149 hrs · 38,007 cycles

LEFT HORIZONTAL STABILIZER, RIGHT SYS PCA, POGO ROD ENDS RUSTY. REMOVED , CLEANED AND INSTALLED IAW PROCESS STANDARD 900-1 AND AMM 27-31-06 424-024.

Part: ROD END — CORRODED (HORIZONTAL STAB) · airframe 82,149 hrs · 38,007 cycles

RIGHT HORIZONTAL STAB, CENTER SYSTEM, POGO ROD ROD ENDS ARE RUSTY. REPLACED THE RT HORIZONTAL STAB CENTER SYSTEM POGO ROD END IAW CMM 27-31-05.

Part: ROD END — CORRODED (HORIZONTAL STAB) · airframe 82,149 hrs · 38,007 cycles

RIGHT HORIZONTAL STAB, LEFT SYSTEM, POGO ROD ENDS ARE RUSTY. REPLACED THE ROD END IAW AMM 27-31-06-424-024.

Part: STRAP — CORRODED (FWD CARGO) · airframe 82,149 hrs · 38,007 cycles

FWD CARGO BAY FLOOR PANEL TO SIDEWALL, RT STRAPS CORRODED AROUND FASTENER. REMOVED AND REPLACED STRAP IAW SRM 51-40-05 AND DWG 453N1719 REV E.

Part: LINKAGE — LOOSE (HORIZONTAL STAB) · airframe 82,149 hrs · 38,007 cycles

RIGHT HORIZONTAL STAB, RIGHT SYSTEM, ELEVATOR PCA POGO ATTACH POINT LINKAGE HAS LOOSE BEARING RACES IN FITTING. ACCOMPLISHED GVI ON RT ELEVATOR RIGHT SYSTEM INPUT LINKAGE FOUND TO BE IN SERVICEABLE CONDITION, REINSTALLED IAW AMM 27-31-06-424-024.

Part: ROD END — CORRODED (HORIZONTAL STAB) · airframe 82,149 hrs · 38,007 cycles

LEFT HORIZONTAL STABILIZER, CENTER SYS PCA, POGO ROD ENDS RUSTY. REPLACED L/H ELEVATOR CENTER SYS PCA POGO IAW B757 AMM 27-31-06-424-024.

Part: ROD END — CORRODED (HORIZONTAL STAB) · airframe 82,149 hrs · 38,007 cycles

LEFT HORIZONTAL STABILIZER, LEFT SYS PCA POGO ROD ENDS RUSTY. REPLACED ROD ENDS IAW AMM 27-31-06-424-024.

Part: ROD END — CORRODED (HORIZONTAL STAB) · airframe 82,149 hrs · 38,007 cycles

RIGHT HORIZONTAL STAB, RIGHT SYSTEM, POGO ROD ROD ENDS ARE RUSTY. REPLACED THE RT ELEVATOR RIGHT SYSTEM POGO IAW AMM 27-31-06-424-024.

Part: STRAP — CORRODED (CARGO BAY) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO COMP FLOOR PANEL 153BF STRAP CORRODED AROUND FASTENER HOLES BOTTOM SIDE. FABRICATED NEW SPLICE STRAP IAW DWG 453N1611 REV - .

Part: DRAIN MAST — CORRODED (FUSELAGE) · airframe 82,149 hrs · 38,007 cycles

AFT FUSELAGE DRAIN MAST REMOVED ON WORK CARD 5683351 HAS CORROSION ON UPPER MOUNTING SURFACE AT CORRODED SCREW. REMOVED AND REPLACED DRAIN MAST FOR AFT FUSELAGE AND PERFORMED OPS CHECK IAW AMM 38-31-01.

Part: PAN — DENTED (LAV SERVICE) · airframe 82,149 hrs · 38,007 cycles

AFT LAV DUMP/SERVICE PAN HAS A DENT IN THE FWD LOWER CORNER. REMOVED AND REPLACED AFT LAV DUMP/SERVICE PAN, IAW SRM 51-40-02 AND DRAWING 146N3650.

Part: INTERCOSTAL — CORRODED (BS 1440-1460) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO BAY BILGE AREA RIGHT SIDE BS 1440 - 1460, STRINGER 26R. CORROSION FOUND ON THE OTBD OF INTERCOSTAL. REMOVED AND REPLACED THE INTERCOSTAL WEB IAW SRM 51-40-02, AND DRAWING 146N1014.

Part: STRUCTURE — CORRODED (BS 1440) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO BAY LOWER SILL AT BS 1440 +2, IS CORRODED ON VERTICAL LEG, STRINGER 26R AREA. COMPLIED WITH PRI ER/A 560596-14, REV 0, AND ER/A 560596-14, REV ORIGINAL.

Part: STRAP — CORRODED (BS 1660 SKIN) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO BAY BS 1660+10, BETWEEN STRINGERS 26R AND DRAIN TUBE, THE SKIN STRAP WAS CORRODED. REMOVED AND REPLACED THE STRAP IAW SRM 51-40-02 AND DRAWING 146N3700, REV J.

Part: STRAP — CORRODED (BS 1360-1380) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO BAY RT BS 1360 - 1380 FLOOR TO SIDEWALL STRAP CORRODED. FABRICATED A NEW STRAP IAW DWG 453N1719, REV E AND PL 453N1719, REV M.

Part: ANGLE — CORRODED (BS 1440-1520) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO BAY FLOOR SUPPORT, BS 1440 TO 1520+10, RBL 22, ZEE ANGLE CORRODED ON UPPER SURFACE AROUND FASTENER HOLES. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 140N5390.

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO BAY FLOOR PANEL 161AF STRAP CORRODED AROUND FASTENER HOLES. FABRICATED A NEW FLOOR PANEL SPLICE STRAP IAW DWG 453N1611, REV B, AND PL 453N1611, REV K.

Part: STRAP — CORRODED (BS 1325) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO BAY, RT BS 1325 FLOOR TO SIDEWALL STRAP CORRODED. FABRICATED A NEW LOWER STRAP BS 1210 - 1380 IAW GWD 453N1719, REV E, AND PL 453N1719, REV M.

Part: CARGO TRACK — CORRODED (BS 1400) · airframe 82,149 hrs · 38,007 cycles

CARGO TRACK AFT OF THE AFT CARGO DOOR BS 1440 CORRODED. REMOVED AND REPLACED THE CARGO TRACK IAW SRM 51-40-02 AND DWG 146N5420.

Part: CARGO TRACK — CORRODED (BS 1440) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO BAY, CARGO TRACK JUST AFT OF THE AFT CARGO DOOR BS 1440 CORRODED. REMOVED AND REPLACED THE CARGO TRACK IAW SRM 51-40-02 AND DWG 146N5420, REV B.

Part: CARGO TRACK — CORRODED (BS 1300-1400) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO BAY BS 1300 - 1400, LBL 24 CARGO TRACK CORRODED. REPLACED THE CARGO TRACK IAW SRM 51-40-02, & DWG 146N1006, REV E.

Part: FLOOR SUPPORT — CORRODED (BS 1460) · corrosion level 2 · airframe 82,149 hrs · 38,007 cycles

AFT CARGO BAY FLOOR SUPPORT BS 1460+10, LBL 3, CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND REPLACED THE FLOOR SUPPORT FROM BS 1440 - 1500, LBL 3, IAW SRM.

Part: DOOR — CORRODED (LAV SERVICE) · airframe 82,149 hrs · 38,007 cycles

LOWER FUSELAGE MID LAVATORY SERVICE DOOR 121AL OUTER SURFACE HAS CORROSION. REMOVED & REPLACED THE LAV SERVICE DOOR IAW SRM 51-40-02.

Part: FLOOR PANEL — CORRODED (FWD CARGO BAY) · airframe 82,149 hrs · 38,007 cycles

FWD CARGO BAY FLOOR PANEL 121BF CORRODED AROUND FASTENER HOLES. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-53. REPLACED THE FLOOR PANEL IAW DWG 453N1805, REV W.

Part: FLOOR PANEL — CORRODED (FWD CARGO BAY) · airframe 82,149 hrs · 38,007 cycles

FWD CARGO BAY FLOOR PANEL 121AF CORRODED AROUND FASTENER HOLES. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. FABRICATED A NEW FLOOR PANEL IAW DWG 453N1805, SHEET 8, REV-.

Part: FLOOR PANEL — CORRODED (FWD CARGO BAY) · airframe 82,149 hrs · 38,007 cycles

FORWARD CARGO COMPARTMENT FLOOR PANEL 121DF LEFT, CORRODED AROUND FASTENER HOLES. REPLACED THE FLOOR PANEL IAW DWG 453N1805, REV W.

Part: ANGLE — CORRODED (BS 1520-1640) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO BAY RIGHT SIDE BS 1520+10 TO 1640, RBL 20. SIDE PANEL ZEE ANGLE CORRODED ON UPPER SURFACE AROUND FASTENER HOLES. BEYOND ALLOWABLE LIMITS IAW SRM 53-00-53, PG 105, DETAIL V. REMOVED AND REPLACED THE ANGLE IAW DWG 146N5390, REV B, AND SRM 51-40-02, PAR 7, AND ERA 37211-14MA.

Part: FLOOR PANEL — CORRODED (FWD CARGO BAY) · airframe 82,149 hrs · 38,007 cycles

FWD CARGO BAY FLOOR PANEL 121BF CORRODED AROUND FASTNER HOLES. EVALUATED CORROSSION ON FLOORBOARD 121BF FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. FABRICATED A NEW FLOOR PANEL I AW DWG 453N1805, SHEET 6, REV A.

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 82,149 hrs · 38,007 cycles

FWD CARGO BAY FLOOR PANEL 121DF CORRODED AROUND FASTENER HOLES. REMOVED CORROSION, FOUND OUT OF LIMITS 100% MATERIAL LOSS IAW SRM53-00-53. REPLACED FLOOR PANEL IAW DWG 453N1805, REV W.

Part: SEAT TRACK — CORRODED (BS 1040-1077) · airframe 82,149 hrs · 38,007 cycles

SEAT TRACK SECTION FROM BS 1040 - 1077, LBL 45 IS CORRODED AT TWO LOCATIONS. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK. RESTORED THE FINISH IAW SRM 53-00-52, REPAIR 4.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 82,149 hrs · 38,007 cycles

SEAT TRACK AT RBL 25 STA 987-1054 CORRODED IN 2 PLACES. DEPTH .07" WIDTH 1.3" LENGTH 4" AT DEEPEST BLEND. FOUND TO BE OUT OF LIMITS. SEAT TRACK NEEDS REPAIR. REMOVED SEAT TRACK DAMAGE AND INSTALLED NEW SEAT TRACK AND RESTORED FINISH IAW SRM53-00-52.

Part: SKIN — DENTED (FWD CARGO DOOR) · airframe 82,149 hrs · 38,007 cycles

FWD CARGO DOOR EXTERNAL SKIN DENTED, 10 INCHES DOWN FROM TOP EDGE, AND 22 INCHES AFT OF FWD EDGE. OPEN

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 82,149 hrs · 38,007 cycles

REF CARD 2021-2084 FOR SEAT TRACK GOUGED AT STA 1324-1326 RBL25. DEPTH .026", WIDTH 1.0", LENGTH 2.4". FOUND TO BE OUT OF LIMITS. SEAT TRACK NEEDS TO BE REPAIRED. REMOVED DAMAGED SECTION OF SEAT TRACK AT STA 1320-1350 RBL 25, IAW SRM 53-00-50. FABRICATED AND INSTALLED REPAIR PARTS AND NEW SECTION OF SEAT TRACK IAW SRM 53-00-52 REPAIR 1.

Part: FLOOR SUPPORT — CORRODED (BS 1460) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO BAY FLOOR SUPPORT BS 1460+10, RBL 3 CORRODED ON LOWER SURFACE. REMOVED THE CORROSION ON THE FLOOR SUPPORT, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53 ALLOWABLE DAMAGE 1, DETAIL IV. REMOVED & REPLACED THE FLOOR SUPPORT IAW DWG 146N5390, REV C, & SRM 51-40-02, PG 4, PAR 7.

Part: SUPPORT CHANNEL — CRACKED (BS 1620) · airframe 82,149 hrs · 38,007 cycles

AFT CABIN, RT LIFE RAFT SUPPORT CHANNEL JUST FWD OF BS 1620 IS CRACKED AND DEFORMED. REPAIRED THE SUPPORT CHANNEL IAW SRM 51-70-11.

Part: INTERCOSTAL — DAMAGED (BS 1600-1620) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO SIDE PLATE SUPPORT INTERCOSTAL BETWEEN BS 1600 AND1620, STRINGER 27R HAS SEVERAL DAMAGED AND CRACKED FASTENER HOLES. REMOVED THE INTERCOSTAL IAW SRM 51-40-02, FIG 8. FABRICATED, DRILLED, APPLIED FINISH, AND INSTALLED A NEW INTERCOSTAL IAW DWG 146N5451, REV-, AND SRM 51-40-02.

Part: SIDEWALL SUPPORT — BENT (BS 1360) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO BAY, BS 1360, STRINGERS 23 - 26R SIDEWALL SUPPORT ANGLE BENT AT THE LOWER END. THE SIDEWALL SUPPORT REMOVED AND REPLACED IAW SRM 51-40-02, PAGE 4, PAR 7, AND DWG 453N1230, REV D.

Part: SHEAR TIE — CRACKED (BS 1360) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO BAY BILGE, BS 1360, STRINGERS 28L TO 28R SHEAR TIE CORRODED. REMOVED CRACKED SHEAR TIE IAW SRM 51-40-02, PARA 4E. LOCATED AND DRILLED A NEW SHEAR TIE IAW 51-40-05, PARA. 4. INSTALLED IAW SRM 51-40-02, PARA . 4 B.

Part: SKIN — DENTED (BS 1961) · airframe 82,149 hrs · 38,007 cycles

TAIL CONE AREA OUTER FUSELAGE SKIN AT BS 1961.175, STRINGER 3L ONE DENT IN THE SKIN. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, DETAIL III. ACCOMPLISHED PRI ER/A 560595-14, REV 0, AND ER/A 560959-14, REV ORIGINAL.

Part: PLATE — CORRODED (BS 646) · airframe 82,149 hrs · 38,007 cycles

FWD CARGO BAY, BS 646, PLATE SPLICE ABOVE STRINGER 26R HAS INTERGRANILUR CORROSION ON THE BOTTOM SIDE. REMOVED AND REPLACED THE PLATE, BS 640 TO 760, IAW SRM 51-40-02, AND DRAWING 143N5320, SHEET 5, REV B.

Part: PLATE — CORRODED (BS 638-646) · airframe 82,149 hrs · 38,007 cycles

FWD CARGO BAY, BETWEEN BS 638 AND 646, TOP AND BOTTOM SIDE PLATE CORRODED ABOVE STRINGER 26R. REMOVED AND REPLACED THE PLATE BS 560 TO 645 IAW SRM 51-40- 02, AND DRAWING 143N5320, SHEET 6, REV E.

Part: SEAT TRACK — CORRODED (BS 790-880) · airframe 82,149 hrs · 38,007 cycles

SEAT TRACK AT BS 790 - 880, LBL 45 GOUGED IN THREE AREAS. FOUND TO BE OUT OF LIMITS. REMOVED THE SEAT TRACK, FABRICATED A NEW SEAT TRACK AND INSTALLED IAW SRM 51-40-02, & DWG 143N5106.

Part: SEAT TRACK — CORRODED (BS 1320-1540) · airframe 82,149 hrs · 38,007 cycles

SEAT TRACK AT BS 1320 - 1540, LBL 45 CORRODED AT FIVE LOCATIONS, FOUND TO BE OUT OF LIMITS. REMOVED THE SEAT TRACK, IAW SRM 53-00-52, REPAIR 3, PAGE 201. FABRICATED, DRILLED, APPLIED FINISH AND INSTALLED THE NEW SEAT TRACK IAW SRM 53-00-52, REPAIR 3.

Part: PLATE — CORRODED (BS 765-839) · airframe 82,149 hrs · 38,007 cycles

FWD CARGO BAY BETWEEN BS 839 AND 765.5, LT SIDE PLATE IS CORRODED IN SEVERAL AREAS ON TOP AND SIDE SURFACES. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM. REPLACED THE SIDE PLATE IAW DWG.

Part: INTERCOSTAL — CORRODED (BS 720-740) · airframe 82,149 hrs · 38,007 cycles

MAIN CABIN L2 DOORWAY INTERCOSTAL CORRODED BS 720 TO 740. REMOVED THE CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-30-15, DETAIL IV. INSTALLED A NEW INTERCOSTAL IAW SRM 51-40-02 AND DWG 143N5400, REV B.

Part: SEAT TRACK — DAMAGED (BS 1440-1540) · airframe 82,149 hrs · 38,007 cycles

SEAT TRACK, BS 1440 - 1540, RBL 45 HAS TWO GOUGES AND ONE AREA OF CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED THE SEAT TRACK IAW SRM. FABRICATED, DRILLED, APPLIED FINISH AND INSTALLED THE NEW SEAT TRACK AND REPAIR IAW SRM.

Part: SEAT TRACK — CORRODED (BS 1274) · airframe 82,149 hrs · 38,007 cycles

SEAT TRACK AT BS 1274, LBL 45 CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED CORROSION, FABRICATED A REPAIR AND INSTALLED IAW SRM.

Part: SEAT TRACK — CORRODED (BS 1433-1449) · airframe 82,149 hrs · 38,007 cycles

SEAT TRACK AT BS 1433 - 1449, LBL 25 CORRODED. FOUND OUT OF LIMITS. REMOVED THE SEAT TRACK5 IAW SRM 53-00-52. FABRICATED, DRILLED, APPLIED FINISH, AND INSTALLED SEAT TRACK IAW SRM 53-00-52, REPAIR 1.

Part: ANGLE — CORRODED (BS 1520-1640) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO BAY, LEFT SIDE BS 1520+10 TO 1640, LBL 20, SIDE PANEL ZEE ANGLE CORRODED ON UPPER SURFACE AROUND FASTENER HOLES. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-0053, PG 105, DETAIL V. REMOVED AND REPLACED THE ANGLE IAW EA 373211-14MA, AND SRM 51-40-02, PG 4, PAR 7.

Part: SEAT TRACK — CORRODED (BS 1089-1110) · airframe 82,149 hrs · 38,007 cycles

SEAT TRACK, RBL 25, BS 1089 - 1110 CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED THE SEAT TACK SECTION FROM BS 1080 TO 1180 IAW SRM 51-40-02. FABRICATED, DRILLED, APPLIED FINISH, AND INSTALLED THE NEW SEAT TRACK SECTION IAW DWG 144N5001, REV A.

Part: SEAT TRACK — GOUGED (BS 880-884) · airframe 82,149 hrs · 38,007 cycles

SEAT TRACK, BS 880 - 884, LBL 45 GOUGED, FOUND TO BE OUT OF LIMITS. REMOVED THE DAMAGED SEAT TRACK IAW SRM 51-40-02, PG 10. FABRICATED, LOCATED, DRILLED, ANODIZED AND PAINTED A NEW SEAT TRACK IAW DRAWING 144N5021, REV. C. INSTALLED THE NEW SEAT TRACK IAW SRM 51-40-02, PAR 7.

Part: SEAT TRACK — CORRODED (BS 1263) · airframe 82,149 hrs · 38,007 cycles

SEAT TRACK AT BS 1263, LBL 25 CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED THE SEAT TRACK IAW SRM 53-00-52, REPAIR 1. FABRICATED A REPAIR, LOCATED, DRILLED, APPLIED FINISH AND INSTALLED THE REPAIR IAW SRM 53-00-52, REPAIR 1.

Part: BRACKET — DAMAGED (NR 1 NACELLE) · airframe 82,149 hrs · 38,007 cycles

NR 1 PYLON UPPER SURFACE AT NACELLE STATION 149.5, HYDRAULIC PRESSURE TUBE SUPPORT BRACKET HAD SEVERAL FASTENERS THAT WERE MISSING AND FASTENER HOLES WERE DAMAGED. REPLACED THE SUPPORT IAW DWG 313N3100 REV D. FABRICATED AND INSTALLED THE ANGLE IAW DWG 312N3903, REV C.

Part: INTERCOSTAL — CORRODED (BS 1600-1620) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO BAY BILGE AREA BS 1600 TO 1620, RBL 2, INTERCOSTAL CORRODED ON LEFT SIDE AT LOWER AFT END. DRILLED, LOCATED, AND TRIMED THE NEW INTERCOSTAL IAW SRM 51-40-05. TREATED, PRIMED, AND PAINTED THE INTERCOSTAL AND INSTALLED IAW SRM 51-20-01, AMM 51-21-15-370-802, SRM 51-40-02 AND DWG 146N5432, REV -.

Part: THRESHOLD — CRACKED (CARGO BAY) · airframe 82,149 hrs · 38,007 cycles

FWD CARGO BAY BOTTOM MID THRESHOLD CRACKED AT AFT END. REPAIRED THE THRESHOLD IAW ER/A 06-489867- 14MA, REV G, SECTION III.

Part: THRESHOLD — CRACKED (R1 DOORWAY) · airframe 82,149 hrs · 38,007 cycles

R1 DOOR THRESHOLD AFT CORNER CRACKED AT WELD. REPAIRED THE THRESHOLD IAW ER/A 06-489867-14MA, REV G, SECTION III.

Part: THRESHOLD — CRACKED (R1 DOORWAY) · airframe 82,149 hrs · 38,007 cycles

R1 DOOR THRESHOLD FWD CORNER CRACKED AT WELD. REPAIRED THE THRESHOLD IAW ER/A 06-489867-14MA, SECTION III.

Part: PLATE — CRACKED (BS 1540-1560) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO BAY FLOOR SUPPORT LEFT SIDE BS 1540 TO 1560, STR 27L, BAFFLE PLATE UPPER ATTACH ANGLE CRACKED IN RADIUS AT FORWARD END. REMOVED & REPLACED THE BAFFLE PLATE UPPER ATTACH ANGLE IAW SRM 51-40-02, PG 2, PAR 4, & DWG 146N5434.

Part: FLOOR SUPPORT — CORRODED (BS 1200-1300) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO BAY FLOOR SUPPORT, BS 1200 TO 1300+10, CORRODED AROUND NUTPLATE HOLES. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, PAR 4 & 7, AND DRAWING 146N5390, REV A & C.

Part: FLOOR SUPPORT — CORRODED (BS 1300-1400) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO BAY FLOOR SUPPORT LEFT SIDE BS 1300+10 TO 1400+10, LBL 24. CORRODED AROUND NUTPLATE HOLES. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 41-40-02, PAR 4, AND 7, DRAWING 146N5390, REV A & C.

Part: DOOR — CORRODED (LAV SERVICE) · airframe 82,149 hrs · 38,007 cycles

LOWER FUSELAGE FWD LAVATORY SERVICE DOOR 119AL OUTER SURFACE HAS CORROSION. REMOVED THE CORROSION WITH 100% MATERIAL LOSS. OUT OF LIMITS IAW SRM 52-40-01, FIG 101, DETAIL V. REMOVED AND REPLACED THE DOOR IAW SRM 51-40-02.

Part: CREASE BEAM — CORRODED (BS 760) · airframe 82,149 hrs · 38,007 cycles

LEFT CREASE BEAM BS 760 +3 CORRODED. OUT OF LIMITS IAW SRM 53-30-13, ALLOWABLE DAMAGE 1. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR IAW SRM 53-00-13, REPAIR 1.

Part: FLOOR SUPPORT — CORRODED (BS 1300-1380) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO FLOOR SUPPORT BS 1300+10 - 1380, RBL 24 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, PG 105, FIG 101, DETAIL V. REMOVED & REPLACED IAW SRM 51-40-02, PG 4, PAR 7, AND ER/A 373211-14 MA, REV G.

Part: FLANGE — CRACKED (BS 1520-1540) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO CEILING AREA BS 1520 TO 1540, BL 0 FLANGE UPPER FLANGE CRACKED AT NUTPLATES. REMOVED AND REPLACED THE FLANGE IAW SRM.

Part: FRAME — CRACKED (LIFE RAFT BOX) · airframe 82,149 hrs · 38,007 cycles

AFT LIFE RAFT BOX STRUCTURE HAS A CRACK ON THE FRAME AT THE LT SIDE, AFT END. SRM 51-70-11 PG 1 PAR 2. ACCOMPLISHED HFEC INSPECTION IAW 757 NDT PART 6 51-00-19, NO DEFECTS NOTED. FABRICATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW SRM 51-70-11 PG 1 PAR 9 AND 10.

Part: SKIN — DAMAGED (BS 419) · airframe 82,149 hrs · 38,007 cycles

LOWER FUSELAGE EXTERIOR SKIN, BS 419 BETWEEN STRINGERS 23R AND 24R, FOUND CREASED. REPAIRED THE SKIN IAW ER/A 560590-14, REV 0, AND ER/A 560590-14, REV A.

Part: INTERCOSTAL — CRACKED (BS 1420-1440) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO BAY CEILING BS 1420 TO 1440, BL 0, INTERCOSTAL UPPER FLANGE CRACKED AT FASTENER HOLES. REMOVED & REPLACED IAW SRM 51-40-02, PARA 4 (B), 4 (E), AND DWG 146N5180, REV. C.

Part: SKIN — DAMAGED (BS 439) · airframe 82,149 hrs · 38,007 cycles

LOWER FUSELAGE EXTERIOR SKIN, BS 439 BETWEEN STRINGERS 23R AND 24R FOUND CREASED. REPAIRED THE SKIN IAW ER/A 560590-14, REV 0, AND ER/A 560590-14, REV A.

Part: SEAT TRACK — GOUGED (BS 1575) · airframe 82,149 hrs · 38,007 cycles

SEAT TRACK GOUGED AT BS 1575. DEPTH .028 INCH, WIDTH .9 INCH, LENGTH, 4.6 INCHES. FOUND TO BE OUT OF LIMITS. THE SEAT TRACK WAS REPLACED IAW SRM 51-40-02 AND DRAWING 146N5120.

Part: FITTING — CORRODED (BS 1720) · airframe 82,149 hrs · 38,007 cycles

G4 GALLEY AFT WET AREA TERMINAL LUG, BS 1720, LBL 54 CORRODED AT THE END OF THE CREASEBEAM. FOUND BEYOND 50 PERCENT. REMOVED AND REPLACED THE FITTING IAW SRM 51-40-02, AND DRAWING 146N8722.

Part: SEAT TRACK — CORRODED (BS 1540-1600) · airframe 82,149 hrs · 38,007 cycles

SEAT TRACK, BS 1540 - 1600, LBL 45 CORRODED AT 3 LOCATIONS, FOUND OUT OF LIMITS. THE SEAT TRACK WAS REPAIRED IAW SRM 51-40-02, AND DRAWING 146N5120.

Part: FLOORBEAM — CORRODED (BS 345) · corrosion level 2 · airframe 82,149 hrs · 38,007 cycles

BS 345, RBL 20 FLOORBEAM CORRODED BOTTOM SIDE OF SCREW HOLE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM. REPAIRED THE FLOORBEAM IAW ERA 560593-14, REV ORIG.

Part: SHEAR WEB — CORRODED (BS 1681) · corrosion level 2 · airframe 82,149 hrs · 38,007 cycles

PASSENGER CABIN AFT WET AREA, BS 1681, LBL 25 SHEAR WEB IS BULGING. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPAIRED THE SHEAR WEB IAW ERA 560592-14, REV ORIG.

Part: DOUBLER — DAMAGED (BS 1500 FRAME) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO BAY, BS 1500, STRINGER 25 TO 26L. PREVIOUS FRAME REPAIR FASTENER HEADS PULLING THROUGH DOUBLER. REMOVED AND REPLACED THE FRAME REPAIR DOUBLER IAW SRM.

Part: ATTACH FITTING — CORRODED (BS 607) · airframe 82,149 hrs · 38,007 cycles

FWD CARGO BAY LOWER DOOR TRESHOLD AREA AT BS 607, DOOR TRESHOLD MOUNT FITTING HAS INTERGRAINULAR CORROSION. REMOVED THE THRESHOLD MOUNT AFT ATTACH PLATE IAW SRM 51-40-02, INSTALLED A NEW ATTACH PLATE IAW SRM 51-40-02.

Part: BRACKET — DAMAGED (BS 680-700) · airframe 82,149 hrs · 38,007 cycles

FWD CARGO BAY BETWEEN BS 680 AND 700 ABOVE STRINGER 28R, TWO BRACKETS ARE DAMAGED, ONE CRACKED AND BOTH CORRODED. CORROSION REMOVED OUT OF LIMITS. THE BRACKETS WERE REMOVED IAW 51-40-02,0. INSTALLED NEW BRACKETS IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 350-365) · airframe 82,149 hrs · 38,007 cycles

FWD CABIN FLOOR SUPPORT BETWEEN BS 350 - 365, LBL 24 IS CRACKED. REMOVED ANE REPLACED IAW SRM 51-40-02, PARA 4 E AND SRM 51-40-02, PARA 4 B.

Part: FLOOR SUPPORT — CORRODED (BS 1400-1520) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO BAY FLOOR SUPPORT BS 1400 TO 1520+10, LBL 22 CORRODED ON UPPER SURFACE AROUND FASTENER HOLES. REMOVED AND REPLACED IAW SRM 51-40-02, PAR 4 AND 7, DRAWING 146N5390, REV C, REV A.

Part: CHANNEL — CORRODED (BS 1380-1440) · airframe 82,149 hrs · 38,007 cycles

AFT CARGO DOOR CUTOUT LOWER THRESHOLD BS 1380 TO 1440, SIDE PANEL ZEE CHANNEL CORRODED AROUND FASTENERS. REMOVED & REPLACED WITH SERVICEABLE SIDE PANEL ZEE ANGLE IAW EA 373211-14MA REV G.

Part: FLOOR SUPPORT — CORRODED (BS 320-345) · airframe 82,149 hrs · 38,007 cycles

PASSENGER CABIN, R1 CREASE BEAM FLOOR SUPPORT CORRODED AROUND FASTNER HOLES BS 320 - 345. REPLACED THE FLOOR SUPPORT IAW DWG 141N5160, REV B, AND SRM 51-40-02. APPLIED CIC TO AREA IAW AMM 51-24-03-110-814C1.

Part: FRAME — CORRODED (BS 1720) · airframe 82,149 hrs · 38,007 cycles

AFT BULK CARGO BAY, FRAME AT BS 1720, LBL 25 HAS CORROSION. COMPLIED WITH PRI 560594-14, REVISION 0, AND ER/A 560594-14, REV ORIGINAL.

Part: MOUNT — CORRODED (BS 1638) · airframe 82,149 hrs · 38,007 cycles

PASSENGER CABIN AFT WET AREA, BS 1638, RBL 25 LAVATORY MOUNT IS CORRODED. REMOVED AND INSTALLED A NEW FITTING IAW SRM 51-40-02, AND DWG 146T5634, REV D.

Part: MOUNT — CORRODED (BS 1638) · airframe 82,149 hrs · 38,007 cycles

PASSENGER CABIN AFT WET AREA BS 1638, LBL 25 LAVATORY MOUNT IS CORRODED. REMOVED AND REPLACED IAW SRM 51-40-02, AND DWG 146T5634, REV D.

Part: FLOORBEAM — CORRODED (BS 365) · airframe 82,149 hrs · 38,007 cycles

PASSENGER CABIN FLOORBEAM BS 365, RBL 26 TO RBL 44 HAS FIVE FASTNER HOLES WITH CORROSION ON BOTTOM SIDE. REPAIRED THE FLOORBEAM IAW SRM 53-00-51, REPAIR 8.

Part: MOUNT — CRACKED · airframe 82,149 hrs · 38,007 cycles

E3-3 RACK FWD MOUNT HOLE CRACKED. REPAIRED THE RACK FWD MOUNT IAW SRM 51-70-11.

Part: FLOORBEAM — CORRODED (BS 1681) · airframe 82,149 hrs · 38,007 cycles

PASSENGER CABIN, AFT WET AREA FLOOR STRUCTURE BS 1681, LBL 54 TO RBL 54, FLOORBEAM HAD SEVERAL NUT PLATE STRIPS CORRODED. REMOVED CORROSION IAW SRM 51-10-02, PG 12, PARA 15. BEYOND ALLOWABLE LIMITS OF SRM 53-00-51, FIG 101. CUT OUT THE DAMAGED AREA. FABRICATED AND INSTALLED A REPAIR IAW SRM 53-60-51, REPAIR 3.

Part: POWER SUPPLY — INOPERATIVE (EMEGENCY LIGHTS) · airframe 82,067 hrs · 37,942 cycles

AFT RIGHT CABIN EMERGENCY LIGHTS INOPERATIVE. REMOVED AND INSTALLED POWER SUPPLY M736 IAW AMM 33-51. REPLACED THE BATTERY, OPS CHECKED GOOD IAW AMM 33-51.

Part: SKIN — DENTED (BS 650) · airframe 82,019 hrs · 37,917 cycles

FUSELAGE SKIN, BS 650 ABOVE STRINGER 26R LAP SPLICE DENTED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 80,611 hrs · 37,211 cycles

FOUND AFT RT SECTION EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK TO M736 POWER SUPPLY IN REF TO AMM 33-51-07 OPS CHECK GOOD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 80,522 hrs · 37,158 cycles

EMERGENCY LIGHTS BATTERY PACK BAD. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-16. OPS CHECKED GOOD.

Part: WIRE — SHORTED (EMEGENCY LIGHTS) · airframe 80,522 hrs · 37,158 cycles

ROW 2 SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. FOUND A SHORT IN THE WIRES WHICH TOOK OUT THE POWER SUPPLY. REMOVED AND REPLACED POWER SUPPLY BATTERY AND REPAIRED WIRE HARNESS IAW AMM 33-51-16. OPS CHECKED GOOD.

Part: WIRE — SEPARATED (CABIN) · airframe 78,709 hrs · 36,223 cycles

EMERGENCY ESCAPE PATHLIGHT INOPERATIVE AT 38R. FOUND WIRES SEPARATED FROM QUICK RELEASE, RETERMINATED WIRE END AND REINSTALLED IAW SWPM, CKS GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 76,937 hrs · 35,503 cycles

SEAT MOUNTED EMERGENCY ESCAPE PATH WHITE ON 43D INOPERATIVE. RELAMPED NO HELP. FWD TO MEL 33-51-03A. NEED MPN 0201720-001, STK 07-3300-3-0210. PART NIS, ACFT OK FOR SERVICE. FOUND DISCONNECTED UNDERSEAT, OPS CKS GOOD, PLACARD REMOVED.

Part: SEQUENCE VALVE — MALFUNCTIONED (LT MLG DOOR) · airframe 76,937 hrs · 35,503 cycles

PERFORMED AN AIR TURNBACK AFTER TAKEOFF DUE TO AN EICAS MESSAGE OF GEAR DISAGREE AFTER RAISING THE LANDING GEAR HANDLE. THE LT GEAR STAYED DOWN AND INDICATED GREEN. THE CREW LOWERED GEAR HANDLE AND RECEIVED A NORMAL GEAR DOWN INDICATIONS. T/S IAW FIM 32-30-00-815-818. REPLACED LT DOOR-OPERATED GEAR SEQUENCE VALVE IAW AMM 32-30-05. OPS CHECK WAS GOOD.

Part: MOUNT — CORRODED (LT WING) · airframe 76,929 hrs · 35,496 cycles

LT WING NR 4 FLAP TRANSMISSION MOUNT, BOLT HOLES ARE CORRODED. NR FOR ADDITIONAL INFORMATION 001-0269:2020-2339/037 00280, COMPLIED WITH ERA 541133-14AD, REV ORIGINAL.

Part: BALL SCREW — CORRODED (TE FLAP) · airframe 76,908 hrs · 35,481 cycles

NR 3 FLAP TRACK BALL SCREW RUSTED. INSTALLED BALL SCREW ASSY IAW AMM.

Part: SHAFT — CORRODED (NR 7 FLAP) · airframe 76,908 hrs · 35,481 cycles

NR 7 FLAP BALLSCREW SHAFT CORRODED AT DRIVE YOLK CONNECTION. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0079:2751-2541-RT/003 00262 REPLACE BALLSCREW ASSY IAW AMM 27-51-21.

Part: BALL SCREW — CORRODED (NR 2 FLAP) · airframe 76,908 hrs · 35,481 cycles

NR 2 FLAP DRIVE BALL SCREW SHAFT IS CORRODED AT YOLK DRIVE ATTACH POINT. REPLACED BALL SCREW ASSY IAW AMM 27-51-21.

Part: BALL SCREW — CORRODED (NR 1 FLAP) · airframe 76,908 hrs · 35,481 cycles

NR 1 FLAP BALLSCREW SHAFT CORRODED AT DRIVE YOLK CONNECTION. REPLACED BALL SCREW ASSY IAW AMM 27-51-21.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 76,439 hrs · 35,293 cycles

STA 140 BULKHEAD OUTER RING CHORD CRACK STR 20L & 20R. REPAIRED IAW ERA 522134-14.

Part: SENSOR — FAILED (BUSS VOLTAGE) · airframe 74,891 hrs · 34,611 cycles

AIRCRAFT, PERFORMED AN AIR TURN BACK DUE TO F/O INSTRUMENT FAILURE FOLLOWED BY ACFT SHUTTER AND YAW. CREW ALSO REPORTED LT ENG RUMBLE/SURGE AND LT ENG LIMIT EICAS MESSAGE. FOUND M10375 F/O INST BUS VOLT SENSE UNIT BLOWN OUT. REPLACED F/O INSTRUMENT BUS VOLTAGE SENSE UNIT M10375 IAW AMM 24-51-08. TESTS GOOD.

Part: LIGHT — INOPERATIVE (SEAT 27D) · airframe 74,295 hrs · 34,357 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT 27D. REPLACED THE LIGHT ASSY. OPS CHECKS GOOD, REF AMM 33-52.

Part: SENSOR — DIRTY (GIRT BAR) · airframe 74,079 hrs · 34,240 cycles

L2 SLIDE LIGHT DIM, CLEANED DEBRI FROM SENSOR ON GIRT BAR ATTACHMENT POINT. OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,028 hrs · 34,214 cycles

SEAT 31D EMERGENCY LIGHT INOPERATIVE. REPLACED THE EMERGENCY LIGHT ASSY, OPS CHECKED GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,435 hrs · 33,521 cycles

FOUND EVERGENCY LIGHTS ON SEATS 38D TO 45D INOPERATIVE. REPLACED CHARGER. OPS CHECKED GOOD.

Part: BATTERY — MISINSTALLED (R2 DOOR SLIDE) · airframe 71,853 hrs · 33,257 cycles

FOUND BATTERY AT R2 DOOR SLIDE MISCONFIGURED. REMOVED & REPLACED BATTERY IAW CARD 2560-01523-01A.

Part: OVEN — ODOR (GALLEY) · airframe 71,853 hrs · 33,257 cycles

F/A REPORTED FIRST CLASS GALLEY HAS ELECTRICAL BURN ODOR. R & R FWD GALLEY OVEN ASSY IAW AMM 25-31-05.

Part: SLIDE — INOPERATIVE (LT OVERWING) · airframe 71,411 hrs · 33,069 cycles

DURING AN INADVERTENT DEPLOYMENT OF THE LT OVERWING SLIDE. SLIDE DID NOT FULLY DEPLOY. LEFT OVERWING SLIDE REPLACED IAW AMM 25-65.

Part: SKIN — GOUGED (BS 500-520) · airframe 70,926 hrs · 32,869 cycles

FS 500-520 S26-27R SKIN GOUGEED. REPAIRED IAW ERA 498888-14 REV D SECTION LLL.

Part: UNKNOWN — ODOR (FWD CABIN) · airframe 70,326 hrs · 32,614 cycles

EXPERIENCED SMOKEAND FUMES OF A RUBBER ODOR IN FORWARD CABIN ROWS 1 & 2 AFTER PUSHBACK AND ENGINE START. INSPECTED ALL ELECTRICAL ITEMS IN FORWARD GALLEY, LIGHTING BALLASTS, AND FIXTURES; INSPECTED RIGHT RECIRCIRCULATION FAN, AND RAN ENGINES, NO ODORS NOTED.

Part: UNKNOWN — ODOR (GALLEY) · airframe 70,187 hrs · 32,561 cycles

ACRID ODOR COMING FROM FWD GALLEY AREA. POWERED UTILITY BUSSES AND FULLY LOADED DOWN F/C GALLEY COMPONENTS, NO ODOR NOTED. ALSO, THOROUGHLY INSP E/E ELEC PANEL COMPONENT WITH NO ODOR OR ANOMALLY NOTED.

Part: BALLAST — DAMAGED (CABIN LIGHTS) · airframe 70,096 hrs · 32,531 cycles

F/A REPORTED ELECTRICAL SMOKE ODOR IN FORWARD JUMPSEAT GALLEY AREA. FOUND OVERHEAD GALLEY LIGHTS BALLAST BAD AND CREATING ODOR. R AND R BALLAST AND LAMPS. CKS GOOD, AMM 25-31 AND AMM 33-27.

Part: SKIN — DAMAGED (AFT CARGO DOOR) · airframe 70,096 hrs · 32,531 cycles

DURING INSPECTION, MX FOUND THE FWD AND AFT CORNERS OFTHE AFT CARGO DOOR EXTERIOR SKIN BENT. REMOVE DAMAGE AND INSPECTED, REPAIRED IAW ERA 499672-14.

Part: ENGINE — FAILED (NR 2) · airframe 69,191 hrs · 32,185 cycles

RT ENGINE FAILED ON TAKEOFF AT 1000 FT AGL. REPLACED ENGINE IAW 6T103.

Part: BOTTLE — LOW PRESSURE (R4 DOOR SLIDE) · airframe 68,499 hrs · 31,898 cycles

R4 DOOR SLIDE RAFT LOW PRESSURE INDICATING IN RED. R & R SLIDE IAW OPEN 7809, CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,947 hrs · 31,699 cycles

OVERHEAD EMERGENCY LIGHTS OUT, SEATS 36C,43C AND 45D. LAMPED OPS CHECKED GOOD.

Part: SQUIB — INOPERATIVE (EVAC SLIDE) · airframe 65,900 hrs · 30,810 cycles

DURING SERVICE CHECK LEFT EMERGENCY SLIDE BOTTLE SQUIB TEST FAILED TO ILLUMINATE GREEN LIGHT. REPLACED SQUIB AND RELAYS, ALL TEST NORMAL.

Part: SKIN — DENTED (BS 518 S27R) · airframe 65,444 hrs · 30,604 cycles

FUSELAGE HAS TWO GOUGED DENTS BS 518 S27R. FOUND OUT OF LIMITS IAW SRM 53-00-01 PG 104 FIG 101 DETAIL II. ACCOMPLISHED ERA 498888-14 AD REV ORIG.

Part: SKIN — DENTED (BS 400-420) · airframe 65,444 hrs · 30,604 cycles

LARGE AREA DENT ON FUSELAGE BS 400-420 BETWEEN S27 AND 28R. DENT OUT OF LIMITS DUE TO BEING WITHIN 10 INCHES OF NLG CUTOUT. ACCOMPLISHED REPAIR PER ERA 498903-14 REV ORIG.

Part: FRAME — DENTED (BS 1520 S26L) · airframe 65,444 hrs · 30,604 cycles

AFT CARGO FRAME DENTED STA 1520 ABOVE STR 26L. FABBED AND INSTALLED REPAIR DOUBLER AT STA 1520 S26L PER SRM 53-00-07 REPAIR 5. THIS IS A CAT B W/THRESHOLD REP. INSP TO START AT 50,000 FLT CYC.S ZONE 1 HFEC INTERVAL EVERY 12,000 FLT CYCS PER NDT PART 6 51-00-01 AND DETAILED INSP EVERY 12,000 FLT CYC.S PER SRM 53-00-07 TABLE II PG 20 REPAIR 5 PG 210 ACFT HAS 30604.0 FLT CYCS REF SAA NRC 193389.

Part: SHEAR TIE — DENTED (BS 1420 S28L-29R) · airframe 65,444 hrs · 30,604 cycles

FUSELAGE CREASED AT SHEAR TIES 3 PLACES STA 1420 FROM S28L - 29R. FABRICATED AND REPLACED SHEAR TIES IAW SRM 53-00-01 REPAIR 11 PG 201 FIG 201.

Part: BULKHEAD — GOUGED (NR 1 NACELLE) · airframe 65,444 hrs · 30,604 cycles

NR 1 PYLON O/B SIDE AT NAC 201.02 BULKHEAD LWR AREA IS GOUGED. FABRICATED AND INSTALLED FILLER PER ERA 499654-14 AD REV ORIG AT SAA DURING HMV ON NRC 186752.

Part: FRAME — DENTED (BS 1500 S23L) · airframe 65,444 hrs · 30,604 cycles

AFT CARGO FRAME DENTED BS 1500 ABOVE S23L. DENTS NOT ALLOWED IAW SRM 53-00-07 FIG 101. FABRICATED AND INSTALLED REPAIR DOUBLER AND REPAIR CLIPS PER SRM 53-00-07 REPAIR 5 PG 201 PARA 4 AND PARA 10 AND 11. THIS IS A CAT B WITH THRESHOLD REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 960-982) · airframe 65,444 hrs · 30,604 cycles

MAIN CABIN FLOOR CUSP ANGLE ASSY CORRODED STA 960-982 LT. FABRICATED AND REPLACED ANGLE IAW SRM 51-40-02 PG 7 PAR 70 AT SAA DURING HMV ON NRC 186440.

Part: FRAME — DENTED (BS 1380 S25L) · airframe 65,444 hrs · 30,604 cycles

AFT CARGO FRAME DENTED AT BS 1380 ABOVE S25L. DENT NOT ALLOWED IN THIS AREA PER SRM 53-00-07 FIG 101. TRIMMED OUT AREA AND REMOVED REPAIR SPLICE AND FABRICATED AND INSTALLED REPAIR DOUBLER AND CLIP PER SRM 53-00-07 FIG 201 REPAIR 5.

Part: FRAME — DENTED (BS 1340 S26L) · airframe 65,444 hrs · 30,604 cycles

AFT CARGO FRAME DENTED ON UPPER FLANGE STA 1340 O/B STR 26L. TRIMMED OUT DAMAGED AREA, FABBED REPAIR SECTION AND CLIP PER 757 SRM 53-00-07 REPAIR 5 PG 201 PAR 4 AND INSTALLED PER 757 SRM 53-00-07 REPAIR 5 PG 201 PARS 10 AND 11. THIS IS A CAT B WITH REPETATIVE INSP THRESHOLD INSP TO START AT 50,000 FLT CYCS WITH REPETATIVE HIGH FREQ EDDY CURRENT EVERY 12,000 FLT CYCS PER NDT 51-00-01 PART 6 AND DETAILED INSP EVERY 12,0000 FLT CYCS PER ZONE 1. A/C HAS 30,604.0 FLT CYCS. REF SAA NRC 193799.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 65,444 hrs · 30,604 cycles

MAIN CABIN FLOOR CUSP WEB CORRODED STA 1400-1420 RT. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER 53-60-13 FIG 101 DETAIL III. REMOVED AND REPLACED CUSP WEB STA 1400-1420 PER B757 SRM 51-40-02 PG 4 DURING HMV. REF NRC 186438.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 65,444 hrs · 30,604 cycles

MAIN CABIN FLOOR CUSP WEB CORRODED STA 960-984 RT. FOUND OUT OF LIMITS PER SRM 53-40-13 PG 103 DETAIL V FIG 101. INSTALLED CUSP WEB AT STA 960-984 RT PER SRM 51-40-02 PG 34 DURING HMV ON N/R CARD 186442.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 65,444 hrs · 30,604 cycles

MAIN CABIN FLOOR CUSP WEB CORRODED STA 996-1020 RT. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-40-13 PG 103 FIG 101 DETAIL III. FABRICATED AND INSTALLED CUSP WEB AT STA 996-1020 RT IAW SRM 51-40-02 GEN PG 7 PARA D DURING HMV. REF NRC 186441.

Part: GATE — CORRODED (L2 DOOR) · airframe 65,444 hrs · 30,604 cycles

L2 DOOR LOWER GATE BOTTOM EDGE CORRODED. FOUND TO BE OUT OF LIMITS DUE TO 40 PERCENT MATERIAL LOSS. REPLACED LOWER GATE PER AMM 52-11-38-404-009 ADJUSTMENT AND OPS CHECK ACCOMPLISHED ON ACJIC CARD 78005 AT SAA DURING HMV ON N/R CARD 186016.

Part: GATE — CORRODED (R1 DOOR) · airframe 65,444 hrs · 30,604 cycles

R1 DOOR LOWER GATE AND SEAL RETAINER GOUGED AT AFT LWR CORNER AND BOTTEM EDGE OF GATE IS CORRODED. CORROSION OUT OF LIMITS. REMOVED AND REPLACED LOWER GATE AT R1 DOOR IAW AMM 52-11-38-404-009 AT SAA DURING HMV. REF NRC 186079.

Part: BEAM — CORRODED (FUSELAGE) · airframe 65,444 hrs · 30,604 cycles

UPON REMOVAL OF FLOOR BOX BEAM FOUND CORROSION ON UNDER SIDE OF WEB MAIN CABIN STA 700-720 LBL 62. FABRICATED AND INSTALLED NEW WEB FROM STA 685-730 LBL 65 PER SRM 51-40-02 PAGES 2 AND 7 DURING HMV ON N/R CARD 198214.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 65,444 hrs · 30,604 cycles

MAIN CABIN FLOOR AFT SHEAR PLATE CORRODED STA 1680-1720 BL 0 LBL 54. MATERIAL LOSS .016 AT AREA 1 ZONE STA 1680-1681 LBL 11.4-12.5 FOUND OUT OF LIMITS. INSTALLED DOUBLER AND FILLER AT STA 1680-1685 LBL8-16 PER B757 SRM 53-60-51 FIG 201 REPAIR 2 AT SAA DURING HMV. REF NRC 185931.

Part: SHEAR PLATE — CORRODED (BS 1680-1720) · airframe 65,444 hrs · 30,604 cycles

MAIN CABIN AFT SHEAR DECK CORRODED BS 1680-1720 BL0 RBL 54. FABRICATED AND INSTALLED REPAIR DOUBLER AT STA 1680-1686 RBL 75-50 REF SRM 53-60-51 FIG 201.

Part: SKIN — DENTED (BS 620-640) · airframe 65,444 hrs · 30,604 cycles

FIVE DENTS OF FUSELAGE STA 620-640 BETWEEN STR 14L AND 16L AND CREASE ON SHEAR TIE BS 620 ABOVE STR 16L. FOUND TWO DENT OUT OF LIMITS IAW B757 SRM 53-00-01 ALLOWABLE DAMAGE PG 104 FIG 101 DET 3. HFEC INSPECTION IAW NDTM 51-00-19 PT6 NO CRACKS NOTED IN FIVE DENTS. COMPLIED WITH PR/I 498881-14 REV 4, PREPPED AND PAINTED FUSELAGE REPAIR AREA IAW B757 AMM 51-21-10-377-003. ACCOMPLISHED ER/A 498881-14 REV A.

Part: DOOR — CORRODED (AFT CARGO BAY) · airframe 65,444 hrs · 30,604 cycles

AFT CARGO DOOR INTERNAL FWD WEB ANGLE HAS CORROSION. REMOVED CORROSION IAW SRM 52-30-02, FOUND OUT OF LIMITS. REMOVED AND REPLACED AFT CARGO DOOR IAW AMM 52-34-01-404.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 65,444 hrs · 30,604 cycles

MAIN CABIN SEAT TRACK GOUGED AND CORRODED STA 440-645 RBL 45. BLENDED GOUGES AND CORROSION, FOUND TO BE OUT OF LIMITS DUE TO TO MATERIAL REMAINING ON LIP OF SCALLOP. REMOVED DAMAGE SECTION, FABRICATED AND INSTALLED IAW B757 SRM 53-00-52 DURING HMV AT ST AEROSPACE SAN ANTONINO.

Part: BULKHEAD — GOUGED (NR 1 NACELLE) · airframe 65,444 hrs · 30,604 cycles

NR 1 PYLON INBOARD SIDE NAC STA 201.02 BULKHEAD LOWER AREA GOUGED. REMOVED .020 MATERIAL DAMAGE REF SRM 54-51-02 PG 104. DAMAGED STILL REMAINS. REMOVED A TOTAL OF .034 MATERIAL. NO DAMAGE PRESENT. HFEC SURFACE INSPECTION IAW DDTM 51-00-19 PT6, NO CRACKS. COMPLIED WITH PR/I 499654-14AD REV O. FABRICATED FILLER IAW ER/A 499654-14AD REV O PG 1 ITEM 5. COMPLIED WITH ER/A 499654-14AD REV ORIG.

Part: STRINGER — BENT (BS 690 S2R) · airframe 65,444 hrs · 30,604 cycles

WHILE WORKING ROUTINE EA 06-085867-03 0101, FOUND STRINGER STA 690 S2R BENT. REPAIRED IAW SRM 51-00-05.

Part: GATE — CORRODED (L4 DOOR) · airframe 65,444 hrs · 30,604 cycles

L4 DOOR LOWER GATE HAS CORROSION AT LOWER EDGE. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 52-10-02. REMOVED AND REPLACED LOWER DOOR GATE IAW AMM 52-11-38-404-009.

Part: FRAME — DENTED (FUSELAGE) · airframe 65,444 hrs · 30,604 cycles

FWD CARGO FRAME DENTED ABOVE STR 23L AND BENT AT UPPER FLANGE STR 23-25L AT STA 580. CUT OUT DAMAGE AREA AT STR 23L PER SRM 53-00-07 FIG 201 REPAIR 5. FABRICATED REPAIR ANGLE PER B757 SRM 53-30-07 FIG 201 REPAIR 5 AT SAA' SAT DURING HMV ON N/R 186856 W/O 89678500001.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,444 hrs · 30,604 cycles

MAIN CABIN FLOORBEAM CORRODED ON UPPER SURFACE STA 1640 LBL 59-RBL 59. CORROSION ON EXISTING REPAIR FROM LBL 13- RBL 9 OUT OF LIMITS. REMOVED EXISTING REPAIR AND FLOORBEAM TO LBL 35 FABRICATED AND INSTALLED FLOORBEAM AND REPAIR ANGLES IAW B757 SRM 53-00-51 DURING HMV AT ST AEROSPACE SAN ANTONIO.

Part: FILL PORT — CORRODED (RT WING) · airframe 65,444 hrs · 30,604 cycles

RT WING OVERWING FILL PORT FAILED BONDING CHECK BETWEEN ADAPTER AND UPPER SKIN. REMOVED FILL PORT. REMOVED CORROSION ON MATING SURFACE IAW SRM 57-20-01 FIG10. HFEC INSPECTION IAW NDTM PT6 51-00-19, NO CRACKS OR CORROSION. FPI PER SOPM 20-20-02 NO CORROSION. COMPLIED WITH ER/A 498907-14AD REV ORIG.

Part: SKIN — DENTED (BS 450) · airframe 65,444 hrs · 30,604 cycles

FUSELAGE DENTED BELOW LAP STA 450 AT STR 14L FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL 3. HFEC INSPECTION PER NDTM PT6 51-00-19, NO CRACKS NOTED. REMOVED PAINT PERFORMED SCRIBE LINE INSPECTION PER PRI 498897-14 REV 0 AT BS 459-557. DEPTH OF SCRIBE LINE RANGE FROM .001 TO .0015. PAINTED FUSELAGE PER AMM 51-21-10-377-003. COMPLIED WITH ER/A 498897-14AD REV ORIG.

Part: SKIN — DENTED (BS 1655 S20L) · airframe 65,444 hrs · 30,604 cycles

FUSELAGE DENTED BELOW LAP AT S20L BS 1655. FOUND DENT TO BE OUT OF LIMITS IAW SRM 53-00-01 PG 104 FIG 101 DETAIL 3. HFEC SURFACE INSPECTION IAW NDTM PT.6 51-00-19. NO CRACKS NOTED AT DENTED AREA. CHEMICALLY REMOVED PAINT ON EXTERIOR SKIN FROM BS 1420-1720 S20L IAW PR/I 498900-14 REV O STEP 1 AND AMM 51-21-157-011. ACCOMPLISHED PR/I 498900-14 REV O. COMPLIED WITH ER/A 498900-14AD REV ORIG. TREATED PRIMED BS 1420-1720 S20L IAW SRM 51-20-01 PG 3-7 & 27 TOPCOAT IAW AMM 51-21-10-377-003 PG 1.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 64,268 hrs · 30,106 cycles

DURING A LAYOVER CHECK, MX FOUND THE EMERGENCY PATHLIGHT AT ROW 40D INOPERATIVE. MX REPLACED THE LIGHT CONNECTOR. OPS CHECK WAS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,357 hrs · 29,662 cycles

DURING LAYOVER CHECK, MAINTENANCE FOUND THE RED EMERGENCY PATH LIGHT AT THE FWD GALLEY WALL INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD. (2010-D1234) (DL757102765)

Part: GEAR — FAILED (TE FLAP XMSN) · airframe 63,127 hrs · 29,547 cycles

TRAILING EDGE FLAP TRANSMISSION GEAR REPLACED IAW EA 06-097281-03, ME04.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 62,874 hrs · 29,433 cycles

DURING LAYOVER CHECK, MX FOUND THE RED EMERGENCY PATH LIGHT AT 26D INOPERATIVE. MX REPLACED THE SEAT WIRE HARNESS. OPS CHECK WAS GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 61,778 hrs · 28,946 cycles

FUSELAGE SKIN STA 553 BELOW S-26L LAP DENT. REPAIRED IAW ERA 099678-14.

Part: SKIN — DENTED (BS 650 S26R) · airframe 61,434 hrs · 28,764 cycles

FUSELAGE DENT STATION 650 JUST ABOVE S26R LAP SPLICE. REPAIRED IAW ERA 479928-14J.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 59,141 hrs · 27,494 cycles

UNINTENTIONAL DEPLOYMENT OF L1 DOOR SLIDE BY CONTRACT CLEANING CREW AT THE GATE. REMOVED AND REPLACED L1 SLIDE AND ASSIST BOTTLE IAW AMM.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 58,468 hrs · 27,174 cycles

FUSELAGE -SECTION 46 DOOR NR 4 AFT FRAME BODY STATION 1. REPAIRED IAW EA 06-465922-03, ME02.

Part: SKIN — DENTED (FS1698 S19L) · airframe 50,501 hrs · 23,691 cycles

FUSELAGE SKIN FS 1698, STR 19L DENT REPAIRED IAW ERA 092627-14.

Part: SKIN — DEFORMED (FUSELAGE) · airframe 47,189 hrs · 22,518 cycles

THE FUSELAGE SKIN AND BEARSTRAP WERE DENTED AT LOWER AFT CORNER OF THE FORWARD CARGO DOORWAY. INSTALLED REPAIR DOUBLERS.

Part: SKIN — GOUGED (BS 1694 S-14L) · airframe 47,189 hrs · 22,518 cycles

THE FUSELAGE SKIN WAS FOUND DENTED AND GOUGED AT STA 1694 BELOW THE S-14L LAP JOINT. DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED.

Part: RAM AIR TURB — MALFUNCTIONED · airframe 47,189 hrs · 22,518 cycles

DURING HMV3PSV19 ROUTINE OPN 6002 WAS BEING PERFORMED TO TEST THE RAM AIR TURBINE DEPLOYMENT SYSTEM. THE RAT FAILED TO DEPLOY TO FULL EXTEND AND LOCK POSITION. MTC CLEANED AND LUBED LINKAGE, DOOR HINGES AND ADJUSTED COMPARTMENT DOOR LINKAGE PER MM. RAT WAS RETESTED PER MM 29-21-00-735-143, OPERATION WAS NORMAL.

Part: WHEEL — DAMAGED (NLG) · airframe 38,902 hrs · 19,068 cycles

ON TAXI OUT BHM, NOSE GEAR STEERING GOT VERY WOBBLY, CALLED MTC, THAY FOUND THE RIGHT NOSE GEAR TIRE ASSEMBLY TO HAVE COME APART. SUSPECT OUTER BEARING FROZEN. REMOVED AND REPLACED NOSE WHEEL.

Part: AXLE — SHEARED (NLG) · airframe 38,849 hrs · 19,038 cycles

A/C NOSE LANDING GEAR RT AXLE SHEARED ON TAXIWAY, HAD TO REPLACE NOSE LANDING GEAR PISTON.

Part: FAN — FAILED (E/E BAY) · airframe 34,417 hrs · 16,979 cycles

EQUIPMENT OVERHEAT LIGHT ON AND ALSO HAD A LIGHT ODOR IN COCKPIT. REPLACED NR 1 FWD EQUIPMENT COOLING FAN AND CLEANED FILTER.OPS OK.

Part: SKIN — DENTED (BS 620)

DURING THE CURRENT HMV, ADDITIONAL DAMAGE WAS FOUND LOCATED TO AN EXISTING SKIN REPAIR. THE SUBJECT SKIN REPAIR WILL BE REMOVED AND A LARGER REPAIR ENCOMPASSING BOTH DAMAGES INSTALLED. REPAIRED PER ERA 362260-14, REV C.

Part: SKIN — DENTED (BS 1690-1700)

FUSELAGE SKIN FS 1690-1710, STRINGER18L, DENT REPAIR. THE FUSELAGE SKIN WAS DENTED JUST BELOW STRINGER 18L BETWEEN FS 1690 AND FS 1710. THE DAMAGE WAS REMOVED WITH TWO SKIN CUTOUTS. THE CUTOUTS WERE REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367505-14, REV C.

Part: SKIN — DAMAGED (BS 1276)

FUSELAGE SKIN FS 1276, STRINGER 4R, LIGHTNING STRIKE REPAIR. THE FUSELAGE SKIN WAS STRUCK BY LIGHTNING AT FS 1276 AND STRINGER 4R. THE DAMAGE WAS REMOVED FROM THE UPPER SKIN WITH AN APPROX 2 CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367569-14, REV A.

Part: SKIN — DENTED (BS 500)

DENT FOUND IN FUSELAGE SKIN AT BS 500 BELOW S26R. DAMAGE CUTOUT IS APPROX 4 BY 6. REPAIRED PER ERA 367513-14.

Part: SKIN — DENTED (BS 1700)

TWO DENTS WERE FOUND AT BS 1690 AND BS 1710, EACH BELOW S18L. REPAIRED PER ERA 367505-14.

Part: SKIN — DAMAGED (BS 620)

WHILE ACCOMPLISHING PERM REPAIR PER ORIGINAL ISSUE OF ERA 362260-14, ADDITION DAMAGE (TOOLING DAMAGE) WAS FOUND, NECESSITATING A LARGER SKIN CUTOUT. REPAIRED PER ERA 362260-14, REV B.

Part: COFFEEMAKER — FAILED (GALLEY)

MID GALLEY AT 2L DOOR AFT SEC COFFEEMAKER BEGAN SMOKING, MODERATE AMOUNT ACRID SMOKE-POWER SECURED. ALL C/B ASSOCIATED WITH GALLEY PULLED, SMOKE STOPPED IT TOOK 10 MIN FOR HEAT TO STOP COMING FROM TOP CORNER AREA, COOLED SLOWLY. NOTE AT ONE TIME BULKHEAD AFT OF GALLEY WAS WARM TO TOUCH. WATER STARTED LEAKING BAD. SECURED WATER VLV. FOUND WATER MAKER BURNED UP. WATER DISCONNECT LEAKING. ELECT AND WATER DISCONNECTED ON NEW COFFEEMAKER. NEED WATER HOSE ASSY.

Part: COFFEEMAKER — FAILED (GALLEY)

SMOKE IN CABIN AT LT MID GALLEY FROM AFT COFFEEMAKER. C/B PULLED, SMOKE STOPPED. REPLACED COFFEEMAKER.

Part: CONNECTOR — LOOSE (CABIN)

AFT EMERGENCY LIGHTING INOP. RESECURED CONNECTOR.

Part: ENGINE — FAILED (NR 2)

NR 2 ENGINE STALLED WITH LOSS OF OIL PRESSURE AND ENGINE ROLL BACK. REPLACED ENGINE PER 6T103.

Part: GIRT BAR — DETACHED (2 R DOOR)

P/R - EMERGENCY SLIDE WILL NOT ARM 2R. REATTACHED ENGAGEMENT LUG TO GIRT BAR, CKS GOOD.

Part: BOLTS — SHEARED (NR 1 ENGINE)

LEFT ENGINE FWD MOTOR MOUNT, I/B SIDE THRUST LINK ROD FWD ATTACHMENT TO FAN, HAS 8 BOLTS DAMAGED OR MISSING. ALL FOUR OUTER BOLTS SHEARED, 1 INNER BOLT SHEARED WITH REMAINING 3 DAMAGED. REPLACED CLEVIS DL (P/N 726701473). REMOVED 099 INNER BOLT DL (P/N 726201036), OUTER BOLT DL (P/N 726201037), 4 OF BOTH BOLTS MM 71-21-01-4 IPC 72-00-33.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

ON LAYOVER, L-1 AND R-1 DOOR EMERGENCY EXIT LIGHS FAIL TO TEST. REPLACED POWER SUPPLY, OPERATION NORMAL.