N939UW

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 81,151 hrs · 28,844 cycles

AIRCRAFT WAS NOT GROUNDED: 2L INBOARD FLASHLIGHT INOPERABLE. MAINTENANCE REPLACED FLASHLIGHT PER STANDARD PRACTICES.

Part: CONTROL BOX — BINDING (RT ENGINE) · airframe 80,456 hrs · 28,650 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS RT THROTTLE STUCK, VERY HARD TO MOVE ON APPROACH, ONE KNOB ABOVE IDLE. AUTO-THROTTLE WAS OFF. MAINTENANCE REMOVED AND REPLACED RT ENG LWR CONTROL BOX. COMPLIED WITH ALL TEST AND ADJUSTMENTS IAW AMM 76-11-10-404-015-ROO AND 76-11-00-825-046-R00. ALL OPS CHECKS GOOD.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 79,849 hrs · 28,515 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS R1 DOOR SLIDE PRESSURE LOW. REMOVED AND REPLACED R1 DOOR EVAC/SLIDE RAFT IAW CARD 19L80025002.

Part: STRAP — CRACKED (BS 377) · airframe 78,763 hrs · 28,264 cycles

CRACKED FLOORBEAM STABILIZER STRAP AT BS 377.7, LBL 24.75. REPLACED THE STRAP IAW SRM 53-10-51-2R-1.

Part: STRINGER — CORRODED (BS 1620-1640) · corrosion level 2 · airframe 78,759 hrs · 28,263 cycles

CORROSION FOUND ON STRINGER 29, BETWEEN BS 1620 AND 1640. REPAIRED THE STRINGER IAW EA 289704.

Part: TRANSITION PANEL — CORRODED (BS 1440-1520) · airframe 78,759 hrs · 28,263 cycles

CORROSION FOUND ON THE AFT CARGO RIGHT TRANSITION PANEL, BS 1440 AND 1520. REPLACED THE TRANSITION PANEL IAW SRM 53-00-53-2R-2, AND 51-40-02-0G.

Part: TRANSITION PANEL — CORRODED (BS 1310-1380) · airframe 78,759 hrs · 28,262 cycles

CORROSION ON THE AFT CARGO COMPARTMENT RIGHT SIDE TRANSITION PANEL BETWEEN BS 1310 AND 1380. REPLACED THE TRANSITION PANEL IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1320-1340) · airframe 78,759 hrs · 28,262 cycles

CORROSION ON AFT THE AFT CARGO BAY FLOOR SUPPORT BETWEEN BS 1320 AND BS 1340, RBL 15. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: FLOORBEAM — CRACKED (BS 1460) · airframe 78,759 hrs · 28,263 cycles

AFT CARGO BAY LEFT SLOPING FLOOREBEAM, BS 1460. REPLACED THE FLOORBEAM IAW SRM 51-40-02.

Part: PANEL — CRACKED (WING-BODY) · airframe 77,834 hrs · 28,049 cycles

CRACKED RIGHT LEADING EDGE WING TO BODY PANEL 192AR. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED A REPAIR TO THE WING - BODY PANEL IAW EA 285262.

Part: UNKNOWN — MALFUNCTIONED (ZONE 700) · airframe 75,181 hrs · 27,459 cycles

AIRCRAFT WAS NOT GROUNDED: AFTER TAKEOFF, WHEN POSITIONED GEAR HANDLE TO OFF POSITION, THE GEARDOOR AMBER LIGHT ILLUMINATED WITH ENGINE INDICATION AND CREW ALERTING SYSTEM MESSAGE OF "GEAR DOOR". FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURE. WHEN GEAR HANDLE TO UP POSITIONED, GEAR DOOR LIGHT EXTINGUISHED. FLIGHT CONTINUED TO DESTINATION WITH NO EMERGENCY DECLARED. MAINTENANCE PERFORMED FAULT ISOLATION MANUAL PROCEDURE 32-30-00-0815-813, NO FAULT FOUND, CYCLED GEAR SEVERAL TIMES, ALL INDICATIONS REMAINED NORMAL AND REPLACED LEFT MAIN LANDING GEAR DOOR ACTUATOR AS PRECAUTIONARY. MAINTENANCE ALSO PERFORMED SATISFACTORY OPERATIONAL CHECKS.

Part: WIRE — OPEN (EMERGENCY LIGHT) · airframe 75,181 hrs · 27,459 cycles

AIRCRAFT WAS NOT GROUNDED. FOUND R-3 DOOR EMERGENCY EXIT LIGHT ABOVE DOOR INOPERATIVE. FOUND OPEN WIRE W3634-0011-20. REPAIRED WIRE PER CH. 20.

Part: LIGHT — DAMAGED (CABIN) · airframe 74,651 hrs · 27,334 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT AT THE L1 DOOR IS DAMAGED. REMOVED AND REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.

Part: SIGN — UNSECURE (CABIN) · airframe 73,778 hrs · 27,139 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN BY THE LOWER L1 DOOR IS NOT SECURED. REFITTED AND SECURED SIGN IAW AMM 33-51-10-402-047. OPERATIONAL CHECK GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 73,749 hrs · 27,133 cycles

EMERGENCY LIGHT AT ROW 25D HAS A MISSING LENS. INSTALLED THE LENS IAW AMM 33-51-05-002-001. OPS CHECKED GOOD.

Part: BRACKET — FOD (L4 DOOR GIRT BAR) · airframe 73,644 hrs · 27,109 cycles

L4 DOOR ARMED ALIGNMENT NEEDS TO BE CHECKED. REMOVED FOD FROM GIRT BAR FLOOR BRACKETS. OPERATIONAL CHECK GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT)

EMERGENCY EXIT IDENTIFIER AT THE L3 DOOR HAS A MISSING LENS. INSTALLED LENS IAW AMM 33-51-10. OPERATIONAL CHECKED GOOD.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 73,241 hrs · 26,998 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND BOTTOM FUSELAGE, WING TO BODY FAIRING SUPPORT (FRAME) STRUCTURE WEB AT STATION 800 BETWEEN STRINGER 29R-30R.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 73,241 hrs · 26,998 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND BOTTOM FUSELAGE, WING TO BODY FAIRING SUPPORT STRUCTURE WEB AT STATION 800 BETWEEN STRINGER 29L-30L. REPAIRED SUPPORT FRAME PER SRM 51-70-11-0G FIGURE 1, SHEET 1, REPAIR 2 AND SRM 51-40-02.

Part: SPRING — BROKEN (ZONE 800)

AIRCRAFT WAS IN BASE MAINTENANCE. R1 DOOR EVACUATION SLIDE MODE SELECT LEVER INDICATOR HAS A BROKEN SPRING. REMOVED AND REPLACED INDICATOR IAW SRM 51-40-02. OPERATIONAL CHECK GOOD.

Part: SPLICE PLATE — CORRODED (FAIRING) · airframe 73,241 hrs · 26,998 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON WING TO BODY FAIRING SPLICE PLATE AT STATION 800 AND BL-0. REPLACED SPLICE PLATE PER SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,241 hrs · 26,998 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FUSELAGE STRINGER 20L AT STATION 758. REPAIRED STRINGER PER SRM 53-00-03-2R-1 REPAIR 1.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 73,241 hrs · 26,998 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CARGO L3 EXIT DOOR LOWER SILL (WEB) AT STRINGER 17L BETWEEN STATION 1320 AND 1360. REPLACED LOWER SILL (WEB) PER SRM 51-40-02 AND 51-40-05.

Part: FRAME — CORRODED (FUSELAGE) · airframe 73,241 hrs · 26,998 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FRAME AT STRINGER 27L AND STATION 780. REPAIRED FRAME PER SRM 53-00-71-1A, SRM 51-40-05 AND SRM 51-40-02.

Part: SLAT — CRACKED (RT WING) · airframe 73,241 hrs · 26,998 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON OUTBOARD END OF RIGHT HAND WING SLAT NR 9. REPAIRED SLAT PER SRM 51-40-02 AND 51-40-05.

Part: PANEL — CRACKED (LE SLAT) · airframe 73,241 hrs · 26,998 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. LEADING EDGE 10 SLAT COVE PANEL HAS A 1 INCH CRACK BETWEEN WING STATION 707 AND 736. FABRICATED COVE PANEL AND INSTALLED IAW SRM 51-40-02 AND 51-40-05.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,241 hrs · 26,998 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT SIDE FORWARD CARGO, BETWEEN SKIN AND STRINGER 21L BETWEEN STATION 749 AND 754. REPAIRED STRINGER PER SRM 53-00-03.

Part: HARNESS — TORN (EVAC SLIDE) · airframe 73,242 hrs · 26,998 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. L1 DOOR EMERGENCY EVACUATION SLIDE HARNESS IS TORN. REMOVED AND REPLACED HARNESS ASSEMBLY IAW AMM 25-66-01-401 AND WORK CARD 19C83125004.

Part: HARNESS — TORN (EVAC SLIDE) · airframe 73,242 hrs · 26,998 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. R1 DOOR EMERGENCY EVACUATION SLIDE HARNESS IS TORN. REMOVED AND REPLACED HARNESS ASSEMBLY IAW AMM 25-66-01-401. OPERATIONAL CHECK GOOD.

Part: HARNESS — TORN (EVAC SLIDE) · airframe 73,242 hrs · 26,998 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. L4 DOOR EMERGENCY EVACUATION SLIDE HARNESS IS TORN. REMOVED AND REPLACED HARNESS ASSEMBLY IAW AMM 25-66-01-401 AND WORK CARD 19C83625004.

Part: STRAP — FRAYED (L2 DOOR) · airframe 70,322 hrs · 26,199 cycles

AIRCRAFT WAS NOT GNDED. BOTTOM PORTION OF HARNESS STRAP FRAYED & TORN. REPLACED L2 DOOR SLIDE IAW TASK CARD 19L80025002.

Part: COVER — CRACKED (CABIN) · airframe 69,960 hrs · 26,091 cycles

AIRCRAFT WAS NOT GNDED. FLOOR MOUNTED EMER PATH LIGHT COVER, BETWEEN 6D - 10D CRACKED. REPLACED COVER IAW AMM 33-51-00.

Part: LIGHT — INOPERATIVE (ZONE 800) · airframe 69,924 hrs · 26,082 cycles

AIRCRAFT WAS NOT GNDED. SLIDE LIGHT DOOR 4R OUT. REPLACED SLIDE LIGHT IAW AMM 33-10-00.

Part: ACTUATOR — DEFECTIVE (RT MLG) · airframe 69,891 hrs · 26,074 cycles

ACFT WAS GNDED. AFTER TAKEOFF CREW RECEIVED A GEAR DOOR OPEN MSG & RETURNED WHERE THE ACFT LANDED SAFELY WITH NO OTHER INCIDENTS REPORTED. NO EMER WAS DECLARED. ACCOMPLISHED FIM TASK 32-30-00-815-813 & FOUND THE RT MLG TRUCK POSITION, TILT, ACTUATOR WHICH WAS REPLACED IAW AMM 32-32-15-401. A SATISFACTORY OPERATIONAL CHECK OF THE LG DOORS WAS ACCOMPLISHED IAW AMM 32-35-00-501.

Part: TRACK — OBSTRUCTED (R1 DOOR) · airframe 69,425 hrs · 25,950 cycles

AIRCRAFT WAS NOT GNDED. 1R DOOR SLIDE DIFFICULT TO ARM. CLEARED TRACK & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BUSHING — WORN (GIRT BAR) · airframe 69,169 hrs · 25,880 cycles

AIRCRAFT IN BASE MX. L1 PAX ENTRY DOOR LOWER GATE, AFT GIRT BAR MECHANISM HAS EXCESSIVE PLAY. R & R 4 EACH BUSHING ON L1 DOOR LOWER GATE, AFT GIRT BAR MECHANISM IAW SOPM 20-50-03 R18.

Part: BUSHING — WORN (GIRT BAR) · airframe 69,169 hrs · 25,880 cycles

AIRCRAFT IN BASE MX. L1 PAX ENTRY DOOR, LOWER GATE FWD GIRT BAR MECHANISM & CRANK HAS EXCESSIVE PLAY. R & R 4 EA BUSHING ON L1 DOOR LOWER GIRT, FWD GIRT BAR MECHANISM IAW SOPM 20-50-03 R4.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 68,730 hrs · 25,743 cycles

NUMBER 3 SLAT LOWER SURFACE OTBD SIDE, 4" FROM OTBD EDGE HAS AREA OF DELAMINATION, APPROX 3" X 4" AGAINST EXTERIOR DOUBLER. R & R NR 3 SLAT IAW AMM 27-81-04-024-001. OPERATIONAL & FUNCTIONAL CHECKED GOOD.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 68,730 hrs · 25,743 cycles

NUMBER 2 SLAT UPPER SURFACE INBD EDGE HAS AREA OF DELAMINATION, APPROX .5" IN DEPTH BY 2" LONG. R & R NR 2 SLAT IAW AMM 27-81-04-024-001. OPERATIONAL & FUNCTIONAL CHECKED GOOD.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 66,990 hrs · 25,314 cycles

RIGHT WING INBD FLAP HAS AREA OF DELAMINATION, 42" IN FROM THE OTBD EDGE. REPAIRED RT WING INBD FLAP IAW SRM 57-53-01-R2 & SRM 51-70-10.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 66,551 hrs · 25,181 cycles

FORWARD LEFT FLIGHT ATTENDANT EMER FLASHLIGHT INOPERATIVE. R & R FLIGHT ATTENDANT EMER FLASHLIGHT BATTERY AT FWD LT POSITION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,412 hrs · 24,553 cycles

C4 CHECK EMER EXIT LIGHT OVER SEAT 1C INOPERATIVE. REPLACED EMER LIGHT IAW AMM 33-51-08-002-001. OPERATIONS CHECKED GOOD IAW AMM 33-01-00-715-039.

Part: WIRE — DISCONNECTED (CABIN) · airframe 64,411 hrs · 24,551 cycles

C4 CHECK CABIN EMER LIGHT INOPERATIVE ON ABOVE L2 DOOR. TROUBLE SHOT SYS IAW WDM 33-51-13. FOUND WIRE W3352-0151-20 PULLED OUT OF SPLICE D4550. APPLIED NEW PIN IN CONNECTOR D4550 IAW SWPM 20-10-13. SYS OPERATIONS CHECKED GOOD IAW MM 33-51-00-715-003.

Part: TERMINAL — DISCONNECTED (CABIN) · airframe 64,411 hrs · 24,551 cycles

C4 CHECK EMERGENCY LIGHT INOPERATIVE ON AFT LT CABIN STOWAGE BIN BY SEAT 27ABC. TROUBLE SHOT SYS IAW WDM 33-51-15. FOUND TERMINAL LUG DISCONNECTED. RECONNECTED LUG TO GND STUD GD492-DC IAW WDM 33-51-15. SYS OPERATIONS CHECKED GOOD IAW AMM 33-51-05-002-001.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON AFT CABIN DECK PLATE AT BS 1704, LBL 50. REPAIRED AFT CABIN DECK PLATE AT BS 1704, LBL 50 IAW SRM 53-60-51-2R, REPAIR 2.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON CREASE BEAM ANGLE BETWEEN BS 297 TO BS 324, RBL 62. REPLACED CREASE BEAM ANGLE BETWEEN BS 297 TO BS 324, RBL 62 IAW SRM 51-40-02.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 EXFOLIATION CORROSION ON WEB BETWEEN BS 297.7 TO BS 310.5, RBL 62. REPLACED WEB BETWEEN BS 297.7 TO BS 310.5, RBL 62 IAW SRM 51-40-02 & DWG 141N8422.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPP0RT CHANNEL BETWEEN BS 310 TO BS 324, RBL 45. REPLACED FLOOR SUPP0RT CHANNEL BETWEEN BS 310 TO BS 324, RBL 45 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN BS 324 TO BS 345, RBL 2. REPLACED FLOOR SUPPORT BETWEEN BS 324 TO BS 345, RBL 2 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN BS 324 TO BS 345, RBL 25. REPLACED FLOOR SUPPORT BETWEEN BS 324 TO BS 345, RBL 25 IAW SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT FITTING BETWEEN BS 297 TO BS 310, RBL 45. REPLACED FLOOR SUPPORT FITTING BETWEEN BS 297 TO BS 310, RBL 45 IAW SRM 51-40-02 & DWG 141N5161.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT CHANNEL AT BS 298 BETWEEN RBL 6 TO RBL 19. REPLACED FLOOR SUPPORT CHANNEL AT BS 298 BETWEEN RBL 6 TO RBL 19 IAW SRM 51-40-02.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT CHANNEL BETWEEN BS 345 TO BS 365, RBL 60. REPLACED FLOOR SUPPORT CHANNEL BETWEEN BS 345 TO BS 365, RBL 60 IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT BS 330 & BETWEEN RBL 26 TO RBL 38. REPLACED FLOOR SUPPORT AT BS 330 & BETWEEN RBL 26 TO RBL 38 IAW SRM 53-00-52 & 51-40-02.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT CHANNEL AT BS 298 BETWEEN RBL 21 TO RBL 35. REPLACED FLOOR SUPPORT CHANNEL AT BS 298 BETWEEN RBL 21 TO RBL 35 IAW SRM 51-40-02.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 FILIFORM CORROSION ON FLOOR SUPPORT CHANNEL AT BS 330 & BETWEEN RBL 5 TO RBL 23. REPLACED FLOOR SUPPORT CHANNEL AT BS 330 & BETWEEN RBL 5 TO RBL 23 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 FILIFORM CORROSION ON FLOOR SUPPORT CHANNEL BETWEEN BS 377 TO BS 395, RBL 10. REPLACED FLOOR SUPPORT CHANNEL BETWEEN BS 377 TO BS 395, RBL10 IAW SRM 51-40-02 & DWG 141N5167.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT FITTING BETWEEN BS 365 TO BS 377, RBL 60. REPLACED FLOOR SUPPORT FITTING BETWEEN BS 365 TO BS 377, RBL 60 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT CHANNEL BETWEEN BS 324 TO BS 345, RBL 60. REPLACED FLOOR SUPPORT CHANNEL BETWEEN BS 365 TO BS 345, RBL 60 IAW SRM 51-10-02, 51-40-02, 51-40-05 & AMM 51-21-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT STRUCTURE BETWEEN BS 720 TO BS 740, LBL 63. REPLACED FLOOR SUPPORT BETWEEN BS 720 TO BS 740, LBL 63 IAW SRM 51-40-02, 51-21-01, 51-10-02 & 51-21-15.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON L2 DOOR SILL SCUFF PLATE SUPPORT ANGLES BETWEEN BS 720 TO BS 740, LBL 67. REPLACED L2 DOOR SILL SCUFF PLATE SUPPORT ANGLES BETWEEN BS 720 TO BS 740, LBL 67 IAW SRM 51-40-02, 51-40-05, 51-21-01 & 51-20-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOORBEAM T CHORD AT BS 324, RBL 61. REPLACED FLOORBEAM T CHORD AT BS 324, RBL 61 IAW SRM 51-40-02, 51-10-02, 51-40-05 & 51-21-10.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT CHANNEL BETWEEN BS 1661 TO BS 1681.8, LBL 58.22. REPLACED FLOOR SUPPORT CHANNEL BETWEEN BS 1661 TO BS 1681.8, LBL 58.22 IAW SRM 51-40-02, 51-10-02 & 51-40-05.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON CREASE BEAM WEB BETWEEN BS 310.5 TO BS 324, RBL 62. REPLACED CREASE BEAM WEB BETWEEN BS 310.5 TO BS 324, RBL 62 IAW SRM 51-40-02, 51-20-01, 51-40-05 & AMM 51-21-10.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON ANGLES AT BS 345, LBL 62. REPLACED ANGLES AT BS 345, LBL 62 IAW SRM 51-40-02, 51-21-00, 53-20-15-1A-1, DETAIL 3 & 4.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON SUPPORT ANGLE BETWEEN BS 345 TO BS 365, LBL 62. REPLACED SUPPORT ANGLE BETWEEN BS 345 TO BS 365, LBL 62 IAW SRM 51-40-02 & 51-10-02.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON R1 DOOR SCUFF PLATE SUPPORT BRACKET AT BS 340, RBL 64. REPLACED R1 DOOR SCUFF PLATE SUPPORT BRACKET AT BS 340, RBL 64 IAW SRM 51-40-05, 51-20-01 & 51-40-02.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON R1 DOOR SCUFF PLATE SUPPORT BRACKET AT BS 346, RBL 64. REPLACED R1 DOOR SCUFF PLATE SUPPORT BRACKET AT BS 346, RBL 64 IAW SRM 51-40-02, 51-10-02, 51-40-05 & 51-20-01.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON R1 DOOR SCUFF PLATE SUPPORT BRACKET AT BS 356, RBL64. REPLACED R1 DOOR SCUFF PLATE SUPPORT BRACKET AT BS 356, RBL 64 IAW SRM 51-40-05 & 51-20-01.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 FILIFORM CORROSION ON R1 DOOR SILL SCUFF PLATE SUPPORT AT BS 351, RBL 64. REPLACED R1 DOOR SILL SCUFF PLATE SUPPORT AT BS 351, RBL 64 IAW SRM 51-40-02 & DWG 1411N8324.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT BETWEEN BS 685 TO BS 720, RBL 58. REPLACED FLOOR SUPPORT BETWEEN BS 685 TO BS 720, RBL 58 IAW SRM 51-10-02 & 51-40-02.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT CHANNEL AT BS 395 BETWEEN RBL 47 TO RBL 55. REPLACED FLOOR SUPPORT CHANNEL AT BS 395 BETWEEN RBL 47 TO RBL 55 IAW SRM 51-40-02 & 51-40-05.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON LOWER WEB AT BS 1350, RBL 58.22. REPLACED LOWER WEB AT BS 1350, RBL 58.22 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN BS 395 TO BS 418, RBL 60. REPLACED FLOOR SUPPORT BETWEEN BS 395 TO BS 418, RBL 60 IAW SRM 51-40-02.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT CHANNEL AT BS 400 BETWEEN RBL 27 TO RBL 43. REPLACED FLOOR SUPPORT CHANNEL AT BS 400 BETWEEN RBL 27 TO RBL 43 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN BS 680 TO BS 700, LBL 63. REPLACED FLOOR SUPPORT BETWEEN BS 680 TO BS 700, LBL 63 IAW SRM 51-10-02, 51-40-05 & 51-21-01.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON INNER CHORD OF CREASE BEAM BETWEEN BS 1300 TO BS 1360, RBL 58.22. REPLACED CREASE BEAM BETWEEN BS 1300 TO BS 1360, RBL 58.22 IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN BS 1080 TO BS 1180, RBL 45.5. REPLACED SEAT TRACK BETWEEN BS 1080 TO BS 1180, RBL 45.5 IAW SRM 51-40-02 & 51-40-05.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK, LEVEL 2 GALVANIC CORROSION ON AFT CABIN DECK PLATE BETWEEN BS 1681 TO BS 1720 & BETWEEN BL0 TO RBL 54. REPAIRED AFT CABIN DECK PLATE BETWEEN BS 1681 TO BS 1720 & BETWEEN BL0 TO RBL 54 IAW SRM 53-60-51, REPAIR 2, FIG 201, SHEET 1-5.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON AFT CABIN DECK PLATE AT BS 1715, RBL 10. REPAIRED AFT CABIN DECK PLATE AT BS 1715, RBL 10 IAW SRM 53-60-51, REPAIR 2, FIG 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN BS 900 TO BS 1080, LBL 24.75. REPLACED SEAT TRACK BETWEEN BS 900 TO BS 1080, LBL 24.75 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT CHANNEL BETWEEN BS 1300 TO BS 1320, LBL 24. REPLACED FLOOR SUPPORT CHANNEL BETWEEN BS 1300 TO BS 1320, LBL 24 IAW SRM 51-40-02.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 EXFOLIATION CORROSION ON SUPPORT ANGLE AT BS 1720, LBL 10. REPLACED SUPPORT ANGLE AT BS 1720, LBL 10 IAW SRM 51-40-02 & DWG 146N5240.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT CHANNEL AT BS 400 BETWEEN RBL 14 TO RBL 23. REPLACED FLOOR SUPPORT CHANNEL AT BS 400 BETWEEN RBL 14 TO RBL 23 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT CHANNEL BETWEEN BS 1640 TO BS 1661, LBL 58.22. REPLACED FLOOR SUPPORT CHANNEL BETWEEN BS 1640 TO BS 1661, LBL 58.22 IAW SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON INTERCOSTAL BETWEEN BS 1661 TO BS 1681, RBL 10. REPLACED INTERCOSTAL BETWEEN BS 1661 TO BS 1681, RBL 10 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT CHANNEL BETWEEN BS 324 TO BS 345, LBL 19. REPLACED FLOOR SUPPORT CHANNEL BETWEEN BS 324 TO BS 345, LBL 19 IAW SRM 51-10-02 & 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK, LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT BS 365 BETWEEN RBL 31 TO RBL 32. REPLACED FLOORBEAM AT BS 365 BETWEEN RBL 31 TO RBL 32 IAW SRM 53-00-51-1A, FIG 101, 53-00-51-2R & 51-40-02.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 EXFOLIATION CORROSION ON CABIN FLOOR SUPPORT CHANNEL BETWEEN BS 1640 TO BS 1661, RBL 58.22. REPLACED CABIN FLOOR SUPPORT CHANNEL BETWEEN BS 1640 TO BS 1661, RBL 58.22 IAW SRM 53-00-51, FIG 101 & 51-40-02.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK, LEVEL 2 GALVANIC CORROSION ON GUSSET AT BS 1681.8, RBL 10. REPLACED GUSSET AT BS 1681.8, RBL 10 IAW SRM 51-40-02.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK, LEVEL 2 GALVANIC CORROSION ON GUSSET AT BS 1681.8, BL0. REPLACED GUSSET AT BS 1681.8, BL0 IAW SRM 51-40-02.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK, LEVEL 2 GALVANIC CORROSION ON GUSSET AT BS 1681.8, RBL 35. REPLACED GUSSET AT BS 1681.8, RBL 35 IAW SRM 51-40-02.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK, LEVEL 2 GALVANIC CORROSION ON GUSSET AT BS 1681.8, RBL 41. REPLACED GUSSET AT BS 1681.8, RBL 41 IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN BS 1540 TO BS 1640, RBL 45.5. REPLACED SEAT TRACK BETWEEN BS 1540 TO BS 1640, RBL 45.5 IAW SRM 53-00-52, FIG 101, DETAIL 1, 51-40-02 & DWG 146N5130.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN BS 1540 TO BS 1640, LBL 24.75. REPLACED SEAT TRACK BETWEEN BS 1540 TO BS 1640, LBL 24.75 IAW SRM 53-00-52, FIG 101, DETAIL 1, 51-40-02 & DWG 146N5130.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK, LEVEL 2 FILIFORM CORROSION ON HAT STIFFENER AT BS 1656, RBL 63. REPLACED HAT STIFFENER AT BS 1656, RBL 63 IAW SRM 51-40-02 & DWG 146N8016.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK, LEVEL 2 FILIFORM CORROSION ON HAT STIFFENER AT BS 1673, RBL 63. REPLACED HAT STIFFENER AT BS 1673, RBL 63 IAW SRM 51-40-02 & DWG 146N8016.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK, LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT CHANNEL BETWEEN BS 1661 TO BS 1681, RBL 58.22. REPLACED FLOOR SUPPORT CHANNEL BETWEEN BS 1661 TO BS 1681, RBL 58.22 IAW SRM 53-80-13-1A, FIG 101 & 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK, LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM UPPER T CHORD AT BS 1640 BETWEEN RBL 12 TO RBL 58. REPLACED FLOORBEAM AT BS 1640 BETWEEN RBL 12 TO RBL 58 IAW SRM 53-00-51-1A, FIG 101, 53-00-51-2R-7 & 51-40-02.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK, LEVEL 2 FILIFORM CORROSION ON HAT STIFFENER AT BS 1673, LBL 63. REPLACED HAT STIFFENER AT BS 1673, LBL 63 IAW SRM 51-40-02 & DWG 146N8016.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 FILIFORM CORROSION ON HAT STIFFENER AT BS 1656, LBL 63. REPLACED HAT STIFFENER AT BS 1656, LBL 63 IAW SRM 51-40-02 & DWG 146N8016.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK, LEVEL 2 EXFOLIATION CORROSION ON CABIN FLOOR SUPPORT BETWEEN BS 700 TO BS 720, LBL 63. REPLACED CABIN FLOOR SUPPORT BETWEEN BS 700 TO BS 720, LBL 63 IAW SRM 53-00-51, FIG 101 & 51-40-02.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 64,411 hrs · 24,551 cycles

C4 CHECK, CORROSION ON FLOOR SUPPORT CHANNEL BETWEEN BS 1661 TO BS 1640, BL0. REPLACED FLOOR SUPPORT CHANNEL BETWEEN BS 1661 TO BS 1640, BL0 IAW SRM 51-40-02 & DWG 146N5242.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON CABIN LT CREASE BEAM INNER CHORD BETWEEN BS 1290 TO BS 1370, LBL 62. REPLACED CREASE BEAM BETWEEN BS 1290 TO BS 1370, LBL 62 IAW SRM 51-40-02.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON CABIN RT CREASE BEAM INNER CHORD BETWEEN BS 725 TO BS 740, RBL 62. REPLACED CREASE BEAM BETWEEN BS 725 TO BS 740, RBL 62 IAW SRM 51-40-02.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON AFT CABIN FLOOR CHANNEL BETWEEN BS 1661 TO BS 1681.1, BL0. REPLACED AFT CABIN FLOOR CHANNEL BETWEEN BS 1661 TO BS 1681.1, BL0 IAW SRM 51-10-02, 51-40-05 & 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK, LEVEL 2 GALVANIC CORROSION ON CABIN FLOOR SUPPORT CLIP BETWEEN BS 1674 TO BS 1680, LBL 53. REPLACED CABIN FLOOR SUPPORT CLIP BETWEEN BS 1674 TO BS 1680, LBL 53 IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,411 hrs · 24,551 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN BS 1540 TO BS 1640, LBL45.5. REPLACED SEAT TRACK BETWEEN BS 1540 TO BS 1640, LBL45.5 IAW SRM 53-00-52, FIG 101, DET 1, 51-40-02 & 51-21-00.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 62,701 hrs · 23,987 cycles

EXIT LIGHT COVER ON 1R DOOR NOT ATTACHED. REPLACED EXIT LIGHT COVER 1R DOOR.

Part: SWITCH — FAILED (CABIN LIGHTS) · airframe 62,357 hrs · 23,880 cycles

ENROUTE, WHEN FWD LAV DOOR WAS CLOSED AND LOCKED, THE FLUORESCENT LIGHT IN LAVATORY WENT OUT. BLACK SMOKE CAME THRU DOOR FRAME. MX FOUND THE FWD LAV DOOR FRAME LIGHT SWITCH MELTED AND SHORTED. MX REPLACED THE FWD LAV DOOR FRAME LIGHT SWITCH. OPS CHECKED OK.

Part: LIGHT — LOOSE (ZONE 200) · airframe 62,178 hrs · 23,830 cycles

EMERGENCY LIGHTS ON FLOOR, LT SIDE ROW 1-2 LOOSE. REPLACED DAMAGED AND MISSING SECTION.

Part: LIGHT — BUCKLED (ZONE 200) · airframe 62,171 hrs · 23,826 cycles

FLOOR TRACK LIGHTING IN FIRST CLASS IS PROTRUDING UPWARD. REPLACED DAMAGED SECTION OF FLOOR TRACK.

Part: COVER — BROKEN (CABIN) · airframe 62,039 hrs · 23,775 cycles

EXIT LIGHT COVER AT 4R DOOR BROKEN MISSING. REINSTALLED EXIT LIGHT COVER.

Part: WIRE HARNESS — FAULTY (ELECTRICAL SYS)

ENROUTE, LT GEN OFF LIGHT ILLUMINATED. BUS ISOLATED. ACARS OH DISPLAYED. SYS OPERATED NORMALLY AFTER GEN CONTROL RESET. BUS TIE RESET NOT ATTEMPTED. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO FIELD. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MX PLACED THE LT GENERATOR ON MEL AND RELEASED THE ACFT FOR FLIGHT. THE LT IDG FEEDER CABLE AND THE FIREWALL CONNECTOR WERE LATER REPLACED, AND CONNECTOR WAS ALSO REPINNED. ACFT OK FOR SERVICE.

Part: SLIDE — OUT OF POSITION (L1 DOOR)

CLT - DOOR MOUNTED EMERGENCY SLIDE OUT OF CONTAINER AT DOOR NR 1L. REMOVED AND REPLACED DOOR NR L1 ESCAPE SLIDE/RAFT.

Part: LIGHT — LOOSE (CABIN) · airframe 61,405 hrs · 23,581 cycles

CLT - ESCAPE PATH LIGHTING STRIP ADJACENT TO SEAT 1C IS LOOSE. SECURED PATH LIGHTING STRIP AT 1C.

Part: LENS — OUT OF ALIGNMENT (L1 DOOR) · airframe 61,126 hrs · 23,478 cycles

CLT - DOOR 1L VIEWING LENSE OUT OF POSITION. REPOSITIONED TRIM BEZEL TO ALIGN WITH VIEWPORT AT 1L DOOR, CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,052 hrs · 23,447 cycles

PHX - EMERGENCY EXIT ROW LIGHTS INOP AT ROW 2 LEFT SIDE A/C. REMOVED AND REPLACED EMERGENCY EXIT ROW OVERHEAD BIN LIGHT FOR ROWS 2 LEFT, OPS NORMAL.

Part: RESERVOIR — LOW PRESSURE (R2 DOOR) · airframe 59,196 hrs · 22,891 cycles

C3 CHECK - R2 DOOR EMERGENCY POWER RESERVOIR PRESSURE LOW. REMOVED AND REPLACED RESERVOIR PER JOB CARD 19C84252003.

Part: SCREW — MISSING (LIGHT PANEL) · airframe 58,487 hrs · 22,671 cycles

PHL - EMERGENCY LIGHT PANEL MID A/C OVERHEAD IS FALLING APART/ MISSING SCREWS. PROPERLY RE-SECURED EMERGENCY LIGHT PANEL ON A/C MID OVERHEAD.

Part: FLOW VALVE — DEBONDED (RT ENGINE)

PHL - FLT 1451 PHL TO PUJ. ABORT TAKEOFF AT 80 KNOTS. AT 80 KNOTS, DID NOT HAVE 1.4 EPR ON RIGHT ENGINE. AT 80 KNOTS, RIGHT EEC LIGHT & RIGHT ENGINE LIMITER LIGHT ON. REPLACED RIGHT FUEL FLOW GOVERNOR. OP'S & LEAK CHECK OK. P4 ORIFICE DEBONDED.

Part: MODULE — FAULTY (STABILIZER)

FLT 1035. WHILE RETURNING FOR A HYDRAULIC INDICATION PROBLEM, THE FLIGHT EXPERIENCED A FLIGHT CONTROL ANOMALY DURING THE APPROACH. AT 3000FT DESCENDING TO 2,500, WITH APP ARMED AND ALL 3 AUTO PILOTS ENGAGED, AUTO PILOT WENT INTO NOSE DOWN HARDOVER ABOUT .75 TO 1 NEG G. MAINTENANCE RAN A/P BIT AND NO FAULTS NOTED. REPLACED NR 2 SAM AND RAN TEST 65. OPS CK GOOD. LAND 30 AND 40 TEST ACCOMPLISHED AND NO FAULTS NOTED. ALSO ACCOMPLISHED AN ELEVATOR FREEPLAY CHECK. NO FLT CONTROL FAULTS NOTED. COULD NOT DUPLICATE CUSTOMER'S TROUBLE REPORTED. INSPECTED AND RESEATED ALL PRINTED CIRCUIT BOARD ASSEMBLIES.

Part: CIRCUIT BREAKER — POPPED (COCKPIT)

PHL - FLT 751 EN ROUTE BRU TO PHL. ON DESCENT, THE FLIGHT DECLARED AN EMERGENCY DUE TO EICAS MESSAGES "APU BLEED VAL", "L HYD ELE PUMP", "C HYD ELE 2", "ANTI-SKID", "PROBE HEAT", "RT UTIL BUS OFF", "R RECIRC FAN", AND "L ENG EEC". THE CIRCUIT BREAKER FOR THE RIGHT DC BUS SECT 1 WAS THEN FOUND POPPED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RESET THE DC BUS SECT 1 CIRCUIT BREAKER. OPERATIONALLY CHECKS NORMAL. NO FAULTS WERE NOTED.

Part: FAN — MALFUNCTIONED (CABIN) · airframe 55,991 hrs · 21,939 cycles

DUB - FLT 724 EN ROUTE PHL TO DUB. L RECIRC FAN DISPLAYED AND RECIRC FAN INOP LIGHT ILLUM WITH SWITCH POSITION TO ON. ELECTRICAL BURNING SMELL DESCENDING INTO DUB. REMOVED AND REPLACED L RECIRC FAN.

Part: FAN — MALFUNCTIONED (CABIN) · airframe 55,737 hrs · 21,865 cycles

MCO - FLT 1857 EN-ROUTE CLT TO MCO. AFTER ENG SHUT DOWN AT THE GATE THERE WAS A PUNGENT ODOR LIKE BURNT MATTRESS IN FIRST CLASS AND REST OF CABIN. TWENTY MINUTES FROM MCO HAZE AND ODOR, TURNED OF RECERC AND HAZE WENT AWAY. PERFORMED VISUAL INSPECTION OF APU DUCTS. NO OIL NOTED. RIGHT RECIRCULATION FAN WAS PLACED ON MEL. MAINTENANCE REPLACED THE RIGHT RECIRCULATION FAN. SYSTEM CHECKS OK.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 54,010 hrs · 21,325 cycles

CLT - C2 - MAJOR REPAIR - CRACK IN SHEAR ANGLE AT BS 1300, S21L. REPLACED SHEAR ANGLE AT BS 1300, S21L IAW B757 SRM 51-40-02.

Part: FUSE — BLOWN (EPSU)

PHX - THE EMERGENCY LIGHT AT ROW 15DEF WAS INOPERATIVE. REPLACED THE FUSE IN EPSU BASE 10699.

Part: CIRCUIT BOARD — FAULTED (LT ENGINE)

PHL FLT 740 EN ROUTE SJU TO PHL. DURING APPROACH, RECEIVED "L ENG LP PUMP" MESSAGE. THE LEFT ENGINE UNSPOOLED AND THE LEFT ENGINE OIL PRESSURE WENT TO 16 PSI AND WITHIN 45 SECONDS CAME BACK TO ALL NORMAL INDICATIONS. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE BVCU BITE TEST PRODUCED FAULT "07". REPLACED THE LEFT ENGINE LOWER DEDICATED GENERATOR CONTROL UNIT. ADDITIONALLY, BY REQUEST, REMOVED THE FOLLOWING UNITS AS A PRECAUTIONARY MEASURE: LEFT ENGINE TPU, L/P FUEL PUMP, FFG, H/P FUEL PUMP, & BVCU. LOW OUTPUT VOLTAGE COMING FROM I/O BOARD ASSEMBLY. REPLACED I/O BOARD ASSEMBLY.

Part: CHARGER — INOPERATIVE (CABIN)

PHL - THE EXTERNAL EMERGENCY LIGHT AT DOOR L4 WAS INOPERATIVE. CLEANED THE TERMINAL AT LIGHT ASSEMBLY AT DOOR L4. ALSO, REMOVED AND REPLACED THE BATTERY PACK AND CHARGER.

Part: PANEL — DELAMINATED (VERTICAL STAB) · airframe 54,010 hrs · 21,325 cycles

CLT - C2 - MAJOR REPAIR - DELAMINATION ON RIGHT VERTICAL STABILIZER PANEL AT FIN STA 116 APPROX 12 INCHES AFT OF LEADING EDGE. REPLACED RIGHT VERTICAL STABILIZER PANEL IAW B757 SRM 55-30-01.

Part: MECHANISM — MALFUNCTIONED (L1 DOOR) · airframe 48,365 hrs · 19,926 cycles

MCN - C1 - EES - L-1 DOOR POWER ASSIST PIN WILL NOT ENGAGE IN RELEASE FORK. REPLACED EMERGENCY POWER TRIGGER MECHANISM ON L-1 DOOR IAW B757 AMM 52-11-32.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 48,365 hrs · 19,926 cycles

MCN - C1 - MAJOR REPAIR - CORROSION ON R-2 DOOR DRAIN TROUGH GUTTER SUPPORT BETWEEN BS 720 TO BS 740, WL 208, RBL 62. REPLACED R-2 DOOR DRAIN TROUGH GUTTER SUPPORT BETWEEN BS720 TO BS 740, WL 208, RBL 62 IAW B757 SRM 51-40-02.

Part: SUPPORT — CORRODED (L4 RAIN GUTTER) · airframe 48,365 hrs · 19,926 cycles

MCN - C1 - MAJOR REPAIR - CORROSION ON L-4 DOOR RAIN GUTTER SUPPORT AT BS 1656, WL 208. REPLACED L-4 DOOR RAIN GUTTER SUPPORT AT BS 1656, WL 208 IAW B757 SRM 51-10-02, 53-60-01 & 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 48,365 hrs · 19,926 cycles

MCN - C1 - MAJOR REPAIR - CORROSION ON FLOOR SUPPORT BETWEEN BS 720 TO BS 740, RBL 54. REPLACED FLOOR SUPPORT BETWEEN BS 720 TO BS 740, RBL 54 IAW B757 SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,365 hrs · 19,926 cycles

MCN - C1 - MAJOR REPAIR - FRAME CHORD CRACKED AT FORWARD END OF PANEL 195BL, BS 1147 INSIDE LEFT MAIN LANDING GEAR WHEEL WELL. REPLACED FRAME CHORD AT FORWARD END OF PANEL 195BL, BS 1147 INSIDE LEFT MAIN LANDING GEAR WHEEL WELL IAW B757 SRM 51-40-02 & BOEING DRAWING 149N7222.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,365 hrs · 19,926 cycles

MCN - C1 - MAJOR REPAIR - CORROSION ON UPPER SURFACE OF FLOORBEAM AT BS 740, WL 208, LBL 55. REPAIRED FLOORBEAM AT BS 740, WL 208, LBL 55 IAW US AIRWAYS EA 130213.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 48,365 hrs · 19,926 cycles

MCN - C1 - MAJOR REPAIR - CORROSION ON SUPPORT ANGLE BETWEEN BS 684 TO BS 700, WL 208, LBL 65. REPLACED SUPPORT ANGLE BETWEEN BS 684 TO BS 700, WL 208, LBL 65 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 48,365 hrs · 19,926 cycles

MCN - MAJOR REPAIR - C1 CHECK - CORROSION ON FLOOR SUPPORT AT BS 720 - BS 740, LBL 65, WL 208.1. REPLACED FLOOR SUPPORT AT BS 720 - BS 740, LBL 65, WL 208.1 IAW B757 SRM 51-40-02.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 48,365 hrs · 19,926 cycles

MCN - C1 - MAJOR REPAIR - CORROSION ON SUPPORT BETWEEN BS 684 TO BS 700, WL 208, LBL 65. REPLACED SUPPORT BETWEEN BS 684 TO BS 700, WL 208, LBL 65 IAW B757 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,365 hrs · 19,926 cycles

MCN - C1 - MAJOR REPAIR - CORROSION ON UPPER SURFACE OF FLOORBEAM AT BS 700, WL 208 BETWEEN LBL 45 & LBL 65. REPAIRED FLOORBEAM AT BS 700, WL 208 BETWEEN LBL 45 & LBL 65 IAW US AIRWAYS EA 130213.

Part: SILL — CORRODED (FUSELAGE) · airframe 48,365 hrs · 19,926 cycles

MCN - MAJOR REPAIR - C1 CHECK - CORROSION ON L2 DOOR SILL CHORD AT BS 600 - BS 740, LBL 65, WL 208.1 REPLACED L2 DOOR SILL CHORD AT BS 600 - BS 740, LBL 65, WL 208.1 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 48,365 hrs · 19,926 cycles

MCN - C1 - MAJOR REPAIR - CORROSION ON INTERCOSTAL AT BS 684, WL 208, LBL 45. REPLACED INTERCOSTAL AT BS 684, WL 208, LBL 45 IAW B757 SRM 51-40-02.

Part: STRUCTURE — DETERIORATED (AILERON) · airframe 48,365 hrs · 19,926 cycles

MCN - C1 - MAJOR REPAIR - DETERIORATED COMPSITE ON AILERON AT WBL 720. REPAIRED DETERIORATED COMPSITE ON AILERON AT WBL 720 IAW B757 SRM 51-70-03.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

SEA - THE AFT FLIGHT ATTENDANT, OUTBOARD POSITION FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE AFT FLIGHT ATTENDANT, OUTBOARD POSITION FLASHLIGHT.

Part: FLAP — DELAMINATED (LT WING) · airframe 46,490 hrs · 19,137 cycles

CLT - C-22 - MAJOR REPAIR - FOUND DELAMINATION ON LEFT OUTBOARD AFT FLAP MEASURES 4"X4.5", 5.5" FORWARD OF TRAILING EDGE. REPAIRED DELAMINATION ON LEFT OUTBOARD AFT FLAP 4"X4.5" AREA., 5.5" FORWARD OF TRAILING EDGE IAW B757 SRM 57-53-01. (S)

Part: MEGAPHONE — DAMAGED (CABIN)

MCO - THE AFT MEGAPHONE WAS FOUND DAMAGED AND INOPERATIVE. MAINTENANCE REPLACED THE AFT MEGAPHONE. OPERATIONALLY CHECKS OK.

Part: SKIN — CRACKED (L/E SLAT) · airframe 43,274 hrs · 17,803 cycles

BMH - MAJOR REPAIR - C-4 CHECK - NR 6000784, RIGHT WING LEADING EDGE SLAT NR 9 INNER SKIN CRACKED, WS 623.5. REPLACED RIGHT WING LEADING EDGE SLAT NR 9 INNER SKIN CRACKED, WS 623.5 IAW B757 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,274 hrs · 17,803 cycles

BFM - MAJOR REPAIR - C-4 CHECK - NR 6000701, CORROSION ON CABIN FLOORBEAM, BS 365, RBL 20 - RBL 25, WL 208. REPAIRED CABIN FLOORBEAM, BS 365, RBL 20 - RBL 25, WL 208 IAW USAIRWAYS TYPICAL REPAIR 53-15-01.

Part: FUSE — BLOWN (CABIN) · airframe 41,778 hrs · 17,179 cycles

R4 DOOR EXTERIOR EMERGENCY LIGHT FOUND INOPERATIVE. MAINTENANCE REPLACED THE FUSE AND RELAMPED.