N940UW

Part: INDICATOR — FAULTY (COCKPIT) · airframe 71,771 hrs · 26,311 cycles

AIRCRAFT WAS GROUNDED. DURING TAKEOFF (HNL), FIRST OFFICER CALLED 80 KTS, BUT CAPTAIN'S AIRSPEED INDICATED 62 KTS. "OFF" FLAG APPEARED BRIEFLY IN CAPTAIN AIRSPEED INDICATOR. ABORTED TAKEOFF. AT GATE, CAPTAIN AIRSPEED INDICATOR OSCILLATED FROM 29-31 KTS, WHILE FIRST OFFICER AIRSPEED INDICATOR STAYS STEADY AT 30 KTS. REPLACED MACH AIRSPEED INDICATOR PER AMM 34-13-02.

Part: SLIDE RAFT — LOW PRESSURE (L1 DOOR) · airframe 70,698 hrs · 26,090 cycles

AIRCRAFT WAS NOT GROUNDED, L1 DOOR SLIDE/RAFT INFLATION RESERVOIR GAUGE, NEEDLE IN THE RED. REPLACED L1 DOOR SLIDE/RAFT IAW TASK CARD 19L80025002.

Part: PRESSURE SWITCH — DEFECTIVE (ZONE 400) · airframe 70,016 hrs · 25,950 cycles

RETURNED TO DEPARTURE; AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED AN RT ENGINE LOW PRESSURE PUMP STATUS MESSAGE OCCURED AT FL 24000, 1 CHANNEL AND RETURNED TO DEPARTURE. MAINTENANCE REPLACED THE NR 2 ENGINE LOW PRESSURE FUEL PUMP AND THE FUEL PRESSURE SWITCH IAW AMM 73-11-01-004-003-ROO AND AMM 73-35-01-404-017-ROO. A SATISFACTORY LEAK AND OPS CHECK WAS ACCOMPLISHED IAW AMM 71-00-00-700-804 R3.

Part: PUMP — DEFECTIVE (NR 2 ENGINE) · airframe 70,016 hrs · 25,950 cycles

RETURNED TO DEPARTURE, AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED A RT ENGINE LOW PRESSURE PUMP STATUS MESSAGE OCCURRED AT FL 24000, 1 CHANNEL AND RETURNED TO DEPARTURE. MAINTENANCE REPLACED THE NR 2 ENGINE LOW PRESSURE FUEL PUMP AND THE FUEL PRESSURE SWITCH IAW AMM 73-11-01-004-003-ROO AND AMM 73-35-01-404-017-ROO. A SATISFACTORY LEAK AND OPS CHECK WAS ACCOMPLISHED IAW AMM 71-00-00-700-804 R3.

Part: LIGHT — UNSECURE (CABIN) · airframe 70,000 hrs · 25,947 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY FLOOR LIGHT AT ROW 17D BOWS UP IN FLIGHT. RESECURED EMERGENCY FLOOR LIGHT AT ROW 17D IAW AMM 20-25-17 AND DWG 19P33D256.

Part: SLIDE — LOW PRESSURE (R3 DOOR) · airframe 69,813 hrs · 25,908 cycles

AIRCRAFT WAS NOT GNDED. R3 DOOR SLIDE PRESS READS LOW. R & R R3 DOOR SLIDE IAW JC 19L83525001.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 69,694 hrs · 25,887 cycles

AIRCRAFT WAS GNDED. DEADHEADING CREW MEMBERS REPORT ODOR IN CABIN AT DOOR 2 & 4, RESEMBLING ELEC BURNING, AFTER ENG START & TAXI. FOUND ROW 16 RT LIGHT BALLAST INOPERATIVE. REPLACED BALLAST & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO ODORS BEING NOTED IAW AMM 33-21-30-962-008 & TASK CARD 19L00021001.

Part: GIRT BAR — LACK OF LUBE (R2 DOOR) · airframe 69,194 hrs · 25,761 cycles

AIRCRAFT WAS NOT GNDED. DOOR 2R DIFFICULT TO ARM. LUBED GIRT BAR FEET. OPERATIONAL CHECKED GOOD.

Part: SLAT — DELAMINATED (LT WING) · airframe 69,162 hrs · 25,754 cycles

AIRCRAFT IN BASE MX. NR 4 SLAT DELAMINATING, UPPER INBD CORNER. R & R 4 SLAT IAW AMM 27-81-02-024-001, TASK CARD 19L52027002 & EA 258612.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 69,162 hrs · 25,754 cycles

AIRCRAFT IN BASE MX. EXIT SIGN INOPERATIVE AT L2 DOOR AREA CEILING. R & R M732 RT SIDE EMER LIGHTS POWER SUPPLY IAW AMM 33-51-07-022-020 & 33-51-07-862-054. OPERATIONAL CHECKED SATISFACTORY.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,162 hrs · 25,754 cycles

AIRCRAFT IN BASE MX. CORROSION ON FWD CARGO COMPARTMENT FLOOR STRINGER, AT BS 653 & LBL 2.90. REPLACED FLOOR STRINGER IAW SRM 53-00-53-1A-1 DET IV SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,162 hrs · 25,754 cycles

AIRCRAFT IN BASE MX. CORROSION ON FWD CARGO COMPARTMENT FLOOR STRINGER, AT BS 653 & RBL 2.9. REPLACED FLOOR STRINGER IAW SRM 53-00-53-1A-1 DET IV SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,162 hrs · 25,754 cycles

AIRCRAFT IN BASE MX. CORROSION ON FWD CARGO COMPARTMENT FLOOR, STRINGER AT BS 653 & RBL 7.55. REPLACED FLOOR STRINGER IAW SRM 53-00-53-1A-1 DET IV & SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,162 hrs · 25,754 cycles

AIRCRAFT IN BASE MX. CORROSION ON FWD CARGO COMPARTMENT FLOOR STRINGER, AT BS 653 & LBL 10.45. REPLACED FLOOR STRINGER IAW SRM 53-00-53-1A-1 DET IV SRM 51-40-02.

Part: SLAT — DELAMINATED (LT WING) · airframe 69,162 hrs · 25,754 cycles

AIRCRAFT IN BASE MX. NR 2 SLAT DELAMINATING, UPPER INBD SIDE. REMOVED NR 2 LE SLAT IAW AMM 27-81-02-024-00. REPAIRED DAMAGE IAW SRM 57-43-02 R1. REINSTALLED SLAT IAW AMM 27-81-02-424-021. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 27-81-00 201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,162 hrs · 25,754 cycles

AIRCRAFT IN BASE MX. CORROSION ON FWD CARGO COMPARTMENT FLOOR STRINGER, AT BS 653 & RBL 16.10. REPLACED FLOOR STRINGER IAW SRM 53-00-53-1A-1 DET IV SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,162 hrs · 25,754 cycles

AIRCRAFT IN BASE MX. CORROSION ON FWD CARGO COMPARTMENT FLOOR STRINGER, AT BS 653 & LBL 7.55. REPLACED FLOOR STRINGER IAW SRM 53-00-53-1A-1 DET IV SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,162 hrs · 25,754 cycles

AIRCRAFT IN BASE MX. CORROSION ON FWD CARGO COMPARTMENT FLOOR STRINGER, AT BS 653 & RBL 10.45. REPLACED FLOOR STRINGER IAW SRM 53-00-53-1A-1 DET IV SRM 51-40-02.

Part: SWITCH — OUT OF ADJUST (L1 DOOR) · airframe 69,162 hrs · 25,754 cycles

AIRCRAFT IN BASE MX. L1 DOOR FWD GIRT BAR SWITCH REQUIRES ADJUSTMENT. ADJUSTED L1 DOOR GIRT BAR SWITCH IAW AMM 25-66-11-822-011. OPERATIONAL CHECKED GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 68,992 hrs · 25,703 cycles

EXIT FLOOR LIGHTING STRIP LOOSE MID CABIN. SECURED EXIT FLOOR LIGHTING STRIP.

Part: SENSOR — FAULTY (ZONE 100) · airframe 68,804 hrs · 25,644 cycles

AIRCRAFT WAS GNDED. DURING CLIMB EXPERIENCED SEVERAL WARNINGS & OR FAILURES, INCLUDING WIND SHEAR WARNING, SIGNIFICANT DIFFERENCE ON CAPTAIN'S & FIRST OFFICER'S AIRSPEED, 25KT. MULTIPLE EICAS MSGS & AUTO FLIGHT FAILURES & LT EEC. RETURNED TO MX. R & R RT ANGLE OF ATTACK SENSOR IAW AMM 34-12-03. PERFORMED JC 19T21034002, 757 AUTO LAND CHECK, SYS CHECKED NORMAL. PARTS CHANGE INDICATED TT 4018934, SN OFF 03081.

Part: WINDOW — DEFECTIVE (R2 DOOR) · airframe 68,061 hrs · 25,448 cycles

FLIGHT 1823 R2 DOOR VIEWING WINDOW FOGGED. R & R R2 DOOR VIEWING WINDOW IAW AMM 56-31-02.

Part: FAN — FAILED (RECIRCULATION) · airframe 67,181 hrs · 25,217 cycles

FLIGHT 739 EN-ROUTE, ELECTRICAL ODOR REPORTED BETWEEN ROWS 24 - 27 INFLIGHT. FUMES WERE CONFIRMED. IFE SWITCH TURNED OFF, BUT FUMES PERSISTED. ALL CABIN LIGHTS WERE TURNED OFF & FUMES SUBSIDED. IFE SWITCH TURNED BACK ON. REPLACED RT CABIN RECIRCULATION FAN AMM TASK 21-25-01-004-092. SYS CHECKED OK FOR SERVICE.

Part: LENS — UNSECURE (L4 DOOR) · airframe 66,965 hrs · 25,170 cycles

EMERGENCY LIGHT COVER COMING OFF AFT OF 4L DOOR. SECURED EMER LIGHT COVER AT 4L DOOR.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 66,365 hrs · 25,013 cycles

LEFT WING NR 3 SLAT HAS DELAMINATION ON THE UPPER & LOWER SURFACES 0.39 INCHES FROM OTBD EDGE & 2 INCHES FROM THE TE. REPLACED NR 3 SLAT IAW 19L52027002.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 66,365 hrs · 25,013 cycles

LEFT WING NR 2 SLAT HAS DELAMINATION ON THE UPPER & LOWER SURFACES 6 INCHES FROM INBD EDGE & 6.5 INCHES FROM THE TE. REPLACED NR 2 SLAT IAW 19L52027002.

Part: OVEN — DIRTY (GALLEY) · airframe 65,819 hrs · 24,864 cycles

EN-ROUTE, GALLEY G4B OVEN DEFECTIVE. EMIT SMOKES, SUSPECT GREASE. REPLACED AFT NR 4 OVEN. OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

EN ROUTE FLAP POSITION DOES NOT AGREE WITH THE FLAP LEVER. TE DISAGREE EICAS ON APPROACH. FLIGHT DECLARED AN EMER INBOUND. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. EICAS MSG CLEARED AFTER ENG SHUTDOWN AT GATE. OPERATIONS CHECK OF TE FLAPS POSITION INDICATE SYSTEM OK. ACCOMPLISHED BITE CHECK OF FSEU. NO FAULTS NOTED. OK FOR SERVICE.

Part: BATTERY — DISCHARGED (MEGOPHONE)

AFT CABIN FLIGHT ATTENDANT MEGA PHONE INOPERATIVE. R & R MEGA PHONE BATTERIES.

Part: CONTROL BOX — BINDING (RT ENGINE) · airframe 65,060 hrs · 24,601 cycles

ON DESCENT, THE RT ENG WOULD NOT RETURN TO IDLE. FUEL FLOW REMAINED AT 3500 POUNDS PER HOUR. THE FLIGHT DECLARED AN EMER. AT 500 FT, THE CREW SHUTDOWN THE RT ENG & THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENG TIME WAS LESS THAN 1 MINUTE. FOUND THE CABLE BINDING BETWEEN THE UPPER & INTERMEDIATE CONTROL BOXES IN THE CABLE SHEATH. THE CABLE & INTERMEDIATE CONTROL BOX WERE REPLACED. ADDITIONALLY, THE POWER CONTROL LINKAGE LOWER BOX & THE THROTTLE ANGLE TRANSDUCER WERE REPLACED. THE CONTROL BOXES WERE MISPLACED BY THE VENDOR & THE THROTTLE ANGLE TRANSDUCER WAS SCRAPPED. THE CABLE TO THE INTERMEDIATE CONTROL BOX IS BELIEVED TO BE THE CAUSE, BUT IT CANNOT BE VERIFIED DUE TO MISPLACED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 64,767 hrs · 24,518 cycles

DURING INTERIOR WALK THRU FOUND 3L EMER EXIT SIGN & 3R SIDEWALL EMER SIGN INOPERATIVE. R & R POWER SUPPLY & BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,679 hrs · 24,498 cycles

R3, L3 HAS EMER LIGHTS INOPERATIVE. R & R BATTERY PACK AT POWER SUPPLY M735.

Part: SIGN — LOOSE (CABIN) · airframe 64,679 hrs · 24,498 cycles

EXIT SIGN ABOVE 3L DOOR FLASHES ON & OFF. SECURED LOOSE SIGN, OPERATIONS GOOD.

Part: IMPELLER — DAMAGED (APU)

ENROUTE, OIL ODOR IN ACFT INTERIOR. BEGAN DURING DESCENT & REMAINED STRONG AFTER ENGINE SHUTDOWN & APU POWERING BOTH PACKS. REPLACED THE APU. HEAVY IMPACT DAMAGE TO INLET GUIDE VANES, LC SOUND ATTENUATOR PANEL, & LC IMPELLER. NORMAL OPERATIONAL WEAR THROUGHOUT EC & TURBINE SECTIONS. THE CONDITION OF THE LOAD COMPRESSOR IS CONSISTENT WITH INGESTION OF A FOREIGN OBJECT. DUE TO THE DAMAGE, THE LOAD COMPRESSOR IMPELLER EXPERIENCED AN OUT OF BALANCE CONDITION COMPROMISING THE LOAD COMPRESSOR CARBON SEAL'S ABILITY TO BLOCK OIL MIGRATION INTO THE BLEED AIR.

Part: SENSOR — FAULTY (L4 DOOR) · airframe 64,399 hrs · 24,437 cycles

4L DOOR DISARMED WITH HANDLE. ARMED LIGHT REMAINED ON. R & R SENSORS S10222 & S10223.

Part: SPAR — DAMAGED (NR 1 PYLON) · airframe 64,324 hrs · 24,416 cycles

C4 CHECK ELONGATED HOLES ON NR 1 PYLON UPPER, AFT SPAR WEB BETWEEN PYLON STATIONS PPS 195 TO 210, PP WL 154. REPAIRED NR 1 PYLON UPPER, AFT SPAR WEB IAW EA 506056.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FUSELAGE SKIN BETWEEN BS 740 TO 760 & BETWEEN STRINGER 19L TO 23L. REPAIRED FUSELAGE SKIN IAW SRM 53-00-01-1A-1, FIG 101, DET III & EA 506048.

Part: LIGHT — BROKEN (CABIN) · airframe 64,324 hrs · 24,416 cycles

C4 CHECK CABIN EMER EXIT IDENTIFIER LIGHT ASSEMBLY AT DOOR L2 HAS BROKEN BASE. REPLACED CABIN EMER EXIT IDENTIFIER LIGHT ASSEMBLY AT DOOR L2 IAW AMM 33-51-01. OPERATIONS CHECKED GOOD IAW AMM 33-51-01.

Part: LIGHT — CRACKED (CABIN) · airframe 64,324 hrs · 24,416 cycles

C4 CHECK CABIN EMER EXIT IDENTIFIER LIGHT ASSEMBLY AT DOOR L1 HAS BROKEN BASE. REPLACED CABIN EMER EXIT IDENTIFIER LIGHT ASSEMBLY AT DOOR L1 IAW AMM 33-51-01. OPERATIONS CHECKED GOOD IAW AMM 33-51-01.

Part: LIGHT — BROKEN (CABIN) · airframe 64,324 hrs · 24,416 cycles

C4 CHECK CABIN EMER EXIT IDENTIFIER LIGHT ASSEMBLY AT DOOR R4 HAS BROKEN BASE. REPLACED CABIN EMER EXIT IDENTIFIER LIGHT ASSEMBLY AT DOOR R4 IAW AMM 33-51-01. OPERATIONS CHECKED GOOD IAW AMM 33-51-01.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FWD CARGO COMPARTMENT FLOOR STRUCTURE ANGLE AT BS 845 BETWEEN STRINGER 26L TO 26R. REPLACED FWD CARGO COMPARTMENT FLOOR STRUCTURE ANGLE AT BS 845 BETWEEN STRINGER 26L TO 26R IAW SRM 51-40-02 & 51-40-05.

Part: LIGHT — BROKEN (CABIN) · airframe 64,324 hrs · 24,416 cycles

C4 CHECK CABIN EMER EXIT IDENTIFIER LIGHT ASSEMBLY AT DOOR L4 HAS BROKEN BASE. REPLACED CABIN EMER EXIT IDENTIFIER LIGHT ASSEMBLY AT DOOR L4 IAW AMM 33-51-01. OPERATIONS CHECKED GOOD IAW AMM 33-51-01.

Part: LIGHT — CRACKED (CABIN) · airframe 64,324 hrs · 24,416 cycles

C4 CHECK CABIN EMER EXIT IDENTIFIER LIGHT ASSEMBLY ON DOOR R1 FOUND CRACKED. REPLACED CABIN EMER EXIT IDENTIFIER LIGHT ASSEMBLY ON DOOR R1 IAW AMM 33-51-01. OPERATIONS CHECKED GOOD IAW AMM 33-51-01.

Part: INDICATOR — BROKEN (R1 DOOR) · airframe 64,324 hrs · 24,416 cycles

C4 CHECK R1 DOOR GIRT BAR AMM LIGHT BROKEN. REPLACED R1 DOOR GIRT BAR SLIDE LIGHT INDICATOR IAW WDM 25-66-11, OPERATIONS CHECKED GOOD IAW AMM 25-66-11-2.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON CHORD AT BS 900 BETWEEN STRINGER 21L TO 29L. REPLACED CHORD AT BS 900 BETWEEN STRINGER 21L TO 29L IAW SRM 51-40-02 & SRM 51-40-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C11 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT BETWEEN BS 333.45 TO 345 LBL 58.22. REPLACED FLOOR SUPPORT IAW SRM 51-10-02 & 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C11 CHECK LEVEL 2 EXFOLIATION CORROSION ON FITTING BETWEEN BS 365.25 TO 377.7 & BETWEEN BL0 TO RBL 24.75. REPLACED FITTING BETWEEN BS 365.25 TO 377.7 & BETWEEN BL0 TO RBL 24.75 IAW SRM 51-00-51 FIG 101 & 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C11 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT BETWEEN BS 347.7 TO 395 & BETWEEN BL0 TO RBL 24.75. REPLACED FLOOR SUPPORT IAW SRM 53-00-51 FIG 101 & 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C11 CHECK LEVEL 2 EXFOLIATION CORROSION ON STRINGER BETWEEN BS 740 TO 760, STRINGER 21L. REPAIRED IAW SRM 53-00-03 FIG 101 & 53-00-03-2R-1.

Part: GATE — CORRODED (R4 DOOR) · airframe 64,324 hrs · 24,416 cycles

C11 CHECK CORROSION ON LOWER GATE OF R4 DOOR AT BS 1661 WL 208.10. REPLACED R4 DOOR LOWER GATE IAW SRM 52-10-02 DETAIL X11 CMM 52-11-25 & MM 52-11-25.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON CREASE BEAM BETWEEN BS 297.7 TO 377.7 RBL 58.22. REPLACED CREASE BEAM BETWEEN BS 297.7 TO 377.7 RBL 58.22 IAW SRM 51-40-02, 51-40-02-0G FIG 8 & AMM 51-21-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON CABIN FLOOR SUPPORT CHANNEL BETWEEN BS 345 TO 365.5 RBL 50. REPLACED CABIN FLOOR SUPPORT CHANNEL BETWEEN BS 345 TO 365.5 RBL 50 IAW SRM 51-40-02, 51-40-02-0G, FIG 8, 51-20-01 & AMM 51-21-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOORBEAM UPPER CHORD AT BS 324, RBL36.20. REPAIRED FLOORBEAM UPPER CHORD AT BS 324, RBL 36.20 IAW SRM 53-10-08-2R-1, 53-00-51-1A, DET 3 & 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN BS 345 TO 377.7 BL0. REPLACED FLOOR SUPPORT BETWEEN BS 345 TO 377.7 BL0 IAW SRM 53-00-51-1A-1, FIG 101, DET 3, 51-40-02 & 51-40-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON CABIN FLOOR SUPPORT CHANNEL BETWEEN BS 310.5 TO 324, RBL 36.20. REPLACED CABIN FLOOR SUPPORT CHANNEL BETWEEN BS 310.5 TO 324, RBL 36.20 IAW SRM 51-40-02, 51-40-05 & AMM 51-21-00.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON STRINGER 20L BETWEEN BS 740 TO 760. REPAIRED STRINGER 20L BETWEEN BS 740 TO 760 IAW SRM 53-00-03-2R-1, 53-00-03-1A-1 FIG 101 & 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON CABIN FLOOR SUPPORT CHANNEL BETWEEN BS 324 TO 345 RBL 36.20. REPLACED CABIN FLOOR SUPPORT CHANNEL BETWEEN BS 324 TO 345, RBL 36.20 IAW SRM 51-40-02, 53-00-51 & AMM 51-21-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON CABIN LONGITUDINAL FLOOR SUPPORT BETWEEN BS 395 TO 418, RBL 24.75. REPLACED CABIN LONGITUDINAL FLOOR SUPPORT BETWEEN BS 395 TO 418, RBL 24.75 IAW SRM 51-40-02, 51-40-05 & AMM 51-21-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON CABIN FLOOR SUPPORT BETWEEN BS 324 TO 345 RBL 50. REPLACED CABIN FLOOR SUPPORT BETWEEN BS 324 TO 345 RBL 50 IAW SRM 51-40-02, 51-20-01 & AMM 51-21-00.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON CABIN FLOOR HORIZONTAL SUPPORT CHANNEL BETWEEN BS 395 TO 418, RBL 24.75. REPLACED CABIN FLOOR HORIZONTAL SUPPORT CHANNEL BETWEEN BS 395 TO 418, RBL 24.75 IAW SRM 51-40-02, 51-30-01, 51-20-01, 51-21-15 & 51-21-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON CABIN FLOOR CHANNEL SUPPORT BETWEEN BS 324 TO 345 BL0. REPLACED CABIN FLOOR CHANNEL SUPPORT BETWEEN BS 324 TO 345, BL0 IAW SRM 51-40-02, 51-40-05 & AMM 51-21-00.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FITTING BETWEEN BS 395 TO 418 RBL 58.22. REPLACED FITTING BETWEEN BS 395 TO 418 RBL 58.22 IAW SRM 51-40-02, 51-40-05, 51-21-02 & AMM 51-21-15.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FWD CABIN FLOOR SUPPORT AT BS 395, BETWEEN RBL 45.50 TO RBL 24.75. REPLACED FWD CABIN FLOOR SUPPORT AT BS 395, BETWEEN RBL 45.50 TO RBL 24.75 IAW SRM 51-40-02, 51-10-02, 53-00-51 & 51-40-05.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON CREASE BEAM INNER CHORD BETWEEN BS 395 TO 460, LBL 58.22. REPAIRED CREASE BEAM INNER CHORD BETWEEN BS 395 TO 460, LBL 58.22 IAW SRM 53-00-51-1A-1, 51-40-02, 51-70-12 & AMM 51-20-00.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON HORIZONTAL SUPPORT CHANNEL AT BS 395 RBL 45.50. REPLACED HORIZONTAL SUPPORT CHANNEL AT BS 395 RBL45.50 IAW SRM 51-40-02 & 51-21-00.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION & .25 INCH CRACK ON R1 LOWER SILL SUPPORT BETWEEN BS 340 TO 358, RBL 67. REPLACED CREASE BEAM ANGLE BETWEEN BS 333 TO 377.7, LBL 58.22 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL FLOOR SUPPORT BETWEEN BS 365.25 TO 418, RBL 45.50. REPLACED LONGITUDINAL FLOOR SUPPORT BETWEEN BS 365.25 TO 418, RBL 45.50 IAW SRM 51-10-02, 51-40-02, 51-40-05, 51-20-01 & 51-20-00.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON CREASE BEAM ANGLE BETWEEN BS 333 TO 377.7, LBL 58.22. REPLACED CREASE BEAM ANGLE BETWEEN BS 333 TO 377.7, LBL 58.22 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FWD CABIN FLOOR SUPPORT CHANNEL BETWEEN BS 395 TO 377.7, RBL 58.22. REPLACED FWD CABIN FLOOR SUPPORT CHANNEL BETWEEN BS 395 TO 377.7, RBL 58.22 IAW SRM 51-40-02, 51-20-01-0G & AMM 51-21-00.

Part: WEB — CRACKED (FUSELAGE) · airframe 64,324 hrs · 24,416 cycles

C4 CHECK CRACK ON MAIN DECK FWD CABIN WEB BETWEEN BS 395 TO 418, LBL 24.75. REPLACED WEB BETWEEN BS 395 TO 418, LBL 24.75 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT CHANNEL BETWEEN BS 324 TO 345, LBL 40. REPLACED FLOOR SUPPORT CHANNEL BETWEEN BS 324 TO 345, LBL40 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT CHANNEL AT BS 333.45 & BETWEEN LBL 40. REPLACED FLOOR SUPPORT CHANNEL AT BS 333.45 & BETWEEN LBL 40 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT CHANNEL BETWEEN BS 333.45 TO 345 & BETWEEN LBL 32 TO LBL 40. REPLACED FLOOR SUPPORT CHANNEL BETWEEN BS 333.45 TO 345 & BETWEEN LBL 32 TO LBL 40 IAW SRM 51-40-02.

Part: STRAP — CRACKED (FUSELAGE) · airframe 64,324 hrs · 24,416 cycles

C4 CHECK CRACK ON MAIN DECK FLOOR STRUCTURE STABILIZER STRAP BETWEEN BS 365.25 TO 377.7, LBL 24.75. REPLACED STABILIZER STRAP BETWEEN BS 365.25 TO 377.7, LBL 24.75 IAW SRM 51-40-02.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON CREASE BEAM BETWEEN BS 450 TO 660, LBL58. REPLACED CREASE BEAM IAW SRM 51-40-02 & SRM 51-40-05.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON MAIN DECK CHANNEL WEB BETWEEN BS 333 TO 345 & BETWEEN LBL 32 TO LBL 20. REPLACED MAIN DECK CHANNEL WEB BETWEEN BS 333 TO 345 & BETWEEN LBL 32 TO LBL 20 IAW SRM 51-40-02 & 51-40-05.

Part: REPAIR — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON EXISTING FLOORBEAM REPAIR AT BS 377.7 BETWEEN BL0 TO LBL 45.5. REPLACED EXISTING FLOORBEAM REPAIR AT BS 377.7 BETWEEN BL0 TO LBL 45.5 IAW SRM 53-00-51-2R-1 & 51-40-02.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 FILIFORM CORROSION ON SUPPORT CHANNEL BETWEEN BS 333 TO 345 LBL32. REPLACED SUPPORT CHANNEL BETWEEN BS 333 TO 345 LBL 32 IAW SRM 53-00-51-1A-1, 51-40-02 & 51-40-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN BS 700 TO 720, LBL 58. REPLACED FLOOR SUPPORT BETWEEN BS 700 TO 720, LBL 58 IAW SRM 51-40-02 & 51-40-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN BS 333.45 TO 345 & BETWEEN LBL 20 TO 32. REPLACED FLOOR SUPPORT BETWEEN BS 333.45 TO 345 & BETWEEN LBL 20 TO 32 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN BS 324 TO 345, LBL 20. REPLACED FLOOR SUPPORT BETWEEN BS 324 TO 345, LBL 20 IAW SRM 51-40-02 & 51-40-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON L1 DOOR LOWER SILL FLOOR SUPPORT BETWEEN BS 365.25 TO 377.7, LBL 56. REPLACED FLOOR SUPPORT BETWEEN BS 365.25 TO 377.7, LBL 56 IAW SRM 51-40-02 & 51-40-05.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON L1 DOOR LOWER SILL FLOOR CHANNEL BETWEEN BS 345 TO 365.25, LBL 58.22. REPLACED FLOOR CHANNEL BETWEEN BS 345 TO 365.25, LBL 58.22 IAW SRM 51-40-02 & 51-40-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK CABIN FLOOR SUPPORT CORRODED AT BS 1320 & LBL 24.75. FABRICATED & INSTALLED REPLACEMENT SUPPORT IAW SRM 51-40-02 & 51-40-05.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK CREASE BEAM CHORD CORRODED AT BS 1320 & BLB 63. R & R CHORD IAW SRM 51-40-02 & 51-40-05.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK CREASE BEAM CORRODED AT BS 1240 & RBL 63. FABRICATED & INSTALLED REPLACEMENT BEAM IAW SRM 53-60-13 FIG 101 DETAIL 8, 51-40-02 & DWG 146N5590.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK CABIN FLOOR SUPPORT CORRODED AT BS 730 AND LBL 58. R & R SUPPORT IAW SRM 51-40-02, 51-40-05 & 51-20-01.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON ANGLE BETWEEN BS 1700 TO 1730, RBL 50. REPLACED ANGLE BETWEEN BS 1700 TO 1730, RBL 50 IAW SRM 51-40-02 & 51-40-05.

Part: TEE FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON TEE CHORD BETWEEN BS 780 TO 800, BL 0. REPAIRED TEE CHORD BETWEEN BS 780 TO 800, BL 0 IAW SRM 51-40-02, 51-40-05 & 51-20-01.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON ANGLE AT BS 1646, RBL 61. REPLACED ANGLE AT BS 1646, RBL 61 IAW SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON ANGLE AT BS 1676, RBL 53. REPLACED ANGLE AT BS 1676, RBL 53 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT INBD CHORD AT BS 1320, RBL 63. REPLACED FLOOR SUPPORT INBD CHORD AT BS 1320, RBL 63 IAW SRM 51-40-02.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON SUPPORT CHANNEL BETWEEN BS 1640 TO 1661, RBL25. REPLACED SUPPORT CHANNEL BETWEEN BS 1640 TO 1661, RBL25 IAW SRM 51-40-02.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON PLATE AT BS 1708, LBL 50. REPLACED PLATE AT BS 1708, LBL 50 IAW SRM 51-40-02.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON SUPPORT CHANNEL BETWEEN BS 1661 TO 1680, RBL 56. REPLACED SUPPORT CHANNEL BETWEEN BS 1661 TO 1680, RBL 56 IAW SRM 51-40-02.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON AFT DECK PLATE AT BS 1715, RBL 51. REPLACED AFT DECK PLATE AT BS 1715, RBL 51 IAW SRM 53-60-51-2A REPAIR 2.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON SUPPORT ANGLE AT BS 1680, RBL 61. REPLACED SUPPORT ANGLE AT BS 1680, RBL 61 IAW SRM 51-40-02 & 51-40-05.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON AFT CABIN DECK PLATE AT BS 1690, BL0. REPLACED AFT CABIN DECK PLATE AT BS 1690, BL 0 IAW SRM 53-60-51 REPAIR 2 FIG 201 SHEET 1-5.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON DECK PLATE DOUBLER AT BS 1715, LBL 5. REPLACED DECK PLATE DOUBLER AT BS 1715, LBL 5 IAW SRM 53-60-51-2A-2 ALT 1 & 51-40-02.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON DECK PLATE DOUBLER AT BS 1715, RBL 5. REPLACED DECK PLATE DOUBLER AT BS 1715, RBL 5 IAW SRM 53-60-51-2R-2 ALT 1 & 51-40-02.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON DECK PLATE AT BS 1680, RBL 51. REPLACED DECK PLATE AT BS 1680, RBL 51 IAW SRM 53-60-51-2R-2 ALT 1 & 51-40-02.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON DECK PLATE AT BS 1718, LBL20. REPLACED DECK PLATE AT BS 1718, LBL 20 IAW SRM 51-10-02 & 53-60-51-2R-2 ALT 1.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON DECK PLATE DOUBLER AT BS 1715, LBL 33. REPLACED DECK PLATE DOUBLER AT BS 1715, LBL 33 IAW SRM 53-60-51-2A-2 ALT 1 & 51-40-02.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON L4 DOOR LOWER SILL STIFFENER AT BS 1656, LBL61. REPLACED L4 DOOR LOWER SILL STIFFENER AT BS 1656, LBL61 IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN BS 1540 TO 1620, RBL 45. REPLACED SEAT TRACK BETWEEN BS 1540 TO 1620, RBL 45 IAW SRM 51-40-02, 53-00-52 FIG 101 DET 1 51-40-05 & 51-20-01.

Part: HARNESS — CUT (EVAC SLIDE) · airframe 64,324 hrs · 24,416 cycles

C4 CHECK R4 ENTRY ESCAPE SLIDE HARNESS ASSEMBLY HAS CUT & TORN. REPLACED R4 ENTRY ESCAPE SLIDE HARNESS ASSEMBLY IAW AMM 25-66-01-PB401.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON L4 DOOR LOWER SILL STIFFENER AT BS 1672, LBL 61. REPLACED L4 DOOR LOWER SILL STIFFENER AT BS 1672, LBL 61 IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN BS 1100 TO 1140, LBL 45.75. REPLACED SEAT TRACK BETWEEN BS 1100 TO 1140, LBL 45.75 IAW SRM 53-00-52, 51-10-02, 51-40-02 & 51-40-05.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON SUPPORT CHANNEL BETWEEN BS 1661 TO 1680, BL0. REPLACED SUPPORT CHANNEL BETWEEN BS 1661 TO 1680, BL0 IAW SRM 51-40-02, 51-10-02 & AMM 51-21-00.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON SUPPORT CHANNEL BETWEEN BS 1640 TO 1661, BL0. REPLACED SUPPORT CHANNEL BETWEEN BS 1640 TO 1661, BL0 IAW SRM 51-40-02, 51-40-05 & 51-21-00.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON SUPPORT CHANNEL BETWEEN BS 1640 TO 1661, RBL 56. REPLACED SUPPORT CHANNEL BETWEEN BS 1640 TO 1661, RBL 56 IAW SRM 51-40-02, 51-40-05 & 51-20-00.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON CREASE BEAM BETWEEN BS 640 - 900, RBL67. REPLACED CREASE BEAM BETWEEN BS 640 - 900, RBL 67 IAW SRM 51-40-02, 51-40-05, 51-20-01 & AMM 51-21-00.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON SUPPORT CHANNEL ATTACH ANGLE AT BS 1676, LBL 52. REPLACED SUPPORT CHANNEL ATTACH ANGLE AT BS 1676, LBL 52 IAW SRM 51-40-02, 51-40-05 & AMM 51-20-00.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON SUPPORT CHANNEL BETWEEN BS 1661 TO 1680, LBL 55. REPLACED SUPPORT CHANNEL BETWEEN BS 1661 TO 1680, LBL 55 IAW SRM 51-40-02, 51-40-05 & 51-10-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT BS 1640 BETWEEN LBL 10 TO RBL 59. REPAIRED FLOORBEAM AT BS 1640 BETWEEN LBL 10 TO RBL 59 IAW SRM 53-00-51-2R-8, REPAIR 8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN BS 1320 TO 1540, RBL45.5. REPAIRED SEAT TRACK BETWEEN BS 1320 TO 1540, RBL 45.5 IAW SRM 51-40-02.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON R4 DOOR LOWER SILL STIFFENER AT BS 1656, RBL 61. REPLACED R4 DOOR LOWER SILL STIFFENER AT BS 1656, RBL 61 IAW SRM 51-40-02.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON R4 DOOR LOWER SILL STIFFENER AT BS 1672, RBL 61. REPLACED R4 DOOR LOWER SILL STIFFENER AT BS 1672, RBL 61 IAW SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON ANGLE AT BS 1680, LBL 61. REPLACED ANGLE AT BS 1680, LBL 61 IAW SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON ANGLE ASSEMBLY AT BS 1644, LBL 61. REPLACED ANGLE ASSEMBLY AT BS 1644, LBL 61 IAW SRM 51-40-02.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON DECK ATTACH PLATE AT BS 1680, RBL 41. REPLACED DECK ATTACH PLATE AT BS 1680, RBL 41 IAW SRM 53-60-13, 51-40-02 & DWG 417N2607.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN BS 1540 TO 1640, RBL 24.75. REPAIRED SEAT TRACK BETWEEN BS 1540 TO 1640, RBL 24.75 IAW SRM 51-40-02.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,324 hrs · 24,416 cycles

C4 CHECK LEVEL 2 GALVANIC CORROSION ON DECK ATTACH PLATE AT BS 1680, RBL 34. REPLACED DECK ATTACH PLATE AT BS 1680, RBL 34 IAW SRM 51-40-02 & DWG 417N2607.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 62,742 hrs · 23,945 cycles

CLT PORTABLE EMERGENCY FLASHLIGHT AT 3L DOOR INOPERATIVE. R & R BATTERY IN FLASHLIGHT AT 3L DOOR, OK FOR SERVICE.

Part: TRANSMISSION — TRIPPED (TE FLAPS) · airframe 61,092 hrs · 23,480 cycles

ENROUTE, FLIGHT CREW OBSERVED A "T/E FLAP DISAGREE" MESSAGE WITH FLAP HANDLE AT 20. DECLARED AN EMERGENCY AND EXECUTED A MISSED APPROACH IN ORDER TO PERFORM THE ALTERNATE FLAPS PROCEDURE. ON SELECTING ALTERNATE FLAPS, "T/E FLAP DISAGREE" MESSAGE DISAPPEARED. FLAPS WERE EXTENDED TO 30 USING ALTERNATE FLAP EXTENSION PROCECDURE. LANDED WITHOUT FURTHER INCIDENT. FOUND NR 1 FLAP TRANSMISSION OVERLOAD INDICATOR TRIPPED. RESET OVERLOAD INDICATOR AND COMPLIED WITH NORMAL FLAP SYS OPS CHECK. NO DEFECTS NOTED. NR ONE FLAP TRANSMISSION OVERLOAD INDICATOR WAS INSPECTED AGAIN SEVERAL DAYS LATER WITH NO FAULTS FOUND.

Part: LIGHT — DAMAGED (CABIN)

DCA - DOOR 4L EXIT LIGHT ASSY IS DAMAGED. REPLACED 4L EMERGENCY EXIT LIGHT ASSY.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 59,814 hrs · 23,071 cycles

FLL - EMERGENCY FLASHLIGHT - FLIGHT ATTENDANT SEAT (LAV D) INOP. REPLACED FLIGHT ATTENDANT SEAT (LAV D) FLASHLIGHT BATTERY.

Part: COOLING FAN — DAMAGED (ZONE 100) · airframe 58,861 hrs · 22,704 cycles

PHL FLT 1020 EN ROUTE PHL TO MCO. SHORTLY AFTER T/O, PASSING APPROX 9,000, COCKPIT FUMES OF RUBBER TYPE SOURCE WAS EXPERIENCED, 4 TO 5 MIN LATER RECEIVED EMERGENCY EQUIP EICAS MESSAGE. THE COCKPIT CREW DONNED THEIR OXYGEN MASKS, AND DECLARED AN EMERGENCY WITH ATC. THE FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE EQUIPMENT COOLING FAN. VENDOR SHOP FINDINGS: UNIT PASSES ELECTRICAL TESTS. APPEARS TO HAVE INGESTED FOD. CARBON AND BURNT FOD ON IMPELLER AND FAN HOUSING. IMPELLER BLADES NICKED AND BENT. ROTOR DIMENSIONS OUT OF TOLERANCE. CHIP MISSING FROM BEARING SEAT ON ROTOR SHAFT. END BELL BEARING LINER DAMAGED.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 58,176 hrs · 22,513 cycles

C3 CHECK - LEFT WING NR 4 SLAT TRAILING EDGE UPPER SURFACE 24.5 INCHES FROM OUTBOARD EDGE IS DELAMINATED (2 IN DIA AREA). REMOVED AND REPLACED SLAT IAW TASK CARD 19L52027002.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 58,176 hrs · 22,513 cycles

C3 CHECK - LEFT WING NR 3 SLAT TRAILING EDGE LOWER SURFACE 40 INCHES FROM OUTBOARD EDGE IS DELAMINATED (2 IN DIA AREA). REMOVED AND REPLACED SLAT IAW TASK CARD 19L52027002.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 58,176 hrs · 22,513 cycles

C3 CHECK - LEFT WING NR 3 SLAT TRAILING EDGE UPPER SURFACE 15 INCHES FROM THE OUTBOARD EDGE IS DELAMINATED AT PREVIOUS REPAIR (2 IN DIA AREA). REMOVED AND REPLACED SLAT IAW TASK CARD 19L52027002.

Part: BEARING — WORN (RECIRC FAN) · airframe 58,056 hrs · 22,472 cycles

ORF - FLT 1020 EN ROUTE PHL TO MCO. UNKNOWN FUMES IN COCKPIT AND CABIN. CREW MEMBERS EXPERIENCED EYE BURNING/ THROAT IRRITATION. CAPT EXPERICENCED EYE BURNING AND DIZZINESS. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO ORF. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT CABIN RECIRCULATION FAN. REPLACED WORN BEARINGS.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,082 hrs · 21,856 cycles

RON CHECK - CORROSION ON FUSELAGE SKIN IN AREA AROUND FORWARD LAV SERVICE PANEL AT BS 420, S27L, BL 0. REPAIRED FUSELAGE SKIN AT FORWARD LAV SERVICE PANEL IAW EA 103410 & 103384.

Part: OVEN — ODOR (GALLEY) · airframe 56,024 hrs · 21,837 cycles

PHL - FLT 769 GLA TO PHL. OVEN 4-13 IN AFT GALLEY SMELLS SMOKEY WHEN HEATED. REMOVED AND REPLACED AFT OVEN (413). OPS CHECK OK.

Part: DUCT — OBSTRUCTED (WASTE DISPOSAL) · airframe 55,268 hrs · 21,650 cycles

MCO - FLT 1020 EN ROUTE PHL TO MCO. F/A IN AFT OF CABIN REPORTED BAD ODOR AND BURNING IN THROAT. REPORTED THAT IT DISSIPATED IN DESCENT AFTER 10,000 SIGNAL. FIRST ADVISED OF PROBLEM 50 MIN INTO CRUISE AT 40,000FT. TROUBLESHOT TO MID LAV BEING ON MEL AND NOT BEING SERVICED FOR SEVERAL DAYS AS A RESULT. REMOVED A TWO FOOT OBSTRUCTION FROM WASTE DUCT IN FORWARD CARGO COMPARTMENT. ALSO, SERVICED THE LAVATORIES. FINALLY, REMOVED AND REPLACED THE HEPA FILTERS.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

MCO - FLASHLIGHT AT FLIGHT ATTENDANT SEAT BY DOOR L2 HAS A DISCHARGED BATTERY. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY FOR THE FLASHLIGHT AT THE L2 DOOR.

Part: VALVE — LOW PRESSURE (R3 DOOR SLIDE)

R3 DOOR ESCAPE SLIDE BOTTLE INDICATES "EMPTY". MAINTENANCE REPLACED THE SLIDE ASSEMBLY. REPAIRED SLIDE. UNIT WAS PARTIALLY DISASSEMBLED, CLEANED AND INSPECTED REPLACING ALL PARTS NECESSARY FOR REPAIR. REPAIRED AND CHARGED RESERVOIR AND VALVE ASSY OVERHAULED VALVE. PASSED PULL FORCE, GAGE SYSTEM AND LEAK TEST. PACKED SLIDE.

Part: WIRE — BROKEN (CABIN)

THE EMERGENCY EXIT LIGHT OVER DOOR L4 WAS INOPERATIVE. A BROKEN WIRE WAS FOUND. MAINTENANCE ACCOMPLISHED A TEMPORARY REPAIR AND DEFERRED THE FINAL REPAIR OF THE AIRCRAFT UNDER ENGINEERING AUTHORIZATION NOT TO EXCEED SEVEN DAYS. ALSO, MOC REQUESTED REPLACEMENT OF THE CHARGER AND BATTERY PACK ASSEMBLY (M737). MAINTENANCE ACCOMPLISHED THE REPLACEMENT OF THE CHARGER AND BATTERY PACK AT THE L4 DOOR. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY ABOVE THE L4 DOOR.

Part: SKIN PANEL — DELAMINATED (VERTICAL STAB) · airframe 53,198 hrs · 20,991 cycles

CLT - MAJOR REPAIR - C2 CHECK - VERTICAL STABILIZER SKIN PANEL 6 INCHES AFT OF AUXILIARY SPAR AT STATION 120 IS DELAMINATED. REPLACED VERTICAL STABILIZER SKIN PANEL 6 INCHES AFT OF AUXILIARY SPAR AT STATION 120 IAW BOEING 757 DRAWING 175N2001.

Part: SLIDE — INOPERATIVE (L4 DOOR) · airframe 53,198 hrs · 20,991 cycles

CLT - EES - C2 CHECK - DURING A SCHEDULED DEPLOYMENT OPERATIONAL CHECK OF THE L4 DOOR SLIDE, THE LOWER AFT LIGHT DID NOT ILLUMINATE. REPLACED SLIDE IAW TASK CARD 19L80025001.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 53,198 hrs · 20,991 cycles

CLT - MAJOR REPAIR - C2 CHECK - CORROSION ON STRINGER AT BS 1412 - BS 1440, S30. REPAIRED STRINGER AT BS 1412 - BS 1440, S30 IAW EA 102306.

Part: PANEL — DELAMINATED (VERTICAL STAB) · airframe 53,198 hrs · 20,991 cycles

CLT - MAJOR REPAIR - C2 CHECK - VERTICAL STABILIZER LEFT TORQUE BOX PANEL HAS DELAMINATION. REPAIRED VERTICAL STABILIZER LEFT TORQUE BOX PANEL IAW EA 139564.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 53,198 hrs · 20,991 cycles

CLT - MAJOR REPAIR - C2 CHECK - LEFT WING LEADING EDGE SLAT NR 4 TRAILING EDGE WEDGE LOWER SURFACE HAS DELAMINATION. REPAIRED LEFT WING LEADING EDGE SLAT NR 4 TRAILING EDGE WEDGE LOWER SURFACE IAW B757 SRM 51-70-10.

Part: BEAM — CRACKED (VERTICAL STAB) · airframe 53,198 hrs · 20,991 cycles

CLT - MAJOR REPAIR - C2 CHECK - VERTICAL STABILIZER T/E BEAM CRACKED AT STATION 90. REPAIRED VERTICAL STABILIZER T/E BEAM AT STATION 90 IAW EA 102285.

Part: BATTERY PACK — DISCHARGED (CABIN)

PIT - AFT EMERGENCY EXIT SIGHT AT R4 DOOR WAS INOPERATIVE. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN)

PIT - THE AFT EMERGENCY EXIT SIGN AT R4 DOOR WAS INOPERATIVE. REPLACED THE BATTERY PACK AT THE R4 DOOR.

Part: CONTROLLER — FAULTY (WINDOW HEAT)

GLA - FLT 768 PHL TO GLA. FRONT RIGHT WINDOW HEAT ON UPPER BORDER OF WINDSHIELD ARCING. ARCING STOPS WHEN POWER REMOVED BY TURNING OFF WINDOW HEAT SWITCH. REPLACED NUMBER ONE WINDSHIELD RIGHT AND WINDOW HEAT CONTROLLER.

Part: WINDSHIELD — ARCED (COCKPIT)

GLA - FLT 768 PHL TO GLA. FRONT RIGHT WINDOW HEAT ON UPPER BORDER OF WINDSHIELD ARCING. ARCING STOPS WHEN POWER REMOVED BY TURNING OFF WINDOW HEAT SWITCH. REPLACED NUMBER ONE WINDSHIELD RIGHT AND WINDOW HEAT CONTROLLER.

Part: LIGHT — INOPERATIVE (L4 DOOR)

PHL - THE 4L DOOR LIGHT INDICATION SLIDE ARMED IS INOP. MAINTENANCE RELAMPED 4L DOOR ARM INDICATION LIGHTS.

Part: RELAY — OVERHEATED (COCKPIT)

PHL FLT 1608 MCO - PHL. WITH BRIGHT DIM LIGHT SWITCH SELECTED TO DIM, LIGHTS WENT AND DIM CONTINUOUSLY. FOR 45 MINUTES OF FLIGHT, SMELL OF SMOKE NOTED IN COCKPIT. REPLACED RELAY K10451.

Part: RELAY — OVERHEATED (COCKPIT)

PHL - FLT 1608 MCO - PHL. WITH BRIGHT DIM LIGHT SWITCH SELECTED TO DIM, LIGHTS WENT BRIGHT AND DIM CONTINUOUSLY. FOR 45 MINUTES OF FLIGHT, SMELL OF SMOKE NOTED IN COCKPIT. REPLACED RELAY K10145.

Part: LIGHT — INOPERATIVE (L2 DOOR)

THE ARMED LIGHT ABOVE BOARDING DOOR L2 DOES NOT ILLUMINATE WHEN DOOR IS CLOSED AND ARMED. MX RELAMPED THE L2 DOOR ARMED LIGHT. OPS CHECK OK. (K)

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,414 hrs · 19,589 cycles

MCN C1 MAJOR REPAIR NR 6186665 CORROSION CREASE BEAM CHORD BETWEEN BS760 TO BS780, S17L, LBL64. REPAIRED CREASE BEAM CHORD BETWEEN BS760 TO BS780, S17L, LBL64 IAW US AIRWAYS EA NR 130190.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,414 hrs · 19,589 cycles

MCN C1 MAJOR REPAIR NR 6186663 CORROSION CREASEBEAM CHORD BETWEEN BS655 TO BS665, S17L. REPAIRED CREASEBEAM CHORD BETWEEN BS655 TO BS665, S17L, IAW EA NR 130190.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,414 hrs · 19,589 cycles

MCN C1 MAJOR REPAIR NR 6186665 CORROSION CREASE BEAM CHORD BETWEEN BS760 TO BS780, S17L, LBL64. REPAIRED CREASE BEAM CHORD BETWEEN BS760 TO BS780, S17L, LBL64 IAW EA NR 130190.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,414 hrs · 19,589 cycles

MCN C1 MAJOR REPAIR NR 6186663 CORROSION CREASE BEAM CHORD BETWEEN BS655 TO BS665, S17L. REPAIRED CREASE BEAM CHORD BETWEEN BS655 TO BS665, S17L, LBL64 IAW US AIRWAYS EA NR 130190.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 47,414 hrs · 19,589 cycles

MCN - C1 - MAJOR REPAIR - NR 6141838 - CORROSION ON DRAIN SUPPORT ANGLE BETWEEN BS700 TO BS720, S17L AT L2 DOOR CUTOUT. REPLACED DRAIN SUPPORT ANGLE BETWEEN BS700 TO BS720, S17L AT L2 DOOR CUTOUT IAW B757 SRM 51-40-02.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 47,414 hrs · 19,589 cycles

MCN - C1 - MAJOR REPAIR - CORROSION ON L2 DOOR INNER GUTTER SUPPORT ANGLE BETWEEN BS 720 TO BS 740, S17L. REPLACED L2 DOOR INNER GUTTER SUPPORT ANGLE BETWEEN BS 720 TO BS 740, S17L IAW B757 SRM 51-40-02.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 47,414 hrs · 19,589 cycles

MCN - C1 - MAJOR REPAIR - CORROSION ON SUPPORT ANGLE BS 729, S17L AT L2 DOOR CUTOUT. REPLACED SUPPORT ANGLE BS 729, S17L AT L2 DOOR CUTOUT IAW B757 SRM 51-40-02.

Part: SUPPORT ANGLE — CORRODED (BS 720-740) · airframe 47,414 hrs · 19,589 cycles

MCN - C1 - MAJOR REPAIR - CORROSION ON L2 DOOR CUTOUT OTBD SUPPORT ANGLE BETWEEN BS 720 TO BS 740, S17L. REPLACED L2 DOOR CUTOUT OTBD SUPPORT ANGLE BETWEEN BS 720 TO BS 740, S17L IAW B757 SRM 51-40-02.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 47,414 hrs · 19,589 cycles

MCN - C1 - MAJOR REPAIR - CORROSION ON GUTTER SUPPORT ON L2 DOOR CUTOUT BETWEEN BS 680 TO BS 700, S17L. REPLACED GUTTER SUPPORT ON L2 DOOR CUTOUT BETWEEN BS 680 TO BS 700, S17L IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 47,414 hrs · 19,589 cycles

MCN - C1 - MAJOR REPAIR - CORROSION ON FLOOR SUPPORT INTERCOSTAL BS 680, LBL 45 TO LBL 55 AT L2 DOOR. REPLACED FLOOR SUPPORT INTERCOSTAL BS 680, LBL 45 TO LBL 55 AT L2 DOOR IAW B757 SRM 51-40-02.

Part: SKIN — DEBONDED (LE SLAT) · airframe 47,414 hrs · 19,589 cycles

MCN - C1 - MAJOR REPAIR - NR 6 SLAT DISBONDED ON UPPER & LOWER SURFACES AT TRAILING EDGE WEDGE ISS110.5. REPAIRED NR 6 SLAT UPPER & LOWER SURFACES AT TRAILING EDGE WEDGE ISS110.5 IAW B757 SRM 51-70-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 47,414 hrs · 19,589 cycles

MCN - C1 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN BS 700 TO BS 740, LBL 45. REPLACED SEAT TRACK BETWEEN BS 700 TO BS 740, LBL 45 IAW B757 SRM 51-40-04.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 47,414 hrs · 19,589 cycles

MCN C1 - MAJOR REPAIR - NR 6143956 - CORROSION ON SUPPORT ANGLE BETWEEN BS700 TO BS720, LBL55 AT L2 DOOR. REPLACED SUPPORT ANGLE BETWEEN BS700 TO BS720, LBL55 AT L2 DOOR IAW B757 SRM 51-40-02.

Part: WEDGE — DEBONDED (LE SLAT) · airframe 47,414 hrs · 19,589 cycles

MCN - C1 - MAJOR REPAIR - NR 10 SLAT TRAILING EDGE WEDGE DISBONDED BETWEEN STATIONS OSS829.92 TO OSS830.42. REPAIRED NR 10 SLAT TRAILING EDGE WEDGE IAW B757 SRM 51-70-10.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 47,414 hrs · 19,589 cycles

MCN - C1 - MAJOR REPAIR - CORROSION ON DRAIN TROUGH SUPPORT BETWEEN BS 720 TO BS 740, LBL 55 AT L2 DOOR. REPLACED DRAIN TROUGH SUPPORT BETWEEN BS 720 TO BS 740, LBL 55 AT L2 DOOR IAW B757 SRM 51-40-02.

Part: SKIN PANEL — CRACKED (LE SLAT) · airframe 47,414 hrs · 19,589 cycles

MCN - C1 - MAJOR REPAIR - CRACK ON NR 9 SLAT COVE PANEL AT 0SS-601. REPLACED NR 9 SLAT COVE PANEL AT 0SS-601 IAW B757 SRM 51-40-02.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,414 hrs · 19,589 cycles

MCN - C1 - MAJOR REPAIR - CORROSION ON INNER CHORD BETWEEN BS 700 TO BS 740, LBL 55. REPLACED L2 DOOR INNER CHORD IAW B757 SRM 51-40-02.

Part: O-RING — BROKEN (RT ENGINE)

CUN FLT 816 EN ROUTE CLT TO CUN: FMC FUEL DISAGREE MESSAGE. RIGHT TANK QTY DECREASED AT A HIGHER RATE. AIRCRAFT USED 4000 LBS MORE THAN FLIGHT PLAN. AFTER ARRIVAL CAPT OBSERVED FUEL LEAKING FROM RT ENGINE ON GROUND. MAINTENANCE FOUND LEAK ON RT ENGINE AT FUEL PIPE BETWEEN HP FUEL PUMP TO FFG. FOUND BROKEN O-RING. REPLACED O-RING AND RAN ENGINE WITH NO LEAKS NOTED.

Part: FLOOR SUPPORT — CORRODED (BS 305-345) · airframe 42,080 hrs · 42,080 cycles

CABIN FLOOR SUPPORT LBL 0, STA 345.0-395 HAS CORROSION. BLENDED AT STA 374 BL 0, REMOVED & REPLACED FLOOR SUPPORT AT STA 324-395 AT BL 0 PER SRM 53-00-51, DEFECT SIZE: 4.5"L X 2"W X .016"D.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 42,080 hrs · 42,080 cycles

STA 345, LBL 0 - LBL 20, CABIN FLOORBEAM CORRODED. BLENDED AREA & INSTALLED DOUBLERS PER TYP REP 53-15-02, 51-20-01, CORR TASK C53-221-03; LEVEL 1, DEFECT SIZE: 1"L X 1"W X .013"D.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 42,080 hrs · 42,080 cycles

RBL 14-17 STA 1660 CABIN FLOORBEAM FASTENER HOLES CORRODED. INSTALLED FAB'D NUT PLATE STRIP ANGLE PER TYP REP 53-15-02, 51-40-02, CORR TASK C53-251-03; LEVEL 1, DEFECT SIZE: 3"L X .800"W X .025"D.

Part: INDICATOR — TRIPPED (GRA) · airframe 40,403 hrs · 16,700 cycles

FLIGHT 773, PHL-LAS: ON APPROACH, RECEIVED LEADING EDGE DISAGREE MESSAGE. EXECUTED GO-AROUND. WHEN CREW BEGAN TO SELECT ALTERNATE FLAP SWITCH, FLAP NEEDLES MATCHED AGAIN AND SYSTEM OPERATED NORMALLY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NR 12 GRA OVERLOAD INDICATOR TRIPPED. ACCOMPLISHED RESET, AND NO FURTHER FAULTS NOTED.