N937UW

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 71,690 hrs · 26,567 cycles

AIRCRAFT WAS NOT GROUNDED, L4 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED L4 DOOR EXTERIOR EMERGENCY LIGHT ASSEMBLY AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 33-51-06-962-049-001.

Part: GATE — CORRODED (R2 DOOR) · airframe 71,203 hrs · 26,460 cycles

DURING MAINTENANCE, R2 DOOR LOWER GATE EDGES HAVE CORROSION. REPLACED THE LOWER GATE IAW AMM 52-11-38-401.

Part: COVER — DETACHED (R4 DOOR) · airframe 71,203 hrs · 26,460 cycles

AIRCRAFT IN BASE MAINTENANCE. R4 DOOR GIRT BAR FORWARD SWITCH COVER DETACHED. REATTACHED R4 DOOR GIRT BAR SWITCH COVER IAW SRM 52-10-02.

Part: SHEAR TIE — CRACKED (BS 1320) · airframe 71,203 hrs · 26,460 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOORBEAM SHEAR TIE CRACKED AT BS 1320 AND LBL 40.50 AS VIEWED FROM THE AFT CARGO COMPARTMENT CEILING AREA. REPLACED THE SHEAR TIE PER SRM 51-40-02.

Part: SHEAR TIE — CRACKED (BS 1320) · airframe 71,203 hrs · 26,460 cycles

CABIN FLOORBEAM SHEAR TIE CRACKED AT BS 1320 AND LBL 24.75 AS VIEWED FROM THE AFT CARGO COMPARTMENT CEILING AREA. REPLACED SHEAR TIE PER SRM 51-40-02

Part: LIGHT — BULGED (CABIN) · airframe 70,943 hrs · 26,403 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHTING STRIPS BULGING ROW 17 BOTH SIDES OF AISLE. REPOSITIONED & SECURED EMER LIGHT STRIPS AT ROW 17.

Part: SLIDE — LOW PRESSURE (R3 DOOR) · airframe 70,799 hrs · 26,370 cycles

AIRCRAFT WAS NOT GNDED. R3 DOOR SLIDE LOW PRESS. REPLACED R3 DOOR SLIDE IAW TASK CARD 19L83525001.

Part: FAN — SEIZED (ZONE 100) · airframe 70,748 hrs · 26,357 cycles

AIRCRAFT WAS GNDED. BURNING RUBBER ODOR IN CABIN FROM ROW 3 TO AFT GALLEY STRONG DOOR, QUICKLY SHUT OFF IFE SYS NO ODOR FOR 2 HOURS. ODOR RETURNED VERY STRONG SHUT OFF BOTH UTILITY BUSES & BOTH RECIRCULATION FANS IAW QRH, NO FURTHER PROBLEM NO EICAS MSGS. FOUND THE RT RECIRCULATION FAN SEIZED. REPLACED FAN & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 21-25-01.

Part: LENS — UNSECURE (CABIN) · airframe 70,626 hrs · 26,329 cycles

AIRCRAFT WAS NOT GNDED. EMER EXIT LIGHT LENS AT SEAT ROW 10D HANGING FROM OVERHEAD BIN. SECURED EMER EXIT LIGHT LENS AT SEAT ROW 10D IAW AMM 33-50-00.

Part: LENS — DETACHED (CABIN) · airframe 70,265 hrs · 26,244 cycles

AIRCRAFT WAS NOT GNDED. AFT DOOR 4R EMER EXIT LIGHT LENS COVER IS OFF. SECURED EXIT LIGHT LENS AT R4 DOOR.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 69,646 hrs · 26,105 cycles

AIRCRAFT WAS NOT GNDED. AFT LT INBD FLASHLIGHT INOPERATIVE. REPLACED AFT LT INBD FLASHLIGHT BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 69,368 hrs · 26,012 cycles

BULLNOSE EMER LIGHT INOPERATIVE. REPLACED POWER SUPPLY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-07-022-020.

Part: LINE — MISROUTED (EVAC SLIDE) · airframe 69,365 hrs · 26,011 cycles

FOUND R1 DOOR SLIDE STATIC LINE & D RING ASSEMBLY IMPROPERLY SECURED. RESTORED R1 DOOR ESCAPE SLIDE STATIC LINE & D RING, CORRECTLY ATTACHED SURVIVAL KIT STRAP TO GIRT SLIDE ASSEMBLY. OPERATIONS CHECKED GOOD IAW AMM 25-66-01-401.

Part: OVEN — DEFECTIVE (GALLEY) · airframe 67,838 hrs · 25,629 cycles

FLIGHT 868, EN-ROUTE FIRST CLASS OVEN NR 2 CB PULLED IN FLIGHT. OVEN SMOKING & METAL ELEMENTS SPARKING. REPLACED THE FWD GALLEY NR 2 OVEN.

Part: TRANSMITTER — FAILED (HYDRAULIC SYS)

FLIGHT 1796 EN-ROUTE, DURING APPROACH, EICAS MSG BRAKE SOURCE & RT HYD SYS PRESS OVERHEAD PANEL LIGHT CAME ON. PERFORMED QRH PROCEDURES, THEN DECLARED AN EMER. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. FOUND AUTO EVENT SHOWED RT SYS PRESS AT 3050, NORMAL. R & R RT SYS PRESS TRANSMITTER. LEAKS & OPERATIONS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,346 hrs · 25,491 cycles

C1 CHECK, CORROSION ON FWD CARGO COMPARTMENT FLOOR STRINGER BETWEEN BS 705 & 771 AT LBL 16.10. REPAIRED FLOOR STRINGER IAW SRM 53-00-53-2R-1.

Part: SIDEWALL PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,346 hrs · 25,491 cycles

C1 CHECK, CORROSION ON FWD CARGO COMPARTMENT FLOOR STRUCTURE SIDE PANEL BETWEEN BS 645 & 765, RBL 19 - RBL26. REPLACED FLOOR STRUCTURE SIDE PANEL IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,346 hrs · 25,491 cycles

C1 CHECK, CORROSION ON FWD CARGO COMPARTMENT FLOOR SUPPORT BRACKET AT BS 670, BETWEEN LBL 10.45 & LBL 16.10. REPLACED FLOOR SUPPORT BRACKET IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,346 hrs · 25,491 cycles

C1 CHECK, CORROSION ON FWD CARGO COMPARTMENT FLOOR SUPPORT BRACKET AT BS 740, BETWEEN RBL 10.45 & 16.10. REPLACED FLOOR SUPPORT BRACKET IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,346 hrs · 25,491 cycles

C1 CHECK, CORROSION ON FWD CARGO COMPARTMENT FLOOR SUPPORT BETWEEN STATION 705 & 845, RBL 7.55. REPLACED FLOOR SUPPORT IAW SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,346 hrs · 25,491 cycles

C1 CHECK, CORROSION ON FWD CARGO COMPARTMENT INTERCOSTAL BETWEEN STATION 740 & 760, STRINGER 26R & 27R. REPLACED INTERCOSTAL IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,346 hrs · 25,491 cycles

C1 CHECK, CORROSION ON FWD CARGO COMPARTMENT FLOOR SUPPORT WEB BETWEEN STATION 680 - 700 AT LBL 2.90. REPLACED WEB IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,346 hrs · 25,491 cycles

C1 CHECK, CORROSION ON FWD CARGO FLOOR SUPPORT WEB BETWEEN STATION 740 & 760 AT LBL 10.45. REPLACED WEB IAW SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,346 hrs · 25,491 cycles

C1 CHECK, CORROSION ON FWD CARGO COMPARTMENT FLOOR STRINGER BETWEEN STATION 705 & 766 AT LBL 10.45. REPLACED STRINGER IAW TR 757-5310-12-0665.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,346 hrs · 25,491 cycles

C1 CHECK, CORROSION ON FWD CARGO COMPARTMENT STIFFENER AT STATION 786 & STRINGER 28L - 28R. REPLACED STIFFENER IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,346 hrs · 25,491 cycles

C1 CHECK, CORROSION ON FWD CARGO COMPARTMENT FLOOR SUPPORT WEB BETWEEN BS 680 & 700, RBL 2.90. REPLACED WEB IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,346 hrs · 25,491 cycles

C1 CHECK, CORROSION ON FWD CARGO COMPARTMENT FLOOR SUPPORT WEB BETWEEN BS 740 & 760, RBL 10.45. REPLACED WEB IAW SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,346 hrs · 25,491 cycles

C1 CHECK, CORROSION ON FWD CARGO COMPARTMENT AFT BULKHEAD LOWER ANGLE AT BS 845 BETWEEN LBL 19 & RBL 19. REPLACED ANGLE IAW SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,346 hrs · 25,491 cycles

C1 CHECK, CORROSION ON FWD CARGO COMPARTMENT FLOOR STRINGER BETWEEN BS 710 - 760, LBL 7.55. REPLACED STRINGER IAW SRM 51-40-02 & TR 757-5310-12-0665.

Part: LIGHT — MISSING (CABIN) · airframe 67,250 hrs · 25,455 cycles

ON DAILY CHECK FOUND DOOR 4L & 4R EMER LIGHT COVERS MISSING, LOWER SMALL LIGHT. REPLACED 4L & 4R EMER LIGHT ASSEMBLIES.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT)

DURING C4 CHECK, EMERGENCY LIGHT AT SEAT 15 RIGHT FAILED. TROUBLESHOT TO AN OPEN WIRE BETWEEN POWER SUPPLY M734 AT BS 1324 OVER R3 DOOR. RECONNECTED WIRES W3634-0014-20 & W0634-0001-20 IAW WDM 33-51-14.

Part: PUSHROD — BENT (L4 DOOR) · airframe 61,994 hrs · 23,975 cycles

DURING C4 CHECK, FOUND A PUSH ROD BENT AT L4 DOOR EMERGENCY ARMING RETRACTABLE DOOR MECHANISM. REPLACED PUSH ROD IAW SRM 51-40-02. PERFORMED OPS CHECKED & FOUND NORMAL.

Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,994 hrs · 23,975 cycles

C4 CHECK - CORROSION ON LOWER FUSELAGE LAVATORY SERVICE PANEL INTERIOR STIFFENER AT BS 1180, BL 0. REPLACED LOWER FUSELAGE LAVATORY SERVICE PANEL INTERIOR STIFFENER IAW SRM 51-10-02, 52-40-02, 51-20-01 & 51-40-02.

Part: CREASE BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,994 hrs · 23,975 cycles

C4 CHECK - CORROSION ON CREASE BEAM WEB AT BS 1636, LBL 60. REPLACED CREASE BEAM WEB IAW SRM 51-10-02 & 51-40-02.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,994 hrs · 23,975 cycles

C4 CHECK - CORROSION ON FLOORBEAM AT BS 1660, LBL 54. REPAIRED FLOORBEAM IAW SRM 51-10-02, 53-00-51-1A & 53-00-51-2R-3.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,994 hrs · 23,975 cycles

C4 CHECK - CORROSION ON FLOORBEAM AT BS 1640, RBL54. REPLACED FLOORBEAM IAW SRM 51-10-02 & 53-00-51-1A.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,994 hrs · 23,975 cycles

C4 CHECK - CORROSION ON FLOORBEAM AT BS 1640, LBL 53. REPLACED FLOORBEAM IAW SRM 51-10-02 & 53-00-51-1A.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,994 hrs · 23,975 cycles

C4 CHECK - CORROSION ON SUPPORT ANGLE AT BS 1348, LBL 62. REPLACED SUPPORT ANGLE IAW SRM 51-10-02, 53-00-51-1A & 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,994 hrs · 23,975 cycles

C4 CHECK - CORROSION ON SEAT TRACK AT BS 1636, RBL 25. REPLACED SEAT TRACK BETWEEN BS 1606 & 1640 IAW SRM 51-10-02, 53-00-52-1A & 53-00-52-2R-3.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,994 hrs · 23,975 cycles

C4 CHECK - CORROSION ON FLOOR SUPPORT BETWEEN BS 1661 TO 1668, LBL 55. REPLACED FLOOR SUPPORT IAW SRM 51-10-02, 53-00-04-1A & 51-40-02.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,994 hrs · 23,975 cycles

C4 CHECK - CORROSION ON INTERCOSTAL BETWEEN BS 1661 TO 1681, RBL 55. REPLACED INTERCOSTAL IAW SRM 51-10-02, 53-00-04-1A & 51-40-02.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,994 hrs · 23,975 cycles

C4 CHECK - CORROSION ON SUPPORT ANGLE AT BS 747, RBL 62. REPLACED SUPPORT ANGLE IAW SRM 51-10-02, 53-30-13-1A, 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,994 hrs · 23,975 cycles

C4 CHECK - CORROSION ON FLOOR SUPPORT BETWEEN BS 324 TO 345, RBL 4. REPLACED FLOOR SUPPORT IAW SRM 51-10-02, 53-00-51-1A & 51-40-02.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,994 hrs · 23,975 cycles

C4 CHECK - CORROSION ON INTERCOSTAL AT BS 740, RBL 62. REPLACED INTERCOSTAL IAW SRM 51-10-02, 53-00-04-1A & 51-40-02.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,994 hrs · 23,975 cycles

C4 CHECK - CORROSION ON INTERCOSTAL BETWEEN BS 700 TO 720, RBL 62. REPLACED INTERCOSTAL IAW SRM 51-10-02, 53-30-13-1A & 51-40-02.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,994 hrs · 23,975 cycles

C4 CHECK - CORROSION ON DECK PLATE BETWEEN BS 1681 TO 1720, RBL 51. REPAIRED DECK PLATE IAW SRM 51-10-02, 53-00-51-1A, 53-00-51-2R & 51-20-01.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,994 hrs · 23,975 cycles

C4 CHECK - CORROSION ON DECK PLATE BETWEEN BS 1681 TO 1720, LBL 50. REPAIRED DECK PLATE IAW SRM 51-10-02, 53-00-51-1A, 53-00-51-2R & 51-20-01.

Part: SUPPORT FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,994 hrs · 23,975 cycles

C4 CHECK - CORROSION ON FLOOR SUPPORT BETWEEN BS 365 TO 377, RBL 11. REPLACED FLOOR SUPPORT IAW SRM 51-10-02, 53-00-51-1A & 51-40-02.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 61,994 hrs · 23,975 cycles

C4 CHECK- L-2 DOOR EMERGENCY ASSIST RESERVOIR BOTTLE PRESSURE EMPTY. REPLACED L2 DOOR EMERGENCY ASSIST RESERVOIR BOTTLE IAW JC 19C8325003.

Part: LENS — MISSING (CABIN) · airframe 59,032 hrs · 23,043 cycles

GLA - DOOR R1 EMERGENCY LIGHT LENS MISSING. REPLACED R1 DOOR LOWER EMERGENCY LIGHT ASSY.

Part: BLADE — OUT OF BALANCE (RT ENGINE) · airframe 57,836 hrs · 22,673 cycles

FLT 1079 EN ROUTE. WHILE IN CRUISE, RIGHT ENGINE VIBRATION HIGH, READS 2.8 WITH NO EICAS MSG. ENG INDICATIONS WERE NORMAL. VIBRATION RETURNED BELOW 2.5 WITH THRUST LEVER RETARDED. MAINTENANCE ACCOMPLISHED SATISFACTORY ALTERNATE FAN TRIM BALANCE PROCEDURE. NORMAL VIBRATION LEVELS RESTORED.

Part: FUEL TANK — LEAKING (LT WING) · airframe 57,272 hrs · 22,469 cycles

CLT - FLT 876 CLT TO AUA. F/A REAR OF A/C DETECTED STRANGE ODOR THAT DID NOT DISSIPATE. MOSTLY IN REAR OF A/C. MAINTENANCE DETERMINED SOURCE OF ODOR TO BE FUEL LEAK AT LT WING DRY BAY. ACCOMPLISHED REPAIR OF LEAK. MAINTENANCE ALSO REPLACED THE LEFT ENGINE P&D VALVE, AND THE CABIN HEPA FILTERS AS A PRECAUTION.

Part: WIRE — DAMAGED (CABIN) · airframe 56,958 hrs · 22,377 cycles

C3 CHECK - FLIGHT STATION EMERGENCY LIGHT WILL NOT ILLLUMINATE. REPAIRED FLIGHT STATION EMERGENCY LIGHT WIRE AT REMOVABLE SPLICE, PINNED & RECONNECTED. OPS CHECK GOOD IAW BSWPM 20-30-12 & 20-60-02 AND TASK CARD # 19C20033001.

Part: WIRE — BROKEN (CABIN) · airframe 56,958 hrs · 22,377 cycles

C3 CHECK - FLIGHT STATION EMERGENCY LIGHT WILL NOT ILLUMINATE. REPAIRED FLIGHT STATION EMERGENCY LIGHT WIRES AT REMOVABLE SPLICE IAW BOEING SPWM 20-60-02.

Part: LIGHT — CRACKED (CABIN) · airframe 56,958 hrs · 22,377 cycles

C3 CHECK - THE L2 DOOR LOWER EMERGENCY EXIT LIGHT CRACKED. REPLACED THE L2 DOOR LOWER EMERGENCY EXIT LIGHT IAW B757 AMM 33-51-10.

Part: LIGHT — BROKEN (CABIN) · airframe 56,958 hrs · 22,377 cycles

C3 CHECK - L-3 AND R-3 DOOR LOWER EMERGENCY EXIT LIGHT BROKEN. REPLACED L-3 AND R-3 DOOR LOWER EMERGENCY EXIT LIGHT IAW B757 AMM 33-51-10-002-045 & 33-51-10-402-047.

Part: SLAT — DEBONDED (LT WING) · airframe 56,958 hrs · 22,377 cycles

C3 CHECK - DISBOND ON LEFT WING 3 SLAT BETWEEN WS425.5. TO WS565.5. REPAIRED NR 3 SLAT IAW B757 CMM 57-43-18, B757 SRM 51-70-10 & EA 141753.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,958 hrs · 22,377 cycles

C3 CHECK - CORROSION ON FLOORBEAM AT BS 345, LBL 18. REPAIRED FLOORBEAM AT BS 345, LBL 18 IAW B757 SRM 53-00-51-2R-5 FIG 201.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,958 hrs · 22,377 cycles

C3 CHECK - CORROSION ON SHEAR TIE AT BS 1620, BETWEEN S28R AND S29R. REPLACED SHEAR TIE AT BS 1620, BETWEEN S28R AND S29R IAW B757 SRM 51-40-02-0G.

Part: FITTING — CORRODED (FUSELAGE) · airframe 56,958 hrs · 22,377 cycles

C3 CHECK - CORROSION ON FLOOR STRUCTURE FITTING AT BS 396.50, RBL 11. REPLACED FLOOR STRUCTURE FITTING AT BS 396.50, RBL 11 IAW B757 SRM 51-40-02-0G & BOEING DRAWING 141N5161.

Part: FITTING — CORRODED (FUSELAGE) · airframe 56,958 hrs · 22,377 cycles

C3 CHECK - CORROSION ON FLOOR STRUCTURE FITTING AT BS 330, RBL 40. REPLACED FLOOR STRUCTURE FITTING AT BS 330, RBL 40 IAW B757 SRM 51-40-02-0G & 53-00-51-1A-1.

Part: FITTING — CRACKED (FUSELAGE) · airframe 56,958 hrs · 22,377 cycles

C3 CHECK - CRACK ON INTERCOSTAL CLIP BETWEEN BS 1620 TO BS 1640, BL 0. REPLACED INTERCOSTAL CLIP BETWEEN BS 1620 TO BS 1640, BL 0 IAW B757 SRM 51-40-02-0G.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,958 hrs · 22,377 cycles

C3 CHECK - CORROSION ON INTERCOSTAL BETWEEN BS 1300 AND BS 1320, BETWEEN S29R AND S30R. REPLACED INTERCOSTAL BETWEEN BS 1300 AND BS 1320, BETWEEN S29R AND S30R IAW B757 SRM 51-40-02-0G.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,958 hrs · 22,377 cycles

C3 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR TIE AT BS1440, BETWEEN S29R TO S30R. REPLACED SHEAR TIE AT BS 1440, BETWEEN S29R TO S30R IAW B757 SRM 51-40-02, BOEING DRAWING 146N1125.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,958 hrs · 22,377 cycles

C3 CHECK - CORROSION ON INTERCOSTAL BETWEEN BS 1400 AND BS 1420, BETWEEN S29L AND S30L. REPLACED INTERCOSTAL BETWEEN BS 1400 AND BS 1420, BETWEEN S29L AND S30L IAW B757 SRM 51-40-02-0G.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,958 hrs · 22,377 cycles

C3 CHECK - LEVEL 2 FILIFORM CORROSION ON INTERCOSTAL BETWEEN BS 1600 TO BS 1620, S29R TO S30R. REPLACED INTERCOSTAL BETWEEN BS 1600 TO BS 1620, S29R TO S30R IAW B757 SRM 51-40-02-OG BOEING DRAWING 146N5451.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,958 hrs · 22,377 cycles

C3 CHECK CORROSION ON INTERCOSTAL BETWEEN BS 1500 AND BS 1520 AND BETWEEN S29R AND S30R. REPLACED INTERCOSTAL BETWEEN BS 1500 AND BS 1520 AND BETWEEN S29R AND S30R IAW B757 SRM 51-40-02-0G.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,958 hrs · 22,377 cycles

C3 CHECK - CORROSION ON SUPPORT AT BS 399 AND RBL 22.34. REPLACED SUPPORT AT BS 399 AND RBL 22.34 IAW BOEING 757 SRM 51-40-02-0G PAR 7D FIG 12.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,958 hrs · 22,377 cycles

C3 CHECK - CORROSION ON HAT CHANNEL SUPPORT BETWEEN BS 324 TO BS 345, RBL 70. REPLACED HAT CHANNEL SUPPORT BETWEEN BS 345 TO BS 365, RBL 70 IAW B757 SRM 51-40-02-0G.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,958 hrs · 22,377 cycles

C3 CHECK - CORROSION ON HAT CHANNEL SUPPORT BETWEEN BS 345 TO BS 365, RBL 70. REPLACED HAT CHANNEL SUPPORT BETWEEN BS 345 TO BS 365, RBL 70 IAW B757 SRM 51-40-02-0G.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,958 hrs · 22,377 cycles

C3 CHECK - CORROSION ON FLOORBEAM AT BS 365, BETWEEN BL 0 TO RBL 70. REPAIRED FLOORBEAM AT BS 365, BETWEEN BL 0 TO RBL 70 IAW B757 SRM 53-00-51-2R-3 FIGURE 201.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,958 hrs · 22,377 cycles

C3 CHECK - CORROSION ON HAT CHANNEL SUPPORT AT BS 399, BETWEEN RBL 56 TO RBL 70. REPLACED HAT CHANNEL SUPPORT AT BS 399, BETWEEN RBL 56 TO RBL 70 IAW B757 SRM 51-40-02-0G.

Part: SKIN — CRACKED (TE FLAP) · airframe 56,958 hrs · 22,377 cycles

C3 CHECK - CRACK ON RIGHT WING INBOARD MAIN TRAILING EDGE FLAP AT WS299.13 TO WS300.38 OUTBOARD END LOWER SURFACE. REPAIRED RIGHT WING INBOARD MAIN TRAILING EDGE FLAP OUTBOARD END LOWER SURFACE IAW B757 SRM 51-70-10-2R-4 REPAIR 4 FIG 202.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,958 hrs · 22,377 cycles

C3 CHECK - RIGHT WING NR 10 SLAT COVE SKIN CRACKED. REPLACED RIGHT WING NR 10 SLAT COVE SKIN IAW B757 SRM 51-40-02-0G PAR 5 & 6 FIG 9 51-30-01 PAR 8.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,958 hrs · 22,377 cycles

C3 CHECK - LEFT WING NR 1 SLAT COVE SKIN CRACKED. REPLACED LEFT WING NR 1 SLAT COVE SKIN IAW B757 SRM 51-40-02-0G PAR 6 FIG 6 PAR 9 FIG 16.

Part: PANEL — DELAMINATED (VERTICAL STAB) · airframe 56,958 hrs · 22,377 cycles

C3 CHECK - DELAMINATION ON VERTICAL STABILIZER TORQUE BOX PANEL BETWEEN FSS119.467 TO FSS270.784. REMOVED RIGHT TORQUE BOX PANEL VERTICAL STABILIZER & SENT PANEL TO OUTSIDE VENDOR FOR REPAIR. INSTALLED SERVICEABLE RIGHT TORQUE BOX PANEL IAW B757 SRM 51-40-02-0G PAR 4 &7 FIG 3, 6, 7, 8 AND 12, EA 141763.

Part: SHUTOFF VALVE — INOPERATIVE (BLEED AIR SYS)

SJU FLT 1078 EN ROUTE SJU TO PHL. DURING CLIMB, WITH LEFT PACK ON MEL, THE RIGHT PACK DUCT PRESSURE WAS 10 PSI. ALMOST NO AIRFLOW, HAD TO SELECT L BLEED TO SUPPLY AIR TO THE RIGHT PACK. THE CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD SJU. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS MAINTENANCE FERRIED TO PHL. MAINTENANCE REPLACED THE RIGHT ENGINE PRESSURE REGULATING AND SHUT-OFF VALVE.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

PHL - THE FLASHLIGHT AT THE L2 DOOR WAS INOPERATIVE. MAINTENANCE INSTALLED A NEW BATTERY IN THE L2 DOOR FLASHLIGHT.

Part: CRASH AX — CRACKED (ZONE 200)

PHL - THE CRASH AXE HAS A DEFECTIVE HANDLE WITH CRACKS. MAINTENANCE REPLACED THE CRASH AXE.

Part: FILTER — DIRTY (CABIN)

CLT - FLT 1422 EN ROUTE SXM TO CLT. AN ACRID SMELL WAS NOTED IN THE COCKPIT, IT SMELLED LIKE DUCTS. TURNED OFF THE LEFT BLEED SWITCH AND THE SMELL DISSIPATED. MAINTENANCE WAS UNABLE TO DUPLICATE. RAN BOTH ENGINES, ISOLATED THEM FOR SMELL, NO SMELLS NOTED. OPEN/CLOSED THE ENGINES TO LOOK FOR LEAKS, NONE WERE NOTED. ISOLATED PACKS, NO PROBLEMS. ALSO CHECKED APU, FOUND BOTH RECIRC FILTERS VERY DIRTY. CHANGED BOTH FILTERS.

Part: SELECTOR — SHORTED (COCKPIT)

STT - THE CAPTAIN'S VOR/DME SELECTOR REPORTED BY CREW TO HAVE ELECTRICAL SHORT. PANEL HAD SMOKE AND ODOR FROM FRONT OF UNIT. CREW REPORT: CREW REMOVED MAN/AUTO SWITCH AND PROBLEM STOPPED. MAINTENANCE FOUND A LIGHT BULB AT THE BOTTOM OF THE SWITCH. REPLACED THE LEFT VOR CONTROL PANEL.

Part: BATTERY PACK — DISCHARGED (CABIN)

PHL - THE EMERGENCY LIGHTS BY DOOR R1, L1, COCKPIT AND THE RIGHT SIDE OF FIRST CLASS WERE INOPERATIVE. REMOVED AND REPLACED THE FORWARD BATTERY PACK.

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,786 hrs · 20,927 cycles

CLT - C2 - MAJOR REPAIR - CORROSION ON FUSELAGE FRAME AT BS 729 BETWEEN S16L TO S18L. REPAIRED FUSELAGE FRAME AT BS 729 BETWEEN S16L TO S18L IAW EA 101761.

Part: PANEL — CRACKED (LE SLAT) · airframe 51,786 hrs · 20,927 cycles

CLT - C1 - MAJOR REPAIR - CRACKS EMANATING FROM RIGHT WING NR 9 SLAT COVE PANEL ATTACH HOLES. REPAIRED RIGHT WING NR 9 SLAT COVE PANEL IAW EA 101742.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,786 hrs · 20,927 cycles

CLT - C2 - MAJOR REPAIR - CORROSION ON CREASE BEAM Z-ANGLE AT BS 680 & BS 740. REPLACED CREASE BEAM Z-ANGLE AT BS 680 & BS 740 IAW B757 SRM 51-40-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,786 hrs · 20,927 cycles

CLT - C2 - MAJOR REPAIR - CORROSION ON FLOORBEAM FORWARD LOWER SURFACE AT BS 377.7 BETWEEN LBL 9.25 TO LBL 35.75. REPAIRED FLOORBEAM AT BS 377.7 BETWEEN LBL 9.25 TO LBL 35.75 IAW B757 SRM 53-00-51.

Part: SLAT — DEBONDED (RT WING) · airframe 51,786 hrs · 20,927 cycles

CLT - C2 - MAJOR REPAIR - NR 6 SLAT HAS DISBOND ON THE OUTBOARD END OF WEDGE. REPLACED NR 6 SLAT IAW JOB CARD 19L51027001.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

LAS - FLASHLIGHT BATTERY DEAD AT F/A SEAT ROW L2. REPLACED FLASHLIGHT BATTERY.

Part: WIRE — BROKEN (CABIN)

LAS - SLIDE RAMP LIGHTS DOORS L3/R3 WILL NOT TEST USING NLG TEST PANEL (LIGHTS DO TEST OK FROM FLIGHT DECK TEST PANEL). REPAIRED BROKEN WIRE AT PIN D OF D40488P.

Part: BOTTLE — IMPROPER PART (R2 DOOR)

PHL - NEED TO REPLACE THE R2 DOOR ASSIST BOTTLE. REPLACED THE R2 DOOR EMERGENCY POWER ACTUATOR.

Part: RESERVOIR — LOW PRESSURE (R2 DOOR)

R2 DOOR RESERVOIR ASSY EMERGENCY POWER LOW PSI. MAINTENANCE REPLACED DOOR R2 RESERVOIR ASSY EMERGENCY POWER.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,349 hrs · 20,387 cycles

BFM - B6 - MAJOR REPAIR - CORROSION ON FLOOR SUPPORT BETWEEN BS 1660 TO BS 1680, LBL 58. REPLACED FLOOR SUPPORT BETWEEN BS 1660 TO BS 1680, LBL 58 IAW B757 SRM 51-10-02.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 49,349 hrs · 20,387 cycles

BFM - B6 - MAJOR REPAIR - CORROSION ON CREASE BEAM BETWEEN BS 760 TO BS 810, RBL 60. REPAIRED CREASE BEAM BETWEEN BS 760 TO BS 810, RBL 60 IAW US AIRWAYS EA 134095.

Part: LIGHT — INOPERATIVE (CABIN)

BOS - THE EMERGENCY ESCAPE SLIDE LIGHT WAS INOPERATIVE AT THE L4 DOOR. MAINTENANCE REPLACED THE L4 DOOR EMERGENCY ESCAPE SLIDE LIGHT ASSEMBLY. OPERATIONALLY CHECKS OK. (S)

Part: LIGHT — INOPERATIVE (CABIN)

BOS - THE EMERGENCY ESCAPE SLIDE LIGHT WAS INOPERATIVE AT THE R4 DOOR. MAINTENANCE REPLACED THE R4 DOOR EMERGENCY ESCAPE SLIDE LIGHT ASSEMBLY. OPERATIONALLY CHECKS OK. (S)

Part: DUCT — LEAKING (BLEED SYS)

LAS FLT 790 LAS-CLT - THE CREW RECEIVED A RT ENG OVERHEAT WARNING ON TAKEOFF, RESULTING IN AN IN-FLIGHT SHUTDOWN. THE FLIGHT RETURNED TO FIELD LAS AND LANDED WITHOUT FURTHER INCIDENT. THERE WAS 30 MINUTES SINGLE ENG TIME. MAINTENANCE REPLACED A LEAKING RT ENG HP 6 DUCT. LEAK AND OPERATIONALLY CHECKS OK. (S)

Part: BELLOWS — BLOWN (BLEED AIR SYS)

CUN - FLT 808 EN-ROUTE CUN TO CLT. ON CLIMBOUT, AT FL290, THE RIGHT ENGINE INDICATED AN OVERHEAT CONDITION. THE CREW REDUCED THE THRUST SETTING. HOWEVER, THE INDICATION DID NOT GO OUT. THE CREW SHUT DOWN THE RIGHT ENGINE AS REQUIRED PER PROCEDURES, AND RETURNED TO CUN. REMOVED AND REPLACED NR 2 HP BELLOWS AND SEALS (CRUSH GASKETS).

Part: ENGINE — OVERHEATED (RIGHT)

CUN FLT 808, ENROUTE CUN TO CLT. ON CLIMB-OUT, AT FL290, THE RIGHT ENGINE INDICATED AN OVERHEAT CONDITION. THE CREW REDUCED THE THRUST SETTING HOWEVER, THE INIDCATION DID NOT GO OUT. THE CREW SHUTDOWN THE RIGHT ENGINE AS REQURIED IAW PROCEDURES, AND RETURNED TO CUN. MAINTENANCE ACTION PENDING. (K)

Part: SKIN — DELAMINATED (L/E SLAT) · airframe 46,897 hrs · 19,332 cycles

BFM - MAJOR REPAIR - C1 CHECK - LEFT WING NR 4 SLAT TRAILING EDGE LOWER SURFACE HAS AREA OF DELAMINATION. REPAIRED LEFT WING NR 4 SLAT TRAILING EDGE LOWER SURFACE HAS AREA OF DELAMINATION IAW B757 SRM 51-70-10.

Part: MEGAPHONE — INOPERATIVE (CABIN)

PHL - THE AFT MEGAPHONE WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE AFT MEGAPHONE. OPERATIONALLY CHECKS OK.

Part: FAN — FAILED (ZONE 200)

TPA FLT 1961 CLT TO TPA - THE CREW RECEIVED EICAS MESSAGE "OUTBRD EX VAL OPEN". A BURNING ODOR WAS ALSO NOTED IN THE COCKPIT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT RECIRCULATION FAN. SYSTEM OPERATIONALLY CHECKS NORMAL.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,637 hrs · 18,351 cycles

MAINTENANCE FOUND THE FORWARD SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LIGHT SOCKET. NO FURTHER DIFFICULTIES.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,801 hrs · 17,619 cycles

MAINTENANCE FOUND AFT GALLEY EMERGENCY LIGHT ABOVE R4 DOOR INOPERATIVE. REPLACED BATTERY CHARGER. NO FURTHER FAULTS.