N201UU

Part: SKIN — DEBONDED (LEFT) · airframe 76,091 hrs · 25,923 cycles

LEFT ELEVATOR TRAILING EDGE HAS A DEBONDED AREA STARTING AT ELEVATOR STATION 160.5 GOING OUTBOARD TO ELEVATOR STATION 175. REPLACED THE ELEVATOR IAW AMM 27-31-01-401, AND TC 19L33027002.

Part: FLOOR SUPPORT — CORRODED (BS 1300-1320) · corrosion level 2 · airframe 76,091 hrs · 25,923 cycles

CORROSION FOUND ON THE FLOOR SUPPORT, BETWEEN BS 1300 - 1320, RBL 16. REPLACED THE FLOOR SUPPORT IAW SRM 53-00-04-1A, AND 51-40-02.

Part: RETAINER — UNSECURE (CARGO DOOR) · airframe 76,091 hrs · 25,923 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT CARGO DOOR CUT OUT AFT FRAME 2ND FROM THE TOP CORNER DOOR STOP ROTATES FREELY (NOT SECURED). REPLACED DOOR STOP SPRING RETAINER PER AMM 52-34-00-825-009.

Part: TORQUE BOX — DELAMINATED (VERTICAL STAB) · airframe 76,091 hrs · 25,923 cycles

VERTICAL STABILZER LEFT FORWARD TORQUE BOX PANEL WAS DELAMINATED 3 INCHES UP FROM BOTTOM EDGE. REPLACED THE TORQUE BOX PANEL IAW SRM 51-40-02.

Part: WEDGE — DELAMINATED (LT WING SLAT) · airframe 76,091 hrs · 25,923 cycles

LEFT WING NR 5 SLAT TRAILING EDGE WEDGE UPPER AND LOWER SURFACES WERE DELAMINATED. REPLACED THE SLAT IAW TC 19L51027001.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,091 hrs · 25,923 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. CORROSION FOUND ON LOWER SECTION OF TRANSITION PANEL. REPAIRED TRANSITION PANEL PER SRM 53-00-53-1A-1 FIGURE 102 AND 51-40-02.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 76,091 hrs · 25,923 cycles

AIRCRAFT IN BASE MAINTENANCE: L4 DOOR LOWER SILL CENTER SCUFF PLATE FORWARD SUPPORT ANGLE CORRODED AT BS 1661 AND LBL 65. REPLACED SUPPORT ANGLE PER SRM 51-40-02.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 76,091 hrs · 25,923 cycles

LEFT WING LEADING EDGE NR 2 SLAT SKIN FOUND CRACKED AT THE INBOARD TRACK COVE AREA. REPLACED THE SLAT IAW TC 19L52027002.

Part: TRANSITION PANEL — CORRODED (BS 1441-1552) · corrosion level 2 · airframe 76,091 hrs · 25,923 cycles

CORROSION FOUND ON THE TRANSITION PANEL BETWEEN BS 1441 TO 1552, RBL 6. REPAIRED THE TRANSITION PANEL IAW SRM 53-00-53-1A, FIGURE 101, AND 51-40-02.

Part: WINDOW — ARCED (COCKPIT) · airframe 76,091 hrs · 25,923 cycles

COCKPIT R1 WINDOW HAS MOISTURE INGRESS AROUND THE PERIPHERY OF THE WINDOW WITH SIGNS OF ARCING NEAR THE BUSS BAR. REPLACED THE WINDOW IAW AMM 56-11-01-004-001.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 75,642 hrs · 25,811 cycles

R2 DOOR SLIDE OUT OF GREEN BAND. REPLACED R2 DOOR SLIDE IAW CARD 19L80025002.

Part: SNUBBER — BENT (L1 DOOR) · airframe 73,867 hrs · 25,429 cycles

AIRCRAFT WAS NOT GROUNDED. L1 DOOR HARD TO OPEN FEELS LIKE SNUBBER BENDING. L1 DOOR ROTARY SNUBBER REPLACED.

Part: LIGHT — UNSECURE (CABIN) · airframe 72,898 hrs · 25,219 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE PATH LIGHTS REFLECTIVE TAPE ON FLOOR BY LEFT ROW 17 IS BOWING UP. RESECURED EMERGENCY LIGHTING STRIP TO FLOOR. OPERATIONAL CHECK GOOD.

Part: RESERVOIR — LOW PRESSURE (EVAC SLIDE) · airframe 72,081 hrs · 25,050 cycles

AIRCRAFT WAS NOT GROUNDED. L1 DOOR EMERGENCY EVACUATION SLIDE RESERVOIR PRESSURE IS LOW. REMOVED AND REPLACED SLIDE/RAFT IAW JOB CARD 19L80025002. OPERATIONAL CHECK GOOD.

Part: PUMP — UNSERVICEABLE (FUEL SYSTEM)

AFTER CENTER FUEL TANK IS EMPTY, LEFT AND RIGHT TANKS HAVE A FUEL IMBALANCE. FUEL FLOW ON BOTH ENGINES UNREADABLE. REMOVED AND INSPECTED CENTER TANK LEFT BOOST PICKUP WITH NO DEFECTS NOTED. REMOVED AND REPLACED LEFT CENTER FUEL BOOST/OVERRIDE PUMP FOR COMPANY CONVENIENCE. LEAK AND OPERATIONAL CHECK GOOD. AIRCRAFT WAS GROUNDED.

Part: SENSOR — DIRTY (ZONE 800)

AIRCRAFT WAS NOT GROUNDED. R2 DOOR EMERGENCY EVACUATION SLIDE INDICATOR LIGHT IS INOPERATIVE. REMOVED DEBRIS AND CLEANED INDICATOR SENSOR. OPERATIONAL CHECK GOOD.

Part: MECHANISM — OBSTRUCTED (L1 DOOR) · airframe 71,721 hrs · 24,970 cycles

AIRCRAFT WAS NOT GROUNDED. L1 DOOR KNUCKLE BUSTER DOES NOT DEPLOY WHEN DOOR IS ARMED. REMOVED OBSTRUCTION. OPERATIONAL CHECK GOOD.

Part: DOOR — LACK OF LUBE (L1) · airframe 71,363 hrs · 24,899 cycles

L1 DOOR VERY DIFFICULT TO OPEN FULLY. MAINTENANCE LUBED DOOR 1L IAW AMM 12-21-18.

Part: LIGHT — DETACHED (CABIN) · airframe 71,171 hrs · 24,853 cycles

FLIGHT ATTENDANT REPORTED EMERGENCY BULL NOSE LIGHT HANGING DOWN AT 33C. MAINTENANCE SECURED THE LIGHT AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: FITTING — CORRODED (FUSELAGE) · airframe 70,981 hrs · 24,811 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CARGO DOOR LOWER OUTBOARD CHORD SILL FITTING (UNDER DOOR) AT STRINGER 26R. REPAIRED OUTBOARD CHORD PER EA 266288.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 70,782 hrs · 24,738 cycles

AFT LEFT BULL NOSE EMERGENCY EXIT LIGHTS INOPERATIVE ABOVE L4 AND L4 SLIDE. REPLACED THE BATTERY PACK IAW AMM 33-51-07. ACCOMPLILSHED SATISFACTORY OPERATIONAL CHECK.

Part: FLASHER — TOO LARGE (EMERGENCY EXIT) · airframe 70,981 hrs · 24,811 cycles

R3 EMERGENCY EXIT DOOR SMALL SPRING LOADED DOOR OVERLAPPING THE EXTERNAL HANDLE. THE DOOR CAN'T BE OPENED FROM THE OUTSIDE. TRIMMED SPRING LOADED DOOR FLAP IAW SRM 52-20-02 AND AMM 52-21-01.

Part: CABLE — MISROUTED (L1 DOOR SLIDE) · airframe 70,981 hrs · 24,811 cycles

FOUND L1 PASSENGER DOOR ESCAPE SLIDE RELEASE STRAP LATCH CABLE ROUTED IMPROPERLY. REMOVED SLIDE ASSEMBLY PER TASK CARD 19C83125001 AND CORRECTLY ROUTED SLIDE RELEASE STRAP CABLE DURING THE SLIDE REINSTALLATION PROCESS PER TASK CARD 19C83125004.

Part: SLIDER — OBSTRUCTED (R2 DOOR) · airframe 70,044 hrs · 24,545 cycles

AIRCRAFT WAS NOT GROUNDED: R2 ARMING LIGHT INOPERATIVE. MAINTENANCE REMOVED DEBRIS AND CLEANED SLIDERS. A SATISFACTORY OPS CHECK WAS ACCOMPLISHED IAW AMM 52-71-00.

Part: SIGN — BROKEN (CABIN) · airframe 67,610 hrs · 23,932 cycles

AIRCRAFT WAS NOT GNDED. EMER EXIT IDENTIFIER SIGN BROKEN OFF WALL BY L4 DOOR. REPLACED EMER EXIT SIGN AT THE L4 DOOR. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-10.

Part: SKIN — WORN (LT PYLON) · airframe 67,499 hrs · 23,892 cycles

RON CHECK, COMMON NOZZLE FAIRING SEAL AFT END HAS HARDWARE WHICH HAS WORN INTO UNDERSIDE OF PYLON. REPAIRED LT AFT FAIRING LOWER PAN IAW ESO 90928.

Part: INDICATOR — OUT OF POSITION (EVAC SLIDE) · airframe 66,912 hrs · 23,697 cycles

DOOR 4RH SLIDE PACK FELL FROM DOOR, UPON OPENING DOOR FROM OUTSIDE BY CATERING. FOUND GIRT BAR STILL ARMED & THE SLIDE DISARMED INDICTOR FLAP OUT OF POSITION. REPOSITIONED IT AS REQUIRED & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: ACTUATOR — DEFECTIVE (FUEL SYSTEM) · airframe 66,887 hrs · 23,692 cycles

FUEL QTY MAIN TANKS EVEN WHEN CTR TANK 1.5 HRS LATER, LEFT TANK 2000 LB LESS THAN RIGHT. ENG FF EQUAL, CROSS FEED CLOSED, APU OFF. REPLACED LT DEFUEL ACTUATOR IAW AMM 28-26-02.

Part: LENS — MISSING (CABIN) · airframe 66,442 hrs · 23,572 cycles

L4 & R4 EMER EXIT IDENTIFIER LENS MISSING. INSTALLED L4 & R4 LENS COVERS TO EMER EXIT IDENTIFIERS IAW AMM 33-51-10-402-047.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 65,862 hrs · 23,425 cycles

C1 CHECK, CORROSION ON AFT CARGO DOOR FWD LOWER CORNER INNER FRAME WEB, BS 1383 & BELOW STOP BEAM 6. REPAIRED AFT CARGO DOOR FWD LOWER CORNER INNER FRAME WEB IAW EA 250877.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

L2 EXIT SIGN & R2 EXIT MARKER INOPERATIVE, DURING EMER LIGHT TEST. REPLACED L2 DOOR EMER LIGHT POWER SUPPLY M733.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,862 hrs · 23,425 cycles

C1 CHECK CORROSION ON FWD CARGO COMPARTMENT SIDE PANEL BETWEEN STATION 560 & 640 AT STRINGER 26R. REPLACED FWD CARGO COMPARTMENT SIDE PANEL IAW SRM 53-00-53-1A-1 DETAIL IV & 51-40-02.

Part: GATE — CORRODED (R1 DOOR) · airframe 65,862 hrs · 23,425 cycles

C1 CHECK, CORROSION ON R1 DOOR GATE ASSEMBLY. REPLACED R1 DOOR GATE ASSEMBLY IAW SRM 52-10-02-10 DETAIL V, VII & 52-11-38.

Part: ATTACH FITTING — CORRODED (CARGO BAY) · corrosion level 2 · airframe 65,862 hrs · 23,425 cycles

C1 CHECK, FWD CARGO COMPARTMENT TIE DOWN FITTING AT LBL 22.50 & STATION 680 IS CORRODED. R & R FITTING IAW SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,862 hrs · 23,425 cycles

C1 CHECK, CORROSION ON FWD CARGO COMPARTMENT FLOOR SUPPORT SIDE PANEL TIE DOWN FITTING BETWEEN STATION 640 & 840 AT RBL 22.50. REPLACED TIE DOWN FITTING IAW SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,862 hrs · 23,425 cycles

C1 CHECK, CORROSION ON FWD CARGO FITTING AT STATION 700 & RBL 22.50. REPLACED FITTING IAW SRM 51-40-02.

Part: PROXIMITY SWITCH — INOPERATIVE (GIRT BAR) · airframe 65,862 hrs · 23,425 cycles

C1 CHECK, L2 DOOR AFT GIRT BAR PROXIMITY SWITCH INOPERATIVE. REPLACED & ADJUSTED L2 DOOR AFT PROXIMITY SWITCH IAW AMM 25-66-11-002-001, 25-66-11-402-007 & 25-66-11-822-011.

Part: DOOR — LACK OF LUBE (L1) · airframe 65,412 hrs · 23,299 cycles

ENTRANCE DOOR L1 IS DIFFICULT TO OPEN. APPLIED LUBE TO L1 DOOR AS REQUIRED. OPERATIONS CHECKED GOOD.

Part: LATCH — OUT OF ADJUST (R4 DOOR) · airframe 64,726 hrs · 23,083 cycles

DURING FLIGHT THE 4R DOOR HANDLE MOVED APPROXIMATELY 3 TO 4 INCHES OUT OF THE CLOSED POSITION. ADJUSTED THE DOOR LATCH FITTINGS, THE DOOR SLIDE WAS NOT DISTURBED.

Part: OVEN — DEFECTIVE (GALLEY) · airframe 63,243 hrs · 22,737 cycles

AFT OVEN DEFECTIVE, FLIGHT ATTENDANT REPORTED ELEC SMELL. FLIGHT ATTENDANT PULLED CB ON NR 2 AFT OVEN, SMELL DISSIPATED. R & R NR 2 OVEN.

Part: SUPPORT ANGLE — CRACKED (CARGO DOOR) · airframe 62,850 hrs · 22,642 cycles

WEEKLY VISIT FWD CARGO DOOR AFT SIDE EDGE SUPPORT ANGLE IS CRACKED AT BS 620, STRINGER 23R. REPLACED FWD CARGO DOOR AFT SIDE EDGE SUPPORT ANGLE AT BS 620, STRINGER 23R IAW SRM 51-40-02.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 62,557 hrs · 22,556 cycles

PHL FLASHLIGHT AT FLIGHT ATTENDANT STATION, 1A, NOT CHARGING, NO FLASHING LIGHT. REPLACED BATTERY IN FLIGHT ATTENDANTS FLASHLIGHT, OPERATIONS CHECKED NORMAL.

Part: FUSE — BLOWN (CABIN) · airframe 61,972 hrs · 22,370 cycles

DFW FOUND FUSE ON M730 INOPERATIVE. FWD EMERGENCY POWER SUPPLY LIGHTING. REPLACED FUSE ON EMERGENCY POWER SUPPLY M730.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 61,972 hrs · 22,370 cycles

DFW EMERGENCY LIGHTS IN FIRST CLASS AREA & EXIT SIGNS ON L1 DOOR INOPERATIVE. FOUND CONNECTOR TO THE POWER SUPPLY M731 NOT INSTALLED & BATTERY DEAD. INSTALLED NEW BATTERY & INSTALLED CONNECTOR. OPERATIONS CHECKED GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,762 hrs · 22,289 cycles

C4 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR BEAM AT BS 1320, LBL 19. REPAIRED FLOOR BEAM AT BS 1320, LBL 19 IAW B757 SRM 53-00-51-2R-1, PROCEDURE 1, REPAIR 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,762 hrs · 22,289 cycles

C4 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR BEAM AT BS 1640, RBL 58. REPLACED FLOOR BEAM AT BS 1640, RBL 58 IAW B757 SRM 53-00-51-2R, REPAIR 8.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,762 hrs · 22,289 cycles

C4 CHECK, CORROSION ON CHANNEL BETWEEN BS 1258 TO 1280, S17L, LBL 65. REPAIRED CHANNEL IAW EA 105316.

Part: FLOORBEAM — CRACKED (BS 365) · airframe 61,762 hrs · 22,289 cycles

C4 CHECK - 4 CRACKS ON FLOORBEAM STABILIZER STRAP AT BS 365, LBL 24. REPAIRED FLOORBEAM STABILIZER STRAP IAW SRM 53-10-51-2R-1, DETAIL VI.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,762 hrs · 22,289 cycles

C4 CHECK, CORROSION FOUND ON FLOOR SUPPORT ANGLE AT BS 1716, RBL 12. REPAIRED FLOOR SUPPORT ANGLE IAW SRM 51-40-02 & 51-20-00.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 61,762 hrs · 22,289 cycles

C4 CHECK, CORROSION FOUND ON FLOOR SUPPORT AT BS 1651, LBL 56. REPAIRED FLOOR SUPPORT IAW SRM 51-10-02.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,762 hrs · 22,289 cycles

DURING C4 CHECK, CORROSION WAS FOUND ON GALLEY FLOORBEAM AT BS 389 BETWEEN RBL 26 - 42. REPAIRED FLOORBEAM IAW SRM 51-20-02 & DWG 141N5162.

Part: STIFFENER — CORRODED (ZONE 100) · airframe 61,762 hrs · 22,289 cycles

C4 CHECK, CORROSION FOUND ON R4 DOOR THRESHOLD STIFFENER AT BS 1661, S17R. REPAIRED STIFFENER IAW SRM 51-40-02.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,762 hrs · 22,289 cycles

DURING C4 CHECK, CORROSION WAS FOUND ON ANGLE AT L3 DOORWAY AT BS 1320, S17L. REPLACED ANGLE IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,762 hrs · 22,289 cycles

C4 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOOR BEAM UPPER T CAP AT BS 345, RBL 61. REPAIRED FLOOR BEAM UPPER T CAP AT BS 345, RBL 61 IAW B757 SRM 53-00-51-2R, PROCEDURE 8, REPAIR 8.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,762 hrs · 22,289 cycles

DURING C4 CHECK, CORROSION WAS FOUND ON FLOORBEAM BS 398 BETWEEN RBL 44-47. REPAIRED FLOORBEAM IAW SRM 51-20-02 & 51-40-05.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,762 hrs · 22,289 cycles

C4 CHECK, CORROSION FOUND ON FLOOR SUPPORT BETWEEN BS 342 TO 365, BL 0. REPLACED FLOOR SUPPORT IAW SRM 51-10-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,762 hrs · 22,289 cycles

C4 CHECK LEVEL 2 INTERGRANULAR CORROSION ON FLOOR BEAM UPPER CHORD AT BS 324 BETWEEN RBL 55 TO RBL 63. REPAIRED FLOOR BEAM UPPER CHORD AT BS 324 BETWEEN RBL 55 TO RBL 63 IAW B757 SRM 53-10-08-2R-1.

Part: ANGLE — CORRODED (ZONE 100) · airframe 61,762 hrs · 22,289 cycles

C4 CHECK, AREA OF HEAVY CORROSION ON ANGLE AT BS 1329, S17R. REPLACED ANGLE IAW SRM 51-40-02.

Part: WEB — CORRODED (ZONE 100) · airframe 61,762 hrs · 22,289 cycles

DURING C4 CHECK, CORROSION FOUND ON FLOOR WEB AT BS 1319, LBL 64. INSTALLED NEW FABRICATED FLOOR WEB IAW DWG 146N8322.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,762 hrs · 22,289 cycles

DURING C4 CHECK, CORROSION FOUND AT L3 EMERGENCY EXIT DOORWAY INTERNAL LOWER SILL AT BS 1320, S17L. REPLACED INTERNAL LOWER SILL IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,762 hrs · 22,289 cycles

DURING C4 CHECK, CORROSION FOUND AT R3 EMERGENCY EXIT DOORWAY INTERNAL FLOORBEAM AT BS 1340, S17R. REPAIRED IAW SRM 51-40-02, DWG 146N8322 & 146N6303,

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,762 hrs · 22,289 cycles

DURING C4 CHECK, CORROSION FOUND AT L3 EMERGENCY EXIT DOORWAY INTERNAL LOWER SILL WEB AT BS 1325, S17L. REPLACED INTERNAL LOWER SILL WEB IAW SRM 51-40-02.

Part: FAILSAFE — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,762 hrs · 22,289 cycles

DURING C4 CHECK, CORROSION WAS FOUND ON AFT CARGO FAIL SAFE AT BS 1280, S17L. REPLACED FAIL SAFE IAW EA 105238.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 61,762 hrs · 22,289 cycles

C4 CHECK, DELAMINATION ON PREVIOUS REPAIR ON NR 8 SLAT LOWER SURFACE APPROX 4.75 INCHES FROM INBD END & 5.25 INCHES FROM T/E. REPLACED NR 8 SLAT IAW 19L52027002.

Part: LIGHT — UNSECURE (CABIN) · airframe 61,764 hrs · 22,291 cycles

TRACK MOUNTED EXIT LIGHTS UNSECURE, AT ROW 11. SECURED LIGHT, CHECKED OK.

Part: SKIN — DEBONDED (NR 7 SLAT) · airframe 61,355 hrs · 22,162 cycles

DEBONDING ON RT WING NR 7 SLAT LOWER SURFACE APPROX 6" FROM TOP & 13" FROM THE INBD SIDE, NOTED DURING UT INSPECTION. REPLACED RIGHT WING NR 7 SLAT IAW JOB CARD 19L52027002.

Part: LIGHT — LOOSE (ZONE 200) · airframe 61,124 hrs · 22,086 cycles

EMERGENCY LIGHTING STRIP LOOSE BETWEEN ROWS 10 & 11 ACFT RT. SECURED TRACK LIGHTING.

Part: LIGHT — NOT SEATED (CABIN) · airframe 60,844 hrs · 22,008 cycles

ROW 11, ACFT RIGHT EMERGENCY LIGHTING STRIP ON FLOOR IS BOWED UP. RESEATED EMERGENCY FLOOR STRIP ON ROW 11 AS REQUIRED. CHECKS OK.

Part: LIGHT — UNSECURE (CABIN) · airframe 60,606 hrs · 21,938 cycles

EMERGENCY FLOOR LIGHT STRIP COMING UP ROW 10 ACFT RT. SECURED AS REQUIRED , OK FOR SERVICE.

Part: LIGHT — UNSECURE (CABIN) · airframe 60,572 hrs · 21,930 cycles

EMERGENCY LIGHTS EMERGENCY PATHWAY LIGHTING IN THE 11D AREA IS COMING UP. NEEDS TO BE REATTACHED, SECURED. RESECURED EMERGENCY PATHWAY LIGHT ROW 11. OPS CHECK GOOD.

Part: LIGHT — UNSECURE (CABIN) · airframe 60,572 hrs · 21,930 cycles

EMERGENCY LIGHTS, EMERGENCY LIGHT ACFT RT BETWEEN ROW 25 AND 26 IS HANGING. NOT MOUNTED PROPERLY. RESECURED EMERGENCY LIGHT ASSY AT ROW 25. OPS CHECK GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 60,558 hrs · 21,928 cycles

FLOOR EMERGENCY LIGHT ROW 11 LOOSE AND BUCKLED UP. SECURED EMERGENCY LIGHT STRIP. OK FOR CONTINUED SERVICE.

Part: TRACK — UNSECURE (CABIN) · airframe 60,358 hrs · 21,867 cycles

PHL - WITH ATTENDANT SWITCH ON EMERGENCY AISLE 1 QT AT SEAT 11+ 12 TRACK COMING UP. RE-SECURED TRACK AT ROW 11&12, OPS CHECK GOOD.

Part: LENS — MISSING (EXIT SIGN) · airframe 60,154 hrs · 21,821 cycles

BRU - FOUND LENS COVER MISSING ON DOOR 1R EMERGENCY EXIT SIGN. MAINTENANCE INSTALLED NEW EXIT SIGN AT DOOR 1R.

Part: LIGHT — UNSECURE (CABIN) · airframe 59,612 hrs · 21,644 cycles

PHL - FLOOR LEVEL LIGHT AT 11C PULLED FROM FLOOR. RE-SECURED FLUORESCENT FLOOR STRIP.

Part: COVER — MISSING (EXIT SIGN) · airframe 59,307 hrs · 21,538 cycles

PHL - L4 DOOR LOWER EMERGENCY LIGHT COVER MISSING AND BRACKET MISSING A PIECE. REPLACED EMERGENCY EXIT SIGN ASSY.

Part: BUSHING — MIGRATED (GIRT BAR) · airframe 59,114 hrs · 21,471 cycles

CLT - 1L DOOR MOUNTED ESCAPE SYSTEM GIRT BAR ENGAGEMENT LIGHT OFF WITH EVACUATION SLIDE ARMING LEVER IN ARMED, ENGAGED POSITION AT ENTRY DOOR. MAINTENANCE SECURED MIGRATING BUSHING IN GIRT BAR ARMING LINK ASSEMBLY.

Part: WIRE — DAMAGED (ELECTRICAL SYS)

CLT - LEFT FWD BOOST PUMP (FUEL) CB POPS. REPAIRED DAMAGED 115VAC GND SERVICE BUS SYSTEM WIRING AT TERMINAL BLOCK TB5015.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 58,455 hrs · 21,248 cycles

PHX - RIGHT OVERDOOR EXIT SIGN AT DOOR 4R & LEFT EXIT INDICATION SIGN AT DOOR 4L INOP. LEFT EMERGENCY POWER SUPPLY ABOVE AFT GALLEY CEILING NOT PRODUCING POWER AT PINS 10 & 12. REMOVED & REPLACED POWER SUPPLY M737. OPS CHECK GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 58,455 hrs · 21,248 cycles

PHL - EMERGENCY LIGHTS 02 (ROW 11 AFT RIGHT) LOOSE. SECURED AS REQUIRED.

Part: STRIP — UNSECURE (CABIN) · airframe 58,013 hrs · 21,118 cycles

CLT - EMERGENCY LIGHTING STRIP IN FLOOR BUCKLED. RE-SECURED LIGHTING STRIP.

Part: STRIP — LOOSE (CABIN) · airframe 57,539 hrs · 20,981 cycles

FLOOR EMERGENCY STRIP LIFTED UP BY ROW 14. MAINTENANCE SECURED FLOOR EMERGENCY STRIP AT ROW 14 RT SIDE.

Part: LIGHT — LOOSE (CABIN) · airframe 56,591 hrs · 20,674 cycles

MCO - EMERGENCY LIGHTING ON FLOOR ROW 12 LOOSE YOU CAN GET YOUR FOOT UNDER IT. RE-SECURED STG PHOTOLUMINESCENT EMERGENCY ESCAPE PATH TRACK LIGHTING STRIP. OK FOR SERVICE.

Part: STRAP — CORRODED (FUSELAGE) · airframe 56,397 hrs · 20,611 cycles

C3 CHECK - CORROSION ON STRAP ON APU INLET DOOR SURROUND AT BS 1825, S6R. REPLACED STRAP ON APU INLET DOOR SURROUND AT BS 1825, S6R IAW EA 103701.

Part: SKIN — DEBONDED (LE SLAT) · airframe 56,397 hrs · 20,611 cycles

C3 CHECK - AREA OF DISBOND ON NR 7 SLAT TRAILING EDGE ON UPPER SURFACE APPROX 2.5 INCHES FROM INBOARD END & 1 INCH FROM TRAILING EDGE. REPAIRED NR 7 SLAT TRAILING EDGE UPPER SURFACE IAW B757 SRM 51-70-10.

Part: ANGLE — CRACKED (TE FLAP) · airframe 56,397 hrs · 20,611 cycles

C3 CHECK - CRACK ON C-CLIP ANGLE OF LEFT OUTBOARD MAIN FLAP AT OUTBOARD EDGE APPROX 12 INCHES UP FROM LOWER SIDE. REPLACED C-CLIP ANGLE ON LEFT OUTBOARD MAIN FLAP IAW B757 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,397 hrs · 20,611 cycles

C3 CHECK - CORROSION ON FLOORBEAM T-CAP AT BS700, Y2218. REPAIRED FLOORBEAM T-CAP AT BS 700, Y2218 IAW B757 SRM 53-00-51-3R.

Part: TORQUE BOX — DELAMINATED (ZONE 300) · airframe 56,397 hrs · 20,611 cycles

C3 CHECK - DELAMINATION ON VERTICAL STABILIZER LOWER RIGHT TORQUE BOX PANEL AT BS 1766 BETWEEN FSS 165 & FSS 195. REPLACED VERTICAL STABILIZER LOWER RIGHT TORQUE BOX PANEL AT BS 1766 BETWEEN FSS165 & FSS195 IAW BOEING DRAWING # 175N2001.

Part: LIGHT — DAMAGED (CABIN) · airframe 55,583 hrs · 20,351 cycles

PHL - EMERGENCY FLOOR LIGHTS BETWEEN ROW 11 & 12 DAMAGED. RESECURED EMERGENCY LIGHT STRIP TO FLOOR. OPS CHECKS OK.

Part: LIGHT — UNSECURE (CABIN) · airframe 55,084 hrs · 20,229 cycles

CLT - EMERGENCY EXIT FLOOR LIGHTING STRIP LOOSE AT ROW 11 & 12. FOUND FLOOR LIGHTING STRIP SECURE. CHECKS OK ROW 11 & 12.

Part: LIGHT — UNSECURE (CABIN) · airframe 54,756 hrs · 20,130 cycles

CLT - EMERGENCY FLOOR LIGHTING BUCKLING AT ROW 11 AIRCRAFT RIGHT. MAINTENANCE REMOVED DEBRIS AND RE-SECURED FLOOR TRACK STRIP. OK FOR SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 54,575 hrs · 20,077 cycles

CLT - EMERGENCY EXIT LIGHT DOOR 4R BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT R4 DOOR.

Part: SPRING — WEAK (LAVATORY DOOR)

DUB - ENTRY DOOR RETURN SPRINGS WEAK (DOOR OPERATION NORMAL). THIS DISCREPANCY HAS SUBSEQUENTLY BEEN FOUND TO BE DUE TO A PROBLEM WITH THE FORWARD LAVATORY DOOR, NOT AN AIRCRAFT ENTRY DOOR. THE MAINTENANCE ACTION WAS: "INSTALLED SPRING IN DOOR FORWARD LAV. OP CHECK GOOD".

Part: LIGHT — BUCKLED (CABIN)

PHL - ROW 12 AIRCRAFT RIGHT FLOOR LIGHTING IS BUCKLED UP. RE-SECURED, OK FOR SERVICE.

Part: SKIN PANEL — DEBONDED (MIDFLAP) · airframe 51,719 hrs · 19,261 cycles

CLT - C2 - MAJOR REPAIR - DISBOND ON RIGHT INBOARD MID FLAP TRAILING EDGE COVE PANEL LOWER SKIN 46 INCHES FROM INBOARD END & 10 INCHES FROM AFT EDGE. REPAIRED RIGHT INBOARD MID FLAP TRAILING EDGE COVE PANEL LOWER SKIN IAW EA 102112 & B757 SRM 51-70-07.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,719 hrs · 19,261 cycles

CLT - C2 - MAJOR REPAIR - CORROSION ON CREASE BEAM BETWEEN BS 1250 TO BS 1270, S17R, RBL 60. REPAIRED CREASE BEAM BETWEEN BS 1250 TO BS 1270, S17R, RBL 60 IAW EA 102116.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

PHL - L1 DOOR FLASHLIGHT WAS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY.

Part: HEAT EXCHANGER — RUPTURED (RT SECONDARY)

THE ACFT HAD A LOSS OF PRESSURIZATION AT FL390. ACFT DIVERTED. ON INSP, THE RT SECONDARY HEAT EXCHANGER WAS FOUND TO BE RUPTURED, CAUSING A LOSS OF PRESURIZATION.

Part: HEAT EXCHANGER — RUPTURED (ACM)

DUB FLT 798 EN ROUTE PHL TO AMS. THE CABIN PRESSURE ALTITUDE BEGAN TO CLIMB. THE CREW WAS ABLE TO STOP THE PRESSURE CLIMB AT 12,000 FEET. THE FLIGHT DIVERTED TO DUB AND LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED THE RT PACK HEAT EXCHANGER ASSEMBLY. THE SECONDARY HEAT EXCHANGER WAS FOUND RUPTURED. THE HEAT EXCHANGER WAS CORED AND OVERHAULED.

Part: SOLENOID — FAULTY (BLEED VALVE)

PHL FLT 1746 ENROUTE MCO TO PHL. ELECTRIC SMOKE ODOR IN ACFT AFTER COMPRESSOR STALLS. THE LEFT ENGINE DUCT PRESSURE, LEFT SIDE, READS LOW. THE ENGINE STALLED TWICE CLIMBING OUT OF FL370 FOR FL410. FOUND HP BLEED VALVE SOLENOID 2 FAULTY. REPLACED SOLENOID.

Part: LIGHT — INOPERATIVE (L4 DOOR)

CLT - THE L4 DOOR GIRT BAR ENGAGEMENT LIGHT WAS EXTINGUISHED WITH THE EVACUATION SLIDE ARMING LEVER IN THE ARMED POSITION. MAINTENANCE REPLACED THE BULBS IN THE L4 DOOR GIRT BAR ENGAGEMENT LIGHT.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT)

BOS - THE CHARGE INDICATOR OF THE FLASHLIGHT AT DOOR R3 WAS NOT FLASHING. MAINTENANCE REPLACED THE BATTERY PACK IN THE FLASHLIGHT AT DOOR R3.

Part: LIGHT — INOPERATIVE (EVAC SLIDE)

CLT - THE R4 DOOR SLIDE GIRT BAR ENGAGEMENT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PLACED THE SYSTEM ON MEL. MAINTENANCE REPLACED THE R4 DOOR SLIDE INDICATION LIGHT ASSEMBLY AND CLEARED THE MEL.

Part: LIGHT — INOPERATIVE (GIRT BAR)

CLT - THE R4 DOOR SLIDE GIRT BAR ENGAGEMENT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PLACED THE SYSTEM ON MEL. FURTHER ACTION PENDING.

Part: FUEL FILTER — CLOGGED (ZONE 400)

BFM - FLT 9244 BFM TO PHL - RECEIVED "RT FUEL FILTER" EICAS MESSAGE ON TAKEOFF. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED RIGHT ENGINE FUEL FILTER. OPERATIONALLY AND LEAK CHECKS OK.

Part: SLIDE — FAILED (ZONE 200) · airframe 42,958 hrs · 17,204 cycles

CLT - EMERGENCY DOOR SLIDE ON EXIT DOOR 4L HAS LOW BOTTLE PRESSURE. MAINTENANCE REMOVED AND REPLACED SLIDE ASSY.

Part: SWITCH — INOPERATIVE (CABIN) · airframe 42,734 hrs · 17,117 cycles

MCN - EES - C4 CHECK - EMERGENCY SLIDE LIGHTS AT L1, R1, L2 & R2 DOORS ARE INOPERATIVE WHEN NLG EMER LT TEST SWITCH IS OPERATED. REPLACED AND FUNCTIONAL CHECKED L1 DOOR TEST SWITCH S10292 IAW B757 AMM 33-51-00.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL / CHANNEL, BS 350 - BS 365, RBL 24, WL 208. REPLACED INTERCOSTAL / CHANNEL, BS 350 - BS 365, RBL 24, WL 208 IAW B757 SRM 51-40-02.

Part: SPOILER — CRACKED (LT WING) · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEFT WING NR 4 SPOILER CRACKED, WS 460 - WS 472. REPAIRED LEFT WING NR 4 SPOILER, WS 460 - WS 472 IAW B757 SRM 51-70-04.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON AFT CABIN FLOOR PRESSURE WEB, BS 1681 - BS 1720, LBL 57 - RBL 57, WL 208. REPAIRED AFT CABIN FLOOR PRESSURE WEB, BS 1681 - BS 1720, LBL 57 - RBL 57, WL 208 IAW B757 SRM 53-60-51.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - CRACKED INTERCOSTAL WEB, BS 395 - BS 418, RBL 45, WL 208. REPLACED INTERCOSTAL WEB, BS 395 - BS 418, RBL 45, WL 208 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL / CHANNEL, BS 345 - BS 365, RBL 45, WL 208. REPLACED INTERCOSTAL / CHANNEL, BS 345 - BS 365, RBL 45, WL 208 IAW B757 SRM 51-40-02.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON R4 DOOR CUTOUT STRUCTURE ATTACH ANGLE, BS 1676, RBL 53, WL 208. REPLACED R4 DOOR CUTOUT STRUCTURE ATTACH ANGLE, BS 1676, RBL 53, WL 208 IAW B757 SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON L4 DOOR THRESHOLD SUPPORT CHANNEL CLIP, BS 1671, LBL 58, WL 208. REPLACED L4 DOOR THRESHOLD SUPPORT CHANNEL CLIP, BS 1671, LBL 58, WL 208 IAW B757 SRM 51-40-02.

Part: SKIN — DENTED (NR 5 SLAT) · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C-4 CHECK - DENTS FOUND ON UPPER AND OUTBOARD END SKIN OF NR 5 SLAT TRAILING EDGE WEDGE AT NR 5 SLAT STA 267.10. REPAIRED DENTS ON NR 5 SLAT TRAILING EDGE WEDGE AT NR 5 SLAT STA 267.10 IAW B757-200 SRM 51-70-10, REPAIR Z, FIG 203.

Part: SKIN — DENTED (NR 8 SLAT) · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C-4 CHECK - DENT ON UPPER OUTBOARD SKIN OF NR 8 SLAT TRAILING EDGE AT NR 8 SLAT STA 569. REPAIRED NR 8 SLAT IAW B757-200 SRM 51-70-10 REPAIR 2 FIG 203.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON INTERCOSTAL, BS 1600 - BS 1620, S29L. REPLACED INTERCOSTAL, BS 1600 - BS 1620, S29L IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (CARGO DOOR) · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON AFT CARGO DOOR LOWER TEE CHORD INTERCOSTAL, BS 1400, S24R - S25R. REPLACED AFT CARGO DOOR LOWER TEE CHORD INTERCOSTAL, BS 1400, S24R - S25R IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (CARGO DOOR) · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON AFT CARGO DOOR LOWER TEE CHORD INTERCOSTAL, BS 1430, S24R - S25R. REPLACED AFT CARGO DOOR LOWER TEE CHORD INTERCOSTAL, BS 1430, S24R - S25R IAW B757 SRM 51-40-02.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON L4 DOOR CUTOUT STRUCTURE ATTACH ANGLE CLIP, BS 1676, LBL 54, WL 208. REPLACED L4 DOOR CUTOUT STRUCTURE ATTACH ANGLE CLIP, BS 1676, LBL 54, WL 208 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (CARGO DOOR) · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON AFT CARGO DOOR LOWER TEE CHORD INTERCOSTAL, BS 1380, S24R - S25R. REPLACED AFT CARGO DOOR LOWER TEE CHORD INTERCOSTAL, BS 1380, S24R - S25R IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL, BS 324 - BS 365, RBL 58, WL 208. REPLACED AFT INTERCOSTAL, BS 324 - BS 365, RBL 58, WL 208 IAW B757 SRM 51-40-02.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON R1 DOOR CUTOUT INNER CREASE BEAM ANGLE, BS 310 - BS 377, RBL 58. REPLACED R1 DOOR CUTOUT INNER CREASE BEAM ANGLE, BS 310 - BS 377, RBL 58 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (BS 1500-1520) · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - NR 6056657, CORROSION ON INTERCOSTAL, BS 1500 - BS 1520, S29R. REPLACED INTERCOSTAL, BS 1500 - BS 1520, S29R IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON INTERCOSTAL, BS 1500 - BS 1520, S30L. REPLACED INTERCOSTAL, BS 1500 - BS 1520, S30L IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (CARGO DOOR) · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON AFT CARGO DOOR INTERCOSTAL WEB, BS 1460, S24R - S25R. REPLACED AFT CARGO DOOR INTERCOSTAL WEB, BS 1460, S24R - S25R IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL / SUPPORT, BS 345 - BS 365, RBL 58, WL 208. REPLACED INTERCOSTAL / SUPPORT, BS 345 - BS 365, RBL 58, WL 208 IAW B757 SRM 51-40-02.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON AFT CABIN FLOOR SUPPORT ATTACH PLATE / GUSSET, BS 1681, BL 0, WL 208. REPLACED AFT CABIN FLOOR SUPPORT ATTACH PLATE / GUSSET, BS 1681, BL 0, WL 208 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (CARGO DOOR) · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON AFT CARGO DOOR INTERCOSTAL WEB, BS 1440, S25R. REPLACED AFT CARGO DOOR INTERCOSTAL WEB, BS 1440, S25R IAW B757 SRM 51-40-02.

Part: TEE FITTING — CORRODED (CARGO DOOR) · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON AFT CARGO DOOR INTERCOSTAL WEB TEE FITTING, BS 1390, S24R - S25R. REPLACED AFT CARGO DOOR INTERCOSTAL WEB TEE FITTING, BS 1390, S24R - S25R IAW B757 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON FLOORBEAM SUPPORT, BS 310 - BS 324, LBL 20, WL 208. REPLACED FLOORBEAM SUPPORT BS 310 - BS 324, LBL 20, WL 208 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL / SUPPORT, BS 324 - BS 345, LBL 36, WL 208. REPLACED INTERCOSTAL / SUPPORT, BS 324 - BS 345, LBL 36, WL 208 IAW B757 SRM 51-40-02.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL SUPPORT, BS 324 - BS 345, LBL 20, WL 208. REPLACED INTERCOSTAL SUPPORT, BS 324 - BS 345, LBL 20, WL 208 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL, BS 365 - BS 377, LBL 63, WL 208. REPLACED INTERCOSTAL, BS 365 - BS 377, LBL 63, WL 208 IAW B757 SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - CRACKED INTERCOSTAL ATTACH ANGLE, BS 1620 - BS 1640, BL 0, WL 208. REPLACED INTERCOSTAL ATTACH ANGLE, BS 1620 - BS 1640, BL 0, WL 208 IAW B757 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION FLOORBEAM, BS 402, RBL 24, WL 208. REPLACED FLOORBEAM, BS 402, RBL 24, WL 208 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL / FITTING, BS 365 - BS 377, RBL 58. REPLACED INTERCOSTAL / FITTING, BS 365 - BS 377, RBL 58 IAW B757 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION FLOORBEAM, BS 377, LBL 58 - RBL 58. REPLACED FLOORBEAM, BS 377, LBL 58 - RBL 58 IAW USAIRWAYS TYPICAL REPAIR 53-15-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON MAIN CABIN FLOOR SUPPORT CHANNEL BS 1640 - BS 1661, BL-0, WL 208. REPLACED MAIN CABIN FLOOR SUPPORT CHANNEL BS 1640 - BS 1661, BL-0, WL 208 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL, BS 345 - BS 365, LBL 63, WL 208. REPLACED INTERCOSTAL, BS 345 - BS 367, LBL 63, WL 208 IAW B757 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON FLOORBEAM, BS 1640, LBL 58 - RBL 58, WL 208. REPAIRED FLOORBEAM, BS 1640, LBL 58 - RBL 58, WL 208 IAW USAIRWAYS TYPICAL REPAIR 53-15-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION FLOORBEAM TOP PLATE / FILLER, BS 297 - BS 310, BL 0. REPLACED FLOORBEAM TOP PLATE / FILLER, BS 297 - BS 310, BL 0 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION INTERCOSTAL / SUPPORT, BS 324 - BS 345, LBL 32. REPLACED INTERCOSTAL / SUPPORT, BS 324 - BS 345, LBL 32 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL CHANNEL, BS 310 - BS 324, RBL 39, WL 208. REPLACED INTERCOSTAL CHANNEL, BS 310 - BS 324, RBL 39, WL 208 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION INTERCOSTAL / SUPPORT, BS 324 - BS 345, RBL 40. REPLACED INTERCOSTAL / SUPPORT, BS 324 - BS 345, RBL 40 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL, BS 324 - BS 350, RBL 24. REPLACED INTERCOSTAL, BS 324 - BS 350, RBL 24 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON AFT CABIN FLOOR SUPPORT CHANNEL, BS 1661 - BS 1681, BL 0, WL 208. REPLACED AFT CABIN FLOOR SUPPORT CHANNEL, BS 1661 - BS 1681, BL 0, WL 208 IAW B757 SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL / FITTING, BS 330, RBL 24 - RBL 45. REPLACED INTERCOSTAL / FITTING, BS 330, RBL 24 - RBL 45 IAW B757 SRM 51-40-02.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON R4 DOOR CUTOUT SUPPORT, BS 1661 - BS 1681, RBL 57, WL 208. REPLACED R4 DOOR CUTOUT SUPPORT, BS 1661 - BS 1681, RBL 57, WL 208 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON FLOOR SUPPORT, BS 1640 - BS 1661, RBL 57, WL 208. REPLACED FLOOR SUPPORT, BS 1640 - BS 1661, RBL 57, WL 208 IAW B757 SRM 51-40-02.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON L4 DOOR CUTOUT SUPPORT, BS 1640 - BS 1661, LBL 56, WL 208. REPLACED L4 DOOR CUTOUT SUPPORT, BS 1640 - BS 1661, LBL 56, WL 208 IAW B757 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON FLOORBEAM, BS 345, LBL 58 - RBL 58. REPAIRED FLOORBEAM, BS 345, LBL 58 - RBL 58 IAW USAIRWAYS TYPICAL REPAIR 53-15-01.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON R4 DOOR THRESHOLD FRAME ATTACH ANGLE, BS 1681, RBL 58, WL 208. REPLACED R4 DOOR THRESHOLD FRAME ATTACH ANGLE, BS 1681, RBL 58, WL 208 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (CARGO DOOR) · airframe 42,734 hrs · 17,117 cycles

MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON AFT CARGO DOOR INTERCOSTAL WEB, BS 1420, S24R - S25R. REPLACED AFT CARGO DOOR INTERCOSTAL WEB, BS 1420, S24R - S25R IAW B757 SRM 51-40-02.

Part: DIFFUSER — CRACKED (COCKPIT) · airframe 41,789 hrs · 16,858 cycles

FLIGHT 731, LGW-PHL: DURING FLIGHT, THE CAPTAIN REPORTED DIFFICULTY HEARING RADIO TRANSMISSIONS DUE TO EXCESSIVE AIR NOISE IN THE COCKPIT. DIVERTED TO SNN. MAINTENANCE PLACED THE LEFT PACK ON MEL. SUBSEQUENT TROUBLESHOOTING DETERMINED THAT THE F/O'S WINDSHIELD AIR DIFFUSER WAS CRACKED AND A LOUD HUM WOULD DEVELOPE WITH THE PACK ON. REPAIRED DIFFUSER. NO FURTHER FAULTS.

Part: CONTROLLER — FAILED (CABIN TEMP) · airframe 41,341 hrs · 16,784 cycles

FLIGHT 724, PHL-SNN: TWENTY MINUTES INTO FLIGHT, COCKPIT TEMPERATURE BEGAN TO RISE. WHEN TEMPERATURE REACHED 97F, THE CAPTAIN ELECTED TO PHL. MAINTENANCE REPLACED THE ZONE TEMP CONTROLLER.

Part: BRAKE — CRACKED (NR 7) · airframe 40,534 hrs · 16,644 cycles

FLIGHT 0728, PHL-GLA: AFTER TAKEOFF, HYDRAULIC QUANTITY STARTED DROPPING ON BOTH LEFT AND RIGHT SYSTEMS. RETURNED TO PHL. MAINTENANCE FOUND THE NUMBER 7 BRAKE HOUSING CRACKED. REPLACED BRAKE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 39,653 hrs · 16,303 cycles

FLIGHT 708, LAS-CLT: DURING FLIGHT, CAPTAINS WINDSHIELD CRACKED. CREW STATED WINDSHIELD WAS BEGINNING TO LEAK AIR. FLIGHT DIVERTED TO MEM. MAINTENANCE REPLACED THE CAPTAINS WINDSHIELD.