N902AW

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 100,157 hrs · 35,135 cycles

EMERGENCY FLASHLIGHT AT FWD FLIGHT ATTENDANT STATION INOPERATIVE. REPLACED FLASHLIGHT AT FWD FLIGHT ATTENDANT STATION.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 99,991 hrs · 35,093 cycles

EMERGENCY FLASHLIGHT RED LIGHT NOT BLINKING AT FLIGHT ATTENDANT JUMP SEAT LOWER STORAGE EQUIPMENT AT 3R DOOR. R & R EMER FLASHLIGHT BATTERY AT FLIGHT ATTENDANT JUMP SEAT LOWER STORAGE EQUIPMENT AT 3R DOOR. OPERATIONAL CHECK IS GOOD

Part: SLIDING WINDOW — OUT OF ADJUST (COCKPIT) · airframe 99,503 hrs · 35,000 cycles

CAPTAINS WINDOW DIFFICULT TO UNLATCH. HANDLE BINDS HALFWAY THRU ARC. ADJUSTED CAPTAINS SLIDING WINDOW.

Part: LOCK — MISSING (GIRT BAR) · airframe 98,976 hrs · 34,900 cycles

DCA AFT LT CABIN SERVICE DOOR GIRT BAR LOCK ASSEMBLY MISSING. REPLACED AFT LT CABIN DOOR GIRT BAR LOCK ASSEMBLY. OPERATIONS CHECKED GOOD.

Part: CONTROLLER — FAULTY (WINDOW HEAT)

EN-ROUTE RT WINDOW HEAT CONTROLLER REQUIRES REPLACEMENT DUE TO ARCING WINDSHIELD. R&R WINDOW HEAT CONTROLLER. VENDOR SHOP FINDINGS, FAILURE WAS NOT RELATED TO REJECTION. FOUND EXTERNAL COVER DAMAGED & INTERNAL FOD. THE EJECTORS & LOCK PINS ON A1, A2, A3 & CCA'S WERE INTERNALLY DAMAGED WHICH WERE CAUSING THE FOD. UNIT FAILED INCOMING FUNCTION TEST INTERMITTENT ON BITE TEST. FAULT CONTROL UNIT REQUIRES REPAIR & RE-CALIBRATION. REPLACED CHASSIS S1 & S2 SWITCHES & EJECTORS A1 CCA, A2 CCA, A3 CCA & A4 CCA. REPAIRED THREE GND LUG TERMINALS WHICH WERE FOUND LOOSE & CLEANED OUT DUST, FOD, FROM INSIDE UNIT. EXTERNAL COVER WAS REPAIRED. THE CONTROLLER WAS RE-CALIBRATED & PASSED THE FINAL TEST.

Part: WINDSHIELD — ARCED (COCKPIT)

PHX FLT 515 EN ROUTE CUN TO PHX. RT NR 1 WINDOW HEAT INOPERATIVE. R & R FIRST OFFICER`S NR 1 WINDOW. VENDOR SHOP FINDINGS, THE WINDSHIELD WAS SCRAPPED BECAUSE IT WAS UNREPAIRABLE.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 98,878 hrs · 34,881 cycles

PHX, R1 DOOR ASSIST BOTTLE INDICATION IN LOWER RED OF INDICATOR. R & R R1 DOOR ASSIST BOTTLE.

Part: BEAM — CRACKED (VERTICAL STAB) · airframe 98,813 hrs · 34,860 cycles

C3 CHECK CRACK ON VERTICAL STABILIZER FIXED TE BEAM AT FIN STA 95.90, LBL10. REPAIRED VERTICAL STABILIZER FIXED TE BEAM AT FIN STA 95.90, LBL 10 IAW SRM 51-40-02, 51-40-05 & DWG173N1300.

Part: VALVE SEAT — LEAKING (EVAC SLIDE) · airframe 98,810 hrs · 34,859 cycles

PHX L1 DOOR ESCAPE SLIDE BOTTLE PRESS LOW. REPLACED L1 DOOR SLIDE. VENDOR SHOP FINDINGS REPAIRED CONTINUED TIME WARRANTY APPROVED LOW PRESS. FOUND BALL SEAT LEAKING & REPLACED.

Part: SLIDE RAFT — UNSERVICEABLE (L4 DOOR) · airframe 98,692 hrs · 34,837 cycles

EN-ROUTE SLIDE LIGHT AT 4L WOULDN’T ILLUMINATE WHEN FLIGHT ATTENDANT ARMED DOOR. REPLACED L4 DOOR SLIDE. VENDOR SHOP FINDINGS PASSED LIGHT SYS TEST. OVERHAULED & CHARGED RESERVOIR & VLV ASSEMBLY. PASSED PULL FORCE & LEAK TEST. OVERHAULED SLIDE. PASSED FUNCTIONAL, INFLATABLE INTEGRITY, HOUSE INTEGRITY & LIGHT SYS TEST. OK FOR SERVICE.

Part: GIRT BAR — DEFECTIVE (L4 DOOR)

PHX DOOR 4L GIRT BAR ATTACHMENT FITTING CAME OFF SLIDE ARMING BAR WHEN DOOR WAS OPENED. REATTACHED AFT GIRT BAR SLIDER SHOE & REATTACHED GIRT BAR TO L4 DOOR SLIDE.

Part: GIRT BAR — DEFECTIVE (L4 DOOR) · airframe 98,208 hrs · 34,742 cycles

PHX L4 DOOR GIRT BAR FWD FOOT NOT SLIDING. R & R L4 DOOR GIRT BAR.

Part: BUSHING — WORN (L4 DOOR)

PHX - INSPECT 4L DOOR GIRT BAR ASSEMBLY & OPERATIONS CHECK THE 4L DOOR LATCHING & ARMING ASSEMBLY DUE TO REPEAT DISCREPANCIES FOR DIFFICULTY IN CLOSING THE 4L DOOR, NO FAULT FOUND. R & R HAT BUSHINGS ON AFT POSITION L4 DOOR GIRT BAR CRANK. COMPLIED WITH L4 DOOR GIRT BAR MECHANISM ADJUSTMENT, OPERATIONS CHECKED GOOD.

Part: SLIDE — LOW PRESSURE (L3 DOOR) · airframe 97,846 hrs · 34,668 cycles

L3 SLIDE PRESS LOW. R & R L3 SLIDE.

Part: STRINGER — CORRODED (BS 1454) · airframe 97,508 hrs · 34,598 cycles

CORROSION ON LOWER SURFACE OF STRINGER 18L AT BS 1454. REPAIRED STRINGER IAW SRM 53-00-03-2R-1.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 97,056 hrs · 34,497 cycles

EMERGENCY FLASHLIGHT L2 DOOR RED LIGHT NOT FLASHING. REPLACED BATTERY IN FLASHLIGHT AT L2 DOOR, OP'S NORMAL.

Part: MECHANISM — LACK OF LUBE (L4 DOOR) · airframe 96,311 hrs · 34,332 cycles

4L DOOR MOUNTED SLIDE MECHANISM DIFFICULT TO MOVE. LUBED 4L DOOR MOUNTED SLIDE MECHANISM. OPS CK NORMAL.

Part: SKIN — CRACKED (BS 345 S7L) · airframe 95,899 hrs · 34,248 cycles

CRACK ON FUSELAGE SKIN AT BS 345, S7L. REPAIRED SKIN IAW EA 204872A, PG 1-13 & SB 757-53-0094 REV 1.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 95,899 hrs · 34,248 cycles

DAILY VISIT - L-1 DOOR FRAME FUSELAGE CUTOUT FORWARD CORNER CUTOUT RADIUS HAS A CRACK INDICATION AT NR 7 FASTENER IN THE BEAR STRAP AT BS 345 BETWEEN S6L TO S7L. REPAIRED L-1 DOOR FRAME FUSELAGE CUTOUT FORWARD CORNER CUTOUT BEAR STRAP AT BS 345 BETWEEN S6L TO S7L IAW EA 204872A.

Part: TRACK — CONTAMINATED (L4 DOOR) · airframe 95,809 hrs · 34,231 cycles

PHX - DOOR 4L DOES NOT DISARM. MECHANICAL LINKAGE MOVE BUT INDICATOR LIGHT REMAINS ON, INTERMITTENTLY. REMOVED EXCESSIVE GREASE FROM PROX SENSOR TRACK, OPS CHECKED GOOD.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 94,533 hrs · 33,980 cycles

C2 CHECK - CORROSION ON L3 EMERGENCY EXIT DOOR STRUCTURE FLOOR LEVEL CHORD ANGLE BETWEEN BS 1335.5 TO BS 1369.9, LBL 63. REPAIRED L3 EMERGENCY EXIT DOOR STRUCTURE FLOOR LEVEL CHORD ANGLE AT BS 1340, LBL 63 IAW EA 104423.

Part: SILL — CORRODED (FUSELAGE) · airframe 94,533 hrs · 33,980 cycles

C2 CHECK - CORROSION ON SILL PLATE WEB AT BS1346, S17L, WL 208.10. REPLACED SILL PLATE WEB AT BS 1346, S17L, WL 208.10 IAW BOEING DRAWING 146N8326.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 94,533 hrs · 33,980 cycles

C2 CHECK - DELAMINATION ON LEFT WING NR 4 SLAT TRAILING EDGE WEDGE AT APPROX 5 INCHES FROM TRAILING EDGE & 2 INCHES FROM INBOARD EDGE. REPAIRED LEFT WING NR 4 SLAT TRAILING EDGE WEDGE IAW B757 SRM 57-43-02 & 51-70-10-2R.

Part: SKIN PANEL — DEBONDED (VERTICAL STAB) · airframe 94,533 hrs · 33,980 cycles

C2 CHECK - AREA OF DISBONDING ON SKIN PANEL ON LOWER RIGHT SIDE OF VERTICAL STABILIZER TORQUE BOX BETWEEN FSS 150 TO FSS 180 & BETWEEN ASS 0 TO FSS 0. REPLACED SKIN PANEL ON LOWER RIGHT SIDE OF VERTICAL STABILIZER IAW B757 SRM 51-40-02.

Part: SCREW — LOOSE (MEGAPHONE) · airframe 93,893 hrs · 33,845 cycles

OGG - MEGAPHONE IN FORWARD CABIN INOP, HANDLE BROKEN. SECURED SCREW ON HANDLE, OPS OK.

Part: RESERVOIR — DEFECTIVE (R4 DOOR) · airframe 91,372 hrs · 33,356 cycles

PHX - R4 DOOR EMERGENCY OPEN RES. LOW ON AIR PRESSURE. REMOVED AND REPLACED R4 DOOR EMERGENCY DOOR OPEN RES.

Part: GUIDE — BROKEN (CABIN)

PHX - EXIT LIGHTING TRACK GUIDE BROKEN ROW 4 & 5 LEFT. INSTALLED EXIT LIGHTS GUIDE AT ROW 4 & 5 AS REQUIRED.

Part: COVER — BROKEN (CABIN)

PHX - L2 LIGHT COVER BROKEN. REMOVED AND INSTALLED L2 DOOR LIGHT COVER AS REQUIRED. OPS OK.

Part: SWITCH — BROKEN (CABIN) · airframe 89,543 hrs · 32,963 cycles

MCN - C1 - L2 DOOR EMERGENCY LIGHTS TEST SWITCH BROKEN. REPLACED L2 DOOR EMERGENCY LIGHTS TEST SWITCH AS REQUIRED. OPS TEST GOOD IAW B757 AMM 31-51-00 TEMP REVISION 33-019AW.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 89,543 hrs · 32,963 cycles

MCN - C1 CHECK - CORROSION ON INTERCOSTAL AT BS 1505, S25L - S26L. REPLACED INTERCOSTAL AT BS 1505, S25L - S26L IAW B757 SRM 51-30-01.

Part: STRUT — CORRODED (NLG) · airframe 89,543 hrs · 32,963 cycles

MCN - C1 - CORROSION ON RIGHT SIDE LOWER FORWARD AREA OF INNER BORE OF NOSE LANDING GEAR STRUT LOWER TORSION LINK LUG. REPLACED NOSE LANDING GEAR INNER CYLINDER ASSEMBLY LOWER STRUT IAW B757 32-51-11-4, 32-51-00-5 & 32-34-00-5.

Part: REVEAL — CRACKED (CARGO DOOR) · airframe 89,543 hrs · 32,963 cycles

MCN - C1 CHECK - CRACKED REVEAL STRIP ASSEMBLY ON THE AFT CARGO DOOR AT BS 1380, S26R. REPLACED REVEAL STRIP ASSEMBLY ON THE AFT CARGO DOOR AT BS 1380, S26R IAW B757-200 SRM 51-70-13, FIGURE 1.

Part: STRAP — CRACKED (FUSELAGE) · airframe 89,543 hrs · 32,963 cycles

MCN - C1 - CRACK ON FLOORBEAM STABILIZATION STRAP AT BS 1620, RBL 24.75. REPAIRED FLOORBEAM STABILIZATION STRAP AT BS 1620, RBL 24.75 IAW B757 SRM 51-70-13.

Part: COLLAR — CORRODED (NLG STEERING) · airframe 895,433 hrs · 2,963 cycles

MCN - C1 - CORROSION ON INNER BORE OF NOSE LANDING GEAR STEERING COLLAR UPPER TORSION LINK LUG. REPLACED NOSE LANDING GEAR STEERING COLLAR IAW B757 AMM 32-51-11-4, 32-51-00-5 & 32-34-00-5.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 8,954 hrs · 23,322 cycles

MCN - C1 CHECK - CORROSION ON INTERCOSTAL AT BS 1300 - BS 1320, LBL 17. REPLACED INTERCOSTAL AT BS 1300 - BS 1320, LBL 17 IAW B757 SRM 51-40-02.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 8,954 hrs · 23,322 cycles

MCN - C1 CHECK - CRACKED SEAT TRACK SUPPORT BEAM AT BS 880, LBL 45.50. REPAIRED SEAT TRACK SUPPORT BEAM AT BS 880, LBL 45.50 IAW EA 130554.

Part: STOP FITTING — CORRODED (L1 DOOR) · airframe 89,543 hrs · 32,963 cycles

MCN - C1 - CORROSION ON L1 DOOR STOP FITTING, NR 4 FROM THE TOP AT BS 377.7, S12L. REPLACED L1 DOOR STOP FITTING, NR 4 FROM THE TOP AT BS 377.7, S12L IAW B757 AMM 20-11-00-2.

Part: TRANSMISSION — LACK OF LUBE (TE FLAP)

LIH FLT 146 EN ROUTE PHX TO LIH. ON FINAL APPROACH, AFTER SELECTING FLAPS 25, THE CREW RECEIVED AN EICAS MESSAGE OF T/E FLAP DISAGREE. THE CREW PERFORMED A GO-AROUND AND COMPLETED THE APPROPRIATE QRH PROCEDURES. ON NEW APPROACH, THE CREW SELECTED FLAPS 20 AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED AN OPERATIONAL TEST OF THE FLAP/SLAT ALTERNATE DRIVE SYSTEM, TRAILING EDGE FLAP LOAD RELIEF SYSTEM, AND THE TRAILING EDGE SYSTEM. MAINTENANCE FOUND THE RIGHT INBOARD FLAP TRANSMISSION OIL QUANTITY LOW. MAINTENANCE SERVICED THE RIGHT INBOARD FLAP TRANSMISSION TO FULL. THE FLAP SYSTEM TESTED NORMAL AFTERWARDS.

Part: WIRE — DAMAGED (LT ENGINE)

LIH - FLT 146 EN ROUTE PHX TO LIH. THE LEFT ENGINE HAD AN INTERMITTENT ENGINE FIRE INDICATION. MAINTENANCE ACCOMPLISHED A TEMPORARY WIRE REPAIR AT THE SIX O'CLOCK, INBOARD SIDE, AFT OF GEAR BOX.

Part: STOWAGE BOX — LEAKING (COCKPIT)

HNL - FLT 22 EN-ROUTE PHX TO HNL. THE FLIGHT WAS IN CRUISE AT FL360, WHEN A CREW O2 SYSTEM LEAK WAS DISCOVERED. THE FLIGHT INITIALLY DESCENDED TO FL 250. WHEN IT WAS DETERMINED THAT THE LEAK COULD NOT BE STOPPED, THE CREW DECLARED AN EMERGENCY AND DESCENDED TO 10,000 FEET. REPLACED THE F/O'S O2 MASK BOX ASSEMBLY AND SERVICED THE CREW O2. ALL LEAK CHECKS OK.

Part: LIGHT — INOPERATIVE (EXTERIOR)

PHX - THE R3 EMERGENCY DOOR EXTERIOR LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE R3 EMERGENCY DOOR EXTERIOR LIGHT.

Part: COFFEEMAKER — FAULTY (GALLEY)

LIH - ODOR OF BURNING RUBBER IN AFT SECTION OF PLANE. TURNED OFF UTILITY BUSSES AND ODOR DISSIPATED. NO SIGN OF SMOKE. REPLACED AFT NUMBER SEVEN COFFEEMAKER.

Part: GUIDE ARM — OUT OF ADJUST (L2 DOOR)

OGG - FOUND THE L2 DOOR DIFFICULT TO CLOSE. COMPLIED WITH ADJUSTMENT/TEST OF L2 DOOR GUIDE ARM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 85,204 hrs · 23,322 cycles

MCN - C4 - MAJOR REPAIR - CORROSION ON ANTENNA MOUNT DOUBLER AT BS 1473, RBL 3. REPLACED ANTENNA MOUNT DOUBLER AT BS 1473, RBL3 IAW EA 130355.

Part: RAIL — CORRODED (FUSELAGE) · airframe 85,204 hrs · 3,209 cycles

MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON RAIL AT BS 1040 - BS 1060, RBL 7. REPLACED RAIL AT BS 1040 - BS 1060, RBL 7 IAW B757 SRM 51-40-02.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 85,204 hrs · 32,090 cycles

MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON TEE CHORD AT BS 1060, BL 0- RBL 25.5. REPAIRED TEE CHORD AT BS 1060, BL 0 - RBL 25.5 IAW B757 SRM 51-70-12.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 85,204 hrs · 32,090 cycles

MCN - MAJOR REPAIR - C4 CHECK - CRACKED STRINGER CLIP AT BS 1480, S30. REPLACED STRINGER CLIP AT BS 1480, S30 IAW B757 SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 85,204 hrs · 32,090 cycles

MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON STRINGER AT BS 1470, S30. REPAIRED STRINGER AT BS 1470, S30 IAW B757 SRM 53-00-03.

Part: PLATE — CORRODED (FUSELAGE) · airframe 85,204 hrs · 32,090 cycles

MCN - MAJOR REPAIR - C4 CHECK - GALVANIC CORROSION ON DECK PLATE AT BS 1680 - BS 1685, LBL 10.51. REPAIRED DECK PLATE AT BS 1680 - BS 1685, LBL 10.51 IAW B757 SRM 53-60-51.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,204 hrs · 32,090 cycles

MCN - C4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT BS 1681, LBL 50. REPAIRED FLOORBEAM AT BS 1681, LBL 50 IAW B757 SRM 53-00-51.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 85,204 hrs · 3,209 cycles

MCN - MAJOR REPAIR - C4 CHECK - GALVANIC CORROSION ON THE L4 DOOR CUTOUT AFT LOWER CORNER ATTACH ANGLE AT BS 1677 - BS 1680, LBL 65. REPLACED THE L4 DOOR CUTOUT AFT LOWER CORNER ATTACH ANGLE AT BS 1677 - BS 1680, LBL 65 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 85,204 hrs · 32,090 cycles

MCN - MAJOR REPAIR - C4 CHECK - GALVANIC CORROSION ON THE L4 DOOR THRESHOLD FLOOR SUPPORT AT BS 1661 - BS 1680, LBL 55. REPLACED THE L4 DOOR THRESHOLD FLOOR SUPPORT AT BS 1661 - BS 1680, LBL 55 IAW B757 SRM 51-40-02.

Part: PLATE — CORRODED (FUSELAGE) · airframe 85,204 hrs · 32,090 cycles

MCN - MAJOR REPAIR - C4 CHECK - GALVANIC CORROSION ON DECK PLATE AT BS 1713 - BS 1718, LBL 1 - LBL 52. REPAIRED DECK PLATE AT BS 1713 - BS 1718, LBL 1 - LBL 52 IAW B757 SRM 53-60-51.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 85,204 hrs · 32,090 cycles

MCN - MAJOR REPAIR - C4 CHECK - GALVANIC CORROSION ON L-4 DOOR THRESHOLD FLOOR SUPPORT BS 1640 - BS 1661, LBL 55. REPLACED L-4 DOOR THRESHOLD FLOOR SUPPORT BS 1640 - BS 1661, LBL 55 IAW B757 SRM 51-40-02.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 85,204 hrs · 32,090 cycles

MCN - MAJOR REPAIR - C4 CHECK - GALVANIC CORROSION ON R-4 DOOR CUTOUT THRESHOLD WEB DRAIN TROUGH SUPPORT Z-ANGLE BS 1650-BS 1670, RBL 59. REPLACED R-4 DOOR CUTOUT THRESHOLD WEB DRAIN TROUGH SUPPORT Z-ANGLE BS 1650-BS 1670, RBL 59 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 85,204 hrs · 23,322 cycles

MCN - MAJOR REPAIR - C4 CHECK - GALVANIC CORROSION ON R-4 DOOR CUTOUT FLOOR SUPPORT AT BS 1650 - BS 1670, RBL 56. REPLACED R-4 DOOR CUTOUT FLOOR SUPPORT AT BS 1650 - BS 1670, RBL 56 IAW B757 SRM 51-40-02.

Part: WEB — CORRODED (FUSELAGE) · airframe 85,204 hrs · 32,090 cycles

MCN - MAJOR REPAIR - C4 CHECK - GALVANIC CORROSION ON SHEAR DECK WEB AT BS 1680 - BS 1685, RBL 20 - RBL 41. REPAIRED SHEAR DECK WEB AT BS 1680 - BS 1685, RBL 20 - RBL 41 IAW B757 SRM 53-60-01.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 85,204 hrs · 32,090 cycles

MCN - MAJOR REPAIR - C4 CHECK - GALVANIC CORROSION ON L-ANGLE STIFFENER ON BOTTOM SIDE OF AFT DECK PLATE IN AFT CABIN AT BS 1715, RBL 5. REPLACED L-ANGLE STIFFENER ON BOTTOM SIDE OF AFT DECK PLATE IN AFT CABIN AT BS 1715, RBL 5 IAW B757 SRM 51-40-02.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 85,204 hrs · 32,090 cycles

MCN - MAJOR REPAIR - C4 CHECK - GALVANIC CORROSION ON SHEAR DECK WEB REPAIR DOUBLER, BS 1710-1717 RBL 20 - RBL 51. REPLACED SHEAR DECK WEB REPAIR DOUBLER BS 1710-1717 RBL 20- RBL 51 IAW B757 SRM 53-60-51.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 85,204 hrs · 32,090 cycles

MCN - MAJOR REPAIR - C4 CHECK - INTERGRANULAR CORROSION ON SHEAR DECK WEB STIFFENER AT BS 1714 - BS 1716, RBL 13 - RBL 14. REPLACED SHEAR DECK WEB STIFFENER AT BS 1714 - BS 1716, RBL 13 - RBL 14 IAW B757 SRM 51-40-02.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 85,204 hrs · 32,090 cycles

MCN - MAJOR REPAIR - C4 CHECK - EXFOLIATION CORROSION ON SHEAR DECK WEB STIFFENER, BS 1713-1716 LBL 2-RBL 2. REPLACED SHEAR DECK WEB STIFFENER, BS 1713-1716 LBL 2 - RBL 2 IAW B757 SRM 51-40-02.

Part: ANGLE — CRACKED (ZONE 100)

MAJOR REPAIR - CRACK ON UPPER ANGLE ON INTERCOSTAL BETWEEN BS 1420 TO BS 1440, BL0. REPLACED ANGLE ON INTERCOSTAL BETWEEN BS 1420 TO BS 1440, BL0 IAW SRM 51-40-02.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,204 hrs · 32,090 cycles

MCN - C4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SUPPORT AT BS 365 BETWEEN RBL 40 TO RBL 48. REPLACED SUPPORT AT BS 365 BETWEEN RBL 40 TO RBL 48 IAW B757 SRM 51-40-02 & 53-00-51.

Part: ROD END — BROKEN (L2 DOOR)

PHX - L2 DOOR ARMING ROD-END BROKEN. REMOVED AND REPLACED L2 DOOR ARMING ROD END.

Part: SWITCH — INOPERATIVE (CABIN)

PHX - L4 DOOR EMERGENCY LIGHT SWITCH INOPERATIVE. REMOVED AND REPLACED TEST SWITCH.

Part: BATTERY PACK — DISCHARGED (CABIN)

PHX - FLIGHT ATTENDANTS REPORTED EVERY EXIT LIGHT ON WITH DARK AIRCRAFT FOR APPROXIMATELY 20 MINUTES DURATION. MAINTENANCE REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERY PACKS. OPERATIONAL CHECKED PER MM 33-51-07-2.

Part: RESERVOIR — EMPTY (L4 DOOR ASSIST)

PHX - THE L4 DOOR EMERGENCY ASSIST BOTTLE HAS ZERO PRESSURE. REPLACED THE L4 DOOR EMERGENCY ASSIST RESERVOIR PER MM 52-11-30-4.

Part: RESERVOIR — DISCHARGED (L4 DOOR)

PHX - THE L4 DOOR EMERGENCY ASSIST BOTTLE HAS ZERO PRESSURE. REPLACED THE L4 DOOR EMERGENCY POWER RESERVOIR.

Part: LANYARD — UNSECURE (EVAC SLIDE)

PHX - THE L4 DOOR SLIDE RAFT TETHER LINE FELL OUT OF SLIDE BUSTLE. VISUALLY INSPECTED DOOR L4. NO FAULTS FOUND. ALL SECURE.

Part: LANYARD — UNSECURE (L4 DOOR SLIDE)

PHX - THE TETHER CORD FOR SLIDE AT DOOR L4 IS COMING LOOSE FROM BENEATH THE SLIDE BUSTLE. RE-INSERTED THE CORD INTO THE SLIDE AT DOOR L4.

Part: LANYARD — UNSECURE (EVAC SLIDE)

HNL - WHEN THE L4 DOOR ESCAPE SLIDE WAS DISARMED, A CHAIN AND BUCKLE FELL OUT. STOWED AND SECURED EXCESS CORD INTO SLIDE PACK.

Part: OUTFLOW VALVE — MALFUNCTIONED (ZONE 200)

PHX FLT 42 PHX TO DCA. THE AIRCRAFT WAS UNABLE TO MAINTAIN CABIN PRESSURE AT FL 370. DURING THE RETURN TO PHX, AS THE FLIGHT DESCENDED TO FL200, THE AIRCRAFT MAINTAINED A CABIN PRESSURE ALTITUDE OF 7,000 FEET WITH THE OUTFLOW VALVE CLOSED, AND LEFT AND RIGHT DUCT PRESSURE AT 40 PSI. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE UPPER CABIN PRESSURE RELIEF VALVE.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 80,759 hrs · 31,050 cycles

MCN - EEL - C12 CHECK - EMERGENCY ESCAPE PATH LIGHTS WILL NOT ILLUMINATE AT SEATS 19L AND 24L. REPLACED EMERGENCY ESCAPE PATH LIGHT HARNESS CONNECTORS AT SEATS 19L AND 24L IAW BSWPM 20-42-01 AND OPERATIONAL CHECKED IAW USAIRWAYS TASK CARD, A1C33606.

Part: SKIN — CRACKED (NR 2 SLAT) · airframe 80,759 hrs · 31,050 cycles

MCN - MAJOR REPAIR - C12 CHECK - LEFT WING NR 2 SLAT COVE PANEL CRACKED, SS 607. REPLACED LEFT WING NR 2 SLAT COVE PANEL CRACKED, SS 607 IAW B737 SRM 51-40-02.

Part: WIRE HARNESS — SHORTED (EMERGENCY LIGHTS) · airframe 80,759 hrs · 31,050 cycles

MCN - EES - C12 CHECK - EMERGENCY BATTERY WIRING HARNESS WIRING SHORTED IN FIRST CLASS CEILING AREA. REPAIRED AND OPERATIONAL CHECKED EMERGENCY BATTERY WIRING HARNESS WIRING SHORTED IN FIRST CLASS CEILING AREA IAW BSWPM 20-30-12 AND B757 AMM 33-017AW.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,759 hrs · 31,050 cycles

MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTERCOSTAL CLIP, BS 660, S17L. REPLACED INTERCOSTAL CLIP, BS 660, S17L IAW EO 5331-01021 AND TASK CARD M1C53611.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 80,759 hrs · 31,050 cycles

MCN - MAJOR REPAIR - C12 CHECK, CRACKED INTERCOSTAL, BS 660, S15L. REPLACED INTERCOSTAL, BS 660, S15L IAW TASK CARD M1C53614.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 80,759 hrs · 23,322 cycles

MCN - MAJOR REPAIR - C12 CHECK - CRACKED VERTICAL STIFFENER ANGLE, BS 700, RBL 24.75. REPLACED VERTICAL STIFFENER ANGLE, BS 700, RBL 24.75 IAW USAIRWAYS EA 130014.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 80,759 hrs · 31,050 cycles

MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTERCOSTAL ATTACH CLIP, BS 1280, LBL 45.5, WL 208. REPLACED INTERCOSTAL ATTACH CLIP, BS 1280, LBL 45.5, WL 208 IAW B757 SRM 51-40-02.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 80,759 hrs · 31,050 cycles

MCN - MAJOR REPAIR - C12 CHECK - CORROSION ON AFT CARGO COMPARTMENT DOOR CUTOUT OUTBOARD CHORD, BS 1374 - BS 1376, S27R. REPAIRED AFT CARGO COMPARTMENT DOOR CUTOUT OUTBOARD CHORD, BS 1374 - BS 1376, S27R IAW USAIRWAYS EA 130016.

Part: ANGLE — CORRODED (BS 1375-1380) · airframe 80,759 hrs · 31,050 cycles

MCN - MAJOR REPAIR - C12 CHECK - CORROSION ON ANGLE, BS 1375 - BS 1380, RBL 23. REPLACED ANGLE, BS 1375 - BS 1380, RBL 23 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,759 hrs · 31,050 cycles

MCN - MAJOR REPAIR - C12 CHECK - LEVEL 2 CORROSION ON FLOOR SUPPORT, BS 720 - BS 740, LBL 60 - LBL 65, WL 206. REPLACED FLOOR SUPPORT, BS 720 - BS 740, LBL 60 - LBL 65, WL 206 IAW B757 SRM 51-40-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 80,759 hrs · 31,050 cycles

MCN - MAJOR REPAIR - C12 CHECK - CORROSION ON INTERCOSTAL ANGLE, BE 1360 - BS 1380, RBL 24.5, WL 208. REPLACED INTERCOSTAL ANGLE, BE 1360 - BS 1380, RBL 24.5, WL 208 IAW B757 SRM 51-40-02.

Part: WEB — CORRODED (ZONE 200) · airframe 80,759 hrs · 31,050 cycles

MCN - MAJOR REPAIR - C12 CHECK - CORROSION ON WEB, BS 1380 - BS 1450, RBL 23. REPLACED WEB, BS 1380 - BS 1450, RBL 23 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,759 hrs · 31,050 cycles

MCN - MAJOR REPAIR - C12 CHECK, LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 720 - BS 740, LBL 65. REPLACED CABIN FLOOR SUPPORT, BS 720 - BS 740, LBL 65 IAW B737 SRM 51-40-02.

Part: STRAP — CRACKED (FUSELAGE) · airframe 80,759 hrs · 31,050 cycles

MCN - MAJOR REPAIR - C12 CHECK - CRACKED FLOORBEAM STABILIZER STRAP, BS 377.7 - 395, LBL 24.75. REPLACED FLOORBEAM STABILIZER STRAP, BS 377.7 - 395, LBL 24.75 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 80,759 hrs · 31,050 cycles

MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTERCOSTAL, BS 660, RBL 45.5. REPLACED INTERCOSTAL, BS 660, RBL 45.5 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,759 hrs · 31,050 cycles

MCN - MAJOR REPAIR - C12 CHECK - LEVEL 2 CORROSION ON MAIN DECK FLOOR SUPPORT, BS 365, RBL 48. REPLACED MAIN DECK FLOOR SUPPORT, BS 365, RBL 48 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,759 hrs · 23,322 cycles

MCN - MAJOR REPAIR - C12 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 348 - BS 358, RBL 55. REPLACED CABIN FLOOR SUPPORT, BS 348 - BS 358, RBL 55 IAW B757 SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,759 hrs · 31,050 cycles

MCN - MAJOR REPAIR - C12 CHECK - LEVEL 2 CORROSION ON STRINGER, BS 760, S21R. REPAIRED STRINGER, BS 760, S21R IAW B757 SRM 53-00-03-2R1, FIGURE 201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,759 hrs · 31,050 cycles

MCN - MAJOR REPAIR - C12 CHECK - LEVEL 2 CORROSION ON MAIN DECK FLOOR SUPPORT, BS 349 - BS 354, LBL 55. REPLACED MAIN DECK FLOOR SUPPORT, BS 349 - BS 354, LBL 55 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,759 hrs · 31,050 cycles

MCN - MAJOR REPAIR - C12 CHECK - LEVEL 2 CORROSION ON MAIN DECK FLOOR SUPPORT, BS 297, RBL 32.50. REPLACED MAIN DECK FLOOR SUPPORT, BS 297, RBL 32.50 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,759 hrs · 31,050 cycles

MCN - MAJOR REPAIR - C12 CHECK, LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 316, LBL 21.50. REPLACED CABIN FLOOR SUPPORT, BS 316, LBL 21.50 IAW B737 SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 80,759 hrs · 31,050 cycles

MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTERCOSTAL AT THE L2 DOOR CUTOUT, BS 660, S11L. REPAIRED INTERCOSTAL AT THE L2 DOOR CUTOUT, BS 660, S11L IAW USAIRWAYS TASK CARD M1C53604.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 80,759 hrs · 31,050 cycles

MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTERCOSTAL ANGLE, BS 795, BL 0, WL 208. REPLACED INTERCOSTAL ANGLE, BS 795, BL 0, WL 208 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 80,759 hrs · 31,050 cycles

MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTEROSTAL, BS 660, S14R. REPAIRED INTEROSTAL, BS 660, S14R IAW USAIRWAYS EO 5331-01021 AND TASK CARD M1C53611.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 80,759 hrs · 31,050 cycles

MCN - MAJOR REPAIR - C12 CHECK - CORROSION ON SHEAR TIE, BS 1376, RBL 24. REPLACED SHEAR TIE, BS 1376, RBL 24 IAW B757 SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,759 hrs · 31,050 cycles

MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTERCOSTAL CLIP, BS 1300, RBL 45.5, WL 208. REPLACED INTERCOSTAL CLIP, BS 1300, RBL 45.5, WL 208 IAW B757 SRM 51-40-02.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 80,759 hrs · 23,322 cycles

MCN - MAJOR REPAIR - C12 CHECK - CRACKED FLOORBEAM UPPER CHORD, BS 700, RBL 24.75 AND RBL 45.5, WL 207. REPLACED FLOORBEAM UPPER CHORD, BS 700, RBL 16.25 - RBL 53.5, WL 207 IAW USAIRWAYS EA 130014.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,759 hrs · 31,050 cycles

MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTERCOSTAL CLIP, BS 1300, LBL 45.5, WL 208. REPLACED INTERCOSTAL CLIP, BS 1300, LBL 45.5, WL 208 IAW B757 SRM 51-40-02.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

PHX - EMERGENCY EXIT SIGN LIGHT AT R-1 DOOR IS INOP DURING TEST. MAINTENANCE REPAIRED BROKEN WIRE. OPS CHECKS OK.

Part: PROXIMITY SWITCH — FAILED (MLG)

PHX FLL-PHX FLT NR 181 AT FL320, CREW RECEIVED RED FLAPS AND 3 GREEN GEAR DOWN LANDING LIGHTS ALONG WITH OTHER CAUTIONS. THE CREW PUT THE LANDING LEVER FROM THE NORMAL POSITION TO THE UP POSITION AND LIGHTS AND TAKEOFF CONFIG HORN WENT OUT. FLIGHT CONTINUED TO PHX WITH MACH/SPEED TRIM, AIR/GROUND DISAGREE WARNING, WARNING ELECTRIC LANDING GEAR MONITOR, AND NOSE AIR/GROUND DISAGREE. CREW DECLARED AN EMERGENCY AND REQUESTED CFR. ON ARRIVAL, LANDING GEAR EXTENDED PROPERLY WITH NORMAL INDICATIONS, LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED PROX SWITCH ELECTRONICS UNIT. OPS CHECKED OK.

Part: WIRE HARNESS — UNKNOWN (EMERGENCY LIGHTS) · airframe 79,371 hrs · 30,701 cycles

MAINTENANCE FOUND FLOOR LEVEL LIGHT AT ROW 33L INOPERATIVE. REPLACED WIRE HARNESS TO LIGHT ASSEMBLY. NO FURTHER FAULTS.

Part: CONTROL PANEL — FAILED (EMERGENCY LIGHTS) · airframe 78,991 hrs · 30,606 cycles

MAINTENANCE FOUND THAT EMERGENCY LIGHTS WILL NOT ARM. REPLACED THE FLIGHT DECK OVERHEAD EMERGENCY LIGHT PANEL. NO FURTHER FAULTS.

Part: MEGAPHONE — FAILED (CABIN) · airframe 77,915 hrs · 30,337 cycles

PHX - EE - CREW REPORTED AFT EMERGENCY MEGAPHONE INOP. MX REPLACED THE MEGAPHONE.

Part: HOSE — RUPTURED (CREW O2 SYSTEM) · airframe 77,674 hrs · 30,267 cycles

LAX - DIV - FLIGHT NR 432 DIVERTED TO LAX DUE TO CREW O2 SYSTEM DEPLETED. FLIGHT CREW DECLARED AN EMERGENCY DUE TO THE INABILITY TO MAINTAIN RVSM ALTITUDE BUT AFTER THE AIRCRAFT WAS OUT OF THE RVSM THE CAPTAIN DEEMED THE SITUATION A NON-EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT AND MAINTENANCE REPLACED A RUPTURED O2 LINE BELOW THE O2 MASK STORAGE BOX IAW AWA TASK CARD R1B35601.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 76,097 hrs · 29,865 cycles

MCN - MAJOR REPAIR - CORROSION ON INTERCOSTAL, BS 728, S26R - S27R, WL 148.50. REPLACED INTERCOSTAL, BS 728, S26R - S27R, WL 148.50 IAW B757-200 SRM 53-00-04 AND 51-40-02.

Part: POWER UNIT — INOPERATIVE (FLASHLIGHT) · airframe 76,097 hrs · 29,865 cycles

MCN - EEL - C-11 CHECK - EMERGENCY FLASHLIGHT AT RIGHT AFT FLIGHT ATTENDANT AT R3 DOOR IS INOPERATIVE. REPLACED RIGHT AFT FLIGHT ATTENDANT AT R3 DOOR EMERGENCY FLASHLIGHT POWER UNIT .

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 76,097 hrs · 29,865 cycles

MCN - MAJOR REPAIR - C-11 CHECK - CORROSION ON AFT CARGO COMPARTMENT INTERCOSTAL, BS 1400 - BS 1420, S27L - S28L. REPLACED AFT CARGO COMPARTMENT INTERCOSTAL, BS 1400 - BS 1420, S27L - S28L IAW B757-200 SRM 51-40-02.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 76,097 hrs · 29,865 cycles

MCN - MAJOR REPAIR - C-11 CHECK - CORROSION ON STRINGER 29R J-CHANNEL, BS 1640 - BS 1660. REPLACED STRINGER 29R J-CHANNEL, BS 1640 - BS 1660 IAW B757-200 SRM 51-40-02 AND DRAWING 146N3642-9.

Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 76,097 hrs · 29,865 cycles

MCN - MAJOR REPAIR - CORROSION ON INTERIOR FUSELAGE SKIN BETWEEN BS 1660 TO 1680 AND STRINGERS 29L TO 29R. REPAIRED INTERIOR FUSELAGE SKIN BETWEEN BS 1660 TO 1680 AND STRINGERS 29L TO 29R IAW AWA ER 19-5300-06314-ES1.

Part: CHANNEL — CORRODED (BS 1981-1686) · airframe 76,097 hrs · 29,865 cycles

MCN - MAJOR REPAIR-C-11, CORROSION ON HAT CHANNEL B/S 1681-1686, RBL 16. REMOVED, FABRICATED AND REPLACED HAT CHANNEL B/S 1681-1686, RBL 16, IAW B757-200 SRM 51-40-02-0G, PAR 4, FIG 3 AND 8 AND DRAWING 146N5300.

Part: SUPPORT — CORRODED (BS 1690-1775) · airframe 76,097 hrs · 29,865 cycles

MCN - MAJOR REPAIR-C-11- CORROSION ON HAT CHANNEL FROM B/S 1690 TO B/S 1715 AT BL 0. REMOVED, FABRICATED AND REPLACED HAT CHANNEL FROM B/S 1690 TO B/S 1715 AT BL 0, IAW B757-200 SRM 51-40-02-0G, PARA 4 B AND E, FIG'S 3 AND 8 AND DRAWING 146N5300.

Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 76,097 hrs · 29,865 cycles

MCN - CORROSION BULGE ON FUSELAGE SKIN INNER SURFACE, BS 728, S22R INSIDE THE FORWARD CARGO COMPARTMENT. REPAIRED FUSELAGE SKIN INNER SURFACE, BS 728, S22R INSIDE THE FORWARD CARGO COMPARTMENT IAW AWA ER 19-5300-06314-ES2.

Part: CHANNEL — CORRODED (BS 1690-1715) · airframe 76,097 hrs · 29,865 cycles

MCN - MAJOR REPAIR - C-11 CHK, CORROSION ON HAT CHANNEL FROM BS 1690 TO 1715 AT RBL 16. REMOVED, FABRICATED AND REPLACED HAT CHANNEL FROM BS 1690 TO 1715 AT RBL 16 IAW B757-200 SRM 51-40-02-06 FIG 3, 8, AND DRAWING 146N5300.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 70,697 hrs · 29,865 cycles

MCN - MAJOR REPAIR - INTERCOSTAL CRACKED ADJACENT TO L2 DOOR STOP NR 4, BS 660 - BS 686, S12L. REPLACED INTERCOSTAL ADJACENT TO L2 DOOR STOP NR 4, BS 660 - BS 686, S12L PER TASKCARD M1C53608.

Part: PLATE — CORRODED (BS 1681-1720) · airframe 76,097 hrs · 29,865 cycles

MCN - MAJOR REPAIR - CORROSION ON CABIN FLOOR SHEAR WEB, B/S 1681-1720 BL 0 TO RBL 55. REPAIRED CABIN FLOOR SHEAR WEB (DECK PLATE), B/S 1681-1720, BL 0 TO RBL 55, IAW B757-200 SRM 53-60-51-2R2, FIG 201.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 76,097 hrs · 29,865 cycles

MCN - MAJOR REPAIR - C-11 CHECK - NR# 5929345, L2 DOOR UPPER HINGE INTERCOSTAL RADIUS CRACKED 2 PLACES, BS 686, S11L. REPLACED L2 DOOR UPPER HINGE INTERCOSTAL RADIUS IAW TASKCARD M1C53606.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 76,097 hrs · 29,865 cycles

MCN - MAJOR REPAIR - R2 DOOR UPPER HINGE INTERCOSTAL RADIUS CRACKED 2 PLACES, BS 686, S11R. REPLACED R2 DOOR UPPER HINGE INTERCOSTAL, BS 686, S11R PER TASKCARD M1C53606.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 76,034 hrs · 29,848 cycles

PHX - EEL - DURING ROUTINE MAINTENANCE IT WAS DISCOVERED THAT THE EMERGENCY PATH LIGHT WAS INOP. MX RECONNECTED THE CONNECTOR FOR THE EMERGENCY ESCAPE PATH LIGHTS. OPS CHECK WAS GOOD.

Part: WIRE HARNESS — BURNED (AFT GALLEY) · airframe 75,374 hrs · 29,669 cycles

PHX - BURNING ODOR - DURING 4-DAY CHECK, TECH APPLIED GROUND PWR AND NOTICED LIGHTS FLICKERING. A FEW SECONDS WENT BY AND POWER WENT OFF. AFTER RESETTING POWER TO A/C PWR CAME BACK ON. AS TECH WAS LEAVING A/C NOTICED FLAMES IN AFT GALLEY AREA. PWR WAS SECURED TO A/C AND TECH WENT TO AFT GALLEY AREA AND NOTICED FLAMES IN AFT GALLEY NR 4 OVEN AREA. TECH GRABBED A FIRE EXTINGUISHER AND DISCHARGED THE EXTINGUISHER TWICE, PUTTING OUT FIRE. UPON INVESTIGATION DISCOVERED THAT COLA HAD SPILLED IN DRY STORAGE AREA ABOVE OVEN AND MADE IT'S WAY DOWN TO CONNECTOR CAUSING CONNECTOR TO SHORT ACROSS PINS AND CAUSING FIRE. MX REPLACED WIRING HARNESS AND CONNECTOR J5 AT AFT GALLEY OVEN NR 4 PER WDM 25-3-1-32 FIG 11 SEC

Part: CHARGER — BURNED (MASTER BATTERY) · airframe 74,615 hrs · 29,481 cycles

PHX - ELECTRICAL POWER - MAINTENANCE DISCOVERED THE MAIN BATTERY CHARGER POSITIVE TERMINAL BURNT. MAINTENANCE REPLACED THE POSITIVE LUG AND MAIN BATTERY CHANGER IAW BOEING MM 24-31-02-4 AND SWP 20-30-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,759 hrs · 31,050 cycles

MCN - MAJOR REPAIR - C12 CHECK, LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 341, RBL 55, WL 208. REPLACED CABIN FLOOR SUPPORT, BS 341, RBL 55, WL 208 IAW B737 SRM 51-40-02.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,030 hrs · 28,130 cycles

SEA - EEL - MAINTENANCE DISCOVERED THE EMERGENCY EXIT AND EXIT LIGHTS AT L4 WERE INOP. REMOVED AND REPLACED THE POWER SUPPLY IAW BOEING AMM 33-51-07-02. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY PACK — INOPERATIVE (FUSELAGE) · airframe 73,501 hrs · 29,192 cycles

DURING OVERNIGHT INSPECTION REPORTED THE EMERGENCY EXIT SIGN AT DOOR L4 AND AISLE LIGHTS AT LT ROW 34 AND 30 WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AFT LT BATTERY PACK IAW MM 33-51-07. OPERATIONAL CHECKS WERE GOOD.

Part: INDICATOR — UNKNOWN (COCKPIT) · airframe 73,406 hrs · 29,157 cycles

CREW REPORTED THAT ON TAKEOFF ROLL THE FO'S AIRSPEED INDICATOR WENT INOPERATIVE AT APPROXIMATELY 80 KTS. AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE MACH AIRSPEED INDICATOR ON THE F/O'S SIDE IAW BOEING 757-200 MM 34-13-02-4. OPS CHK GOOD. COULD NOT CONFIRM FAULT. UNIT INSPECTED AND TESTED IAW CMM 34-13-09 REV 12.

Part: INDICATOR — FAILED (AIRSPEED) · airframe 73,339 hrs · 29,129 cycles

DFW - ABORTED TAKEOFF - FLT 654 - CREW REPORTED THAT ON TAKEOFF ROLL, THE F/O GOT MACH AND AIRSPEED FLAGS ON THE AIRSPEED INDICATOR AT 80 KT. F/0'S AIRSPEED NEEDLE WAS READING ZERO. CREW ABORTED TAKEOFF AT 80 KNOTS AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECKS IAW BOEING 757-200 MM 34-13-02-4. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,266 hrs · 29,102 cycles

PHX - EEL - DURING OVERNIGHT INSPECTION DISCOVERED EXTERIOR EMERGENCY LIGHT AT DOOR 4 LEFT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK, OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,266 hrs · 29,102 cycles

PHX - EEL - DURING INSPECTION DISCOVERED LEFT AFT BULLNOSE EMERGENCY LIGHTS INOPERATIVE AT ROWS 30 AND 34. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT BATTERY PACK IAW BOEING 757 MM 39-50. OPERATIONAL CHECKS WERE GOOD.

Part: WIRE — SHORTED (EMERGENCY LIGHT) · airframe 72,822 hrs · 28,910 cycles

PHX - EEL - DURING OVERNIGHT MAINTENANCE DISCOVERED ROWS 27 THROUGH 35 EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPAIRED WIRE UN SEAT 29 IAW BOEING SWPM 20-30. OPERATIONAL CHECKS WERE GOOD.

Part: A/C PACK — TRIPPED (LEFT) · airframe 72,770 hrs · 28,880 cycles

PHX - ABORTED TAKEOFF - FLT 662 - AFTER ADVANCING THROTTLES FOR TAKEOFF THE LEFT PACK AND BLEED TRIPPED OFF. AIRCRAFT TAXIED OFF RUNWAY AND RESET THE LEFT PACK SYSTEM PER MOC. SYSTEMS RETURNED TO NORMAL, AIRCRAFT ATTEMPTED SECOND TAKEOFF WITHOUT FURTHER INCIDENT.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 72,772 hrs · 28,883 cycles

SAN - ABORTED TAKEOFF - FLT 542 - CREW REPORTED THAT ON TAKEOFF THE NR 2 ENGINE EGT EXCEEDED AND ENGINE ROLLED DOWN PAST IDLE. AIRCRAFT TAXIED OFF RUNWAY AND CONTINUED BACK TO THE GATE WITHOUT FURTHER INCIDENT. AIRCRAFT IS STILL IN WORK. THE NR. 2 ENGINE WAS REMOVED AND REPLACED IAW AMERICA WEST AIRLINES TASK CARD R5M71601. OPERATIONAL CHECKS WERE GOOD.

Part: LINE — CRACKED (HYD SYS) · airframe 71,832 hrs · 28,496 cycles

DURING FLIGHT, LT HYDRAULIC QUANTITY SHOWED ZERO. RETURNED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND HYDRAULIC LINE TO PTU PRESSURE SWITCH CRACKED. REMOVED AND REPLACED LINE IAW BOEING 757 MM 29-31-00 AND BOEING 757 MM 20-11-00. NO LEAKS WERE NOTED.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 71,527 hrs · 28,356 cycles

DURING C-10 CHECK, EXFOLIATION CORROSION WAS FOUND INBOARD OF R1 DOOR THRESHOLD ON SUPPORT CHANNEL BETWEEN BS 324 AND BS 345. MAINTENANCE REMOVED CORRODED R1 DOOR THRESHOLD SUPPORT CHANNEL FROM BS 324 TO BS 345; FABRICATED A NEW REPLACEMENT SUPPORT CHANNEL; AND INSTALLED REPAIR PART IAW BOEING 757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 71,527 hrs · 28,356 cycles

DURING C-10 CHECK CORROSION WAS FOUND AT NUT PLATE HOLES ON UPPER SURFACE OF AFT CARGO DOOR SILL FLOOR SUPPORT FRAME BETWEEN BS 1380 AND BS 1410. MAINTENANCE REMOVED CORRODED AFT CARGO DOOR SILL FLOOR SUPPORT FRAME FROM BS 1380 TO BS 1410; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; AND INSTALLED REPAIR PART IAW BOEING 757 SRM 51-40-02.

Part: WIRE — BROKEN (SEAT ROW 23 LT) · airframe 71,222 hrs · 28,212 cycles

PHX - EEL - DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 23 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 23 LT, OPERATIONAL CHECK WAS GOOD.

Part: BRAKE ASSY — DAMAGED (NR 3, RT MLG) · airframe 69,784 hrs · 27,581 cycles

AFTER ARRIVAL IN PHX EN ROUTE FROM LAS, FLIGHT CREW NOTICED HYDRAULIC FLUID WAS LOW ON QUANTITY GAUGE, FURTHER INSPECTION REVEALED DAMAGE TO NR 3 BRAKE ASSEMBLY. IT APPEARS BRAKE ROD DISCONNECTED CAUSING NR 3 BRAKE TO ROTATE SHEARING HYDRAULIC LINES AND TEMPERATURE SENSOR WIRES. NR 3 BRAKE ROD CONTACTED THE NR 7 BRAKE ROD DIRECTLY BEHIND IT CAUSING THE NR 7 BRAKE ROD TO BEND. MAINTENANCE REMOVED AND REPLACED THE NR 3 BRAKE ASSEMBLY IAW T/C R4M32604. REPLACED NR 3 AND NR 7 BRAKE RODS IAW BMM 32-11-19-4, AND REPLACED WIRING AND CONDUIT FROM JUNCTION BOX TO CONNECTOR D022656. REMOVED AND REPLACED HYDRAULIC FLEX LINE PER T/C R4M32604, LEAK AND OPERATIONAL CHECKS WERE GOOD.

Part: SKIN — DELAMINATED (RT WING LE) · airframe 68,558 hrs · 27,036 cycles

UPPER SURFACE OF RT FIXED WING LEADING EDGE DELAMINATED AT WS 421. MAINTENANCE REMOVED DAMAGED AREA OF SKIN ON UPPER SURFACE OF R/H FIXED WING LEADING EDGE AT WS 421; FABRICATED A FILLER, NEW SECTION OF SKIN, AND A SPLICE PLATE; INSTALLED REPAIR PART IAW AWA E.R. 19-5700-00012-DD5.

Part: SKIN — DELAMINATED (RT WING LE) · airframe 68,558 hrs · 27,036 cycles

RIGHT FIXED WING LEADING EDGE UPPER SURFACE DISBONDED AT WS 397. MAINTENANCE REMOVED DAMAGE ON RIGHT FIXED WING LEADING EDGE UPPER SURFACE WS 397 AND PERFORMED BOND REPAIR PER AWA ER 19-5700-00012-DD4 & 757-200 SRM 51-70-17.

Part: INDICATOR — FAILED (COCKPIT) · airframe 67,327 hrs · 26,571 cycles

SJD - ABORTED TAKEOFF - FLT 0052 - ON TAKEOFF AT SJD EN ROUTE FOR PHX THE CAPTAINS AIRSPEED INDICATOR FAILED, REJECTED TAKEOFF AT 85 KTS. MAINTENANCE PERFORMED BACKFLOW OF STATIC DRAIN LINES, NO MOISTURE NOTED, PERFORMED AIR DATA COMPUTER BITE TEST, SYSTEM OPERATES NORMALLY PER BMM 34-12-00 PG 110-113. WHEN AIRCRAFT ARRIVED IN PHX MAINTENANCE RE-INSPECTED SYSTEM AND CHECKED ALL CONNECTIONS FOR SECURITY. PROBLEM COULD NOT BE DUPLICATED.

Part: SUPPORT ANGLE — CRACKED (NR 1 PYLON) · airframe 67,197 hrs · 26,513 cycles

LCQ - MINOR REPAIR - DURING C-09 CHECK A .625 INCH CRACK WAS FOUND ON NR 1 ENGINE PYLON FORWARD OUTBOARD SUPPORT ANGLE. MAINTENANCE REMOVED CRACKED FORWARD OUTBOARD SUPPORT ANGLE; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE PER DWG 311N5002; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, PARA 7-D.

Part: PAN — CRACKED (FUSELAGE) · airframe 67,197 hrs · 26,513 cycles

DURING C-09 CHECK 3 EACH CRACKS WERE FOUND AT MOUNT HOLES ON EXTERNAL POWER PANEL PAN ASSEMBLY BS 419. MAINTENANCE PERFORMED HFEC INSPECTION TO VERIFY CRACK ENDS; STOP DRILLED CRACKS; RE-ACCOMPLISHED HFEC INSPECTION TO VERIFY CRACKS CONTAINED; PERFORMED WELD REPAIR IAW AWA ER 19-5316-03265-SS2.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 67,197 hrs · 26,513 cycles

DURING C-09 CHECK 3 EACH CRACKS WERE FOUND AT FASTENER HOLES ON CABIN FLOOR SUPPORT ANGLE BETWEEN BS 1200 TO BS 1210, BL 0. MAINTENANCE REMOVED CRACKED FLOOR SUPPORT ANGLE AT BS 1200 TO BS 1210, BL 0; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW B757-200 SRM 53-00-51, PG 214-215 FIG 204.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 67,197 hrs · 26,513 cycles

DURING C-09 CHECK CABIN FLOOR PANEL L-1 WAS FOUND DELAMINATED BEYOND LIMITS. MAINTENANCE FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 144N5330, AND INSTALLED INSERTS IAW AWA ER 19-5322-03267-SS1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 67,197 hrs · 26,513 cycles

DURING C-09 CHECK CABIN FLOOR PANEL T-3 WAS FOUND DELAMINATED BEYOND LIMITS. MAINTENANCE FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG 146N5750, AND INSTALLED INSERTS IAW AWA E.R. 19-5322-03267-SS1.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,197 hrs · 26,513 cycles

DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND AROUND NUT PLATE HOLES ON FLOOR STRINGER IN AFT CARGO COMPARTMENT BS 1500 TO BS 1560, LBL 18 TO RBL 18. MAINTENANCE CUTOUT CORRODED AREAS OF FLOOR STRINGER BS 1500 TO BS 1560, LBL 18 TO RBL 18; FABRICATED REPAIR PLATES AND FILLERS; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-12, PG. 1, FIG. 1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 67,197 hrs · 26,513 cycles

DURING C-09 CHECK CABIN FLOOR PANEL S-6 WAS FOUND DELAMINATED BEYOND LIMITS. MAINTENANCE FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 146N5750, AND INSTALLED INSERTS IAW AWA ER 19-5322-03267-SS1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 67,197 hrs · 26,513 cycles

DURING C-09 CHECK CABIN FLOOR PANEL K-1 WAS FOUND DELAMINATED BEYOND LIMITS. MAINTENANCE FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 144N5330, AND INSTALLED INSERTS IAW AWA ER 19-5322-03267-SS1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 67,197 hrs · 26,513 cycles

DURING C-09 CHECK CABIN FLOOR PANEL M-5 WAS FOUND DELAMINATED BEYOND LIMITS. MAINTENANCE FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG 144N5330, AND INSTALLED INSERTS IAW AWA E.R. 19-5322-03267-SS1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 67,197 hrs · 26,513 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK CABIN FLOOR PANEL K-4 WAS FOUND DELAMINATED BEYOND LIMITS. MAINTENANCE FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG 144N5330, AND INSTALLED INSERTS IAW AWA E.R. 19-5322-03267-SS1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 67,197 hrs · 26,513 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK CABIN FLOOR PANEL N-5 WAS FOUND DELAMINATED BEYOND LIMITS. MAINTENANCE FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 146N5330, AND INSTALLED INSERTS IAW AWA ER 19-5322-03267-SS1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 67,197 hrs · 26,513 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK CABIN FLOOR PANEL P-6 WAS FOUND DELAMINATED BEYOND LIMITS. MAINTENANCE FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 146N5750, AND INSTALLED INSERTS IAW AWA ER 19-5322-03267-SS1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 67,197 hrs · 26,513 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK CABIN FLOOR PANEL K-2 WAS FOUND DELAMINATED BEYOND LIMITS. MAINTENANCE FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 144N5330, AND INSTALLED INSERTS IAW AWA ER 19-5322-03267-SS1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 67,197 hrs · 26,513 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK CABIN FLOOR PANEL M-2 WAS FOUND DELAMINATED BEYOND LIMITS. MAINTENANCE FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG 144N5330, AND INSTALLED INSERTS IAW AWA ER 19-5322-03267-SS1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 67,197 hrs · 26,513 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK CABIN FLOOR PANEL N-2 WAS FOUND DELAMINATED BEYOND LIMITS. MAINTENANCE FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG 146N5330, AND INSTALLED INSERTS IAW AWA E.R. 19-5322-03267-SS1.

Part: STRINGER — CORRODED · corrosion level 2 · airframe 67,197 hrs · 26,513 cycles

DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND AROUND NUT PLATE HOLES ON FLOOR STRINGER IN AFT CARGO COMPARTMENT BS 1280 TO BS 1360, LBL 18 TO RBL 20. MAINTENANCE CUTOUT CORRODED AREAS OF FLOOR STRINGER BS 1280 TO BS 1360, LBL 18 TO RBL 20; FABRICATED REPAIR PLATES AND FILLERS; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-12, PG. 1, FIG. 1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 67,197 hrs · 26,513 cycles

DURING C-09 CHECK CABIN FLOOR PANEL K-3 WAS FOUND DELAMINATED BEYOND LIMITS. MAINTENANCE FABRICATED A NEW REPLACEMENT FLOOR PANEL IAW DWG 146N5330, AND INSTALLED INSERTS IAW AWA E.R. 19-5322-03267-SS1.

Part: SUPPORT ANGLE — CRACKED (WING TO BODY) · airframe 7,197 hrs · 26,513 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK A .75 INCH CRACK WAS FOUND ON SUPPORT BRACKET UNDER RT WING TO BODY FAIRING AT BS 1300, STR 21 RT. MAINTENANCE CUT OUT DAMAGE ON SUPPORT BRACKET UNDER RT WING TO BODY FAIRING AT BS 1300, STR 21 RT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-60-71, PG 203 FIG 202.

Part: SUPPORT ANGLE — CRACKED (WING TO BODY) · airframe 67,197 hrs · 26,513 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK A 1.25 INCH CRACK WAS FOUND ON SUPPORT BRACKET UNDER RT WING TO BODY FAIRING AT BS 1300, STR 25 RT. MAINTENANCE CUT OUT DAMAGE ON SUPPORT BRACKET UNDER RT WING TO BODY FAIRING AT BS 1300, STR 25 RT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-60-71, PG 203 FIG 202.

Part: SLIDE — BINDING (PAX DOOR) · airframe 66,294 hrs · 26,113 cycles

FLIGHT CREW REPORTED THE R-1 DOOR EVACUATION SLIDE ARMING LEVER WAS BINDING. MAINTENANCE REMOVED AND REPLACED THE R-1 DOOR EMERGENCY EVACUATION SLIDE IAW AWA T/C R1C25602, OPERATIONAL CHECK OF R-1 DOOR ARMING LEVER WAS NORMAL. VENDOR OVERHAULED SLIDE, TEARDOWN REPORT DESCRIBED ONLY PARTS ON PACKING LIST, NO MENTION OF DISCREPANCIES.

Part: FAN — OVERHEATED (ZONE 821) · airframe 63,025 hrs · 24,714 cycles

BURNING SMELL - EN ROUTE OBSERVED A STRONG ELECTRICAL ODOR IN FLT DECK WITH EXCESSIVE HEAT, UNABLE TO LOCATE SOURCE, NO C/B POPPED. MX DISCOVERED EQUIPMENT COOLING FAN NR 2 CIRCUIT BREAKER POPPED. COLLARED CIRCUIT BREAKER AND PLACED ON MEL 21-58-3, COND 1, ONE FWD EQUIPMENT COOLING FAN INOP. MX REMOVED AND REPLACED EQUIPMENT COOLING FAN IAW BMM 21-58-06, AND FORWARD EQUIPMENT EXHAUST SMOKE DETECTOR (TS164) IAW BMM 21-58-19-201; OPS CHECKS GOOD. *S/D* VENDOR TEARDOWN OF EQUIPMENT COOLING FAN (AXIAL FLOW) S/N 0706 CONFIRMED FAILURE OF UNIT. TEARDOWN REVEALED THE MOTOR BEARING WAS SHATTERED & FAN CONTACTED CASE HOUSING. UNIT REPAIRED & TESTED IAW OHM 21-58-15. NO PART REPLACED, INFO SUPPLIED BY VENDOR.

Part: HOSE — RUPTURED (ZONE 700 - LANDI) · corrosion level 0 · airframe 63,025 hrs · 2,471 cycles

PHX - NOSE WHEEL STEERING FAILURE - FLT 0716 - AFTER NORMAL LANDING AT PHX EN ROUTE FROM LAS NOSE WHEEL STEERING FAILED ON TAXIWAY, AND L/H HYDRAULIC QUANTITY DECREASED TO ZERO WITH SYSTEM PRESSURE LIGHT ILLUMINATED. EICAS MESSAGE FOR L/H HYDRAULIC SYSTEM DISPLAYED. AIRCRAFT REQUIRED TOW TO GATE. MAINTENANCE FOUND L/H LANDING GEAR DOWN LOCK ACTUATOR FLEX LINE RUPTURED. REMOVED AND REPLACED L/H LANDING GEAR DOWN LOCK ACTUATOR FLEX LINE; LEAK CHECK COMPLIED WITH IAW BMM 32-32-02, PG. 407, STEP 11 & 12.

Part: RESERVOIR — LEAKING (EMERGENCY DOOR) · airframe 65,299 hrs · 25,674 cycles

DURING INSPECTION THE L-2 DOOR EMERGENCY POWER RESERVOIR WAS FOUND TO HAVE LOW PRESSURE. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR EMERGENCY POWER RESERVOIR IAW BMM 52-11-30, LEAK AND OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (LAV FLASHLIGHT) · airframe 64,816 hrs · 25,440 cycles

FLIGHT CREW REPORTED EMERGENCY FLASHLIGHT BATTERIES DEPLETED AT FLIGHT ATTENDANT STATION 2 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.

Part: TRANSCEIVER — SHORTED (WEATHER RADAR) · airframe 64,535 hrs · 25,333 cycles

BWI - AIR TURN BACK - FLT 0083 - EN ROUTE FROM BWI TO LAS A WEATHER RADAR FAIL MESSAGE APPEARED INTERMITTENTLY FOLLOWED BY A STRONG ELECTRICAL BURNING SMELL. DUE TO WEATHER EN ROUTE AIRCRAFT TURNED BACK TO BWI. MAINTENANCE REMOVED AND REPLACED THE WEATHER RADAR R/T UNIT IAW 34-43-01. OPERATIONAL CHECK WAS GOOD.

Part: SMOKE DETECTOR — FAILED (LAVATORY) · airframe 63,971 hrs · 25,106 cycles

FLT 0051 - RETURNED TO GATE DUE TO STRONG ELECTRICAL ODOR COMING FROM THE FORWARD LAVATORY. MAINTENANCE IDENTIFIED BURNING ODOR WAS COMING FROM FORWARD LAVATORY SMOKE DETECTOR. REMOVED AND REPLACED SMOKE DETECTOR, OPERATIONAL CHECK GOOD PER BMM 26-14-00.

Part: WIRE — BROKEN (SEAT ROW 18 L/H) · corrosion level 0 · airframe 63,067 hrs · 24,733 cycles

PHX - EEL - DURING INSPECTION SEAT ROW 18 L/H EMERGENCY EXIT PATH LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED LIGHT BULB, DID NOT CORRECT THE PROBLEM, FOUND BROKEN WIRE AT SEAT ROW 18 L/H, REPAIRED BROKEN WIRE PER BOEING SWP 20, OPERATIONAL CHECK WAS GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 63,025 hrs · 24,714 cycles

AMS - EEL - DURING C-08 CHECK SEAT ROW 6 LT WAS FOUND TO HAVE A MISSING EMERGENCY ESCAPE PATH LIGHT. MAINTENANCE INSTALLED 1 WHITE EMERGENCY ESCAPE PATH LIGHT AT ROW 6, OPS CHECK GOOD REF MM 33-51-00 PG 501.

Part: STRINGER — CRACKED · corrosion level 0 · airframe 63,025 hrs · 24,714 cycles

GYR - MAJOR REPAIR - DURING C-08 CHECK A 3/8" CRACK WAS FOUND AT FASTENER HOLE ON STRINGER 15 L/H, BS 590. MAINTENANCE CUTOUT DAMAGED AREA OF STRINGER, FABRICATED 2 EACH REPAIR ANGLES & CHANNELS, AND 1 EACH SHIM & FILLER, AND INSTALLED REPAIRS IAW SRM 53-00-03, FIG 201, PG. 201-209.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,025 hrs · 24,714 cycles

MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON FLOORBEAM TEE CAP AT BS 345, BL 0 TO LBL 23.0. MAINTENANCE CLEANED CORROSION OFF FLOORBEAM AND FOUND MATERIAL REMAINING TO BE OUT OF LIMITS IAW B757-200 SRM 53-00-51. REMOVED DAMAGED SECTION OF FLOORBEAM FROM LBL 01 TO LBL 23, FABRICATED 2 EACH REPAIR ANGLES AND 1 EACH REPAIR FILLER AND INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-51, FIG 205, SHT 3, DETAIL I, PG. 218.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,025 hrs · 24,714 cycles

GYR - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT BEAM AT BS 377, LBL 45 TO LBL 60. REMOVED DAMAGED SECTION OF FLOORBEAM, FABRICATED AND INSTALLED REPAIR IAW B757-200 SRM 53-10-51, AND SRM 51-21-1, FIG 203, PG 210.

Part: TRACK — CORRODED · corrosion level 2 · airframe 63,025 hrs · 24,714 cycles

GYR - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 398, RBL 45.0. MAINTENANCE REMOVED DAMAGED SECTION OF FLOOR SUPPORT BETWEEN BS 363 AND BS 415, RBL 45, FABRICATED NEW SECTION OF FLOOR SUPPORT AND INSTALLED REPAIR IAW B757-200 SRM 51-40-0, AND SRM 53-10-51, PG. 1-6.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,025 hrs · 24,714 cycles

DURING C-08 CHECK CORROSION WAS FOUND ON TOP AND BOTTOM OF FLOORBEAM UPPER CHORD AT BS 365, BL 0 TO RBL 62.0. FABRICATED NEW SECTION OF UPPER CHORD AND INSTALLED NEW CHORD.

Part: WIRE — SHORTED (ROW 18L) · airframe 60,402 hrs · 23,679 cycles

SEAT MOUNTED EMERGENCY PATH LIGHTING INOP IN MID CABIN; APPROX 8 ROWS. FOUND FUSE BLOWN IN AFT POWER SUPPLY AND DIODE BLOWN IN DIODE PANEL; WIRE SHORTED TO GROUND AT ROW 18; REPLACED FUSE, DIODE AND REPAIRED WIRE AT ROW 18; OPS CHECKS GOOD.

Part: WIRE — BROKEN (ROW 29 - 31) · airframe 58,422 hrs · 22,816 cycles

NON ROUTINE LINE, EMERGENCY LIGHTS NOT WORKING AT ROW 29 AND 31. FOUND WIRES CUT AND STOWED AT ROW 29 AND WIRE NOT CONNECTED TO CONNECTOR AT ROW 31. REPAIRED WIRING AT ROW 29 AND 31, OPS CHECK GOOD.

Part: SEAL — LEAKING (COCKPIT WINDOW) · airframe 57,761 hrs · 22,559 cycles

AIR TURNBACK-- F/O''S WINDOW LEAK. LOUD SQUEAL PASSING 1700 FT SOUNDED LIKE PRESSURE LEAK, SQUEAL STOPPED IN DESCENT AT 6 PSI. REMOVED AND REPLACED PRESSURE SEAL AT F/O NR 2 WINDOW, LEAK CK GOOD. CURRENT HISTORY: DEBRIS CLEANED FROM SEAL FOR SIMILAR WRITE-UPS, FLIGHT PRIOR AND 8/06/99 SEE LP 7571030 AND 7470337. RECOMMENDATION: REMAIN OPEN AND MONITOR.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,740 hrs · 22,551 cycles

C-CHECK, CRACKED FLOOR SUPPORT STA 687 RBL 2.5 WL 155. REMOVED AND REPLACED FLOOR SUPPORT AT STA 630 - 840 WL 155 LBL 2.5. ALL WORK DONE IAW 757-200 SRM 51-40-2 AND 51-20-01.

Part: PAN — CRACKED (COCKPIT SEAT) · airframe 57,740 hrs · 22,551 cycles

C-CHECK, 2ND OBSERVERS SEAT FWD LT LOWER CORNER CRACKED UNDERSIDE. REMOVED SEAT, FABRICATED AND INSTALLED REPAIR PARTS IN FWD LT LWR CORNER AND RE-INSTALLED SEAT IAW ER 19-2511-00086-JS2 AND 757 MM 25-11-01.

Part: PAN — CRACKED (COCKPIT SEAT) · airframe 57,740 hrs · 22,551 cycles

C-CHECK, 2ND OBSERVERS SEAT AFT RT AND LT HINGE BRACKETS CRACKED. REMOVED SEAT, FABRICATED AND INSTALLED REPAIR PARTS AND RE-INSTALLED 2ND OBSERVERS SEAT IAW ER 19-2511-00086-JS2 AND 757 MM 25-11-01.

Part: BRACKET — CRACKED (COCKPIT SEAT) · airframe 57,740 hrs · 22,551 cycles

C-CHECK, F/O SEAT AFT LOWER WEB BRACKETS ARE CRACKED. REMOVED CRACKED BRACKETS USING AS TEMPLATE, FABRICATED 2 BRACKETS .040 2024T3, ALODINED, PRIMED, AND PAINTED IAW 737 SRM 51-20-01 AND 737 MM 51-21-00. INSTALLED PARTS IAW 737 SRM 51-40-02.

Part: BEAM — CRACKED (LT MLG WW) · airframe 57,740 hrs · 22,551 cycles

C-CHECK, LT MLG WHEEL WELL CANTED BEAM IS CRACKED. CRACKS ON LT MLG WHEEL WELL CANTED BEAM REPAIRED IAW EO 53-10-13 FIG 3.

Part: BEAM — CRACKED (RT MLG WW) · airframe 57,740 hrs · 22,551 cycles

C-CHECK, RT MLG WHEEL WELL CANTED BEAM IS CRACKED. CRACKS ON RT MLG WHEEL WELL CANTED BEAM REPAIRED IAW EO 53-10-13 FIG 3.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,740 hrs · 22,551 cycles

C-CHECK, CRACKED FLOOR SUPPORT STA 687 LBL 2.5 WL 155. REMOVED AND REPLACED FLOOR SUPPORT AT STA 630 - 840 LBL 2.5. ALL WORK DONE IAW 757-200 SRM 51-40-2 AND 51-20-1.

Part: CHARGER — FAILED (ROW 10 - 18)

EMERGENCY LIGHTS ROWS 10-18 INOP. REPLACED FWD BATTERY CHARGER AND BATTERY. REPAIRED WIRES AT ROWS 10 AND 13. RELAMPED ALL OTHERS (WIRE BMS 13-13-1/1-22).

Part: FASTENER — SHEARED (RT PYLON)

DURING ENGINE CHANGE SEVERAL FASTENERS ON THE PYLON ATTACH FITTING, WHERE THE DIAGONAL WING BRACE ATTACHES WERE LOOSE AND 2 WERE SHEARED. ACTION IS CURRENTLY BEING EVALUATED FOR DISPOSITION AND REPAIR.

Part: SWITCH — LEAKING (LT HYD SYS)

EMERGENCY LANDING, LT SYS QTY ZERO. PERFORMED QRH PROCEDURES, PRESS REMAINED IN L/G SYS. FOUND PRESS SWITCH LEAKING. REMOVED AND REPLACED PRESS SWITCH AND UNION AS REQUIRED. RESERVICED, LEAK CHECKED OK.

Part: HYD PUMP — FAILED (LT ENGINE)

LT HYD SYS FAILED, RT MLG DID NOT EXTEND NORM. LT HYD QTY DROPPED TO .11. CYCLED OFF BOTH ELECT AND ENG PUMPS. GEAR GREEN DOWN LIGHT FAILED TO ILLUM WITH GEAR HANDLE DOWN. EICAS MESSAGE, GEAR DISAGREE, GEAR DOOR DISPLAY DOOR AND GEAR AMBER LIGHTS ILLUM. ALTERNATE GEAR EXTENSION ATTEMP. FOUND LT ENG DRIVEN PUMP CASE DRAIN QD OFF AT PUMP. R&R'D LT ENG DRIVEN PUMP AND LT AC MOTOR PUMP. ALSO CHANGED MLG ALTERNATE UPLOCK ACTUATOR AND RT MAIN GEAR DOOR SEQUENCE VALVE.

Part: FAN — FAILED (LEFT)

ENROUTE TO BOS LEFT RECIRC INOP LIGHT AND LEFT RECIRC FAN STATUS MESSAGE APPEARED. A SLIGHT ELECTRICAL ODOR WAS NOTED BUT NO SMOKE. SELECTED LEFT RECIRC FAN OFF AND PULLED LEFT RECIRC CB. ODOR DISAPPEARED. REMOVED AND REPLACED LEFT RECIRC FAN. OPS CHECK GOOD.

Part: SUPPORT — CORRODED (BS 367-375)

DURING SCHEDULED C-6 INSPECTION, FOUND FWD CABIN STATION 367 - 375 LBL 60 FLOOR SUPPORT CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-10-00.

Part: SUPPORT — CORRODED (BS 324-365.25)

DURING SCHEDULED C-6 INSPECTION, FOUND FLOOR SUPPORT CHANNEL AT NR 1 R CABIN SERVICE DOOR, BETWEEN BS 324 TO 365.25 RBL 62L, CORRODED WITH HOLES AND CORROSION ON TOP SURFACE (CHANNEL IS TWO PIECES). REMOVED AND REPLACED FLOOR SUPPORT CHANNELS PER SRM 51-10-00.

Part: SUPPORT — CORRODED (BS 330)

DURING SCHEDULED C-6 INSPECTION, FOUND FWD CABIN FLOOR SUPPORT AT STA 330, RBL 5 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-40-02.

Part: SUPPORT — CORRODED (BS 345-365)

DURING SCHEDULED C-6 INSPECTION, FOUND FWD CABIN STATION 345 - 365 RBL - 0 FLOOR SUPPORT CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-40-02.

Part: CHANNEL — CORRODED (BS 335-345)

DURING SCHEDULED C-6 INSPECTION, FOUND FWD CABIN STATION 335 - 345 LBL 60 FLOOR CHANNEL CORRODED. REMOVED AND REPLACED FLOOR CHANNEL PER 51-10-00.

Part: CONNECTOR — FAILED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND AFT SECTION OF EMERGENCY EXIT LIGHTS INOP ON SEATS AND DOORS. REMOVED AND REPLACED FUSE ON POWER SUPPLY AND REPAIRED CONNECTOR AT L-4 DOOR, OPS CHECK NORMAL.

Part: COFFEE MAKER — MALFUNCTIONED (CABIN)

FOUND CM-8 COFFEE MAKER SMOKED AND C/B PULLED. REMOVED AND REPLACED CM-8 COFFEE MAKER. OPS CHECK NORMAL.

Part: WIRE — DISCONNECTED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT MOUNTED EMERGENCY LIGHTS INOP AT ROW 5 AND 17. CONNECTED AND SECURED WIRES, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT SEAT LIGHT INOP AT ROW 11 LEFT. REPLACED SEAT LIGHT ASSEMBLY, OPS CHECK GOOD.

Part: CREASE BEAM — CORROSION (BS 1320-1350)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION AROUND NUTPLATE HOLES IN DOOR CREASE BEAM CHORD BS 1320 TO 1350, RBL 625, WL 208. FOUND BLEND OUT AREAS TO BE WITHIN LIMITS PER ER 5-53-15-02, TCO-PAN-97-0346RR.

Part: STRINGER — CORRODED (BS 1330)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION AROUND NUTPLATES ON FLOOR STRINGER AT BS 1330, LBL 16, WL 158. FABRICATED NEW EXTRUSION, ANGLES AND INSTALLED AT BS 1330, LBL 16, WL 158.

Part: STRINGER — CORRODED (BS 1330-1340)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION AROUND NUTPLATES ON FLOOR STRINGER AT BS 1330 TO 1340, LBL 7, WL 158. FABRICATED REPLACEMENT STRINGER, ANGLES AND INSTALLED AT BS 1290 TO 1344, LBL 7, WL 158 PER SRM 51-70-12.

Part: STRINGER — CORRODED (BS 1330-1344)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR STRINGER AROUND NUTPLATES AT BS 1330 TO 1340, RBL 16, WL 158. REPAIRED FLOOR STRINGER BS 1290 TO 1344, RBL 16 PER SRM 51-70-12.

Part: STRINGER — CORRODED (BS 1510)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR STRINGER AROUND NUTPLATES AT BS 1510, LBL 12, WL 156. FABRICATED REPAIR STRINGER, ANGLES AND INSTALLED AT BS 1494 TO 1549, LBL 12, WL 156 PER SRM 51-70-12.

Part: STRINGER — CORRODED (BS 1510)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR STRINGER AROUND NUTPLATES AT BS 1510, LBL 2, WL 156. REMOVED, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 51-70-12.

Part: SUPPORT — CORRODED (BS 1380)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON UPPER SURFACE OF AFT CARGO DOOR FLOOR SUPPORT AT BS 1380 TO 1440, RBL 20, WL 158. REMOVED AFT CARGO DOOR FLOOR SUPPORT, FABRICATED NEW FLOOR SUPPORT AND INSTALLED AT BS 1380 TO 1440, RBL 20, WL 158 PER SRM 51-30-01, 53-60-53, 51-40-02.

Part: SUPPORT — CORRODED (BS 1430-1520)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION AROUND NUTPLATES ON FLOOR/SIDEWALL SUPPORT BS 1430 TO 1520, LBL 20, WL 158. FABRICATED REPAIR DOUBLERS, FILLERS AND INSTALLED PARTS AT BS 1430 TO 1520, LBL 20, WL 158 PER ER 5-53-10-01 AND SRM 51-70-13.

Part: STRINGER — CORRODED (BS 1330)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR STRINGER AROUND NUTPLATES AT BS 1330, LBL 2, WL 158. FABRICATED AND INSTALLED NEW FLOOR STRINGER AT BS 1330, LBL 2, WL 158 PER SRM 51-70-12.

Part: STRINGER — CORRODED (BS 1481)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR STRINGER AROUND NUTPLATES AT BS 1481, LBL 16, WL 156. REPAIRED FLOOR STRINGER AT BS 1981 IAW SRM 53-00-53.

Part: PANEL — CORRODED (BS 1440-1530)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON UPPER SURFACE RT FLOOR SUPPORT AT BS 1440 TO 1520. REMOVED AND REPLACED FLOOR SUPPORT FROM BS 1440 TO 1530, RBL 17 PER SRM 51-40-02.

Part: STRINGER — CORRODED (BS 1330-1340)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR STRINGER AROUND NUTPLATES AT BS 1330 TO 1340, RBL 7, WL 158. REPAIRED FLOOR STRINGER PER SRM 51-70-12 AT BS 1330 TO 1340, RBL 7, WL 158.

Part: STRINGER — CORRODED (BS 1343-1363)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR STRINGER AT BS 1343 TO 1363, RBL 16, WL 158. CUT EXISTING STRINGER AT BS 1353 AND REMOVED SPLICE AT BS 1368. FABRICATED NEW SECTION OF STRINGER AND INSTALLED FROM PRODUCTION SPLICE AT BS 1368 TO REPAIR SPLICE AT 1343 PER SRM 51-70-12.

Part: STRINGER — CORRODED (BS 1343-1360)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR STRINGER AT BS 1343 TO 1360, RBL 11, WL 158. REMOVED CORRODED STRINGER FROM BS 1343 TO 1360. FABRICATED STRINGER AND INSTALLED IAW SRM 51-70-1, SRM 53-00-53.

Part: STRINGER — CORRODED (BS 1330-1340)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR STRINGER AROUND NUTPLATES AT BS 1330 TO 1340, RBL 11, WL 158. FABRICATED AND INSTALLED NEW FLOOR STRINGER AT BS 1290 TO 1340, RBL 11 PER SRM 51-40-02, 51-70-12, RIG 1.

Part: STRINGER — CORRODED (BS 1330)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR STRINGER AROUND NUTPLATES AT BS 1330, RBL 2, WL 158. INSTALLED FABRICATED REPLACEMENT FLOOR STRINGER AND REPAIR PARTS (SPLICES) FROM BS 1328 TO 1343, RBL 2, WL 158 WET WITH SEALANT, INSTALLED PER SRM 51-70-12.

Part: STRINGER — CORRODED (BS 1330)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION AROUND NUTPLATES ON FLOOR STRINGER AT BS 1330, LBL 11, WL 158. REMOVED, FABRICATED AND INSTALLED STRINGER BS 1290 TO BS 1340 IAW SRM 51-70-02 AND SRM 53-00-53.

Part: STRINGER — CORRODED (BS 1510)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR STRINGER AROUND NUTPLATES AT BS 1510, LBL 7, WL 156. REMOVED, FABRICATED REPAIR PARTS PER SRM 51-70-12 AND INSTALLED.

Part: SUPPORT — CORRODED (BS 1590)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT IN AFT CARGO BAY BS 1590, LBL 17, WL 155. REMOVED FLOOR TO SIDEWALL SUPPORT FROM BS 1530 TO 1640, LBL 17. REPAIRED AREA AT BS 1564 TO 1569, LBL 13 AND REINSTALLED FLOOR TO SIDEWALL PER SRM 51-70-13 AND 51-40-02.

Part: STRINGER — CORRODED (BS 1510)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR STRINGER IN AFT CARGO BAY AT BS 1510, RBL 7, WL 156. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 51-70-12.

Part: SUPPORT — CORRODED (BS 1470)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR SUPPORT STRUCTURE BS 1470, RBL 12, WL 157. REMOVED, FABRICATED NEW FLOOR SUPPORT AND INSTALLED AT BS 1458 TO 1480, RBL 12, WL 157 PER SRM 53-60-53, 51-40-02.

Part: SUPPORT — CORRODED (BS 1310-1410)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 1310 TO BS 1410, LBL 20, WL 158. REMOVED DAMAGED MATERIAL, FABRICATED REPAIR PART IAW, SRM 51-40-02 AND SRM 51-70-13.

Part: SUPPORT — CORRODED (BS 1520-1570)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 1520 TO 1570, RBL 17, WL 155. REPAIRED FLOOR TO SIDEWALL SUPPORT PER SRM 51-70-13.

Part: STRINGER — CORRODED (BS 1510)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR STRINGER AT BS 1510, RBL 2, WL 156. REMOVED, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 51-70-12.

Part: STRINGER — CORRODED (BS 1564-1570)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON CARGO BAY FLOOR STRINGER BS 1564 TO 1570 RBL 2 WL 152. REMOVED, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 51-70-12.

Part: DOWNLOCK PIN — NOT REMOVED (NLG)

AIR TURNBACK, AFTER DEPARTURE RECEIVED GEAR DISAGREE AND GEAR DOORS EICAS MESSAGE. BURNED FUEL DOWN TO 46,000 LBS. LANDED OVERWEIGHT AT 220000 LBS. FOUND DOWNLOCK PIN INSTALLED IN NOSE GEAR. REMOVED DOWNLOCK PIN, PERFORMED OVERWEIGHT INSPECTION PER CARD I8M51601 WITH NO DISCREPANCIES FOUND.

Part: SWITCH — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY TEST BUTTON ON FORWARD CSR SEAT INOPERATIVE. REMOVED AND REPLACED THE FORWARD ATTENDENT'S PANEL EMERGENCY LIGHT SWITCH, SYSTEM OPERATIONS CHECKED NORMAL.

Part: SWITCH — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY TEST BUTTON ON FWD CSR SEAT INOPERATIVE. REMOVED AND REPLACED THE FWD ATTENDANT'S PANEL EMERGENCY LIGHT SWITCH, SYSTEM OPERATIONS CHECK NORMAL.

Part: WIRE — BROKEN (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT 31 A, B, C EMERGENCY LIGHT INOPERATIVE. RECONNECTED WIRING, OPERATIONS CHECK GOOD.

Part: PIN — UNSEATED (CABIN)

PHX - FLT 25 - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 32 R SEAT MOUNTED EMERGENCY LIGHT INOP. FOUND PIN NOT SEATED AT SEAT 32C. RESEATED PIN. OPERATIONS CHECK GOOD. (M)

Part: LATCH CAM — OUT OF RANGE (AFT ENTRY DOOR)

LAS - FLT 6 - LEFT AFT ENTRY DOOR EICAS LIGHT ILLUMINATED MOMENTARILY. FLIGHT ATTENDANT NOTED, HANDLE CAME WAY UP AND HAD TO BE MANUALLY PUSHED DOWN TWICE. FOUND UPPER AFT LATCH CAM OUT OF ADJUSTMENT. ADJUSTED LATCH CAM PER 757 BMM 52-11-00. OPS CHECK GOOD, DOOR NOW NORMAL. SRTC ISSUED. CHECKED THE DOOR RIG PER 52-11-00, PAGE 501 AND THE DOOR IS RIGGED PROPERLY AS FAR AS WE CAN SEE WITH NO OBVIOUS DEFECTS. THE DOOR HANDLE OVER CENTER FORCE IS APPROXIMATELY 32 POUNDS. WHEN PRESSURIZED, THE A/C OVERCENTER HANDLE FORCE WAS LIGHTER, BUT IT WAS STILL VERY FIRM IN THE OVER CENTER POSITION. (M)

Part: PROX SENSOR — OUT OF LIMITS (LT AFT DOOR)

PHX - FLT FLT 9 - ON DESCENT AT 500 FEET, LEFT AFT DOOR EICAS MESSAGE. READJUSTED THE DOOR PROX SENSOR, IT WAS OUT OF LIMITS. OPS CHECK GOOD. (M)

Part: GUIDE ARM — OUT OF ADJUST (ENTRY DOOR)

PHX - FLT 9 - L-4 ENTRY DOOR LIGHT ILLUMINATED IN FLIGHT. ADJUSTED L-4 GUIDE ARM AND SERRATED PLATE PER BMM 52-11-04. PRESSURIZED A/C AND RAN ENGINES TO P/POWER. DOOR IS SECURE, NO WARNING LIGHTS. (M)

Part: FLEX LINE — RUPTURED (RT MLG)

PHX - FLT 2068 - PHX-LAS - AIR TURNBACK, HYDRAULIC QUANTITY LOSS. RIGHT GEAR DOWNLINE RUPTURED. INSTALLED TEMPORARY FLEX LINE AND SERVICED SYSTEM. PLACED ON 106, DMI NR 28375 TO BE REPLACED BY PERMANENT LINE WITHIN 25 DAYS. (M)

Part: DOOR SLIDE — FELL OFF (L-2 DOOR)

LAS - FLT 292 - L-2 SLIDE FELL OFF DURING FLIGHT. REHUNG L-2 DOOR SLIDE. (M)

Part: FLOOR BEAM — CORRODED (BS 1681)

PAE - FLT NR 1018 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION OUT OF LIMITS UPPER CHORD OF FLOOR BEAM, BS 1681 RBL 15 - LBL 53. REPAIRED FLOOR BEAM IAW TRAMCO EWO 95-4073, MWO INTERIOR 151 AND 152. (M)

Part: FLOOR BEAM — CORRODED (BS 1640)

PAE - CORROSION OUT OF LIMITS ON FLOOR BEAM UPPER CHORD BS 1640, RBL 59-BLQ, WL 208 SEVERAL AREAS. REPAIRED FLOOR BEAM IAW 53-00-51 (MWO INTERIOR 134). (M)

Part: FLOOR BEAM — CORRODED (BS 1661)

PAE - FOUND CORROSION OUT OF LIMITS, FLOOR BEAM UPPER CHORD BS 1661 LBL 56-RBL 56, WL 208. REPAIRED FLOOR BEAM IAW SRM 53-00-51 (MWO INTERIOR 122). (M)

Part: EEL BATT PACKS — DISCHARGED (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT L1, L4, R2 AND R3 DOORS. REMOVED AND REPLACED BATTERY PACKS AT M737, M734, M733 AND M731. OPS CHECK GOOD. (M)

Part: ENGINE — MALFUNCTIONED (NR 1)

PHX - FLT 91 - ON TAKEOFF, THE LT EEC LIGHT AND LT ENGINE LIMITER LIGHT ILLUMINATED AFTER NR 1 ENG START, UMSR ISSUED. REDUCED TAKEOFF EPR OF 1.54, THE NR 1 ENG EGT ENTERED CAUTION RANGE OF 805 DEGREES. FUEL FLOW ON NR 1 ENG 1400 LBS HIGHER THAN NR 2 ENG. AC RETURNED TO PHX WITHOUT FURTHER PROBLEMS. MX REMOVED AND REPLACED THE NR 1 ENG PER AWA TASK CARD R5M71601. ENGINE TEST RUNS GOOD AND AC RETURNED TO SERVICE. (W)

Part: FFG — FAILED (NR 1 ENG)

PHX - FLT 696 - AT ROTATION, THE NR 1 ENGINE EGT WENT TO 878 DEGREES. CREW RETARDED THRUST LEVER TO KEEP EGT BELOW RED LINE. AIRCRAFT RETURNED TO PHX WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 1 ENG FFG. LEAK AND OPERATION CHECKS NORMAL. AIRCRAFT RELEASED FOR FURTHER SERVICE. (M)

Part: TPU — FAILED (NR 1 ENG)

PHX-LAX - FLT NR 20 - CREW ABORTED TAKEOFF DUE TO HIGH EGT ON NR 1 ENGINE. OAT 101 DEGREES, EPR 1.66, EGT 852 DEGREES AND CLIMBING. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 ENG TRANSIENT PRESSURE UNIT (TPU) PER BMM 75-32-15. NO FAULTS NOTED. AS A PRECAUTIONARY MEASURE, THE NR 1 ENGINE EPR TRANSMITTER WAS ALSO REMOVED AND REPLACED. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. REF RECORD NR AWX9500516.

Part: EPR TRANSMITTER — MALFUNCTIONED (NR 1 ENG)

PHX-LAX - FLT NR 20 - CREW ABORTED TAKEOFF DUE TO HIGH EGT ON NR 1 ENGINE. OAT 101 DEGREES, EPR 1.66, EGT 852 DEGREES AND CLIMBING. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 ENG TRANSIENT PRESSURE UNIT (TPU) PER BMM 75-32-15. NO FAULTS NOTED. AS A PRECAUTIONARY MEASURE, THE NR 1 ENGINE EPR TRANSMITTER WAS ALSO REMOVED AND REPLACED. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: HYD LINE — LEAKING (LT MLG)

PHX\JFK - FLT 290 - AIR TURNBACK, DURING CLIMB-OUT, CREW REPORTED EICAS 'L HYD QTY' MESSAGE. CREW VERIFIED QTY WAS DROPPING QUICKLY WITH DECREASING PRESSURE. DURING RETURN TO PHX, CREW REPORTED EICAS 'POWER XFER UNIT' MESSAGE. CREW DECLARED EMERGENCY, LANDING WITHOUT FURTHER INCIDENT. AIRCRAFT WAS TOWED FROM RUNWAY TO GATE. MAINTENANCE REPLACED HIGH PRESSURE DOWNLOCK ACTUATOR LINE AT LT MLG. LEAK CHECK COMPLIED WITH. AIRCRAFT RELEASED FOR SERVICE. (X)