N901AW

Part: PUMP — INOPERATIVE (FUEL SYSTEM) · airframe 102,295 hrs · 35,462 cycles

THE FLIGHT DIVERTED DUE TO LT CTR FUEL PUMP INOPERATIVE & ASSOCIATED PRESS EICAS MSG. R & R LT CTR FUEL BOOST PUMP IAW AMM 28-22-03.

Part: RIVET — LOOSE (GIRT BAR) · airframe 101,463 hrs · 35,290 cycles

L4 DOOR EVACUATION SLIDE GIRT BAR SLIDER LOOSE AT RIVET. REPLACED RIVETS IAW SRM 51-42-11.

Part: SLIDE — LOW PRESSURE (L4 DOOR) · airframe 101,463 hrs · 35,290 cycles

L4 DOOR SLIDE PRESS LOW. REPLACED L4 DOOR SLIDE IAW 19L80025002.

Part: SNUBBER — WORN (L4 DOOR)

DOOR L4 ROTARY SNUBBER MINIMUM WEAR PIN EXTENSION IS NOT CORRECT. REPLACED DOOR L4 ROTARY SNUBBER.

Part: STRAP — CRACKED (FUSELAGE) · airframe 100,506 hrs · 35,101 cycles

C4 CHECK, STABILIZER STRAP CRACKED. FABRICATED REPAIR PARTS & INSTALLED REPAIR DOUBLER PLATES IAW EA 106499.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,506 hrs · 35,101 cycles

C4 CHECK, RT CREASE BEAM INNER CHORD IS CORRODED ON UPPER & LOWER SURFACES. INSTALLED FABRICATED REPAIR PARTS IAW SRM 51-40-02 & DWG 146N8322.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,506 hrs · 35,101 cycles

CORROSION ON MAIN DECK SUPPORT STRUCTURE BY R1 DOOR. REMOVED, FABRICATED & INSTALLED NEW FLOOR SUPPORT IAW DWG 141N5186 & SRM 51-40-02.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 100,506 hrs · 35,101 cycles

C4 CHECK, CRACKED T CLIP AT STATION 960, STRINGER 7R. REPLACED T CLIP IAW DWG 140N2001.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 100,506 hrs · 35,101 cycles

C4 CHECK, VERTICAL ANGLE CRACKED BELOW FLOORBEAM. FABRICATED & INSTALLED NEW ANGLE IAW DWG 143N5532 & SRM 51-10-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,506 hrs · 35,101 cycles

C4 CHECK CORROSION ON FLOORBEAM AT STATION 365.25 BETWEEN RBL 38 & 50. REPLACED FLOORBEAM UPPER T CAP IAW SRM 53-00-51-2R.

Part: PANEL — DELAMINATED (ZONE 300) · airframe 100,506 hrs · 35,101 cycles

C4 CHECK, RT SIDE OF VERTICAL STABILIZER TORQUE BOX PANEL ON INSIDE SKIN IS DELAMINATED. R & R TORQUE BOX PANEL IAW SRM 51-40 & DWG 175N2001-4.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 100,506 hrs · 35,101 cycles

C4 CHECK, FUSELAGE FRAME REPAIR DOUBLER GOUGED IN TWO PLACES ABOVE FLOOR RT SIDE. THE REPAIR DOUBLER WAS REMOVED & FRAME REPAIRED IAW SRM 53-00-07-2R-1.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 100,506 hrs · 35,101 cycles

C4 CHECK, ANGLE CRACKED ON UPPER SIDE OF L1 ENTRY DOOR WEB CUT OUT. REPLACED ANGLE IAW SRM 51-10-02 & DWG 141N-8321.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 100,506 hrs · 35,101 cycles

C4 CHECK, CRACKED ANGLE ON UPPER SIDE OF FWD ENTRY DOOR TOP CUT OUT WEB. R & R FABRICATED ATTACH ANGLE IAW DWG 141N8321 & SRM 51-10-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,506 hrs · 35,101 cycles

C4 CHECK, CORROSION ON INTERCOSTAL BY R1 DOOR FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51-1A. INSTALLED NEW PART IAW SRM 51-10-02.

Part: PANEL — CRACKED (LE SLAT) · airframe 100,506 hrs · 35,101 cycles

C4 CHECK, NR 9 SLAT COVE PANEL BETWEEN OTBD MAIN TRACK LUG & AUX TRACK IS CRACKED AROUND FASTENER THAT MEASURED 2.125 INCH CRACK FROM COVE PANEL FASTENER, 2'6 INCHES FROM OTBD END & 1'1 INCH FROM TE. FABRICATED NEW COVE PANEL IAW DWG 141N4076. COMPLETED INSTALLATION OF COVE PANEL IAW DWG 114N4003 & SRM 51-10-02 PAR 9.

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 100,047 hrs · 35,005 cycles

ENROUTE, CAPTAIN`S FWD WINDOW WAS ARCING. R & R THE CAPTAIN'S FWD WINDSHIELD.

Part: BOTTLE — LOW PRESSURE (R2 DOOR)

PHX R2 DOOR ASSIST BOTTLE LOW. SERVICED THE R2 DOOR ASSIST BOTTLE.

Part: SKIN PANEL — DELAMINATED (LT HORIZ STAB) · airframe 97,221 hrs · 34,441 cycles

C3 CHECK, DELAMINATED AREA ON LT UPPER HORIZONTAL STABILIZER INBD FWD SKIN PANEL BETWEEN FSS 56.05 TO FSS 83.48, APPROXIMATELY 18 INCHES OTBD FROM FUSELAGE. REPAIRED LT UPPER HORIZONTAL STABILIZER INBD FWD SKIN PANEL BETWEEN FSS 56.05 TO FSS 83.48 IAW EA 505913.

Part: SLIDE RAFT — LOOSE (L2 DOOR) · airframe 97,221 hrs · 34,441 cycles

C1 CHECK, L2 DOOR SLIDE RAFT NOT PROPERLY SECURED. INSTALLED & SECURED L2 DOOR ESCAPE SLIDE IAW JOB CARD 19C83225004.

Part: SKIN — DEBONDED (LE SLAT) · airframe 97,221 hrs · 34,441 cycles

C3 CHECK, DIS BONDING ON 10 SLAT UPPER TE SKIN AT OSS 791.97. REPAIRED NR 10 SLAT UPPER TE SKIN AT OSS 791.97 IAW B757 SRM 51-70-10-2R & 57-43-02.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 96,700 hrs · 34,318 cycles

DELAMINATION & SEPARATION ON RT WING INBD T/E FLAP UPPER SURFACE AT MF BS 220 APPROX 8 FT FROM AFT END. REPLACED RT WING INBD T/E FLAP IAW JC 19L50027003.

Part: GIRT BAR — WORN (L1 DOOR SLIDE)

L1 FWD DOOR GIRT BAR SPRINGS WORN. MX R & R GIRT BAR ASSY.

Part: HARNESS — ROTTED (L1 DOOR SLIDE)

HARNESS ASSY FOR L1 DOOR SLIDE DRY ROTTED. HARNESS ASSY REQUIRES REPLACEMENT. MX INST SERV L1 DOOR SLIDE APRON HARNESS.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 96,460 hrs · 34,254 cycles

EMERGENCY LIGHT ABOVE ROW 8L INOPERATIVE. R & R FUSE IN POWER SUPPLY M731.

Part: ROD END BEARING — WORN (GIRT BAR)

L-1 DOOR GIRT BAR FWD & AFT ROD END BEARINGS WORN. R & R L1 DOOR GIRT BAR FWD & AFT ROD ENDS, AND INST ROD.

Part: DOOR — LACK OF LUBE (L1) · airframe 95,866 hrs · 34,111 cycles

DOOR L1 HARD TO OPEN AFTER COLD SOAKED. WILL ONLY OPEN 18" FREELY, THEN REQUIRES UNDUE FORCE. MOVES FREELY AFTER WARM UP. LUBED L1 DOOR. NO FAULT NOTED AT THIS TIME. OK FOR FLIGHT.

Part: HINGE — LACK OF LUBE (L1 DOOR) · airframe 95,747 hrs · 34,090 cycles

L1 DOOR WAS VERY HARD TO FULLY OPEN. APPEARS JAMMED IN HINGE AREA. LUBED DOOR HINGES. DOOR OPENS AND CLOSES NORMALLY.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 95,138 hrs · 33,962 cycles

RON VISIT - DELAMINATION ON LOWER SURFACE OF LEFT WING 5 SLAT TRAILING EDGE WEDGE BETWEEN SLAT STA 200 TO SLAT STA 224 APPROX 26 INCHES FROM OUTBOARD END. REPLACED LEFT WING 5 SLAT ASSEMBLY IAW B757 JOB CARD 19L51027001.

Part: COVER — UNSECURE (CABIN) · airframe 95,092 hrs · 33,953 cycles

PHX - PLASTIC COVER OVER DOOR 2L FALLS OFF. REPLACED EXIT LIGHT COVER ON L2 DOOR WAY, OPS CHECK GOOD.

Part: BOTTLE — ACTIVATED (L2 DOOR) · airframe 95,036 hrs · 33,940 cycles

KOA - DOOR 2L ASSIST BOTTLE ACTIVATED WHEN CLOSING DOOR. MAINTENANCE REMOVED AND REPLACED L-2 DOOR ASSIST BOTTLE. ALSO PERFORMED EMERGENCY POWER ACTUATION CABLE SYSTEM TEST. OPS CHECKED GOOD.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 94,953 hrs · 33,924 cycles

RON - NR 6 SLAT HAS A 6 INCH X 6 INCH AREA OF DELAMINATED SKIN 4 INCHES INBOARD OF INBOARD END ON BOTTOM SIDE. REMOVED AND REPLACED SLAT IAW JOB CARD 19L51027001.

Part: MECHANISM — OUT OF ADJUST (GIRT BAR)

PHX - DOOR 4L WILL NOT ARM FLIGHT ATTENDANT REPORTS. FOUND GIRT BAR MECHANISM FWD ROD ARM SAFETY LOOSE. ADJUSTED ROD ARM MECHANISM FOR GIRT BAR.

Part: BOLT — OVERTORQUED (NLG) · airframe 92,330 hrs · 33,391 cycles

PHX - FLT 9251 PHX TEST FLT. NO NOSE GEAR EXT WITH ALT GEAR EXTENSION. MAINTENANCE CORRECTED BINDING CONDITION OF NOSE GEAR LOCK LINK AT APEX BOLT. PERFORMED ALTERNATE GEAR EXTENSION TEST. NO FAULTS NOTED DURING THREE CYCLES.

Part: WEDGE — DEBONDED (LE SLAT) · airframe 92,326 hrs · 33,389 cycles

C2 CHECK - DISBONDING ON NR 5 SLAT TRAILING EDGE WEDGE APPROX 58 INCHES FROM OUTBOARD END AT WS 257. REPAIRED NR 5 SLAT TRAILING EDGE WEDGE IAW B757 SRM 51- 70-10.

Part: WEDGE — DEBONDED (LE SLAT) · airframe 92,326 hrs · 33,389 cycles

C2 CHECK - DISBONDING ON NR 5 SLAT TRAILING EDGE WEDGE APPROX 5 INCHES FROM OUTBOARD END BETWEEN WS 285.65. REPAIRED NR 5 SLAT TRAILING EDGE WEDGE IAW B757 SRM 51- 70-10.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 92,326 hrs · 33,389 cycles

C2 CHECK - CORROSION ON STRINGER AT BS 1455, S28L. REPAIRED STRINGER AT BS 1455, S28L IAW EA 103875.

Part: LATCH — LACK OF LUBE (COCKPIT SEAT) · airframe 92,313 hrs · 33,384 cycles

F/O SEAT DIFFICULT TO KEEP LATCHED IN J TRACK. LUBED LATCH MECHANISM, OPS CHECK GOOD.

Part: SLIDE — FAILED (L4 DOOR) · airframe 91,945 hrs · 33,308 cycles

EVACUATION SLIDE ARMING LEVER FAILED TO MOVE AT SERVICE DOOR 4L. SLIDE PACK AND GIRT BAR UNROLLED. INSTALLED SLIDE PACK AND GIRT BAR. INSPECTED OK.

Part: SHADE — STUCK (CABIN) · airframe 91,378 hrs · 33,197 cycles

PHX - 27F (EXIT ROW) WINDOW SHADE WILL NOT STAY UP. MAINTENANCE UNSTUCK AND RE-SECURED WINDOW SHADE AT 27F (EXIT ROW).

Part: FAN — INOPERATIVE (CABIN) · airframe 91,196 hrs · 33,147 cycles

PHX FLT 43 EN ROUTE DCA TO PHX. EICAS MSG R RECIR FAN INOP AND INOP LIGHT ILLUMINATED WITH SWITCH POSITIONED ON. STRONG SMELL OF BURNING ELECTRICAL. MAINTENANCE REMOVED AND REPLACED RT RECIRCULATION FAN.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 90,796 hrs · 33,056 cycles

DAILY CHECK - NR 5 SLAT HAS DELAMINATION ON TRAILING EDGE WEDGE OF UPPER SURFACE AT SLAT STATION ISS220, 51 INCHES FROM OUTBOARD END. REPAIRED NR 5 SLAT IAW B757 SRM 51-70-10.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 90,796 hrs · 33,056 cycles

DAILY CHECK - NR 5 SLAT HAS DELAMINATION ON TRAILING EDGE WEDGE MIDDLE OF UPPER SURFACE AT SLAT STA ISS155, 42 INCHES FROM INBOARD END. REPAIRED NR 5 SLAT IAW B757 SRM 51-70-10.

Part: PUMP — INOPERATIVE (FUEL SYSTEM) · airframe 90,200 hrs · 32,924 cycles

HNL - FLT 31 EN ROUTE OGG TO PHX. DURING CLIMBOUT FROM MAUI, RECIEVED A FUEL CONFIG WARNING DUE TO FUEL IMBALANCE. LEFT GAUGE REPORTED 12.0 AND RIGHT GAUGE REPORTED 14.3. PROGRESSIVE FUEL LEAK IN LEFT MAIN TANK. DIVERTED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED FOR FUEL LEAKS. NONE WERE NOTED. FOUND THE LEFT FUEL OVER-RIDE PUMP CIRCUIT BREAKER OUT. REMOVED AND REPLACED THE LEFT FUEL OVER-RIDE PUMP IMPELLER. THE SYSTEM OPERATIONALLY AND LEAK CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 90,142 hrs · 32,911 cycles

L-4 DOOR EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK.

Part: WIRE — BROKEN (CABIN) · airframe 88,773 hrs · 32,633 cycles

MCN - C1 - EEL - CABIN BULLNOSE EMERGENCY LIGHT ABOVE SEAT ROW 15R DOES NOT ILLUMINATE WHEN TESTED. REPAIRED BROKEN WIRE WITH NEW TERMINAL IAW B757 SWPM 20-30-11 AT SEAT ROW 15R, OPS CHECK GOOD IAW B757 AMM 33-51-05-2.

Part: SWITCH — FAILED (CABIN) · airframe 88,773 hrs · 32,633 cycles

MCN - C1 - EEL - L-2 DOOR EMERGENCY LIGHT TEST SWITCH DOES NOT ILLUMINATE EMERGENCY LIGHTS. REPLACED L-2 DOOR EMERGENCY LIGHT TEST SWITCH IAW B757 AMM 33-51-05-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 88,773 hrs · 32,633 cycles

MCN - C1 - MAJOR REPAIR - CRACK ON INTERCOSTAL ATTACH ANGLE BETWEEN BS 440 TO BS 460, BL 0. REPLACED INTERCOSTAL ATTACH ANGLE BETWEEN BS 440 TO BS 460, BL 0 IAW B757 SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 88,773 hrs · 32,633 cycles

MCN - C1 - MAJOR REPAIR - CRACK ON INTERCOSTAL ATTACH ANGLE BETWEEN BS 480 TO BS 500, RBL 9. REPLACED INTERCOSTAL ATTACH ANGLE BETWEEN BS 480 TO BS 500, RBL 9 IAW B757 SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 88,773 hrs · 32,633 cycles

MCN - C1 - MAJOR REPAIR - CORROSION ON STRINGER AT BS 1620, S28L. REPAIRED STRINGER AT BS 1620, S28L IAW B757 SRM 53-00-03.

Part: LIGHT — INOPERATIVE (EXTERIOR)

PHX - THE L4 DOOR EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD.

Part: MECHANISM — LACK OF LUBE (L4 DOOR)

PHX - DOOR L4 HARD TO CLOSE. LUBED DOOR MECHANISM.

Part: LIGHT — INOPERATIVE (CABIN)

PHX - THE THIRD FROM AFT EMERGENCY ESCAPE PATH LIGHT ON BULLNOSE ABOVE SEAT ROW 30L WAS INOPERATIVE. REMOVED AND REPLACED THE LEFT EMERGENCY LIGHT AISLE LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN)

PHX - AFT MOST EMERGENCY ESCAPE PATH LIGHT ON BULLNOSE ABOVE SEAT ROW 3, 3L WAS INOPERATIVE. REMOVED AND REPLACED THE LEFT EMERGENCY AISLE ASSEMBLY.

Part: WIRE — BROKEN (CABIN)

PHX - THE AFT EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW L1 WAS INOPERATIVE. REPAIRED BROKEN WIRE.

Part: MEGAPHONE — INOPERATIVE (CABIN)

PHX - FIRST CLASS MEGAPHONE WAS INOPERATIVE. REMOVED AND REPLACED FIRST CLASS MEGAPHONE.

Part: TRIGGER — BROKEN (L4 DOOR)

PHX - THE L4 DOOR ASSIST POWER TRIGGER WAS BROKEN AND BOTTLE WAS DISCHARGED. REMOVED AND REPLACED POWER TRIGGER AND DOOR ASSIST BOTTLE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS)

L-2 DOOR EMERGENCY BATTERY PACK INOPERATIVE. REPLACED BATTERY CHARGER ASSY AT L-2 DOOR. (K)

Part: LIGHT — INOPERATIVE (EXTERIOR)

PHX - THE EMERGENCY EXIT EXTERIOR LIGHT WAS FOUND INOPERATIVE AT THE L3 DOOR. MAINTENANCE REPLAMPED THE EMERGENCY EXIT EXTERIOR LIGHT AT THE L3 DOOR.

Part: TACH GENERATOR — MALFUNCTIONED (LT ENGINE)

HNL - FLT 125 EN ROUTE HNL TO PHX. WHILE CLIMBING OUT OF FL 250, THE LEFT ENGINE BLEED LIGHT ILLUMINATED, FOLLOWED BY A LEFT CENTER FUEL PUMP PRESSURE LIGHT. SHORTLY AFTERWARDS, THE LEFT N3 INDICATION WAS ZERO. THE FLIGHT RETURNED TO FIELD HNL. UPON LANDING, THE LEFT ENGINE OIL PRESSURE INDICATED AMBER AND WENT DOWN TO 22 PSI. DURING TAXI, THE CREW SHUT DOWN THE LEFT ENGINE. AT THE GATE, THE LEFT GENERATOR CONTROL OFF LIGHT ILLUMINATED. MAINTENANCE INSPECTED THE LEFT ENGINE CHIP DETECTORS, AND INSPECTED AND REPLACED THE OIL SCAVENGE AND PRESSURE FILTERS. NO DEBRIS OR CONTAMINATION WAS FOUND. ALSO REPLACED THE LEFT ENGINE OIL PRESSURE TRANSMITTER. FINALLY, MAINTENANCE REPLACED THE LEFT ENGINE N3 TACHOMETER GENERATOR, WHICH IS IDENTIFIED AS THE CAUSE OF THE MULTIPLE SYSTEM FAILURES. AIRCRAFT OPERATIONALLY AND LEAK CHECKS OK.

Part: ANTI-ICE VALVE — FAULTY (LT ENGINE)

HNL FLT 26 - EN ROUTE OGG TO PHX. AFTER TAKEOFF, THE CREW TURNED ON THE ENGINE ANTI-ICE AND NOTICED A POWER LOSS AND FLUCTUATION ON THE LEFT ENGINE. THE ENGINE ANTI-ICE WAS TURNED OFF, AND THE LEFT ENGINE POWER PARAMETERS RETURNED TO NORMAL. THE FLIGHT DIVERTED TO HNL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE ANTI-ICE VALVE. OPERATIONALLY CHECKS OK.

Part: FITTING — CRACKED (ZONE 400) · airframe 80,043 hrs · 30,683 cycles

MCN - MAJOR REPAIR - C12 CHECK - LT PYLON MID BULKHEAD FITTING CRACKED, PYLON STATION 174. REPLACED LEFT PYLON MID BULKHEAD FITTING, PYLON STATION 174 I/A/W USAIRWAYS EA 100260.

Part: ATTACH FITTING — CRACKED (ZONE 100) · airframe 80,043 hrs · 30,683 cycles

MCN - MAJOR REPAIR - C12 CHECK, CRACKED CLIP, BS 620, S24R - S26R, WL 163. REPLACED CLIP, BS 620, S24R - S26R, WL 163 IAW B757 SRM 51-40-02.

Part: STIFFENER — CRACKED (ZONE 400) · airframe 80,043 hrs · 30,683 cycles

MCN - MAJOR REPAIR - C12 CHECK - CRACKED STIFFENER ON NR 1 PYLON STRUT, PYLON STATION 153.90. REPLACED STIFFENER ON NR 1 PYLON STRUT, PYLON STATION 153.90 IAW B757 SRM 51-40-02.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 80,043 hrs · 30,683 cycles

MCN - MAJOR REPAIR - C12 CHECK - LEFT ELEVATOR HAS DELAMINATION, ELEVATOR STATION 310- 318. REPAIRED LEFT ELEVATOR, ELEVATOR STATION 310- 318 IAW B757 SRM 51-70-04.

Part: STRINGER CLIP — CRACKED (ZONE 100) · airframe 80,043 hrs · 30,683 cycles

MCN - MAJOR REPAIR - C12 CHECK - CRACKED STRINGER CLIP, BS 845, S22R. REPLACED STRINGER CLIP, BS 845, S22R IAW B757 SRM 51-40-02.

Part: GUSSET — CRACKED (INTERCOSTAL) · airframe 80,043 hrs · 30,683 cycles

MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTERCOSTAL GUSSET, BS 845, S22R. REPLACED INTERCOSTAL GUSSET, BS 845, S22R IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 80,043 hrs · 30,683 cycles

MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTERCOSTAL, BS 480, LBL 38.25, WL 208. REPLACED INTERCOSTAL, BS 480, LBL 38.25, WL 208 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 80,043 hrs · 30,683 cycles

MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTERCOSTAL/SHEAR WEB, BS 1320, LBL 24, WL 133 - WL 138. REPLACED INTERCOSTAL/SHEAR WEB, BS 1320, LBL 24, WL 133 - WL 138 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 80,043 hrs · 30,683 cycles

MCN - MAJOR REPAIR - CRACKED INTERCOSTAL, BS 661, RBL 48, WL 207. REPLACED INTERCOSTAL, BS 661, RBL 48, WL 207 IAW B757 SRM 51-40-02.

Part: SILL — CORRODED (ZONE 200) · airframe 80,043 hrs · 30,683 cycles

MCN - MAJOR REPAIR - C12 CHECK - CORROSION ON L2 DOOR CUT OUT LOWER SILL INNER CHORD, BS 692 - BS 728, LBL 48, WL 208. REPLACED L2 DOOR CUT OUT LOWER SILL INNER CHORD, BS 692 - BS 728, LBL 48, WL 208 IAW B757 SRM 51-40-02.

Part: STIFFENER — CRACKED (ZONE 200) · airframe 80,043 hrs · 30,683 cycles

MCN - MAJOR REPAIR - C12 CHECK - CRACKED STIFFENER, BS 1600, RBL 49, WL 208. REPLACED STIFFENER, BS 1600, RBL 49, WL 208 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 80,043 hrs · 30,683 cycles

MCN - MAJOR REPAIR - C12 CHECK - CORROSION ON INTERCOSTAL CHORD, BS 1540 - BS 1564, S26R - S27R. REPLACED INTERCOSTAL CHORD, BS 1540 - BS 1564, S26R - S27R IAW B757 SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (ZONE 200) · airframe 80,043 hrs · 30,683 cycles

MCN - MAJOR REPAIR - C12 CHECK - CRACKED CLIP, BS 660 - BS 680, BL 0, WL 208. REPLACED CLIP, BS 660 - BS 680, BL 0, WL 208 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 80,043 hrs · 30,683 cycles

MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTERCOSTAL, BS 680, S11R - S12R. REPLACED INTERCOSTAL, BS 680, S11R - S12R IAW USAIRWAYS TASK CARD M1C53608.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 80,043 hrs · 23,321 cycles

MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTERCOSTAL, BS 680, S12L. REPLACED INTERCOSTAL, BS 680, S12L IAW USAIRWAYS TASK CARD M1C53608.

Part: ACTUATOR — FAILED (LT MLG) · airframe 79,380 hrs · 30,513 cycles

FLIGHT 146, PHX-LIH: AFTER TAKEOFF AND GEAR SELECTED TO 'UP' POSITION, RECEIVED GEAR DISAGREE LIGHT. SELECTED GEAR DOWN AND RECEIVED DOWN AND LOCKED INDICATIONS. FLIGHT RETURNED TO PHX. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR RETRACTION ACTUATOR.

Part: SKIN — DELAMINATED (SPOILER) · airframe 78,376 hrs · 30,231 cycles

PHX - MAJOR REPAIR - RIGHT WING NR 10 SPOILER, UPPER SURFACE DELAMINATED, WS 459.50 - WS 510.00. REPAIRED, RE-INSTALLED AND OPERATIONAL CHECKED RIGHT WING NR 10 SPOILER IAW B757-200 SRM 27-61-01.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 77,645 hrs · 30,032 cycles

PHX - CRACKED CABIN INTERCOSTAL ANGLES, BS 660, S17L, WL 208. REPLACED CABIN INTERCOSTAL ANGLES, BS 660, S17L, WL 208 IAW B757-200 SRM 51-40-02 AND 51-30-01.

Part: HYDRAULIC LINE — CRACKED (LEFT PYLON) · airframe 75,859 hrs · 29,526 cycles

LOG 7387973 - AIRCRAFT LOST LT HYDRAULIC SYSTEM QUANTITY/PRESSURE. THE CREW DECLARED AN EMERGENCY. AIRCRAFT RETURNED TO DEPARTURE. THE LANDING WAS UNEVENTFUL. MAINTENANCE DISCOVERED A HYDRAULIC LINE IN THE LT PYLON AREA CRACKED AT THE (B) NUT AND LEAKING. MAINTENANCE REPLACED THE LINE. OPS CHECK/LEAK TEST WAS GOOD.

Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 75,672 hrs · 29,475 cycles

HNL - EES - 1L FRONT LAVATORY SMOKE DETECTOR WENT OFF EN ROUTE WHILE FWD GALLEY OVENS WERE IN USE. TAMPER STRIP WAS BROKEN NEEDS REPLACEMENT. MAINTENANCE INSPECTED SMOKE DETECTOR AND REPLACED THE TAMPER STRIP.

Part: RESERVOIR — LOW (L2 DOOR) · airframe 75,522 hrs · 29,421 cycles

MCN - EE - L2 DOOR EMERGENCY POWER RESERVOIR IS DEPLETED. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR EMERGENCY POWER RESERVOIR IAW B757-200 AMM TASK 52-11-30-004-001 AND 52-11-30-404-013.

Part: STRUCTURE — DELAMINATED (T/E FLAP) · airframe 75,522 hrs · 29,421 cycles

MCN - LT WING I/B MAIN FLAP HAS A DISBONDED AREA AT THE O/B T/E CORNER. REPAIRED LT WING, I/B MAIN FLAP O/B T/E CORNER, IAW B757-200, SRM 51-70-10-2R, FIG 201.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 75,522 hrs · 29,421 cycles

CHECK NR C-11. NR 5870966. INTERCOSTAL CRACKED AT BS 660, ADJACENT TO L2 DOOR, LOWER HINGE. CRACK EXTENDS BEYOND AFT EDGE OF BEND RELIEF RADIUS. REPAIRED INTERCOSTAL AT BS 660, ADJACENT TO L2 DOOR LOWER HINGE, IAW AWA TASKCARD MIC 53612.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 75,522 hrs · 29,421 cycles

CHECK NR C-11. NR N 5870967. INTERCOSTAL CRACKED AT BS 660, ADJACENT TO R2 DOOR, NR 3 STOP FITTING. REPAIRED THE R2 DOOR, NR 3 STOP INTERCOSTAL IAW AWA CARD MIC 53604.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 75,522 hrs · 29,421 cycles

CHECK NR C-11. NR 5870965. INTERCOSTAL CRACKED AT BS 660, ADJACENT TO L2 DOOR, NR 3 STOP FITTING. REPAIRED INTERCOSTAL AT BS 660, ADJACENT TO L2 DOOR, NR 3 STOP FITTING, IAW AWA CARD MIC 53604.

Part: WIRE HARNESS — BROKEN (EMERGENCY LIGHTS) · airframe 75,522 hrs · 29,421 cycles

MCN - LT PASSENGER CABIN SEAT ROWS 10. 12, AND 29 HAVE BAD PLUGS ON EMERGENCY PATH LIGHT HARNESS. REMOVED AND REPLACED EMERGENCY PATH LIGHT HARNESSES AT LT PASSENGER SEAT ROWS 10, 12, AND 29, OPS CHECKED GOOD, IAW B757-200, AMM 33-59-00, T/R 33-015 AW.

Part: WIRE HARNESS — BROKEN (EMERGENCY LIGHTS) · airframe 75,522 hrs · 29,421 cycles

MCN - LT PASSENGER SEAT ROWS 21, 22, 27, 33, AND 34 HAVE BAD EMERGENCY PATH LIGHT HARNESSES. REMOVED AND REPLACED EMERGENCY PATH LIGHT HARNESSES AT SEATS 21, 22, 27, 33, AND 34 LEFT, AND OPS CHECKED GOOD IAW B757-200 AMM 39-59-00, TR 33-015AW.

Part: WIRE HARNESS — BROKEN (EMERGENCY LIGHTS) · airframe 75,522 hrs · 29,421 cycles

MCN - EEL - EMERGENCY ESCAPE PATH LIGHT HARNESS MISSING JIFFY FUNCTIONS, DAMAGED CONNECTORS AND WIRES, BS 400 - BS 660, RBL 45. REPAIRED EMERGENCY ESCAPE PATH LIGHTING HARNESS JIFFY JUNCTIONS AND CONNECTORS IAW BSWDM 20-90-14, AND 20-30-12, OPS TESTED GOOD ON AWA T/C, A1C 33606.

Part: FLOOR SKIN — CRACKED (FUSELAGE) · airframe 75,522 hrs · 29,421 cycles

MCN - FLIGHT STATION FLOOR HAS CRACK DAMAGE ON LEFT SIDE JUST AFT OF FIRST OBSERVERS FOOT REST. REPAIRED FLIGHT STATION FLOOR ON LEFT SIDE JUST AFT OF FIRST OBSERVERS FOOT REST, IAW B757-200, SRM 51-70-13-06, FIG 1.

Part: POWER SUPPLY — INOPERATIVE (FLASHLIGHT) · airframe 75,522 hrs · 29,421 cycles

MCN - EEL - FWD FLIGHT ATTENDANT FLASHLIGHT INOP. REMOVED AND REPLACED FWD FLIGHT ATTENDANT FLASHLIGHT POWER SUPPLY AS REQUIRED. OPS CHECKS WERE GOOD.

Part: POWER SUPPLY — INOPERATIVE (FLASHLIGHT) · airframe 75,522 hrs · 29,421 cycles

MCN - EEL - AFT FLIGHT ATTENDANT FLASHLIGHT INOP. REMOVED AND REPLACED AFT FLIGHT ATTENDANT POWER SUPPLY AS REQUIRED. OPS CHECKS WERE GOOD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 75,522 hrs · 29,421 cycles

CHECK NR C-11, NR 5870968 INTERCOSTAL CRACKED AT BS 660, ADJACENT TO R2 DOOR, LOWER HINGE. REPAIRED BS 660 INTERCOSTAL AT R2 DOOR LOWER HINGE, IAW AWA TASKCARD MIC 53611.

Part: SKIN — CRACKED (NR 3 SLAT) · airframe 75,522 hrs · 29,421 cycles

MCN - CRACK ON NR 3 SLAT COVE SKIN, OSS 472. REMOVED AND REPLACED NR 3 SLAT COVE SKIN AT OSS 472, IAW B757-200, SRM 51-40-02-06, PAR 5, 6, FIGS 9, 10, 11, 51-30-01-06, FIG 7, AND BOEING DWG, 114N4076.

Part: SKIN — CRACKED (NR 2 SLAT) · airframe 75,522 hrs · 29,421 cycles

MCN - CRACK ON NR 2 SLAT, COVE SKIN, OSS 677. REMOVED AND REPLACED NR 2 SLAT COVE SKIN, OSS 677, IAW B757-200, SRM 51-30-01-06, FIG 7, AND 51-40-02-06, PAR 5, 6 FIGS 9, 10, 11, AND BOEING DWG, 114N4077.

Part: STRINGER — CRACKED (BS 595) · airframe 75,522 hrs · 29,421 cycles

MCN - FOUND STRINGER 15 LEFT, B/S 595 HAS A CRACK 1.250" LONG. REPAIRED STRINGER 15L AT B/S 595, IAW B757-200, SRM 53-00-03-2R, 1 FIG 201.

Part: FLOOR SUPPORT — CORRODED (BS 1303-1319) · corrosion level 2 · airframe 75,522 hrs · 29,421 cycles

FOUND CORROSION ON CABIN FLOOR SUPPORT B/S 1303-1319, LBL 21. REMOVED AND REPLACED CABIN FLOOR SUPPORT B/S 1303-1319, LBL 21, IAW B757-200, SRM 51-40-02-OG, PARA 4B, 7D, FIGS 4, 8, 12.

Part: ANGLE — CRACKED (BS 1620-1640)

CABIN FLOOR INTERCOSTAL UPPER ATTACH ANGLE CRACKED, BS 1623 - BS 1634, BL0. REMOVED, FABRICATED AND REPLACED CRACKED CABIN FLOOR INTERCOSTAL UPPER ATTACH ANGLE, BS 1623 - BS 1634, BL0 IAW B757-200 SRM 51-40-02-06 PARAGRAPH 4 FIGURES 3 & 8.

Part: SILL — CORRODED (L3 DOOR) · airframe 75,522 hrs · 29,421 cycles

FOUND CORROSION ON THE L3 DOOR LOWER SILL INNER CHORD REPAIR ANGLE, BS -1342 - BS 1348, LBL 63. REMOVED AND REPLACED L3 DOOR LOWER SILL INNER CHORD ANGLE, BS 1342 - BS 1348, LBL 63 I/A/W B757-200 SRM 51-40-02-06, FIGURE 4 & 8 PARAGRAPH 4.

Part: FLOOR SUPPORT — CORRODED (BS 1300-1320) · corrosion level 2 · airframe 75,522 hrs · 29,421 cycles

MCN - FOUND CORROSION ON CABIN FLOOR SUPPORT B/S 1303-1319, RBL 21. REMOVED AND REPLACED CABIN FLOOR SUPPORT B/S 1300-1320, RBL 21 IAW B757-200 SRM 51-40-02, PAR 7D, FIGS 3, 12, 8.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 75,413 hrs · 29,391 cycles

SAL - DURING MAINTENANCE CHECK, NR 5945413 EMERGENCY PATH-WAY LIGHTING AT OVERHEAD BIN 2R, 5R, 11R, 1L, 14L, 14R, 18L, 12L INOP. REMOVED AND REPLACED EMERGENCY PATH WAY LIGHTING BATTERY PACK AND POWER SUPPLY AT L2 DOOR. OPS CHECK IS GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 75,413 hrs · 29,391 cycles

PHX - EEL - MAINTENANCE CHECK. NR. NO. 7248842. EMERGENCY PATH-WAY LIGHTING AT OVERHEAD BIN 2R, 5R, 11R, 1L, 14L, 14R, 18L, 12L INOP. REMOVED AND REPLACED EMERGENCY PATHWAY LIGHTING BATTERY PACK AND POWERSUPPLY AT L2 DOOR OPS CHECK IS GOOD. CHANGED STATION TO PHX AND MAJOR REPAIR TO EEL.

Part: HYDRAULIC LINE — LEAKING (NR 1 PYLON) · airframe 75,014 hrs · 29,292 cycles

AIR TURN BACK - FLT 922 - LOG 7257329 - DURING CLIMB OUT, ENROUTE, CREW REPORTED THAT THE LT HYDRAULIC LEVEL WENT TO ZERO BUT THEY WERE ABLE TO MAINTAIN PRESSURE. CREW RETURNED AND LANDED HAVING TO BE BEING TOWED TO THE GATE. MAINTENANCE REMOVED AND REPLACED A HYDRAULIC LINE IN THE NR 1 ENGINE PYLON. LEAK CHECK WAS GOOD. LT HYDRAULIC SYSTEM WAS SERVICED.

Part: FLASHLIGHT — INOPERATIVE (L2 DOOR) · airframe 74,424 hrs · 29,156 cycles

PHX - EEL - MAINTENANCE REPORTED THAT THE FLASHLIGHT AT DOOR L2 HAD A DEAD BATTERY. MAINTENANCE REMOVED AND REPLACED THE FLASHLIGHT AT THE L2 DOOR. OPERATIONAL CHECKS WERE GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,666 hrs · 28,957 cycles

PHX - EEL - DURING 8 DAY DISCOVERED EMERGENCY EXIT LIGHT AT ROW 27 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY AND POWER SUPPLY, OPS CHECKS WERE GOOD, BATTERY; PN 2013-1A; MFG RADIANT ILLUM; SN UNK.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,621 hrs · 28,936 cycles

MAJOR REPAIR - DURING C-00 CHECK DISCOVERED FLOORBEAM CRACKED, 1.5 INCHES LONG, AT BS 700, WL 206 AND BL 24R. MAINTENANCE CUT OUT DAMAGE ON FLOORBEAM IAW ENGINEERING REPAIR NR 19-5335-05346-RC3. FABRICATED REPAIR ANGLES AND REPAIR SECTION IAW AWA ER NR 19-5335-05346-RC3. INSTALLED FABRICATED REPAIR PARTS IAW AWA ER NR19-5335-05346-RC3.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 73,063 hrs · 28,706 cycles

LAS - EEL - DURING 4 DAY CHECK, DISCOVERED THE FORWARD F/A EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD F/A EMERGENCY FLASHLIGHT. OPERATIONAL CHECKS GOOD.

Part: FUEL CONTROL — INOPERATIVE (NR 1 ENGINE) · airframe 72,575 hrs · 28,507 cycles

DURING ENGINE SHUTDOWN, AT GATE, LT ENGINE WOULD NOT SHUT DOWN WITH FUEL CONTROL SWITCH AT CUT OFF POSITION. PULLED LT ENGINE FIRE HANDLE. ENGINE SHUT DOWN. MAINTENANCE REMOVED AND REPLACED NR 1 FUEL FLOW GOVERNOR IAW AMERICA WEST AIRLINES (AWA) TASK CARD R5M73603 AND AWA TASK CARD F5M73601. OPERATIONAL CHECKS GOOD. VENDOR REPORTS THAT THEY COULD NOT CONFIRM FAULT. FFG WAS RECEIVED AND FOUND TO BE FUNCTIONING PROPERLY. UNIT WAS TESTED AND RE-CALIBRATED IAW CMM 73-21-02 REV 5.

Part: RELAY — MALFUNCTIONED (STALL WARNING) · airframe 72,517 hrs · 28,482 cycles

DURING TAKEOFF BELOW 60 KNOTS REJECTED TAKEOFF FOR LT AOA PROBE EICAS MESSAGE. MESSAGE EXTINGUISED AFTER ABOUT 10 SECONDS. LT AOA WAS MEL'D. MX REMOVED AND REPLACED LT AOA CURRENT SENSING RELAY K401 IAW BOEING 757 MM 30-32-00-5, OPS CHECKS WERE GOOD. MEL WAS CLEARED.

Part: SPAR — CRACKED (NR 2 PYLON) · airframe 71,895 hrs · 28,199 cycles

SAL - MAJOR REPAIR - DURING ACCOMPLISHMENT OF SB 757-54A0039 A 1.375 INCH CRACK WAS FOUND ON NR 2 ENGINE PYLON UPPER SPAR WEB. MAINTENANCE STOP DRILLED CRACK ON NR 2 ENGINE PYLON UPPER SPAR WEB; PERFORMED HFEC INSPECTION TO VERIFY CRACK CONTAINED; FABRICATED 2 EACH DOUBLERS; INSTALLED REPAIR PARTS IAW ER 19-5450-05099-HF2.

Part: WIRE — BROKEN (SEAT ROW 7 LT) · airframe 71,313 hrs · 27,944 cycles

PHX - EEL - DURING A-06 CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 7 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 7 LT, OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 71,213 hrs · 27,896 cycles

PHX - EMERGENCY EQUIPMENT - DURING INSPECTION THE FORWARD EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,207 hrs · 27,893 cycles

SAL - MAJOR REPAIR - DURING C-10 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM UPPER CHORD AT BS 324, RBL 50. MAINTENANCE CUT OUT CORRODED SECTION OF FLOORBEAM UPPER CHORD AT BS 324, RBL 50; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM UPPER CHORD, 2 EACH SPLICE STRAPS, AND 2 EACH SPLICE REPAIR ANGLES; INSTALLED REPAIR PARTS IAW ER 19-5310-04365-RC3.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,207 hrs · 22,893 cycles

SAL - MAJOR REPAIR - DURING C-10 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN SUPPORT STRUCTURE AT RBL 60 BETWEEN BS 350 AND BS 365.25. MAINTENANCE REMOVED CORRODED SUPPORT STRUCTURE AT RBL 60 FROM BS 350 TO BS 365.25; INSTALLED NEW REPLACEMENT SUPPORT STRUCTURE IAW B757-200 SRM 51-10-02.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,207 hrs · 27,893 cycles

SAL - MAJOR REPAIR - DURING C-10 CHECK EXFOLIATION CORROSION WAS FOUND ON PASSENGER CABIN SUPPORT SECTION AT BS 365.25, RBL 55. MAINTENANCE REMOVED CORRODED SUPPORT SECTION AT BS 365.25, RBL 55; FABRICATED A NEW SUPPORT SECTION PER DWG 141N5186; INSTALLED REPAIR PART IAW B757-200 SRM 51-10-02.

Part: TUBE — LEAKING (LT PYLON)

PHX - DIVERSION - FLT 0058 - AFTER TAKEOFF FROM LAS EN ROUTE FOR JFK RECEIVED EICAS MESSAGE M56 LT HYDRAULIC SYSTEM PRESSURE, HYDRAULIC QUANTITY DECREASED TO ZERO AND SYSTEM PRESSURE WARNING LIGHT ILLUMINATED, DIVERTED TO PHX FOR REPAIR. MAINTENANCE FOUND LT PYLON HYDRAULIC CASE DRAIN TUBE ASSEMBLY THAT RUNS TO FIRE SEAL DISCONNECT LEAKING. REMOVED AND REPLACED HYDRAULIC TUBE ASSEMBLY IN LT PYLON, LEAK CHECK WAS GOOD.

Part: LIGHT — INOPERATIVE (SEAT ROW 21 LT) · airframe 70,056 hrs · 27,384 cycles

DFW - EEL - DURING 8-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT, OPERATIONAL CHECK WAS GOOD.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 69,846 hrs · 27,288 cycles

PHX - MAJOR REPAIR - DURING 8-DAY CHECK A CRACK WAS FOUND IN SKIN AND BEAR STRAP AT L-1 DOOR WAY FORWARD UPPER CORNER BS 350. MAINTENANCE CUT OUT CRACKS IN SKIN AND BEAR STRAP AT L-1 DOOR WAY FORWARD UPPER CORNER BS 350; PERFORMED HFEC OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A DOUBLER, TRIPLER, AND QUADRUPLER; INSTALLED REPAIR PARTS IAW AWA ER 19-531104167-BA1.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 69,577 hrs · 27,154 cycles

PHX - EEL - DURING THRU-FLIGHT INSPECTION FOUND DAMAGED WIRE SPLICED INTO THREE OTHER WIRES THAT TERMINATE IN PINS 1, 7, AND 18 OF AFT GALLEY CENTER OVERHEAD EMERGENCY POWER SUPPLY. MAINTENANCE REPAIRED DAMAGED WIRE AT AFT GALLEY CENTER OVERHEAD EMERGENCY POWER SUPPLY BS 1678; OPERATIONAL CHECK WAS GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 69,570 hrs · 27,148 cycles

PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 25 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE UNDER SEAT ROW 25 LT, OPERATIONAL CHECK WAS GOOD.

Part: WIRE — BROKEN (SEAT ROW 5 LT) · airframe 69,345 hrs · 27,058 cycles

PHX - EEL - EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LEFT INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 5 LT, OPERATIONAL CHECK WAS GOOD.

Part: CONNECTOR — DAMAGED (SEAT ROW 12 LT) · airframe 68,776 hrs · 26,838 cycles

PHX - EEL - DURING A-08 CHECK FOUND EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 12 LT INOPERATIVE. MAINTENANCE FOUND DAMAGED CONNECTOR UNDER SEAT 12 LT. REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT HARNESS CONNECTOR AND SOCKET ASSEMBLIES AT SEAT ROW 12 LT; OPERATIONAL CHECK WAS GOOD. PART NAME; SOCKET, CONN, 22-18, GOLD PLATE, MFG; AMP INC, P/N; 170366-3, LOC; SEAT ROW 12 LT.

Part: CIRCUIT CARD — FAULTY (E/E RACK) · airframe 68,716 hrs · 26,819 cycles

BWI - ABORTED TAKEOFF - FLT 0085 - ON TAKEOFF AT PHX EN ROUTE FOR BWI TAKEOFF WARNING HORN SOUNDED AND RED STABILIZER EICAS MESSAGE WAS DISPLAYED, REJECTED TAKEOFF BELOW 10 KTS, STAB TRIM WAS AT 4.5. MAINTENANCE COMPLIED WITH FAULT ISOLATION MANUAL 31-51-00, REMOVED AND REPLACED M620 TAKEOFF CONFIGURATION CIRCUIT CARD MODULE IAW BMM 31-51-04, OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 68,203 hrs · 26,641 cycles

DURING INSPECTION FOUND THE L-1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR EMERGENCY EXIT LIGHT BATTERY POWER SUPPLY (M731), OPERATIONAL CHECK WAS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,305 hrs · 20,634 cycles

PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 11 LT, OPERATIONAL CHECK WAS GOOD.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,785 hrs · 26,059 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION FOUND ON L-4 DOOR THRESHOLD SUPPORT ANGLE AT B/S 1681. MAINTENANCE REMOVED L-4 DOOR THRESHOLD SUPPORT ANGLE AT B/S 1681; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE PER DWG 143N8328; INSTALLED REPAIR PART IAW B757 SRM 51-70-11 PAGES 1-7.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,785 hrs · 26,059 cycles

DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON 3 EACH GALLEY SUPPORT FITTINGS ON AFT SHEAR DECK AT BS 1681 LT, BS 1681R/H, AND BS 1715 LT. MAINTENANCE REMOVED AND REPLACED 3 EACH GALLEY SUPPORT FITTINGS ON AFT SHEAR DECK AT BS 1681 LT, BS 1681 RT, AND BS 1715 LT IAW B757-200 SRM 51-40-02, PG. 12.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,785 hrs · 26,059 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON L-4 DOOR THRESHOLD SUPPORT FITTING AT BS 1675, LBL 68. MAINTENANCE REMOVED L-4 DOOR THRESHOLD SUPPORT FITTING AT BS 1675, LBL 68; FABRICATED A NEW REPLACEMENT THRESHOLD SUPPORT FITTING; INSTALLED REPAIR PART IAW 51-40-05, PG. 5-8.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,785 hrs · 26,059 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON RT CORNER FITTING AT BS 1720. MAINTENANCE REMOVED CORRODED RT CORNER FITTING AT BS 1720; FABRICATED A NEW REPLACEMENT CORNER FITTING PER DWG 146N8722; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, PG 1-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,785 hrs · 26,059 cycles

DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOOR SUPPORT BETWEEN BS 1680 AND BS 1700, LBL 50. MAINTENANCE REMOVED DAMAGED FLOOR SUPPORT BETWEEN BS 1680 AND BS 1700, LBL 50; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, PG 7.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,785 hrs · 26,059 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN FLOOR SUPPORT AT RBL 70, B/S 1660-1680. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED FLOOR SUPPORT RBL 70, BS 1660-1680; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02 PG 7-8.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,785 hrs · 26,059 cycles

DURING C-O9 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOOR SUPPORT BS 1640 TO BS 1660, RBL 70. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED FLOOR SUPPORT BS 1640 TO BS 1660, RBL 70; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; INSTALLED REPAIR PART IAW 51-40-02, PG. 7.

Part: CARGO TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,785 hrs · 26,059 cycles

DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND UNDER NUT PLATES ON AFT CARGO COMPARTMENT TIE DOWN FITTING AT BS 1360, RBL 36. MAINTENANCE REMOVED AND REPLACED DAMAGED TIE DOWN FITTING AT BS 1360, RBL 36 IAW B757-200 SRM 51-40-02, PG 11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,785 hrs · 26,059 cycles

DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON LOWER SURFACE OF AFT CARGO COMPARTMENT FLOOR SUPPORT STRINGER 29 LT AT BS 1470, LBL 7. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED SECTION OF FLOOR SUPPORT STRINGER 29 LT AT BS 1470, LBL 7; FABRICATED A NEW SECTION OF FLOOR SUPPORT STRINGER, AND REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11, PG. 1-7, FIG. 1.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,785 hrs · 26,059 cycles

DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN SHEAR DECK HAT CHANNEL BS 1714-1716, RBL 12. MAINTENANCE REMOVED DAMAGED HAT CHANNEL BS 1714-1716, RBL 12; FABRICATED A NEW REPLACEMENT HAT CHANNEL PER DWG 146N5300; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-05, PG. 1, 2, & 5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,785 hrs · 26,059 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON LOWER SURFACE OF AFT CARGO COMPARTMENT FLOORBEAM AT BS 1469, RBL 16. MAINTENANCE FOUND CORROSION TO BE ON EXISTING REPAIR ANGLE; REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT LIMITS; REMOVED CORRODED REPAIR ANGLE AT BS 1469, RBL 16; FABRICATED A NEW REPLACEMENT REPAIR ANGLE; INSTALLED REPAIR PART IAW 51-70-11, PG. 1-7, FIG. 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,785 hrs · 26,059 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON UPPER SURFACE OF AFT CABIN SHEAR DECK BS 1701 TO BS 1720, STR 17 LT TO STR 17 RT. MAINTENANCE REMOVED SHEAR DECK WEB FROM BS 1680 TO BS 1720; FABRICATED REPLACEMENT SHEAR DECK WEB PER DWG 146NB5318; INSTALLED REPAIR PART IAW 51-40-02, PG. 4, 11, & 16.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,785 hrs · 26,059 cycles

DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF AFT CARGO COMPARTMENT FLOOR SUPPORT STRINGER 29 LT AT BS 1470, LBL 3. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED SECTION OF FLOOR SUPPORT STRINGER 29 LT AT BS 1470, LBL 3; FABRICATED A NEW SECTION OF FLOOR SUPPORT STRINGER, AND REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11, PG. 1-7, FIG. 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,785 hrs · 26,059 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOOR SUPPORT IN SEVERAL SPOTS BETWEEN BS 1380 AND BS 1405, RBL 20. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED AFT CARGO COMPARTMENT FLOOR SUPPORT BETWEEN BS 1380 AND BS 1405, RBL 20; FABRICATED A REPAIR SUPPORT ANGLE; INSTALLED REPAIR PART IAW B757-200 SRM 51-70-11, PG 1-7.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,785 hrs · 26,059 cycles

DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON SHEAR DECK HAT CHANNEL BS 1716, BL 0. MAINTENANCE REMOVED CORRODED HAT CHANNEL BS 1716, BL 0; FABRICATED A NEW REPLACEMENT CHANNEL PER DWG 146N5300; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-05, PG. 1-2, & 5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,785 hrs · 26,059 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOORBEAM AT BS 1470, RBL 13. MAINTENANCE FOUND CORROSION TO BE ON EXISTING REPAIR ANGLE; REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT LIMITS; REMOVED CORRODED REPAIR ANGLE AT BS 1470, RBL 13; FABRICATED A NEW REPLACEMENT REPAIR ANGLE; INSTALLED REPAIR PART IAW 51-40-02, PG. 11-12.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,785 hrs · 26,059 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON CABIN FLOOR SUPPORT AT B/S 1640, BL 0. MAINTENANCE FOUND CORROSION WAS ON EXISTING REPAIR; REMOVED CORRODED REPAIR PART AT BS 1640, BL 0; FABRICATED A LEACH CHANNEL PER DWG 146N5242-1, AND A NEW REPLACEMENT FLOOR SUPPORT PER DWG 146N5230; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-20-01, PG. 10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,785 hrs · 26,059 cycles

DURING C-09 CHECK CORROSION WAS FOUND ON L/H CABIN FLOOR SUPPORT UNDER CUSP PANEL BS 1640 TO 1661. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FLOOR SUPPORT FROM BS 1640 TO 1661; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; INSTALLED REPAIR PART IAW B 757-200 SRM 51-40-02, PG. 7.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,785 hrs · 26,059 cycles

DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND AT 2 EACH NUT PLATES UNDER CABIN FLOOR PANEL BS 1708, RBL 50. MAINTENANCE REMOVED NUT PLATE CLIPS FROM FLOOR SUPPORT ANGLE BS 1708, RBL 50, AND FOUND FLOOR SUPPORT ANGLE TO ALSO BE CORRODED; REMOVED CORROSION AND FOUND MATERIAL LOSS BEYOND LIMITS; REMOVED DAMAGED FLOOR SUPPORT ANGLE; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART AND NEW NUT PLATE CLIPS IAW B757-200 SRM 51-70-11, PG. 1-7, FIG 1.

Part: PROBE — FAULTY (NR 1 ENGINE P1) · airframe 66,451 hrs · 25,909 cycles

EN ROUTE FROM SJD TO PHX RECEIVED NR 1 ENGINE PROBE HEAT STATUS MESSAGE, DECLARED EMERGENCY AND LANDED WITHOUT EVENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE P1 PROBE, OPERATIONAL CHECK WAS GOOD IAW BMM 30-34-00.

Part: WIRE — BROKEN (SEAT ROW 17 L/H) · corrosion level 0 · airframe 66,094 hrs · 25,745 cycles

PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 17 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE FOUND UNDER THE SEAT ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 17 L/H, OPERATIONAL CHECK WAS GOOD.

Part: WIRE — BROKEN (SEAT ROW 10) · airframe 65,718 hrs · 25,564 cycles

FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 10 LT, WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE FOUND AT SEAT ROW 10 LEFT, OPERATIONAL CHECK WAS GOOD.

Part: HARNESS — BROKEN (SEAT ROW 3 L/H) · corrosion level 0 · airframe 65,718 hrs · 25,564 cycles

PHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 3 L/H WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT HARNESS AT SEAT ROW 3 L/H, OPERATIONAL CHECK WAS GOOD.

Part: WIRE — BROKEN (SEAT ROW 6 L/H) · corrosion level 0 · airframe 65,425 hrs · 25,421 cycles

PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH ISLE LIGHT AT SEAT ROW 6 L/H WAS FOUND INOPERATIVE. MAINTENANCE DISCOVERED A BROKEN WIRE ON THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 6 L/H, SPLICED WIRE, OPERATIONAL CHECK WAS GOOD.

Part: WIRE — BROKEN (SEAT ROW 28 L/H) · corrosion level 0 · airframe 65,047 hrs · 25,258 cycles

PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 28 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT SEAT ROW 28 L/H, OPERATIONAL CHECK WAS GOOD.

Part: HYDRAULIC LINE — LEAKING (HYD SYSTEM) · airframe 64,927 hrs · 25,207 cycles

BWI - EMERGENCY LANDING - FLT 0778 - EN ROUTE FROM LAS TO BWI AT CRUISE THE LT HYDRAULIC QUANTITY DECREASED TO ZERO AND THE SYSTEM PRESSURE LIGHT ILLUMINATED WITH AN EICAS MESSAGE FOR LT HYDRAULIC SYSTEM PRESSURE DISPLAYED. DECLARED EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED A HYDRAULIC LINE THAT RUNS FROM THE NR 1 ENGINE HYDRAULIC PRESSURE MANIFOLD TO THE HYDRAULIC PRESSURE SWITCH. REPLACED THE ENGINE DRIVEN HYDRAULIC PUMP, FLUSHED SYSTEM, AND REPLACED THE PRESSURE, RETURN, AND CASE DRAIN FILTERS IAW R5M29601; LEAK AND OPERATIONAL CHECKS WERE GOOD.

Part: TUBE — CHAFED (#1 ENG.) · airframe 62,922 hrs · 24,417 cycles

LAS - EMERGENCY LANDING - FLT 085 - "C" - DURING CRUISE ENROUTE FROM JFK TO LAS AT FL 390 THE FLIGHT CREW RECEIVED EICAS MSG FOR L/H HYDRAULIC QUANTITY WITH A L/H RESERVIOR LIGHT ILLUMINATED, L/H HYDRAULIC QUANITY INDICATION WAS .48RF AND DECREASING .08 EVERY 10 MINUTES. QUANTITY DECREASED TO .04 AND STATUS MESSAGE FOR POWER TRANSFER UNIT APPEARED FOLLOWED BY L/H HYDRAULIC QUANITY INDICATION OF 0.00. AIRCRAFT CONTINUED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND A PINHOLE SIZE LEAK COMING FROM A CHAFED AREA OF TUBING CAUSED BY A CLAMP ON THE CASE DRAIN LINE. MAINTENANCE PERFORMED A RYNGLOK REPAIR ON TUBING IAW BMM 20-10-09, PG 801, 810, 828-831. LEAK CHECK OF REPAIR WAS GOOD UND

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,381 hrs · 24,203 cycles

PHX - MAJOR REPAIR -C- DENT FOUND IN FUSELAGE SKIN AFT OF L-2 DOOR, 3 X 3 X .156 INCH DEEP AT BS 780 AT STR 16L. AFTER ACCESSING INTERNAL AREA, STR 16L FOUND TO BE DEFORMED AND CRACKED ABOUT 1 INCH. MAINTENANCE MADE A STRINGER SPLICE REPAIR IAW B757 SRM 53-00-03, FIG 201 AND CUT OUT THE DAMAGED SKIN AREA, FABRICATED REPAIR PARTS AND INSTALLED A FLUSH REPAIR IAW B757 SRM 53-00-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,268 hrs · 24,160 cycles

PHX - C8 CK - C - CORROSION FOUND ON FLOORBEAM UPPER CAP AT BS 365.25, RBL 18, BEYOND SRM LIMITS AFTER CORROSION REMOVAL. MAINTENANCE MADE STRAP REPAIR ON FLOORBEAM UPPER CAP IAW AWA ER 19-5310-01289-KB1.

Part: CHANNEL — CORRODED · corrosion level 2 · airframe 62,268 hrs · 24,160 cycles

PHX - C8 CK - "C" - CORROSION FOUND ON FLOOR SUPPORT CHANNEL STIFFENER ON THE LOWER SIDE AROUND A NUT PLATE AT BS 400, RBL 29. MAINTENANCE REMOVED CORRODED CHANNEL, FABRICATED REPLACEMENT PART AND INSTALLED IAW B757 SRM 51-40-02, PG 1.

Part: FRAME — DENTED · airframe 62,268 hrs · 24,160 cycles

PHX - C8 CK - "C" - DENT FOUND ON UPPER FLANGE OF FRAME AT BS 1600, STR 25L. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE AND INSTALLED IAW B757 SRM 51-70-11, FIG 1, PG 1 - 7.

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 62,268 hrs · 24,160 cycles

PHX - C8 CK - "C" - CORROSION FOUND AROUND NUTPLATES ON L-1 DOOR THROUGH SUPPORT ANGLE, BS 370, LBL 60, WL 208. MAINTENANCE REMOVED SUPPORT ANGLE AND REPLACED WITH NEW PART IAW B757 SRM 51-20-01, PG 1.

Part: FRAME — DENTED · airframe 62,268 hrs · 24,160 cycles

PHX - C8 CK - "C" - DENT FOUND IN FRAME UPPER FLANGE AT BS 1540, STR 25R. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE AND INSTALLED IAW B757 SRM 51-70-11, FIG 1, PG 1 - 7.

Part: FRAME — BROKEN (AFT CARGO COMP.) · airframe 62,268 hrs · 24,160 cycles

PHX - C8 CK - "C" - E-6 EQUIPMENT RACK, CENTER LOWER I/B SUPPORT FRAME AT CARGO FLOOR LEVEL FOUND BROKEN BETWEEN BS 1440 & 1480. MAINTENANCE REMOVED DAMAGED SUPPORT, FABRICATED REPLACEMENT PART AND INSTALLED IAW B757 SRM 51-40-02, PG 1 AND BOEING DWG 284N1474.

Part: FRAME — DENTED · airframe 62,268 hrs · 24,160 cycles

PHX - C8 CK - "C" - DENT FOUND ON AFT CARGO COMPARTMENT FRAME UPPER FLANGE AT BS 1300, STR 25R. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE AND INSTALLED IAW B757 SRM 51-70-11, FIG 1, PG 1 - 7.

Part: STIFFENER — CRACKED (NR 1 PYLON) · airframe 62,268 hrs · 24,160 cycles

PHX - C8 CK - C - CRACK FOUND IN NR 1 PYLON, O/B SIDE VERTICAL STIFFENER, 1 INCH LONG AT PPS 153, PPWL 143. MAINTENANCE REMOVED AND REPLACED THE STIFFENER IAW B757 SRM 51-10-02, PG 2.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 62,268 hrs · 24,160 cycles

PHX - C8 CK - C - CRACK FOUND ON NR 1 PYLON O/B SIDE SKIN AND DOUBLER 3 INCHES LONG AT PPS 156, PPWL 140, COMMON TO LOWER CHORD. MAINTENANCE FABRICATED REPAIR DOUBLER AND INSTALLED IAW AWA ER 19-5450-01283-TB3.

Part: INTERCOSTAL — CRACKED · airframe 62,268 hrs · 24,160 cycles

PHX - C8 CK - "C" - CRACK FOUND IN INTERCOSTAL ON AFT SIDE OF FLOOR BEAM AT BS 1320, RBL 45.5, .5" LONG. MAINTENANCE REMOVED DAMAGED INTERCOSTAL, FABRICATED REPLACEMENT PART AND INSTALLED IAW B757 SRM 51-20-02, 51-40-02, PG 1 AND BOEING DWG #140N2506.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,268 hrs · 24,160 cycles

PHX - C8 CK - C - GOUGE AND CRACK FOUND IN FRAME RADIUS AT BS 1320, STR 26R, .25 INCH LONG. MAINTENANCE CUT OUT DAMAGED SECTION OF FRAME, FABRICATED REPAIR ANGLES AND FILLER AND INSTALLED IAW B757 SRM 53-60-07 AND 51-70-11.

Part: FRAME — GOUGED (FUSELAGE) · airframe 62,268 hrs · 24,160 cycles

PHX - C8 CK - C - DENT FOUND IN FRAME WITH A GOUGE IN THE RADIUS AT BS 1340, STR 26R. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE AND INSTALLED IAW B757 SRM 51-70-11 FIG 1, PG 1 - 7.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,268 hrs · 24,160 cycles

PHX - C8 CK - "C" - CORROSION FOUND ON FLOOR SUPPORT AT BS 395 TO 400, RBL 22. MAINTENANCE REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED REPLACEMENT PART IAW B757 SRM 51-40-02, PG 1 AND BOEING DWG 141N5186.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,268 hrs · 24,160 cycles

PHX - C8 CK - C - CORROSION FOUND ON TOP CAP OF FLOORBEAM AT BS 377, LBL 15 TO LBL 60, BEYOND SRM ALLOWABLE LIMITS. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM UPPER CAP, FABRICATED REPAIR PARTS AND INSTALLED IAW AWA ER 19-5311-01269-DL4.

Part: ANGLE — CORRODED · corrosion level 2 · airframe 62,268 hrs · 24,160 cycles

PHX - C8 CK - "C" - CORROSION FOUND ON FLOOR SUPPORT ANGLE AT BS 324 TO 395, RBL 60. MAINTENANCE REMOVED CORRODED SUPPORT ANGLE AND REPLACED IAW B757 SRM 51-40-02, PG1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,268 hrs · 24,160 cycles

PHX - C8 CK - "C" - CORROSION FOUND ON FLOOR SUPPORT AT BS 365, RBL 50 TO RBL 60, BEYOND SRM LIMITS AFTER CLEAN UP. MAINTENANCE REMOVED DAMAGED FLOOR SUPPORT, FABRICATED REPLACEMENT PART AND INSTALLED IAW B757 SRM 51-40-02, PG 1 AND BOEING DWG 141N5186.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,268 hrs · 24,160 cycles

PHX - C8 CK - "C" - CORROSION FOUND ON FLOOR SUPPORT AT BS 398, RBL 24 TO RBL 44, BEYOND SRM LIMITS AFTER CLEAN UP. MAINTENANCE REMOVED FLOOR SUPPORT, FABRICATED REPLACEMENT PARTS AND INSTALLED IAW B757 SRM 51-40-02, PG 1 & 51-20-01, PG 1 AND BOEING DWG 141N5186-9, -15 & -16.

Part: FRAME — DENTED · airframe 62,268 hrs · 24,160 cycles

PHX - C8 CK - "C" - DENT IN FRAME UPPER FLANGE AT BS 680, STR 24R. MAINTENANCE CUT OUT DAMAGED AREA, FRABRICATED REPAIR ANGLE AND INSTALLED IAW B757 SRM 51-70-11, FIG 1, PG 1.

Part: FRAME — DENTED · airframe 62,268 hrs · 24,160 cycles

PHX - C8 CK - "C" - DENT FOUND IN FRAME UPPER FLANGE AT BS 680, STR 23L & 24L. MAINTENANCE CUT OUT DAMAGED AREAS, FABRICATED REPAIR ANGLE AND INSTALLED IAW B757 SRM 51-70-11, FIG 1, PG 1.

Part: FRAME — DENTED · airframe 62,268 hrs · 24,160 cycles

PHX - C8 CK - "C" - DENT FOUND FWD CARGO COMPARTMENT FRAME FLANGE AT BS 660, STR 23L & 24L. MAINTENANCE CUT OUT DAMAGED AREAS, FABRICATED REPAIR ANGLE AND INSTALLED IAW B757 SRM51-70-11, FIG 1, PG 1.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 62,268 hrs · 24,160 cycles

PHX - C8 CK - C - INTERIM FUSELAGE SKIN EXTERNAL REPAIR AT BS 1180, STR 6L REQUIRES REPLACEMENT. MAINTENANCE REMOVED EXISTING REPAIR AND REPLACED WITH PERMANENT FLUSH REPAIR IAW AWA ER 19-5341-01288-TB1A.

Part: FRAME — BENT · airframe 62,268 hrs · 24,160 cycles

PHX - C8 CK - "C" - BEND IN RADIUS OF FRAME UPPER FLANGE AT BS 660, STR 24R. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE AND INSTALLED IAW B757 SRM 51-70-11, FIG 1, PG 3.

Part: SKIN — IMPROPER · airframe 62,268 hrs · 24,160 cycles

PHX - C8 CK - "C" - RIVITS ON EXTERNAL FUSELAGE SKIN REPAIR AT BS 1100, STR 6L FOUND NOT TO BE PROPERLY SEATED. MAINTENANCE REMOVED EXTERNAL REPAIR AND REPLACED WITH FLUSH REPAIR IAW AWA ER 19-5331-01274-DL1.

Part: BRACKET — CORRODED (FWD / AFT) · corrosion level 2 · airframe 62,268 hrs · 24,160 cycles

PHX - C8 CK - "C" - CORROSION FOUND ON LOWER FWD CENTER CARGO TIE DOWN FITTING FWD & AFT FACE AT BS 1556 TO 1600, STR 27R. MAINTENANCE REMOVED FITTING ASSY AND REPLACED FWD & AFT BRACKETS IAW B757 SRM 51-40-02, PG 1 AND BOEING DWG 69-45579.

Part: GOVERNOR — MALFUNCTIONED (NR 1 ENGINE) · airframe 57,850 hrs · 22,382 cycles

NR 1 ENG SURGES FROM 1.4 TO 1.7 EPR ON CLIMB. TURNED LIMITERS OFF, NO EFFECT. REPLACED NR 1 ENG FUEL FLOW GOVERNOR, LK AND OPS CK GOOD. TT 0068634 M+E=19-7320-9-0004. RECOMMENDATION: REMAIN OPEN PENDING REVIEW OF TEARDOWN REPORT, NO HISTORY.

Part: FLOORBEAM — CORRODED (BS 365.25)

DURING SCHEDULED C-6 INSPECTION, FOUND CABIN FLOORBEAM AT BS 365.25 CORRODED AT RBL 5, 12, 16, 20 AND 29. REMOVED AND REPLACED FLOORBEAM PER SRM 53-00-51.

Part: FLOORBEAM — CORRODED (BS 365.35)

DURING SCHEDULED C-6 INSPECTION, FOUND CABIN FLOORBEAM AT BS 365.35 CORRODED AT RBL 38, 45, 53 AND 59. REMOVED AND REPLACED FLOORBEAM PER SRM 53-00-51.

Part: LATCH — OUT OF ADJUST (PAX DOOR)

LEFT AFT ENTRY DOOR HANDLE WOULD NOT STAY SECURE IN FLIGHT. DOOR POPPED OPEN ON TOUCHDOWN. NO EMERGENCY DECLARED BY FLIGHT CREW. AIR RETURN TO LAS WITHOUT INCIDENT. INSPECTED DOOR AND FOUND SOFT DOOR HANDLE. C/W ADJUSTMENT AND TEST IAW MM 52-11-00 501. ADJUSTED DOOR LATCH CAMS AND HANDLE MECHANISM. FUNCTION TEST GOOD.

Part: SCAVENGE LINE — LOOSE (NR 1 ENGINE)

EICAS MESSAGE AND LOW OIL PRESSURE LIGHT ON NR 1 ENGINE. ENGINE SHUT DOWN IN FLIGHT, AIR TURNBACK. OPENED COWLING AND C-DUCTS, FOUND SCAVENGE LINE LOOSE. RETIGHTENED AND SAFETIED. CHECKED MAGNETIC CHIP DETECTORS REF MM 79-21-03. CHECKED SCAVENGE AND PRESSURE FILTERS REF MM 79-32-00. NO DEFECTS NOTED. SERVICED OIL, ACCOMPLISHED ENGINE RUNS. NO LEAKS NOTED, CLOSED COWLS AND C-DUCTS.

Part: FUSE — BLOWN (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND LEFT AFT SIDE SEAT EMERGENCY LIGHTS INOP FROM MID-LAVS TO AFT GALLEY. 4L AND 4R LOWER EMERGENCY LIGHTS INOP ALSO. REMOVED AND REPLACED BAD FUSE IN POWER SUPPLY SYSTEM. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND BULLNOSE EMERGENCY LIGHTS AT 3L, 4L AND 7L INOP. CHARGED EMERGENCY LIGHT BATTERY. OPS CHECK GOOD.

Part: BLEED VALVE — LEAKING (APU)

FLIGHT ATTENDANTS REPORTED LOUD BANG AND ACCOMPANYING VIBRATION IN AFT GALLEY AREA. FUMES IN AFT GALLEY. ASSOCIATED LEFT DUCT LEAK LIGHT ILLUMINATED IN COCKPIT. FOUND APU BLEED VALVE LEAKING, RESECURED. OPS CHECK GOOD.

Part: HYD LINE — BROKEN (RT MLG)

LEFT HYDRAULIC SYSTEM QUANTITY DECREASED TO .06. AIRCRAFT RETURNED TO PHX. EMERGENCY LANDING DECLARED. FOUND BROKEN HYDRAULIC LINE AT RIGHT MAIN LANDING GEAR DOWNLOCK ACTUATOR. REMOVED AND REPLACED HYDRAULIC LINE, LEAK CHECK GOOD.

Part: PLUG — DISCONNECTED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS AT SEAT 14C INOP. CONNECTED PLUG, OPS CHECK NORMAL.

Part: FRAME — CRACKED (E/E BAY DOORWAY)

DURING ROUTINE MAINTENANCE CHECK, FOUND E/E BAY DOOR FRAME CRACKED THROUGH FASTENER HOLE AT BUMPER PAD ON RT FWD CORNER, PANEL NR 119BL. FABRICATED AND DRILLED REPAIR DOUBLER AND INSTALLED PER ER 5-52-41-01.

Part: STRINGER — CORRODED (BS 1470)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR SUPPORT STRINGER BS 1470, RBL 2. REMOVED DAMAGED FLOOR SUPPORT SECTION. FABRICATED AND INSTALLED NEW SUPPORT PER IAW, SRM 51-70-12.

Part: STRINGER — CORRODED (BS 1470)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR SUPPORT BS 1470, LBL 16. REMOVED CORRODED SECTION. FABRICATED AND INSTALLED REPAIR PARTS ON FLOOR SUPPORT STRINGER AT BS 1470, LBL 16 AS PER SRM 51-70-11.

Part: SEAT TRACK — GOUGED (BS 1480)

DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT TRACK GOUGED AT BS 1480, LBL 45, WL 208. BLENDED SEAT TRACK, FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK. FABRICATED AND INSTALLED NEW SEAT TRACK IAW, SRM 53-00-52.

Part: STRINGER — CORRODED (BS 1510)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON LOWER SURFACE FLOOR SUPPORT STRINGER BS 1510, RBL 2. REPAIRED FLOOR SUPPORT STRINGER BS 1510, RBL 2 PER SRM 51-7-012.

Part: SUPPORT — CORRODED (BS 1410-1530)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON LOWER SURFACE OF FLOOR SUPPORT SIDE PANEL BS 1410 - 1530, LBL 20. REMOVED DAMAGED AREA OF FLOOR. FABRICATED AND INSTALLED SIDEWALL SUPPORT IAW, SRM 51-40-2.

Part: STRINGER — CORRODED (BS 1510)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON LOWER SURFACE (AFT CARGO) FLOOR SUPPORT STRINGER BS 1510, RBL 11. REPAIRED FLOOR SUPPORT STRINGER BS 1510, RBL 11 PER SRM 51-70-12.

Part: STRINGER — CORRODED (BS 1510)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON LOWER SURFACE FLOOR SUPPORT STRINGER BS 1510, LBL 7, WL 146. REMOVED DAMAGE 2 BY 1 TO MAXIMUM DEPTH OF .017 FROM ORIGINAL THICKNESS OF .063. OUT OF LIMITS PER SRM 53-00-03. REPAIRED FLOOR SUPPORT STRINGER BS 1510, LBL 7 PER SRM 51-70-12.

Part: STRINGER — CORRODED (BS 1290 - 1440)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON LOWER SURFACE OF FLOOR SUPPORT STRINGER BS 1328 - 1331, LBL 3, WL 146. REMOVED CORROSION FROM AREA 7 BY 1 TO A MAXIMUM DEPTH OF .025 FROM ORIGINAL THICKNESS OF .063. OUT OF LIMITS IAW SRM 53-00-03. REPAIRED FLOOR SUPPPORT STRINGER FROM BS 1298 - 1440, LBL 3 PER SRM 51-70-12.

Part: STRINGER — CORRODED (BS 1495)

DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR SUPPORT STRINGER BS 1495 - 1548, RBL 6 CORRODED. REPAIRED FLOOR SUPPORT STRINGER AT BS 1495 - BS 1548, RBL 6 PER SRM 51-70-12.

Part: STRINGER — CORRODED (BS 1328-1334)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON LOWER SURFACE FLOOR SUPPORT STRINGER BS 1328 - 1334, RBL 15. FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR PARTS PER SRM 51-70-12.

Part: STRINGER — CORRODED (BS 1343-1369.5)

DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR SUPPORT STRINGER BS 1343 - 1369.5, RBL 7 CORRODED. REMOVED, FABRICATED AND INSTALLED FLOOR SUPPORT STRINGER FROM BS 1343 TO BS 1369.5, RBL 7.

Part: STRINGER — CORRODED (BS1380-1334)

DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR SUPPORT STRINGER BS 1328 - 1334, LBL 7 HAS CORROSION ON LOWER SURFACE (AFT CARGO). REMOVED CORRODED FLOOR SUPPORT STRINGER AND FABRICATED REPAIR PARTS BS 1242 - 1343, LBL 7 PER SRM 51-70-12.

Part: STRINGER — CORRODED (BS 1343-1445)

DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR SUPPORT STRINGER BS 1343 - 1445, RBL 15 CORRODED. REPAIRED DAMAGED FLOOR SUPPORT STRINGER AT BS 1343 - 1445, RBL 15, IAW, SRM 51-70-11, 51-40-02.

Part: STRINGER — CORRODED (BS 1328 - 1337)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON LOWER SURFACE OF FLOOR SUPPORT STRINGER BS 1328 - 1337, RBL 10. FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR PARTS PER SRM 51-70-12.

Part: SIDE PANEL — CORRODED (BS 1380-1440)

DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR SUPPORT AT AFT CARGO DOOR BS 1380 - 1440, RBL 20 HAS CORROSION, UPPER AND LOWER SURFACES F AND R AFT CARGO FLOOR SUPPORT BS 1380 - 1440, RBL 20, IAW, SRM 51-40-02 AND OHM 20-50-01.

Part: STRINGER — CORRODED (BS 1495-1549)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON LOWER SURFACE FLOOR SUPPORT STRINGER BS 1495 - 1549, LBL 3, WL 146. REMOVED DAMAGE IN AREA 2 BY 1. FOUND CORROSION TO EXTEND COMPLETELY THROUGH MATERIAL. OUT OF LIMITS PER SRM 53-00-03. REPAIRED FLOOR SUPPORT STRINGER AT BS 1495 - BS 1549, LBL 3 PER SRM 51-70-12.

Part: STRINGER — CORRODED (BS 1510)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON LOWER SURFACE OF FLOOR SUPPORT STRINGER BS 1510, LBL 12, WL 146. REMOVED DAMAGE IN AREA OF 2 BY 1 TO A MAXIMUM DEPTH OF .021 FROM ORIGINAL OF .063. OUT OF LIMITS PER SRM 53-00-03. REPAIRED FLOOR SUPPORT STRINGER AT BS 1495 - BS 1549, LBL 12 PER SRM 51-70-12.

Part: STRINGER — CORRODED (BS 1347-1460)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON LOWER SURFACE OF FLOOR SUPPORT STRINGER BS 1347, RBL 10. REMOVED DAMAGED FLOOR SUPPORT STRINGER AND INSTALLED FABRICATED FLOOR SUPPORT STRINGER BS 1343 - 1460, RBL 10.45 PER SRM 51-10-00, SRM 51-30-02 AND SRM 53-00-53, 53-60-05.

Part: STRINGER — CORRODED (BS 1328-1331)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON LWR SURFACE (AFT CARGO) FLOOR SUPPORT STRINGER BS 1328 - 1331, LBL 11. REPAIRED CORRODED FLOOR SUPPORT STRINGER BS 1290 TO 1343, LBL 11 AS PER SRM 51-70-12.

Part: STRINGER — CORRODED (BS 1328-1331)

DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR SUPPORT STRINGER BS 1328 - 1331, RBL 2 HAS CORROSION ON LOWER SURFACE, AFT CARGO. REMOVED STRINGER FROM BS 1200 - BS 1343. FABRICATED AND INSTALLED REPAIR PARTS IAW, SRM 51-70-12.

Part: STRINGER — CORRODED (BS 1470)

DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR SUPPORT STRINGER BS 1470, RBL 15 CORRODED. REMOVED CORRODED SECTION. FABRICATED AND INSTALLED REPAIR PART IAW, SRM 51-70-11.

Part: STRINGER — CORRODED (BS 1328-1334)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON LOWER SURFACE (AFT CARGO) FLOOR SUPPORT STRINGER BS 1328 - 1334, LBL 16. REMOVED DAMAGED AREA IAW, SRM 51-40-02. FABRICATED AND INSTALLED REPAIR PARTS.

Part: SUPPORT — CORRODED (BS 1470)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON LOWER SURFACE FLOOR SUPPORT BS 1470, RBL 10. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS AND INSTALLED PER SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1260-1310)

DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR SUPPORT SIDE PANEL BS 1260 - 1310, RBL 20 HAS CORROSION LOWER SURFACE. REPAIRED DAMAGED FLOOR SUPPORT AT BS 1260 - 1310, RBL 20, IAW 53-00-53, 51-70-11, 51-40-02.

Part: SUPPORT — CORRODED (BS 1310-1380)

DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR SIDEWALL SUPPORT PANEL CORRODED BS 1310 - BS 1380, RBL 20. CUT OUT DAMAGED SECTION, FABRICATED AND INSTALLED NEW PART PER AWER 5-53-10-01.

Part: STRINGER — CORRODED (BS 1470)

DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON LOWER SURFACE FLOOR SUPPORT STRINGER BS 1470, RBL 7. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED REPAIR PARTS IAW, SRM 51-70-11.

Part: CONNECTOR — DIRTY (RUDDER TRIM)

CREW REPORT ON FINAL, FIRST OFFICER REQUESTED CAPTAIN TO RETURN RUDDER TRIM TO ZERO. CAPTAIN REPORTED WITH TRIM AT 1.5 UNITS TO RIGHT, THE RUDDER TRIM WOULD NOT RESET. CAPTAIN SELECTED TO LEFT, NO MOVEMENT, RESELECTED TO RIGHT, NO MOVEMENT. AIRCRAFT LANDED WITHOUT INCIDENT. CLEANED AND RESEATED THE C/PS ON THE AILERON AND RUDDER TRIM PANEL. OPERATIONS CHECK OK, NO FURTHER PROBLEMS.

Part: FUSE — BLOWN (CABIN)

PHX - FLT 0001 - DURING ROUTINE MAINTENANCE CHECK, FOUND AFT ROW EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE IN AFT BATTERY PACK ASSEMBLY. OPERATIONS CHECK GOOD AT THIS TIME. (X)

Part: FIRE DETECTOR — DIRTY (CARGO COMPT)

ATL/PHX - FLT 0610 - ABORTED TAKEOFF. CREW ABORTED TAKEOFF AT 135 KNOTS WHEN THE AFT CARGO FIRE WARNING WENT OFF WITH ASSOCIATED WARNING BELL. INSPECTED AFT PIT BAGGAGE PIT AND PERFORMED SYSTEM TEST OF CARGO WARNING FIRE DETECTION SYSTEM. FOUND DETECTORS AND DUCTS DIRTY. CLEANED DETECTORS AND DUCTS. (X)

Part: TAT PROBE — FAILED (COCKPIT)

PHX - FLT NR 3808 - AIR-TURNBACK - EICAS MESSAGE FOR TAT. LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED TAT PROBE. ALSO, REPLACED RELAYS K203 AND K410, PRECAUTIONARY. (M)

Part: FLOOR — CORRODED (BS 1691)

PHX - DURING SCHEDULED C4 INSPECTION, FOUND FLOOR PAN AT BS 1691 TO BS 1710 LBL 55 CORRODED. INSTALLED REPAIR IAW ER 5-53-16-11. (M)

Part: THRESHOLD — CORRODED (BS 1661)

PHX - DURING SCHEDULED C4 INSPECTION, FOUND CORROSION ON FLOOR BEAM AT STATION 1661 LBL 45 TO L4 DOOR THRESHOLD. INSTALLED REPLACEMENT T-CAP AND REPAIR PARTS PER SRM 53-00-51, FIGURE 203. (M)

Part: SEAT TRACK — CORRODED (BS 1640)

PHX - DURING SCHEDULED C4 INSPECTION, FOUND SEAT TRACK CORRODED AT STATION 1640 LBL 45. FABRICATED AND INSTALLED SEAT TRACK IAW SRM 51-10-00 AND SRM 51-40-02. (M)

Part: FLOOR — CORRODED (FS 1681-1740)

PHX - DURING SCHEDULED C4 INSPECTION, FOUND AFT GALLEY FLOOR PAN CORRODED IN NUMEROUS AREAS FROM STATION 1681.8 THROUGH STATION 1740, RBL 2 THROUGH LBL 55. REPAIRED PER ER 5-53-16-11. (M)

Part: EEL BATT PACK — DISCHARGED (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND R3 DOOR EXTERIOR AND MIDDLE EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M)

Part: EEL BATT PACK — INOPERATIVE (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND LT MID SECTION EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT R2 DOOR. OPS CHECK GOOD. (M)

Part: HYD PUMP — LEAKING (LT ENGINE)

PHX-JFK - FLT 294 - EN ROUTE PILOT REPORTED, EICAS MESSAGE 'LT ENGINE HYD PUMP FAULT' AND ASSOCIATED OVERHEAD SWITCH FAULT. EICAS MESSAGE FOR LOW QUANTITY LT SYS HYD APPREARED. DURING DESCENT INTO JFK, THE T/E FLAPS STUCK BETWEEN 0 AND 1 UNIT, AFTER SELECTING 1 UNIT. ALTERNATE FLAP DRIVE METHOD USED, FLAPS DID NOT RESPOND. GEAR HANDLE SELECTED DOWN, GEAR DID NOT RESPOND, GEAR WAS MANUALLY EXTENDED. MAINTENANCE REPLACED LEAKING LT HYD PUMP AND FLUSHED SYSTEM. OPERATIONAL AND LEAK CHECK GOOD. MAINTENANCE RESET FLAP/SLAT ELECTRONIC UNIT, OPERATIONAL CHECK GOOD. LANDING GEAR EXTENDED MANUALLY DUE TO LOSS OF LT HYD QTY, NO ACTION REQUIRED PER BOEING MM. (W)

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE IN FORWARD CABIN. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M)

Part: PRESSURE SWITCH — FAILED (LT HYD MODULE)

LAS-JFK - FLT 297 - AIR TURNBACK DUE TO LOSS OF LT HYDRAULIC SYSTEM FLUID, EICAS MESSAGE INDICATED FLUID LEVEL DROPPED TO .25. ACFT RETURNED TO LAS AND LANDED WITHOUT FURTHER INCIDENT. MX FOUND PRESSURE SWITCH ON LT HYDRAULIC MODULE IN LT PYLON DEFECTIVE. REMOVED AND REPLACED PRESSURE SWITCH. HYDRAULIC SYSTEM SERVICED, OPS AND LEAK CHECK GOOD. ACFT RETURNED TO SERVICE. (W)