N908AW

Part: WARNING LIGHT — FALSE ACTIVATION (MLG) · airframe 93,111 hrs · 30,128 cycles

GEAR DISAGREE MESSAGE & FWD LIGHT APPEARED DURING GEAR EXTENSION. ABORTED APPROACH. RETRACTED GEAR, DURING GO AROUND MSG WENT OUT & DID NOT REAPPEAR. PREFORMED BITE TEST ON PSEU IAW AMM 32-09-03-815-804 WITH NO FAULTS OR DISCREPANCIES NOTED. ACFT GOOD FOR SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 92,917 hrs · 30,083 cycles

FLASHLIGHT AT L2 DOOR INOPERATIVE, NO FLASHING RED INDICATOR. REPLACED FLASHLIGHT BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: WIRE — BROKEN (CABIN) · airframe 92,441 hrs · 29,976 cycles

FLIGHT 583 SEAT MOUNTED EMER LIGHT INOPERATIVE AT SEAT 19C. FOUND WIRE BROKEN. R & R SEAT MOUNTED EMER LIGHT ASSEMBLY AT SEAT 19C. OPERATIONAL CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 92,044 hrs · 29,891 cycles

AFT GALLEY FLIGHT ATTENDANT EMER FLASHLIGHT NO LED FLASH. REPLACED FLASHLIGHT.

Part: LATCH — OUT OF ADJUST (O2 BOX) · airframe 91,629 hrs · 29,815 cycles

FORWARD LAVATORY O2 DOOR LATCH ACTUATOR FAILED TEST, COULD NOT RESET. ADJUSTED LATCH MECHANISM AS REQUIRED. OPERATIONS OK.

Part: PIN — WORN (NLG) · airframe 91,358 hrs · 29,754 cycles

NOSE LANDING GEAR RT TRUNNION PIN WORN. REPLACED TRUNNION PIN.

Part: PIN — WORN (NLG) · airframe 91,358 hrs · 29,754 cycles

NOSE LANDING GEAR LT TRUNNION PIN WORN. REPLACED TRUNNION PIN.

Part: MODULE — FAULTY (ZONE 100) · airframe 91,355 hrs · 29,749 cycles

FLIGHT 663 EN-ROUTE, EICAS MSG & AUDIO ALARM. GEAR NOT DOWN RED CONFIGURATION LIGHT, RED WARNING LIGHT ON GLARE SHIELD. GEAR HANDLE UP & OFF, NO CHANGE. PRESSED GND PROX & CONFIG GEAR OVERRIDE TO TURN OFF AUDIO WARNING ALARM. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. REPLACED THE LANDING CONFIGURATION WARNING MODULE M983. OPERATIONALLY CHECKED GOOD.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 91,250 hrs · 29,727 cycles

C4 CHECK, STRINGER AT STRINGER 13R CRACKED AT BS 619. REPAIRED CRACKED STRINGER IAW EA 250005.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 91,250 hrs · 29,727 cycles

C4 CHECK, L4 DOOR FUSELAGE UPPER LOBE INTERIOR FRAME & SKIN SHEAR TIE HAS 0.5 INCH CRACK NEXT TO RADIUS AT STATION 1661 BETWEEN STRINGER 5L & 6L. R & R SHEAR TIE IAW SRM 51-40-02 & DWG 146N1024.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 91,250 hrs · 29,727 cycles

C4 CHECK, CRACK IN INTERCOSTAL BETWEEN STATION 680 & 685 BELOW STRINGER 11L, FWD OF L2 DOOR IN RADIUS NEXT TO SKIN. R & R CRACKED INTERCOSTAL IAW SRM 51-10-02 & DWG N8338.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 91,250 hrs · 29,727 cycles

C4 CHECK, FLOORBOARD SUPPORT ANGLE CRACKED BETWEEN STATION 780 & 800 AT BL 0. FABRICATED & INSTALLED NEW ANGLE IAW DWG 143N5140.040 7075 T6 FROM BAC1493-412.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,250 hrs · 29,727 cycles

C4 CHECK, CORROSION ON GALLEY SUPPORT FITTING AT STATION 398, RBL 14. R & R SUPPORT FITTING IAW DWG 141N5186 & SRM 51-10-02 51-40-02.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,250 hrs · 29,727 cycles

C4 CHECK, CORROSION ON GALLEY AREA FLOOR STRUCTURE AT STATION 398, RBL 20. R & R CHANNEL IAW DWG 141N5186 & SRM 51-10-02 51-40-02.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 91,250 hrs · 29,727 cycles

C4 CHECK, CORROSION ON INNER ATTACH FLANGE OF KEEL BEAM IN RT WW AT APPROX STATION 1120 & RBL 10. REPAIRED IAW EA 106566.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 91,250 hrs · 29,727 cycles

C4 CHECK, CORROSION ON FLOORBEAM T CAP AT BS 365 & RBL 45.5. REPAIRED FLOORBEAM T CAP IAW SRM 53-00-51-2R PROCEDURE 10.

Part: FRAME — CRACKED (BS 1400) · airframe 91,250 hrs · 29,727 cycles

C4 CHECK, CRACK FOUND ON FRAME AT BS 1400, LT STRINGER 24. REMOVED DAMAGED AREAS OF FRAME. FABRICATED REPAIR SECTION OF FRAME & TWO DOUBLERS. INSTALLED REPAIR & FASTENERS IAW EA 250014.

Part: SLIDE — UNSERVICEABLE (R4 DOOR) · airframe 90,400 hrs · 29,558 cycles

R4 DOOR SLIDE OUT OF GREEN BAND. R & R R4 DOOR EVACUATION SLIDE. REPAIRED SLIDE. UNIT WAS PARTIALLY DISASSEMBLED, CLEANED & INSPECTED, REPLACING ALL PARTS NECESSARY FOR REPAIR. PASSED LIGHT SYS TEST & HEIGHT CHECK. OVERHAULED & CHARGED RESERVOIR & VLV ASSEMBLY. PASSED HYDDRO, PULL FORCE & LEAK TEST. RE-BANDED SLIDE FOR OVEN CYCLE.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 90,319 hrs · 29,544 cycles

RON REPLACE THE CAPTAINS NR 3 WINDOW FOR DELAMINATION. R & R CAPTAINS NR 3 WINDOW IAW AMM 56-11-10-424-015. PERFORMED WINDOW HEAT TEST IAW AMM 30-11-00-715-001.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 89,106 hrs · 29,319 cycles

AFT GALLEY COFFEE MAKERS REPORTED TO HAVE ELEC SMOKE SMELL WHEN TURNED ON, REMAINED OFF DURING FLIGHT. COULD NOT DISTINGUISH WHICH POSITION ON BOTH. REPLACED ALL COFFEE MAKERS IN AFT GALLEY. OPERATIONS CHECKED NORMAL.

Part: ACCESS DOOR — MISSING (NR 1 COWLING) · airframe 88,397 hrs · 29,185 cycles

FLT 693 NR 1 ENG OIL SERVICE DOOR MISSING AFTER FLIGHT. REPLACED NR 1 ENG OIL SERVICE DOOR IAW SRM 51-40-02. OK FOR SERVICE.

Part: DOOR — MISSING (NR 1 COWLING) · airframe 88,397 hrs · 29,185 cycles

OIL FILL DOOR MISSING NR 1 ENG AFTER FLIGHT. REPLACED NR 1 ENG OIL SERVICE DOOR IAW SRM 51-40-02. OK FOR SERVICE.

Part: SKIN PANEL — DELAMINATED (LT HORIZ STAB) · airframe 87,590 hrs · 29,032 cycles

C1 CHECK DELAMINATION ON LT HORIZONTAL SKIN UPPER SURFACE INBD PANEL AT STAB STATION 224.249 APPROXIMATELY 6 INCHES FROM LE. REPLACED LT HORIZONTAL UPPER INBD PANEL IAW SRM 51-40-02, EA 105500 & EA 105582.

Part: WIRE HARNESS — DISCONNECTED (CABIN) · airframe 85,199 hrs · 28,525 cycles

PHX - SEAT ROW 35 C EMERGENCY SEAT LIGHTS INOP. RELAMPED, NO HELP. CHANGED LIGHT ASSY, NO HELP. CONNECTED SEAT HARNESS, OPS CHECK GOOD.

Part: DOOR FRAME — CRACKED (L2 DOOR) · airframe 83,272 hrs · 28,121 cycles

C2 CHECK - CRACK ON L2 UPPER HINGE CUTOUT AT FORWARD DOOR FRAME. REPAIRED L2 UPPER HINGE CUTOUT AT FORWARD DOOR FRAME IAW B757 SRM 52-10-02-2R-1.

Part: SKIN — DEBONDED (LE SLAT) · airframe 83,272 hrs · 28,121 cycles

C2 CHECK - DISBONDING ON UPPER TRAILING EDGE SURFACE OF NR 3 SLAT AT INBOARD CORNER. REPAIRED NR 3 SLAT UPPER SURFACE IAW B757 SRM 51-70-10 & TYPICAL REPAIR TR-757-5130-10-0058.

Part: ATTACH FITTING — SEVERED (NR 1 PYLON) · airframe 82,470 hrs · 27,962 cycles

PYLON FITTING INSPECTION - NR 1 ENGINE INBOARD C DUCT AFT MOUNT PYLON ATTACH FITTING CENTER LUG UPPER MATERIAL SEVERED. REPLACED NR 1 ENGINE INBOARD C DUCT AFT MOUNT PYLON ATTACH FITTING AT PP STA 174.30 IAW EA 202636, EA 202610A AND EO 5408R114.

Part: LOCK PIN — WORN (COCKPIT SEAT) · airframe 81,837 hrs · 27,837 cycles

FLT 23. F/O SEAT LATERAL ADJUSTMENT LOCKING MECHANISM NOT LOCKING PROPERLY SEAT UNLOCKED AND SLID AFT DURING CLIMB. REMOVED AND REPLACED SEAT. SHOP FOUND GUIDE STRAP WORN, HARDWARE WORN/MISSING, LABELS MISSING, ARMREST PADS TORN, END PLUGS WORN, GROMMETS MISSING, PINS WORN, CLAMPS WORN, BUNGEES WEAK, LINKS DAMAGED, GUIDE BLOCK CRACKED, FAIRINGS CRACKED, SUPPORTS CRACKED, ROLLERS WORN, WEB STOPS CRACKED, HANDLE DAMAGED, REFINISH. REPAIRED UNIT.

Part: HINGE FITTING — CRACKED (NR 2 PYLON) · airframe 81,711 hrs · 27,816 cycles

PHX VISUAL - NR 2 ENGINE OUTBOARD `C` DUCT AFT MOUNT PYLON ATTACH FITTING, CENTER LUG CRACKED APPROX 1 INCH. REPLACED NR 2 ENGINE OUTBOARD THRUST REVERSER AFT HINGE FITTING IAW EA 201955 & EO 5408R114.

Part: WIRE HARNESS — FAULTY (CABIN)

PHX - AISLE SEAT 8L EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE HARNESS ON ROW 8L EMERGENCY LIGHTS. OPS CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (L4 DOOR)

PHX - THE L4 DOOR ASSIST BOTTLE READS LOW ON PRESSURE. MAINTENANCE REMOVED AND REPLACED THE L4 DOOR ASSIST BOTTLE.

Part: BEARING — FAILED (LT ENGINE)

SAT EN-ROUTE CUN TO PHX. ABOUT 20 MINUTES FROM SAT, IT WAS DETERMINED THAT THE LEFT ENGINE OIL QUANTITY AND PRESSURE WERE DROPPING. THE CAPTAIN SHUT DOWN THE LEFT ENGINE AND DIVERTED TO SAT. SINGLE ENGINE TIME WAS APPROXIMATELY 20 MINUTES. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE. ENGINE OIL EXITED THROUGH A CRACK IN THE RADIAL DRIVE SHAFT SHROUD TUBE. MASTER AND HIGH SPEED GEARBOX MAGNETIC CHIP DETECTORS CONTAINED METAL. REMAINS OF THE STEADY BEARING WERE FOUND IN THE RADIAL DRIVE SHAFT FAIRING CAVITY. THE FAILURE IS SURMISED TO BE DUE TO THE FAILURE OF THE STEADY BEARING.

Part: BEARING — SMOKE (ZONE 400)

FLT 432, WHILE IN CRUISE FLIGHT, EXPERIENCED SMOKE IN THE COCKPIT AND CABIN. THE COCKPIT CREW SELECTED LEFT BLEED WITH PACK OFF, WHICH RESULTED IN SMOKE REDUCTION. THE FLIGHT DIVERTED TO SFO. AFTER LANDING, THE LT ENGINE OIL QUANTITY WENT TO ZERO WHILE ALL OTHER ENGINE PARAMETERS WERE NORMAL. MAINTENANCE R & R LT ENGINE. THE STEADY BEARING FOR THE RADIAL DRIVESHAFT FAILED, CAUSING A CRACK IN THE RADIAL DRIVE SHAFT TUBE THAT ALLOWED OIL TO LEAK THROUGH. AS THE FAILURE PROGRESSED, METAL AND OTHER MATERIAL BUILT UP IN THE OIL SCAVENGE PUMP, CAUSING A BUILD UP OF OIL. THE OIL BREACHED THE LABYRINTH SEALS AND LED TO THE OIL VAPORS IN THE CABIN.

Part: FAN — FAULTY (CABIN RECIRC)

PHX FLT 23 EN ROUTE HNL TO PHX. AN UNUSUAL ODOR COMING FROM THE GASPER VENTS OVER ROW 19, AIRCRAFT LEFT, WAS NOTICED. THE ODOR WAS DESCRIBED AS SIMILAR TO BURNING RUBBER, OR OIL ODOR. SMELL STOPS WITH THE GASPER VENT CLOSED. NO SMOKE OR HOT FLOOR, SIDEWALL, OR CEILING PANELS. THE ODOR DISSIPATED AFTER 30 MINUTES. FOUND THE LEFT RECIRCULATION FAN BAD. REMOVED AND REPLACED THE LEFT RECIRCULATION FAN. ALSO, REPLACED LEFT AND RIGHT RECIRCULATION FILTERS. SMELL IN CABIN CAME FROM UNIT BEING CONTAMINATED WITH SOOT. BOX CRACKED AND PLUG BENT FROM CUSTOMER DAMAGE. IMPELLER HAD BROKEN BLADE.

Part: SLAT — CORRODED (LT WING) · airframe 74,953 hrs · 26,483 cycles

PHX - A-CHECK - MAJOR REPAIR - CORROSION ON NR 2 SLAT AT WS 594. REPAIR COMPLETED.

Part: AIR FILTER — DIRTY (CABIN)

PHX FLT 9254 MCN TO PHX. DURING DESCENT, ODOR IN CABIN/FLT DECK. ODOR CLEARED WHEN POWER ABOVE IDLE THRUST, NOT BELIEVED TO BE ELECTRICAL OR PETROLEUM. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED RECIRCULATION FILTERS.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - MAJOR REPAIR - CRACK AT NR 1 PYLON OUTBOARD THRUST REVERSER AFT MOUNT FITTING UPPER AFT FASTENER HOLE AT 12:30 POSITION ON PYLON ALUMINUM OUTER SKIN ONLY. REPAIRED NR 1 PYLON OUTBOARD THRUST REVERSER AFT MOUNT FITTING SKIN IAW EA 130334.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - MAJOR REPAIR - CRACK AT NR 1 PYLON INBOARD THRUST REVERSER AFT MOUNT FITTING UPPER AFT FASTENER HOLE AT 12:30 POSITION ON PYLON ALUMINUM OUTER SKIN ONLY. REPAIRED NR 1 PYLON INBOARD THRUST REVERSER AFT MOUNT FITTING SKIN IAW EA 130334.

Part: SOCKET — DAMAGED (CABIN) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - EEL - EMERGENCY EXTERIOR DOOR LIGHT NOT ILLUMINATING AT THE R-3 & L-2 DOORS. REPLACED SOCKETS IN D74 PIN 9 & D72 PIN9 IAW BSWPM 20-60-02, OPS CHECK GOOD.

Part: PIN — NOT SEATED (EMERGENCY LIGHTS) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - EEL - EMERGENCY ESCAPE PATH LIGHTS AND EMERGENCY EXIT IDENTIFIER LIGHT QUIT WORKING. RESEATED PIN ON CONNECTOR ON LEFT EMERGENCY EXIT SIGN, OPS CHECKED GOOD IAW B757 AMM 33-51-11-3.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - EEL - BULLNOSE EMERGENCY LIGHT NOT FUNCTIONING AT ROWS 5L, 17L, 30L, 22R & 18R. REPLACED EMERGENCY POWER SUPPLY FUSE, BULLNOSE EMERGENCY LIGHT ROWS 5L, 17L, 30L, 22R & 18R. OPS CHECK GOOD IAW B757 AMM 33-51-05-2.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - MAJOR REPAIR - CRACK ON CHORD BETWEEN BS 1480 TO BS 1500. REPLACED CHORD BETWEEN BS 1480 TO BS 1500 IAW B757 SRM 51-40-02 & BOEING DRAWING 146N5448.

Part: FITTING — CORRODED (FUSELAGE) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - MAJOR REPAIR - CORROSION ON CLIP AT BS 1380, RBL 20. REPLACED CLIP AT BS 1380, RBL 20 IAW B757 SRM 51-40-05 & 53-00-53.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - MAJOR REPAIR - CORROSION ON SHEAR TIE AT BS 1380, S27R, RBL 20. REPLACED SHEAR TIE AT BS 1380, S27R, RBL 20 IAW B757 SRM 51-40-05 & 53-00-53.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - EEL - FLIGHT ATTENDANTS FLASHLIGHT INOP AT L-2 DOOR (2 EACH). REPLACED L-2 DOOR FLIGHT ATTENDANTS FLASHLIGHT BATTERIES (2 EACH) AS REQUIRED.

Part: INTERCOSTAL — CORRODED (ZONE 100)

CORROSION ON INTERCOSTAL UPPER CHORD BETWEEN BS1360, WL514, RBL20. REPLACED INTERCOSTAL UPPER CHORD BETWEEN BS1360 TO BS1380, WL514, RBL20 IAW SRM 51-40-02. (K)

Part: SHEAR TIE — CORRODED (ZONE 100)

CORROSION ON SHEAR TIE AT BS1380, WL145, RBL20. REPLACED SHEAR TIE AT BS 1380, WL145, RBL20 IAW SRM 51-40-02 AND DWG 146N5421. (K)

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - MAJOR REPAIR - CRACK ON CHORD AT FLOOR LEVEL AT BS 1360, S17R, WL 208. REPLACED CHORD AT FLOOR LEVEL AT BS 1360, S17R, WL 208 IAW B757 SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - MAJOR REPAIR - CRACK ON CLIP AT BS 1526, BL 0. REPLACED CLIP AT BS 1526, BL 0 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 73,707 hrs · 76,227 cycles

MCN - C4 - MAJOR REPAIR - CRACK ON UPPER CHORD FLOOR SUPPORT INTERCOSTAL WEB BETWEEN BS 1620 TO BS 1640, BL 0. REPLACED FLOOR SUPPORT INTERCOSTAL WEB BETWEEN BS 1620 TO BS 1640, BL 0 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - MAJOR REPAIR - CRACK ON INTERCOSTAL UPPER CHORD AT BS 1661, RBL 10. REPLACED INTERCOSTAL UPPER CHORD AT BS 1661, RBL 10 IAW B757-200 SRM 51-40-02 AND SRM 53-60-51.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 73,707 hrs · 76,227 cycles

MCN - C4 - MAJOR REPAIR - EXFOLIATION CORROSION ON FLOOR SUPPORT CHANNEL BETWEEN BS 1300 TO BS 1318, RBL 21.5. REPLACED FLOOR SUPPORT CHANNEL BETWEEN BS 1300 TO BS 1318, RBL 21.5 IAW B757 SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - MAJOR REPAIR - CRACK ON CLIP AT BS 1429, BL 0. REPLACED CLIP AT BS 1429, BL 0 IAW B757-200 SRM 51-40-02 AND BOEING DRAWING 140N2505.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - MAJOR REPAIR - EXFOLIATION CORROSION ON FLOOR SUPPORT CHANNEL BETWEEN BS 1660 TO BS 1681, BL 0. REPLACED FLOOR SUPPORT CHANNEL BETWEEN BS 1660 TO BS 1681, BL 0 IAW B757 SRM 51-40-02.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - MAJOR REPAIR - CRACK ON SHEAR WEB BETWEEN BS 1320 TO BS 1340, RBL 45.5. REPLACED SHEAR WEB BETWEEN BS 1320 TO BS 1340, RBL 45.50 IAW B757 SRM 51-40-02 & BOEING DRAWING 140N2506.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,510 hrs · 43,450 cycles

MCN - C4 - MAJOR REPAIR - CORROSION ON CABIN LONGITUDINAL FLOORBEAM UPPER CAP AT BS 330 BETWEEN RBL 24 TO RBL 25. REPLACED CABIN LONGITUDINAL FLOORBEAM AT BS 330 BETWEEN RBL 24 TO RBL 25 IAW B757 SRM 51-40-02 & 53-00-51.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - MAJOR REPAIR - CRACK ON VERTICAL STIFFENER AT BS 1320, LBL 45.50. REPLACED VERTICAL STIFFENER AT BS 1320, LBL 45.50 IAW B757-200 SRM 51-40-02.

Part: WEB — CORRODED (FUSELAGE) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - MAJOR REPAIR - EXFOLIATION CORROSION ON WEB BETWEEN BS 1320 TO BS 1350, S17L. REPLACED WEB BETWEEN BS 1320 TO BS 1350, S17L IAW B757 SRM 51-40-02.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 73,707 hrs · 76,227 cycles

MCN - C4 - MAJOR REPAIR - EXFOLIATION CORROSION ON FLOORBEAM GALLEY SUPPORT CHANNEL AT BS 365.25 & BETWEEN RBL 51 TO RBL 60. REPLACED FLOORBEAM GALLEY SUPPORT CHANNEL AT BS 365.25 & BETWEEN RBL 51 TO RBL 60 IAW B757 SRM 51-40-02.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - MAJOR REPAIR - CRACK ON CHANNEL AT BS 1320, RBL 24.75. REPLACED CHANNEL AT BS 1320, RBL 24.75 IAW B757-200 SRM 51-40-02 AND BOEING DRAWING 146N5140.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - MAJOR REPAIR - CRACK ON WEB ANGLE BETWEEN BS 1200 AND BS 1220, BL 0. REPLACED WEB ANGLE BETWEEN BS 1200 AND BS 1220, BL 0 IAW B757-200 SRM 51-40-02 AND BOEING DRAWING 140N2505.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 73,707 hrs · 26,277 cycles

MCN - C4 - MAJOR REPAIR - EXFOLIATION CORROSION ON FLOOR SUPPORT CHANNEL AT BS333 BETWEEN RBL 25 TO RBL 37. REPLACED FLOOR SUPPORT CHANNEL AT BS 333 BETWEEN RBL 25 TO RBL 37 IAW B757 SRM 51-40-02.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - MAJOR REPAIR - CRACK ON SHEAR WEB AT BS 1320, RBL 24.75. REPLACED SHEAR WEB AT BS 1320, RBL 24.75 IAW B757-200 SRM 51-40-02 AND BOEING DRAWING 140N2506-1.

Part: CHANNEL — CRACKED (ZONE 100)

CRACK ON CHANNEL AT BS 1320, WL208, RBL45.50. REPLACED CHANNEL AT BS 1320, WL208, RBL45.50 IAW SRM 51-40-02 AND 51-40-05. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - MAJOR REPAIR - EXFOLIATION CORROSION ON FLOOR SUPPORT CHANNEL BETWEEN BS 330 TO BS 333 & BETWEEN RBL 6 TO RBL 23. REPLACED FLOOR SUPPORT CHANNEL BETWEEN BS 330 TO BS 333 & BETWEEN RBL 6 TO RBL 23 IAW B757 SRM 51-40-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - MAJOR REPAIR - CRACK ON WEB ANGLE BETWEEN BS 660 AND BS 680, BL 0. REPLACED WEB ANGLE BETWEEN BS 660 AND BS 680, BL 0 IAW B757-200 SRM 51-40-02 AND BOEING DRAWING 140N2505.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - MAJOR REPAIR - MAIN DECK FLOORBEAM CRACKED AT BS 700, WL 208, RBL 24.75. REPAIRED MAIN DECK FLOORBEAM AT BS 700 ,WL 208, RBL 24.75 IAW US AIRWAYS EA 130329.

Part: FITTING — CRACKED (FUSELAGE) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - MAJOR REPAIR - CRACK ON FLOOR STRUCTURE WEB ANGLE CLIP BETWEEN BS 660 AND BS 680, RBL 24.75. REPLACED FLOOR STRUCTURE WEB ANGLE CLIP BETWEEN BS 660 AND BS 680, RBL 24.75 IAW B757-200 SRM 51-40-02 AND BOEING DRAWING 140N2505.

Part: FITTING — CRACKED (FUSELAGE) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - MAJOR REPAIR - CRACK ON ATTACH FITTING AT BS 700, RBL 24.75. REPAIRED ATTACH FITTING AT BS 700, RBL 24.75 IAW B757 SRM 51-40-02.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,707 hrs · 26,227 cycles

MCN - C4 - MAJOR REPAIR - CRACK ON FLOORBEAM AT BS 1320, RBL 45.50. REPAIRED FLOORBEAM AT BS 1320, RBL 45.50 IAW EA 130332.

Part: PROXIMITY SENSOR — MALFUNCTIONED (L1 DOOR)

PHX - THE L1 DOOR SLIDE ARMED LIGHT WAS INTERMITTENTLY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE L1 DOOR SLIDE GIRT BAR PROXIMITY SENSOR S01215.

Part: LIGHT — INOPERATIVE (CABIN)

PHX - THE R4 DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE RELAMPED THE R4 DOOR EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKS OK.

Part: CONTROL UNIT — FAULTY (LT ENGINE)

HNL FLT 125 EN ROUTE HNL TO PHX. DURING CLIMB OUT FROM HNL, THE CABIN CREW REPORTED A LOUD NOISE, POSSIBLY COMING FROM THE DOOR. THE FLIGHT CREW REPORTED THAT THE AIRCRAFT WAS UNABLE TO PRESSURIZE, ALTHOUGH THERE NO EICAS MESSAGES OR OTHER INDICATIONS FROM THE AIRCRAFT TO INDICATE WHAT THE PROBLEM WAS. FLIGHT RETURNED TO HNL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE BVCU. OPERATIONALLY CHECKED THE PACKS AND INSPECTED THE L2 DOOR SEAL WHILE THE CABIN WAS PRESSURIZED. NO FAULTS WERE FOUND. OK FOR SERVICE.

Part: FUEL FILTER — LEAKING (LT ENGINE)

PHX - FLT 432 - EN ROUTE PHX TO OGG. DURING TAKEOFF, COMPANY WITNESSES SAW FUEL MISTING FROM THE LEFT ENGINE. THE FLIGHT WAS CONTACTED AND WAS DIRECTED TO RETURN TO FIELD IN PHX. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED A HIGH PRESSURE FUEL FILTER ASSEMBLY ON THE LEFT ENGINE. ENGINE LEAK CHECKED OK.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 68,873 hrs · 25,203 cycles

MCN - EMERGENCY EQUIPMENT - C3 CHECK - FORWARD INBOARD FLIGHT ATTENDANTS FLASHLIGHT INOPERATIVE. REPLACED FORWARD INBOARD FLIGHT ATTENDANTS FLASHLIGHT BATTERY.

Part: PUSHROD — STUCK (R4 DOOR) · airframe 68,873 hrs · 25,203 cycles

MCN - EES - C3 CHECK - THE R4 DOOR EMERGENCY MECHANISM MANUAL SELECT HANDLE STUCK IN THE ARMED POSITION. ADJUSTED AND OPERATIONAL CHECKED THE R4 DOOR GIRT BAR CRANK PUSHRODS IAW B757 AMM 52-11-25-5.

Part: PANEL — CRACKED (L/E SLAT) · airframe 68,873 hrs · 25,203 cycles

MCN - MAJOR REPAIR - C3 CHECK - LEFT WING NR 2 SLAT COVE PANEL CRACKED, OSS 658. REPLACED LEFT WING NR 2 SLAT COVE PANEL, OSS 658 IAW B757 SRM 51-40-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,873 hrs · 25,203 cycles

MCN - MAJOR REPAIR - C3 CHECK - CRACKED INTERCOSTAL ANGLE, BS 780 - BS 800, BL 0, 208. REPLACED INTERCOSTAL ANGLE, BS 780 - BS 800, BL 0, 208 IAW B757 SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,873 hrs · 25,203 cycles

MCN - MAJOR REPAIR - C3 CHECK - LEVEL 2 CORROSION ON ANGLE, BS 1715, RBL 20.5 - RBL 25, WL 208. REPLACED ANGLE, BS 1715, RBL 20.5 - RBL 25, WL 208 IAW B757 SRM 51-30-01.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,873 hrs · 25,203 cycles

MCN - MAJOR REPAIR - C3 CHECK - LEVEL 2 CORROSION ON ANGLE, BS 1701 - BS 1712, LBL 50, WL 208. REPLACED ANGLE, BS 1701 - BS 1712, LBL 50, WL 208 IAW B757 SRM 51-30-01.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,873 hrs · 25,203 cycles

MCN - MAJOR REPAIR - C3 CHECK - LEVEL 2 CORROSION ON ANGLE, BS 1715, LBL 10.5 - LBL 14.5, WL 208. REPLACED ANGLE, BS 1715, LBL 10.5 - LBL 14.5, WL 208 IAW B757 SRM 51-30-01.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,873 hrs · 25,203 cycles

MCN - MAJOR REPAIR - C3 CHECK - LEVEL 2 CORROSION ON AFT GALLEY FLOOR PLATE, BS 1680 - BS 1720, LBL 50 - RBL 50, WL 208. REPLACED AFT GALLEY FLOOR PLATE, BS 1680 - BS 1720, LBL 50 - RBL 50, WL 208 IAW B757 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,873 hrs · 25,203 cycles

MCN - MAJOR REPAIR - C3 CHECK - LEVEL 2 CORROSION ON FLOORBEAM, BS 1640, BL 0 - RBL 55, WL 208. REPAIRED FLOORBEAM, BS 1640, BL 0 - RBL 55, WL 208 IAW USAIRWAYS TYPICAL REPAIR 53-15-01.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,873 hrs · 25,203 cycles

MCN - MAJOR REPAIR - C3 CHECK - LEVEL 2 CORROSION ON ANGLE, BS 1715, RBL 33 - RBL 39, WL 208. REPLACED ANGLE, BS 1715, RBL 33 - RBL 39 IAW B757 SRM 51-30-01.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,873 hrs · 25,203 cycles

MCN - MAJOR REPAIR - C3 CHECK - LEVEL 2 CORROSION ON FUSELAGE SKIN, BS 1941 - BS 1992.8, S26L - S26R. REPAIRED FUSELAGE SKIN, BS 1941 - BS 1992.8, S26L - S26R IAW B757 SRM 51-70-10-2R4.

Part: PANEL — CRACKED (L/E SLAT) · airframe 68,873 hrs · 25,203 cycles

MCN - MAJOR REPAIR - C3 CHECK - RIGHT WING NR 10 SLAT COVE PANEL CRACKED, WS 707 - WS 736. REPLACED RIGHT WING NR 10 SLAT COVE PANEL IAW B757 SRM 51-40-02.

Part: PANEL — CRACKED (L/E SLAT) · airframe 68,873 hrs · 25,203 cycles

MCN - MAJOR REPAIR - C3 CHECK - RIGHT WING NR 10 SLAT COVE PANEL CRACKED, OSS 737 - OSS 749. REPLACED RIGHT WING NR 10 SLAT COVE PANEL, OSS 737 - OSS 749 IAW B757 SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,873 hrs · 25,203 cycles

MCN - MAJOR REPAIR - C3 CHECK , CRACKED CLIP, BS 860 - BS 880, BL 0. REPLACED CLIP, BS 860 - BS 880, BL 0 IAW B757 SRM 51-40-02.

Part: ROTARY ACTUATOR — BINDING (LE FLAPS)

PHX FLT NR 144 KOA-PHX, DURING APPROACH, AFTER SELECTING FLAP LEVER TO 1, CREW RECEIVED EICAS MESSAGE "LE SLAT DISAGREE" FLAPS INDICATED BETWEEN 0 AND 1. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEADING EDGE SLAT ROTARY ACTUATOR. OPS CHECKED OK.

Part: ENGINE — VIBRATION (LEFT) · airframe 66,737 hrs · 24,688 cycles

CREW REPORTED LEFT ENGINE VIBRATION. CREW THROTTLED BACK LT ENGINE TO FLT IDLE. VIBRATION INDICATION WAS STABLE AT .8 AND VIBRATION MESSAGE EXTINGUISHED. THE CREW DID NOT SECURE THE ENGINE AND DIVERTED TO ITO. EMERGENCY EQUIPMENT WAS DISPATCHED. THE LANDING WAS UNEVENTFUL. MX IN WORK ON LEFT ENGINE REPLACEMENT.

Part: CLAMP — DISLODGED (NR 2 ENG PNEU SY) · airframe 64,686 hrs · 24,239 cycles

FLIGHT 320: PHX - LAS - AT FL 240 NR 2 ENGINE (RT OVHT) ILLUM, EICA AND LOWER PANEL MSG. THE CREW COMPLIED W/QRH, SHUTDOWN NR 2 ENG, (CAPT STATED LIGHT EXTINGUISHED AFTER THROTTLE REDUCTION, AND ILLUMINATED AFTER POWERED BACK UP, THAT'S WHEN INITIATED AN IN-FLIGHT SHUT DOWN OF THE NR 2 ENGINE. MX FOUND NR 2 ENG CLAMP OFF PNEUMATIC DUCT GOING TO ENGINE ANTI-ICE IN PYLON. REPLACED CLAMP AND SEAL ON DUCT PER MM 36-11-01-4. RAN AT TAKEOFF POWER NO FAULTS MESSAGES, LEAK CHECK WAS GOOD. MX INSPECTED HP2 "Y" DUCT CLAMPS ON THE NR 1 ENGINE PER BOEING MM 36-11-01-4 SUB TASK 424-296. NO DEFECTS NOTED.

Part: ENGINE — SHUTDOWN (NR 1) · airframe 64,663 hrs · 24,230 cycles

908 - IFSD - KOA - PHX - DURING CLIMB, THE CREW NOTICED THE NR 1 ENGINE HAD SHUTDOWN IN-FLIGHT. THE CREW DECLARED AN EMERGENCY AND RETURNED TO KOA. MX FOUND PINS 2 AND 5 SHORTED IN CON. D2142, FOUND DAMAGED WIRING IN SHIELD TERMINATION FOR WIRE W3306/R/Y/B-20 NEAR D2142. MX REMOVED OLD CABLE, ROUTED NEW CABLE, TERMINATED PER ESWP 20-10-15, REF. 76-11-11 FOR CONNECTOR D40902P. TERMINATED NEW WIRE INTO D2142, REF WDM 28-22-21 AND ESPM 20-10-15. PERFORMED OPS CHECK OF SPAR VALVE. OPS CHECK WAS GOOD PER MM 28-22-00-5. RAN NR 1 ENGINE FOR 25 MIN, NO DEFECTS NOTED.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 64,229 hrs · 24,131 cycles

PHX - APPROXIMATELY 1 HR INTO FLIGHT, STATUS PAGE INDICATED O2 PRESS OF 110 NR. THE CREW DECLARED AN EMERGENCY AND RETURNED TO PHX. THE PAX DID NOT BRACE. THE LANDING WAS UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED THE O2 BOTTLE PER TC NR R2A35601. NO LEAKS NOTED. MAINTENANCE REMOVED REPLACED THE CAPTAIN'S AND FIRST OFFICER'S O2 MASK PER TC NR R1B35601. OBSERVED SYSTEM PRESSURE FOR 30 MINUTES, NO DEFECTS NOTED. MASK, O2 - FIRST OFFICERS, P/N 174660N5 - S/N 6508 - TSR 2113.

Part: SKIN — BULGED (FUSELAGE) · airframe 63,927 hrs · 24,061 cycles

PHX - MAJOR REPAIR - 4-DAY CHECK - FUSELAGE SKIN HAS POPPED RIVET AND BULGING SKIN, BS 1378 - 1380, S28R.

Part: SUPPORT — CORRODED (BS 1661) · airframe 63,919 hrs · 24,058 cycles

MCN - FOUND CORROSION ON L-4 DOORWAY LOWER SILL INNER CHORD (SUPPORT), BS 1661, LBL 57, WL 208. REPLACED L-4 DOORWAY LOWER SILL INNER CHORD (SUPPORT), BS 1661, LBL 57, WL 208 IAW B757-200 SRM 51-40-02 FIGURE 12.

Part: SUPPORT — CORRODED (BS 1640-1661) · airframe 63,919 hrs · 24,058 cycles

MCN - FOUND CORROSION ON R4 DOORWAY LOWER SILL INNER CHORD (SUPPORT), BS 1640 - BS 1661, RBL 57, WL 208. REPLACED CORROSION ON R4 DOORWAY LOWER SILL INNER CHORD (SUPPORT), BS 1640 - BS 1661, RBL 57, WL 208 IAW B757-200 SRM 51-40-02 FIGURE 12.

Part: SUPPORT FITTING — CORRODED (ZONE 200) · airframe 63,919 hrs · 24,058 cycles

MCN - CORROSION ON R-4 DOOR SILL UPPER SURFACE OF LOWER SILL AFT INNER CHORD, B/S 1661-1681, RBL 57, WL 208. REPLACED R-4 DOOR SILL AFT INNER CHORD B/S1661-1681, RBL 57, WL 208 IAW B757-200 SRM 51-40-02-0G PARA 7D FIG 12.

Part: DOOR FRAME — CRACKED (ZONE 100) · airframe 63,919 hrs · 24,058 cycles

C-02 CHECK - NR 5934562, FWD CARGO COMPARTMENT, UPPER DOOR FRAME 3RD FROM AFT, ANGLE BRACKET CRACKED. REMOVED AND REPLACED FWD CARGO COMPARTMENT, UPPER DOOR FRAME 3RD FROM AFT, ANGLE BRACKET IAW SRM 51-40-02-0G F IG 12 PAR 7D.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,919 hrs · 24,058 cycles

C-02 CHECK - NR 5934564, FWD CARGO COMPARTMENT DOOR UPPER AFT FRAME ANGLE BRACKET CRACKED. REMOVED AND REPLACED FWD CARGO COMPARTMENT DOOR UPPER AFT FRAME ANGLE BRACKET IAW SRM 51-40-02-0G FIG 8 AND SRM 51-40-02-0G FIG 13. .

Part: STIFFENER — CORRODED (ZONE 200) · airframe 63,919 hrs · 24,058 cycles

MCM - MAJOR REPAIR-C-02 CHECK-NR 5934085, CORROSION UNDER R-4 DOOR LOWER SILL SCUFF PLATE ATTACH FITTING (STIFFENER) BS 1669. REMOVED AND REPLACED ATTACH FITTING AT R-4 DOOR BS 1669 IAW SRM 51-40-02-0G PARA 7D FIG 12.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 63,919 hrs · 24,058 cycles

C-2 CHECK - NR 5934563, FWD CARGO COMPARMENT DOOR, FWD FRAME UPPER ANGLE BRACKET CRACKED. REPLACED FWD CARGO COMPARMENT DOOR, FWD FRAME UPPER ANGLE BRACKET IAW SRM 51-40-02, FIGURES 8 & 12.

Part: LIFE RAFT — FAILED (CABIN) · airframe 63,919 hrs · 24,058 cycles

MCN - EMERGENCY EQUIPMENT LIFE RAFT FAILED TO DEPLOY AND INFLATE COMPLETELY, P/N 63800-101 S/N L6037. ROTATABLE PARTS CHANGE WAS INDICATED.

Part: WIRE — BROKEN (CABIN) · airframe 63,305 hrs · 23,914 cycles

PHX - EEL - NR - 4104203 - DURING OVERNIGHT MAINTENANCE IT WAS DISCOVERED THAT ROW 29L SEAT EMERGENCY LIGHT WAS INOP. MAINTENANCE REPAIRED THE BROKEN WIRES TO THE LIGHT IAW 20-10-3.

Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 62,609 hrs · 23,758 cycles

CREW REPORTED RECEIVING "HYD QTY EICAS MESSAGE PRIOR TO DEP L HYD QTY DROPPED TO 0.26, RT HYD PRESS DROPPED TO 2940 PSI." CREW DIVERTED TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND METAL IN LT CASE DRAIN PRESSURE MODULE FILTER. ALSO, FOUND THE LT FILTER MODULE BYPASS INDICATOR LEAKING. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENG EDP AND THE DIFF PRESS INDICATOR ON THE LT FILTER MODULE. LEAK CHECKS WERE GOOD.

Part: STRUCTURE — DAMAGED (LT ELEVATOR T/E) · airframe 61,530 hrs · 23,511 cycles

DURING POST FLIGHT INSPECTION DISCOVERED A 6 INCH PIECE OF ALUMINUM STICKING UP FROM TRAILING EDGE OF LT ELEVATOR. TEMP REPAIR WAS PERFORMED AND AIRCRAFT WENT ON A ONE-TIME FERRY FLIGHT FOR PERMANENT REPAIR. MAINTENANCE REPAIRED LT ELEVATOR BY REMOVING CONDUCTIVE FRAME AND FABRICATING NEW FRAME MFG DWG 183N2006. INSTALLED FRAME AND FASTENERS THROUGH OUT SKIN IAW MFG DWG 183N2006.

Part: TRANSCEIVER — INOPERATIVE (HF SYSTEM) · airframe 61,395 hrs · 23,484 cycles

PHX - AIR TURN BACK - FLT 932 - PRIOR TO ETOPS ENTRY CREW REPORTED, WAS UNABLE TO TRANSMIT ON THE LEFT HF AT ALL STATIONS. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE LT HF RT. OPERATIONAL CHECKS WERE GOOD. VENDOR CONFIRMED FAILURE DUE TO BEING OUT OF CALIBRATION. THE UNIT WAS REPAIRED AND TESTED IAW CMM 23-10-70 REV.6

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 61,063 hrs · 23,345 cycles

SEA - EEL - DURING OVERNIGHT INSPECTION FOUND ROW 8 FORWARD EMERGENCY PATHWAY LIGHT INOPERATIVE. MAINTENANCE FOUND WIRE BROKEN AT SPLICE. INSTALLED NEW SPLICE AT ROW 8 AND OPERATIONAL CHECKS WERE GOOD.

Part: RESERVOIR — LOW (PAX DOOR ASSIST) · airframe 61,043 hrs · 23,338 cycles

PHX - EES - DURING OVERNIGHT INSPECTION DISCOVERED THE L2 DOOR ASSIST BOTTLE BELOW LIMITS. MAINTENANCE REMOVED AND REPLACED THE L2 DOOR ASSIST BOTTLE IAW BOEING 757 AMM 51-11-30.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,119 hrs · 22,533 cycles

SAL - MAJOR REPAIR - DURING C-1 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK AT BS 1180, LBL 45.5. MAINTENANCE REMOVED DAMAGED SECTION OF SEAT TRACK AT BS 1180, LBL 45.5; FABRICATED A NEW REPLACEMENT SECTION OF SEAT TRACK, A STRAP, AND ANGLE; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-52, FIG 201.

Part: TUBE — CHAFED (NR 1 ENGINE) · airframe 58,113 hrs · 22,103 cycles

PHX - EMERGENCY LANDING - FLT 0568 - EN ROUTE FROM MCO TO PHX LT ENGINE EPR INDICATED HIGH, DECLARED EMERGENCY, EPR APPEARED NORMAL ON APPROACH AND LANDING. MAINTENANCE PERFORMED BITE TEST OF ELECTRONIC ENGINE CONTROL AND FOUND CODE 47, FOLLOWED FIM 73-21-00 AND INSPECTED P1 SENSE LINE CONNECTIONS. FOUND UPPER P1 SENSE CHAFED WHERE IT PASSES THROUGH INLET COWL. REMOVED AND REPLACED P1 SENSE LINE AND PERFORMED PRESSURE CHECK. RAN ENGINE TO TAKEOFF POWER, ALL EPR INDICATIONS NORMAL.

Part: RADAR — FROZEN (ZONE 113) · airframe 56,752 hrs · 21,498 cycles

ON CLIMBOUT OF PHX EN ROUTE FOR LAS BOTH THE CAPTAINS AND FIRST OFFICERS WEATHER RADAR LOCKED IN TEST MODE, SWITCHING SYMBOL GENERATORS AND CYCLING TERRAIN SWITCHES, NO HELP. DUE TO WEATHER EN ROUTE, TURNED BACK TO PHX FOR REPAIR. MAINTENANCE REMOVED AND REPLACED WEATHER RADAR RECEIVER TRANSMITTER IAW BMM 34-43-01, OPERATIONAL CHECK WAS GOOD. FUNCTIONAL TEST OF WEATHER RADAR RECEIVER TRANSMITTER S/N 3652 WAS NO FAULT FOUND, PERFORMED A VISUAL INSPECTION OF UNIT, RETESTED, RETURNED TO SERVICE IAW CMM 34-45-21, REV. 009.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 55,717 hrs · 21,067 cycles

PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE CAPTAINS OXYGEN MASK WAS DEFECTIVE FRM 35-11-06-01. EMERGENCY, 100 PERCENT, AND NORMAL SELECTIONS ROTATE BEYOND EMERGENCY STOP VENTING MASK INTO COCKPIT AIR. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS OXYGEN MASK AND REGULATOR ASSEMBLY IAW BMM 35-11-51, OPERATIONAL CHECK WAS GOOD.

Part: SKIN — CRACKED (RT WING) · airframe 55,028 hrs · 20,826 cycles

DURING C-12 CHECK A 3 INCH CRACK WAS FOUND ON RT WING UPPER LEADING EDGE SKIN AT NR 8 SLAT INBOARD CORNER. MAINTENANCE REMOVED CRACKED RT WING UPPER LEADING EDGE SKIN PANEL FROM WS 425.50 TO WS 471.30; FABRICATED 3 EACH REPAIR STRAPS & FILLERS; INSTALLED REPAIR PARTS IAW AWA ER 19-5700-00012-DD5.

Part: BLOCK — CORRODED (GIRT BAR) · airframe 55,028 hrs · 20,826 cycles

DURING C-12 CHECK CORROSION WAS FOUND ON THE L-1 DOOR GIRT BAR CENTERING BLOCK. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR GIRT BAR CENTERING BLOCK IAW B757-200 SRM 51-40-02, PG 1, PARA 9A & 9B.

Part: BEAM — CRACKED (VERTICAL STAB) · airframe 55,028 hrs · 20,826 cycles

DURING C-12 CHECK 2 EACH CRACKS WERE FOUND ON VERTICAL STABILIZER TRAILING EDGE BEAM AT RT SIDE OF YAW DAMPER CAVITY INTERIOR, APPROXIMATELY RIB STA 100. MAINTENANCE REMOVED CRACKED SECTION OF VERTICAL STABILIZER BEAM AT RT SIDE OF YAW DAMPER CAVITY INTERIOR, RS 100; FABRICATED A NEW SECTION OF REPLACEMENT BEAM AND 4 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-12, PG 1-6, FIG 1.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 53,485 hrs · 20,170 cycles

EN ROUTE, THE CAPTAINS FORWARD WINDSHIELD BEGAN TO MAKE A POPPING SOUND, WINDOW CRACKED, DESCENDED TO LOWER ALTITUDE AND SLOWER SPEED FOR FEAR OF LOSING WINDOW, DIVERTED TO ONT. MAINTENANCE REMOVED AND REPLACED LT FORWARD WINDSHIELD IAW AMM 56-11-01, PG. 401. AS PRECAUTION, REPLACED WINDOW HEAT CONTROLLER LT FRONT IAW AMM 30-41-01, PG. 401. VENDOR FUNCTIONAL TEST OF WINDOW HEAT CONTROL S/N 107C-1046 WAS NO FAULT FOUND. UNIT PASSED BENCH TEST IAW HONEYWELL CMM 30-41-07, REV 12, AND WAS RETURNED TO SERVICE. VENDOR CONFIRMED FAILURE OF WINDSHIELD S/N 908AWCPT1, FAILURE ANALYSIS NOT ACCOMPLISHED, WINDSHIELD SCRAPPED AT VENDOR.

Part: BATTERY — DISCHARGED (LAV FLASHLIGHT) · airframe 52,202 hrs · 19,576 cycles

FLIGHT CREW REPORTED THAT THE EMERGENCY FLASHLIGHT AT THE L-4 DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE L-4 DOOR EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD.

Part: WIRE — BROKEN (SEAT ROW 19 L/H) · corrosion level 0 · airframe 51,807 hrs · 19,420 cycles

PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 L/H WAS FOUND INOPERATIVE. MAINTENANCE SPLICED A BROKEN WIRE AT SEAT ROW 19 L/H, OPERATIONAL CHECK WAS GOOD.

Part: SWITCH — BROKEN (BS 1638) · corrosion level 0 · airframe 50,572 hrs · 18,926 cycles

GYR - EEL - DURING C-11 CHECK THE L4 DOOR EMERGENCY LIGHTING TEST SWITCH WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT TEST SWITCH AT THE L4 DOOR IAW WDM 33-51-15, PG . 1. EMERGENCY LIGHT TEST WAS GOOD IAW BMM 33-51-00, PG. 502.

Part: FRAME — CHAFED · corrosion level 0 · airframe 50,572 hrs · 18,926 cycles

GYR - MAJOR REPAIR - DURING C-11 CHECK A CHAFED FRAME WAS FOUND AT BS 1280 BETWEEN STR 11-14 L/H. MAINTENANCE REMOVED DAMAGED SECTION OF FRAME, FABRICATED NEW FRAME SPLICE ANGLES, TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-07, FIG. 201, SHEET 1-3.

Part: WEB — CRACKED (R2 DOOR) · airframe 50,566 hrs · 18,924 cycles

GYR - MAJOR REPAIR - DURING C-11 CHECK A .5 INCH CRACK WAS FOUND ON THE WEB OF THE R2 DOOR AT THE UPPER HINGE CUTOUT. MAINTENANCE CUTOUT DAMAGED AREA, FABRICATED A REPAIR DOUBLER AND FILLERS, AND INSTALLED REPAIR PARTS IAW AWA ER 19-5211-021280-ES1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,572 hrs · 18,926 cycles

GYR - MAJOR REPAIR - DURING C-11 CHECK EXFOLIATION CORROSION FOUND ON UPPER HORIZONTAL FLANGE AT BS 1681. NUMEROUS AREAS OF CORROSION FROM LBL 50 - RBL 53. MAINTENANCE CUT OUT CORROSION AND INSTALLED REPAIR PARTS PER AWA ER 19-5360-02119-JS1.

Part: WEB — CORRODED (FUSELAGE) · airframe 50,566 hrs · 18,924 cycles

GYR - MAJOR REPAIR - DURING C-11 CHECK CORROSION WAS FOUND ON AFT GALLEY FLOOR WEB IN MULTIPLE AREAS BETWEEN BS 1681 TO 1720, LBL 56 TO RBL 56. MAINTENANCE REMOVED CORRODED AFT GALLEY FLOOR WEB BETWEEN BS 1681 TO 1720, LBL 56 TO RBL 56, FABRICATED AND INSTALLED REPAIR PER DWG 146N5318.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,572 hrs · 18,926 cycles

GYR - MAJOR REPAIR - DURING C-11 CHECK EXFOLIATION CORROSION WAS FOUND ON THE RT CREASE BEAM AT BS 1597, RBL 61.0. MAINTENANCE CUT OUT DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-12 FIG 1, SHEET 1-6.

Part: FRAME — CHAFED · corrosion level 0 · airframe 50,572 hrs · 18,926 cycles

GYR - MAJOR REPAIR - DURING C-11 CHECK MAIN FRAME WAS FOUND CHAFED BEYOND LIMITS AT BS 1280, STR 14R TO STR 12R. MAINTENANCE REMOVED DAMAGED SECTION OF FRAME, FABRICATED REPAIR FRAME SPLICE ANGLES, TREATED, PRIMED AND INSTALLED IAW B757-200 SRM 53-00-07, FIG 201, SHEET 1-3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,572 hrs · 18,926 cycles

GYR - MAJOR REPAIR - DURING C11 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBOARD SUPPORT ANGLE (INNER CHORD) AT BS 1350, RBL 64. MAINTENANCE REMOVED INNER CHORD FROM BS 1290 TO BS 1405 RT, FABRICATED NEW INNER CHORD, AND INSTALLED REPAIR PARTS IAW DWG 146N8326, AND SRM 51-40-01 PG 1.

Part: RIB — CRACKED · corrosion level 0 · airframe 50,566 hrs · 18,924 cycles

GYR - MAJOR REPAIR - DURING C-11 CHECK A CRACK WAS FOUND ON THE VERTICAL STAB TOP LEADING EDGE SUPPORT WEB (RIB), L/H AND R/H SIDES AT FSS 417.169. MAINTENANCE REMOVED DAMAGED RIB, FABRICATED AND INSTALLED A NEW RIB IAW B757-200 SRM 51-40-01, PG. 1.

Part: DOUBLER — WORN (FUSELAGE) · airframe 50,566 hrs · 18,924 cycles

GYR - MAJOR REPAIR - DURING C-11 CHECK THE INTERNAL DOUBLER FOR THE AFT POTABLE WATER SERVICE PANEL LATCH WAS FOUND WORN BEYOND LIMITS. MAINTENANCE REMOVED FLOORBOARD BS 1510-1640, REMOVED CLIPS AT BS 1640, AND 1660, STR 29 RT TO 29 LT, REMOVED POTABLE WATER SERVICE DOOR INTERNAL DOUBLER AT BS 1640-1660, STR 29 RT TO 29 LT, FABRICATED DOUBLER AND INSTALLED REPAIR PART AND REINSTALLED FLOORBOARD AND CLIPS PER DWG 146N3600, AND SRM 51-10-02.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 49,896 hrs · 18,674 cycles

WHEN MX ARRIVED AT AIRCRAFT FOUND EMERGENCY LIGHTING WAS LEFT ON FOR AN UNDETERMINED PERIOD OF TIME. MX REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERY PACKS. DURING EMERGENCY LIGHT OPERATIONAL TEST MX FOUND THAT THE AISLE EMERGENCY LIGHTS WERE COMING ON INTERMITTENTLY WITH EMERGENCY LIGHT ARM SWITCH IN OFF POSITION. AT THIS TIME NOTED THAT EMERGENCY EXIT LIGHT OVER L1 DOOR DID NOT ILLUMINATE. FOUND THE L1 DOOR BATTERY PACK THAT HAD JUST BEEN INSTALLED WAS BAD. REPLACED EMERGENCY BATTERY PACK AT L1 DOOR IAW BMM 33-51-07. MX TROUBLESHOT THE INTERMITTENT EMERGENCY AISLE LIGHT PROBLEM TO THE EMERGENCY LIGHT ARM SWITCH PANEL AND REPLACED THE PANEL. OPERATIONAL CHECK OF EMERGENCY LIGHTING SYS TESTED GOOD.

Part: SENSE LINE — SEVERED (NR 2 ENGINE) · airframe 48,941 hrs · 18,312 cycles

MCI - DIVERTED FLT - FLT 807 - ENROUTE FROM BWI TO PHX, FL 390, THE NR 2 ENGINE WOULD NOT PRODUCE COMMANDED POWER AND THE AIRCRAFT DIVERTED TO MCI MAKING AN UNEVENTFUL LANDING. MAINTENANCE TROUBLESHOT AND FOUND THE NR 2 ENG P-1 AIR SENSE LINE, PN UL16688 CHAFFED THROUGH AND SEVERED BY A CLAMP. THE SAME LINE AND CLAMPS HAD BEEN REPLACED ON 7/9/01 DUE TO WEAR FOUND DURING A-7 CHECK.

Part: AUTOTHRUST SYS — MALFUNCTIONED (COCKPIT) · airframe 48,052 hrs · 17,969 cycles

MCO- ABORTED TAKEOFF- FLT 560- THRUST LEVERS INITIALLY ADVANCED FROM IDLE POSITION, EICAS MESSAGE AUTO THROTTLE DISCONNECT AND AUTO THROTTLE DISCONNECT AMBER LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED BELOW 60KTS. THE AUTO THROTTLE SYSTEM WAS PLACED ON MEL 22-30-1 COND 1 AND THE FLIGHT CONTINUED TO PHX. IN PHX MAINTENANCE CHECKED CURRENT STATUS WHICH WAS GOOD. MAINTENANCE CHECKED HISTORY FOR PREVIOUS 30 DAYS, NO DISCREPANCIES FOUND. PERFORMED AUTO THROTTLE BITE TEST AND TESTED GOOD. THE MEL WAS CLEARED AND NO FURTHER DISCREPANCIES HAVE BEEN REPORTED.

Part: SKIN — PUNCTURED (APU DOOR)

APU ACCESS DOOR HAS .5 INCH PUNCTURE IN SKIN. STOP DRILLED CRACK, FABED AND INSTALLED REPAIR DOUBLER IAW SRM 52-40-01.

Part: INTERCOSTAL — CRACKED (FWD CARGO BAY)

FWD CARGO PIT FLOOR STRUCTURE AT STA 690 LBL 3 INTERCOSTAL CRACKED. REMOVED, FABED AND INSTALLED FLOOR SUPPORT INTERCOSTAL IAW SRM 53-30-53 FIG 1 AND SRM 51-40-02.

Part: FLOORBEAM — CRACKED (FUSELAGE)

FWD CARGO PIT STA 680 RBL 20 INTERCOSTAL IS CRACKED AT ITS UPPER CHORD (UPPER FLOORBEAM). REMOVED, FABED AND INSTALLED INTERCOSTAL REPAIR ANGLE IAW SRM 51-30-01 AND ENGINEERING SUPPORT; TREATED AND PRIMED IAW SRM 51-20-01.

Part: ATTACH ANGLE — CRACKED (LT FLAP)

ATTACH ANGLE CRACKED ON LT WING I/B MID FLAP O/B END. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-40-02.

Part: SHEAR TIE — CRACKED (FUSELAGE)

AFT CARGO COMPARTMENT STA 1300 LEFT SIDE BETWEEN STR 20L AND 21L SHEAR TIE ANGLE CRACKED. REMOVED CRACKED ANGLE, FABED REPAIR ANGLE AND INSTALLED REPAIR ANGLE IAW SRM 51-40-02, 51-30-02 AND 51-30-01.

Part: FLOOR SUPPORT — CRACKED (AFT CARGO BAY)

RT LAV FLOOR VERT SUPPORT CRACKED, AFT CARGO BAY STA 1320 RBL 46. REMOVED AND REPLACED RT LAV FLOOR VERT SUPPORT IN AFT CARGO BAY IAW SRM 51-10-02 AND 51-40-02.

Part: FLOORBEAM — CRACKED (FUSELAGE)

FWD CARGO PIT UPPER FLOORBEAM INTERCOSTAL IS CRACKED AT STA 780-800 BL 0. REMOVED, FABED AND REPLACED UPPER INTERCOSTAL ANGLE IAW SRM 53-30-51, 51-40-02, 51-20-05.

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

INTERCOSTAL ATTACH ANGLE FOUND CRACKED AT FS 660 AFT SIDE OF FLOORBEAM AT RBL 45.5. REMOVED CRACKED ANGLE; FABED NEW ANGLE IAW SRM 51-30-01 FIG 7 AND INSTALLED NEW ANGLE IAW SRM 51-40-02.

Part: BRACKET — CRACKED (FUSELAGE)

LT LAV FLOOR SUPPORT INTERCOSTAL, AFT SUPPORT BRACKET CRACKED, AFT CARGO BAY STA 1300 LBL 46. REMOVED INTERCOSTAL IAW SRM 51-40-02, FABED INTERCOSTAL SUPPORT BRACKET AND INSTALLED SUPPORT BRACKET IAW SRM 51-40-02 AND SRM 51-30-01.

Part: FLOOR SUPPORT — BENT (AFT CARGO BAY)

AFT CARGO STA 1320 RBL 20 FLOORBOARD SUPPORT IS BENT. REMOVED DAMAGED SECTION OF FLOORBOARD SUPPORT; FABED SPLICE AND FLOOR SUPPORTS INSTALLED IAW SRM 51-70-12.

Part: FLOORBEAM — CRACKED (FUSELAGE)

FWD CARGO PIT UPPER FLOORBEAM STA 560 RBL 0 INTERCOSTAL CRACKED. REMOVED, FABED AND INSTALLED ANGLE IAW SRM 53-30-51, 51-30-02, AND 51-40-02.

Part: BULKHEAD — CRACKED (NR1 PYLON)

NR 1 PYLON NSA 290 AFT ELECTRICAL SUPPORT BULKHEAD CRACKED. REMOVED, FABED, AND INSTALLED REPAIR ANGLE IAW SRM 51-40-02 AND 51-30-01 FIG 7.

Part: FLOORBEAM — CRACKED (FUSELAGE)

FWD CARGO PIT STA 660 BL 0, UPPER FLOORBEAM INTERCOSTAL IS CRACKED. REMOVED, FABED AND REPLACED ANGLE IAW SRM 53-30-51, 51-30-01 FIG 7, 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN FLOOR SUPPORT AT STA 365 BL 0 HAS CORROSION. REMOVED CORROSION; OG MAT .071, MAT LOSS .040 - OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW 51-40-05, 51-10-02, 51-40-02.

Part: BRACKET — CRACKED (FUSELAGE)

LT FUSELAGE UNDER WING TO BODY FAIRING FWD OF EMERGENCY EXIT HAS CRACKED ATTACH BRACKET. FABED REPAIR ANGLE, REMOVED DAMAGED ANGLE AND INSTALLED REPAIR ANGLE IAW SRM 51-40-02 AND 51-70-11.

Part: FITTING — CORRODED (LT AFT LAV)

LT AFT LAV AFT RETAINER BRACKET HAS CORROSION AND BLUE WATER STAIN. REPLACED LAV AFT RETAINER BRACKET IAW MM 25-41-03.

Part: SKIN — DENTED (FUSELAGE)

THERE IS A DENT IN THE FUSELAGE AT STA 634 AT STR 16L. CUT OUT DAMAGE; FABBED, TREATED, PRIMED AND INSTALLED REPAIR IAW SRM 53-00-01 FIG 205.

Part: SHEAR TIE — CRACKED (FUSELAGE)

AFT CARGO COMPARTMENTS STA 1300 LEFT SIDE BETWEEN STR 20L AND 21L SHEAR TIE ANGLE CRACKED. REMOVED CRACKED ANGLE; FABED ANGLE; INSTALLED ANGLE IAW SRM 51-40-02, 51-30-02, AND 51-30-01.

Part: BRACKET — CRACKED (WING TO BODY)

LT FUSELAGE UNDER WING TO BODY FAIRING FWD OF EMERGENCY EXIT HAS CRACKED ATTACH BRACKET. FABBED REPAIR ANGLE; REMOVED DAMAGED ANGLE AND INSTALLED REPLACEMENT ATTACH ANGLE IAW SRM 51-40-02 AND 51-70-11.

Part: STRUCTURE — CRACKED (AFT CARGO)

RT LAV FLOOR VERTICAL SUPPORT CRACKED, AFT CARGO BAY STA 1320 RBL 46. REMOVED AND REPLACED RT LAV FLOOR VERT SUPPORT IAW SRM 51-10-02 AND 51-40-02.

Part: COMPUTER — FAILED (E/E BAY)

AIR TURNBACK, CAPT''S INSTRUMENT LOSS, UNCOMMANDED ROLL. AT FL 370, RIGHT AP ENGAGED, AIRCRAFT BEGAN A SLOW ROLL TO LEFT WITH RIGHT AILERON CORRECTION. LOST DATA INPUT TO AIRSPEED, ALTIMETER, IVSI, AND CABIN PRESSURE STARTED CLIMBING. EEC BITE CHECK SHOWED FAILED LEFT AIR DATA COMPUTER. REPLACED AIR DATA COMPUTER IAW MM 34-12-01, TEST OK. RECOMMENDATION: REMAIN OPEN PENDING RESULTS OF TEARDOWN REPORT.

Part: CHARGER — FAILED (E/E BAY)

AIR TURN-BACK, MAIN BATTERY CHARGER ON STATUS PAGE. REMOVED AND REPLACED MAIN BATTERY CHARGER. INSTALLED SERVICABLE BATTERY, TT 0047079, M+E 19-2431-9-0001 S/N 5791 CHARGER TT 0043476 M+E 19-2430-9-0002, S/N 0084.

Part: STARTER — FAILED (NR 1 ENGINE)

BOTH ENGINES RUNNING BURNING SMELL NOTICED IN REAR OF A/C AND IN COCKPIT VERIFIED SMELL WITH NR 1 BLEED ON, LT PACK ON, ISO VALVE CLOSED. COULD NOT DUPLICATE IN ANY OTHER CONFIG. FOUND NR 1 STARTER OIL LOW WITH METAL CHIPS. REMOVED AND REPLACED STARTER, TT 0107843.

Part: SENSOR — DAMAGED (RUDDER)

BASE OF LEAD WIRE FOUND PINCHED AND/OR BROKEN AT COIL CAUSING A FAILURE IN THE SENSOR ASSY OF THE RUDDER PCU ASSY. WIRES BEING PINCHED AND/OR CUT DURING INSTALLATION AND THE TORQUING OF CAP P/N 315123-1. WIRE GAUGE/DIAMETER OF COIL LEADS IS TOO SMALL.

Part: WIRE — DAMAGED (RT FUEL VLV)

GATE RETURN FOR NR 2 ENGINE FLAME OUT AFTER ONE MINUTE AFTER START. RT ENGINE VALVE AND SPAR VALVE LIGHT ILLUMINATED AND EICAS MESSAGE. RT FUEL SPAR VLV AND RT ENGINE FUEL VLV DISPLAYED, WITH FUEL CONTROL SWITCH IN RUN. NO FUEL FLOW INDICATED. REPAIR BAD WIRE ON PIN 2 OF RT WING SPAR VALVE CANNON PLUT. OPS CHECKED GOOD ON ENGINE RUNS AT THIS TIME (WIRE WAS BARE AND BROKEN INSIDE PER MECHANIC). (M)

Part: FLOORBEAM — CORRODED (BS 310)

DURING SCHEDULED C-8 INSPECTION, FOUND CORROSION ON FLOORBEAM STA 310, WL 208, RBL 5. REMOVED CORROSION AT BS 310, WL 208, RBL 5, FOUND OUT OF LIMITS. FABRICATED REPAIR PARTS AND INSTALLED PARTS AT BS 310, WL 208, RBL 5 PER SRM 53-00-51.

Part: LIGHT — MISSING (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROXIMITY LIGHT LENS MISSING AT ROW 10. REMOVED AND REPLACED LIGHT ASSEMBLY, OPS CHECK GOOD.

Part: FUEL GOVERNOR — MALFUNCTIONED (NR 2 ENGINE)

ON SHORT FINAL LANDING APPROACH, THE RIGHT ENGINE N1 RED LINED AT 111.3 AND N2 RED LINED AT 102 FOR SEVERAL SECONDS. PRONOUNCED YAW. ENGINE RETURNED TO NORMAL AND LANDING WAS NORMAL. REMOVED AND REPLACED NR 2 ENGINE FUEL FLOW GOVERNOR.

Part: HYDRAULIC PUMP — LEAKING (LT ENGINE)

AIR TURNBACK, LEFT HYDRAULIC QUANTITY DECREASED TO ZERO AND SYSTEM PRESSURE LIGHT ILLUMINATED. EICAS MESSAGE LEFT HYDRAULIC SYSTEM PRESSURE DISPLAYED. REMOVED AND REPLACED LEFT ENGINE DRIVEN PUMP. ENGINE RUN AND LEAK CHECK NORMAL.

Part: LIGHT — BROKEN (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT AT ROW 10C BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY, OPS CHECK GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS INOP FROM ROW 1 TO 8. REMOVED AND REPLACED POWER SUPPLY. ALSO, FOUND SHORTED WIRING ROW 1L. SECURED WIRING, ALL LIGHTS CHECK NORMAL.

Part: BATTERY — DISCHARGED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND SEATS 1-L TO 8-L EMERGENCY LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY BATTERY AND F-1 FUSE, OPS CHECK GOOD.

Part: TEAR STRAP — NO EDGE DISTANCE (YS 1280)

PAE - FLT 7829 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, AT BS 1280, STRINGER 6R, FOUND REPAIR FASTENER BREAKING THROUGH EDGE OF TEAR STRAP, NO ED. REMOVED EXT DOUBLER, CUT OUT INTERNAL TEAR STRAP, FABRICATED REPAIR PARTS AND INSTALLED IAW ER 5-53-34-02, TCO-PAN 96-1173RR. (M)

Part: TEAR STRAP — NO EDGE DISTANCE (BS 1220)

PAE - FLT 7829 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK WHILE ACCESSING AREA AT BS 1220, STRINGER 5R, FOUND REPAIR FASTENERS BREAKING THROUGH EDGE OF TEAR STRAP, NO ED. REMOVED EXTERNAL DOUBLER. REMOVED DAMAGED SECTION OF TEAR STRAP. FABRICATED AND INSTALLED REPAIR PARTS PER ER 5-53-34-02 AND PER TCO-PAN-96-1173RR. (M)

Part: FLOOR BEAM — CORRODED (BS 1681)

PAE - FLT 7829 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK WHILE WORKING INT 57, CUSTOMER ID NR 00312737, FOUND BS 1681 FLOOR BEAM TO BE CORRODED LBL 33-48 AROUND NUT PLATES ON UPPER CHORD. CUT OUT DAMAGE AT BS 1681, LBL 43-RBL 48. CLEANED CORROSION AT BS 1681, LBL 33 - LBL 40. FABRICATED PARTS AND INSTALLED FASTENERS PER ER TCO-PAN 1159RR AND SRM 53-60-51. (M)

Part: WEB — CORRODED (BS 1681)

PAE - FLT 7829 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON PRESSURE WEB BS 1681, BL 0 - LBL 50. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS IAW, SRM 53-60-51, 53-00-51. (M)

Part: FLOOR BEAM — CORRODED (BS 1640)

PAE - FLT 7829 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION AT BS 1640 UPPER CHORD OF FLOOR BEAM LBL 65 - RBL 65. REMOVED CORRODED PART AT BS 1640, LBL 65 - RBL 65, WL 208 AND INSTALLED FABRICATED PART PER SRM 51-30-01, SRM 53-00-51. (M)

Part: BLEED AIR LIGHT — ILLUMINATED (NR 2 ENGINE)

PHX - FLT 292 - AIR TURNBACK, CREW REPORTED NR 2 ENGINE BLEED OFF LIGHT ILLUMINATED AND THE PACK WAS OFF. CREW TRIED CIRCUIT BREAKER RESET TO NO AVAIL. CREW DID SEVERAL RESETS AND BLEED STILL DID NOT COME BACK ON. AIRCRAFT RETURNED TO PHX FOR REPAIR DUE TO POSSIBLE ICING CONDITIONS AT JFK. UNABLE TO DUPLICATE PROBLEM. BLEED SYSTEM CHECKED GOOD ON GROUND WITH ENGINE RUNS. (M)

Part: BLEED SYSTEM — MALFUNCTIONED (NR 2 ENGINE)

PHX/JFK - FLT 0292 - AIR TURNBACK. CREW REPORTED NR 2 ENGINE BLEED OFF LIGHT ILLUMINATED AND THE PACK WAS OFF. CREW TRIED CIRCUIT BREAKER RESET TO NO AVAIL. CREW DID SEVERAL RESETS AND BLEED STILL DID NOT COME BACK ON. AIRCRAFT RETURNED TO PHX FOR REPAIR DUE TO POSSIBLE ICING CONDITIONS AT JFK. UNABLE TO DUPLICATE PROBLEM. BLEED SYSTEM CHECKED GOOD ON GROUND WITH ENGINE RUNS. (X)

Part: EEL LAMP — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP, OPS CHECK GOOD. (Z)