N910AW

Part: SLAT — DELAMINATED (LT WING) · airframe 91,481 hrs · 29,782 cycles

LEFT WING NR 4 SLAT HAS DELAMINATION AT INBD TE BOTTOM SIDE. REPLACED SLAT IAW 19L52027002.

Part: SLAT — DELAMINATED (RT WING) · airframe 91,481 hrs · 29,780 cycles

RIGHT WING NR 8 SLAT HAS DELAMINATION AT PREVIOUS REPAIRS, 3 EACH, AREA 1. APPROX 70" FROM INBD EDGE. AREA 2, 19" FROM INBD EDGE. AREA 3, 13" FROM OTBD END & 2" FROM TE. R & R NR 8 SLAT IAW 19L52027002.

Part: LIGHT — INOPERATIVE (ROW 26) · airframe 89,687 hrs · 29,423 cycles

ROW 26 LT EMERGENCY LIGHT INOPERATIVE. REPLACED SEAT 26 LT EMERGENCY LIGHT.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 89,617 hrs · 29,398 cycles

RIGHT WING FUEL ACCESS PANEL 641GB CRACKED & LEAKING FUEL. REPLACED RT WING FUEL ACCESS PANEL 641GB IAW AMM 28-11-00. LEAK CHECKED GOOD.

Part: LOCK — LACK OF LUBE (COCKPIT SEAT) · airframe 88,963 hrs · 29,260 cycles

EN-ROUTE, CAPTAIN`S SEAT TRACK LOCK FAILED ON TAKEOFF, SEAT ROLLED BACK. LUBED THE SEAT TRACK LOCK MECHANISM.

Part: AILERON — DEBONDED (LT WING) · airframe 88,850 hrs · 29,240 cycles

C2 CHECK, DISBONDING ON LT AILERON AT MOST INBD END & 12 INCHES FWD OF TE. REPLACED LT AILERON IAW JOB CARD 19L56827001.

Part: SKIN PANEL — DELAMINATED (FUSELAGE) · airframe 88,877 hrs · 29,242 cycles

C2 CHECK DELAMINATION & CRACK AT APU COMPARTMENT TAIL CONE RT INTERIOR FUSELAGE SKIN PANEL AT STATION 1925 ON BACK SIDE OF ELEVATOR INDEX. ACCOMPLISHED TIME LIMITED REPAIR IAW EA 106387.

Part: SKIN PANEL — DELAMINATED (FUSELAGE) · airframe 88,850 hrs · 29,240 cycles

C2 CHECK, DELAMINATION ON APU COMPARTMENT RT INTERIOR SKIN PANEL AT BS 1926, WL 247.6. REPAIRED APU COMPARTMENT RT INTERIOR SKIN PANEL AT BS 1926, WL 247.6 IAW SRM 51-70-10, REPAIR 4 & EA 106387.

Part: PANEL — CRACKED (LE SLAT) · airframe 88,850 hrs · 29,240 cycles

C2 CHECK, CRACK AT FASTENER HOLE OF LT WING NR 3 LE COVE PANEL AT APPROX 354 INCHES FROM INBD EDGE & 14 INCHES DOWN FROM TE. REPLACED LT WING NR 3 LE COVE PANEL IAW DWGS 114N4004 & 114N4077.

Part: PANEL — CRACKED (LE SLAT) · airframe 88,850 hrs · 29,240 cycles

C2 CHECK, CRACK AT FASTENER HOLE OF LT WING NR 1 LE COVE PANEL AT APPROX 54 INCHES FROM INBD EDGE & 11.250 INCHES DOWN FROM TE. REPLACED LT WING 1 LE COVE PANEL IAW DWG 114N4075.

Part: PANEL — CRACKED (LE SLAT) · airframe 88,850 hrs · 29,240 cycles

C2 CHECK, CRACK AT FASTENER HOLE OF LT WING NR 1 LE COVE PANEL AT APPROX 30 INCHES FROM OTBD EDGE & 13 INCHES DOWN FROM TE. REPLACED LT WING NR 3 LE COVE PANEL IAW DWG 114N4075.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 87,213 hrs · 28,902 cycles

PHX SEAT ROW 6 EMERGENCY LIGHT HAS BROKEN WIRE AT CONNECTOR. REPLACED WIRE HARNESS, OPERATIONS GOOD.

Part: SWITCH — NO TEST (CABIN)

PHX IAW OVERNIGHT CHECK STEP 4, EMERGENCY LIGHTING TEST SWITCH OVER L3 DOOR ESCAPE WILL NOT TEST. R & R EMERGENCY LIGHT TEST SWITCH AT L3 DOOR.

Part: SLIDE — MULTIPLE FAIL (L4 DOOR) · airframe 86,596 hrs · 28,782 cycles

DOOR 4L GIRT BAR CAME OUT FROM SLIDE ASSEMBLY. 4L SLIDE REMOVED & REINSTALLED. PROBLEM WITH ARM & DISARM RIG. REPLACED THE L4 DOOR GIRT BAR OPERATING MECHANISM AFT LIFTER ATTACHMENT BRACKET & PIVOT POINT BEARINGS, VERTICAL ROD LOWER ROD END BEARINGS, AFT CRANK ASSEMBLY & BUSHINGS & AFT GIRT BAR LIFTER ASSEMBLY. ALSO REPLACED THE L4 DOOR GIRT BAR OPERATING MECHANISM FWD LIFTER ATTACHMENT BRACKET & FWD LIFTER ASSEMBLY. REPLACED THE L4 DOOR SLIDE ASSEMBLY & THE L4 DOOR GIRT BAR. OVERHAULED SLIDE ASSEMBLY.

Part: GIRT BAR — DEFECTIVE (L4 DOOR) · airframe 86,189 hrs · 28,705 cycles

PHX 4L DOOR ARMED LIGHT WOULD NOT ILLUMINATE WHEN ARMED. REINSTALLED GIRT BAR FOOT, OPERATIONS CHECKED GOOD.

Part: TRANSCEIVER — FAULTY (HF COMM) · airframe 85,760 hrs · 28,621 cycles

FLIGHT 694 ENROUTE. HF NR 1 WILL NOT TUNE. DETECTED SMOKE & TURNED OFF HF NR 1 RADIO UNTIL SMOKE ODOR WENT AWAY. LEFT OFF REMAINDER OF FLIGHT. HF NR 2 TUNE & WORKS NORMAL. REPLACED LEFT HF TRANSCEIVER. OPS CHECKED NORMAL.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 85,647 hrs · 28,596 cycles

C1 CHECK ELEC ARCING DAMAGE AT TERMINAL LUG BRACKET & FRAME ATTACH POINTS AT BS 1480 BETWEEN STRINGER 23R TO STRINGER 24R. REPAIRED FUSELAGE FRAME AT BS 1480 BETWEEN STRINGER 23R TO STRINGER 24R IAW EA 105310.

Part: SKIN — CRACKED (LT WING) · airframe 85,647 hrs · 28,596 cycles

DURING C1 CHECK, CRACK FOUND ON NR 2 OTBD SLAT COVE PANEL AT APPROX. 29 INCHES INBD FROM OTD EDGE & 3 INCHES UP FROM LOWER SIDE. REPLACED LT WING 2 OTBD SLAT COVE PANEL IAW SRM 51-40-02 & DWG 114N4076.

Part: SKIN — CRACKED (LT WING) · airframe 85,647 hrs · 28,596 cycles

DURING C1 CHECK, CRACK FOUND ON NR 3 SLAT COVE PANEL AT APPROX 5 INCHES INBD FROM OTBD PANEL EDGE & 2 INCHES UP FROM BOTTOM EDGE. REPLACED LT WING NR 3 SLAT COVE PANEL IAW SRM 51-40-02 & DWG 114N4004.

Part: STATOR — FAILED (RECIRC FAN) · airframe 83,389 hrs · 28,137 cycles

HNL - FLT 22 EN ROUTE PHX TO HNL. SMOKE SMELL IN CABIN, EICAS R RECIRC FAN, OVERHEAD RIGHT RECIRC FAN INOP. REPLACED THE RIGHT CABIN AIR RECIRCULATION FAN. FOUND STATOR AND BEARING FAILED.

Part: LENS — DAMAGED (CABIN) · airframe 82,464 hrs · 27,952 cycles

PHX - SEAT MOUNTED EMERGENCY EXIT LIGHT (RED) LENSES DAMAGED 2 EA ROW 10ABC. REPLACED LENSES AS NEEDED.

Part: SOLENOID — FAILED (CONTROL SERVO) · airframe 81,919 hrs · 27,840 cycles

PHX FLT 125 EN ROUTE HNL TO PHX. WHEN AUTOPILOT WAS DISCONNECTED AT 6000FT ON APPROACH THE ROLL YOKE CONTROL WAS VERY HEAVY (ABOUT 3X NORMAL FORCE). IT WAS THE SAME IN BOTH CAPT AND F/O YOKE. (PITCH CONTROL WAS NORMAL) THIS HEAVINESS REMAINED AFTER LANDING DURING TAXI. WHEN THE ENGINES WERE SHUT DOWN THE CONTROL EQUALLY (OVER ABOUT 10 SEC SPAN) RETURNED TO NORMAL. MAINTENANCE REMOVED AND REPLACED THE CENTER AUTOPILOT LATERAL CONTROL SERVO. SYSTEM FEEL, CENTERING & TRIM TEST WAS PERFORMED. AUTOPILOT FUNCTION AND FEEL FORCE IS NORMAL. VENDOR SHOP FINDINGS: VISUAL INSPECTION OK. SOLENOID NR 2 FAILS CONTINUITY, UNIT FAILS DE-ENERGIZED FRICTION, OUTPUT FORCE, ROD END BEARING STICKS.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 81,884 hrs · 27,826 cycles

PHX - AFT MEGAPHONE INOP. REPLACED AFT EMERGENCY MEGAPHONE.

Part: SYNCRONIZER — FAILED (INDICATOR) · airframe 80,938 hrs · 27,648 cycles

PHX - FLT 26 EN ROUTE OGG TO PHX. FLAPS FAILED TO MOVE, TRAILING EDGE LIGHT ON, AND EICAS MSG TRAILING EDGE DISAGREE DISPLAYED. FLAPS NORMAL ON ALTERNATE SYS. THE FLIGHT PERFORMED A GO-AROUND TO RUN THE CHECKLIST. ON THE SECOND APPROACH, THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED A FLAP POSITION INDICATOR FOR A STICKING NEEDLE. REPLACED AND REWIRED BOTH SYNCHRO'S.

Part: DIODE — FAILED (FSEU) · airframe 80,938 hrs · 27,648 cycles

PHX - FLT 26 EN ROUTE OGG TO PHX. FLAPS FAILED TO MOVE, TRAILING EDGE LIGHT ON, AND EICAS MSG TRAILING EDGE DISAGREE DISPLAYED. FLAPS NORMAL ON ALTERNATE SYS. THE FLIGHT PERFORMED A GO-AROUND TO RUN THE CHECKLIST. ON THE SECOND APPROACH, THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FSEU, AND PERFORMED A VISUAL INSPECTION OF THE FLAP DIVE SYSTEM. REPLACED TRANSISTOR Q38 (MPN H00212-2), DIODE ARRAY MICROCIRCUIT U92 (MPN 057070-001), AND DIODE ARRAY MICROCIRCUIT U94 (MPN 057070-001) ON A4 PCA DUE TO TEST FAILURES. UNIT PASSED FINAL ACCEPTANCE TESTING. RETURNED TO SERVICE.

Part: SURVIVAL KIT — UNSERVICEABLE (SLIDE RAFT) · airframe 80,616 hrs · 27,588 cycles

PHX - INFLIGHT CREW REPORTS SLIDE RAFT SURVIVAL KITS NOT SEALED. REPLACED 4 EA SLIDE RAFT SURVIVAL KITS ASSY.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 80,300 hrs · 27,523 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR WEB PANEL AT BS 1420, S17R. REPAIRED FLOOR WEB PANEL AT BS 1420, S17R IAW EA 103818.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 80,300 hrs · 27,523 cycles

C4 CHECK - CRACK ON FORWARD SIDE OF FRAME L-ANGLE AT BS 350, S7L. REPLACED FRAME L-ANGLE AT BS 350, S7L IAW B757 SRM 51-40-10.

Part: PIN — CRACKED (RT NACELLE) · airframe 80,300 hrs · 27,523 cycles

C4 CHECK - CRACK IN LOWER FUSE PIN OF RIGHT ENGINE NACELLE STRUT DIAGONAL BRACE AT PPS 300, PPWL 161.70. REPLACED LOWER FUSE PIN OF DIAGONAL BRACE AT PPS 300, PPWL 161.70 IAW B757 AMM 54-51-02.

Part: WEDGE — DELAMINATED (NR 7 SLAT) · airframe 80,300 hrs · 27,523 cycles

C4 CHECK - DELAMINATION ON NR 7 SLAT TRAILING EDGE WEDGE AT WS 397.50, WBL 740.00, 6 INCHES FROM INBOARD END AT LOWER SKIN. REPAIRED NR 7 SLAT TRAILING EDGE WEDGE AT WS 397.50, WBL 740.00 IAW B757 SRM 51-70-10.

Part: SKIN — DAMAGED (TE FLAP) · airframe 80,300 hrs · 27,523 cycles

C4 CHECK - SMALL 1 INCH SPLIT IN RIGHT INBOARD AFT FLAP ON OUTBOARD END AT WS 258.50, WBL 740. REPAIRED RIGHT INBOARD AFT FLAP SKIN IAW B757 SRM 51-70-17.

Part: STRAP — CRACKED (FUSELAGE) · airframe 80,300 hrs · 27,523 cycles

C4 CHECK - CRACK ON STRAP AT BS 720, LBL 24. REPAIRED STRAP AT BS 720, LBL 24 IAW TYPICAL REPAIR TR 757-5335-11-0334.

Part: STIFFENER — CRACKED (ZONE 100) · airframe 80,300 hrs · 27,523 cycles

C4 CHECK - CRACK ON FLOORBEAM STIFFENER STRAP AT BS 718, RBL 48. REPAIRED FLOORBEAM STABILIZER STRAP AT BS 718, RBL 48 IAW EA 103787.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,300 hrs · 27,523 cycles

C4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT BS 377.7 & BETWEEN LBL 54 TO LBL 60. REPAIRED FLOORBEAM AT BS 377.7 & BETWEEN LBL 54 TO LBL 60 IAW B757 SRM 53-00-51-2R-5.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 80,300 hrs · 27,523 cycles

C4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOOR BEAM T-CAP AT BS 365 BETWEEN RBL 36 TO RBL 59. REPAIRED FLOORBEAM T-CAP AT BS 365 BETWEEN RBL 36 TO RBL 59 IAW EA 103801.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,300 hrs · 27,523 cycles

C4 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOOR SUPPORT AT BS 1316, RBL 18. REPLACED FLOOR SUPPORT AT BS 1316, RBL 18 IAW B757 SRM 51-10-02 & 51-40-00.

Part: FITTING — MISSING (GIRT BAR) · airframe 79,983 hrs · 27,464 cycles

PHX - GIRT BAR ENGAGEMENT LIGHT EXTIN WITH EVACUATION SLIDE ARMING LEVER IN ENGAGE POS AT ENTRY/SERVICE DOOR L-4. FOUND FWD GIRT BAR END FITTING MISSING. REPLACED MISSING GIRT BAR END FITTING.

Part: GIRT BAR — MISSING (L4 DOOR) · airframe 79,759 hrs · 27,420 cycles

PHX - AFT LEFT SLIDE ARM DOOR LIGHT INOP. FOUND L4 DOOR, FWD GIRT BAR SLIDER MISSING. INSTALLED SLIDER. DOOR ARM LIGHT OPS GOOD.

Part: PIN — BACKED OUT (CONNECTOR) · airframe 78,658 hrs · 27,200 cycles

PHX - EMERGENCY LIGHT ON SEAT 7 INOP. RELAMP, NO HELP. RESEATED PUSHED PIN IN EMER LIGHT CONNECTOR FOR SEAT 7.

Part: WIRE HARNESS — INOPERATIVE (CABIN) · airframe 78,601 hrs · 27,190 cycles

PHX - EMERGENCY LIGHT ON SEAT 23 INOP. MAINTENANCE REPLACED FLOOR TO LIGHT HARNESS. OPS GOOD.

Part: GIRT BAR — BENT (L4 DOOR)

PHX - THE L4 DOOR GIRT BAR AFT SPRING TAB WAS BENT. REMOVED AND REPLACED THE L4 DOOR GIRT BAR.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,080 hrs · 26,725 cycles

CLT - C3 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FORWARD CARGO LATERAL SUPPORT ANGLE AT BS 690, LBL 14. REPLACED FORWARD CARGO LATERAL SUPPORT ANGLE AT BS 690, LBL 14 IAW B757 SRM 51-10-01 & 51-20-05.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,080 hrs · 26,725 cycles

CLT - C3 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON LOWER AFT CARGO BULKHEAD SUPPORT ANGLE AT BS 848, RBL 2. REPLACED LOWER AFT CARGO BULKHEAD SUPPORT ANGLE AT BS 848, RBL 2 IAW BOEING DRAWING 453N1814.

Part: FITTING — CORRODED (CARGO DOOR) · airframe 76,080 hrs · 26,725 cycles

CLT - C3 - MAJOR REPAIR - NR I2D52602/007 - CORROSION ON SMALL CLIP ON AFT CARGO DOOR LOWER FORWARD CORNER INTERIOR. REPLACED SMALL CLIP ON AFT CARGO DOOR LOWER FORWARD CORNER INTERIOR IAW B757 SRM 51-10-00, 51-40-02 & BOEING DRAWING 69-47423-7.

Part: SLIDE — LOW PRESSURE (R3 DOOR)

PHX - R3 EMERGENCY DOOR SLIDE HAS LOW PRESSURE. REPLACED R3 DOOR SLIDE.

Part: PIN — UNSECURE (EMERGENCY LIGHT)

SEA - EMERGENCY ESCAPE PATH LIGHT AT ROW 31 IS INOP. MAINTENANCE RE-SECURED PIN.

Part: STRUT — DAMAGED (RT MLG) · airframe 72,818 hrs · 26,058 cycles

PHX - LINE - MAJOR REPAIR - UPON DISASSEMBLY OF RIGHT MAIN LANDING GEAR STRUT FOR REPACK FOUND DAMAGE TO INNER BARREL & BROKEN PARTS / COMPONENTS OF INNER STRUT & PISTON. REPLACED RIGHT MAIN LANDING GEAR IAW JOB CARD R4M32607.

Part: SLAT — DEBONDED (RT WING) · airframe 72,405 hrs · 25,978 cycles

PHX - OVERNIGHT - MAJOR REPAIR - NR 5 WING LEADING EDGE SLAT DISBONDED AND BREAKING OFF BETWEEN WS 125 TO WS 180. REPLACED NR 5 WING LEADING EDGE SLAT IAW B737 MM 27-81-01-401.

Part: SLIDE — LOW PRESSURE (R2 DOOR)

PHX - THE R2 DOOR SLIDE INDICATES LOW PRESSURE. REPLACED THE R2 SLIDE ASSEMBLY.

Part: CIRCUIT BREAKER — FAILED (TAT PROBE)

PHX FLT 24 PHX TO LAX. EICAS MESSAGE TAT PROBE DISPLAYED, AND TAT PROBE HEAT LIGHT ILLUMINATED. REPLACED TAT PROBE HEATER CIRCUIT BREAKER (C4003).

Part: PIN — NOT SEATED (CONNECTOR) · airframe 71,147 hrs · 25,696 cycles

MCN - C2 - EEL - EMERGENCY ESCAPE LIGHT AT SEAT 11L DOES NOT ILLUMINATE. RESEATED PINS IN MOLEX CONNECTOR FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT 11L.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 71,147 hrs · 25,696 cycles

MCN - C2 - EEL - FLASHLIGHTS (2 EACH) INOP AT FORWARD ATTENDANT SEAT. REPLACED FLASHLIGHTS (2 EACH) AT FORWARD ATTENDANT SEAT.

Part: STRAP — CRACKED (FUSELAGE) · airframe 71,147 hrs · 25,696 cycles

MCN - C2 - MAJOR REPAIR - CRACK ON MAIN DECK STABILIZER FLOOR STRAP AT BS 367, BL 0. REPAIRED MAIN DECK STABILIZER FLOOR STRAP AT BS 367, BL 0 IAW B757 SRM 53-10-51.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 71,147 hrs · 25,696 cycles

MCN - C2 - MAJOR REPAIR - TWO EACH CRACKS IN FLOORBEAM INTERCOSTAL UPPER ANGLE BETWEEN BS 860 TO BS 880, BL 0. REPLACED FLOORBEAM INTERCOSTAL UPPER ANGLE BETWEEN BS 860 TO BS 880, BL 0 IAW B757 SRM 51-40-02.

Part: ROD — BENT (L4 DOOR) · airframe 71,147 hrs · 25,696 cycles

MCN - C2 - EES - L-4 DOOR FORWARD SLIDE ENGAGE ROD BENT. REPLACED ROD ASSEMBLY ON L-4 DOOR IAW B757 AMM 52-11-25-5.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 71,147 hrs · 25,696 cycles

MCN - C2 - MAJOR REPAIR - NR 1 PYLON SKIN CRACKED AT AFT OUTBOARD & INBOARD THRUST REVERSER FITTING UPPER AFT HOLE. REPAIRED NR 1 PYLON SKIN AT AFT OUTBOARD & INBOARD THRUST REVERSER FITTING UPPER AFT HOLE IAW US AIRWAYS EA 130245.

Part: PLATE — CORRODED (FUSELAGE) · airframe 71,147 hrs · 25,696 cycles

MCN - C2 - MAJOR REPAIR - CORROSION ON AFT CABIN DECK PLATE BETWEEN BS 1681 TO BS 1690, BETWEEN LBL 14 TO LBL 50. REPAIRED AFT CABIN DECK PLATE BETWEEN BS 1681 TO BS 1690, BETWEEN LBL 14 TO LBL 50 IAW B757 SRM 53-60-51 & 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,147 hrs · 25,696 cycles

MCN - C2 - MAJOR REPAIR - 3 CRACKS ON INTERCOSTAL CLIP BETWEEN BS 663 TO BS 672, BL 0. REPAIRED INTERCOSTAL CLIP BETWEEN BS 663 TO BS 672, BL 0 IAW B757 SRM 51-40-02, 53-00-51, & BOEING DRAWING 140N2505.

Part: FITTING — CRACKED (FUSELAGE) · airframe 71,147 hrs · 25,696 cycles

MCN - C2 - MAJOR REPAIR - 2 CRACKS ON INTERCOSTAL CLIP BETWEEN BS 793.5 TO BS 795, WL 208, BL 0. REPAIRED INTERCOSTAL CLIP BETWEEN BS 793.5 TO BS 795, WL 208, BL 0 IAW B757 SRM 51-40-02, 53-00-51, & BOEING DRAWING 140N2505.

Part: CONTACT — CORRODED (L2 DOOR)

PHX - THE SLIDE ARMED LIGHT AT DOOR L2 WAS OPERATING INTERMITTENTLY. MAINTENANCE CLEANED THE CORROSION ON THE CONTACTS AND RELAMPED THE LIGHT. OPERATIONALLY CHECKS OK.

Part: LIGHT — INOPERATIVE (EVAC SLIDE)

PHX - THE SLIDE LIGHT FOR THE L2 DOOR WOULD NOT ILLUMINATE. MAINTENANCE CLEANED THE SENSORS AND REPLACED THE BULBS FOR THE L2 DOOR SLIDE INDICATION LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN)

PHX - THE EMERGENCY LIGHTS AT POSITIONS TWO AND THREE ON LEFT BULLNOSE WERE FOUND INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. OPERATIONALLY CHECKS OK.

Part: CHARGER — INOPERATIVE (CABIN)

PHX - THE EMERGENCY SEAT LIGHTING WAS FOUND INOPERATIVE FROM ROWS 1 - 8. MAINTENANCE REPLACED THE BATTERY CHARGER FOR SEATS AT ROWS 1 - 8. OPERATIONALLY CHECKS OK.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

HNL FLT 47 - EN ROUTE LIH TO PHX. AIRCRAFT DISPLAYED EICAS MESSAGE "L ENG LP PUMP". THE CREW DECIDED TO DIVERT BACK TO HNL. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING. (OPEN)

Part: PUMP — MALFUNCTIONED (LT ENGINE)

HNL FLT 47 EN ROUTE LIH TO PHX. AIRCRAFT DISPLAYED EICAS MESSAGE "L ENG LP PUMP". THE CREW DECIDED TO DIVERT BACK TO HNL. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE LP PUMP.

Part: PRESSURE SWITCH — FAILED (FUEL SYSTEM)

HNL - FLT 9030 OGG TO PHX. DURING CLIMB, RECEIVED EICAS MESSAGE "L ENG LP PUMP", WITH A FUEL TEMP OF +35. FLIGHT DIVERTED TO HNL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED, INSPECTED, THEN REPLACED THE LEFT ENGINE LOW PRESSURE FUEL FILTER. AFTERWARDS, MAINTENANCE REPLACED THE FUEL PRESSURE SWITCH. OPERATIONALLY AND LEAK CHECKS OK.

Part: INDICATOR — ERRATIC (FUEL QTY)

PHX FLT NR 22 PHX - HNL WHILE IN CRUISE FLIGHT, THE CENTER TANK FUEL QTY READINGS BECAME ERRATIC. FLIGHT RETURNED TO PHX WITHOUT FURTHER INCIDENT.

Part: DENSITOMETER — FAULTY (FUEL SYSTEM)

PHX FLT 22 PHX - HNL. WHILE IN CRUISE FLIGHT, THE CENTER TANK FUEL QUANTITY READINGS BECAME ERRATIC. FLIGHT RETURNED TO PHX WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CENTER FUEL TANK FUEL DENSITOMETER. OK FOR SERVICE.

Part: FUSE — BLOWN (CABIN)

PHX - EMERGENCY LIGHTS INOP ROW 1 THRU 8. MAINTENANCE REPLACED FUSE. OPS CHECKS NORMAL.

Part: TERMINAL — LOOSE (CABIN) · airframe 67,189 hrs · 24,846 cycles

MAINTENANCE FOUND ROW 12L EMERGENCY LIGHT INOPERATIVE IN OVERHEAD BIN COVE. TIGHTENED LOOSE TERMINAL. NO FURTHER FAULTS.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,176 hrs · 24,390 cycles

PHX - EEL - SEAT ROWS 1 THRU 20 EMERGENCY EXIT LIGHTS ARE INOPERATIVE. REPLACED AFT EMERGENCY LIGHT BATTERY CHARGER IAW B757-200 AMM 33-51.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,382 hrs · 23,992 cycles

FUSELAGE BS 800 BETWEEN S14 AND S15L HAS TWO PLUGGED HOLES THAT WERE R/R THE SHEAR TIE UNDERNEATH. COUNTER SANK THE INNER SKIN AT BS 800 BETWEEN S-14L AND S-15L TO ACCOMODATE THE RIVETS BUTTON. PLUGGED THE TWO HOLES USING BACR15CE AND DOUBLE FLUSHED THE RIVETS IAW ER 19-5330-06321-HF1. FINAL REPAIR WILL BE FOLLOWED UP AT NEXT C-CHECK. AFTER FURTHER REVIEW IT WAS DETERMINED THAT THE PLUGGED HOLES WERE REMOVED IN ORDER TO PLACE SHIMS BETWEEN THE SHEAR TIE AND THE FUSELAGE SKIN TO CORRECT A SKIN BULGE / DENT IN THIS LOCATION. THE PLUGGED AREA WILL BE HFEC INSPECTED EVERY 500 FLIGHT CYCLES AND FINAL REPAIR PERFORMED AT THE NEXT "C" CHECK, NO FURTHER FOLLOW UPS WILL BE REQUIRED.

Part: CONTROL UNIT — OUT OF TOLERANCE (BLEED VALVE) · airframe 62,378 hrs · 23,730 cycles

THE CREW ADVANCED THE NR 2 THRUST LEVER TO TAXI AND THE NR 2 ENGINE SHUT DOWN. EGT REACHED 620C. ENGINE SHUTDOWN WAS NOT INITIATED BY THE CREW. THE NR 2 ENGINE BLEED VALVE CONTROL UNIT DISPLAYED A VOLTAGE FAULT. MX REMOVED AND REPLACED THE NR 2 BLEED VALVE CONTROL UNIT IAW CARD R5M75601 AND TESTED IAW F5M72603. OPS CHECK GOOD.

Part: PIN — BURNED (CONNECTOR) · airframe 61,856 hrs · 23,613 cycles

OGG - EEL - LG 7250100 & 7250101 - OVERHEAD EMERGENCY LIGHTS BETWEEN SEAT ROWS 4 AND 5 DO NOT ILLUMINATE ON GROUND TEST. M731 POWER SUPPLY BAD. OGG MAINTENANCE REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK IAW MM 33-51-07. AIRCRAFT WAS FERRIED BACK TO PHX FOR FURTHER MAINTENANCE. PHX MAINTENANCE PERFORMED OPS CHECK PER M 33-51-00-5 STEP 2. INSPECTED AND REPLACED 3 BURNT PINS IAW MM 20-01-11. CONNECTOR IS GOOD FOR SERVICE.

Part: CONNECTOR — DAMAGED (SLAT SYS) · airframe 61,777 hrs · 23,590 cycles

PHX - FLT 7832 - DURING REPO FLIGHT CREW REPORTED THAT INBOUND TO PHX RECEIVED LEADING EDGE FLAP ASYMMETRY AND DISAGREE LIGHT. QRH PROCEDURES WERE FOLLOWED. LANDED IN PHX WITHOUT FURTHER EVENT. MAINTENANCE CHECKED WIRING BETWEEN FSEU 1, FSEU 2 AND RT SLAT POSITION SENSOR TS5047. OPS CHECK WAS GOOD. MAINTENANCE REPLACED CONNECTOR D1805 DUE TO PIN 4 NOT LOCKING. ALSO REPLACED ROTARY ACTUATORS 1, 9, 10, 11 AND 20 DUE TO POPPED OVERLOAD PINS. FUNCTIONAL CHECK FLIGHT WAS PERFORMED AND FAILED. AIRCRAFT IS STILL OUT OF SERVICE.

Part: TRANSMITTER — FAULTY (SLAT SYS) · airframe 61,771 hrs · 23,589 cycles

HNL - FLT 920 - CREW REPORTED THAT AFTER SELECTING FLAPS 1 ON APPROACH INTO HNL, RECEIVED "LE SLAT DISAGREE" CAUTION MSG. CREW FOLLOWED QRH CHECK LIST AND THEN RECEIVED "LE SLAT ASYMMETRY" CAUTION MSG. CREW FOLLOWED QRH AND PERFORMED ALL FLAPS/SLATS UP LANDING. EMERGENCY WAS DECLARED GOING INTO HNL. LANDED WITHOUT FURTHER EVENTS. MAINTENANCE REMOVED AND REPLACED THE RT LEADING EDGE SLAT POSITION INDICATOR TRANSMITTER IAW MM 27-88-01. WAS ADJUSTED AND TESTED IAW MM 27-88-00-5.

Part: BATTERY PACK — OVERHEATED (EMERGENCY LIGHT) · airframe 61,692 hrs · 23,571 cycles

GYR - EEL - NR 5919942 - DURING C12 CHECK DISCOVERED THE EMERGENCY LIGHTS BATTERY PACK, JUST AFT OF FWD ENTRY LIGHT, WAS OVERHEATING. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK IAW BOEING 757-200 AMM 33-51-07-2. OPERATIONAL CHECKS WERE GOOD IAW AMM 33-51-07-2 STEP 3D.

Part: CHANNEL — CRACKED (L4 DOOR) · airframe 61,692 hrs · 23,571 cycles

GYR - DURING C12 CHECK DISCOVERED CHANNEL ASSEMBLY CRACKED ON THE L4 DOOR. MAINTENANCE REMOVED AND INSTALLED NEW L4 DOOR CHANNEL ASSEMBLY IAW BOEING 757-200 SRM 51-40-02-06 PAGE 8.

Part: GATE — CORRODED (R2 DOOR) · airframe 61,692 hrs · 23,571 cycles

GYR - DURING C12 CHECK DISCOVERED LEVEL 2 CORROSION ON THE R2 DOOR UPPER GATE HINGE AREA, ALONG FULL LENGTH. MAINTENANCE REMOVED AND INSTALLED NEW UPPER GATE IAW MM 52-11-38-4. GATE WAS ADJUSTED IAW MM 52-11-00-5.

Part: ATTACH FITTING — GALLED (RT PYLON) · airframe 61,692 hrs · 23,571 cycles

DURING C12 CHECK DISCOVERED RT WING OUTBOARD STRUT ATTACH FITTING LUGS FOR PYLON GALLED FROM BUSHING CONTACT ON THE INBOARD AND OUTBOARD SIDES OF LUG AT WBL 263R . MAINTENANCE REMOVED OUTBOARD BUSHING IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 19-5704-06114-RC2. REMOVED MINOR GALLING FROM BORE OF HOLE. FABBED, ALODINED AND PRIMED FILLERS. RECEIVED CAD PLATED BUSHING AND INSTALLED OUTBOARD BUSHING AT WBL 248L IAW AWA ER NO. 19-5704-06114-RC2 AT WBL 263R.

Part: SHIM — MIGRATED (NR 1 PYLON) · airframe 61,692 hrs · 23,571 cycles

GYR - DURING C12 CHECK DISCOVERED NR 1 PYLON DIAGONAL BRACE FITTING SHIMS MIGRATING LEFT SHIM HORIZONTAL MOVEMENT 0.400 INCHES AND VERTICAL MOVEMENT 0.900 INCHES. MAINTENANCE REPAIRED PER AWA ER 19-5453-06060-BA1 AND BOEING SB 757-54-0035 FIG. 21, STEPS 8, 12, 22, 30, 31 AND FIG 34 SHEET 3 AND 4. ALSO AWA TASK CARD I5M54605 SEQ 6A AND B.

Part: SHIM — MIGRATED (RT WING) · airframe 61,692 hrs · 23,571 cycles

GYR - DURING C12 CHECK DISCOVERED NR 2 ENGINE PYLON DIAGONAL BRACE ATTACH FITTING VERTICAL SHIMS MIGRATED LT 0.200 INCHES AND R/H 0.030 INCHES. MAINTENANCE REMOVED AND REPLACED LEFT AND RIGHT DIAGONAL BRACE ATTACH FITTING SHIMS PER AWA ER 19-5453-06060-BA1.

Part: ATTACH FITTING — GALLED (RT PYLON) · airframe 61,692 hrs · 23,571 cycles

DURING C12 CHECK DISCOVERED RT WING INBOARD STRUT ATTACH FITTING FOR PYLON GALLED FROM BUSHING CONTACT ON THE INBOARD AND OUTBOARD SIDES OF LUG AT WBL 248R. MAINTENANCE REMOVED OUTBOARD BUSHING IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 19-5704-06114-RC2. REMOVED MINOR GALLING FROM BORE OF HOLE. FABBED, ALODINED AND PRIMED FILLERS. RECEIVED CAD PLATED BUSHING AND INSTALLED INBOARD BUSHING AT WBL 248R IAW AWA ER NO. 19-5704-06114-RC2.

Part: ATTACH FITTING — GALLED (LT PYLON) · airframe 61,692 hrs · 23,571 cycles

DURING C12 CHECK DISCOVERED LUG SURFACES GALLED FROM BUSHING CONTACT ON THE INBOARD AND OUTBOARD SIDES OF LEFT WING INBOARD STRUT ATTACH FITTING FOR PYLON AT WBL 248L. MAINTENANCE REMOVED INBOARD BUSHING IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 19-5704-06114-RC2. REMOVED MINOR GALLING FROM BORE OF HOLE. FABBED, ALODINED AND PRIMED FILLERS. RECEIVED CAD PLATED BUSHING AND INSTALLED INBOARD BUSHING AT WBL 248L IAW AWA ER NR 19-5704-06114-RC2.

Part: ATTACH FITTING — GALLED (LT PYLON) · airframe 61,692 hrs · 23,571 cycles

DURING C12 CHECK DISCOVERED LT WING OUTBOARD STRUT ATTACH FITTING FOR PYLON GALLED FROM BUSHING CONTACT ON THE INBOARD AND OUTBOARD SIDES OF LUG AT WBL 263L. MAINTENANCE REMOVED OUTBOARD BUSHING IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 19-5704-06114-RC2. REMOVED MINOR GALLING FROM BORE OF HOLE. FABBED, ALODINED AND PRIMED FILLERS. RECEIVED CAD PLATED BUSHING AND INSTALLED OUTBOARD BUSHING AT WBL 263L IAW AWA ER NR 19-5704-06114-RC2.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 1 · airframe 61,692 hrs · 23,571 cycles

GYR - DURING C12 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON THE MAIN CABIN FLOORBEAM UPPER EDGE AT BS 365 FROM BL 15R TO BL 35R. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 757-200 SRM 53-00-51-2A. MAINTENANCE CUT OUT AND REMOVED DAMAGED AREA IAW BOEING 757-200 SRM 53-00-51-2R-3 FIG 201. FABRICATED CHORD, REPAIR ANGLES, REPAIR STRAPS AND SHEAR CLIPS IAW BOEING 757-200 SRM 53-00-51-2R-3. INSTALLED FABRICATED REPAIR PARTS ON THE MAIN CABIN FLOORBEAM AT BS 365 FROM BL 15R TO BL 35R IAW BOEING 757-200 SRM 53-00-51-2R-3. LEVEL OF CORROSION HAS BEEN RE-EVALUATED AND DOWNGRADED FROM LEVEL 2 TO A LEVEL 1.

Part: FLOORBEAM — CORRODED (BS 700) · corrosion level 2 · airframe 616,920 hrs · 23,571 cycles

GYR - DURING C12 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT BS 740 FROM BL 45.5R TO BL 55.5R, WL 208. MAINTENANCE CUT OUT DAMAGED AREA AT BS 740 BL 45.5R IAW SRM 53-00-51-2R. CORROSION FOUND TO BE OUT OF SRM LIMITS. FABRICATED REPAIR ANGLES, STRAPS AND TEE ANGLE IAW SRM 53-00-51-2R. INSTALLED FABRICATED REPAIR PARTS AT BS 740 FROM BL 45.5R TO BL 55.5R, WL 208 IAW SRM 53-00-51-2R.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,692 hrs · 23,571 cycles

GYR - DURING C12 CHECK DISCOVERED LEVEL 2 CORROSION ON FASTENER HOLE AT BOTTOM SURFACE OF FLOOR PANEL SUPPORT ANGLE AT BL 60R AND BS 684.5. CORROSION WAS FOUND TO BE OUT OF LIMITS. INSTALLED NEW FLOOR PANEL SUPPORT ANGLE AT BL 60R AND BS 684.5.

Part: WEB — CORRODED (BS 1340-1360) · corrosion level 2 · airframe 61,692 hrs · 23,571 cycles

GYR - DURING C12 CHECK DISCOVERED CORROSION, LEVEL 2 INTERGRANULAR, ON L3 DOOR EMERGENCY LOWER WEB FROM BS 1340 TO BS 1360 AT STR 17L. MAINTENANCE REMOVED CORROSION FROM LOWER WEB FROM BS 1340 TO BS 1360 AT STR 176 IAW BOEING 757-200 SRM 51-10-02. CORROSION FOUND OUT OF LIMITS IAW BOEING 757-200 SRM 53-60-15-1A 1. REMOVED THRESHOLD WEB FROM BS 1340 TO BS 1360 AT STR 17L IAW BOEING 757-200 SRM 51-40-02. INSTALLED FABRICATED THRESHOLD WEB FROM BS 1340 TO BS 1360 AT STR 17L IAW BOEING 757-200 SRM 51-40-02.

Part: WEB — CORRODED (BS 1340-1360) · corrosion level 2 · airframe 61,692 hrs · 23,571 cycles

GYR - DURING C12 CHECK DISCOVERED CORROSION, LEVEL 2 INTERGRANULAR, ON R3 LOWER DOOR EMERGENCY LOWER WEB FROM BS 1340 TO BS 1360, WL 208.1, STR 17R, FROM BL 70R TO BL 79R. MAINTENANCE REMOVED CORROSION FROM WEB LOWER SIDE FROM BS 1340 TO BS 1360, WL 208.1, STR 17R, FROM BL 70R TO BL 79R IAW BOEING 757-200 SRM 51-40-02-0G. CORROSION FOUND OUT OF SRM LIMITS. REMOVED THRESHOLD WEB FROM BS 1340 TO BS 1360, WL 208.1, STR 17R, FROM BL 70R TO BL 79R IAW BOEING 757-200 SRM 51-40-02. INSTALLED FABRICATED THRESHOLD WEB FROM BS 1340 TO BS 1360, WL 208.1, STR 17R, FROM BL 70R TO BL 79R IAW BOEING 757-200 SRM 51-40-02.

Part: FLOORBEAM — CRACKED (BS 700) · airframe 61,692 hrs · 23,571 cycles

DURING C12 CHECK DISCOVERED FLOORBEAM CRACKED IN TWO PLACES AT BS 700, ONE CRACK AT BL 24R AND THE OTHER AT BL 46R. EACH CRACK WAS APPROXIMATELY 1 INCH LONG. MAINTENANCE CUT OUT DAMAGED AREA. FABRICATED SUPPORT ANGLES, REINFORCEMENT STRAPS, AND FILLER IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 19-5335-06115-SS1. INSTALLED REPAIR PARTS AT BS 700 BL 24R TO BL 46R IAW AWA ER 19-5335-06115-SS1.

Part: SKIN — DELAMINATED (NR 8 SLAT) · airframe 61,692 hrs · 23,571 cycles

DURING C12 CHECK DISCOVERED 2 SQUARE INCH AREA OF DELAMINATION ON THE UPPER SURFACE OF THE NR 8 SLAT, TRAILING EDGE WEDGE AT THE INBOARD END AT WBL 440R. MAINTENANCE REMOVED DAMAGED AREA IAW BOEING 757-200 SRM 51-70-10-2R. FABRICATED FILLER AND DOUBLER IAW BOEING 757-200 SRM 51-70-10-2R. BONDED REPAIR PARTS TO THE NR 8 SLAT, TRAILING EDGE WEDGE AT WBL 440R IAW BOEING 757-200 SRM 51-70-10-2R.

Part: WEDGE — DELAMINATED (NR 7 SLAT) · airframe 61,692 hrs · 23,571 cycles

GYR - DURING C12 CHECK DISCOVERED ONE SQUARE INCH DELAMINATION AREA ON TOP SURFACE OF NR 7 L/E SLAT 28 INCHES FROM OB EDGE. MAINTENANCE CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER. BONDED FABRICATED PARTS TO TOP SURFACE OF NR 7 L/E SLAT 28 INCHES FROM OB EDGE IAW SRM 57-43-02-01 ITEM 9 AND SRM 51-70-10-2R PAR 4.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,490 hrs · 23,262 cycles

SEA - EEL - DURING OVERNIGHT INSPECTION, DISCOVERED EMERGENCY PATHWAY LIGHT AT ROW 23, LEFT, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT ROW 23L. OPERATIONAL CHECKS WERE GOOD.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 60,154 hrs · 23,099 cycles

PHX - DISCOVERED THE LT INBOARD FLAP DELAMINATING, 20.5" BY 17.5", ADJACENT TO AND UNDERNEATH THE NR 5 SPOILER PANEL. MAINTENANCE REMOVED DELAMINATED CORE AND INNER SKIN IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 19-5753-05275-HF1. FABRICATED FILLER AND DOUBLER IAW BOEING 757-200 SRM 51-70-10 AND AWA ER 19-5753-05275-HF1. BONDED REPAIR PARTS TO THE LT INBOARD TRAILING EDGE FLAP IAW AWA ER 19-5753-05275-HF1. TAP TEST WAS PERFORMED ON REPAIR AREA TO ENSURE NO DAMAGE EXISTED. THE T/E FLAP PANEL WAS PLACED ON MONITOR TO BE REPLACED NO LATER THAN THE NEXT C CHECK.

Part: WIRE — BROKEN (CABIN) · airframe 57,292 hrs · 21,902 cycles

PHX - EEL - DURING 8-DAY CHECK FUNCTIONAL TEST OF EMERGENCY LIGHTING, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 14 LT, OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (ZONE 900 -) · airframe 57,150 hrs · 21,835 cycles

PHX - EMERGENCY EQUIPMENT - DURING 4-DAY CHECK THE FORWARD EMERGENCY FLASHLIGHT DID NOT FLASH RED EVERY 10 SECONDS AS REQUIRED. MAINTENANCE REMOVED AND REPLACED FORWARD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHTS) · airframe 56,543 hrs · 21,583 cycles

DURING C-11 CHECK THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 14 AND 15 WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AT THE L-2 DOOR, OPERATIONAL CHECK OF EMERGENCY LIGHTS WAS GOOD.

Part: TPU — MALFUNCTIONED (NR 1 ENGINE) · airframe 52,245 hrs · 19,761 cycles

DURING DESCENT INTO LAS, WITH IDLE THRUST LEVERS THE NR 1 ENGINE SHUTDOWN. ENGINE RESTARTED AND OPERATED NORMALLY, RECEIVED STATUS MESSAGE LT ENG LP PUMP WITH ENGINE FAILURE FRM 73-11-05-01. DECLARED EMERGENCY, AND LANDED WITH NO FURTHER DIFFICULTIES. MAINTENANCE TROUBLESHOT IAW FIM 71-05-00, REMOVED AND REPLACED THE NR 1 ENGINE FUEL FLOW GOVERNOR IAW T/C R5M73603, AND REPLACED ENGINE TRANSIENT PRESSURE UNIT IAW BMM 75-32-15-004-001. HIGH PRESSURE FUEL PUMP WAS REMOVED AND REINSTALLED IAW T/C R5M73602, OPERATIONAL CHECK WAS GOOD. PART NAME; FUEL FLOW GOVERNOR, MFG; ROLLS-ROYCE, P/N; FFG021BH, S/N; 1947551, TT; 50415, TC; 19771, TSR; 439.

Part: FLASHLIGHT — DISCHARGED (L-2 DOOR) · airframe 52,994 hrs · 20,116 cycles

EMERGENCY EQUIPMENT - DURING 4-DAY CHECK FOUND THE EMERGENCY FLASHLIGHT AT L2 DOOR STATION INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT AT L2 DOOR, OPERATIONAL CHECK WAS GOOD.

Part: INTERCOSTAL — CRACKED · corrosion level 0 · airframe 51,867 hrs · 19,578 cycles

LCQ - MAJOR REPAIR - DURING C-10 CHECK A 1" CRACK WAS FOUND ON MAIN CABIN INTERCOSTAL AT BS 1620, LBL 45. MAINTENANCE CUTOUT CRACKED SECTION ON MAIN CABIN INTERCOSTAL BETWEEN BS 1620 TO BS 1640, LBL 45; FABRICATED A REPAIR DOUBLER AND FILLER; AND INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-13, PG. 1-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,867 hrs · 19,578 cycles

LCQ - MAJOR REPAIR - DURING C-10 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOOR BEAM UPPER CAP AT BS 1640, LBL 60. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED TEE CHORD BS 1640, LBL 65 TO RBL 55; FABRICATED A NEW REPLACEMENT TEE CHORD, 2 EACH REPAIR ANGLES, AND 2 EACH REINFORCEMENT STRAPS; AND INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-51, FIG. 210.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,867 hrs · 19,578 cycles

LCQ - MAJOR REPAIR - DURING C-10 CHECK INTERGRANULAR CORROSION WAS FOUND ON PASSENGER CABIN SHEAR DECK AT BS 1716, BL 0 TO RT CUSP. MAINTENANCE BLENDED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT CORRODED AREA OF SHEAR DECK; FABRICATED A REPAIR DOUBLER AND SHIMS; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-60-51, PG 205-208.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,867 hrs · 19,578 cycles

LCQ - MAJOR REPAIR - DURING C-10 CHECK INTERGRANULAR CORROSION WAS FOUND ON FLOOR BEAM UPPER CAP AT BS 1640, BL 0 TO LBL 5. MAINTENANCE REMOVED CORROSION ON FLOOR BEAM AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED UPPER FLOOR BEAM TEE CAP BS 1640, LBL 65 TO RBL 55; FABRICATED 2 EACH REPAIR ANGLES, 2 EACH STRAPS, AND A NEW REPLACEMENT TEE CHORD; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-51, PG. 209-213.

Part: FRAME — CHAFED · corrosion level 0 · airframe 51,867 hrs · 19,578 cycles

LCQ - MAJOR REPAIR - DURING C-10 CHECK THE CABIN FRAME WAS FOUND CHAFED AT BS 1280, STR 11 R/H, RBL 68. MAINTENANCE REMOVED CHAFED REPAIR DOUBLER AT BS 1280, STR 11 R/H, RBL 68; FABRICATED A REPAIR DOUBLER; AND INSTALLED REPAIR PART IAW B757-200 SRM 53-00-07, PG. 201-203, FIG. 201.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,867 hrs · 19,578 cycles

LCQ - MAJOR REPAIR - DURING C-10 CHECK INTERGRANULAR CORROSION WAS FOUND ON PASSENGER CABIN SHEAR DECK BS 1716, FROM BL 0 TO LT CUSP. MAINTENANCE BLENDED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT CORRODED AREA PASSENGER CABIN SHEAR DECK BS 1716, FROM BL 0 TO LBL 4, AND LBL 27 TO LBL 65; FABRICATED A DOUBLER, FILLER, AND SHIMS; AND INSTALLED REPAIR PARTS IAW B757-200 SRM 53-60-51, FIG. 203, PG. 204-208.

Part: FLAP — SATURATED · corrosion level 0 · airframe 51,867 hrs · 19,578 cycles

LCQ - MAJOR REPAIR - DURING C-10 CHECK X-RAY INSPECTION FOUND MOISTURE ENTRAPMENT IN R/H WING INBOARD AFT FLAP; X-RAY ALSO REVEALED A CRACK IN ENVIRONMENTAL END SEAL. MAINTENANCE CUTOUT AND CLEANED DAMAGED AREAS OF R/H WING INBOARD AFT FLAP; INSTALLED BOND REPAIR IAW B757-200 SRM 51-70-04, FIG. 5, PG. 32.

Part: SKIN — CHAFED · corrosion level 0 · airframe 51,867 hrs · 19,578 cycles

LCQ - MAJOR REPAIR - DURING C-10 CHECK FUSELAGE SKIN PANELS BELOW R/H HORIZONTAL STABILIZER BS 1862 WERE FOUND CHAFED FROM STAB SLIDING SEAL. MAINTENANCE BLENDED CHAFED AREA AND FOUND MATERIAL LOSS OUT OF LIMITS PER B757-200 SRM 53-80-01, PG. 103; REMOVED 2 EACH CHAFED FUSELAGE SKIN PANELS AT BS 1862; FABRICATED 2 EACH NEW REPLACEMENT PANELS; INSTALLED NEW REPAIR PARTS IAW AWA E.R. 19-5381-03002-ES1

Part: SEAT TRACK — CRACKED · corrosion level 0 · airframe 51,867 hrs · 19,578 cycles

LCQ - MAJOR REPAIR - DURING C-10 CHECK A 3/4" CRACK WAS FOUND ON THE UPPER RADIUS OF THE OUTBOARD R/H SEAT TRACK IN THE AFT CARGO COMPARTMENT. MAINTENANCE REMOVED THE SEAT TRACK FROM BS 1180 TO BS 1280, RBL 45.5; FABRICATED A NEW REPLACEMENT SEAT TRACK ; INSTALLED REPAIR PART IAW B757-200 SRM 53-60-52, PG. 1-2.

Part: SKIN — CHAFED · corrosion level 0 · airframe 51,867 hrs · 19,578 cycles

LCQ - MAJOR REPAIR - DURING C-10 CHECK FUSELAGE SKIN PANELS BELOW L/H HORIZONTAL STABILIZER BS 1862 WERE FOUND CHAFED FROM STAB SLIDING SEAL. MAINTENANCE BLENDED CHAFED AREA AND FOUND MATERIAL LOSS OUT OF LIMITS PER B757-200 SRM 53-80-01, PG. 103; REMOVED 2 EACH CHAFED FUSELAGE SKIN PANELS AT BS 1862; FABRICATED 2 EACH NEW REPLACEMENT PANELS; INSTALLED NEW REPAIR PARTS IAW AWA E.R. 19-5381-03002-ES1

Part: SKIN — CORRODED · corrosion level 2 · airframe 51,867 hrs · 19,578 cycles

LCQ - MAJOR REPAIR - DURING C-10 CHECK INTERGRANULAR CORROSION WAS FOUND ON LOWER FUSELAGE SKIN UNDER AFT AIR PHONE ANTENNA BASE, BS 1480. MAINTENANCE REMOVED AFT AIR PHONE ANTENNA AND BLENDED CORROSION AT BS 1480; MATERIAL LOSS OUT OF LIMITS WITH MORE THAN 15 % OF ORIGINAL MATERIAL REMOVED; FABRICATED A REPAIR DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-01, PG. 222-225. AIR PHONE REMOVED PER AWA E.R. 19-2310-01257-KB1.

Part: BUSHING — MIGRATED (NR 2 PYLON) · airframe 51,867 hrs · 19,578 cycles

DISCREPANCY WAS "RT WING NR 2 ENGINE PYLON UPPER LINK, FRONT SPAR ATTACH O/B LUG BUSHING IS MIGRATED O/B LUG I/B BUSHING APPROX .040"". MAINTENANCE PLACED ITEM ON MONITOR TO BE REINSPECTED EVERY 3000 CYCLES AND TO TERMINATE IN 12,000 CYCLES IAW AWA ER 19-5449-99349-BA1. MONITOR WAS CLEARED ON 26APR06 (TT 61692, TC 23571) IN GYR. MAINTENANCE REMOVED AND REPLACED THE UPPER LINK, OUTBOARD LUG, INBOARD LUG BUSHING IAW AWA EO 54-40-10.

Part: CHARGER — FAILED (CABIN) · airframe 49,821 hrs · 18,722 cycles

PHX - EEL - DURING INSPECTION 3 EACH AFT EMERGENCY LIGHTS WERE FOUND INOPERATIVE; RT AFT BULLNOSE, AND THE R4 DOOR SLIDE LIGHT. MAINTENANCE REPLACED BATTERY CHARGER AND BATTERY PACK M736 PER T/C A1C33607, OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 63,477 hrs · 24,624 cycles

PHX - EMERGENCY EQUIPMENT -C- DURING INSPECTION OF EMERGENCY EQUIPMENT THE AFT LT EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERIES IAW GENERAL PRACTICES, REF MPPM 9-1,9. OPERATIONAL CHECK WAS GOOD.

Part: WIRE — BROKEN · airframe 48,792 hrs · 18,313 cycles

PHX - EEL - "C" - EMERGENCY ISLE LIGHT INOPERATIVE AT ROW 23 L/H. MAINTENANCE DISCOVERED BROKEN SPLICE AT OUTBOARD SEAT TRACK ROW 23 L/H. REPAIRED WIRE WITH ENVIRONMENTAL SPLICE OUTBOARD SEAT TRACK ROW 23 L/H IAW SWPM 20-10-00, OPERATIONAL CHECK WAS GOOD.

Part: DUCT — SPLIT (CARGO BAY) · airframe 47,758 hrs · 17,909 cycles

FLT 776 LAS - BW, UPON DEPARTURE A LOUD NOISE AND REVERBERATION CABIN ALT REMAINED AT FIELD ALT. RETURNED TO LAS. REPLACED DUCT, RAN ACFT AND PRESSURIZED TO MORE THAN 3 PSI. ALL INDICATIONS NORMAL.

Part: CONTROL BOX — FAILED (NR 2 ENGINE) · airframe 44,493 hrs · 16,580 cycles

DURING DESCENT THROUGH FL 190 RIGHT CENTER ELECTRIC HYD PUMP PRESS LIGHT ILLUMINATED FOLLOWED BY RIGHT ENGINE FLAME-OUT. RT ENGINE RESTART SUCCESSFUL. BIT CHECK OF ENGINE TRANSIENT PRESSURE UNIT (TPU) DISPLAYED CODE 50, REMOVED AND REPLACED TPU. OPS CHECK GOOD, A/C RETURNED TO SERVICE.

Part: INTERCOSTAL — CORRODED (BS 365 - 377)

CABIN FLOOR INTERCOSTAL BETWEEN FLOORBEAM STA 365-377 AT RBL 14 CORRODED. REMOVED CORROSION, NDT FOR MATL LOSS, OK, TREATED, PRIMED, AND PAINTED. REINSTALLED IAW 757 MM 51-10-00 AND 757 MM 25-41-00.

Part: FLOORBEAM — CORRODED (BS 377)

CORROSION ON FLOORBEAM CENTERLINE SUPPORT AT STA 377 BL 0 INTERSECTION. DRILLED, PAINTED, AND INSTALLED NEW CENTERLINE FLOORBEAM IAW 757 SRM 51-40-02.

Part: CIRCUIT BREAKER — FAILED (COCKPIT)

AFTER TAKEOFF INFLIGHT CREW REPORTED EMERGENCY EXIT LIGHTS ILLUMINATED. FLIGHT DECK SWITCH MOVED FROM ON TO OFF AND BACK TO ARMED, LIGHTS REMAINED ILLUMINATED. REPLACED BATTERY PACKS M9001, M731, M735, M9002 AND M737 AND FOUND CHARGING CB TO BE FAULTY, REPLACED CB. OPERATIONAL CHECK GOOD.

Part: LIGHTS — INOP (ROW 4-8-34)

INTERIOR EMERGENCY LIGHTS ROWS 4 ABC, 8 ABC AND 34 AC INOP. DPI ISSUED MEL 33-51-1 COND 1C. BATTERIES CHARGERS CHARGED EMER BATTERIES NORMALLY IN FLIGHT. ALL EMER LIGHTS OP NORMAL. DPI CLEARED.

Part: FLOOR PAN — CORRODED (BS 1681)

DURING SCHEDULED C-7 INSPECTION, FOUND CABIN FLOOR PAN/WEB AT STA 1681 HAS CORROSION AT FWD EDGE ALONG ENTIRE EDGE. REPAIRED PER SRM 53-60-51, FIGURE 203.

Part: WIRE — DISCONNECTED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROX LIGHTS INOP AT 15L, 20L, AND 21L. REPAIRED AND RECONNECTED LIGHT WIRING.

Part: AIR DISTR — ODOR (COCKPIT)

PHX - FLT 7902 - STRONG FUEL SMELL IN COCKPIT JUST AFTER TOUCH AND GO LANDINGS. SMELL ONLY LASTS A FEW SECONDS, BUT WAS SIGNIFICANT. OPERATED BOTH PACKS WITH APU RUNNING. OPERATED BOTH PACKS WITH BOTH ENGINES RUNNING. UNABLE TO DETECT FUEL SMELL IN FLIGHT DECK. (M)

Part: SUPPORT — CRACKED (RADAR BAY)

PAE - FLT 7849 - DURING ROUTINE SCHEDULED C-6 MAINTENANCE CHECK, FOUND FORWARD RADAR BAY LEFT VERTICAL SUPPORT FOR BATTERY TRAY 13 CRACKED IN RADIUS. REPAIRED PER SRM 53-10-2, SRM 51-40-2. (M)

Part: FRAME — DENTED (BS 1540)

PAE - FLT 7849 - DURING ROUTINE SCHEDULED C-6 MAINTENANCE CHECK, FOUND STATION 1540, LBL 30, WL 153 FRAME DENTED. REPAIRED PER SRM 51-70-11, 51-40, 51-20-01. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

PHX - FLT 2616 - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT MOUNTED EMERGENCY EXIT LIGHTING AT ROW 15 INOPERATIVE. RECONNECTED SEAT HARNESS AT ROW 15. OPERATIONS CHECK GOOD. (X)

Part: MECHANISM — LACK OF LUBE (L2 DOOR)

PHX/SAN - FLT NR 19 - AIR TURNBACK, L2 DOOR WARNING LIGHT ILLUMINATED DURING CLIMB-OUT OF PHX. FLIGHT CREW VERIFIED HANDLE WAS ROTATED TOWARD OPEN, AND MANUALLY HELD HANDLE DOWN. AIRCRAFT RETURNED TO PHX, LANDING WITH FURTHER INCIDENT. MAINTENANCE CLEANED AND LUBED MICRO-SWITCH PLUNGER, AND CHECKED DOOR RIB IAW BMM 52-11-01 AND 52-11-00. CYCLED DOOR TEN TIMES, ALL INDICATIONS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY PACK INOPERATIVE AT POSITION M734. REMOVED AND REPLACED PACK M734, OPS CHECK GOOD. (M)

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY PACK INOPERATIVE AT ROW 24 RT OVERHEAD. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND SEVERAL EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 28 THROUGH ROW 35. REINSTALLED TRACK LIGHTING WIRES AS REQUIRED. OPS CHECK GOOD. (M)

Part: EEL CONNECTOR — LOOSE (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE IN AFT CABIN AND FROM ROW 17 THROUGH ROW 25. REPAIRED WIRE IN AFT CABIN AND RESECURED LOOSE CONNECTOR AT ROW 17. OPS CHECK GOOD. (W)

Part: EEL WIRE — BROKEN (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 30 THROUGH 33. REPAIRED BROKEN WIRING, OPS CHECK GOOD. (W)

Part: EEL ASSY — INOPERATIVE (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 25 TO AFT. REPAIRED LIGHTS, OPS CHECK GOOD. (M)

Part: EEL ASSY — DISCONNECTED (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 30 TO AFT OF AIRCRAFT. RECONNECTED NUMEROUS LIGHTS FROM ROW 30 AFT, OPS CHECK GOOD. (M)

Part: EEL FUSE — FAILED (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE IN AFT CABIN. RECONNECTED SEVERAL LIGHT ASSY'S AND REPLACED FUSE IN BATTERY CHARGER ASSEMBLY IN AFT RT GALLEY. OPS CHECK GOOD. (W)

Part: EEL ASSEMBLY — DISCONNECTED (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR TRACK EMERGENCY EXIT LIGHTS INOPERATIVE, ROW 26 THROUGH ROW 32. RECONNECTED LOWER LIGHT ASSEMBLY AT ROW 32, OPS CHECK GOOD. (W)

Part: EEL — DAMAGED (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROXIMITY EMERGENCY EXIT LIGHTS DAMAGED IN SEVERAL AREAS. REMOVED AND REPLACED LIGHTS AS REQUIRED, OPS CEHCK GOOD. (M)

Part: EEL WIRE — BROKEN (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR TRACK EMERGECNY EXIT LIGHTS INOPERATIVE FROM AFT LAVS TO AFT GALLEY, APPROXIMITELY 20 ROWS. REPAIRED SEVERAL BROKEN WIRES, OPS CHECK GOOD. (Z)

Part: EEL WIRE — DISCONNECTED (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE IN AREA OF L2 DOOR. RECONNECTED WIRES, OPS CHECK GOOD. (Z)

Part: EEL WIRING — BROKEN (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 18 THROUGH ROW 29. RESECURED AND REPAIRED WIRING AT ROWS 18, 24 AND 25, OPS CHECK GOOD. (Z)

Part: EEL ASSY — BROKEN (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND SEVERAL EMERGENCY TRACK LIGHTS BROKEN. REPAIRED BROKEN FLOOR LIGHTING, OPS CHECK GOOD. (M)

Part: INTERCOSTAL — CORRODED (BS 310)

PHX - DURING C-6 INSPECTION, FOUND INTERCOSTAL AT FWD LAV THRESHOLD CORRODED, BS 310 TO 325. REMOVED, FABRICATED AND INSTALLED NEW INTERCOSTAL PER SRM 51-40-02. (Z)

Part: ANGLE — CRACKED (FS 780)

PHX - DURING C-6 INSPECTION, FOUND MID CABIN FLOOR STABILIZER BEAM ANGLE FITTING CRACKED BETWEEN STA 780 AND 800. REMOVED, FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-40-02. (Z)

Part: FLOORBEAM — CORRODED (BS 377.7)

PHX - DURING C-6 INSPECTION, FOUND CORROSION OUT OF LIMITS ON FLOORBEAM AT BS 377.7 LBL 1, 2, 6, 10, 47 AND 51. REPAIRED PER ER 5 53 12 04 AND SRM 53 10 51. (Z)

Part: SUPPORT — CORRODED (FS 398)

PHX - DURING C-6 INSPECTION, FOUND SEAT TRACK SUPPORT ASSEMBLY UPPER CHORD CORRODED BEYOND LIMITS AT STA 398 RBL 24. REMOVED, FABRICATED AND INSTALLED SEAT TRACK SUPPORT PER SRM 51-40-02. (Z)

Part: CHANNEL — CORRODED (BS 400)

PHX - DURING C-6 INSPECTION, FOUND FLOOR HAT CHANNEL CORRODED, STA 400 RBL 24 TO TO RBL 45. REMOVED, FABRICATED AND INSTALLED NEW HAT CHANNEL PER SRM 51-40-02. (Z)

Part: CONNECTOR — LOOSE (CABIN EEL)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND RT AISLE OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE AT R2 AND R3 DOORS. RESEATED CONNECTORS AT M732, M734, AND M735. OPS CHECK GOOD. (X)

Part: BATTERY ASSEMBLY — INOPERATIVE (CABIN EEL)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PATH EMERGENCY EXIT LIGHTS INOPERATIVE, ROWS 20 THROUGH 25 AND FROM THE L3 DOOR THROUGH ROW 32. REMOVED AND REPLACED BATTERY ASSEMBLY AT M734, OPS CHECK GOOD. (X)

Part: EEL WIRE — FAILED (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, SEVERAL AREAS OF EMERGENCY EXIT LIGHTS FAILED TEST. FLOOR MOUNTED LIGHTS BETWEEN ROWS 18 AND 24, AND BOTH FLOOR AND OVERHEAD LIGHTS BETWEEN ROWS 27 AND 32. REPAIRED WIRES, OPS CHECK GOOD. (W)

Part: EEL CONNECTOR — LOOSE (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE ROWS 15 THROUGH 18. RECONNECTED EMERGENCY LIGHTS AT ROW 16, OPS CHECK GOOD. (X)

Part: EEL WIRE — BROKEN (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PATH EMERGENCY EXIT LIGHTS INOPERATIVE, ROWS 5 THROUGH 7 AND ROW 33 TO AFT. RECONNECTED WIRING AND RESECURED LIGHTS AS REQUIRED, OPS CHECK GOOD. (W)