N909AW

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 92,804 hrs · 30,120 cycles

SEAT MOUNTED EMERGENCY LIGHT AT SEAT 13C INOPERATIVE. REPAIRED HARNESS AT 13C. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 92,804 hrs · 30,120 cycles

SEAT MOUNTED EMERGENCY LIGHT AT SEAT 18C INOPERATIVE. CONNECTED LOOSE CONNECTOR AT 18C. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: MONITOR — FAULTY (CABIN) · airframe 89,841 hrs · 29,491 cycles

2 HRS INTO FLIGHT, FLIGHT ATTENDANT NOTICED A SLIGHT BURNING SMELL IN FWD GALLEY AREA, SHE & ANOTHER FLIGHT ATTENDANT TRACED IT TO THE LT FWD VIDEO MONITOR IN 1ST CLASS. MONITOR GOT SHUTDOWN & SMELL WENT AWAY. R & R LT FWD MONITOR.

Part: KNOB — MISSING (COCKPIT DOOR) · airframe 89,222 hrs · 29,365 cycles

UPPER EMER EXIT PANEL ON FLIGHT DECK DOOR IS MISSING THE LT PIN SO IT CANNOT BE OPENED. KNOB WAS MISSING FROM PIN, INSTALLED KNOB ON PIN ON UPPER EXIT PANEL ON FLIGHT DECK DOOR.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 88,988 hrs · 29,318 cycles

C3 CHECK DELAMINATION ON RT INBD FLAP UPPER SKIN AT APPROX 77 INCHES INBD FROM OTBD END & 5.75 INCHES FWD OF TE. REPAIRED RT INBD FLAP UPPER SKIN IAW SRM 51-70-10-2R-4.

Part: HEATER — SHORTED (COCKPIT) · airframe 87,154 hrs · 28,979 cycles

PHX FLT 675 EN-ROUTE HNL TO PHX. CAPTAIN'S FOOT HEATER SHORTED WHEN ACTIVATED. SPARKS FROM ON FLOOR TO LT OF YOKE. R & R CAPTAIN`S LT FOOT WARMER ASSEMBLY. OPERATIONS CHECKED GOOD.

Part: KEELBEAM — CORRODED (ZONE 100 - FUSE) · airframe 85,572 hrs · 28,667 cycles

CORROSION ON RT WHEEL WELL ON KEELBEAM BETWEEN BS 1119 TO 1121, WL 140, RBL 7.5. REPAIRED KEELBEAM IAW EA 205581.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 85,262 hrs · 28,605 cycles

EMERGENCY FLASHLIGHT IN AFT GALLEY INOPERATIVE. REPLACED AFT GALLEY FLASHLIGHT BATTERY, OPS CHECKED OK.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 85,155 hrs · 28,583 cycles

EMERGENCY LIGHTS ON SEATS ROW 29 & 33 INOPERATIVE, BROKEN WIRE. REPAIRED WIRE. OP CHECKED GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 84,222 hrs · 28,392 cycles

PHX - SEAT ROW 14L - EMERGENCY PATH LIGHT INOP. RECONNECTED LOOSE CONNECTOR. OPS CHECK GOOD.

Part: STRAP — CRACKED (FUSELAGE) · airframe 83,682 hrs · 28,287 cycles

C2 CHECK - CRACK ON FUSELAGE SUPPORT STRAP AT BS 1342, RBL 24.25. REPAIRED FUSELAGE SUPPORT STRAP AT BS 1342, RBL 24.25 IAW EA 104525.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 83,682 hrs · 28,287 cycles

C2 CHECK - CRACK ON TIE CLIP AT BS 1300, LBL 24.75. REPLACED TIE CLIP AT BS 1300, LBL 24.75 IAW B757 SRM 51-40-05 & EA 104519.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 83,682 hrs · 28,287 cycles

C2 CHECK - CRACK ON TIE CLIP AT BS 1280, WL 207, LBL 45.5. REPLACED TIE CLIP AT BS 1280, WL 207, LBL 45.5 IAW B757 SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,682 hrs · 28,287 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON RIGHT KEEL SPLICE FITTING AT BS 1180 BETWEEN BL 0 TO LBL 4. REPLACED RIGHT KEEL SPLICE FITTING AT BS 1180 BETWEEN BL 0 TO LBL 4 IAW B757 SRM 51-10-02 & 51-40-02.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,682 hrs · 28,287 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FITTING AT RIGHT KEEL STRUCTURE AT BS 1180, WL 138.5, RBL 3. REPLACED FITTING AT RIGHT KEEL STRUCTURE AT BS 1180, WL 138.5, RBL 3 IAW B737 SRM 51-40-02 & BOEING DRAWING 144N8034.

Part: WIRE — BROKEN (CABIN) · airframe 83,178 hrs · 28,184 cycles

PHX - ROW 26 LT EMERGENCY LIGHT WIRE BROKEN. MAINTENANCE REPINNED BROKEN WIRE ON ROW 26 LT EMERGENCY LIGHT.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 82,769 hrs · 28,106 cycles

PHX - ROW 26L EMERGENCY LIGHT WIRE BROKEN. REMOVED AND REPLACED SEAT HARNESS. OPS CHECK GOOD.

Part: HANDLE — OUT OF ADJUST (L1 DOOR)

LIH - L1 PASSENGER ENTRY DOOR UNABLE TO OPEN OR CLOSE WITH BUTTERFLY HANDLES. MAINTENANCE ADJUSTED ENTRY DOOR. OK FOR SERVICE.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 82,320 hrs · 28,004 cycles

PHX - ROW 12 EMERGENCY LIGHT INOP. REPAIRED CONNECTOR, OP'S NORMAL.

Part: LENS — IMPROPER PART (CABIN) · airframe 80,461 hrs · 27,661 cycles

PHX - SEAT ROW 35 LT HAS INCORRECT ESCAPE PATH LIGHT LENSES. INSTALLED CORRECT RED LENSES ON SEAT ROW 35 LT ESCAPE PATH LIGHTS.

Part: O-RING — CUT (HYDRAULIC SYS)

HNL FLT 125 EN ROUTE HNL TO PHX. DURING FLIGHT, THE RIGHT HYDRAULIC SYSTEM BECAME INOPERATIVE DUE TO LOST HYDRAULIC QUANTITY. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO FIELD HNL. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE AFT DIFFERENTIAL PRESSURE INDICATOR OF THE RIGHT ENGINE FILTER MODULE LEAKING. REPLACED TWO O-RINGS (LARGE O-RING WAS CUT). SERVICED THE RIGHT HYDRAULIC SYSTEM. RAN AND OPS CHECKED THE HYDRAULIC SYSTEM SEVERAL TIMES. OPS CHECKED NORMAL. NO LEAKS NOTED.

Part: SCREW — MISSING (COCKPIT DOOR) · airframe 80,288 hrs · 27,628 cycles

HNL - UPPER RIGHT COCKPIT DOOR EMERGENCY EXIT PIN KNOB MISSING. ACCOMPLISHED INTERIM REPAIR. MAINTENANCE REMOVED TEMP BOLT AND INSTALLED KNURLED SCREW IN LOWER DECOMPRESS PANEL LATCH. OPS GOOD.

Part: SKIN — DEBONDED (LE SLAT) · airframe 79,388 hrs · 27,447 cycles

C1 CHECK - DISBONDING ON UPPER SURFACE OF NR 9 SLAT TRAILING EDGE WEDGE. REPAIRED UPPER SURFACE OF NR 9 SLAT TRAILING EDGE WEDGE IAW B757 SRM 57-43-02 & 51-70-10.

Part: PLUNGER — INOPERATIVE (COCKPIT) · airframe 78,928 hrs · 27,359 cycles

PHX - FLIGHT DECK HOLD OPEN PLUNGER WILL NOT KEEP DOOR OPEN. MAINTENANCE REMOVED AND REPLACED DOOR HOLD OPEN ASSEMBLY.

Part: MEGAPHONE — INOPERATIVE (CABIN)

PHX - THE MEGAPHONE IN FIRST CLASS WAS INOPERATIVE. REPLACED THE FIRST CLASS MEGAPHONE.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

PHX - THE AFT FLIGHT ATTENDANT SEAT FLASHLIGHT BATTERY HAD A LOW CHARGE. MAINTENANCE REMOVED AND REPLACED THE AFT FLIGHT ATTENDANT SEAT FLASHLIGHT BATTERY.

Part: SEAL — CRACKED (LT ENGINE)

PHX FLT 26 EN ROUTE OGG TO PHX. THE CREW NOTED AN ODOR THAT STARTED ON THE GROUND, AND CONTINUED THROUGH CLIMB. THE ODOR DISSIPATED AT CRUISE ALTITUDE. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT ENGINE HAS OIL LEAKING FROM THE NR 1 BEARING CAVITY. MAINTENANCE REPLACED THE LEFT ENGINE. VENDOR SHOP FINDINGS: FOUND CRACKED/BROKEN LPC DISC REAR SEAL PANEL.

Part: SLIDE — READS LOW (EMERGENCY EXIT)

PHX - THE LEFT, NUMBER THREE EMERGENCY ESCAPE EXIT HATCH SLIDE PRESSURE IS OUT OF THE GREEN BAND. REMOVED AND REPLACED SLIDE. PASSED ALL TESTS AS REQUIRED BY MAINTENANCE MANUALS, AND OVERHAULED.

Part: LIGHT — INOPERATIVE (CABIN)

PHX - EMERGENCY LIGHT WAS INOPERATIVE AT SEAT ROW 28L. REMOVED AND REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 28L.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 74,123 hrs · 24,522 cycles

MCN - MAJOR REPAIR - C4 CHECK - GALVANIC CORROSION ON STRINGER AT BS 758, S20R. REPAIRED STRINGER AT BS 758, S20R IAW EA 130379.

Part: SKIN — CORRODED (FUSELAGE) · airframe 74,123 hrs · 26,433 cycles

MCN - C4 - MAJOR REPAIR - CORROSION ON FUSELAGE SKIN AIRPHONE FORWARD ANTENNA AREA BETWEEN BS 1520 TO BS 1530 LOWER LOBE. REPAIRED FUSELAGE SKIN AIRPHONE FORWARD ANTENNA AREA BETWEEN BS 1520 TO BS 1530 LOWER LOBE IAW EA 130375.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 74,123 hrs · 26,433 cycles

MCN - C4 - MAJOR REPAIR - CRACKS ON MAIN DECK FLOORBEAM AT BS 700, RBL 24.75 & BS 700, RBL 45.5. REPAIRED MAIN DECK FLOORBEAM AT BS 700, RBL 24.75 & BS 700, RBL 45.5 IAW B757 SRM 53-00-51.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 74,123 hrs · 26,433 cycles

MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON CHANNEL AT BS 716, WL 208. REPLACED CHANNEL AT BS 716, WL 208 IAW B757 SRM 51-40-02.

Part: SKIN — CORRODED (FUSELAGE) · airframe 74,123 hrs · 26,433 cycles

MCN - C4 - MAJOR REPAIR - CORROSION ON FUSELAGE SKIN AT BS 763, S20R. REPAIRED FUSELAGE SKIN AT BS 763, S20R IAW B757 SRM 53-00-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 74,123 hrs · 26,433 cycles

MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON FLOORBEAM AT BS 365.25, BL 0 - RBL 14, WL 208. REPAIRED FLOORBEAM AT BS 365.25, BL 0 - RBL 14, WL 208 IAW B757 SRM 53-00-51.

Part: SILL — CORRODED (FUSELAGE) · airframe 74,123 hrs · 26,433 cycles

MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON THE L3 DOOR LOWER SILL WEB LOWER SURFACE AT BS 1345, WL 208. REPLACED THE L3 DOOR LOWER SILL WEB LOWER SURFACE AT BS 1345, WL 208 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 74,123 hrs · 26,433 cycles

MCN - MAJOR REPAIR - C4 CHECK - CRACKED CABIN FLOOR SUPPORT AT BS 377.7, BL 0, WL 208. REPLACED CABIN FLOOR SUPPORT AT BS 377.7, BL 0, WL 208 IAW B757 SRM 51-40-02.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,123 hrs · 26,433 cycles

MCN - C4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON CHANNEL AT L-4 DOOR LOWER SILL AT BS 1667, WL 208. REPLACED CHANNEL AT L-4 DOOR LOWER SILL AT BS 1667, WL 208 IAW B757 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,123 hrs · 26,433 cycles

MCN - C4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT BS 740, WL 208 BETWEEN RBL 50 TO RBL 58. REPAIRED FLOORBEAM AT BS 740, WL 208 BETWEEN RBL 50 TO RBL 58 IAW B757 SRM 53-00-51.

Part: SKIN — CORRODED (FUSELAGE) · airframe 74,123 hrs · 26,433 cycles

MCN - C4 - MAJOR REPAIR - CORROSION ON ATC LEFT ANTENNA BLANKING PLATE LOWER SURFACE. REPLACED AFT ATC LEFT ANTENNA BLANKING PLATE & INSTALLED IAW JOB CARD 19C12053004.

Part: PLATE — CORRODED (FUSELAGE) · airframe 74,123 hrs · 26,433 cycles

MCN - C4 - MAJOR REPAIR - CORROSION ON L-2 DOOR SILL PLATE SUPPORT AT BS 716. REPLACED L-2 DOOR SILL PLATE SUPPORT AT BS 716 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 74,123 hrs · 26,433 cycles

MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON INTERCOSTAL AT BS 1402, S4L, WL 160. REPLACED INTERCOSTAL AT BS 1402, S4L, WL 160 IAW BOEING DWG 146N5425-19.

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,123 hrs · 26,443 cycles

MCN - C4 - MAJOR REPAIR - CRACK ON INTERCOSTAL CLIP AT BS 660, WL 208, RBL 45.50. REPLACED INTERCOSTAL CLIP AT BS 660, WL 208, RBL 45.50 IAW B757 SRM 51-40-05 & BOEING DRAWING 140N2505.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,123 hrs · 26,433 cycles

MCN - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON ANGLE AT BS 1716, WL 207, LBL 14. REPLACED ANGLE AT BS 1716, WL 207, LBL 14 IAW B757 SRM 51-40-02 & BOEING DRAWING 146N5240.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,123 hrs · 26,433 cycles

MCN - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON CREASE BEAM INNER CHORD AT BS 1343, WL 208, LBL 61. REPLACED CHORD AT BS 1343, WL 208, LBL 61 IAW B757 SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,123 hrs · 26,443 cycles

MCN - C4 - MAJOR REPAIR - CRACK ON INTERCOSTAL CLIP BETWEEN BS 1320 TO BS 1340, WL 208, BL 0. REPLACED INTERCOSTAL CLIP BETWEEN BS 1320 TO BS 1340, WL 208, BL 0 IAW B757 SRM 51-40-02 & BOEING DRAWING 140N2505.

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,123 hrs · 26,433 cycles

MCN - C4 - MAJOR REPAIR - CRACK IN CLIP BETWEEN BS 860 TO BS 880, WL 208, BL 0. REPLACED CLIP BETWEEN BS 860 TO BS 880, WL 208, BL 0 IAW B757 SRM 51-40-02 & BOEING DRAWING 140N2505.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 74,123 hrs · 26,433 cycles

MCN - C4 - MAJOR REPAIR - NR # 6167458 - CRACK IN ANGLE BETWEEN BS780 TO BS800, WL208, BL0. REPLACED ANGLE BETWEEN BS780 TO BS800, WL208, BL0 IAW B757 SRM 51-40-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 74,123 hrs · 26,443 cycles

MCN - C4 - MAJOR REPAIR - CRACKS ON ANGLE BETWEEN BS 440 TO BS 460, WL 208, BL 0. REPLACED ANGLE BETWEEN BS 440 TO BS 460, WL 208, BL 0 IAW B737 SRM 51-40-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 74,123 hrs · 26,433 cycles

MCN - C4 - MAJOR REPAIR - CRACKS IN ANGLE BETWEEN BS 540 TO BS 560, WL 208, BL 0. REPLACED ANGLE BETWEEN BS 540 TO BS 560, WL 208, BL 0 IAW B757 SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,123 hrs · 26,433 cycles

MCN - C4 - MAJOR REPAIR - CRACKS IN CLIP BETWEEN BS 660 TO BS 680, WL 208, BL 0. REPLACED CLIP BETWEEN BS 660 TO BS 680, WL 208, BL 0 IAW B757 SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,123 hrs · 26,433 cycles

MCN - C4 - MAJOR REPAIR - CRACK IN CLIP AT BS 660, WL 208, RBL 45.50. REPLACED CLIP AT BS 660, WL 208, RBL 45.50 IAW B757 SRM 51-40-02.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,123 hrs · 26,433 cycles

MCN - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON CHANNEL AT BS 1670, S17L, WL 207. REPLACED CHANNEL AT BS 1670, S17L, WL 207 IAW B757 SRM 51-40-02.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,123 hrs · 26,433 cycles

MCN - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON STIFFENER AT BS 1670, S17R, WL 207. REPLACED STIFFENER AT BS 1670, S17R, WL 207 IAW B757 SRM 51-40-02.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,123 hrs · 26,433 cycles

MCN - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON STIFFENER AT BS 1659, S17L, WL 207. REPLACED STIFFENER AT BS 1659, S17L, WL 207 IAW B757 SRM 51-40-02.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,123 hrs · 26,433 cycles

MCN - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON STIFFENER AT BS 1655, S17R, WL 208. REPLACED STIFFENER AT BS 1655, S17R, WL 208 IAW B757 SRM 51-40-02.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,123 hrs · 26,433 cycles

MCN - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON CLIP CHANNEL AT BS 1655, S17L, WL 207. REPLACED CLIP CHANNEL AT BS 1655, S17L, WL 207 IAW B757 SRM 51-40-02.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,123 hrs · 26,433 cycles

MCN - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON STIFFENER AT BS 1659, S17R, WL 208. REPLACED STIFFENER AT BS 1659, S17R, WL 208 IAW B757 SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 74,123 hrs · 26,433 cycles

MCN - C4 - MAJOR REPAIR - CRACK IN CLIP AT BS 350, S10L. REPLACED CLIP AT BS 350, S10L IAW B757 SRM 51-40-02 & BOEING DRAWING 141N8321.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 74,123 hrs · 26,443 cycles

MCN - C4 - MAJOR REPAIR - CRACK ON CHANNEL AT BS 310.5, WL 208, BL 0. REPLACED CHANNEL AT BS 310.5, WL 208, BL 0 IAW BOEING DRAWING 141N5810.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,123 hrs · 26,433 cycles

MCN - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON DECK PLATE AT BS 1716, WL 208 BETWEEN BL 0 TO LBL 14. REPAIRED DECK PLATE AT BS 1716, WL 208 BETWEEN BL 0 TO LBL 14 IAW B757 SRM 53-60-51.

Part: AILERON — DELAMINATED (RT WING) · airframe 72,270 hrs · 26,031 cycles

PHX - RON - MAJOR REPAIR - LOG 4521789 - DELAMINATION WITH PARTIAL SEPARATION ON RIGHT HAND AILERON LOWER LEADING EDGE JUST INBOARD OF OUTBOARD PCA. REPAIRED RIGHT HAND AILERON LOWER LEADING EDGE IAW B757 SRM 57-60-01, 51-70-04, & 51-70-17.

Part: LIGHT — INOPERATIVE (R4 DOOR)

GIRT BAR ENGAGEMENT LIGHT EXTIN WITH EVACUATION SLIDE ARMING LEVER IN ENGAGE POSITION AT ENTRY/SERVICE DOOR 4R. MAINTENANCE RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN)

PHX - THE RED EMERGENCY LIGHT ON THE END OF SEAT ROW 10L WAS INOPERATIVE. MAINTENANCE REPLACED THE BULBS IN THE EMERGENCY LIGHT AT SEAT ROW 10L. OK FOR SERVICE.

Part: WEB — CRACKED (ZONE 200) · airframe 70,089 hrs · 25,537 cycles

MCN C3 MAJOR REPAIR NR 6122889 WEB CRACKED AT BS 1620 S10L. REPLACED WEB AT BS 1620 S10L IAW SRM 51-40-02-OG.

Part: SUPPORT — CORRODED (ZONE 200) · airframe 70,089 hrs · 25,537 cycles

MCN-C3 -MAJOR REPAIR- INTERGRANULAR CORROSION ON SUPPORT AT BS 1681.8, WL 208.1, BL 0. REPLACED SUPPORT AT BS 1681.8, WL 208.1, BL 0 IAW B757 SRM 51-40-02-0G. (S)

Part: STRAP — CRACKED (ZONE 200)

MCN-C3- MAJOR REPAIR - CRACK ON STABILIZATION STRAP BS 1660 BL 24.75. REPAIRED STABILIZATION STRAP BS 1660 BL 24.75 IAW B757 SRM 51-40-02-0G. (S)

Part: SLIDE — LOW PRESSURE (L4 DOOR)

PHX- THE L4 DOOR EMERGENCY ESCAPE SLIDE PRESSURE WAS FOUND LOW. MAINTENANCE REPLACED THE L4 DOOR EMERGENCY ESCAPE SLIDE. OK FOR SERVICE. (B)

Part: BATTERY — DISCHARGED (FLASHLIGHT)

PHX - THE FLASHLIGHT AT FLIGHT ATTENDANT SEAT AFT OF AFT RIGHT LAVATORY WAS INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY. OK FOR SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

PHX - THE FLASHLIGHT AT DOOR L2 FLIGHT ATTENDANT SEAT WAS INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT BATTERY AT DOOR L2 FLIGHT ATTENDANT SEAT.

Part: LIGHT — BROKEN (ROW 10L) · airframe 67,295 hrs · 24,927 cycles

MAINTENANCE FOUND THE EMERGENCY LIGHT AT ROW 10L INOPERATIVE. REPLACED LIGHT ASSEMBLY. NO FURTHER FAULTS.

Part: WIRE — BURNED (CABIN LIGHTS) · airframe 65,508 hrs · 24,513 cycles

PHX - SMOKE - 7763452 - WHILE TROUBLE SHOOTING FORWARD LAV AND THRESHOLD LIGHTING ISSUES, MX DISCOVERED ARCED WIRING AT ROW 4 OVERHEAD AREA NEXT TO THE NR 2 VIDEO MONITOR. MX COMPLIED WITH ER 19-2335-07142-KK1 FOR ARCED WIRING. SYSTEM OPERATIONAL CHECKS WERE GOOD PER AMM 33-25-00, 33-26-00, 33-24-00, 38-32-00, 38-13-51-4, 33-51-00-5 AND T/C A1B23604. THE A/C WAS RETURNED TO SERVICE.

Part: TACH GENERATOR — FAILED (RT SIDE) · airframe 64,712 hrs · 24,346 cycles

DURING CRUISE FLIGHT, THE CREW DOCUMENTED THE FOLLOWING FAULTS ON LPS 7446894, 7446895, 7446896. CREW REPORTED THE FOLLOWING: RIGHT CENTER FUEL PUMP WAS INOPERATIVE. RIGHT ENGINE BLEED INOPERATIVE. RIGHT ENGINE N3 INDICATION INOPERATIVE. MX REPLACED THE N3 TACH GENERATOR AND THE NR 2 ENGINE SPEED CARD. OPERATIONAL CHECK WAS GOOD DURING ENGINE RUN.

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 64,568 hrs · 243,183 cycles

FLIGHT 432: PHX - OGG - ATB - PRIOR TO REACHING THE COAST, THE CREW NOTICED AN ELECTRICAL SMELL IN THE FLIGHT STATION. THE CREW SHUT DOWN THE LEFT PACK AND THE SMELL WENT AWAY. BASED ON THE REQUIREMENTS TO HAVE BOTH PACKS OPERATING FOR ETOPS OPERATION, THE CREW RETURNED TO PHX. NO EMERGENCY DECLARED. THE LANDING WAS UNEVENTFUL. MX NOTICED THE CAPTAINS WINDSHIELD SHOWED SIGNS OF ARCHING, MX REMOVED AND REPLACED THE CAPTAINS WINDSHIELD, OPS/LEAK CHECK WAS GOOD. THE A/C WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (ZONE 600) · airframe 64,314 hrs · 24,258 cycles

MCN - CRACK FOUND ON COVE SKIN OF RIGHT WING NR 9 SLAT INBOARD PANEL 624CB, WS 574.8 - 605.3. REPAIRED COVE SKIN OF RIGHT WING NR 9 SLAT INBOARD PANEL 624CB, WS 574.8 - 605.3 IAW BOEING DWG 114N4076, B757 SRM 51-40-02-06 PAR 4-7/4-9, FIG 8-12/8-16, AND B757 SRM 51-40-04-0E, FIG 1.

Part: ATTACH ANGLE — CRACKED (ZONE 200) · airframe 64,314 hrs · 24,258 cycles

MCN - MAIN CABIN INTERCOSTAL UPPER ATTACH ANGLE CRACKED, BS 1520 - BS 1540, BL 0. REPLACED MAIN CABIN INTERCOSTAL UPPER ATTACH ANGLE CRACKED, BS 1520 - BS 1540, BL 0 IAW B737-300SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (ZONE 200) · airframe 64,314 hrs · 24,258 cycles

MCN - MAJOR REPAIR - MAIN CABIN INTERCOSTAL UPPER ATTACH ANGLE CRACKED, BS 1420 - BS 1440, BL 0. REPLACED MAIN CABIN INTERCOSTAL UPPER ATTACH ANGLE CRACKED, BS 1420 - BS 1440, BL 0 IAW B737-300SRM 51-40-02.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 64,314 hrs · 24,258 cycles

MCN - MAJOR REPAIR - C-02 CHECK - CRACKS ON TEE CAP, AFT CLIP, BS 1320, LBL 45.5, WL 208.10. REPLACED T-CAP, AFT CLIP, BS 1320, LBL 45.5, WL 208.10 IAW B757-200 SRM 51-40-02.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 64,314 hrs · 24,258 cycles

MCN - MAJOR REPAIR - C-02 CHECK - FLOORBEAM SUPPORT CLIP, BS 1300, RBL 48.5, WL 208. REPLACED FLOORBEAM SUPPORT CLIP CRACKED, BS 1300, RBL 48.5, WL 208 I/A/W B757-200 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 64,314 hrs · 24,258 cycles

MCN - CORROSION ON MAIN CABIN SUPPORT, BS 1664 - BS 1681.8, RBL 56, WL 208. REPLACED MAIN CABIN SUPPORT, BS 1664 - BS 1681.8, RBL 56, WL 208 IAW B757-200 SRM 51-40-02.

Part: WEDGE — DELAMINATED (ZONE 500) · airframe 64,314 hrs · 24,258 cycles

MCN - MAJOR REPAIR - LEFT WING NR 1 SLAT OUTBOARD TRAILING EDGE WEDGE DELAMINATED, WS 799 - WS 801. REPAIRED LEFT WING NR 1 SLAT OUTBOARD TRAILING EDGE WEDGE, WS 799 - WS 801 IAW B757-200 SRM 51-70-10-2R4, REPAIR 4, FIG 201.

Part: WEDGE — DELAMINATED (ZONE 500) · airframe 64,314 hrs · 24,258 cycles

MCN - LEFT WING NR 5 SLAT INBOARD AND OUTBOARD TRAILING EDGE WEDGES DELAMINATED, WS 177.50 AND WS 258.50. REPAIRED LEFT WING NR 5 SLAT INBOARD AND OUTBOARD TRAILING EDGE WEDGES, WS 177.50 AND WS 258.50 IAW B757-200 SRM 51-70-10-2R2, REPAIR 2, FIGURE 203.

Part: SKIN — CORRODED (ZONE 100) · airframe 64,314 hrs · 24,258 cycles

MCN - CORROSION ON FUSELAGE EXTERIOR SKIN, BS 1556, S30, UNDER THE AFT AIRPHONE ANTENNA. REPAIRED FUSELAGE EXTERIOR SKIN, BS 1556, S30 IAW B757-200 SRM 53-00-01-2R3.

Part: SKIN — CRACKED (ZONE 500) · airframe 64,314 hrs · 24,258 cycles

MCN - MAJOR REPAIR - LEFT WING NR 2 SLAT LOWER SURFACE SKIN CRACKED, SS 574. REPLACED LEFT WING NR 2 SLAT LOWER SURFACE SKIN, SS 574 IAW B737-300 SRM 51-40-04 AND 51-40-02.

Part: SKIN — CRACKED (ZONE 600) · airframe 64,314 hrs · 24,258 cycles

MCN - RIGHT WING NR 9 SLAT INNER COVE SKIN CRACKED, SS 594.50 - SS 623.50. REPLACED RIGHT WING NR 9 SLAT INNER COVE SKIN, SS 594.50 - SS 623.50 IAW B757-200 SRM 51-40-02 AND BOEING DRAWING 114N4076.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 62,670 hrs · 23,895 cycles

HNL - DIVERSION - FLT 931 - DURING CLIMB-OUT OF OGG EN ROUTE TO PHX, THE CREW NOTICED THAT THE CABIN WAS CLIMBING WITH THE AIRCRAFT IN AUTO 1 POSITION. RECEIVED CABIN ALT MASTER CAUTION AND SWITCHED TO AUTO 2, THERE WAS NO CHANGE. RECEIVED CABIN ALT 1 AND 2 STATUS MESSAGE WITH BOTH C/B/S IN. CREW DIVERTED TO HNL AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE AUTO 2 CABIN PRESSURE CONTROLLER IAW MM 21-31-02-4. THE CABIN ALT AUTO CONTROLLER (AUTO 1) FAILED BITE CHECK, FAULTING THE AC MOTOR. REMOVED AND REPLACED BOTH A/C MOTORS ON THE OUTFLOW VALVE ACTUATOR IAW AMM 21-31-05-4. OPERATIONAL CHECKS WERE GOOD FOR BOTH AUTO CONTROLLERS.

Part: WIRE — BROKEN (CABIN) · airframe 62,537 hrs · 23,860 cycles

PHX - EEL - DURING OVERNIGHT MAINTENANCE DISCOVERED BOTH RED EMERGENCY LIGHTS WERE INOPERATIVE AT ROW 27. MAINTENANCE REPAIRED BROKEN WIRE AT ROW 27L FOR EMERGENCY ESCAPE PATH LIGHTING. OPERATIONAL CHECKS WERE GOOD.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,782 hrs · 23,443 cycles

PHX - EEL - DURING INSPECTION DISCOVERED ROW 15 ABC EMERGENCY ESCAPE PATH LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SEAT HARNESS AT ROW 15 ABC. OPERATIONAL CHECKS WERE GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 59,550 hrs · 22,899 cycles

DURING 4 DAY CHECK, FOUND EMERGENCY PATH LIGHTS FROM SEAT ROW 1 TO ROW 8 INOPERATIVE. MAINTENANCE REPAIRED WIRING PER CAP 20. REMOVED AND REPLACED SEAT HARNESS AT ROW 5. ALSO, REMOVED AND REPLACED POWER SUPPLY AND BATTERY.

Part: CONNECTOR — LOOSE (TACH) · airframe 59,510 hrs · 22,887 cycles

LAX - ABORTED TAKEOFF - FLT 0033 - DURING TAKEOFF HAD NO N3 INDICATION AT 90 KNOTS. ABORTED TAKEOFF, RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND CONNECTOR D1338 LOOSE, N3 TACH TRANSMITTER. TIGHTENED LOOSE CONNECTOR, D1338, IAW BOEING 757 FIM 77-12-00 FIG 105. PERFORMED OPERATIONAL CHECK IAW BOEING 757 AMM 71-00-00-2. OPERATIONAL CHECKS WERE GOOD.

Part: RESERVOIR — LOW (DOOR R2) · airframe 59,483 hrs · 22,874 cycles

SAL - EES - DURING C1 CHECK FOUND THE L2 EMERGENCY RESERVOIR PRESSURE LOW. MAINTENANCE REMOVED AND REPLACED THE RESERVOIR IAW BOEING 757 MM 52-11-30.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,483 hrs · 22,874 cycles

SAL - MAJOR REPAIR - DURING C1 CHECK FOUND CORROSION ON SEAT TRACK LOCATED AT STA 1560, BL 24.5R, WL 208.1. MAINTENANCE REMOVED CORROSION AT SEAT TRACK LOCATED AT STA 1560, BL 24.5R, WL 208.1 IAW BOEING 757 SRM 53-00-52 AND FOUND OUT OF LIMITS IAW BOEING 757 SRM 53-00-52 FIG 101. REMOVED SEAT TRACK AT STA 1560, BL 24.5R, WL 208 AND INSTALLED REPLACEMENT SEAT TRACK IAW BOEING 757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,483 hrs · 22,874 cycles

SAL - MAJOR REPAIR - DURING C1 CHECK DISCOVERED GALVANIC CORROSION LOCATED ON THE FLOOR SUPPORT EXTRUSION AT STA 1718, BL 0, WL 208.1. NO ALLOWABLE DAMAGE LIMITS FOUND. MAINTENANCE REMOVED CORRODED FLOOR EXTRUSION LOCATED AT STA 1718, BL 0, WL 208.1 IAW BOEING 757 SRM 51-40-02 PG 1. INSTALLED REPLACEMENT FLOOR EXTRUSION AT STA 1718, BL 0, WL 208.1 IAW BOEING 757 SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE)

SAL - MAJOR REPAIR - DURING C1 CHECK FOUND CORROSION ON LOWER SILL FITTING CUTOUT FROM STA 1380 TO STA 1440. NO ALLOWABLE DAMAGE LIMITS LISTED. MAINTENANCE REMOVED AND REPLACED THE LOWER SILL FITTING CUT OUT FROM STA 1380 TO STA 1440 IAW BOEING 757 SRM 51-10-02.

Part: FRAME — DAMAGED (BS 720) · airframe 59,148 hrs · 22,723 cycles

PHX - FORWARD CARGO LOADING SYSTEM, AT BL 0, FROM STA 720 THROUGH STA 820, FRAMES DAMAGED BY LOADING JACK SCREW. MAINTENANCE TRIMMED OUT DAMAGE AREA IAW AWA ER 19-5332-05121-RA2. FABRICATED REPAIR ANGLES AND FRAME CLIPS IAW AWA ER NR 19-5332-05121-RA2. INSTALLED FABRICATED REPAIR PARTS FROM STA 720 THROUGH STA 820 IAW AWA ER NR 19-5332-05121-RA2.

Part: CONNECTOR — SHORTED (LT MLG) · airframe 57,305 hrs · 21,926 cycles

ON CLIMB OUT OF PHX EN ROUTE TO MSP WHEN SELECTING LANDING GEAR UP THE LANDING GEAR WOULD NOT RETRACT, TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE TROUBLESHOT WIRING AND FOUND SHORT TO GROUND ON PIN 11 OF L/H MAIN LANDING GEAR TILT SENSOR CONNECTOR D40084J. REMOVED PINS 11 AND 12 FROM CONNECTOR D40084J AND RESISTANCE DISAPPEARED. REPLACED CONNECTOR D40084J IAW WDM REF. D280N012. PERFORMED LANDING GEAR RETRACTION TEST IAW BMM 32-32-00, TILT SENSOR TEST IAW BMM 32-09-07, L/H LANDING GEAR TRANSDUCER TEST IAW BMM 32-41-06, AND BRAKE TEMPERATURE TEST IAW BMM 32-46-00, ALL TESTS WERE GOOD.

Part: WIRE — BURNED (EMER LIGHT CONN) · airframe 56,005 hrs · 21,350 cycles

PHX - EEL - DURING 8-DAY CHECK A BURNED WIRE WAS FOUND AT EMERGENCY LIGHT POWER SUPPLY CONNECTOR D9006 PIN 18, BS 1650. MAINTENANCE SPLICED DAMAGED WIRE AT EMERGENCY LIGHT POWER SUPPLY CONNECTOR D9006 PIN 18, BS 1650, OPERATIONAL CHECK WAS GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,001 hrs · 21,348 cycles

DURING INSPECTION FOUND THE L-1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER FOR L-1 DOOR EXTERIOR EMERGENCY EXIT LIGHT, OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,826 hrs · 21,276 cycles

LAS - EEL - DURING 8-DAY CHECK THE L-1 DOOR OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY M731 AT BS 369, LBL 5, WL 290, OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 55,002 hrs · 20,973 cycles

LCQ - EMERGENCY EQUIPMENT - DURING C-12 CHECK FOUND THE EMERGENCY FLASHLIGHTS INOPERATIVE AT THE L-4 & R-3 DOORS. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERIES AT THE L-4 & R-3 DOOR, OPERATIONAL CHECK WAS GOOD.

Part: SENSOR — FAULTY (GIRT BAR) · airframe 51,699 hrs · 30,031 cycles

LCQ - EEL - DURING C-17 CHECK FOUND THE R-1 DOOR FORWARD & AFT GIRT BAR PROXIMITY SENSORS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BOTH FORWARD & AFT R-1 DOOR GIRT BAR PROXIMITY SENSORS IAW BMM 25-66-11, OPERATIONAL CHECK WAS GOOD.

Part: WEB — CRACKED (THRESHOLD) · airframe 55,002 hrs · 20,973 cycles

LCQ - MAJOR REPAIR - DURING C-12 CHECK A .5625 INCH CRACK WAS FOUND ON R-1 DOOR THRESHOLD WEB AT BS 350, RBL 64, STR 17 RT. MAINTENANCE CUT OUT CRACKED AREA OF R-1 DOOR THRESHOLD WEB AT BS 350, RBL 64, STR 17 RT; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B757 SRM 51-70-13, FIG 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,002 hrs · 20,973 cycles

LCQ - MAJOR REPAIR - DURING C-12 CHECK EXFOLIATION CORROSION WAS FOUND AROUND NUT PLATES ON FLOOR SUPPORT CHANNEL AT R-1 DOOR THRESHOLD BS 332 TO BS 360, RBL 59. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT CHANNEL FROM BS 332 TO BS 360, RBL 59; FABRICATED A NEW REPLACEMENT SUPPORT CHANNEL PER DWG 141N1560; INSTALLED REPAIR PART IAW B757 SRM 51-40-02 FIG 8 PG 1.

Part: FITTING — CORRODED (FUSELAGE) · airframe 55,002 hrs · 20,973 cycles

LCQ - MAJOR REPAIR - DURING C-12 CHECK PITTING CORROSION WAS FOUND ON INBOARD FACE AROUND BORE OF NR 1 ENGINE PYLON OUTBOARD WING SIDE LOAD ATTACH FITTING. MAINTENANCE INCREASED BORE REMOVING CORROSION DAMAGE ON OUTBOARD WING SIDE LOAD ATTACH FITTING; FABRICATED A REPAIR BUSHING PER DWG 112N7005; INSTALLED REPAIR PART IAW AWA ER 19-5704-04008-ES1.

Part: FITTING — CRACKED (BULKHEAD) · airframe 55,002 hrs · 20,973 cycles

LCQ - MAJOR REPAIR - DURING C-12 CHECK A .0625 INCH CRACK WAS FOUND IN FORWARD SLEEVE BOLT HOLE OF NR 1 ENGINE PYLON RT MID BULKHEAD FITTING PPS 174.30. MAINTENANCE REAMED OUT HOLE; FABRICATED A BUSHING; INSTALLED REPAIR PART IAW AWA ER 19-5453-04006-SS1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 55,002 hrs · 20,973 cycles

LCQ - MAJOR REPAIR - DURING C-12 CHECK A 3 INCH CRACK WAS FOUND ON CABIN FLOOR INTERCOSTAL BS 780-800, BL-0. MAINTENANCE REMOVED CRACKED INTERCOSTAL BS 780-800, BL-0-; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW B757-200 SRM 53-00-51, FIG 204, PG 214-215.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 55,002 hrs · 20,973 cycles

LCQ - MAJOR REPAIR - DURING C-12 CHECK A 2 INCH CRACK WAS FOUND ON CABIN FLOOR INTERCOSTAL BS 860-880, BL-0. MAINTENANCE REMOVED CRACKED INTERCOSTAL BS 860-880, BL-0; FABRICATED A REPAIR ANGLE; INSTALLED REPAIR PART IAW B757-200 SRM 53-00-51 FIG 204, PG 214-215.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 55,002 hrs · 20,973 cycles

LCQ - MAJOR REPAIR - DURING C-12 CHECK CORROSION WAS FOUND ON FLOOR ATTACH FITTING BS 365-377, RBL 50. MAINTENANCE REMOVED CORRODED FLOOR ATTACH FITTING BS 365-377, RBL 50; FABRICATED A NEW REPLACEMENT FITTING; INSTALLED REPAIR PART IAW B757 SRM 51-40-02 FIG 9.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 5,502 hrs · 20,973 cycles

LCQ - MAJOR REPAIR - DURING C-12 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM THAT EXTENDS UNDER R-1 DOOR THRESHOLD DRAIN PLATE BS 365, RBL 45 TO RBL 62. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM BS 365, RBL 45 TO RBL 62; FABRICATED A NEW REPLACEMENT SECTION OF CHORD, 2 EACH REPAIR ANGLES & STRAPS; INSTALLED REPAIR PARTS IAW B757 SRM 53-00-51 FIG 203, SHTS 1-5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,002 hrs · 20,973 cycles

LCQ - MAJOR REPAIR - DURING C-12 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR ATTACH ANGLE BS 440, LBL 64. MAINTENANCE REMOVED CORRODED FLOOR ATTACH ANGLE FROM BS 430 TO BS 450, LBL 64; FABRICATED A NEW REPLACEMENT ATTACH ANGLE PER DWG 140N0504; INSTALLED REPAIR PART IAW B757 SRM 51-40-02, PG 1 PARA D.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,498 hrs · 19,914 cycles

PHX - EEL - DURING INSPECTION, THE EMERGENCY SEAT LIGHT WAS FOUND INOPERATIVE AT LEFT HAND ROW 7 . MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AT LEFT HAND SIDE ROW 7 AS REQUIRED. OPERATIONAL CHECK WAS GOOD.

Part: SELECTOR VALVE — FAILED (HYD SYSTEM) · airframe 51,716 hrs · 19,566 cycles

FLT 0035 - AFTER TAXI TO RUNWAY & SETTING THE PARKING BRAKES, BRAKE PRESSURE DROPPED TO 1150, RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE PARKING BRAKE ACCUMULATOR IAW BMM 32-44-05, AND HYDRAULIC ALTERNATE BRAKE SELECT VALVE IAW 32-41-04. OPERATIONAL AND LEAK CHECKS WERE GOOD. TEARDOWN OF HYD BRAKE SELECT VALVE, CONFIRMED FAILURE OF UNIT, PROBLEM WAS IDENTIFIED AS WORN O-RINGS AND SEALS. UNIT WAS OVERHAULED, TESTED, AND RETURNED TO SERVICE.

Part: CHARGER — DEFECTIVE (STA 1663) · corrosion level 0 · airframe 50,892 hrs · 19,206 cycles

LCQ - EEL - DURING C-11 CHECK EMERGENCY EXIT LIGHTS AND SLIDE LIGHTS AT THE L4/R4 DOOR INOP ALSO AFT SECTION OF EMERGENCY ESCAPE PATH SEAT MOUNTED LIGHTS WILL NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED THE AFT SEAT LIGHT BATTERIES AND BATTERY CHARGER ASSEMBLY, OPERATIONAL CHECK WAS GOOD IAW B757 MM 33-51-07, PG. 203-207.

Part: PAN — CORRODED (CABIN FLOOR) · airframe 50,892 hrs · 19,206 cycles

DURING C-11 CHECK CORROSION WAS FOUND ON CABIN FLOOR PAN AT BS 1681-1720, RBL 12. MAINTENANCE BLENDED OUT CORROSION, TREATED AREA, FABRICATED A REPAIR DOUBLER, AND INSTALLED REPAIR IAW B757-200 SRM 53-60-51, PG. 204.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,892 hrs · 19,206 cycles

DURING C-11 CHECK CORROSION WAS FOUND ON FLOORBEAM NUTPLATE HOLE AT BS 1340 RT, JUST INBOARD OF THE R-3 DOOR. MAINTENANCE REMOVED INBOARD CHORD RT FROM BS 1300 TO BS 1400, FABRICATED NEW REPAIR CHORD, AND INSTALLED REPAIR IAW B757-200 SRM 53-60-13.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 50,892 hrs · 19,206 cycles

LCQ - MAJOR REPAIR - DURING C-11 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT AT BS 1660 TO BS 1680, LBL 56. MAINTENANCE REMOVED DAMAGED FLOOR SUPPORT AT BS 1660 TO BS 1680, LBL 56. FABRICATED NEW FLOOR SUPPORT AND INSTALLED REPAIR IAW B757-200 SRM 51-40-02, PG. 11-12.

Part: SKIN — CHAFED · corrosion level 0 · airframe 50,892 hrs · 19,206 cycles

LCQ - MAJOR REPAIR - DURING C-11 CHECK THE FUSELAGE SKIN WAS FOUND CHAFED BELOW THE AFT END OF THE L/H HORIZONTAL STABILIZER BS 1865. MAINTENANCE REMOVED DAMAGED SKIN PANEL PER B737-300 SRM 51-40-02, PG. 16. FABRICATED A NEW SKIN PANEL, A FILLER, AND A DOUBLER, AND INSTALLED REPAIR PARTS IAW AWA ER 19-5381-02200-ES1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,892 hrs · 19,206 cycles

LCQ - MAJOR REPAIR - DURING C-11 CHECK CORROSION WAS FOUND ON CABIN FLOORBEAM AT BS 1640, LBL 25 TO LBL 35. MAINTENANCE REMOVED DAMAGED SECTION OF FLOORBEAM BS 1640, FABRICATED 2 EACH REPAIR ANGLES, 2 EACH STRAPS, AND A CHORD, AND INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-51, PG. 209-213.

Part: ATTACH ANGLE — CORRODED (GALLEY SUPPORT) · airframe 50,892 hrs · 19,206 cycles

DURING C-11 CHECK CORROSION WAS FOUND ON CABIN FLOOR ATTACH ANGLES (GALLEY SUPPORT) AT BS 1718, LB 0, RBL 10. MAINTENANCE REMOVED DAMAGED HAT SECTION, FABRICATED NEW HAT SECTION, AND INSTALLED REPAIR PARTS IAW DWG 146N5300, AND B757-200 SRM 51-40-02, PG. 1-6.

Part: PAN — CORRODED (CABIN FLOOR) · corrosion level 2 · airframe 50,892 hrs · 19,206 cycles

DURING C-11 CHECK CORROSION WAS FOUND ON CABIN FLOOR PAN AT BS 1718, RBL 14 TO RBL 40. MAINTENANCE REMOVED CORROSION, MATERIAL LOSS OUT OF LIMITS AT BS 1718, RBL 23. TREATED AND PRIMED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B757-200 SRM 53-60-51, PG. 204-208.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,892 hrs · 19,206 cycles

DURING C-11 CHECK EXFOILIATION CORROSION WAS FOUND ON THE LOWER SIDE OF FLOORBEAM UPPER CHORD BETWEEN THE BEAM AND NUTPLATE BRACKET, BS 1680, RBL 15 - 20. REMOVED DAMAGED SECTION OF FLOORBEAM UPPER CHORD, FABRICATED 2 EACH REPAIR ANGLES AND 2 EACH STRAPS, AND INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-51, FIG. 201, PG. 206-208.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 50,892 hrs · 19,206 cycles

DURING C-11 CHECK CORROSION WAS FOUND ON THE FORWARD CARGO COMPARTMENT RT LOADING JACK SCREW TRACK BS 691 TO BS 696, RBL 4. MAINTENANCE REMOVED DAMAGED SECTION OF FLOOR TRACK, FABRICATED A NEW SECTION OF TRACK AND 2 EACH REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-12, PG. 1.

Part: WIRE — BROKEN (SEAT 19 L/H) · airframe 50,010 hrs · 18,862 cycles

PHX - EEL - "C" - EMERGENCY EXIT LIGHT INOPERATIVE AT SEAT ROW 19 L/H. MAINTENANCE REPAIRED BROKEN WIRE ON SEAT 19 L/H, FUNCTIONAL CHECK GOOD.

Part: DOUBLER — DENTED (FUSELAGE)

DENT IN PREVIOUS REPAIR AT STA 619, 5 INCHES ABOVE STR 17L ON FUSELAGE EXTERIOR. REMOVED EXISTING REPAIR DOUBLER; FABBED AND INSTALLED REPAIR DOUBLER IAW AWA ER 19-5331-01104-SS1.

Part: FLOORBEAM — CORRODED (FUSELAGE)

FLOORBEAM AT BS 350 HAS CORROSION AND BARE METAL AROUND FLOORBOARD FASTENERS HOLES ON THE UPPER AND LOWER SURFACE OF THE TOP FLANGE FROM LBL 60 RBL 60. REMOVED EXISTENT SPLICE CHORD IAW SRM 51-40-02; FABBED EXISTENT SPLICE CHORD IAW SRM 53-00-51; INSTALLED SPLICE IAW SRM 51-40-02.

Part: ANGLE — CHAFED (CARGO DOOR)

AFT CARGO DOOR FWD EDGE ANGLE CHAFED AT LWR END APPROX 1.9 INCH LONG BY 0.3 INCH WIDE. REMOVED DAMAGED AREA; FABBED AND INSTALLED REPAIR PARTS IAW SRM 52-30-02 FIG 3 AND SRM 51-70-13 FIG 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

R-1 SERVICE DOOR FLOOR AREA STRUCTURE - CORROSION AROUND FASTENER HOLES FOR FLOORBOARDS ON CHORD ASSY, RBL 62 BS 339-363. REMOVED DAMAGED AREA; FABBED REPAIR ANGLE DOUBLER; INSTALLED REPAIR IAW SRM 53-00-51.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 47,004 hrs · 17,687 cycles

D: PHX - AIR TURNBACK - 3/26/01 - IN FLIGHT EICAS SPOILERS DISPLAYED WITH SPOILERS DOWN; AILERON DISPLACEMENT OBSERVED AS FLAPS RETRACTED AND THEN EXTENDED FOR LANDING; FLAPS 20 USED FOR LANDING. ON DEBRIEF OF FLIGHT CREW, REPORTED LEFT WING HEAVY. MAINTENANCE VISUALLY INSPECTED FLAPS AND SPOILERS - NO DEFECTS NOTED. TROUBLESHOT IAW FIM 27-09-00 FIG 105; SCM 3R FAULTS PCA FAULT; RESET THE FAULTBALL AND OPERATED THE SPOILERS AND FAULT DID NOT RETURN. AS A PRECAUTION MEL 27-61-1 CONDITION 1 WAS APPLIED AND SPOILERS 4 AND 9 DEACTIVATED IN THE DOWN POSITION.

Part: VALVE — FAILED (NR1 ENGINE) · airframe 46,552 hrs · 17,500 cycles

BWI - AIR TURNBACK - 2/10/01 - ON TAKEOFF THE NR 1 ENGINE HIGH STAGE LIGHT ILLUMINATED. DURING CLIMB THE AIRCRAFT WAS UNABLE TO MAINTAIN CABIN PRESSURIZATION IN AUTO AND THE CREW SWITCHED TO MANUAL AND CONTROL OF PRESSURIZATION WAS ESTABLISHED AT 10000 FT CABIN ALTITUDE. THE AIRCRAFT RETURNED TO BWI MAKING AN UNEVENTFUL OVERWEIGHT LANDING. MAINTENANCE REPLACED THE HIGH STAGE VALVE AND FOUND A FOREWARD CARGO COMPARTMENT NET STRAP CAUGHT IN THE DOOR. AN ENGINE RUN AND PRESSURIZATION TEST WAS PERFORMED; ALL CHECKS WERE GOOD. AN OVERWEIGHT LANDING INSPECTION WAS PERFORMED AND NO DISCREPANCIES NOTED.

Part: SWITCH — DEFECTIVE (LE FLAPS) · airframe 46,415 hrs · 17,450 cycles

LAS-AIR TURNBACK- DURING FLAP RETRACTION AFTER TAKEOFF, EICAS DISPLAYED LEADING EDGE SLAT DISAGREE MESSAGE AS FLAP HANDLE WAS MOVED TO THE FLAP UP POSITION. THE AIRCRAFT RETURNED TO LAS AND MADE AN UNEVENTFUL LANDING. IN LAS MAINTENANCE TROUBLESHOT AND REPLACED THE LT AND RT INBOARD LEADING EDGE SLAT LOSS SENSING SWITCHES. SYSTEM TESTED GOOD. SWITCH P/N''S (LT) 31EN101-6, (RT) 31EN102-6.

Part: WIRE — BROKEN (SEAT 17C) · airframe 46,028 hrs · 17,294 cycles

EMERGENCY PATHWAY LIGHT AT SEAT 17C INOP. SPLICED BROKEN WIRE AT SEAT 17C.

Part: CIRCUIT BOARD — MALFUNCTIONED (COCKPIT) · airframe 43,713 hrs · 16,291 cycles

STATUS MSG APU FIRE LOOP 1 AND APU FIRE LOOP 2 ALONG WITH MASTER WARNING FIRE LIGHTS AND FIRE DISCRETE LIGHT ILLUMINATED. REMOVED AND REPLACED APU LOGIC FIRE CARD, OPS CHECK GOOD. RECOMMENDATION: REMAIN OPEN PENDING REVIEW OF TEARDOWN REPORT M+E = 19-2610-9-0003.

Part: WIRE — BROKEN (SEAT 6) · airframe 43,702 hrs · 16,287 cycles

NON ROUTINE LINE, EMERGENCY LIGHT OUT AT SEAT 6C. REPLACED WIRING.

Part: ACTUATOR — FAILED (LE SLAT)

DURING APPROACH INTO MCO, HAD LEADING EDGE DISAGREE MESSAGE AND LIGHT. ACCOMPLISHED L/E SLAT DISAGREE, WHICH LED TO THE L/E SLAT ASYMMETRY CHECK LIST. EMERGENCY DECLARED, HAD NORMAL APPROACH AND LANDING. T/S, FOUND L/E ROTARY ACTUATORS 4, 9, 11, 12 HAD POPPED LIMITER PINS. RESET 9 & 11 ACTUATORS PER FIM 27-81-00. BITE TEST RESULTED IN REPLACING ROTARY ACTUATORS 1, 2, 3, 4, 12, 13, 14 &15 IAW MM 27-81-18, ADJUSTMENT AND TEST ALL OK. SLAT ROTARY ACTUATOR, (P/N 5006397R), (S/N 5211, 5235, 5202, 4776, 5130, 4830, 5227) OFF. SLAT ROTARY ACTUATOR, (P/N 5006398N), (S/N 0695) OFF. NO OTHER SLAT PROBLEMS SINCE ROTARY ACTUATOR REPLACEMENT.

Part: DOOR — OUT OF ADJUST (PAX DOOR)

AFT ENTRY DOOR EICAS MESSAGE DURING CLIMB. CABIN DOOR HANDLE COULD NOT BE LATCHED UNTIL A/C WAS DEPRESSURIZED PER QRH PROCEDURE WAS ACCOMPLISHED. ADJUSTED L4 PASSENGER DOOR IAW MM 52-11-00, OPS CK GOOD.

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: PIN — SHORTED (ROW 20)

IN MAINTENANCE, SEAT EMERGENCY EXIT LIGHTS FROM ROW 19L TO OVERWING EXITS INOP, OVERWING LOWER EXIT LIGHTS DIM. REPLACED BATTERY PACK AND POWER SUPPLY. ALSO, FOUND PIN SHORTED TO SEAT TRACK, REINSERTED PIN. EMERGENCY LIGHTS OPS CK GOOD.

Part: FLOORBEAM — CORRODED (BS 345)

DURING SCHEDULED C-8 INSPECTION, FOUND CORROSION ON TOP OF FLOORBEAM BS 345, BL 0, LBL 13. REMOVED, FABRICATED TOP CHORD OF FLOORBEAM FROM RBL 19 TO LBL 52, BS 345, WL 208 PER SRM 53-00-51.

Part: LIGHT — INOPERATIVE (CABIN)

SEAT EMERGENCY LIGHT AT 14C INOP. REPAIRED AND STOWED WIRING, OPS CHECKED NORMAL.

Part: LENS — MISSING (CABIN)

EMERGENCY LIGHT LENS COVER, ON OVERHEAD IN FIRST CLASS GALLEY, MISSING. PLACED ON OIL CONT NR 86900, PART NUMBER 844126.

Part: WIRE — DISCONNECTED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY PATH LIGHT AT ROW 29C INOP. RECONNECTED SEAT WIRE, OPS CHECK OK.

Part: WIRE — DISCONNECTED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT ROWS 22L AND 35L. RELAMPED ROW 22L. REPAIRED BROKEN WIRES AND RELAMPED AT 35L, OPS CHECK GOOD.

Part: WIRE — DISCONNECTED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 22 SEAT EMERGENCY LIGHT FAILED TO ILLUMINATE. RECONNECTED WIRE HARNESS AT SEAT 22. OPS CHECK GOOD.

Part: CONNECTORS — LOOSE (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS INOP AT SEAT ROW 16 AND 22. REPAIRED SEAT CONNECTORS, OPS CHECK GOOD.

Part: CONNECTOR — LOOSE (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 12 INOP. REPINNED CONNECTOR, OPS CHECK OK.

Part: WIRE — BROKEN (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS AT ROWS 8, 15 AND 33 INOP. REPAIRED WIRING.

Part: WIRE — BROKEN (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROX LIGHTS INOP ROW 13 TO 18. REPAIRED BROKEN WIRING, OPS CHECK GOOD.

Part: WIRE — DISCONNECTED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT AT ROW 29 INOPERATIVE. RECONNECTED EMERGENCY LIGHT AT ROW 19, OPERATIONS CHECK GOOD.

Part: POWER SUPPLY — FAILED (NR 2 RIGHT)

PHX - FLT 25 - AIRCRAFT ROLLED TO THE LEFT UPON SELECTING FLAPS 30 DEGREES (WENT DIRECTLY FROM 20 TO 30 DEGREES). APPROXIMATELY 4 DEGREES OF RIGHT AILERON WAS REQUIRED TO HOLD WINGS LEVEL. FLAPS 20 WAS SELECTED AND GROUND PROX FLAP OVERRIDE WAS SELECTED. ROLL DISAPPEARED AND A NORMAL LANDING WAS MADE. RESET SPOILER ACTUATOR RVDT NULL PER 27-61-00. REPLACED CSEU 2R FOR EICAS MESSAGE. SYSTEM OPS CHECK GOOD SPOILER NR 3 IS NOW NULLED IN LIMITS OK FOR SERVICE. (M)

Part: SOCKET — DISCONNECTED (CABIN)

PHX - FLT 2209 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT INOP AT ROW 24. RESEAT RECESSED SOCKET AT SEAT CONNECTOR. OPERATIONS CHECK GOOD. (M)

Part: CONNECTOR — LOOSE (CABIN)

PHX - FLT 2016 - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 5 EMERGENCY EXIT LIGHTS ON SEAT INOP PLACED ON MEL 33-51-03. REF MEL 33-51-01 RE-SEATED CONNECTOR PIN ON HARNESS AT ROW 5 EMERGENCY LIGHTS CHECK OK MEL REMOVED. (M)

Part: WIRE — DISCONNECTED (CABIN)

PHX - FLT 0020 - DURING ROUTINE MAINTENANCE CHECK, FOUND RT OVERHEAD EMERGENCY LIGHTS INOP AT R2 AND R3 DOORS. RESECURED CONNECTOR ON POWER SUPPLY AT 23 D, E, F, OVERHEAD. SYSTEM OPS CHECK NORMAL. STC SA3432NM. (X)

Part: PIN — PULLED (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 24-26 FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE. REINSTALLED PIN IN CONNECTOR AT ROW 26, OPS CHECK GOOD. (M)

Part: CRANK ASSY — BROKEN (NLG)

EWR-PHX - FLT NR 16 - DURING CLIMB, GEAR DOOR MESSAGE APPEARED ON EICAS. CREW CYCLED GEAR AND RESET CIRCUIT BREAKERS WITH NO HELP. AIRCRAFT RETURNED TO EWR LANDING UNEVENTFULLY. CMH MAINTENANCE TECHS FOUND NLG SEQUENCING VALVE LOWER CRANK ASSEMBLY BROKEN. MAINTENANCE REPLACED VALVE ASSEMBLY PER MM 32-34-06. OPS CHECK OK PER MM 32-34-00. OVERWEIGHT INSPECTION C/W PER AWM386. AIRCRAFT RETURNED TO SERVICE. (M)

Part: EEL FUSE — FAILED (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 20 THROUGH ROW 25. REPLACED PICO FUSE, OPS CHECK GOOD. (W)

Part: IDG ASSY — FAILED (NR 1 ENGINE)

PHX - FLT NR 11 - ON FLIGHT FROM JFK TO LAS, THE APU SHUTDOWN FOR LACK OF OIL. SINCE THE NR 1 ENG IDG WAS PLACARDED INOPERATIVE, THE PILOT ELECTED TO DIVERT AIRCRAFT TO PHX. MAINTENANCE REMOVED AND REPLACED THE NR 1 INTEGRATED DRIVE GENERATOR ASSY. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SUPPORT — CORRODED (BS 364)

PHX - DURING C6 INSPECTION, FOUND R1 DOOR THRESHOLD SUPPORT AND INTERCOSTAL CORRODED BEYOND LIMITS AT STATION 344. REPLACED DAMAGED PARTS PER SRM 51-10-00. REF 95ZZZW757.

Part: INTERCOSTAL — CORRODED (BS 364)

PHX - DURING C6 INSPECTION, FOUND R1 DOOR THRESHOLD SUPPORT AND INTERCOSTAL CORRODED BEYOND LIMITS AT STATION 344. REPLACED DAMAGED PARTS PER SRM 51-10-00. REFERENCE AWXA9500269.

Part: FLOORBEAM — CORRODED (BS 364)

PHX - DURING C6 INSPECTION, FOUND UPPER CAP OF FLOORBEAM AT STATION 364 RBL 23 AND RBL 60 CORRODED BEYOND CLEAN UPLIMITS. REPAIRED PER ER 5-53-12-03. (W)

Part: THRESHOLD — CRACKED (L4 DOOR)

PHX - DURING C6 INSPECTION, FOUND L4 DOOR FORWARD THRESHOLD PLATE CRACKED. REMOVED WELD REPAIR AND INSTALLED PER ER 5-53-30-02B. (W)

Part: ANGLE — CRACKED (BS 660)

PHX - DURING C6 INSPECTION, FOUND FLOOR BEAM TO INTERCOSTAL VERTICAL ANGLE CRACKED, BS 660. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 51-10-00 AND SRM 51-40-02. (W)

Part: EEL WIRE — LOOSE (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE, ROWS 25 THROUGH 27. REPINNED WIRE AT ROW 25, OPS CHECK GOOD. (Z)

Part: OIL COOLER — INOPERATIVE (NR 1 ENGINE)

PHX-JFK - FLT 294 - AIR TURNBACK DURING TAKEOFF, CABIN AND COCKPIT HAD A STRONG OIL SMELL WITH SMOKE IN CABIN. THE NR 1 ENGINE WAS REDUCED TO IDLE FOR LANDING. THE NR 1 ENGINE OIL TEMP ROSE TO 174 DEGREES FOR 5 TO 8 SECONDS. ON GROUND THE NR 1 ENGINE OIL PRESSURE WAS 26 PSI. A/C LANDED AND RETURNED TO GATE WITHOUT FURTHER PROBLEMS. MX TROUBLESHOT PER FIM 79-34-00, PG 105 BLK 1 AND 22. OIL QUANTITY WAS 21 QTS AND HAD SMELL OF FUEL. DRAINED OIL SYSTEM AND RESERVICED. REMOVED AND REPLACED NR 1 ENGINE FCOC PER BMM 79-21-01. RAN NR 1 ENGINE, LEAK CHECK GOOD PER MM 71-00-00. CHECKED CHIP DETECTOR AFTER ENGINE RUNS, NO METAL NOTED AT THIS TIME. A/C RETURNED TO SERVICE. (W)