N905AW

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 100,110 hrs · 35,003 cycles

WEEKLY VISIT 6 INCH CRACK ON INTERCOSTAL AT BS 1440, STRINGER 24R. REPLACED INTERCOSTAL IAW SRM 51-40-02 & DWG 146N8545.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 98,879 hrs · 34,748 cycles

C3 CHECK 2 INCH CRACK IN INTERCOSTAL CHORD ANGLE AT BS 1671, WL 208 & BL 0. REPLACED INTERCOSTAL CHORD ANGLE AT BS 1671, WL 208 & BL0 IAW SRM 51-10-02 & DWG 146N5180.

Part: STRAP — CRACKED (FUSELAGE) · airframe 98,879 hrs · 34,748 cycles

C3 CHECK, 1 INCH CRACK ON STABILIZATION STRAP AT BS 1380, RBL 45. REPAIRED STABILIZATION STRAP AT BS 1380, RBL 45 IAW SRM 53-00-51-2R-12.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 98,879 hrs · 34,748 cycles

C3 CHECK, LEVEL 2 CORROSION ON STRINGER BETWEEN BS 1408 TO S1420, S29R. REPAIRED STRINGER BETWEEN BS 1408 TO S1420, S29R IAW EA 105708.

Part: BEARING — FAILED (NLG WHEEL)

DURING LANDING ROLL OUT, CREW FELT A VIBRATION IN THE NOSE GEAR SIMILAR TO A FLAT TIRE. MAINTENANCE INSPECTED ACFT AND FOUND THE RT NLG WHEEL ASSY BEARING ON AXLE NUT SIDE OF THE WHEEL ASSY HAD FAILED. A TEMPORARY RT NLG WHEEL ASSY WAS INSTALLED. FURTHER INSPECTION FOUND AXLE GOUGED BEYOND LIMITS. NLG LOWER INNER CYLINDER AND SEALS, AND THE NLG RIGHT AXLE NUT, ALONG WITH THE TEMPORARY RIGHT NLG WHEEL ASSY AND THE LT NLG WHEEL ASSY WERE REPLACED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 96,696 hrs · 34,289 cycles

EMER LIGHT IN FWD DOOR SURROUND LIGHT L7 AND R4 INOP. R & R AFT LT POWER SUPPLY M736.

Part: FUSE — BLOWN (CABIN)

PHX - LOWER EXIT SIGN AT 1L AND R1 DOOR INOP. REMOVED AND REPLACED BAD FUSE ON POWER SUPPLY/BATTERY PACK FOR LOWER EMERGENCY SIGNS 1L 1R.

Part: PANEL — DELAMINATED (VERTICAL STAB) · airframe 94,715 hrs · 33,893 cycles

C2 CHECK - AREA OF DELAMINATION ON LEFT VERTICAL STABILIZER FORWARD TORQUE BOX PANEL AT FSS 220. REPLACED LEFT VERTICAL STABILIZER FORWARD TORQUE BOX PANEL AT FSS 220 IAW B757 SRM 55-30-01 & 51-70-10.

Part: SKIN PANEL — DELAMINATED (HORIZ STAB) · airframe 94,715 hrs · 33,893 cycles

C2 CHECK - DELAMINATION ON RIGHT STABILIZER TORQUE BOX, UPPER SKIN PANEL, INNER SKIN AT STAB STA 130 APPROX 10 INCHES AFT OF AUXILLARY SPAR. REPAIRED RIGHT STABILIZER TORQUE BOX, UPPER SKIN PANEL IAW B737 SRM 51-40-03 & EA 502286.

Part: WEB — CRACKED (FUSELAGE) · airframe 94,715 hrs · 33,893 cycles

C2 CHECK - CRACK AT L2 DOOR CUTOUT WEB PANEL AT BS 686 APPROX 1 INCH ABOVE S13L. REPAIRED L2 DOOR CUTOUT WEB PANEL AT BS 686 APPROX 1 INCH ABOVE S13L IAW # 104310.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 94,099 hrs · 33,762 cycles

PHX - FWD F/A FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY. OPS CHECK GOOD.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 9,390 hrs · 33,722 cycles

WEEKLY CHECK - DELAMINATION ON NR 7 SLAT ON UPPER SURFACE AT INBOARD END AT WS 397. REPLACED NR 7 SLAT IAW JOB CARD 19L52027002.

Part: BEARING — WORN (AILERON) · airframe 93,616 hrs · 33,670 cycles

PHX FLT 47 EN ROUTE LIH TO PHX. AILERONS STIFF- DO NOT RETURN TO CENTER. REMOVED AND REPLACED CENTERING BEARING ON LATERAL CONTROL FEEL AND TRIM MECHANISM ASSY. OP'S CHECKS GOOD. RIGGING NOT DISTURBED.

Part: OVEN — INOPERATIVE (GALLEY) · airframe 91,617 hrs · 33,249 cycles

OGG FLT 432 EN ROUTE PHX TO OGG. BOTH OVENS AT G1B FIRST CLASS GALLEY INOP. INTERMITTENT ON AND OFF WITH ACRID ELECTRICAL ODOR. REPLACED BOTH FWD GALLEY OVENS.

Part: HUB — LOOSE (L4 DOOR)

PHX - THE L-4 DOOR INTERIOR OPEN/CLOSE HANDLE IS LOOSE. REMOVED AND REPLACED HANDLE HUB.

Part: LANYARD — OUT OF POSITION (EVAC SLIDE) · airframe 91,228 hrs · 33,173 cycles

PHX - DOOR 1R VERY DIFFICULT TO ARM AND DOES NOT APPEAR NORMAL WHEN FORCED TO ARM. REF PRIOR ENTRY LOG PAGE 7583660. MAINTENANCE FOUND LANYARD FROM SLIDE IMPEDING GIRT BAR. STOWED LANYARD INTO SLIDE, VERIFIED GIRT BAR ENGAGES BRACKETS FULLY, OP NORMAL.

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 91,228 hrs · 33,173 cycles

PHX - SMOKE DET INOP LAV MID RT. MAINTENANCE REMOVED AND REPLACED RT MID LAV SMOKE DETECTOR TR26-005AW, NO FAULTS NOTED ON GROUND AT THIS TIME.

Part: PIN — BACKED OUT (EMERGENCY LIGHT) · airframe 39,318 hrs · 15,774 cycles

MCN - C1 - EEL - LOWER LEFT EMERGENCY LIGHT NEXT TO L-3 DOOR SAYING "EXIT" IS INOP. RESEATED PUSHED BACK PIN ON LOWER LEFT EMERGENCY LIGHT NEXT TO L-3 DOOR SAYING "EXIT" AS REQUIRED. OPS CHECK GOOD.

Part: BATTERY — WEAK (FLASHLIGHT) · airframe 89,890 hrs · 32,927 cycles

MCN - C1 - EEL - L-2 DOOR FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY IS WEAK. REPLACED L-2 DOOR FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY AS NEEDED. OPS CHECK GOOD.

Part: FITTING — CRACKED (FUSELAGE) · airframe 89,890 hrs · 32,927 cycles

MCN - C1 - MAJOR REPAIR - CRACK ON CLIP AT BS 865, BL 0. REPLACED CLIP AT BS 865, BL 0 IAW B757 SRM 51-40-02.

Part: PANEL — CRACKED (LE SLAT) · airframe 39,318 hrs · 15,774 cycles

MCN - C1 - MAJOR REPAIR - CRACK ON LEFT WING NR 2 SLAT COVE PANEL AT WS 580. REPLACED LEFT WING NR 2 SLAT COVE PANEL AT WS 580 IAW B757 SRM 51-40-02.

Part: RESERVOIR — LOW PRESSURE (L2 DOOR)

THE L2 DOOR EMERGENCY POWER RESERVOIR HAS LOW PRESSURE. REMOVED AND REPLACED THE L2 DOOR EMERGENCY POWER RESERVOIR. ASSEMBLY WAS REPLACED WITH AN EQUIVALENT ASSEMBLY.

Part: LIGHT — INOPERATIVE (COCKPIT)

LAX - EN ROUTE FROM PHX TO LAX, CREW REPORTED THE FIRST OFFICER'S VOR/DME SWITCH WAS INOPERATIVE. WHEN SWITCH WAS PUSHED, A POP WAS HEARD AND A SMELL OF FUMES WAS NOTED. MAINTENANCE FOUND DEFECTIVE LAMP IN SWITCH BUTTON. REPLACED LAMP. TEST/OPS CHECK GOOD. REF TASK 34-51-02-032-001.

Part: LIGHT — INOPERATIVE (CABIN)

PHX - RED AISLE EMERGENCY EXIT LIGHT WAS INOPERATIVE AND MISSING AT SEAT 10C. REMOVED AND REPLACED RED AISLE EMERGENCY EXIT LIGHT ASSEMBLY.

Part: SOCKET — INOPERATIVE (CABIN)

PHX - THE 16ABC SEAT MOUNT EMERGENCY LIGHT INOP. MAINTENANCE REPLACED SOCKET ASSEMBLY.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,763 hrs · 32,098 cycles

BFM - C4 - MAJOR REPAIR - LEVEL 2 CORROSION ON LOWER SILL & CHORD BETWEEN BS 1380 TO BS 1440, WL 145, RBL 20. REPLACED LOWER SILL & CHORD BETWEEN BS 1380 TO BS 1440, WL 145, RBL 20 IAW B757 SRM 51-40-02 & 51-20-01.

Part: SLAT — CORRODED (RT WING) · airframe 85,763 hrs · 32,098 cycles

BFM - C4 - MAJOR REPAIR - CORROSION AROUND FASTENERS ON NR 8 SLAT AT WS 509.50. REPLACED NR 8 SLAT AT WS 509.50 IAW B757 AMM 27-81-02.

Part: SKIN — CORRODED (FUSELAGE) · airframe 85,763 hrs · 32,098 cycles

BFM - C4 - MAJOR REPAIR - CORROSION ON FUSELAGE SKIN AT BS 1554 BETWEEN S29L TO S30L. REPAIRED FUSELAGE SKIN AT BS 1554 BETWEEN S29L TO S30L IAW EA 134169.

Part: SKIN — CORRODED (FUSELAGE) · airframe 85,763 hrs · 32,098 cycles

BFM - C4 - MAJOR REPAIR - CORROSION ON FUSELAGE SKIN AT BS 1525 BETWEEN S29L TO S30L. REPAIRED FUSELAGE SKIN AT BS 1525 BETWEEN S29L TO S30L IAW EA 134168.

Part: DOUBLER — CRACKED (NR 2 PYLON) · airframe 85,763 hrs · 32,098 cycles

BFM - MAJOR REPAIR - C4 CHECK - CRACKED PYLON SKIN REPAIR DOUBLER ON NR 2 PYLON. REPLACED PYLON SKIN REPAIR DOUBLER ON NR 2 PYLON IAW EA 134171.

Part: SKIN — CORRODED (FUSELAGE) · airframe 85,763 hrs · 32,098 cycles

BFM - MAJOR REPAIR - C4 CHECK - CORROSION ON FUSELAGE SKIN AT BS 1480 - BS 1500, S29R - S30, BL 0. REPAIRED FUSELAGE SKIN AT BS 1480 - BS 1500, S29R - S30, BL 0 IAW EA 134.

Part: PLATE — CORRODED (FUSELAGE) · airframe 85,763 hrs · 32,098 cycles

BFM - MAJOR REPAIR - C4 CHECK - CORROSION ON AFT GALLEY FLOOR DECK PLATE AT BS 1715, LBL 6 - RBL 47, WL 208.1. REPAIRED AFT GALLEY FLOOR DECK PLATE AT BS 1715, LBL 6 - RBL 47, WL 208.1 IAW B757 SRM 53-60-51, 51-21-01 AND 53-00-51.

Part: PLATE — CORRODED (FUSELAGE) · airframe 857,632 hrs · 32,098 cycles

BFM - MAJOR REPAIR - C4 CHECK - CORROSION ON AFT GALLEY FLOOR DECK PLATE, BS 1687 - BS 1715 RBL 50, WL 208.1. REPAIRED AFT GALLEY FLOOR DECK PLATE, BS 1687 - BS 1715 RBL 50, WL 208.1 IAW B757 SRM 53-60-01 AND 51-40-02.

Part: PLATE — CORRODED (FUSELAGE) · airframe 857,632 hrs · 32,098 cycles

BFM - MAJOR REPAIR - C4 CHECK - CORROSION ON AFT GALLEY FLOOR DECK PLATE AT BS 1681, RBL 50, WL 208.1. REPAIRED AFT GALLEY FLOOR DECK PLATE AT BS 1681, RBL 50, WL 208.1 IAW B757 SRM 53-60-01 AND 51-40-02.

Part: SKIN — DELAMINATED (SPOILER) · airframe 85,763 hrs · 32,098 cycles

BFM - C4 - MAJOR REPAIR - NR 4 SPOILER DISBONDED BETWEEN ACTIVATOR & INBOARD HINGE. REPAIRED NR 4 SPOILER SKIN IAW B757 SRM 57-50-01 & 51-70-04.

Part: FUSE — BLOWN (CABIN)

PHX - EMERGENCY LIGHTS FROM ROW 19 THROUGH AFT GALLEY WERE INOPERATIVE. REPLACED FUSES EXT AFT EMERGENCY LIGHT BATTERY PACK.

Part: ACTUATOR — DEFECTIVE (GIRT BAR)

PHX - THE SLIDE ARMED LIGHT OVER DOOR L4 DOES NOT ILLUMINATE. REPLACED FORWARD GIRT ACTUATOR.

Part: LANYARD — UNSECURE (EVAC SLIDE)

PHX - THE LANYARD FOR SLIDE AT DOOR R1 NEEDS TO BE PROPERLY STOWED. THE LANYARD ON SLIDE AT DOOR R1 WAS STOWED.

Part: LIGHT — INOPERATIVE (CABIN)

PHX - THE L1 DOOR EXIT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE RELAMPED THE L1 DOOR EXIT EMERGENCY LIGHT. OPERATIONALLY CHECKS GOOD.

Part: PROXIMITY SENSOR — FAULTY (R4 DOOR)

PHX - THE ARMING INDICATOR LIGHT AT DOOR 4R WAS FOUND INOPERATIVE. MAINTENANCE REPLACED PROXIMITY SENSOR (S10224) ON DOOR 4R. OPERATIONALLY CHECKS OK.

Part: GCU — LOOSE (NR 1)

PHX - FLT 45 PHX TO KOA. UPON ROTATION, THE LEFT AC BUS TRIPPED OFF AND COULD NOT BE RESET, OR POWERED BY ANOTHER GENERATOR. THE FLIGHT RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE BITE CHECKED THE BUS PROTECTION CONTROL UNIT (BPCU) AND FOUND "NO RESPONSE FROM CONTROL" MESSAGE. THE NUMBER ONE GENERATOR CONTROL UNIT (GCU) WAS INSPECTED AND FOUND LOOSE IN ITS RACK. THE NUMBER ONE GCU WAS REPLACED. OPERATIONAL CHECKS WERE FOUND OK.

Part: CIRCUIT BREAKER — FAILED (ELECTRICAL SYS)

FLT 119- IN CRUISE, LT AC BUSS FAILED. GENERATOR RESET DID NOT CORRECT CONDITION. ATTEMPTS TO POWER LT AC BUSS FROM OTHER POWER SOURCES NOT SUCCESSFUL. FLT DIVERTED & LANDED WITHOUT INCIDENT. REPLACED GROUND POWER CONTACTOR, CURRENT XFORMERS, & BUSS TIE C/B, NO EFFECT. PERFORMED FIM PROCEDURE 24-22-00. NO FAULTS FOUND. FOUND A SUSPECTED SHORTED AFT GALLEY FEEDER WIRE. WIRES DISCONNECTED, ISOLATION STILL OCCURRED. PROBLEM ISOLATED TO LT XFER BUSS & CAPTAIN'S CDU. WITH CDU REMOVED, OPS OK. DETERMINED CAPTAIN'S CDU C/B HAD MALFUNCTIONED. REPLACEMENT FIXED THE CONDITION. WIRE CHECKED OK & REINSTALLED. COFFEEMAKERS & GALLEY POWER LOAD CONTROL UNIT REPLACED.

Part: CIRCUIT BREAKER — MALFUNCTIONED (CDU)

FLT 119 IN CRUISE, EICAS MESSAGES "L GEN OFF" AND "L AC BUS OFF". DISPLAYED WITH THE CORRESPONDING "L GEN OFF" AND "L BUS OFF" LIGHTS ILLUMINATED. A GENERATOR RESET DID NOT CORRECT THE CONDITION. ATTEMPTS TO POWER THE L AC BUSS FROM THE OTHER POWER SOURCES WERE NOT SUCCESSFUL. FLT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MX REPLACED GROUND POWER EXTERNAL CONTACTOR K114, CURRENT TRANSFORMERS T112 & T127, AND BUSS TIE BREAKER C902, WITH NO EFFECT. ALSO, PERFORMED FIM 24-22-00. NO FAULTS FOUND. MX FOUND WHAT WAS BELIEVED TO BE A SHORTED AFT GALLEY FEEDER WIRE, W3538-0005. WIRE STOWED IN PREPARATION FOR A FERRY FLT WITH THE WIRES DISCONNECTED, THE AC BUSS ISOLATION STILL OCCURRED. PROBLEM ISOLATED TO THE LT TRANSFER BUSS & CAPTAIN'S CDU. WHEN CDU REMOVED, LT AC BUSS OPERATED OK. DETERMINED THE CAPTAIN'S CDU CIRCUIT BREAKER MALFUNCTIONED. REPLACEMENT OF CDU & CIRCUIT BREAKER FIXED LT AC BUSS TIE. ACFT MX FERRIED WHERE WIRE W3538-0005 CHECKED OK & REINSTALLED, AND THE AFT GALLEY COFFEEMAKERS & AFT GALLEY POWER ELECTRICAL LOAD CONTROL UNIT REPLACED.

Part: ANGLE — CRACKED (FUSELAGE) · corrosion level 3

C12/ NR 6109923 - INTERCOSTAL UPPER ANGLE CRACKED BS 440 TO 460, WL 208.1, BL0 (HFEC VERIFIED). REPLACED INTERCOSTAL UPPER ANGLE CRACKED BS 440 TO 460, WL 208.1, BL 0 IAW SRM 51-40-02-0G. (K)

Part: STRUCTURE — CORRODED (FUSELAGE)

MCN - C12 - MAJOR REPAIR - NR 6061159 - R2 DOOR CUTOUT HAS CORROSION ON INNER STRUCTURE AT BS 686 TO 729.6, WL 208.1. REPLACED R2 DOOR CUTOUT INNER STRUCTURE AT BS 686 TO 729.6, WL 208.1 IAW SRM 51-40-02-0G. (K)

Part: FLOORBEAM — CRACKED (FUSELAGE)

MCN - C12 - MAJOR REPAIR - NR 6111603 - FLOORBEAM CRACKED UPPER T-CAP AFT RADIOS B/S 700 RBL 45 W/L 208.1. REPAIRED FLOORBEAM UPPER T-CAP AFT B/S 700 RBL 45 W/L 208.1 IAW B757 SRM 53-00-51-2R1. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

MCN - C112 - MAJOR REPAIR - NR 6109932 - INTERCOSTAL WEB CRACKED B/S 550 RBL 54 W/L 208.1 (HFEC VERIFIED). REPLACED INTERCOSTAL WEB B/S 550 RBL 54 W/L 208.1 IAW SRM 51-40-02-0G. (K)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,602 hrs · 31,118 cycles

CMN - C12 - MAJOR REPAIR - LEVEL 2 CORROSION AT INTERCOSTAL OUTER CHORD 4"X1" AREA AT BS 900 WL 133 BL 0. REPAIRED LEVEL 2 CORROSION AT INTERCOSTAL OUTER CHORD 4"X1" AREA AT BS 900 WL 133 BL 0 IAW B757-200 SRM 51-70-12-0G. (S)

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 80,602 hrs · 31,118 cycles

MCN - C12 - MAJOR REPAIR - LEVEL 2 CORROSION ON CHANNEL SUPPORT AT BS 1200 - 1220, WL 133, BL 10R. REPLACED CHANNEL SUPPORT AT BS 1200 - 1220, WL 133, BL 10R IAW B757-200 SRM 51-40-02-0G. (S)

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 81,602 hrs · 31,118 cycles

MCN - C12 - MAJOR REPAIR - NR 6109942 - INTERCOSTAL UPPER CLIP CRACKED B/S 860 TO 879 B/L 208.1 (HFEC VERIFIED). REPLACED INTERCOSTAL UPPER CLIP B/S 860 TO 879 B/L 208. IAW SRM 51-40-02-0G. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

NR 6109926, INTERCOSTAL UPPER ANGLE CRACKED B/S 480 TO 500 RBL 10 W/L 208.1. REPLACED INTERCOSTAL UPPER ANGLE B/S 480 TO 500 RBL 10 W/L 208.1 IAW SRM 51-40-02-0G. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

MCN - C12 - MAJOR REPAIR - NR 6109924 - INTERCOSTAL UPPER ANGLE CRACKED B/S 540 TO 560 B/LO W/L 208.1. (HFEC VERIFIED). REMOVED AND REPLACED INTERCOSTAL UPPER ANGLE B/S 540 TO 560 B/LO W/L 208.1 IAW SRM 51-40-02-0G. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

MCN - C12 - MAJOR REPAIR - NR 6109944 - INTERCOSTAL UPPER ANGLE CRACKED B/S 660 TO 680, W/L 208.1, BL 0 (HFEC VERIFIED). REPLACED INTERCOSTAL UPPER ANGLE B/S 660 TO 680, W/L 208.1, BL 0 IAW SRM 51-40-02-0G. (K)

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,602 hrs · 31,118 cycles

NR 6110496 - LEVEL 2 CORROSION ON CREASE BEAM CHORD AT BS 443, WL 208, BL 64L. REMOVED AND REPLACED CREASE BAM CHORD AT BS 443, LW 208, BL 64I, IAW SRM 51-40-02-0G. (K)

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 3

NR 6109913 - LEVEL 2 CORROSION ON CREASE BEAM INNER CHORD AT BS 734, WL 208, BL64L. REPLACED CREASE BEAM INNER CHORD AT BS 734, WL208, BL 64L IAW SRM 51-40-02-0G. (K)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 81,602 hrs · 31,118 cycles

MCN-C12-MAJOR REPAIR - NR 6109932 - INTERCOSTAL WEB CRACKED B/S 480 LBL 38 W/L 201.1 (HFEC VERIFIED). REPAIRED INTERCOSTAL WEB B/S 480 LBL 38 W/L 201.1 IAW SRM 51-40-02-0G. (K)

Part: SKIN — DEBONDED (T/E FLAP)

MCN - C12 - MAJOR REPAIR - NR 6108532 - I/B TRAILING EDGE DISBONDED, RIGHT WING I/B AFT FLAP. REPAIRED I/B TRAILING EDGE RIGHT WING I/B AFT FLAP DISBONDED IAW SRM 51-70-04-0G. (K)

Part: ANGLE — CRACKED (FUSELAGE)

MCN - C12 - MAJOR REPAIR - NR 6108587 - L-ANGLE CLIP CRACKED B/S 350 S6L JUST ABOVE L-1 DOOR SURROUND (HFEC VERIFIED). REPAIRED L-ANGLE CLIP B/S 350 S6L JUST ABOVE L-1 DOOR SURROUND IAW SRM 51-40-02-0G. (K)

Part: LIGHT — BURNED OUT (CABIN)

PHX FLT 332 - EN ROUTE PHX TO SJD. THE CABIN CREW REPORTED AN ELECTRICAL SMOKE ODOR IN THE REAR CABIN OF THE AIRCRAFT. THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC, AND REQUESTED THE CABIN CREW TO TURN OFF THE IN-FLIGHT ENTERTAINMENT EQUIPMENT. WITH THE EQUIPMENT TURNED OFF, THE ODOR DISSIPATED WHILE THE FLIGHT RETURNED TO PHX, LANDING WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE IN-FLIGHT ENTERTAINMENT SYSTEM, AIR CONDITIONING SYSTEM, THE AFT GALLEY AND LAVATORIES, CABIN LIGHTING SYSTEMS, AND THE AFT CARGO BAY FOR ELECTRICAL ODORS AND OVERHEAT CONDITIONS. NO ODORS WERE DETECTED, HOWEVER, THE CEILING LIGHTS BY ROW 30 WERE REPLACED. AIRCRAFT OK FOR SERVICE.

Part: ACTUATOR — INOPERATIVE (RUDDER)

PHX FLT 25 PHX TO HNL - THE RUDDER TRIM FAILED. DECISION WAS MADE TO RETURN TO FIELD PHX, AND LAND WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RUDDER TRIM ACTUATOR. OK FOR SERVICE.

Part: ROTARY ACTUATOR — BINDING (L/E SLAT)

HNL - FLT20 - DURING APPROACH TO HNL FROM PHX, CREW RECEIVED A "LE SLAT DISAGREE" LIGHT AT FIRST SELECTION OF FLAPS FOR ARRIVAL. CREW ACCOMPLISHED QRH AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED FIM 27-81-00 THRU ITEM 1B. SYSTEM CHECKED OK. NO FAULTS OR MESSAGES. ADDITIONAL FOLLOW-UP REVEALED 5 SLAT ROTARY ACTUATORS WITH TRIPPED TORQUE LIMITER INDICATORS AT POSITIONS 4, 8, 9, 11 AND 20. MAINTENANCE REMOVED AND REPLACED POSITIONS 4, 8, 9, 11 AND 20 SLAT ROTARY ACTUATORS. OPERATIONAL CHECK GOOD.

Part: ROTARY ACTUATOR — MALFUNCTIONED (L/E SLAT)

PHX FLT 432 EN ROUTE CLT TO PHX. DURING APPROACH, CREW RECEIVED "LE FLAP DISAGREE" MESSAGE ON EICAS, WHEN FLAPS WERE POSITIONED TO ONE. THE FLIGHT DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NUMBER 2 SLAT ROTARY ACTUATOR. OPS CHECKED OK.

Part: COMPUTER — MALFUNCTIONED (EICAS)

HNL FLT 125 HNL-PHX LEFT EICAS PROBLEM, FLIGHT CREW DECISION TO RETURN-TO-FIELD. MAINTENANCE REPLACED LEFT EICAS COMPUTER & LOADED SOFTWARE.

Part: CIRCUIT BOARD — FAILED (COOLING SYSTEM) · airframe 78,583 hrs · 30,370 cycles

PHX - OTHER - LOG NR 7809150 - CREW REPORTED EQUIPMENT SMOKE TEST STATUS MESSAGE ILLUMINATED. MX REPLACED THE EQUIPMENT COOLING CARD M10650 IAW MM 21-58-20-4. OPERATIONAL CHECK WAS GOOD.

Part: SLIDE — NO TEST (L4 DOOR) · airframe 77,480 hrs · 30,072 cycles

PHX - EES - L-4 DOOR SLIDE DEPLOYMENT FAILED DUE TO THE SLIDE COVER. MX REPOSITIONED THE SLIDE COVER, DEPLOYMENT WAS NORMAL.

Part: POWER SUPPLY — DISCHARGED (FLASHLIGHT) · airframe 76,503 hrs · 29,807 cycles

MCN - EEL - AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT POWER SUPPLY.

Part: STRINGER — CRACKED (ZONE 200) · airframe 76,503 hrs · 29,807 cycles

MCN - STRINGER 15L CRACKED, BS 630 AND BS 635. REPAIRED STRINGER 15L, BS 630 AND BS 635 IAW B757-200 SRM 53-00-03 FIGURE 201.

Part: STRINGER CLIP — CRACKED (BS 620 S15L) · airframe 76,503 hrs · 29,807 cycles

MCN - STRINGER CLIP CRACKED, BS 620, S15L. REPLACED STRINGER CLIP, B/S 620, S15L IAW B757-200 SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (BS 620 S16L) · airframe 76,503 hrs · 29,807 cycles

MCN - STRINGER CLIP CRACKED, BS 620, S16L. REPLACED STRINGER CLIP, BS 620, S16L IAW B757-200 SRM 51-40-02.

Part: SILL — CORRODED (BS 1320-1350) · airframe 76,503 hrs · 29,807 cycles

MCN - CORROSION L-3 DOOR SILL WEB TOP AND BOTTOM, BS 1320 - BS 1350, LBL 65, WL 208. REPLACED L-3 DOOR SILL WEB , BS 1320 - BS 1350, LBL 65, WL 208 IAW BOEING 757-200 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 1681) · airframe 76,503 hrs · 29,807 cycles

MCN - CORROSION ON MAIN CABIN FLOORBEAM UPPER FLANGE LOWER SURFACE, B/S 1681.8, RBL 32 - RBL 40, WL 208.1. REPAIRED MAIN CABIN FLOORBEAM UPPER FLANGE LOWER SURFACE, B/S 1681.8, RBL 32 - RBL 40, WL 208.1 IAW B757-200 SRM 53-00-51 FIGURE 201.

Part: STRUCTURE — CORRODED (L3 DOOR) · airframe 76,503 hrs · 29,807 cycles

MCN - CORROSION ON THE L3 DOOR INNER CHORD, BS 1320 - BS 1360, LBL 65, WL 208. REPLACED L3 DOOR INNER CHORD, BS 1320 - BS 1360, LBL 65, WL 208 IAW BOEING 757-200 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 1660) · airframe 76,503 hrs · 29,807 cycles

MCN - CORROSION ON MAIN CABIN FLOORBEAM, BS 1660, BL 0 - RBL 51, WL 208. REPAIRED MAIN CABIN FLOORBEAM, BS 1660, BL 0 - RBL 51, WL 208 IAW B757-200 SRM 53-00-51 FIGURE 201.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 76,503 hrs · 29,807 cycles

MCN - CORROSION ON MAIN CABIN FLOORBEAM, BS 1640, LBL 11 - RBL 66, WL 208. REPAIRED MAIN CABIN FLOORBEAM, BS 1640, LBL 11 - RBL 66, WL 208 IAW AWA ER 19-5310-06335-ES2.

Part: INTERCOSTAL — CRACKED (BS 1620-1640) · airframe 76,503 hrs · 29,807 cycles

MCN - MAIN CABIN FLO0R INTERCOSTAL SUPPORT WEB CRACKED, BS 1620 - BS 1640, BL 0, WL 208. REPLACED MAIN CABIN FLO0R INTERCOSTAL SUPPORT WEB, BS 1620 - BS 1640, BL 0, WL 208 IAW B757-200 SRM 51-40-02.

Part: SKIN — CRACKED (ZONE 500) · airframe 760,503 hrs · 29,807 cycles

MCN - LEFT WING NR 2 SLAT LOWER AFT COVE SKIN CRACKED, SS 574.8 - SS 605.3 AT MAIN TRACK ATTACHMENT LOCATION. REPLACED LEFT WING NR 2 SLAT LOWER AFT COVE SKIN, SS 574.8 - SS 605.3 IAW B757-200 SRM 51-40-02.

Part: SKIN — CRACKED (NR 8 SLAT) · airframe 76,503 hrs · 29,807 cycles

MCN - RIGHT WING NR 8 SLAT COVE SKIN CRACKED, WS 537.50. REPAIRED RIGHT WING NR 8 SLAT COVE SKIN, WS 537.50 IAW B757-200 SRM 51-70-13 FIGURE 1.

Part: SKIN — CRACKED (ZONE 500) · airframe 76,503 hrs · 29,807 cycles

MCN - LEFT WING NR 2 SLAT LOWER AFT COVE SKIN CRACKED, SS 677.5 - SS 705.5 AT OUTBOARD MAIN TRACK ATTACHMENT LOCATION. REPLACED LEFT WING NR 2 SLAT LOWER AFT COVE SKIN, SS 677.5 - SS 705.5 IAW B757-200 SRM 51-40-02.

Part: SKIN — CRACKED (NR 3 SLAT) · airframe 76,503 hrs · 29,807 cycles

MCN - LEFT WING NR 3 SLAT COVE SKIN CRACKED, WS 459. REPLACED LEFT WING NR 3 SLAT COVE SKIN, WS 459 IAW B757-200 SRM 51-40-02 AND BOEING DRAWING 114N4077.

Part: SKIN — CRACKED (NR 8 SLAT) · airframe 765,032 hrs · 29,807 cycles

MCN - RIGHT WING NR 8 SLAT COVE SKIN CRACKED, WS 537.50. REPAIRED RIGHT WING NR 8 SLAT COVE SKIN, WS 537.50 IAW B757-200 SRM 51-70-13 FIGURE 1.

Part: STRINGER — CORRODED (BS 1462-1468) · airframe 76,503 hrs · 29,807 cycles

MCN - CORROSION ON STRINGER 28L, BS 1462 - BS 1468. REPAIRED STRINGER 28L, BS 1462 - BS 1468 IAW AWA ER 19-5300-06336-SS2 .

Part: SKIN — CORRODED (BS 1463 S28L) · airframe 76,503 hrs · 29,807 cycles

MCN - CORROSION BULGE ON FUSELAGE EXTERIOR SKIN, BS 1463, S28L. REPAIRED CORROSION BULGE ON FUSELAGE EXTERIOR SKIN, BS 1463, S28L REPAIRED IAW AWA ER 19-5300-06336-SS2.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 76,179 hrs · 29,711 cycles

PHX - EEL - DURING MAINTENANCE IT WAS DISCOVERED AISLE EMERGENCY LIGHTS WERE INOP AT ROW 10 LT SIDE. MAINTENANCE DISCOVERED THAT A WIRE WAS DISCONNECTED. MAINTENANCE RE-CONNECTED THE WIRE, OP CHECKS GOOD.

Part: OVEN — SMOKE (AFT GALLEY) · airframe 75,109 hrs · 29,470 cycles

SNA - SMOKE - FLT 652 - DURING CRUISE REPORTED THE NR 1 AFT OVEN WAS SMOKING, REPORTEDLY DUE TO CRUMBS INSIDE OVEN. FLIGHT ATTENDANT DISCHARGED HALON FIRE EXTINGUISHER, PULLED AND COLLARED CIRCUIT BREAKER. NR 1 AFT OVEN WAS PLACED ON MEL. PHX - MAINTENANCE REMOVED AND REPLACED THE NR 1 AFT OVEN.

Part: PTU — LEAKING (HYDRAULIC SYS) · airframe 75,036 hrs · 29,452 cycles

PHX - EMERGENCY LANDING - FLT 944 - DURING APPROACH CREW REPORTED LOSING LT HYD QUANTITY AND INDICATION SHOWING 18RF. CREW DECLARED EMERGENCY INTO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND THE PTU PRESSURE SWITCH LEAKING. REMOVED AND REPLACED THE PTU PRESSURE SWITCH IAW BOEING 757-200 MM 29-11-17-4. RAN NR 1 ENGINE, NO LEAKS WERE NOTED.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 74,059 hrs · 29,238 cycles

REPORTED LOSING THE LT HYDRAULIC QUANTITY AND PRESSURE DURING CLIMB. ALSO RECEIVED -L HYD ELECT PUMP- EICAS MSG DISPLAYED AND -L ELECTRIC HYD PUMP-, -LOW PRESSURE- LIGHT ILLUMINATED OVERHEAD. CREW RETURNED TO PHX AND LANDED WITH EMERGENCY EQUIPMENT STANDING BY. LANDING UNEVENTFUL AND AIRCRAFT WAS TOWED TO GATE. MX R & R LT ELECTRICAL PUMP. OPS TESTS GOOD. TEAR DOWN REPORT DID CONFIRM REASON FOR REMOVAL. THE L/H ELEC. PUMP WAS FOUND WITH THE STATOR BURNED THROUGH AND ROTOR BADLY DAMAGED, DUE TO STARVATION. IT WAS CONCLUDED THAT THE ENGINE DRIVEN PUMP THAT WAS ALSO CHANGED OUT, IN ADDITION TO THE ELECTRICAL PUMP, WAS MORE THAN LIKELY THE CAUSE OF FLUID LOSS. THE ENGINE DRIVEN PUMP HAD DISINTEGRATED SEAL

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 73,910 hrs · 29,193 cycles

PHX - EEL - DURING OVERNIGHT INSPECTION DISCOVERED EMERGENCY ESCAPE PATH LIGHT ON SEAT 4L INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE ON EMERGENCY PATH LIGHT ON ROW 4 IAW STANDARD PRACTICES.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 73,592 hrs · 29,066 cycles

PHX - EEL - DURING OVERNIGHT INSPECTION DISCOVERED ROW 13 LT SEAT EMERGERNCY PATH LIGHT OUT. MAINTENANCE REPAIRED BROKEN WIRE AT ROW 13. OPERATIONAL CHECKS WERE GOOD.

Part: ENGINE — BIRD INGESTION (NR 2) · airframe 73,584 hrs · 29,063 cycles

CREW ABORTED TAKE OFF AT 140 KNOTS DUE TO NR 2 ENGINE BIRD INGESTION. CREW RETURNED TO THE GATE WITHOUT ANY FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED DAMAGED FAN BLADE AND ANNULUS FILLER ON THE NR 2 ENGINE. REPORTED FOR PRECAUTIONARY PURPOSES. BORESCOOPE WAS PERFORMED IAW AMERICA WEST AIRLES TASK CARD I5M72609, DAMAGE THAT WAS FOUND WAS BLADE TIP DAMAGE TO THE NR 2 FAN BLADE ON THE NR 2 ENG. THE LEADING EDGE TIP WAS BENT .4 WHICH WAS OUT OF LIMTS.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 72,824 hrs · 28,736 cycles

PHX - EEL - DISCOVERED EMERGENCY FLASHLIGHT AT FLIGHT ATTENDANT STATION 4 NOT DISPLAYING THE RED CHARGING LIGHT AND FORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BOTH FLASHLIGHT. OPERATIONAL CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,814 hrs · 28,730 cycles

PHX - EEL - DURING A9 CHECK DISCOVERED SEAT MOUNTED EMERGENCY EXIT LIGHT AT ROW 29 LEFT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXIT LIGHT ASSEMBLY AT ROW 29 LEFT. OPS CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,814 hrs · 28,730 cycles

PHX - EEL - DURING A9 CHECK DISCOVERED SEAT MOUNTED EMERGENCY EXIT LIGHT AT ROW 29 LEFT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXIT LIGHT ASSEMBLY AT ROW 29 LEFT. OPS CHECKS WERE GOOD.

Part: CONTROL SYSTEM — MALFUNCTIONED (LE FLAPS) · airframe 72,537 hrs · 28,590 cycles

PHX - FLIGHT CONTROL - FLT 0059 - UPON SELECTION OF FLAPS THE CREW REPORTED AN EICAS MESSAGE FOR LEADING EDGE SLAT DISAGREE MESSAGE WITH FLAPS SELECTED IN THE FIRST DETENT. CREW COMPLETED QRH CHECKLIST AND CALLED OUT EMERGENCY EQUIPMENT FOR PRECAUTIONARY PURPOSES. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, TESTED AND CYCLED FLAPS/SLATS WITH NO DEFECTS OR FAULTS BEING NOTED. AIRCRAFT WAS RETURNED TO SERVICE. AT THE TIME OF THIS INCIDENT THERE WAS A FOLLOW UP CURRENTLY ISSUED AGAINST THIS AIRCRAFT. THE FOLLOW UP WAS COMPLIED WITH ON 19AUG05, WITH SEVERAL ROTARY ACTUATORS BEING REPLACED CLEARING THE FOLLOW UP.

Part: WARNING SYSTEM — ACTIVATED (SLATS) · airframe 72,509 hrs · 28,575 cycles

FLT 563 - WHILE DEPLOYING FLAPS CREW REPORTED LEADING EDGE SLAT DISAGREE EICAS MESSAGE. MESSAGE CLEARED WITH ALTERNATE EXTENSION. EMERGENCY LANDING FOR PRECAUTIONARY PURPOSES. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECK IAW TASK CARD F1B27629, OPERATIONAL CHECKS GOOD. NO FAULTS FOUND.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,750 hrs · 36,526 cycles

DURING C-10 CHECK FOUND SEVERAL EMERGENCY BULL NOSE LIGHTS INOPERATIVE AT L3 AND R3 DOORS. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY AT M735. OPERATIONAL CHECKS WERE GOOD.

Part: CABLE — LOOSE (L1 DOOR) · airframe 72,102 hrs · 28,419 cycles

DURING C-10 CHECK THE L1 DOOR EMERGENCY POWER ASSIST CABLE FAILED TRAVEL CHECK. MAINTENANCE ADJUSTED TRAVEL OF L1 EMERGENCY POWER ASSIST CABLE IAW BOEING 757 MM 52-11-32-4. OPERATIONAL CHECKS WERE GOOD.

Part: SLIDE — BROKEN (L3 DOOR) · airframe 72,102 hrs · 28,419 cycles

DURING C-10 CHECK, FOUND MAIN CABIN L-3 DOOR SLIDE UPPER END TANGS BROKEN. MAINTENANCE REMOVED AND REPLACED L-3 DOOR SLIDE IAW BOEING 757 MM 25-66-03-4.

Part: GIRT BAR — OUT OF ADJUST (R4 DOOR) · airframe 72,102 hrs · 28,419 cycles

DURING C-10 CHECK THE R4 DOOR GIRT BAR WAS NOT FULLY ENGAGING IN LATCHES ON FLOOR. MAINTENANCE ADJUSTED R4 GIRT BAR AND LATCHES IAW BOEING 757 MM 52-11-25-5 PAGE 2, STEP F2. OPERATIONAL CHECKS WERE GOOD.

Part: GIRT BAR — OUT OF ADJUST (L4 DOOR) · airframe 72,102 hrs · 28,419 cycles

DURING C-10 CHECK THE L4 DOOR GIRT BAR WAS NOT PROPERLY ENGAGING LATCHES ON FLOOR. MAINTENANCE ADJUSTED L4 GIRT BAR AND LATCHES IAW BOEING 757 MM 52-11-25-5 PAGE 2, STEP F2. OPERATIONAL CHECKS WERE GOOD.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 72,102 hrs · 28,419 cycles

DURING C-10 CHECK THE R1 DOOR GIRT BAR WAS NOT FULLY ENGAGING IN LATCHES ON FLOOR.. MAINTENANCE ADJUSTED R1 GIRT BAR AND LATCHES IAW BOEING 757 MM 52-11-25-5 PAGE 2, STEP F2. OPERATIONAL CHECKS WERE GOOD.

Part: FITTING — DAMAGED (ZONE 600) · airframe 72,102 hrs · 28,419 cycles

DURING C-10 CHECK, FOUND ELONGATED HOLE ON THE RT WING SIDE LOAD DRAG FITTING. MAINTENANCE OVERSIZED THE HOLE IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REPAIR (ER) 19-5704-05175-ES3. FABRICATED BUSHING WITH AN INTERNAL HOLE DIAMETER OF .375 IAW SERVICE BULLETIN 757-54-0035 R2, STEP 14. INSTALLED SIDE LINK AND TENSION CLIP WITH SB 757-54-0035 R2 BOLTS IAW AWA ER 19-5704-05175-ES3.

Part: SKIN — DAMAGED (RT WING PYLON) · airframe 72,102 hrs · 28,419 cycles

DURING C-10 CHECK, DRILL DAMAGE OCCURRED TO FASTENER HOLE ON RT WING PYLON SIDE LOAD FITTING AT BL 9R, 3RD HOLE FROM AFT END ON OUTBOARD SIDE OF FITTING. MAINTENANCE SPOT FACED AND REMOVED DAMAGE FROM DISCREPANT HOLE IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REQUEST (ER) 19-5704-05174-ES3. FLAP PEENED, TREATED AND PRIMED AREA IAW BOEING 757 SRM 51-20-06, SOPM 20-10-03, AND ER 19-5704-05174-ES3.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,102 hrs · 28,419 cycles

DURING C-10 CHECK, FOUND CORROSION IN AFT CARGO BAY ON UPPER SURFACE OF CARGO FLOOR AT THRESHOLD PLATE BETWEEN STA 1380 TO STA 1440, WL 142, STRINGER 27R. MX REMOVED CORRODED THRESHOLD PLATE BETWEEN STA 1380 TO STA 1440, WL 142, STRINGER 27R AND INSTALLED NEW THRESHOLD PLATE IAW BOEING 757 SRM 53-00-53, 51-70-01, AND 51-40-02.

Part: SPAR — DAMAGED (ZONE 500) · airframe 72,102 hrs · 28,419 cycles

DURING C-10 CHECK FOUND TWO ELONGATED HOLES ON BRACKET, FORWARD FLAP SPAR AND FLAP SKIN LOCATED ON THE LT WING INBOARD MAIN FLAP, FORWARD OF LOWER SPAR AND SKIN. MAINTENANCE REMOVED DAMAGE FROM ELONGATED HOLES ON BRACKET, FORWARD FLAP SPAR AND FLAP SKIN LOCATED ON THE LT WING INBOARD MAIN FLAP, FORWARD OF LOWER SPAR AND SKIN IAW AWA ER 19-5753-05175-ES1. FABRICATED FREEZE PLUGS AND REPAIR DOUBLERS IAW AWA ER 19-5753-05175-ES1. INSTALLED FABRICATED REPAIR PARTS IAW BOEING 757 SRM 51-20-07, SOPM 20-10-03 AND AWA ER 19-5753-05175-ES1.

Part: SKIN — DAMAGED (TE FLAPS) · airframe 72,102 hrs · 28,419 cycles

DURING C-10 CHECK A PYLON STAND HIT RT INBOARD AFT FLAP TRAILING EDGE, DELAMINATING AFT EDGE APPROX 8 INCHES BY 2 INCHES. ALSO, CRACKING LOWER SKIN MEASURING .76 INCHES IN LENGTH EXTENDING FROM AFT EDGE FORWARD LOCATED AT STA 205, BL 21.5L. MAINTENANCE REMOVED DAMAGED AREA FROM RT INBOARD AFT FLAP TRAILING EDGE AND PREPPED REPAIR AREA FOR BONDING OF UPPER AND LOWER SKIN PLYS IAW BOEING 57 SRM 51-70-17, PARAGRAPH 4M. BONDED UPPER AND LOWER SKIN IAW BOEING 757 SRM 51-70-17, PARAGRAPH 4M AND AMERICA WEST AIRLINES ENGINEERING REQUEST 19-5733-05173-ES1.

Part: SELECTOR PANEL — SHORTED (COCKPIT) · airframe 68,338 hrs · 26,790 cycles

PHX - SMOKE - FLT 0052 - EN ROUTE FROM SJD TO PHX FLIGHT CREW NOTICED SMOKE EMANATING FROM BOOM / OXYGEN SWITCH ON NR 2 AUDIO SELECTOR PANEL, SMOKE STOPPED SHORTLY AFTER IT WAS NOTICED. MAINTENANCE REMOVED AND REPLACED THE NR 2 AUDIO SELECTOR PANEL IAW BMM 23-51-01, OPERATIONAL CHECK WAS GOOD. VENDORS SHOP EVALUATION OF AUDIO SELECTOR PANEL S/N D00410 CONFIRMED REASON FOR REMOVAL FINDING RESISTOR (R1) AND CAPACITOR (C1) ON A2 CIRCUIT BOARD BURNED. REPLACED RESISTOR (R1) AND CAPACITOR (C1) ON A2 CIRCUIT BOARD, AND REPLACED OXYGEN / BOOM SWITCH PER E.O. 2350 01001. UNIT CLEANED, INSPECTED, AND TESTED IAW CMM 23-51-54, REV. 27.

Part: SLIDE — LEAKING (L-4 DOOR) · airframe 67,991 hrs · 26,661 cycles

PHX - EES - DURING 4-DAY CHECK MAINTENANCE FOUND THE L-4 DOOR SLIDE BOTTLE PRESSURE IN RED ZONE. MAINTENANCE REMOVED AND REPLACED L-4 DOOR SLIDE ASSEMBLY IAW T/C R1C25602.

Part: HOUSING — DAMAGED (SEAT ROW 6-8 LT) · airframe 67,417 hrs · 26,436 cycles

DURING INSPECTION FOUND THE EMERGENCY ESCAPE PATH LIGHTS SEAT ROWS 1-8 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULLNOSE LIGHT HOUSING BETWEEN SEAT ROWS 6-8, OPERATIONAL CHECK WAS GOOD.

Part: PANEL — LOOSE (GOUND POWER) · airframe 67,313 hrs · 26,397 cycles

ON TAKEOFF ROLL AT LAS EN ROUTE FOR JFK THE TOWER ADVISED FLIGHT CREW A PANEL WAS OPEN, TAKEOFF WAS REJECTED AT LOW SPEED. TAXIED BACK TO RAMP AND MAINTENANCE SECURED THE FORWARD GROUND POWER PANEL. TAXIED BACK TO RUNWAY, DEPARTED WITHOUT FURTHER EVENT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,287 hrs · 26,390 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND AT NUT PLATES ON AFT CARGO COMPARTMENT FLOORBEAM BS 1502-1517, RBL 2. MAINTENANCE REMOVED DAMAGED SECTION OF CARGO FLOORBEAM FROM BS 1502 TO BS 1517, RBL 2; FABRICATED A REPAIR ANGLE & FILLER; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11 PG 1-7 FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,287 hrs · 26,390 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND AT NUT PLATES ON AFT CARGO COMPARTMENT FLOORBEAM BS 1503-1540, LBL 2. MAINTENANCE REMOVED DAMAGED SECTION OF CARGO FLOORBEAM FROM BS 1503 TO BS 1540, LBL 2; FABRICATED A REPLACEMENT FLOORBEAM AND SPLICES; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11 PG 1-7 FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,287 hrs · 26,390 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND AROUND NUT PLATES HOLES OF AFT CARGO COMPARTMENT FLOORBEAM BS 1624 TO BS 1638, RBL 14. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM UPPER CAP AT BS 1624 TO BS 1638, RBL 14; FABRICATED REPAIR ANGLES AND NEW REPLACEMENT SECTION OF UPPER CAP; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11, PG 1-6.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,287 hrs · 26,390 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND AT NUT PLATES ON AFT CARGO COMPARTMENT FLOORBEAM FROM BS 1503 TO BS 1513, RBL 9. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM FROM BS 1503 TO BS 1513, RBL 9; FABRICATED 2 EACH FILLERS, AND 2 EACH REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11 PG 6 FIG 1.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,287 hrs · 26,390 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK A .5625 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT FLOORBEAM BS 1600, LBL 2. MAINTENANCE REMOVED DAMAGED SECTION OF CARGO FLOORBEAM FROM BS 1545 TO BS 1640, LBL 2; FABRICATED A REPAIR CHANNEL; INSTALLED REPAIR PART IAW B757-200 SRM 51-70-11 PG 1-6 FIG 1.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,287 hrs · 26,390 cycles

DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT SHEAR DECK LOWER SUPPORT ANGLE BS 1701-1720, LBL 45. MAINTENANCE REMOVED DAMAGED AFT SHEAR DECK LOWER SUPPORT ANGLE FROM BS 1701 TO BS 1720, LBL 45; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 146N5323; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02 PG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,287 hrs · 26,390 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND AT NUT PLATES ON LOWER SIDE OF AFT CARGO COMPARTMENT FLOORBEAM BS 1500 TO BS 1540, LBL 9. MAINTENANCE REMOVED DAMAGED SECTION OF CARGO FLOORBEAM FROM BS 1500 TO BS 1540, LBL 9; FABRICATED A REPAIR ANGLE AND CHANNEL; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11, PG 1-6 FIG 1.

Part: WEB — CORRODED (FUSELAGE) · airframe 67,287 hrs · 26,390 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FORMER WEB AT LOWER PORTION OF WEB WHERE ATTACHED TO SKIN BS 1500 TO BS 1520. MAINTENANCE REMOVED DAMAGED FORMER WEB FROM BS 1500 TO BS 1520; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, PG 1, PARA B1-A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,287 hrs · 26,390 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOORBEAM AT NUT PLATES BETWEEN BS 1500 TO BS 1510, LBL 14. MAINTENANCE REMOVED CORRODED FLOORBEAM CAP BETWEEN BS 1500 TO BS 1510, LBL 14; FABRICATED A NEW REPLACEMENT CHANNEL AND REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-1 FIG 1.

Part: WEB — CORRODED (FUSELAGE) · airframe 67,287 hrs · 26,390 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FORMER WEB BS 1420, LBL 2. MAINTENANCE REMOVED DAMAGED FORMER WEB FROM BS 1420, LBL 2; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, PG 1, PARA B1-A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,287 hrs · 26,390 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOORBEAM AT BS 1362, RBL 14. MAINTENANCE REMOVED DAMAGED AREA OF FLOORBEAM BETWEEN BS 1343 AND BS 1365, RBL 14; FABRICATED 4 EACH REPAIR ANGLES & 2 EACH CHANNELS; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11 FIG 1 PG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,287 hrs · 26,390 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON NUT PLATES LOWER SIDE OF AFT CARGO COMPARTMENT FLOORBEAM BS 1470, RBL 20. MAINTENANCE REMOVED DAMAGED FLOORBEAM FROM BS 1440 TO BS 1500, RBL 20; FABRICATED A NEW REPLACEMENT FLOORBEAM; INSTALLED REPAIR PART IAW B757-200 SRM 51-70-11 PG 1-7.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,287 hrs · 26,390 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON NUT PLATES LOWER SIDE OF AFT CARGO COMPARTMENT FLOORBEAM BS 1304 TO BS 1312, LBL 2. MAINTENANCE REMOVED DAMAGED FLOORBEAM FROM BS 1215 TO BS 1320, LBL 2; FABRICATED A NEW REPLACEMENT FLOORBEAM AND SPLICES; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11, PG 1-6.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,287 hrs · 26,390 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND AT NUT PLATES ON AFT CARGO COMPARTMENT FLOORBEAM BS 1470, LBL 2. MAINTENANCE REMOVED DAMAGED SECTION OF CARGO FLOORBEAM BS 1470, LBL 2; FABRICATED A REPAIR ANGLE & FILLER; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11 PG 1-7 FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,287 hrs · 26,390 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND AT NUT PLATES ON AFT CARGO COMPARTMENT FLOORBEAM BS 1320, LBL 2. MAINTENANCE REMOVED DAMAGED SECTION OF CARGO FLOORBEAM FROM BS 1215 TO BS 1320, LBL 2; FABRICATED A REPLACEMENT FLOORBEAM AND SPLICES; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11 PG 1-7 FIG 1.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,287 hrs · 26,390 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOORBEAM SUPPORT BRACKET BS 1310, RBL 14. MAINTENANCE REMOVED CORRODED FLOORBEAM SUPPORT BRACKET BS 1310, RBL 14; FABRICATED A NEW REPLACEMENT BRACKET; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02 PG 7A.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,287 hrs · 26,390 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOORBEAM SUPPORT BRACKET BS 1310, LBL 14. MAINTENANCE REMOVED CORRODED FLOORBEAM SUPPORT BRACKET BS 1310, LBL 14; FABRICATED A NEW REPLACEMENT BRACKET; INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02 PG 7A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,287 hrs · 26,390 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF AFT CARGO COMPARTMENT FLOORBEAM BS 1474, RBL 9. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM FROM BS 1474, RBL 9; FABRICATED REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11, PG 6 FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,287 hrs · 26,390 cycles

DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOORBEAM AT BS 1330, RBL 14. MAINTENANCE REMOVED DAMAGED AREA OF FLOORBEAM AT BS 1330, RBL 14; FABRICATED REPAIR ANGLES AND A FILLER; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11 FIG 1 PG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,287 hrs · 26,390 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOORBEAM BS 1460-1480, RBL 18. MAINTENANCE REMOVED DAMAGED T-ANGLE AND ATTACH BRACKETS FROM BS 1460-1480, RBL 18; FABRICATED A NEW REPLACEMENT ANGLE AND ATTACH BRACKETS; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-40-05 PG 5 FIG 3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,287 hrs · 26,390 cycles

DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOORBEAM AT BS 1470, RBL 2. MAINTENANCE REMOVED DAMAGED AREA OF FLOORBEAM BETWEEN BS 1450 AND BS 1480, RBL 2; FABRICATED 4 EACH REPAIR ANGLES AND 2 EACH CHANNELS; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11 FIG 1 PG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,287 hrs · 26,390 cycles

DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOORBEAM AT BS 1320 AND BS 1330, RBL 2. MAINTENANCE REMOVED DAMAGED AREA OF FLOORBEAM BETWEEN BS 1235 AND BS 1340, RBL 2; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM AND REPAIR SPLICES; INSTALLED REPAIR PARTS IAW B757-200 SRM 51-70-11 FIG 1 PG 6.

Part: GIRT BAR — DAMAGED (ESCAPE SLIDE) · airframe 66,399 hrs · 26,031 cycles

FLIGHT CREW REPORTED THE L-4 DOOR SLIDE ARMING HANDLE JAMS, DOOR EVACUATION SLIDE ARMING LEVER DIFFICULT TO POSITION TO ENGAGE POSITION. MAINTENANCE FOUND GIRT BAR FORWARD TANG BROKEN, REMOVED AND REPLACED L-4 DOOR SLIDE ASSEMBLY IAW T/C R1C25602, OPERATIONAL CHECK WAS GOOD.

Part: BLEED VALVE — FAILED (ZONE 420) · airframe 65,866 hrs · 25,803 cycles

ON TAKEOFF FROM PHX EN ROUTE FOR LAX AS THROTTLES ADVANCED HEARD A LOUD BANG, REJECTED TAKEOFF DUE TO POSSIBLE NR 2 ENGINE COMPRESSOR STALL. PAX ALSO REPORTED SEEING FLAMES COMING OUT REAR OF ENGINE. MAINT PERFORMED ENGINE SURGE PROCEDURES AND BORESCOPED THE NR 2 ENGINE. NO DEFECTS WERE NOTED. PERFORMED COMPRESSOR AIRFLOW CONTROL TEST NR 3 PER T/C F5M72603. NR 2 ENGINE HIGH PRESSURE (HP) BLEED VALVE FAILED TO OPEN AND CLOSE PER SCHEDULE TABLE 1, COND. A & C. REMOVED AND REPLACED HP2 BLEED VALVE IAW BMM 75-32-04. HP2 BLEED SOLENOID SHOWED EVIDENCE OF CONTAMINATION SO IT WAS ALSO REMOVED AND REPLACED IAW BMM 75-32-05. BLEW OUT LINES AND RE-ACCOMPLISHED TEST NR , SYS OPERATES NORMALLY. PART

Part: STRUCTURE — VIBRATION (AIRFRAME) · airframe 65,462 hrs · 25,618 cycles

LAS - EMERGENCY LANDING - FLT 0048 - ON APPROACH INTO LAS EN ROUTE FROM DCA WITH FLAPS AT 5, LANDING GEAR DOWN, AND SPEED BRAKES ARMED, A VIBRATION DEVELOPED THROUGHOUT THE AIRCRAFT. HYDRAULICS AND ENGINE INDICATIONS APPEARED NORMAL, AND AIRCRAFT CONTROL WAS NOT A PROBLEM, DECLARED AN EMERGENCY, AND LANDED WITHOUT EVENT. MAINTENANCE INSPECTED FUSELAGE AND WINGS FOR LOOSE OR MISSING PANELS; INSPECTED THE FLIGHT CONTROLS, FLAPS, LANDING GEAR, AND LANDING GEAR DOORS; INSPECTED THE TAIL AND HORIZONTAL STABILIZER, ALL CHECKS WERE GOOD.

Part: BATTERY — DISCHARGED (ZONE 900 - LAV) · airframe 64,944 hrs · 25,371 cycles

PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT AT L-1 DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERIES IN THE EMERGENCY FLASHLIGHT AT THE L-1 DOOR, FUNCTIONAL CHECK WAS GOOD.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 63,650 hrs · 24,829 cycles

LCQ - MAJOR REPAIR - DURING C-8 INSPECTION A CRACK WAS FOUND ON THE NR 1 ENGINE PYLON FRAME AT THE LOWER FORWARD CORNER OF ACCESS APNEL 433AL CUTOUT. MAINTENANCE STOP DRILLED CRACK IAW B757 SRM 51-10-02 PAGE 17. FABRICATED REPAIR DOUBLER .125 STELL 15 SPH, HEAT TREATED IAW BAC 5619 PAGE 5 AND PASSVATED DOUBLER IAW E.R. 19-5451-02163-SS3. MAINTENANCE THEN INSTALLED DOUBLER AND ACCESS PANEL IAW AWA ER 19-5451-02163-SS3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,650 hrs · 24,829 cycles

DURING C-08 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF OUTBOARD LONGITUDINAL FLOOR SUPPORT AT LBL 64, WL 208, FROM BS 377 TO 395. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS, REMOVED DAMAGED PORTION OF WEB, FABRICATED NEW WEB, AND INSTALLED REPAIR IAW B757-200 SRM 51-30-01, PG. 20, FIG. 7.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,650 hrs · 24,829 cycles

LCQ - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON FLOORBEAM UPPER CHORD SURFACE AT BS 377, LBL 15, WL 208. MAINTENANCE REMOVED 64 INCHES CORRODED SECTION OF UPPER CHORD; FABRICATED A NEW CHORD, 2 REPAIR ANGLES, AND 2 STRAPS; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-51, FIG 203, PG 209-213.

Part: SKIN — CHAFED (VERTICAL STAB) · airframe 63,650 hrs · 24,829 cycles

DURING C-8 INSPECTION TWO CHAFED AREAS OF SKIN WERE FOUND ON THE VERTICAL STAB LEADING EDGE AT FIN STATION 80 AND 90. MAINTENANCE BLENDED AND REMOVED CHAFED AREAS OF SKIN AT FSS STA.80 PER ASTM E797-95 PAGES 369-374 AND B757 SRM 55-30-01 FIG 101 PAGE 104. MAINTENANCE BLENDED AND REMOVED CHAFFED AREA OF SKIN AT FSS STA 90 IAW ASTM 797-95 PAGES 369-374 AND B757 SRM 55-30-01 FIG 101 PAGE 104. MAINTENANCE TREATED AND PRIMED AREAS IAW B757 SRM 51-20-01 PAGE 9 AND B757 AMM 51-21-10 PAGE 701. MAINTENANCE INSTALLED REPAIR DOUBLERS IAW B757 SRM 55-30-01 PAGES 201-202.

Part: IDG — DEFECTIVE (#2 ENGINE) · airframe 62,988 hrs · 24,566 cycles

PHX - ELECTRICAL POWER LOSS - FLT 813 - "C" - WHILE CLIMBING OUT OF PHX ENROUTE TO SFO THE APU FAILED, AIRCRAFT ALREADY OPERATING ON MEL 24-00-1 CONDITION #1 FOR #2 ENGINE DRIVEN GENERATOR INOPERATIVE, AIRCRAFT TURNED BACK TO PHX AND LANDED UNEVENTFULLY. MAINTENANCE REPLACED THE INTEGRATED DRIVE GENERATOR IAW T/C R5M24601, AND THE GENERATOR FIELD PANEL IAW BMM 31-10-00. MAINTENANCE ALSO FOUND A BENT PIN ON THE FIRE CONTROL MODULE CONNECTOR; REPAIRED THE PIN AND THE #2 ENGINE DRIVEN GENERATOR OPERATIONALLY CHECKED GOOD. THE APU INDICATED UNDERSPEED ON BITE AND WAS TROUBLESHOT IAW FAULT ISOLATION MANUAL 49-11-00, FIG 106, THE APU FUEL CONTROL UNIT WAS FOUND FAULTY AND REPLACED IAW T/C R6D49604. PART NAME; PANEL F

Part: WIRE — BROKEN (SEAT 3 L/H) · airframe 62,869 hrs · 24,524 cycles

PHX - EEL - "C" - DURING INSPECTION OF EMERGENCY LIGHTING SYSTEM EMERGENCY ESCAPE LIGHT ON SEAT ROW 3 L/H WAS FOUND INOPERATIVE. MAINTENANCE FOUND BROKEN WIRE AT SEAT ROW 3 L/H AND REPAIRED BROKEN WIRE IAW BOEING SWP 20-30-12, OPERATIONAL CHECK WAS GOOD.

Part: OVEN — SMOKE (GALLEY)

MCO- SMOKE IN FWD GALLEY - FLT 561 - EN ROUTE FROM PHX TO MCO THE OUTBOARD OVEN IN GALLEY GIB STARTED SMOKING. THE FLIGHT ATTENDANT TURNED THE OVEN OFF AND PULLED THE CIRCUIT BREAKER. REMOVED THE GALLEY HALON FIRE EXTINGUISHER AND STOOD BY TO ENSURE THERE WAS NO FIRE. THE FIRE EXTINGUISHER WAS NOT USED HOWEVER CREW DID BREAK THE TAMPER PROOF SEAL. AFTER TURNING THE OVEN OFF AND PULLING THE C/B THE OVEN QUIT SMOKING. IN MCO MAINTENANCE INSPECTED THE GALLEY AND DETERMINED THE OTHER OVENS IN OPERATIONAL STATUS. THE OUTBOARD OVEN WAS PLACED ON MEL 25-20-01, COND 1. THE TAMPER PROOF SEAL WAS REPLACED ON THE FIRE EXTINGUISHER. IN PHX THE NEXT DAY MAINTENANCE REMOVED THE OVEN AND FURTHER INSPECTED.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FWD CARGO COMPARTMENT FLOOR SUPPORT BEAM AT FS 543 AND LBL 8 IS DENTED AND CRACKED. REMOVED DAMAGED AREA; FABBED REPAIR ANGLE AND 1 FLOOR SUPPORT IAW SRM 51-70-12 AND 53-30-53; TREATED AND PRIMED REPAIR PARTS; INSTALLED REPAIR ANGLE AND REPLACEMENT SUPPORT IAW SRM 51-70-12 AND 51-40-02.

Part: BRACKET — CORRODED (FUSELAGE)

CABIN STA 1671 RBL 65 DOOR SILL ANGLE BRACKET HAS CORROSION. REMOVED CORROSION - FOUND OUT OF LIMITS; CUT OUT DAMAGE; FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-70-13.

Part: ATTACH ANGLE — CRACKED (NR 2 PYLON)

NR 2 PYLON AFT BLKHD ATTACH ANGLE IS CRACKED AT PP STA 200. REMOVED ANGLE IAW SRM 51-40-02; FABBED REPLACEMENT ANGLE IAW DWG 311N5041; INSTALLED IAW SRM 51-40-02.

Part: SKIN — DAMAGED (FUSELAGE)

DAMAGED RIVETS AND SKIN FWD OF L2 DOOR FS 620-640. CUT OUT DAMAGE AND REPAIRED IAW SRM 53-00-01 FIG 204, SRM 51-40-02.

Part: SKIN — GOUGED (NLG DOOR)

NOSE WHEEL WELL LEFT AFT DOOR FWD HINGE POINT SKIN IS GOUGED AFT SIDE OF HINGE. REPAIRED IAW ER 19-5310-01061-JS2.

Part: STRINGER — DENTED (FUSELAGE)

AFTER REMOVING DOUBLER AT STA 626 STR 16L, FOUND STR 16L DENTED. CUT OUT DAMAGE; FABBED AND INSTALLED REPAIR SPLICE IAW SRM 53-00-03 FIG 201.

Part: FITTING — CORRODED (CARGO BAY)

AFT CARGO COMPARTMENT ANCHOR FITTING AT FS 1380 LBL 23 HAS EXFOLIATION CORROSION AROUND FITTING. REMOVED STRUCTURE TO GAIN ACCESS TO REPAIR AREA IAW SRM 51-40-02; REMOVED DMGD SECTION OF SIDE PANEL; FABBED REPAIR SECTION AND REPAIR DOUBLER; INSTALLED PARTS IAW SRM 51-70-13; INSTALLED ACCESS STRUCTURE IAW SRM 51-40-02.

Part: SKIN — WRINKLED (R4 DOOR)

R4 DOOR SKIN EDGE WRINKLED AT FWD LWR CORNER. CUT OUT DAMAGED AREA, NDT - NO CRACKS. FABBED AND INSTALLED FILLER AND DOUBLER IAW SRM 52-10-01.

Part: SKIN — DENTED (L2 DOOR)

L2 DOOR FWD LWR CORNER EDGE SKIN HAS 2 DENTS. CUT OUT DAMAGED SKIN, NDT - NO CRACKS. FABBED DOUBLER AND FILLER IAW SRM 52-10-01; INSTALLED REPAIR PARTS IAW SRM 51-40-02.

Part: SKIN — DENTED (FUSELAGE)

DENT IN FUSELAGE SKIN AT FS 460 STR 19L .050 DEEP X .50 WIDE OUT OF LIMITS IAW SRM 53-00-01 FIG 101. CUT OUT DAMAGE AND REPAIRED SKIN IAW SRM 53-00-01 FIG 204.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

CABIN STA 1690-1720 RBL 12 FLOOR BOARD SUPPORT CORRODED. REMOVED, FABBED REPLACEMENT SUPPORT AND INSTALLED REPLACEMENT PART IAW SRM 51-40-02, 51-30-01 AND DWG 146N5180.

Part: SKIN — DENTED (L2 DOOR)

L2 DOOR FWD LWR CORNER EDGE SKIN HAS 2 DENTS. CUT OUT DAMAGED SKIN; NDT - NO CRACKS. FABBED DOUBLER AND FILLER IAW SRM 52-10-01; INSTALLED REPAIR PARTS IAW SRM 51-40-02.

Part: STRINGER — DENTED (FUSELAGE)

AFTER REMOVING DOUBLER AT STA 626 STR 16L FOUND STR 16L DENTED AND CREASED. CUT OUT DAMAGE; FABBED AND INSTALLED REPAIR SPLICE IAW SRM 53-00-03 FIG 201.

Part: COMPUTER — FAILED (COCKPIT) · airframe 42,079 hrs · 23,874 cycles

CAPTAIN''S FLIGHT DIRECTOR FAILED AND THE SMELL OF HOT ELECTRICAL WIRES WAS NOTICED. INVESTIGATED ELECTRICAL SMELL, NOTHING FOUND. REPLACED CAPT''S FLIGHT CONTROL COMPUTER. RECOMMENDATION: REMAIN OPEN PENDING REVIEW OF TEARDOWN REPORT, NO HISTORY.

Part: BLOWER — FAILED (SMOKE DETECTOR)

CARGO DETECTION AIR STATUS MESSAGE WHILE IN CRUISE FLT, RESET C/B MESSAGE. REPLACED NR AND NR 2 BLOWERS FOR FWD CARGO SMOKE DETECTOR. SMOKE DETECTOR CHECK OK, TT 0003663 SN DE5991, TT 0003662, SN DL1528 M+E 19-2610-9-0012.

Part: WIRE — CHAFED (RT MLG)

AFTER GEAR RETRACTION LANDING GEAR MONITOR EICAS MSG APPEARED. FOUND PROXIMITY SENSOR RT MLG INBOARD WIRING DOWN AND LOCK SENSOR HAD A CHAFED WIRE. REPAIRED WIRING PER MM CHAPTER 20 BITE OF THE PSEU, OPS CHECK GOOD RT MLG DOWNLOCK SENSOR.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP. REPLACED SEVERAL EMERGENCY LIGHT BATTERY PACKS.

Part: WIRE — DISCONNECTED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT ON SEAT 26 LEFT INOP. RESPLICED WIRES, OPS CHECK GOOD.

Part: HARNESS — DISCONNECTED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY SEAT LIGHT INOP AT ROW 18. RELAMPED AND CONNECTED SEAT HARNESS. OPS CHECK GOOD.

Part: DUCT — DETERIORATED (LT ENGINE)

LEFT ENGINE FIRE WARNING CLIMB THROUGH 15,000 FT. PERFORMED ENGINE FIRE CHECKLIST. FIRE BOTTLE DISCHARGED, IN FLIGHT SHUTDOWN. REMOVED AND REPLACED HP2 AND HP6 DUCTS. LEAK CHECKED GOOD. NO EICAS MESSAGE DISPLAYED AFTER ENGINE RUN. HP6 DUCT 16J08-1 12900845 DETERIORATED.

Part: DOOR SLIDE — BLOWN (R1 DOOR)

DURING MAINTENANCE PROCEDURE, R-1 DOOR SLIDE INADVERTENTLY BLOWN. REMOVED AND REPLACED EVACUATION DOOR SLIDE PER BMM 25-66-01. REMOVED AND REPLACED EMERGENCY POWER RESERVOIR PER BMM 52-11-30. PART TOTAL CYCLES, 9,299.

Part: OVEN — DIRTY (GALLEY)

PHX - FLT 25 - INBOARD OVEN IN FORWARD GALLEY PRODUCED SMOKE WHEN TURNED ON TO HEAT MEALS. CLEANED FOIL FROM OVEN. OPERATES GOOD. (M)

Part: COOLING FAN — FAILED (E/E BAY)

CMH - FLT 820 - SMELLED ELECTRICAL BURNING ODOR AT CRUISE. FIFTEEN MINUTES LATER, EICAS MESSAGE EQUIPMENT COOLING FAN DISPLAYED. REMOVED AND REPLACED ALTERNATE EQUIPMENT COOLING FAN. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND BATTERY PACK AT R2 DOOR INOPERATIVE. REMOVED AND REPLACED PACK, OPS CHECK GOOD. (M)

Part: EEL BATT PACK — DISCHARGED (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT L4 DOOR AND AFT LT AISLE. REMOVED AND REPLACED AFT LT BATTERY PACK, OPS CHECK GOOD. (M)

Part: EEL WIRE — BROKEN (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR TRACK EMERGENCY EXIT LIGHTS INOPERATIVE BETWEEN ROW 18 AND ROW 30. REPAIRED BROKEN WIRE AT R3 DOOR, OPS CHECK GOOD. (M)

Part: FRAME — GOUGED (FS 820)

PHX - DURING SCHEDULED C3 INSPECTION, FOUND DEEP GOUGE IN MAIN FRAME AT CENTER LINE, STATION 820. REPAIRED IAW SRM 53-00-07. (M)

Part: FLOORBEAM — CORRODED (FS 377)

PHX - DURING SCHEDULED C3 INSPECTION, FOUND 'I' BEAM IN FORWARD GALLEY AREA CORRODED BEYOND LIMITS AT STATION 377 LBL 0 TO LBL 10. FABRICATED REPAIR PART AND INSTALLED PER SRM 51-70-12. (M)

Part: FLOORBEAM — CORRODED (FS 345)

PHX - DURING SCHEDULED C3 INSPECTION, FOUND FWD GALLEY AREA 'I' BEAM CORRODED BEYOND LIMITS AT STATION 345 LBL 10. FABRICATED REPAIR PART AND INSTALLED PER SRM 51-70-12, FIG 2. (M)

Part: FRAME — GOUGED (FS 760)

PHX - DURING SCHEDULED C3 INSPECTION, FOUND DEEP GOUGE IN MAIN FRAME AT CENTER LINE, STATION 760. FABRICATED DOUBLER AND SUPPORTS, AND INSTALLED PARTS PER SRM 53-00-07, FIG 201. (M)

Part: CORNER — CRACKED (AFT CARGO DOOR)

PHX - DURING SCHEDULED C3 INSPECTION, FOUND AFT CARGO DOOR LOWER FORWARD CORNER CRACKED. REMOVED AND REPLACED CORNER PER SRM 51-40-02 AND SRM 51-10-00. (M)

Part: FRAME — GOUGED (FS 780)

PHX - DURING SCHEDULED C3 INSPECTION, FOUND DEEP GOUGE IN MAIN FRAME AT CENTER LINE, STATION 780. FABRICATED REPAIR PARTS, AND INSTALLED PARTS PER SRM 53-00-07, FIG 201. (M)

Part: FRAME — GOUGED (FS 800)

PHX - DURING SCHEDULED C3 INSPECTION, FOUND DEEP GOUGE IN MAIN FRAME AT CENTER LINE, STATION 800. FABRICATED DOUBLER AND SUPPORT, INSTALLED REPAIR AND SUPPORTS IAW WITH SRM 53-00-07, FIGURE 301. (M)

Part: EEL WIRING — BROKEN (CABIN)

PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE, LAST ROW IN AFT. REPAIRED WIRING TO LIGHTS, OPS CHECK NORMAL. (W)

Part: RETRACT MECH — MALFUNCTIONED (LANDING GEAR)

JFK - FLT 11 - AIR TURNBACK, CREW UNABLE TO RETRACT LANDING GEAR. LEVER WOULDN'T GO PAST THE 'OFF' POSITION. GEAR OVER RIDE WAS NOT ATTEMPTED, AND THERE WERE NO ASSOCIATED EICAS MESSAGES. A/C RETURNED TO GATE. MX PERFORMED VISUAL INSPECTION OF GEAR, AND NO DEFECTS WERE FOUND. MX PERFORMED BITE CHECK ON PSEU, NO ABNORMALITIES NOTED. MX PINNED GEAR AND VERIFIED OVER RIDE FUNCTION OPERATES NORMALLY. UNMANNED STATION RELEASE ISSUED PER MEL 32-31-01. ON DEPARTURE, GEAR SELECTED UP AND RETRACTED. ON ARRIVAL, MX PERFORMED PSEU BITE CHECK, ALL SYSTEMS CHECK NORMAL PER FIM 32-61-00. SYSTEM RESET AND PERFORMED VISUAL INSPECTION OF ALL GEAR SENSORS, NO DEFECTS NOTED. A/C RELEASED TO SERVICE. (W)