N906AW

Part: CONNECTOR — DIRTY (EVAC SLIDE) · airframe 102,263 hrs · 35,565 cycles

FLIGHT 452, R2 DOOR SLIDE LIGHT REMAINS ON. INSPECTED & CLEANED R2 DOOR SLIDE CONNECTORS. CYCLED DOOR ARM HANDLE NUMEROUS CYCLES. SYS OPERATIONAL CHECKED GOOD.

Part: OXYGEN BOTTLE — LEAKING (CREW O2) · airframe 101,086 hrs · 35,323 cycles

FLIGHT 663, EN-ROUTE AT COAST OUT, CREW O2 WAS FOUND TO HAVE DROPPED TO 80PSI. THE FLIGHT DECLARED AN EMER & DESCENDED TO 10,000 FEET. THE FLIGHT DIVERTED & LANDED WITHOUT FURTHER INCIDENT. REPLACED THE CREW OXYGEN BOTTLE. OPERATIONALLY & LEAK CHECKS OK.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,385 hrs · 34,966 cycles

C3 CHECK STRINGER 29L IS CORRODED AT FUSELAGE STATION 1640. REPAIRED STRINGER IAW EA 106306.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,385 hrs · 34,966 cycles

C3 CHECK STRINGER 29R IS CORRODED AT FUSELAGE STATION 1640. REPAIRED STRINGER IAW EA 106306.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,385 hrs · 34,966 cycles

C3 CHECK LEVEL 2 EXFOLIATION CORROSION ON EXTRUSION SPLICE SECTION OF FLOOR STRINGER AT BS 1519, RBL 7.5. REPAIRED EXTRUSION SPLICE SECTION OF FLOOR STRINGER , RBL 7.5 IAW TR 757-5310-12-0665.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,385 hrs · 34,966 cycles

C3 CHECK LEVEL 2 INTERGRANULAR CORROSION ON EXTRUSION SPLICE SECTION OF FLOOR STRINGER AT BS 1507, RBL 2.5. REPAIRED EXTRUSION SPLICE SECTION OF FLOOR STRINGER IAW TR 757-5310-12-0665.

Part: SKIN — DELAMINATED (RT AILERON) · airframe 99,385 hrs · 34,966 cycles

C3 CHECK DELAMINATION ON RT AILERON LOWER SURFACE APPROX 9.0 INCHES FROM TE & 21 INCHES FROM INBD END. REPAIRED RT AILERON LOWER SURFACE IAW SRM 57-60-01 & SRM 51-70-17.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,385 hrs · 34,966 cycles

C3 CHECK LEVEL 2 FILIFORM CORROSION ON TERMINATING CLIP AT BS 1620, STRINGER 30. REPLACED TERMINATING CLIP & SPLICE CHANNEL IAW DWG 146N3821.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,385 hrs · 34,966 cycles

C3 CHECK LEVEL 2 FILIFORM CORROSION ON STRINGER 29L BETWEEN BS 1621 TO 1670 AT WATER SERVICE AREA. REPAIRED STRINGER 29L BETWEEN BS 1621 TO 1670 AT WATER SERVICE AREA IAW EA 106306.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,385 hrs · 34,966 cycles

C3 CHECK LEVEL 2 FILIFORM CORROSION ON WATER SERVICE PAN BETWEEN BS 1621 TO 1670 & BETWEEN STRINGER 29L TO 29R. REPLACED WATER SERVICE PAN IAW EA 106306.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,385 hrs · 34,966 cycles

C3 CHECK LEVEL 2 EXFOLIATION CORROSION ON EXTRUSION SPLICE SECTION OF FLOOR STRINGER AT BS 1510, RBL 12. REPAIRED EXTRUSION SPLICE SECTION OF FLOOR STRINGER IAW SRM 53-00-53-1A-1 & TR 757-5310-12-0665.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,385 hrs · 34,966 cycles

C3 CHECK LEVEL 2 FILIFORM CORROSION ON STRINGER 29R BETWEEN BS 1621 TO 1670 AT WATER SERVICE AREA. REPAIRED STRINGER IAW EA 106306.

Part: BOTTLE — DISCHARGED (L1 DOOR) · airframe 98,972 hrs · 34,883 cycles

L1 SLIDE DOOR ASSIST BOTTLE READS 0 PSI. REPLACED L1 SLIDE DOOR ASSIST BOTTLE.

Part: COVER — OUT OF POSITION (L1 DOOR) · airframe 98,578 hrs · 34,808 cycles

DOOR L1 STIFF HARD TO OPEN & CLOSE. MX REPOSITIONED THE SLIDE BUSSEL & D RING, L1 DOOR OPERATES NORMAL..

Part: SLIDE RAFT — UNSECURE (L1 DOOR) · airframe 98,566 hrs · 34,806 cycles

LT SLIDE PACK DOOR 1L PARTIALLY OUT OF BUSTLE. SLIDE REMOVED FROM BUSTLE. MX FOUND DOOR 1L SLIDE ON JET WAY. R & R DOOR 1L SLIDE. ALSO R & R EMER POWER RESERVOIR. THE LACING COVER CABLE WAS PULLED OUT, UNIT WAS PARTIALLY DISASSEMBLED, CLEANED & INSPECTED, REPLACING ALL PARTS NECESSARY FOR REPAIR. PASSED LIGHT SYS TEST & HEIGHT CHECK. PACKED SLIDE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 98,343 hrs · 34,765 cycles

AFT FLIGHT ATTENDANT REPORTS EMER FLASHLIGHT INOPERATIVE. R & R AFT FLIGHT ATTENDANT FLASHLIGHT.

Part: SPRING — BENT (GIRT BAR) · airframe 97,940 hrs · 34,683 cycles

PHX R4 DOOR GIRT BAR LEAF SPRING BENT. R & R LEAF SPRING.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

PHX ROW 18 RT EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHTS POWER SUPPLY M732.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

PHX R2 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHTS POWER SUPPLY M732.

Part: BOLT — LOOSE (R1 DOOR)

PHX R1 DOOR DIFFICULT TO CLOSE. MX SECURED LOOSE BOLTS ON GUIDE ARM BRACKET, DOOR OPERATIONS CHECKED GOOD.

Part: ANGLE — CORRODED (BS 1360-1380) · airframe 96,160 hrs · 34,311 cycles

C3 CHECK, CORROSION IN AFT CARGO AT MULTIPLE FASTENER HOLES ALONG ENTIRE LENGTH OF ANGLE BETWEEN BS 1360 TO 1380, RBL 24. REPLACED ANGLE IAW SRM 51-40-02.

Part: SKIN — DELAMINATED (HORIZONTAL STAB) · airframe 96,160 hrs · 34,311 cycles

C2 CHECK, DELAMINATION ON RT HORIZONTAL STABILIZER SKIN PANEL AT STAB STA 92.70 APPROX 3" FORWARD OF FORWARD SPAR.

Part: PANEL — CRACKED (RT WING) · airframe 96,160 hrs · 34,311 cycles

C2 CHECK, CRACK FOUND ON RT WING NR 9 SLAT COVE PANEL AT APPROX 12 INCHES FROM INBD END LOWER SURFACE AT L/E. REPLACED RT WING 9 SLAT COVE PANEL IAW DWG 114N4003.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 96,160 hrs · 34,311 cycles

C2 CHECK, COMPOSITE DAMAGE ON LT OTBD T/E FLAP AT APPROX 52 INCHES OTBD FROM INBD END AT L/E 3 INCHES AFT OF FLAP SPAR. REPAIRED LT OTBD T/E FLAP IAW SRM 57-53-01 & 51-70-04.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 95,219 hrs · 34,118 cycles

PILOT REPORT - 13" CRACK IN CABIN FLOOR PANEL BETWEEN BS680 TO BS700, WL208.10. REPLACED FLOOR PANEL BETWEEN BS680 TO BS700, WL208.10 IAW AMM 53-01-01 & EA 204996.

Part: DUCT — LEAKING (LT ENGINE) · airframe 94,827 hrs · 34,031 cycles

FLT 47, EN ROUTE. FLIGHT EXPERIENCED A LEFT ENGINE OVERHEAT DURING CRUISE. PULLED ENGINE BACK TO HALF POWER, AND DECLARED AN EMERGENCY. LANDED AT DESTINATION WITHOUT FURTHER INCIDENT. MX FOUND THE HP 6 DUCT LEAKING. REPLACED THE DUCT. SHOP FOUND DUCT LEAKING AT SLIDER. SPHERICAL SEAL ASSY , PISTON RING, AND GUIDE RINGS CHIPPED AND CRACKED BEYOND LIMITS. PARTS REPLACED WITH NEW. DUCT ASSY WAS REPAIRED AND OVERHAULED.

Part: ACTUATOR — BYPASSING (LT MLG) · airframe 94,827 hrs · 34,031 cycles

PHX - FLT 47 EN ROUTE LIH TO PHX. DURING RETRACTION: EICAS MSG GEAR DISAGREE AND GEAR DOORS DISPLAYED WITH GEAR HANDLE UP, DOORS & GEAR AMBER LIGHTS ON, ALL GREEN DN LIGHTS OFF. WHEN GEAR HANDLE MOVED TO OFF, LEFT GREEN DOWN LIGHT CAME ON 2ND TRY TO RETRACT GEAR WAS NORMAL. MAINTENANCE REPLACED LEFT MLG RETRACT ACTUATOR.

Part: GIRT BAR — LACK OF LUBE (R4 DOOR SLIDE) · airframe 91,326 hrs · 33,326 cycles

DOOR 4R EVACUATION SLIDE ARMING LEVER WILL NOT MOVE INTO DETACH POSITION. THE LEVER MOVED ABOUT HALF NORMAL TRAVEL BEFORE STOPPING. "KNUCKLE-BUSTER" INDICATOR NOT FULLY STOWED. GIRT BAR ENGAGEMENT INDICATOR LIGHT NOT ILLUMINATED. LUBRICATED GIRT BAR END AND BAR LOCKS ON THE DOOR. BAR LOCK WAS HANGING UP ON LEAF SPRINGS. DOOR ARM-DISARM MECHANISM OPERATES SMOOTHLY.

Part: GIRT BAR — LACK OF LUBE (L4 DOOR SLIDE) · airframe 91,326 hrs · 33,326 cycles

DOOR 4L EVACUATION SLIDE ARMING LEVER WILL NOT MOVE INTO DETATCH POSITION. THE LEVER MOVED ABOUT HALF NORMAL TRAVEL BEFORE STOPPING. "KNUCKLE-BUSTER" INDICATOR NOT FULLY STOWED. GIRT BAR ENGAGEMENT INDICATOR LIGHT NOT ILLUMINATED. LUBRICATED GIRT BAR END AND BAR LOCKS ON THE DOOR. BAR LOCK WAS HANGING UP ON LEAF SPRINGS. DOOR ARM-DISARM MECHANISM OPERATES SMOOTHLY.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,300 hrs · 33,319 cycles

C1 CHECK - LEVEL 2 EXFOLIATION CORROSION ON PRODUCTION SPLICE AT BS 675.5, S28L. REPAIRED PRODUCTION SPLICE AT BS675.5, S28L IAW EA # 103685.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,300 hrs · 33,319 cycles

C1 CHECK - LEVEL 2 EXFOLIATION CORROSION ON RIGHT KEEL BEAM CHANNEL BETWEEN BS 640 TO BS 700, S28R. REPAIRED RIGHT KEEL BEAM CHANNEL BETWEEN BS 640 TO BS 700, S28R IAW EA 103702.

Part: SKIN — DEBONDED (TE FLAP) · airframe 91,300 hrs · 33,319 cycles

C1 CHECK - DISBONDING ON AREA OF RIGHT OUTBOARD FLAP AT WS459.59 ON UPPER SURFACE APPROX 2.75 INCHES FROM TRAILING EDGE. REPAIRED RIGHT OUTBOARD FLAP AT WS459.59 IAW B757 51-70-04 & 57-53-01.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 91,300 hrs · 33,319 cycles

C1 CHECK - AREA OF DELAMINATION ON RIGHT OUTBOARD FLAP UPPER SURFACE 4.5 INCHES FROM AFT EDGE & 161 INCHES FROM INBOARD END. REPAIRED RIGHT OUTBOARD FLAP UPPER SURFACE IAW B757 SRM 51-70-17.

Part: RESERVOIR — LOW PRESSURE (L4 DOOR) · airframe 90,749 hrs · 33,209 cycles

PHX - L-4 DOOR EMERGENCY POWER RESERVOIR PRESSURE LOW. REMOVED AND REPLACED L-4 DOOR EMERGENCY POWER RESERVOIR.

Part: WIRE — BROKEN (CABIN)

PHX - EMERGENCY EXIT LIGHT SWITCH OVER L-2 DOOR INOP. RE-TERMINATED TERMINAL ON WIRE W3532-0038-22. OPS CHECK GOOD.

Part: BEARING — WORN (L1 DOOR) · airframe 90,157 hrs · 33,071 cycles

LIH FLT 146 PHX TO LIH. ON ARRIVAL FOUND DOOR 1 LEFT EXTERIOR BUTTERFLY HANDLE OUT AND PARTIALLY TURNED. MAINTENANCE REPLACED BEARINGS IN EXTERIOR DOOR HANDLE ON L1 DOOR AND RE-ASSEMBLED SHAFT ASSY.

Part: LANYARD — OUT OF POSITION (EVAC SLIDE)

PHX - FLIGHT ATTENDANT UNABLE TO ARM DOOR 2L. RE-STOWED GIRT BAR LANYARD.

Part: LANYARD — OUT OF POSITION (EVAC SLIDE)

PHX - RIGHT FORWARD ENTRY DOOR WILL NOT ARM. MAINTENANCE FOUND LANYARD FOR SLIDE INTERFERING WITH GIRT BAR. STOWED LANYARD.

Part: PANEL — DEBONDED (VERTICAL STAB) · airframe 89,367 hrs · 32,911 cycles

CLT - RON - DEBONDED FIXED PANEL ON LEADING EDGE OF RIGHT OF VERTICAL STABILIZER BETWEEN FSS 0 TO FSS 119.46. REPLACED FIXED PANEL ON LEADING EDGE OF RIGHT OF VERTICAL STABILIZER BETWEEN FSS 0 TO FSS 119.46 IAW B757 AMM 06-42-00-201.

Part: PANEL — DEBONDED (VERTICAL STAB) · airframe 89,367 hrs · 32,911 cycles

DISBONDING ON LEFT SIDE OF VERTICAL STABILIZER. NOTE: A SUPPLEMENT WILL BE SUBMITTED UPON COMPLETION OF REPAIR.

Part: BEARING — WORN (L1 DOOR)

PHX - THE L1 DOOR OUTER HANDLE WAS STIFF AND BINDING, MAKING IT DIFFICULT TO OPEN. MAINTENANCE REPLACED THE L1 DOOR OUTER HANDLE GUIDE BEARING.

Part: SLIDE — LOW PRESSURE (L4 DOOR)

PHX - THE L4 DOOR EVACUATION SLIDE PRESSURE GAUGE IS IN THE RED. MAINTENANCE REMOVED AND REPLACED THE L4 DOOR SLIDE.

Part: SPRING — BENT (GIRT BAR)

PHX - THE L4 DOOR GIRT BAR SPRING WAS BENT. MAINTENANCE REPLACED THE L4 DOOR GIRT BAR.

Part: SLIDE — LOW PRESSURE (L2 DOOR)

PHX - THE DOOR SLIDE AT DOOR L2 INDICATES BELOW THE GREEN BAND. MAINTENANCE REMOVED AND REPLACED THE L2 DOOR SLIDE.

Part: GIRT BAR — DEFECTIVE (SERVICE DOOR)

PHX - THE GIRT BAR ENGAGEMENT LIGHT EXTINGUISHED WITH THE EVACUATION SLIDE ARMING LEVER IN ENGAGE POSITION AT SERVICE DOOR R1. REMOVED AND REPLACED THE R1 GIRT BAR ASSEMBLY.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 87,768 hrs · 32,574 cycles

MCN - C4 - MAJOR REPAIR - CRACK ON ATTACH ANGLE CHORD AT BS 1480 TO BS 1500, LBL 23. REPLACED ATTACH ANGLE CHORD AT BS 1480 TO BS 1500, LBL 23 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 87,768 hrs · 32,574 cycles

MCN - C4 - MAJOR REPAIR - CORROSION ON INTERCOSTAL BETWEEN BS 1600 TO BS 1620, RBL 2.9 IN AFT CARGO COMPARTMENT. REPLACED INTERCOSTAL BETWEEN BS 1600 TO BS 1620, RBL 2.9 IN AFT CARGO COMPARTMENT IAW B757 SRM 51-40-02.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,768 hrs · 32,574 cycles

MCN - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FUSELAGE FRAME AT BS 922, LBL 50. REPAIRED FUSELAGE FRAME AT BS 922, LBL 50 IAW B757 SRM 51-70-12.

Part: ATTACH FITTING — DAMAGED (R2 DOOR) · airframe 87,768 hrs · 32,574 cycles

MCN - C4 - MAJOR REPAIR - R-2 DOOR ATTACHMENT CLIP FOR NR 6 STOP FITTING HAS ELONGATED OVERSIZED HOLES AT UPPER STOP FITTING AT BS 724. REPLACED R-2 DOOR ATTACHMENT CLIP FOR NR 6 STOP FITTING AT UPPER STOP FITTING AT BS 724 IAW EA 130188A.

Part: STOP FITTING — DAMAGED (R2 DOOR) · airframe 87,768 hrs · 32,574 cycles

MCN - C4 - MAJOR REPAIR - R-2 DOOR WEB BEAM FOR NR 6 STOP FITTING HAS ELONGATED OVERSIZED HOLES AT STOP FITTING AT BS 724. REPLACED R-2 DOOR WEB BEAM FOR NR 6 STOP FITTING AT STOP FITTING AT BS 724 IAW EA 130188A.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,768 hrs · 32,574 cycles

MCN - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION (5 SPOTS) ON SUPPORT INNER CHORD BETWEEN BS 1660 TO BS 1680, LBL 54 TOP & BOTTOM SURFACES. REPLACED SUPPORT INNER CHORD BETWEEN BS 1660 TO BS 1680, LBL 54 IAW B757 SRM 51-10-02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 87,768 hrs · 32,574 cycles

MCN - C4 - MAJOR REPAIR - 2 CRACKS ON STRINGER AT BS 1100, S16L. REPAIRED STRINGER AT BS 1100, S16L IAW EA 130441.

Part: STRUT — DAMAGED (NACELLE) · airframe 87,768 hrs · 32,574 cycles

MCN - C4 - MAJOR REPAIR - ELONGATED HOLE WITH EXISTING PLUG ON INBOARD SIDE OF NR 1 PYLON STRUT AT PPS180.25, WL 136.5. REMOVED EXISTING PLUG & REPAIRED PYLON IAW EA 130439.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 87,768 hrs · 32,574 cycles

MCN - C4 - MAJOR REPAIR - 2 CRACKS ON STRINGER AT BS 1100, S15L. REPAIRED STRINGER AT BS 1100, S15L IAW EA 130440.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 87,768 hrs · 32,574 cycles

MCN - C4 - MAJOR REPAIR - TOP ANGLE ON INTERCOSTAL CRACKED AT ALL 6 NUT PLATE HOLES BETWEEN BS 1620 TO BS 1640, BL 0. REPLACED ANGLE AT BS 1620 TO BS 1640, BL 0 IAW B757 SRM 53-00-51.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,768 hrs · 32,574 cycles

MCN - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON HAT CHANNEL AT L-4 DOOR OPENING BS 1672 BETWEEN LBL 60 TO LBL 65. REPLACED HAT CHANNEL AT L-4 DOOR OPENING BS 1672 BETWEEN LBL 60 TO LBL 65 IAW B757 SRM 51-10-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 87,768 hrs · 32,574 cycles

MCN - C4 - MAJOR REPAIR - TOP ANGLE ON INTERCOSTAL CRACKED BETWEEN BS 1661 TO BS 1680, RBL 10. REPLACED TOP ANGLE ON INTERCOSTAL BETWEEN BS 1661 TO BS 1680, RBL 10 IAW B757 SRM 53-60-51.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,768 hrs · 32,574 cycles

MCN - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON HAT CHANNEL AT L-4 DOOR OPENING BS 1655 BETWEEN LBL 60 TO LBL 65. REPLACED HAT CHANNEL AT L-4 DOOR OPENING BS 1655 BETWEEN LBL 60 TO LBL 65 IAW B757 SRM 51-10-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 87,768 hrs · 32,574 cycles

MCN - C4 - MAJOR REPAIR - CRACK ON INTERCOSTAL ANGLE BETWEEN BS 1520 TO BS 1540, BL 0. REPLACED INTERCOSTAL ANGLE BETWEEN BS 1520 TO BS 1540, BL 0 IAW B757 SRM 53-00-51.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 87,768 hrs · 32,574 cycles

MCN - C4 - MAJOR REPAIR - 2 CRACKS ON STRINGER AT BS 1100, S14L. REPAIRED STRINGER AT BS 1100, S14L IAW EA 130440.

Part: SKIN — CRACKED (PYLON) · airframe 87,768 hrs · 32,574 cycles

MCN - C4 - MAJOR REPAIR - CRACK ON NR 2 PYLON INBOARD SKIN AT PPS179.25, WL 139. REPAIRED 2 PYLON INBOARD SKIN AT PPS179.25, WL 139 IAW EA 130434.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 87,768 hrs · 32,574 cycles

MCN - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON SUPPORT BETWEEN BS 1640 TO BS 1660, LBL 54. REPLACED SUPPORT BETWEEN BS 1640 TO BS 1660, LBL 54 IAW B757 SRM 51-40-02.

Part: SKIN — CRACKED (TE FLAP) · airframe 87,768 hrs · 32,574 cycles

MCN - C4 - MAJOR REPAIR - LEFT WING OUTBOARD AFT FLAP HAS A CRACK IN LOWER SKIN AT NR 1 FLAP TRACK AREA AT WBL 483.69 TO WBL 484.89. REPAIRED LEFT WING OUTBOARD AFT FLAP LOWER SKIN AT NR 1 FLAP TRACK AREA AT WBL 483.69 TO WBL 484.89 IAW B757 51-70-04 REPAIR 5.

Part: STOP FITTING — CRACKED (R2 DOOR) · airframe 87,768 hrs · 32,574 cycles

MCN - C4 - MAJOR REPAIR - CRACK ON R-2 DOOR STOP FITTING SECOND FROM THE BOTTOM AT BS 724. REPAIRED R-2 DOOR STOP FITTING SECOND FROM THE BOTTOM AT BS 724 IAW EA 130188A.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 87,768 hrs · 32,574 cycles

MCN - C4 - MAJOR REPAIR - CRACK ON INTERCOSTAL BETWEEN BS 820 TO BS 839, RBL 19. REPLACED INTERCOSTAL BETWEEN BS 820 TO BS 839, RBL 19 IAW B757 SRM 51-40-02.

Part: DUCT — LEAKING (RT ENGINE)

PHX FLT 429 EN ROUTE PHX TO OGG. THE RIGHT ENGINE WAS SHUT DOWN AT 23,000 FEET DURING CLIMBOUT DUE TO RIGHT ENGINE OVERHEAT CHECKLIST. RECEIVED STATUS MESSAGE RIGHT ENGINE STRUT DET NR 1 AT 20,000 FEET. THEN, OUT OF 22,000, ON CLIMBOUT, ENGINE OVERHEAT RIGHT ENGINE. FOLLOWED THE CHECKLIST WHICH REQUIRED ENGINE SHUTDOWN. THE FLIGHT RETURNED TO FIELD PHX AND LANDED WITHOUT FURTHER INCIDENT. SINGLE ENGINE FLIGHT TIME WAS 20 MINUTES. REPLACED LEAKING AIR DUCTS AT THE RIGHT ENGINE PRSOV. LEAK CHECKS OK.

Part: SLIDE — UNSERVICEABLE (L3 DOOR)

L3 DOOR SLIDER POINTER ON PRESSURE GAUGE IN LOWER RED. REMOVED AND REPLACED L3 EVAC SLIDE. REPAIRED AND CHARGED RESERVOIR AND VALVE ASSEMBLY, BY REPLACING AN O-RING AND PACKING BACKUP RETAINER FOR LEAKING.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

OGG - THE EMERGENCY FLASHLIGHT AT DOOR L1 WAS INOPERATIVE. REPLACED THE EMERGENCY FLASHLIGHT BATTERY AT L1 DOOR.

Part: SPRING — BROKEN (CAPTAIN SEAT)

KOA - CAPTAIN SEAT LATERAL ADJUSTMENT INOPERATIVE. TENSION SPRINGS FOR MANUAL FORWARD AND AFT CONTROL LEVER FOUND BROKEN. REPLACED BROKEN SPRINGS.

Part: PROXIMITY SWITCH — INOPERATIVE (R1 DOOR)

OGG - 1R SLIDE LIGHT NOT ILLUMINATING. MAINTENANCE REPLACED R1 FORWARD PRX SWITCH.

Part: ACCESS DOOR — MISSING (NR 1 ENGINE)

SFO - FLT 403 - EN ROUTE PHX TO SFO. PANEL ON INSIDE OF LEFT ENGINE CAME OFF ON DEPARTURE. THE FLIGHT CONTINUED TO SFO AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 1 ENG OIL SERVICE ACCESS DOOR.

Part: TERMINAL — LOOSE (CABIN)

PHX - THE EMERGENCY EXIT LIGHT ABOVE THE L1 DOOR WAS INOPERATIVE. TIGHTENED LOOSE TERMINAL IN CEILING PANEL.

Part: CONNECTOR — FAULTY (CABIN)

PHX - THE L1 DOOR EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE UPON TESTING. REPLACED CONNECTOR FOR L1 DOOR OVERHEAD EMERGENCY LIGHTS.

Part: BOTTLE — DISCHARGED (L1 DOOR)

PHX - THE L1 DOOR EMERGENCY ASSIST BOTTLE IS DOWN TO 0 PSI. REPLACED L1 DOOR EMERGENCY POWER RESERVOIR.

Part: WIRE — LOOSE (CABIN)

PHX - THE L1 DOOR OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE SECURED WIRE DISCONNECTS BEHIND THE LIGHT ASSEMBLY.

Part: PANEL — CRACKED (LE SLAT) · airframe 82,904 hrs · 31,542 cycles

MCN - C12 - MAJOR REPAIR - NR 9 SLAT COVE PANEL CRACKED INBOARD SIDE OF INBOARD MAIN TRACK. REPLACED NR 9 SLAT COVE PANEL IAW BOEING DRAWING 114N4076.

Part: SKIN — CORRODED (FUSELAGE) · airframe 82,904 hrs · 31,542 cycles

MCN - C12 - MAJOR REPAIR - CORROSION ON FUSELAGE SKIN AT MID LAV SERVICE COMPARTMENT AROUND FILL PORTS BS 1200, BETWEEN S29R TO S30R. REPAIRED FUSELAGE SKIN AT MID LAV SERVICE COMPARTMENT AROUND FILL PORTS BS 1200, BETWEEN S29R TO S30R IAW US AIRWAYS EA 130192.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 82,904 hrs · 31,542 cycles

MCN - C12 - MAJOR REPAIR - EXFOLIATION CORROSION ON RIGHT CREASE BEAM INNER CHORD AT BS 680, RBL 63. REPLACED RIGHT CREASE BEAM INNER CHORD AT BS 680, RBL 63 IAW B757 SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 82,904 hrs · 31,542 cycles

MCN - C12 - MAJOR REPAIR - CRACK ON STABILIZATION CHANNEL CLIP UPPER CHORD BETWEEN BS 860 TO BS 878, BL 0. REPLACED STABILIZATION CHANNEL CLIP UPPER CHORD BETWEEN BS 860 TO BS 878, BL 0 IAW B757 SRM 51-40-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 82,904 hrs · 31,542 cycles

MCN - C12 - MAJOR REPAIR - INTERCOSTAL ANGLE CRACKED ON UPPER CHORD BETWEEN BS 660 TO BS 672.5, BL 0. REPLACED INTERCOSTAL ANGLE UPPER CHORD BETWEEN BS 660 TO BS 672.5, BL 0 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 82,904 hrs · 31,542 cycles

MCN - C12 - MAJOR REPAIR - INTERCOSTAL UPPER CHORD CRACKED BETWEEN BS 487 TO BS 493, WL 208, RBL 10.75. REPLACED INTERCOSTAL UPPER CHORD BETWEEN BS 487 TO BS 493, WL 208, RBL 10.75 IAW B757 SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 82,904 hrs · 31,542 cycles

MCN - C12 - MAJOR REPAIR - ANGLE CRACKED BETWEEN BS 451 TO BS 455, WL 208, BL 0. REPLACED ANGLE BETWEEN BS 451 TO BS 455, WL 208, BL 0 IAW B757 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 82,904 hrs · 31,542 cycles

MCN C12 MAJOR REPAIR NR 6187584 EXFOLIATION CORROSION FLOOR BEAM CHORD AT BS324, WL208, RBL54. REPAIRED FLOOR BEAM CHORD AT BS324, WL208, RBL54 IAW US AIRWAYS EA NR 130185.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,904 hrs · 31,542 cycles

MCN - C12 - MAJOR REPAIR - EXFOLIATION CORROSION ON FLOOR CHANNEL SUPPORT AT BS 344 TO BS 364, RBL 58. REPLACED FLOOR CHANNEL SUPPORT AT BS 344 TO BS 364, RBL 58 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,904 hrs · 31,542 cycles

MCN - C12 - MAJOR REPAIR - GALVANIC CORROSION ON FLOOR SUPPORT AT L1 DOOR ENTRY BS 325 TO BS 344, RBL 58. REPLACED FLOOR SUPPORT AT L1 DOOR ENTRY BS 325 TO BS 344, RBL 58 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 82,904 hrs · 31,542 cycles

MCN - C12 - MAJOR REPAIR - EXFOLIATION CORROSION FLOOR SUPPORT BRACKET AT BS 365, RBL 53. REPAIRED FLOOR SUPPORT BRACKET AT BS 365, RBL 53 IAW B757 SRM 51-40-02.

Part: STRAP — CRACKED (FUSELAGE) · airframe 82,904 hrs · 31,542 cycles

MCN - C12 - MAJOR REPAIR - CRACK ON MAIN DECK FLOOR CHANNEL STRAP BETWEEN BS 365.25 TO BS 377.70, LBL 45.5. REPAIRED MAIN DECK FLOOR CHANNEL STRAP BETWEEN BS 365.25 TO BS 377.70, LBL 45.5 IAW B757 SRM 53-10-51.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 82,904 hrs · 31,542 cycles

MCN - C12 - MAJOR REPAIR - CRACK ON MAIN DECK FLOOR CHANNEL STRAP BETWEEN BS 365.25 TO 377.70, LBL 24.75. REPAIRED MAIN DECK FLOOR CHANNEL STRAP BETWEEN BS 365.25 TO 377.70, LBL 24.75 IAW B757 SRM 53-10-51.

Part: STIFFENER — CRACKED (RT PYLON) · airframe 82,904 hrs · 31,542 cycles

MCN - C12 - MAJOR REPAIR - RIGHT PYLON STIFFENER CRACKED AT PP STA 153.90 AT INBOARD END. REPLACED RIGHT PYLON STIFFENER AT PP STA 153.90 AT INBOARD END IAW B757 SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 82,904 hrs · 31,542 cycles

MCN - C12 - MAJOR REPAIR - CLIP CRACKED AT BS 1300, WL 206, LBL 50. REPLACED CLIP AT BS 1300, WL 206, LBL 50 IAW B757 SRM 51-40-02.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 82,904 hrs · 31,542 cycles

MCN N12 MAJOR REPAIR NR 6184171 INTERGRANULAR CORROSION MID LAV SERVICE PAN DOUBLER AT BS710 BETWEEN S20R TO S22R. REPLACED MID LAV SERVICE PAN DOUBLER AT BS710 BETWEEN S20R TO S22R IAW B757 SRM 51-40-02.

Part: PANEL — CRACKED (LE SLAT) · airframe 82,904 hrs · 31,542 cycles

MCN - C12 - MAJOR REPAIR - NR 9 SLAT COVE PANEL CRACKED ON RIGHT WING AT OUTBOARD TRACK. REPLACED NR 9 SLAT COVE PANEL AT OUTBOARD TRACK IAW B757 SRM 51-40-02.

Part: PANEL — CRACKED (LE SLAT) · airframe 82,904 hrs · 31,542 cycles

MCN - C12 - MAJOR REPAIR - NR 10 SLAT COVE PANEL CRACKED ON RIGHT WING AT OUTBOARD TRACK. REPLACED NR 10 SLAT COVE PANEL AT OUTBOARD TRACK IAW B757 SRM 51-40-02 & 51-40-04.

Part: STOP FITTING — CRACKED (R2 DOOR) · airframe 82,904 hrs · 31,542 cycles

MCN - C12 - MAJOR REPAIR - R2 DOOR AFT STOP FITTING CRACKED, SECOND FROM BOTTOM. REPLACED R2 DOOR AFT STOP FITTING IAW US AIRWAY EA 130188.

Part: FUSE — BLOWN (BATTERY PACK)

PHX THE LT HAND SEATS, ROWS 27 THROUGH 35, SEAT MOUNTED EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX REPLACED FUSE NR 1 IN BATTERY PACK SUPPLY. OPS CHECKS OK.

Part: POWER SUPPLY — DISCHARGED (CABIN)

PHX ALL SEAT MOUNTED LIGHTS AFT OF AFT LAVATORIES WERE FOUND INOPERATIVE. MX REPLACED THE EMERGENCY LIGHT POWER SUPPLY AT AFT GALLEY, LEFT HAND SIDE. OK FOR SERVICE.

Part: EPR SYSTEM — INOPERATIVE

PHX FLT 146 ENROUTE PHX TO LIH. THE FLIGHT REJECTED TAKE-OFF DUE TO NO EPR INDICATION AND AUTO THROTTLES WOULD NOT ENGAGE. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MX CYCLED THE THRUST MANAGEMENT COMPUTER (TMC) CIRCUIT BREAKER. PERFORMED BITE CHECK OF TMC AND EPR SYSTEMS. SYSTEMS TEST OK.

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

PHX FLT 146 - PHX TO LIH. ON DEPARTURE FROM PHX, THE CREW RECEIVED A 'LE SLAT DISAGREE' EICAS MESSAGE WITH A LEADING EDGE LIGHT ILLUMINATED. THE FLAPS INDICATOR REMAINED BETWEEN FLAPS UP AND FLAPS ONE POSITIONS. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NUMBER 13 SLAT ROTARY ACTUATOR DUE TO AN OVERTORQUED INDICATION. OPERATIONALLY CHECKS OK.

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

PHX FLT 146 - PHX TO LIH. ON DEPARTURE FROM PHX, THE CREW RECEIVED A 'LE SLAT DISAGREE' EICAS MESSAGE WITH A LEADING EDGE LIGHT ILLUMINATED. THE FLAPS INDICATOR REMAINED BETWEEN FLAPS UP AND FLAPS ONE POSITIONS. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NUMBER ONE SLAT ROTARY ACTUATOR DUE TO AN OVERTORQUED INDICATION. OPERATIONALLY CHECKS OK.

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

PHX FLT 146 PHX TO LIH. ON DEPARTURE FROM PHX, THE CREW RECEIVED A 'LE SLAT DISAGREE' EICAS MESSAGE WITH A LEADING EDGE LIGHT ILLUMINATED. THE FLAPS INDICATOR REMAINED BETWEEN FLAPS UP AND FLAPS ONE POSITIONS. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NUMBER 12 SLAT ROTARY ACTUATOR DUE TO AN OVERTORQUED INDICATION. OPERATIONALLY CHECKS OK.

Part: INDICATION SYS — MALFUNCTIONED (LT ENGINE)

PHX FLT 429 PHX TO OGG. ON TAKEOFF, THE LEFT ENGINE OVER TEMPED AT 871 AND FLUCTUATING. THE FLIGHT RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED EGT THERMOCOUPLE PROBE TEST, A DETAILED VISUAL INSPECTION OF CONNECTORS, AND A COMPRESSOR AIRFLOW TEST. ALL CHECKS OK.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

OGG - THE FLASHLIGHT WAS INOPERATIVE AT THE 1L DOOR. MAINTENANCE REPLACED THE BATTERY IN THE FLASHLIGHT AT THE 1L DOOR. OPERATIONALLY CHECKS OK.

Part: PROXIMITY SENSOR — FAULTY (L2 DOOR)

OGG - THE EMERGENCY SLIDE LIGHT AT DOOR 2L WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE GIRT BAR PROXIMITY SENSOR. OPERATIONALLY CHECKS OK.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

OGG - THE 2L DOOR FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IN THE FLASHLIGHT AT DOOR 2L. OPERATIONALLY CHECKS OK.

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

PHX - FLT 653 - EN ROUTE SNA TO PHX. DURING APPROACH, RECEIVED SLAT DISAGREE MESSAGE WHEN THE FLAPS WERE SELECTED TO 1 DEGREE. COMPLIED WITH APPROPRIATE PROCEDURES. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT WING, NR 3 LEADING EDGE SLAT ROTARY ACTUATOR. OPERATIONALLY CHECKS OK.

Part: TRANSCEIVER — FAILED (HF COMM)

PHX PHX-OGG FLT 432 - CREW STATED A/C HAD LOST ITS NUMBER 2 HF RADIO. RADIO WOULD NOT TRANSMIT AT ALL. TRIED TO RESET CB AND RADIO WOULD STILL NOT TRANSMIT. CAPT AND CONTROLLING DISPATCHER AGREE TO RETURN TO PHX. MAINTENANCE REPLACED NR 2 HF COMM TRANSCEIVER & PERFORMED SATISFACTORY OPS CHECK.

Part: POWER SUPPLY — DISCHARGED (CABIN)

SNA - MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHTING IN THE AFT OF AIRCRAFT INOPERATIVE ALONG WITH THE L4 DOOR ESCAPE SLIDE LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND POWER SUPPLY. OPERATIONAL CHECK OF LIGHTS GOOD.

Part: WIRE HARNESS — BROKEN (CABIN)

PHX - ROW 19L EMERGENCY LIGHT INOP. MAINTENANCE REMOVED & REPLACED WIRE HARNESS & EMERGENCY LIGHT ON ROW 19L. OPS CHECKS GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHTS)

MAINTENANCE FOUND EMERGENCY LIGHT AT SEAT ROW 19LH INOP. REPAIRED WIRING.

Part: TACH GENERATOR — FAILED · airframe 79,301 hrs · 30,659 cycles

FLT 146 PHX-LIH CREW STATES, CLIMBING FROM FL280 TO FL340, N3 BEGAN TO FLUCTUATE FROM 10% TO 93%, RIGHT DUCT PRESSURE FLUCTUATED FROM 0 TO 35, CABIN RATE FLUCTUATED BETWEEN 1000 UP AND 1000 DOWN, RIGHT CENTER FUEL PUMP PRESSURE LIGHT ILLUMINATED INTERMITTENTLY. ALL OTHER INDICATIONS NORMAL. MAINTENANCE REMOVED AND REPLACED N3 TACH GENERATOR, REMOVED AND REPLACED RT SPEED CARD.

Part: ANGLE — CRACKED (ZONE 200) · airframe 78,460 hrs · 30,450 cycles

MCN - MAJOR REPAIR - C-11 CHECK - NR 5988833, CRACKED CABIN INTERCOSTAL ANGLE, BS 180 - BS 1600, RBL 45.5, WL 208. REPLACED CABIN INTERCOSTAL ANGLE, BS 180 - BS 1600, RBL 45.5, WL 208 IAW B757-200 SRM 51-40-02.

Part: ATTACH FITTING — CORRODED (ZONE 200) · airframe 78,460 hrs · 30,450 cycles

MCN - MAJOR REPAIR - C-11 CHECK - NR 5988878, CORROSION ON THE L4 DOOR CUT LOWER SILL ATTACH CHANNEL CLIP, BS 1640, S17L, WL 208. REPLACED THE L4 DOOR CUT LOWER SILL ATTACH CHANNEL CLIP, BS 1640, S17L, WL 208 IAW B757-200 SRM 51-40-02.

Part: SKIN — DELAMINATED (RUDDER) · airframe 78,460 hrs · 30,450 cycles

MCN - MAJOR REPAIR - C-11 CHECK - NR 5988823 AND 5988924, RUDDER TRAILING EDGE HAS AREA OF DELAMINATION, RUDDER STATION 228.850, RUDDER STATION 233.852. REPAIRED RUDDER TRAILING EDGE, RUDDER STATION 228.850 - RUDDER STATION 233.852 IAW USAIRWAYS EA 120229.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 78,460 hrs · 30,450 cycles

MCN - MAJOR REPAIR - C-11 CHECK - NR 5988776, CRACKED CABIN SEAT TRACK, BS 1600, RBL 45.50, WL 208. REPLACED CABIN SEAT TRACK, BS 1600, RBL 45.50, WL 208 IAW B757-200 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 78,460 hrs · 30,450 cycles

MCN - MAJOR REPAIR - C-11 CHECK - NR 5988773, CORROSION ON CABIN FLOOR SUPPORT, BS 1660 - BS 1681.8, RBL 54, WL 208. REPLACED CABIN FLOOR SUPPORT, BS 1660 - BS 1681.8, RBL 54, WL 208 IAW B757-200 SRM 51-40-02.

Part: SLAT TRACK — CORRODED (ZONE 500) · airframe 78,460 hrs · 30,450 cycles

MCN - MAJOR REPAIR - C-11 CHECK - NR 5988782, CORROSION ON LEFT WING NR 2 SLAT OUTBOARD TRACK, SS 665.75. REPLACED LEFT WING NR 2 SLAT OUTBOARD TRACK, SS 665.75 IAW B757-200 AMM 27-81-13-4.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 78,460 hrs · 30,450 cycles

MCN - MAJOR REPAIR - C-11 CHECK - NR 5988769, CORROSION ON CABIN FLOOR SUPPORT, BS 1640 - BS 1660, RBL54 - RBL 55, WL 208. REPLACED CABIN FLOOR SUPPORT, BS 1640 - BS 1660, RBL54 - RBL 55, WL 208 IAW B757-200 SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 78,460 hrs · 30,450 cycles

MCN - MAJOR REPAIR - C-11 CHECK - NR 5988676, CRACKED STRINGER CLIP, BS 1220, S9L. REPLACED STRINGER CLIP, BS 1220, S9L IAW B757-200 SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 78,460 hrs · 30,450 cycles

MCN - MAJOR REPAIR - C-11 CHECK - NR 5988669, CRACKED DOOR CUT OUT SURROUND STRUCTURE "T" CLIP, BS 1681.8, S11R. REPLACED DOOR CUT OUT SURROUND STRUCTURE "T" CLIP, BS 1681.8, S11R IAW B757-200 SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (ZONE 200) · airframe 78,460 hrs · 30,450 cycles

MCN- MAJOR REPAIR - C-11 CHECK - NR 5988573, CRACK ON INTERCOSTAL ATTACHED ANGLE, BS 540 - BS 560, BL 0. REPLACED INTERCOSTAL ATTACHED ANGLE, BS 540 - BS 560, BL 0 IAW B757-200 SRM 51-40-02-0G, PAR 4B, FIG 3 AND 8.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 78,460 hrs · 30,450 cycles

MCN - MAJOR REPAIR - C-11 CHECK - NR 5988574, CRACKED INTERCOSTAL ANGLE, BS 660- BS 680, BL 0, WL 208. REPLACED INTERCOSTAL ANGLE, BS 660- BS 680, BL 0, WL 208 IAW B757-200 SRM 51-40-02.

Part: BRACKET — CRACKED (ZONE 200) · airframe 78,460 hrs · 30,450 cycles

MCN - MAJOR REPAIR - C-11 CHECK - NR 5988668, CRACK ON INTERCOSTAL SUPPORT CLIP, BS 1600, S-6L. REPLACED INTERCOSTAL SUPPORT CLIP, BS 1600, S-6L IAW B757-200 SRM 51-40-02-0G, FIG 8 AND 12.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 78,460 hrs · 30,450 cycles

MCN- MAJOR REPAIR - C-11 CHECK - NR 5988361, CRACK ON FUSELAGE FRAME SHEAR TIE, BS 1459, S-28R - S-29R. REPLACED FUSELAGE FRAME SHEAR TIE, BS 1459, S-28R - S-29R IAW BOEING DWG 140N2002 AND B757-200 SRM 51-30-01-06, FIG 3, 7, 8, 9.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 78,460 hrs · 30,450 cycles

MCN - MAJOR REPAIR - C-11 CHECK - NR 5988360, CRACK ON FUSELAGE FRAME SHEAR TIE, BS 1459, S-29R - S-30R. REPLACED FUSELAGE FRAME SHEAR TIE, BS 1459, S-29R - S-30R IAW BOEING DWG 140N2002 AND B757-200 SRM 51-30-01-06, FIG 3, 7, 8, AND 9.

Part: SKIN — CRACKED (ZONE 600) · airframe 78,460 hrs · 30,450 cycles

MCN - MAJOR REPAIR - C-11 CHECK - NR 5988280, RIGHT WING NR 10 SLAT COVE SKIN CRACKED, OSS 797.46 - OSS 809.46. REPLACED RIGHT WING NR 10 SLAT COVE SKIN, OSS 797.46 - OSS 809.46 IAW B757-200 SRM 51-40-02.

Part: SKIN — CRACKED (ZONE 500) · airframe 78,460 hrs · 30,450 cycles

MCN - MAJOR REPAIR - C-11 CHECK - NR 5988286, LEFT WING NR 2 SLAT COVE SKIN CRACKED, OSS 691. REPLACED LEFT WING NR 2 SLAT COVE SKIN, OSS 691 IAW B757-200 SRM 51-40-02.

Part: STOP FITTING — CRACKED (ZONE 200) · airframe 78,460 hrs · 30,450 cycles

MCN - MAJOR REPAIR - C-11 CHECK - NR 5988104, CRACKED STOP FITTING, R2 DOOR, BS 726.50, RBL 78, WL 227. REPLACED STOP FITTING, R2 DOOR , BS 726.50, RBL 78, WL 227 IAW USAIRWAYS EA 120230.

Part: SKIN — CRACKED (ZONE 500) · airframe 78,460 hrs · 30,450 cycles

MCN - MAJOR REPAIR - C-11 CHECK - NR 5988285, LEFT WING NR 2 SLAT COVE SKIN CRACKED, OSS 665.50 - OSS 677.50. REPLACED LEFT WING NR 2 SLAT COVE SKIN, OSS 665.50 - OSS 677.50 IAW B757-200 SRM 51-40-02.

Part: SKIN — CRACKED (ZONE 500) · airframe 78,460 hrs · 30,450 cycles

MCN - MAJOR REPAIR - C-11 CHECK - NR 5988289, LEFT WING NR 3 SLAT COVE SKIN CRACKED, OSS 542.70 - OSS 573.30. REPLACED LEFT WING NR 3 SLAT COVE SKIN, OSS 542.70 - OSS 573.30 IAW B757-200 SRM 51-40-02.

Part: DISPLAY — FAILED (COCKPIT) · airframe 75,808 hrs · 29,747 cycles

PHX - DURING CRUISE, CREW REPORTED THAT THE UPPER DISPLAY UNIT FAILED. THE CREW DECLARED AND EMERGENCY AND RETURNED TO PHX. THE PAX DID NOT BRACE, THE LANDING WAS UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED BOTH EICAS DISPLAY UNITS AND REPAIRED A BROKEN WIRE. EICAS DISPLAYS OPS CHECK WAS GOOD PER T/C R1B31602. THE AIRCRAFT WAS RETURNED TO SERVICE. DISPLAY - P/N - 622-7999-003 - S/N 2399 - TSR - 68515.

Part: LINE — CHAFED (HYDRAULIC SYS) · airframe 74,692 hrs · 29,478 cycles

PHX - ATB - FLT - 920 - LOG 7288157 - AIRCRAFT LOST LEFT HYDRAULIC SYSTEM QUANTITY/PRESSURE. AIRCRAFT RETURNED TO PHX. THE LANDING WAS UNEVENTFUL. MAINTENANCE DISCOVERED A HYDRAULIC LINE IN THE LEFT HAND PYLON AREA HAD BEEN CHAFED THREW BY A CLAMP. MAINTENANCE REPLACED THE LINE.

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

PHX FLT 146 - PHX TO LIH. ON DEPARTURE FROM PHX, THE CREW RECEIVED A 'LE SLAT DISAGREE' EICAS MESSAGE WITH A LEADING EDGE LIGHT ILLUMINATED. THE FLAPS INDICATOR REMAINED BETWEEN FLAPS UP AND FLAPS ONE POSITIONS. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NUMBER TWO SLAT ROTARY ACTUATOR DUE TO AN OVERTORQUED INDICATION. OPERATIONALLY CHECKS OK.

Part: BUSHING — MISSING (GIRT BAR) · airframe 73,985 hrs · 29,318 cycles

MAINTENANCE REPORTED THAT THE GIRT BAR ENGAGE CRANK ROD CONTACTS CAM DURING DOOR OPERATION AND THAT IT APPEARED TO BE MISSING A SPACER ON BUSHING AT THE R-1 DOOR. MAINTENANCE INSTALLED MISSING BUSHING ON EMERGENCY BELL CRANK MECHANISM PER IPC 52-11-20. OPERATIONAL CHECKS WERE GOOD.

Part: SWITCH — SHEARED (R1 DOOR) · airframe 73,669 hrs · 29,246 cycles

PHX - EES - DURING OVERNIGHT MAINTENANCE DISCOVERED THE R-1 EMERG DOOR ASSIST TRIGGER SHEARED OFF. MAINTENANCE REMOVED AND REPLACED THE R1 EMERGENCY EXIT DOOR ASSIST TRIGGER IAW BOEING 757-200 MM 52-11-32-404-010.

Part: SKIN — CRACKED (TE FLAP) · airframe 93,648 hrs · 29,237 cycles

GYR - DURING C10 CHECK DISCOVERED THE LT OUTBOARD TRAILING EDGE FLAP HAD HAIRLINE CRACKS IN THE END POTTING COMPOUND. MAINTENANCE CLEANED AREA ON THE LT OUTBOARD TRAILING EDGE FLAP IAW AWA ER NR 19-2750-06075-RC1. FILLED INBOARD AND OUTBOARD EDGES ON THE LT OUTBOARD TRAILING EDGE FLAP WITH SEALANT BMS 5-95 B1/2 IAW AWA ER NR 19-2750-06075-RC1.

Part: BEAR STRAP — CORRODED (BS 460) · corrosion level 2 · airframe 73,648 hrs · 29,327 cycles

GYR - DURING C10 CHECK DISCOVERED LEVEL 2 CORROSION ON LOWER FUSELAGE SKIN AT BS 460, WL 148 AND STR 30R ON THE MEC BAY DOOR FORWARD INTERNAL DOUBLER. MAINTENANCE REMOVED CORROSION AND FOUND TO BE BEYOND SRM LIMITS. FABRICATED REPAIR DOUBLER IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NO. 19-5360-06055-RC1. INSTALLED FABRICATED REPAIR PARTS AT BS 460,WL 148 AND STR 30R IAW AWA ER NO. 19-5360-06055-RC1.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 73,648 hrs · 29,237 cycles

GYR - DURING C10 DISCOVERED LT TRAILING EDGE FLAP, AFT FLAP AREA, DISBOND AT THE INBOARD END, UPPER SURFACE AT WBL 71.0L. MAINTENANCE REMOVED DELAMINATED PREVIOUS REPAIR PLY, CLEANED AND PREPPED AREA FOR BONDING OF REPLACEMENT REPAIR PLIES IAW BOEING 757-200 SRM 51-70-17. APPLIED REPAIR PLIES AND BONDED TO THE LT TRAILING EDGE FLAP, UPPER SURFACE, AT WBL 71.0L IAW BOEING 757-200 SRM 51-70-17-0G.

Part: LIGHT — INOPERATIVE (ROW 21) · airframe 73,601 hrs · 29,223 cycles

PHX - EEL - DURING OVERNIGHT MAINTENANCE DISCOVERED THE EMERGENCY ESCAPE PATH LIGHT AT ROW 21 LEFT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT AT ROW 21L IAW BMM 33-51-00. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 73,195 hrs · 29,057 cycles

SEA - EEL - DURING OVERNIGHT CHECK, MAINTENANCE FOUND EMERGENCY FLASHLIGHT AT RT MID CABIN FLIGHT ATTENDANT STATION INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT MID CABIN FLIGHT ATTENDANT FLASHLIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY PACK — FAULTY (EMERGENCY EXIT) · airframe 71,590 hrs · 28,358 cycles

PHX - EEL - DURING 4-DAY CHECK, THE LT EMERGENCY EXIT EXTERIOR SLIDE LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IAW B757 MM 33-51-07. OPERATIONAL CHECK WAS GOOD.

Part: SWITCH — FAULTY (CABIN) · airframe 70,101 hrs · 27,704 cycles

JFK - EEL - DURING 8-DAY CHECK, THE L-4 AND R-4 DOOR EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT TEST SWITCH AT AFT FLIGHT ATTENDANT PANEL BS 1640 LT, OPERATIONAL CHECK WAS GOOD.

Part: CHARGER — FAULTY (EMERGENCY LIGHT) · airframe 70,074 hrs · 27,696 cycles

PHX - EEL - DURING 4-DAY CHECK, EMERGENCY ESCAPE PATH LIGHTS BETWEEN SEAT ROWS 27 AND 35 LT WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER AND BATTERY AT BS 1650, OPERATIONAL CHECK WAS GOOD.

Part: FLASHLIGHT — DISCHARGED (ZONE 900) · airframe 69,846 hrs · 27,605 cycles

FLIGHT CREW REPORTED THE LT FORWARD ENTRY WAY EMERGENCY FLASHLIGHT HAD A LOW BATTERY. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLASHLIGHT ASSEMBLY AT THE LT FORWARD ENTRY WAY, OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (ZONE 800) · airframe 69,463 hrs · 27,447 cycles

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

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,561 hrs · 27,043 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT SHEAR DECK LOWER SUPPORT ANGLE AT BS 1718, RBL 40. MAINTENANCE REMOVED CORRODED AFT SHEAR DECK LOWER SUPPORT ANGLE AT BS 1718, RBL 40; FABRICATED A NEW REPLACEMENT ANGLE AND INSTALLED REPAIR PART IAW DWG 146N5240-23.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,561 hrs · 27,043 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT SHEAR DECK LOWER SUPPORT ANGLE AT BS 1701, LBL 45. MAINTENANCE REMOVED CORRODED AFT SHEAR DECK LOWER SUPPORT ANGLE AT BS 1701, LBL 45; FABRICATED A NEW REPLACEMENT ANGLE AND INSTALLED REPAIR PART IAW DWG 146N5300-22.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,561 hrs · 27,043 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT SHEAR DECK LOWER SUPPORT ANGLE AT BS 1701, RBL 45. MAINTENANCE REMOVED CORRODED AFT SHEAR DECK LOWER SUPPORT ANGLE AT BS 1701, RBL 45; FABRICATED A NEW REPLACEMENT ANGLE AND INSTALLED REPAIR PART IAW DWG 146N5300.

Part: ANGLE — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 68,561 hrs · 27,043 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT SHEAR DECK LOWER SUPPORT ANGLE AT BS 1718, LBL 48. MAINTENANCE REMOVED CORRODED AFT SHEAR DECK LOWER SUPPORT ANGLE AT BS 1718, LBL 48; FABRICATED A NEW REPLACEMENT ANGLE AND INSTALLED REPAIR PART IAW DWG 146N5240-7.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,561 hrs · 27,043 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER FORWARD FLANGE OF FLOORBEAM AT BS 1681, RBL 32. MAINTENANCE CUT OUT DAMAGE ON FLOORBEAM AT BS 1681, RBL 32; FABRICATED 2 EACH ANGLES AND STRAPS; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-51 FIG 202.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,561 hrs · 27,043 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT SHEAR DECK AT BS 1715 FROM BL 0 TO LBL 48. MAINTENANCE CUT OUT DAMAGE ON AFT SHEAR DECK AT BS 1715 FROM BL 0 TO LBL 48; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-60-51 FIG 203 PG 204-208.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,561 hrs · 27,043 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT SHEAR DECK BETWEEN BS 1681 AND BS 1720 LBL 50. MAINTENANCE CUT OUT DAMAGE ON AFT SHEAR DECK FROM BS 1681 AND BS 1720 LBL 50; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-60-51 FIG 203 PG 204-208.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,561 hrs · 27,043 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON AFT SHEAR DECK AT BS 1681 FROM BL 0 TO RBL 48. MAINTENANCE REMOVED CORRODED AFT SHEAR DECK AT BS 1681 FROM BL 0 TO RBL 48; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-60-51 FIG 203 PG 204-208.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,561 hrs · 27,043 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT SHEAR DECK UNDER G4B GALLEY BETWEEN BS 1681 AND BS 1725, RBL 50. MAINTENANCE CUT OUT DAMAGE ON AFT SHEAR DECK FROM BS 1681 TO BS 1725, RBL 50; FABRICATED A FILLER AND REPAIR DOUBLER; INSTALLED REPAIR PARTS IAW B757-200 SRM 53-60-51 FIG 203 PG 204-208.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,561 hrs · 27,043 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON MAIN CABIN AFT SHEAR DECK UNDER G4B GALLEY AT BS 1715, BL 0 TO RBL 48. MAINTENANCE CUTOUT DAMAGE ON AFT SHEAR DECK BS 1715, BL 0 TO RBL 48; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B757-200 SRM 53-60-51, FIG 203 PG 204-208.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,561 hrs · 27,043 cycles

LCQ - MAJOR REPAIR - DURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND ON UPPER SURFACE OF AFT SHEAR DECK AT BS 1681 FROM BL 0 TO LBL 48. MAINTENANCE CUTOUT DAMAGE ON AFT SHEAR DECK AT BS 1681 FROM BL 0 TO LBL 48; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PART IAW B757-200 SRM 53-60-51 FIG 203 PG 204-208.

Part: PRESSURE SWITCH — DEFECTIVE (NR 1 ENGINE) · airframe 67,766 hrs · 26,694 cycles

AFTER TAKEOFF AT PHX EN ROUTE FOR MSP RECEIVED EICAS MESSAGE -L ENG ANTI-ICE- WITH NR 1 ENGINE ANTI-ICE VALVE LIGHT ILLUMINATED. DUE TO ICING CONDITIONS AT MSP TURNED BACK TO PHX FOR REPAIR. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE ANTI-ICE VALVE, DID NOT CORRECT THE PROBLEM, REPLACED ENGINE ANTI-ICE LOW PRESSURE SWITCH IAW BMM 30-21-01. PERFORMED ENGINE RUN, ANTI-ICE VALVE OPERATED NORMALLY, NO LIGHT OR EICAS MESSAGES NOTED. FUNCTIONAL TEST OF ANTI-ICE LOW PRESSURE SWITCH S/N TR565 WAS NO FAULT FOUND, INSULATION, LEAKAGE, AND CALIBRATION TESTS WERE GOOD.

Part: LIGHT — BROKEN (SEAT ROW 16 LT) · airframe 67,764 hrs · 26,693 cycles

DURING INSPECTION EMERGENCY ESCAPE PATH LIGHT LENS AT SEAT ROW 16 LT WAS FOUND MISSING. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 LT, OPERATIONAL CHECK WAS GOOD.

Part: LIGHT — INOPERATIVE (SEAT ROW 14) · airframe 67,385 hrs · 26,552 cycles

PHX - EEL - DURING A-03 CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLE AT SEAT ROW 14 LT, OPERATIONAL CHECK WAS GOOD.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 67,009 hrs · 26,391 cycles

PHX - EEL - DURING INSPECTION FOUND AN INTERMITTENT EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 23 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 23 LT, OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 67,009 hrs · 26,391 cycles

PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE EMERGENCY FLASHLIGHT AT L-2 DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERIES IN THE L-2 DOOR EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.

Part: WIRE — BROKEN (SEAT ROW 7) · airframe 65,597 hrs · 25,835 cycles

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

Part: RESERVOIR — DISCHARGED (ESCAPE SLIDE) · airframe 65,490 hrs · 25,792 cycles

PHX - EES - FLT 0046 - L-2 DOOR EMERGENCY SLIDE PULLED FROM BONNET WITH GIRT STILL ATTACHED, ASSIST BOTTLE DISCHARGED AND SLIDE HANDLE FOUND ENGAGED. MAINTENANCE REINSTALLED L-2 DOOR SLIDE IAW BMM 25-66-01-404. REMOVED AND REPLACED DOOR ASSIST BOTTLE IAW BMM 52-11-30-4, OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 64,352 hrs · 25,280 cycles

DURING C-08 CHECK THE EMERGENCY FLASHLIGHT AT THE L-2 DOOR FLIGHT ATTENDANT SEAT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT BATTERY AT THE L-2 DOOR FLIGHT ATTENDANT SEAT IAW BMM 25-60-00, PG. 1, AND AW2560010.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 64,350 hrs · 25,279 cycles

LCQ - MAJOR REPAIR - DURING C-08 CHECK 1 1/2" CRACK WAS FOUND ON FLOOR SUPPORT OF MAIN EQUIPMENT CENTER COMPARTMENT AT BS 460, BETWEEN STR 24 & 26R. MAINTENANCE REMOVED DAMAGED FLOOR SUPPORT AT BS 460 BETWEEN STR 24 & 26R; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; AND INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, PG. 3-4.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 64,350 hrs · 25,279 cycles

DURING C-08 CHECK A 1 3/4 INCH CRACK WAS FOUND ON AFT CARGO COMPARTMENT SIDEWALL SUPPORT ANGLE AT BS 1630, STR 21 RT. MAINTENANCE REMOVED DAMAGED AFT CARGO COMPARTMENT SIDEWALL SUPPORT ANGLE AT BS 1630, STR 21 RT; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE; AND INSTALLED REPAIR PART IAW B757-200 SRM 51-70-13, FIG. 1, PG. 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,350 hrs · 25,279 cycles

DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER CAP OF CABIN FLOORBEAM BS 377.5, LBL 55. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED SECTION OF FLOORBEAM AT BS 377.5, LBL 55; FABRICATED 2 EACH ANGLES, A STRAP, A FILLER, AND A SHIM; AND INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-51, PG. 216-218, FIG. 205.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,350 hrs · 25,279 cycles

LCQ - MAJOR REPAIR - DURING C-08 CHECK INTERGRANULAR CORROSION WAS FOUND ON UPPER SURFACE AND BASE OF FLOOR SUPPORT ANGLE AT BS 365.5, RBL 50. MAINTENANCE REMOVED NUTPLATES AND BLENDED CORROSION; REMOVED GALLEY SUPPORT ANGLE, AND HAT CHANNEL SUPPORT ANGLE BENEATH GALLEY SUPPORT ANGLE AT BS 365.5, RBL 5, FOR FURTHER INSPECTION; MATERIAL LOSS WITHIN LIMITS ON GALLEY SUPPORT ANGLE; MATERIAL LOSS OUT OF LIMITS ON HAT CHANNEL SUPPORT ANGLE; FABRICATED A NEW REPLACEMENT HAT CHANNEL SUPPORT ANGLE PER DWG 141N5186; AND INSTALLED REPAIR PART AND GALLEY SUPPORT ANGLE IAW B757-200 SRM 51-40-02, PG. 16-17.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,350 hrs · 25,279 cycles

LCQ - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON CABIN FLOOR SUPPORT HAT CHANNEL BS 375, LBL 55. MAINTENANCE BLENDED CORROSION AND FOUND MATERIAL LOSS BEYOND LIMITS; REMOVED DAMAGED FLOOR SUPPORT AT BS 375, LBL 55; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; AND INSTALLED REPAIR PART IAW DWG 141N5170, AND B757-200 SRM 51-40-01, PG. 3.

Part: WEB — CORRODED · corrosion level 2 · airframe 64,350 hrs · 25,279 cycles

LCQ - MAJOR REPAIR - DURING C-08 CHECK EXFOLIATION CORROSION WAS FOUND ON WEB IN MAIN CABIN BS 1375, RBL 69. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED WEB AT BS 1375, RBL 69; FABRICATED A NEW REPLACEMENT WEB; AND INSTALLED REPAIR PART IAW DWG 146N8322, AND B757-200 SRM 51-40-02, PG. 3-5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 64,350 hrs · 24,279 cycles

LCQ - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON CABIN FLOOR SUPPORT AT BS 330, RBL 11 TO RBL 39. MAINTENANCE REMOVED DAMAGED FLOOR SUPPORT AT BS 330 FROM BL O TO RBL 24; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT PER DWG 141N5160; AND INSTALLED REPAIR PART IAW B757-200 SRM 51-40-02, PG. 4, 16-17, 39-40.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,350 hrs · 25,279 cycles

LCQ - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON CABIN GALLEY FLOOR SUPPORT BS 400, RBL 53. MAINTENANCE REMOVED DAMAGED FLOOR SUPPORT AT BS 400, RBL 53; FABRICATED A NEW REPLACEMENT GALLEY FLOOR SUPPORT; AND INSTALLED REPAIR PART IAW DWG 141N5186, AND B757-200 SRM 51-40-02, PG. 4.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,350 hrs · 25,279 cycles

DURING C-08 CHECK A 3/4 INCH CRACK WAS FOUND ON UPPER FLOORBEAM "T" CAP AT SEAT TRACK ATTACH POINT BS 700, RBL 46. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOORBEAM AT BS 700, RBL 46, AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM, 2 EACH SUPPORT ANGLES, 2 EACH REINFORCEMENT STRAPS, A RADIUS FILLER, AND A CLIP; AND INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-51, PG. 201-205, FIG. 201.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,350 hrs · 25,279 cycles

DURING C-08 CHECK A 2 INCH CRACK WAS FOUND ON UPPER FLOORBEAM "T" CAP AT SEAT TRACK ATTACH POINT BS 700, RBL 25. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOORBEAM AT BS 700, RBL 25, AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A NEW REPLACEMENT SECTION OF FLOORBEAM, 2 EACH SUPPORT ANGLES, 2 EACH REINFORCEMENT STRAPS, A RADIUS FILLER, AND A CLIP; AND INSTALLED REPAIR PARTS IAW B757-200 SRM 53-00-51, PG. 201-205, FIG. 201.

Part: SKIN — DELAMINATED (LT WING LE) · airframe 64,350 hrs · 25,279 cycles

DURING C-08 CHECK REPAIR OF DELAMINATED AREA OF LT WING LEADING EDGE REQUIRED TO TERMINATE MONITOR. WS 106 TO WS 169 LT. MAINTENANCE REMOVED PREVIOUS REPAIR AND CUTOUT A 11 X 6.5 INCH DELAMINATED AREA OF LT INBOARD FIXED WING LEADING EDGE AT WS 106 TO WS 169; APPLIED FIBERGLASS REPAIR AND CONDUCTIVE COATING PER B757-200 SRM 51-70-08, FIG. 5, PARA 4.A.

Part: SEAL — CONTAMINATED (BLEED SOLENOID) · airframe 64,188 hrs · 25,211 cycles

EXHAUST DAMAGE - DURING WALK AROUND INSPECTION A LARGE SECTION OF HONEYCOMB FOUND MISSING AT RT ENGINE LT COWLING HEAT DAMAGE TO NR 2 ENGINE C-DUCT WAS DUE TO DEFECTIVE HIGH PRESSURE SOLENOID BLEED VALVE. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE LT HIGH PRESSURE BLEED VALVE ON BOTH THE LT AND RT BLEED SOLENOIDS. NR 2 ENGINE INBOARD C-DUCT WAS REPLACED. IP & HP COMPRESSOR AIRFLOW CONTROL TEST CHECKED GOOD. VENDOR BENCH TEST OF BLEED SOLENOID RELIEF HP3 VALVE FAILED FUCNTIONAL TEST AND INLET / EXHAUST VALVE LEAKAGE TEST AT 15 LBS. UNIT WAS DISASSEMBLED AND FOUND TO BE CONTAMINATED WITH A CARBON MATERIAL. TRIPLE SEALS ALSO CONTAMINATED WITH AN ABRADABLE MATERIAL, AND THE RELIEF VALVE SEALING SURFACE WAS DAMAGE

Part: SLAT — DELAMINATED · corrosion level 0 · airframe 63,909 hrs · 25,098 cycles

LCQ - MAJOR REPAIR - APPROXIMATELY 12" OF TRAIL EDGE WEDGE HAS SKIN AND CORE DAMAGE ON # 6 LEADING EDGE SLAT. REMOVED #6 LEADING EDGE SLAT; CLEANED, PREPARED, AND REPLACED TRAILING EDGE WEDGE IAW E.O. 57-55-10. REINSTALLED # 6 LEADING EDGE SLAT IAW BMM 27-81-01, PG. 401-422.

Part: WIRE — BROKEN (SEAT ROW 22 L/H) · corrosion level 0 · airframe 63,239 hrs · 24,833 cycles

PHX - EEL - DURING INSPECTION OF EMERGENCY ESCAPE PATH LIGHTING THE SEAT LIGHT AT SEAT ROW 22 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT THE LIGHT ASSEMBLY, SEAT ROW 22 L/H, OPERATIONAL CHECK WAS GOOD.

Part: CABLE — OUT OF ADJUST (L4 DOOR) · airframe 62,719 hrs · 24,624 cycles

PHX - EMERGENCY ESCAPE SYS - POST FLT L4 DOOR DID NOT DEACTIVATE FROM EMERGENCY OPERATION WHEN CATERING OPENED THE DOOR FROM THE OUTSIDE. THE DOOR ASSIST RESERVOIR DISCHARGED PRIOR TO THE DOOR ROTATING OUT AND BOTH THE LOWER LINER PANEL AND SLIDE COVER CAUGHT ON THE GATE AND WERE DAMAGED. SLIDE DID NOT DEPLOY. MX INSTALLED THE DOOR ASSIST RESERVOIR SAFETY PIN AND TROUBLESHOT L4 DOOR FINDING DOOR DISARM CABLE WAS OUT OF ADJUSTMENT.

Part: FLOORBEAM — CORRODED (FUSELAGE)

FS 365 BL 0 TO RBL 60 FOUND SURFACE CORROSION ON UPPER T-CAP AT FLOORBEAM. REMOVED DAMAGED T-CAP, FABRICATED NEW T-CAP AND INSTALLED PER SRM 53-0051 FIG 203 SH 2.

Part: FLOOR SUPPORT — CORRODED (STA 330-360)

D: corrosion on top surface of floor structure, FS 350 BL 00C: Removed damaged section of floor support from STA 330 to STA 360 BL0 fabricated installed repair per SRM 51-70-11 fig 1 pg 1

Part: SKIN — DAMAGED (FUSELAGE)

CREASE IN FUSELAGE EXTERIOR SKIN AT BS 456 STR L-17. REMOVED DAMAGED SECTION OF SKIN. FABRICATED AND INSTALLED REPAIR PER ER 19-5331-01172-KB1.

Part: SKIN — CRACKED (LT.WS.797)

D: L/H Wing Leading Edge Slat #1 cracked In the Cove Skin At W.S. 797C: Repaired #1 Slat Per SRM 51-70-13 Fig 1 Pg 1

Part: WEB — CORRODED

D: Aft galley shear web corroded F$ 1715 at RBL 14 to LBL 51C Removed corrosion, fabricated and installed repair doublers at F5 1715 LBL 17-34 and RBL 14-23 Per SRM 53-60-51 fig 203 and SRM 51-40-02

Part: DOOR FRAME — DENTED (CARGO DOOR)

FWD cargo door FWD LWR corner frame dented. removed damaged FWD cargo door FWD LWR frame corner IAW SRM 51-40-2; installed customer supplied p/n 143N6618-6 R844567 IAW SRM 51-40-2.

Part: HYDRAULIC LINE — LEAKING (LT MLG) · airframe 59,941 hrs · 23,535 cycles

PHX - EMERGENCY LANDING - 3/28/01 - ON FINAL APPROACH INTO PHX THE AIRCRAFT LOST LEFT HYDRAULIC SYSTEM PRESSURE AND QUANTITY; THE AIRCRAFT LANDED W/O INCIDENT. MAINTENANCE FOUND THE LT MAIN LANDING GEAR DOWNLOCK ACTUATOR LINE LEAKING AND REPLACED IT; NO OTHER LEAKS WERE FOUND.

Part: RELAY — MALFUNCTIONED (LT ENGINE)

PHX - AIR TURNBACK - ENROUTE FROM PHX TO BWI THE CREW GOT EICAS STATUS MESSAGE L ENG PROBE HEAT; DUE TO ICING CONDITIONS THE A/C RETURNED TO PHX. MAINTENANCE TROUBLESHOT IAW FIM 30-34-00 AND REPLACED THE FOLLOWING RELAYS: K178, K10107, K10337 (ALL P/N BACR13CG2A) AND K10478 (P/N 770-540-1); THE MESSAGE CLEARED AND FUNCTIONAL CHECKS WERE NORMAL.

Part: UNKNOWN — ODOR (LAVATORY) · airframe 57,555 hrs · 22,516 cycles

FLIGHT ATTENDANT REPORTED FOUL LAVATORY ODOR IN AFT OF AIRCRAFT AFTER ENGINE START. DURING FLIGHT, ODOR COULD BE SMELLED THROUGHOUT THE AIRCRAFT. ALSO, SMELLED IN FLIGHT DECK FOR THE FIRST TWO HOURS OF FLIGHT. FOUND THE FORWARD LAV DUMP HANDLE TY-WRAPPED CLOSED. FIRST CLASS LAV DID HAVE BAD ODOR. SERVICED ALL LAVATORIES. PERFORMED OVERBOARD EXHAUST VALVE TEST PER 21-58-00. EXHAUST VALVE TESTED NORMAL.

Part: FAN — FAILED (E/E BAY) · airframe 57,013 hrs · 22,280 cycles

ACRID ELECTRICAL ODOR DETECTED IN CABIN AND FLIGHT DECK. DECLARED EMERGENCY AND DIVERTED TO NEAREST SUITABLE AIRFIELD. T/S SYS AND FOUND RT RECIRC FAN INOPERATIVE AND BURNT. REPLACED RT RECIRC FAN, OPS CHECKED GOOD. RECOMMENDATION: REMAIN OPEN PENDING REVIEW OF TEARDOWN REPORT.

Part: OVEN — DIRTY (GALLEY)

NR 3 OVEN IN AFT GALLEY SMOKES WHEN HEATED. CLEANED NR 3 OVEN.

Part: FRAME — CRACKED (BS600)

FWD CARGO FS 600 BETWEEN STR 24L AND 26L FRAME IS CRACKED IN UPPER FLANGE. REMOVED DAMAGED SECTION OF FRAME BS 600 BETWEEN 24L-26L. FABRICATED AND INSTALLED REPLACEMENT FRAME SECTION AND SPLICE CHANNEL IAW 53-00-07 FIG 201.

Part: FRAME — CRACK (BS 1340)

FRAME DENTED AND CRACKED JUST BELOW FACTORY SPLICE AT STA 1340 STR 23R. TRIMMED OUT DAMAGED FRAME IAW SRM 53-00-07 FIG 201. FABRICATED REPAIR PARTS PER SRM 53-00-07, 7075-0 .071 R710334. ALODINED AND PRIMED CUTOUT IAW SRM 51-20-01. INSTALLED REPAIR PART AND ACCESS TREATED WITH LPS3.

Part: ANGLE — CRACKED (BS 660)

INTERCOSTAL CRACKED AT RADIUS AT RT STA 660 AND RBL 26. REMOVED AND FABRICATED INTERCOSTAL FWD ATTACH ANGLE PER SRM 53-30-51. INSTALLED IAW SRM 53-00-51 FIG 20.

Part: FRAME — CRACKED (BS 600)

FRAME CRACKED IN UPPER FLANGE OF FWD CARGO DOOR CUTOUT FS 600 BETWEEN STR 24L AND 26 L. REMOVED DAMAGED SECTION OF FRAME IAW SRM 53-00-07 FIG 201, FABRICATED REPLACEMENT FRAME SECTION AND SPLICE CHANNEL IAW SRM 53-00-07 FIG 201. INSTALLED REPLACEMENT FRAME SECTION AND INSTALLED REPLACEMENT PART IAW 53-00-07.

Part: FRAME — CRACKED (BS 1340)

STA 1340 STR 23R JUST BELOW FACTORY SPLICE, FRAME DENTED AND CRACKED. CUT OUT DAMAGED AREA AT STA 1340 BETWEEN 23-24 R PER SRM 53-00-07 FIG 201. ALODINED AND PRIMED CUTOUT IAW SRM 51-20-01 AND AMM 51-21. INSULATION AND PANEL INSTALLED PER 20-12-00.

Part: TPU — FAILED (NR 2 ENGINE)

ENGINE SHUTDOWN, NUMBER 2 ENGINE FLAMED OUT DURING DESCENT. EICAS MESSAGE APPEARED NR 2 ENGINE LOW PRESSURE PUMP. FOM PROCEDURE COMPLIED WITH. PRECAUTIONARY INSPECTIONS COMPLIED WITH. BITE TEST ON TPU SHOWED FAULT CODES B3, B5, B6, B9 & B20. REMOVED AND REPLACED TPU. REMOVED AND REPLACED THE DFDU DISC. INSPECTED WIRE HARNESS FROM TPU TO TFU FOR SECURITY AND ANY CHAFING. NO DEFECTS NOTED.

Part: WIRE — BROKEN (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY FLOOR PATH LIGHT AT SEAT 7C INOP. REPAIRED BROKEN WIRE, OPS CHECK GOOD.

Part: FAN — INOPERATIVE (E/E COMPT)

FLIGHT DECK EICAS ILLUMINATED FOLLOWED SHORTLY BY THE SMELL OF ELECTRICAL SMOKE. A FEW MINUTES LATER THE SMOKE SMELL INTENSIFIED AND GOT AN EQUIP COOLING FOR STATUS. DIVERTED TO STL. REMOVED AND REPLACED NR 2 EQUIPMENT COOLING FAN, SYSTEM OPS CHECKED NORMAL.

Part: FLOOR BEAM — CORRODED (BS 324)

PAE - FLT 7825 - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR BEAM AT STATION 324 HAS CORROSION AT RBL 51 TO RBL 65, WL 208. FABRICATED, ALODINED, PRIMED AND INSTALLED PARTS PER ER 5-23-12-06 AND TCO PAN 96-1358RR-8110-3. (M)

Part: SEAT TRACK — CORRODED (BS 397)

PAE - FLT 7825 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK BS 397, RBL 45, WL 208. REMOVED AND REPLACED SEAT TRACK PER IAW SRM 51-40-02 AND SRM 51-40-00. (M)

Part: SEAT TRACK — CORRODED (BS 397)

PAE - FLT 7825 - DURING ROUTINE MAINTENANCE CEHCK, FOUND CORROSION ON SEAT TRACK BS 397, RBL 24, WL 208. REMOVED AND INSTALLED REPAIR PARTS PER SRM 51-40-02. (M)

Part: FLOOR BEAM — CORRODED (BS 377)

PAE - FLT 7825 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 377, RBL 2, WL 208. FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR PARTS PER SRM 53-00-51 AND 51-20-01. (M)

Part: SKIN — DENTED (BS 1500-1520)

PAE - FLT 7825 - DURING ROUTINE MAINTENANCE CHECK, FOUND TWO DENTS IN SKIN ON LEFT AFT FUSELAGE BETWEEN BS 1500 AND 1520, BETWEEN STRINGER 26L AND STRINGER 27L. CUT OUT DAMAGE, FABRICATED PARTS AND INSTALLED PER SRM 53-00-01 AND ER 5-53-35-02. (M)

Part: WIRE — BROKEN (CABIN)

PHX - FLT 2616 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AFT OF LAVATORIES INOPERATIVE. REPAIRED BROKEN WIRES AS REQUIRED. OPERATES NORMALLY. (X)

Part: WIRE — BROKEN (CABIN)

PHX - FLT 2211 - REFERENCE MEL 33-51-03, EMERGENCY LIGHT ROW 20 INOP. REPAIRED BROKEN WIRE UNDER SEAT. OPS CHECKED NORMAL. MEL REMOVED. (M)

Part: BATTERY PACK — INOP (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS AT DOOR L-4 OVERHEAD INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK FOR DOOR L-4. OPS NORMAL. (M0

Part: WIRE — DISCONNECTED (CABIN)

PHX - FLT 700 - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 25 EMERGENCY LIGHT INOP. RECONNECTED TERMINAL. (M)

Part: HYD PUMP — FAILED (RT ENGINE)

ATL - FLT 610 - PHX-ATL - RIGHT ENGINE DRIVE HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED AT CRUISE ALTITUDE. RIGHT HYDRAULIC ENGINE PUMP EICAS MESSAGE DISPLAYED. REPLACED RIGHT ENGINE DRIVE HYDRAULIC PUMP, REPLACED CASE DRAIN AND PRESSURE AND RETURN FILTERS. OPERATES OK GOOD ON RUN. REPLACED FILTERS AGAIN. LEAK CHECK GOOD. (M)

Part: DUCT — FAILED (NR 1 ENGINE)

PHX/EWR - FLT 0684 - AIR TURNBACK. NR 1 ENGINE OVERHEAT IN CLIMB. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED HP6 DUCT. PART TOTAL CYCLES, 7016. (X)

Part: FIRE LOOP — OUT OF POSITION (LT ENGINE)

PHX/ATL - FLT 0610 - AIR TURNBACK. LEFT ENGINE OVERHEAT EICAS AND LIGHT AT 20,000 FEET ON CLIMB-OUT. CHECK COMPLETE LIGHTS EXTINGUISHED, LEFT ENGINE AT IDLE AND RETURNED TO PHX. PER FIM 26-11-10, INSPECTED LEFT BLEED DUCTS, NO LEAKS FOUND. FOUND 3 AREAS OF FIRE LOOP TOUCHING ATTACH TUBE. REPOSITIONED. RAN ENGINE AT HIGH IDLE. (X)

Part: STARTER — FAILED (NR 2 ENG)

JFK-PHX - ENGINE SHUTDOWN, AIRCRAFT DIVERTED TO CMH. NR 2 ENGINE SHUTDOWN IN FLIGHT DUE TO OIL QUANTITY DECREASING. REMOVED THE COVER HOUSING OFF OF THE AIR/OIL SEPARATOR AND FOUND THE SEAL THAT GOES ON THE SEPARATOR SHAFT MISSING AND SHAFT GALLED, AS WELL AS THE BUSHING THAT GOES ON THE MATES TO THE COVER HOUSING AND SHAFT. REMOVED AND REPLACED 06 GEARBOX MODULE. STARTER FAILED DURING START. REMOVED AND REPLACED STARTER. REFERENCE AWXA960116.

Part: GEARBOX — FAILED (NR 2 ENG)

JFK-PHX - ENGINE SHUTDOWN, AIRCRAFT DIVERTED TO CMH. NR 2 ENGINE SHUTDOWN IN FLIGHT DUE TO OIL QUANTITY DECREASING. REMOVED THE COVER HOUSING OFF OF THE AIR/OIL SEPARATOR AND FOUND THE SEAL THAT GOES ON THE SEPARATOR SHAFT MISSING AND SHAFT GALLED, AS WELL AS THE BUSHING THAT GOES ON THE MATES TO THE COVER HOUSING AND SHAFT. REMOVED AND REPLACED 06 GEARBOX MODULE. STARTER FAILED DURING START. REMOVED AND REPLACED STARTER. (M)

Part: WIRE — BROKEN (CABIN)

PHX - FLT NR 20 - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT INOP AT SEAT 20 A,B,C. REPAIRED WIRING. OPS CHECK GOOD. (M)

Part: WIRE — BROKEN (CABIN)

PHX - FLT NR 0700 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT AT SEAT ROW 20 INOP. REPAIRED WIRING AS REQUIRED, OPS CHECK GOOD. (M)

Part: FITTINGS — CORRODED (CARGO COMPT)

PHX - DURING SCHEDULED C3 INSPECTION, FOUND THRESHOLD STANCHION FITTINGS FOR CARGO NETS CORRODED IN AFT CARGO PIT. REMOVED ADN REPLACED FITTINGS PER SRM 51-40-02. (M)

Part: FLOOR BEAM — CORRODED (FS 365)

PHX - DURING SCHEDULED C3 INSPECTION, FOUND FLOOR BEAM TOP CAP CORRODED IN SEVERAL AREAS, STATION 365 BL 0 TO RBL 40. FABRICATED ANGLE REPAIR AND INSTALLED PER SRM 53-00-51. (M)

Part: STRAP — CRACKED (BS 1681)

PHX - DURING SCHEDULED C3 INSPECTION, FOUND INTERCOSTAL DOUBLER STRAP CRACKED, BS 1681 RBL 12. REMOVED, FABRICATED AND INSTALLED STRAP PER SRM 51-10-00 AND SRM 51-40-02. (M)

Part: FLOOR BEAM — CORRODED (STA 377.7)

PHX - DURING SCHEDULED C3 INSPECTION, FOUND FLOOR BEAM TOP CAP CORRODED BEYOND LIMITS AT STATION 377.7 LBL 10. REPAIRED FLOOR BEAM PER SRM 51-70-12. (M)

Part: FLOOR BEAM — CORRODED (FS 345)

PHX - DURING SCHEDULED C3 INSPECTION, FOUND FLOOR BEAM CORRODED AT FASTENER HOLE, STATION 345 BL 0. REPAIRED PER SRM 51-40-02. (M)