N632DL

Part: SKIN — DAMAGED (BS 418 S6L) · airframe 74,768 hrs · 35,569 cycles

LOG ITEM J614634-001, POSSIBLE RT SIDE ACFT LIGHTENING STRIKE. ACFT INSPECTED IAW AMM 05-51-19. DAMAGE TRANSFERRED TO NR'S 1 THRU 9. DAMAGE ON N/R'S 1-3 AND 5-9 C/W IAW SRM 53-00-01. DAMAGE ON N/R 4 (STA 418 STR 6L) C/W ON ERA 488577-14.

Part: B-NUT — LOOSE (HYD LINE) · airframe 72,632 hrs · 34,623 cycles

AFTER T/O RAISED GEAR, MAIN GEAR DID NOT RETRACT, NOSE GEAR DID. RAN THE GEAR DISAGREE CHECKLIST, THEN GOT A L HYD QTY EICAS MSG. RAN THAT CHECKLIST. LANDED TAXIED OFF RUNWAY AND NOTED RF W/ DECREASE HYD QUANITY. RAN THAT CHECKLIST AND GOT TOWED TO GATE. DID NOT SHUT OFF PUMPS UNTIL LOST PRESSURE. FOUND B NUT ON NR 1 ENG HYD PRESSURE LINE LOOSE, SECURED. INSPECTED AND REPLACED BOTH CASE DRAIN AND PRESSURE FILTERS. RAN ENG, NO LKS NOTED. PUMP CK OK

Part: ANTI-ICE VALVE — FAILED (NR 2 ENGINE) · airframe 71,819 hrs · 34,252 cycles

RT ENG ANTI ICE EICAS MESSAGE WITH SWITCH ON, CIRCUIT BREAKER POPPED, RESET BREAKER, POPPED AGAIN INSPECTED WIRES NO DEFECT NOTED SHOOK DOWN HARNESS AT D42322P. UNABLE TO GET C/B TO POP236039ADEL CLAMP ABOVE A/I VALVE DISCONNECTED, 238039, REMOVED WIRE W5600-3501RYB AT CONNECTOR D5050 A/I VALVE9899730INSTALLED ADEL CLAMP ABOVE A/I VLV3849166FINISHED INSTALL OF WIRE. CKS GOOD. REINSTALLED BALLCAP FAIRING.

Part: TEE FITTING — CRACKED (FUSLEAGE) · airframe 70,963 hrs · 33,734 cycles

REPLACED TEE CLIP 146N8748-17 WITH P/N 146N8748U17 FOR DOOR STOP NR 3 AT L4 DOOR STA 1681.8 REPLACED TEE CLIP 146N8748-21 WITH P/N 146N8748U21 FOR DOOR STOP NR 4 AT L4 DOOR STA 1681.8. REPLACED TEE CLIP 146N8748-18 WITH P/N 146N8748U18 FOR DOOR STOP NR 3 AT R4 DOOR STA 1681.8. REPLACED TEE CLIP 146N8748-22 WITH P/N 146N8748U22 FOR DOOR STOP NR 4 AT R4 DOOR. ALL THE ABOVE CLIPS WERE REPLACED PER EA 06-465922-03 AD ME02 REV B.

Part: MOUNT — CORRODED (NR 2 NACELLE) · airframe 62,114 hrs · 29,843 cycles

DURING THE CURRENT HMV3 CHECK, THE NR 2 PYLON P/N 311N3211 -1 FORWARD ENGINE MOUNT FITTING WAS FOUND WITH FRETTING CORROSION ON THE LOWER SURFACE AROUND THE MOUNT HOLES. PERMANENT REPAIR WAS ACCOMPLISHED PER PRODUCTION PERMIT B757-54-25940PA AND ERA 457245-14. BLENDED ENG MOUNT SURFACES PER PP, PASSIVATED BUSHING PER PP, REINSTALLED BUSHING PER PP, FLAP PEEN AND REAPPLIED PRIMER.

Part: MOUNT — CORRODED (NR 1 NACELLE) · airframe 62,114 hrs · 29,843 cycles

NR 1 ENGINE FORWARD LOWER MOUNT ON PYLON WAS BLENDED TO A DEPTH OF .003 INCHES TO REMOVE DAMAGE. ACCOMPLISHED PERMANENT REPAIR PER ACTS PRODUCTION PERMIT B757-71-25751. REFERENCE ERA 457046-14.

Part: MOUNT — CORRODED (NR 2 NACELLE) · airframe 62,114 hrs · 29,843 cycles

DURING THE CURRENT HMV3 CHECK, THE NR 1 PYLON P/N 311N3211-1 FORWARD ENGINE MOUNT FITTING WAS FOUND WITH FRETTING CORROSION ON THE LOWER SURFACE AROUND THE MOUNT HOLES. ACCOMPLISHED PERMANENT REPAIR PER PRODUCTION PERMIT B757-54-25939PA REF ERA 457244-14.

Part: MOUNT — CORRODED (NR 2 NACELLE) · airframe 62,114 hrs · 29,843 cycles

NR 2 ENGINE FORWARD LOWER MOUNT FITTING HAD PITTING, REMOVED BY BLENDING. ACCOMPLISHED PERMANENT REPAIR PER PRODUCTION PERMIT B757-71-25751 REF ERA 457048-14.

Part: FITTING — DAMAGED (NR 2 NACELLE) · airframe 62,106 hrs · 29,840 cycles

NR 2 PYLON STRUT FITTINGS HAVE ELONGATED HOLES. ACCOMPLISHED PERMANENT REPAIR PER ACTS PRODUCTION PERMIT B757-54-25720. REFERENCE ERA 456938-14.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,049 hrs · 29,817 cycles

THE L1 DOOR OPENING, UPPER FORWARD CORNER, HAS A CRACK IN THE FUSELAGE SKIN. THE CRACKED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.

Part: FITTING — OVERSIZED (NR 2 PYLON) · airframe 62,045 hrs · 29,816 cycles

NR 2 PYLON UPPER LINK WING FITTING WAS FOUND WITH AN INNER LUG DIA. GREATER THAN ALLOWED. THE HOLE WAS OVERSIZED AND INSPECTED. AN OVERSIZED BUSHING WAS INSTALLED. REF AD 2003-18-05

Part: FITTING — MISREPAIRED (NR 1 PYLON) · airframe 62,045 hrs · 29,816 cycles

THE NR 1 PYLON INBOARD MID SPAR FITTING WAS INCORRECTLY OVERSIZED. THE HOLE WAS OVERSIZED TO THE NEXT SIZE FASTENER AND A LARGER FASTENER WAS INSTALLED REF 2003-18-05.

Part: WINDOW — CRACKED (COCKPIT) · airframe 61,244 hrs · 29,548 cycles

DURING FLIGHT, R-1 WINDOW BEGAN TO ARC AND DELAMINATE. FOLLOW POM PROCEDURES AND TURNED OFF WINDOW HEAT. R-1 WINDOW THEN SPIDER WEB CRACKED. REPLACED R-1 WINDOW, OPS CHECK GOOD.

Part: CIRCUIT BREAKER — FAULTY (COCKPIT) · airframe 60,622 hrs · 29,331 cycles

EMERGENCY LIGHTS ALONG MAIN AISLE FLOOR ILLUMINATED WITH COCKPIT SW IN ARMED POS AND FLT ATTENDANT PANEL SW IN NORMAL POS. REPLACED C/B TO CHARGER.

Part: ANNUNCIATOR — SHORTED (COCKPIT) · airframe 57,877 hrs · 28,351 cycles

ENTRY DOOR LIGHT ON OVERHEAD INDICATOR PANEL SHORTING OUT AND TRIPPING R IND LIGHT C/B. REMOVED AND REPLACED OVERHEAD IND LIGHT PANEL PER MM, CHECKS OK.

Part: PIN — CRACKED (NR 1 DIAG BRACE) · airframe 55,067 hrs · 27,361 cycles

CRACKS WERE NOTED IN THE FUSE PINS ON THE NR 1 PYLON DIAGONAL BRACE. COMPLIED WITH ERA 091408-14AD.

Part: ACTUATOR — UNSERVICEABLE (NR 12 SPOILER) · airframe 51,195 hrs · 25,778 cycles

UNCOMMANDED ROLL TO THE RIGHT. SPOILER MESSAGE DISPLAYED. REPLACED NR 12 SPOILER PCA. ADJUSTED AND TEST PER AMM.

Part: BOTTLE — INOPERATIVE (CARGO BAY) · airframe 48,458 hrs · 24,520 cycles

EMERGENCY ESCAPE TEST 2 BOTTLE PRESSURE INOP ON RIGHT SIDE. REPLACED BOTTLE ASSY PER M/M, TESTS GOOD.

Part: SWITCH — FAULTY (CARGO BAY) · airframe 48,276 hrs · 24,436 cycles

ON L/O CHECK, AFT CARGO LIGHT SWITCH CAUGHT ON FIRE. REPLACED SWITCH.

Part: OVEN — MALFUNCTIONED (GALLEY) · airframe 46,110 hrs · 23,391 cycles

F/C AFT OVEN WORKING INTERMITTENTLY, MAY HAVE SEEN SPARKS ABOVE BUN WARMER. OVEN APPEARS TO OPERATE NORMAL AT GATE. FOR PRECAUTION C/B PULLED AND COLLARED. OVEN FWD TO MCO AND PLACARD.

Part: SKIN — DENTED (FUSELAGE) · airframe 43,222 hrs · 22,074 cycles

THE FUSELAGE SKIN AND UNDERLYING BEARSTRAP WERE FOUND DENTED AND GOUGED JUST FWD OF THE LOWER AFT CORNER OF THE C2 DOOR. THE DAMAGE WAS REMOVED WITH A 6 X 1 INCH CUTOUT IN THE SKIN AND BEARSTRAP. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER WHICH WRAP AROUND THE DOOR CORNER PER ER/A 377925-14.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 43,222 hrs · 22,074 cycles

THE FUSELAGE SKIN WAS FOUND WITH SEVERAL LIGHTNING STRIKE AREAS BETWEEN FS 440 & 460 AND BETWEEN STRINGERS 18R. THE LIGHTNING STRIKES WERE REMOVED WITH 3 SMALL CUTOUTS IN THE SKIN. THE CUTOUTS WERE REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER INSTALLED PER ER/A 377924-14, REV A.

Part: CABLE FRAYED (PEDESTAL)

STAB TRIM LEVERS MOVE WHEN SPEEDBRAKE IS DEPLOYED APPEARS THAT THE LEFT STAB TRIM LEVER BINDS ACTS AS IF THE SPRING IS BROKEN. FOUND STAB TRIM CABLE STB1/STB2 MISROUTED AROUND SPOILER, NO BRAKE CLUTCH ASSY BENEATH STAB TRIM HANDLES CABLE FRAYED. CABLES REPLACED ON ROUTINE OPN 2000 RC NR 1 CABLES RIGGED IAW MM REF 27-41-00-05.

Part: LIGHT — INOPERATIVE (CABIN)

FWD RIGHT OVERWING EMERGENCY EXIT TRACK LIGHT SIGN INOP. REPLACED LIGHT ASSY, OPN OK.

Part: SKIN — DELAMINATED (NR 2 LE SLAT)

DURING SHOP INSPECTION FOR NR 2 L/E SLAT, FOUND T/E WEDGE DELAMINATED. REPAIRED PER SRM 57-43-02.

Part: PRESS CONTROLLER — MALFUNCTIONED (CABIN)

LOG ITEM-CABIN PRESS EICAS MSG RED AND CABIN WARN SOUNDED AT FL 330. EMERG DESCENT ACCOMPLISHED. MANUAL CONT WORKS OK. STATUS MSG CABIN ALT AUTO 1 AND CABIN ALT AUTO 2 CAME ON IN FLT. CORRECTIVE ACTION-NR 1 CONTROLLER FAULTS CONTROLLER AND LOW INFLOW. NR 2 CONTROLLER FAULTS LOW INFLOW. REPLACED NR 1 AND NR 2 CABIN PRESS CONTROLLERS. RPL COCKPIT PRESS AND IND WARN MODULE. PRESSURIZED A/C TO 6 PSI, A/C HELD PRESS. PERFORMED BITE TEST OF PRESS CONTROLLERS AND OPN CHECKED NORMAL PER M/M CONTROLLER REPLACEMENT.

Part: ACTUATOR — FAULTY (NR 2 ENGINE)

DURING CRUISE, HAD SVA FAILSAFE MSG, NR 2 ENGINE FLAMED-OUT. LANDED RDU. RAN ENGINE PER PFHB TEST 14 SVA, TEST NORMAL. FERRIED AC TO ATL. REPLACED STATOR VANE ACTUATOR, RETURNED TO SERVICE.