N666A

Part: SLAT — CORRODED (RT WING) · corrosion level 2 · airframe 69,627 hrs · 24,457 cycles

NUMBER 8 SLAT CORRODED, AREA BLENDED OUT OF LIMITS 44 INCHES FROM OTBD END. REPAIRED SLAT IAW AARD 57-43-00-1.

Part: BULKHEAD — CRACKED (LT PYLON) · airframe 69,627 hrs · 24,457 cycles

HORIZONTAL CRACK ON LT ENG PYLON, MID BULKHEAD, ON THE INBD SIDE. REPAIRED FOLLOWING INSTRUCTIONS OUTLINED IN EA 54-037894 DATED 12/22/2014.

Part: SKIN — GOUGED (FUSELAGE) · airframe 69,627 hrs · 24,457 cycles

FUSELAGE SKIN HAS DEEP GOUGE AT STATION 1556 & STRINGER 18 LT. REPAIRED SKIN IAW EA 53-037141 DATED 11/6/2014.

Part: CONTACT — DIRTY (EXTERIOR LIGHT) · airframe 68,121 hrs · 23,887 cycles

EXTERIOR EMERGENCY LIGHT AT RT NR 2 DOOR INOPERATIVE. CLEANED CONTACTS ON LIGHT ASSEMBLY FOR EXTERIOR EMERGENCY LIGHT AT RT NR 2 DOOR. OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — FAILED (FUEL SYSTEM) · airframe 67,808 hrs · 23,781 cycles

DFW INFLIGHT MIA EGE CREW REPORTED RT FUEL TANK QUANTITY INDICATION & TOTALIZER GAUGE INOPERATIVE. EMERGENCY DECLARED FLIGHT DIVERTED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. INSTALLED NEW CONNECTOR D6884 AT RT MAIN TANK. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: FITTING — WORN (LT PYLON) · airframe 66,953 hrs · 23,484 cycles

LT WING INBD SIDE LOAD FITTING, INBD SURFACE HAS WEAR. ACCOMPLISHED REPAIR IAW EA B757-54-031845.

Part: FITTING — WORN (LT PYLON) · airframe 66,953 hrs · 23,484 cycles

LT WING INBD SIDE LOAD FITTING, OTBD SURFACE HAS WEAR. ACCOMPLISHED REPAIR IAW EA B757-54-031845.

Part: FITTING — WORN (LT PYLON) · airframe 66,953 hrs · 23,484 cycles

LT WING OTBD LOAD FITTING, OTBD SURFACE HAS WEAR. ACCOMPLISHED REPAIR IAW EA B757-54-031845.

Part: FITTING — WORN (RT PYLON) · airframe 66,953 hrs · 23,484 cycles

RT WING, OTBD SIDE LOAD FITTING, OTBD SURFACE HAS WEAR. ACCOMPLISHED REPAIR IAW EA B757-54-031845.

Part: FITTING — WORN (RT PYLON) · airframe 66,953 hrs · 23,484 cycles

RT WING, INBD SIDE LOAD FITTING, OTBD SURFACE HAS WEAR. ACCOMPLISHED REPAIR IAW EA B757-54-031845.

Part: FITTING — WORN (RT PYLON) · airframe 66,953 hrs · 23,484 cycles

RT WING, INBD SIDE LOAD FITTING, INBD SURFACE HAS WEAR. ACCOMPLISHED REPAIR IAW EA B757-54-031845.

Part: FITTING — WORN (LT WING) · airframe 66,953 hrs · 23,484 cycles

LT WING, OTBD SIDE LOAD FITTING, INBD SURFACE HAS WEAR. ACCOMPLISHED REPAIR IAW EA B757-54-031845.

Part: PLATE — CORRODED (HORIZ STAB) · corrosion level 3 · airframe 65,098 hrs · 22,807 cycles

LEFT LOWER STABILIZER PIVOT PLATE HAS CORROSION ON THE FORWARD END. REMOVED CORROSION AND ACCOMPLISHED REPAIR PER EA B757-55-029365.

Part: PLATE — CORRODED (HORIZ STAB) · corrosion level 3 · airframe 65,098 hrs · 22,807 cycles

HORIZONTAL STABILIZER RIGHT LOWER INNER PIVOT SPLICE HAS CORROSION AT THE FORWARD END. REMOVED CORROSION AND ACOCMPLISHED REPAIR PER EA B757-55-029366.

Part: LIGHT — BROKEN (CABIN) · airframe 63,845 hrs · 22,362 cycles

EMERGENCY EXIT LIGHT BROKEN IN AFT GALLEY BY RIGHT NUMBER 3 DOOR. REPLACED EMERGENCY LIGHT LOCATED AT AFT GALLEY BY RIGHT NUMBER 3 DOOR. OPS CHECK NORMAL.

Part: PLACARD — DAMAGED (CABIN) · airframe 63,755 hrs · 22,326 cycles

LEFT AFT OVERWING EXIT PLACARD DAMAGED. REPLACED LEFT AFT OVERWING EXIT PLACARD. OPS CHECK NORMAL.

Part: COMPRESSOR — STALLED (LT ENGINE) · airframe 63,488 hrs · 22,241 cycles

LAX - CREW REPORTED AFTER TAKEOFF WITH GEAR RETRACTED, FLAPS FIVE, THE AIRCREW FELT A JOLT, HEARD A BOOM AND THE AIRCRAFT VEERED LEFT AND RIGHT. EMERGENCY DECLARED FLIGHT RETURNED LAX LANDED WITHOUT INCINDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEFT ENGINE HAD A COMPRESSOR STALL. REPLACED LEFT ENGINE AT LAX ON 07/25/2012. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 62,415 hrs · 21,840 cycles

PUNCTURE IN SKIN AT STATION 1649 BETWEEN STRINGERS 26 AND 28 LEFT. INSTALLED DOUBLER REPAIR PER EA B757-53-022409.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,415 hrs · 21,840 cycles

AREA AFT OF BULK CARGO COMPARTMENT CEILING AREA FLOOR BEAM UPPER CHORD SURFACE CORRODED AT BODY STATION 1681, RIGHT BUTTLINES 47 TO 38. ACCOMPLISHED NESTED ANGLE REPAIR AT STATION 1681 FLOORBEAM PER EA B757-53-022340.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 62,415 hrs · 21,840 cycles

AREA AFT OF BULK CARGO COMPARTMENT LOWER ANGLE BARE METAL BODY STATION 1700, STRINGERS 27R TO 29 RIGHT. INSTALLED AFT BULK CARGO COMPARTMENT LOWER ANGLE PER SRM 51-40-02.

Part: PAN — GOUGED (L2 DOOR) · airframe 62,415 hrs · 21,840 cycles

LEFT NUMBER 2 DOOR EXTERIOR HANDLE PAN IS GOUGED. REMOVED GOUGED HANDLE PAN AND INSTALLED NEW HANDLE PAN PER B757-200 SRM 51-40-02 AND ESO 90282.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 62,415 hrs · 21,840 cycles

LEFT WING OUTBOARD SLAT NUMBER 3 UPPER SKIN CORRODED AROUND FASTENERS. INSTALLED DOUBLER REPAIR PER SRM 57-43-00-1.

Part: PAN — GOUGED (R4 DOOR) · airframe 62,415 hrs · 21,840 cycles

RIGHT NUMBER 4 DOOR BUTTERFLY HANDLE PAN LOWER END GOUGED. REMOVED AND REPLACED PAN PER SRM 51-40-02.

Part: ANGLE — GOUGED (R1 DOOR) · airframe 62,415 hrs · 21,840 cycles

RIGHT NUMBER 1 DOOR EMERGENCY MECHANISM HOUSING AT UPPER HINGE INTERNAL DOOR IS GOUGED. REPLACED WEB, STIFFENER, FITTING, SHIM, BRACKET AND ANGLE PER SRM 51-20-01 AND SRM 51-40-02-06.

Part: SKIN — GOUGED (TE FLAP) · airframe 62,415 hrs · 21,840 cycles

RIGHT WING INBOARD MID FLAP BOTTOM SIDE HAS GOUGE. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-07 AND AMM 51-20-00-0.

Part: SKIN — DENTED (TE FLAP) · airframe 62,415 hrs · 21,840 cycles

RIGHT WING TRAILING EDGE INBOARD FLAP LOWER TRAILING EDGE INNER SKIN DENTED. INSTALLED DOUBLER REPAIR PER SRM 57-53-01 AND SRM 51-70-10.

Part: STRAP — CRACKED (FUSELAGE) · airframe 62,415 hrs · 21,840 cycles

AFT CARGO STATION 1380 RIGHT BUTTLINE 40 CEILING STRAP CRACKED. REPLACED CEILING STRAP PER SRM 53-10-51-7R-1 AND SRM 51-40-02.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 62,415 hrs · 21,840 cycles

NUMBER 10 SLAT LEADING EDGE SKIN INBOARD CORRODED. INSTALLED DOUBLER REPAIR PER SRM 57-43-01-2R AND AARD 57-43-00-1.

Part: SKIN — DAMAGED (TE FLAP) · airframe 62,415 hrs · 21,840 cycles

LEFT WING OUTBOARD MAIN FLAP UPPER SURFACE AFT OF NUMBER 1 SPOILER HAS SMALL AREA OF EXPOSED HONEYCOMB. REMOVED DAMAGE PLIES, LAYED UP REPAIR PLIES AND CURED, APPLIED SEALER RESIN AND CURED PER SRM 57-53-01 AND SRM 51-70-07.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,415 hrs · 21,840 cycles

MAIN CABIN SEAT TRACK INNER FACE AND CROWN CORRODED AT BODY STATION 685, RIGHT BUTTLINE 24. INSTALLED SEAT TRACK PER SRM 51-40-02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 62,415 hrs · 21,840 cycles

MAIN CABIN FUSELAGE STRINGER SECTION CRACKED BODY STATION 680, STRINGER 12 RIGHT. REMOVED AND REPLACED WEB PER SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 62,415 hrs · 21,840 cycles

FUSELAGE INTERCOSTAL WEB UPPER ANGLE CRACKED FROM BODY BS 660 TO 680, BUTTLINE 0. CRACK 14 INCHES. REPLACED ANGLE PER SRM 53-00-51-2R AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,415 hrs · 21,840 cycles

MAIN CABIN FLOOR SUPPORT WEB UPPER SURFACE, BIDY STATION 1685 BUTTLINE 0, MOUNT FITTING CORRODED. INSTALLED NEW FITTING PER SRM 51-40-02.

Part: CHANNEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,415 hrs · 21,840 cycles

MAIN CABIN FLOOR SUPPORT HAS CORROSION BS 1644 - 1660, BL 0. REMOVED AND REPLACED CHANNEL PER SRM 51-40-02 AND DWG 146N5242.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,415 hrs · 21,840 cycles

MAIN CABIN FLOOR SUPPORT UPPER SURFACE CORRODED BODY STATIONS 345 TO 365, RIGHT BUTTLINE 62. INSTALLED FLOOR SUPPORT PER SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,415 hrs · 21,840 cycles

MAIN CABIN FLOOR SUPPORT WEB DOUBLER UPPER UPPER SURFACE HAS CORROSION AT BODY STATION 1717 LEFT BUTTLINE 36. REMOVED AND REPLACED AFT PRESSURE DECK WEB PER BAC DWG 146N5300 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 371) · airframe 62,415 hrs · 21,840 cycles

MAIN CABIN FLOOR SUPPORT CRACKED AT SCREW HOLE BS 371, BL 0. INSTALLED REPAIR DOUBLER PER SRM 51-40-02.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,415 hrs · 21,840 cycles

MAIN CABIN FLOORBEAM UPPER TEE SURFACE CORRODED AT BS 1640, LBL 6 TO RBL 17. INSTALLED NEW STRAP PER SRM`S 53-00-51, 51-20-01 AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,415 hrs · 21,840 cycles

MAIN CABIN FLOOR SUPPORT UPPER SURFACE CORRODED FROM BS 324 TO 344, RBL 62. INSTALLED NEW FLOOR SUPPORT PER SRM 51-40-02.

Part: CHANNEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,415 hrs · 21,840 cycles

MAIN CABIN RIGHT NUMBER 4 DOOR LOWER SILL U CHANNEL CORRODED FROM BS 1640 - 1660. INSTALLED NEW U CHANNEL PER SRM 51-40-02 AND DRAWING 146N5230.

Part: CHANNEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,415 hrs · 21,840 cycles

MAIN CABIN, LEFT NUMBER 4 DOOR SILL U CHANNEL CORRODED FROM BODY STATIONS 1640 TO 1660. REPLACED LEFT NUMBER 4 DOOR LOWER SILL U CHANNEL PER SRM 51-40-02.

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,415 hrs · 21,840 cycles

MAIN CABIN, RIGHT NUMBER 4 DOOR LOWER SILL, L ANGLE CORRODED AT BODY STATIONS 1675 TO 1680. REPLACED L ANGLE PER SRM 51-40-02.

Part: CHANNEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,415 hrs · 21,840 cycles

MAIN CABIN, LEFT NUMBER 4 DOOR LOWER SILL U CHANNEL CORRODED FROM BS 1660 TO 1680. REPLACED LEFT NUMBER 4 DOOR LOWER SILL U CHANNEL PER SRM 51-40-02.

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,415 hrs · 21,840 cycles

MAIN CABIN, LEFT NUMBER 4 DOOR LOWER SILL L ANGLE CORRODED FROM BS 1674 TO 1679. REPLACED LEFT NUMBER 4 DOOR LOWER SILL L ANGLE PER SRM 51-40-02.

Part: CHANNEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 62,415 hrs · 21,840 cycles

MAIN CABIN, RIGHT NUMBER 4 DOOR LOWER SILL, U CHANNEL CORRODED FROM BODY STATIONS 1660 TO 1680. REMOVED AND REPLACED U CHANNEL PER SRM 51-40-02.

Part: TERMINAL — ARCED (LANDING LIGHT) · airframe 62,415 hrs · 21,840 cycles

LEFT LOWER WING TO BODY AREA, LANDING LIGHT TERMINAL WIRE ARCING AGAINST STRUCTURE AT BULB. REMOVED AND REPLACED TERMINAL BACTM 140. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,461 hrs · 21,485 cycles

RIGHT AFT EXTERIOR OVERWING SLIDE LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT AFT EXTERIOR OVERWING SLIDE LIGHT. OPS CHECK NORMAL.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 61,461 hrs · 21,485 cycles

SEAT 35D EMERGENCY LIGHT PULLED OUT OF SEAT. REPAIRED LIGHT. OPS CHECK NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 61,461 hrs · 21,485 cycles

RIGHT AFT EXTERIOR OVERWING SLIDE LIGHT INOPERATIVE. REPLACED BATTERY AND CHARGER ASSEMBLY. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,381 hrs · 21,094 cycles

RIGHT NUMBER ONE DOOR SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER ONE DOOR SLIDE EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: PIN — BACKED OUT (CONNECTOR) · airframe 58,402 hrs · 20,405 cycles

EMERGENCY LIGHT AT SEAT 36D INOPERATIVE. RESEATED PUSHED BACK PIN AT CONNECTOR FOR EMERGENCY LIGHT AT SEAT 36D.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,893 hrs · 20,229 cycles

FLOORBOARD SUPPORT BETWEEN STATIONS 680 TO 700 LEFT BUTTLINE 48 HAS CRACK AT AFT MOUNTING HOLE. REMOVED AND INSTALLED SUPPORT BRACKET PER AARD 53-30-51-2.

Part: SLAT — CORRODED (RT WING) · corrosion level 2 · airframe 57,893 hrs · 20,229 cycles

NUMBER NINE SLAT CORRODED. ACCOMPLISHED DOUBLER REPAIR.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,893 hrs · 20,229 cycles

FLOORBEAM AT STATION 700 LEFT BUTTLINE 24 TO 48 IS CRACKED. REPAIRED FLOORBEAM AT STATION 700 LEFT BUTTLINE 24 TO LEFT BUTTLINE 48 PER PATTERN CARD 53-98--01 SRM 53-00-51-2R AND AARD 53-30-51-2.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 57,893 hrs · 20,229 cycles

CORROSION ON NUMBER NINE SLAT UPPER SKIN 30 INCHES FROM INBOARD END AT REAR SPAR. INSTALLED DOUBLER.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 57,893 hrs · 20,229 cycles

FLOORBOARD SUPPORT STATION 680 TO 700 LEFT BUTTLINE 48 CRACKED. REPLACED SUPPORT PER AARD 53-30-51-2.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 57,893 hrs · 20,229 cycles

RIGHT WING NUMBER 9 SLAT CORRODED ON LOWER TRAILING EDGE SKIN AT INBOARD DRIVE. RIGHT WING NUMBER 9 SLAT REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 57-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 57,893 hrs · 20,229 cycles

RIGHT WING CORROSION ON NUMBER 9 SLAT UPPER SKIN 30 INCHES FROM INBOARD END. RIGHT WING NUMBER 9 SLAT REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 57-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 57,893 hrs · 20,229 cycles

CORROSION ON NUMBER 8 SLAT UPPER SKIN 33 INCHES FROM INBOARD END. INSTALLED REPAIR DOUBLER PER SRM 57-43-01-2 AND AARD 57-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 57,893 hrs · 20,229 cycles

CORROSION ON NUMBER 8 SLAT UPPER SKIN 67 INCHES FROM OUTBOARD END. INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 57,893 hrs · 20,229 cycles

RIGHT WING NUMBER 8 SLAT CORROSION ON UPPER SKIN 67 INCHES FROM OUTBOARD END. RIGHT WING NUMBER 8 SLAT INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 57,893 hrs · 20,229 cycles

RIGHT WING NUMBER 7 SLAT CORRODED AT FASTENER ON UPPER SKIN AT INBOARD DRIVE TRACK. RIGHT WING NUMBER 7 SLAT REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 57-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 57,893 hrs · 20,229 cycles

RIGHT WING NUMBER 7 SLAT CORROSION ON UPPER SKIN 27 INCHES INBOARD OF FLUSH REPAIR. RIGHT WING NUMBER 7 SLAT REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 57-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 57,893 hrs · 20,229 cycles

RIGHT WING NUMBER 8 SLAT CORROSION ON UPPER SKIN 33 INCHES FROM INBOARD END. RIGHT WING NUMBER 8 SLAT INSTALLED REPAIR DOUBLER PER SRM 57-43-01-2 AND AARD 57-43-00-1.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,677 hrs · 19,797 cycles

BULLNOSE MOUNTED AISLE EMERGENCY LIGHT INOPERATIVE AT SEAT ROW 23AB. REPLACED LAMP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,920 hrs · 19,536 cycles

SEAT MOUNTED EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. RELAMPED LIGHT AT 22D.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,920 hrs · 19,536 cycles

SEAT MOUNTED EMERGENCY LIGHT AT SEAT 14D INOPERATIVE. RELAMPED LIGHT AT SEAT 14D.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - LEFT AFT OVERWING DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT AFT OVERWING DOOR EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - CENTER SECTION COACH SEAT MOUNTED EMERGENCY LIGHT DIM. REPLACED BATTERY PACK FOR CENTER SECTION COACH SEAT MOUNTED EMERGENCY LIGHT.

Part: LENS — MISSING (CABIN) · airframe 54,399 hrs

DFW - EMERGENCY LIGHT AT SEAT 18D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 18D.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,399 hrs

DFW - EMERGENCY LIGHTS AT SEAT 18 INOPERATIVE. REPLACED LAMP AT SEAT 18D FOR EMERGENCY LIGHT.

Part: ENGINE — VIBRATION (NR 2) · airframe 52,891 hrs

DFW INFLIGHT - AT CRUISE NR 2 ENGINE VIBRATIONS WERE ABOVE 2.0. FLUX BETWEEN 3.0 AND 1.6. CREW SHUT DOWN ENGINE. LANDED DFW WITHOUT INCIDENT. COMPRESSOR AND TURBINE BLADES CHECKED OKAY. REPLACED NR 2 ENGINE ON 14 NOV AT DFW DUE TO VIBRATIONS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,891 hrs · 18,487 cycles

TRANSITION PANEL CORRODED, REPAIRED TRANSITION PANEL IAW SRM 51-10-02.

Part: BRACKET — CRACKED (ZONE 100) · airframe 52,891 hrs · 18,487 cycles

FORWARD CARGO VERTICAL CHANNEL ON FORWARD SIDE OF FLOORBEAM CRACKED. REPLACED BRACKET IAW SRM 53-00-51.

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,891 hrs · 18,487 cycles

TRANSITION PANEL CORRODED. REPLACED TRANSITION PANEL IAW SRM 51-10-02.

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,891 hrs · 18,487 cycles

SIDE PANEL CORRODED, REPAIRED SIDE PANEL IAW SRM 53-00-53-1A.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,891 hrs · 18,487 cycles

AFT GALLEY FORWARD RT TIE DOWN CORRODED, REPAIRED IAW SRM 53-60-51-2R.

Part: GALLEY TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,891 hrs · 18,487 cycles

AFT GALLEY RT TIE DOWN CORRODED, REPAIRED TIE DOWN IAW SRM 53-60-51-2R.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,487 hrs

FLOORBOARD SUPPORT CORRODED. REPAIRED IAW SRM 53-60-51-2R1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,891 hrs · 18,487 cycles

FLOORBOARD SUPPORT CORRODED, REPAIRED IAW SRM 53-60-51-2R1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,891 hrs · 18,487 cycles

FLOORBOARD SUPPORT CORRODED, REPAIRED IAW SRM 53-60-51-2R1.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,891 hrs · 18,487 cycles

AFT MAIN DECK PLATE CORRODED, REPAIRED AFT DECK PLATE IAW SRM 53-60-51-2R2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,891 hrs · 18,487 cycles

FLOORBEAM CORRODED, REPAIRED IAW AARD 53-60-51-5.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 52,891 hrs · 18,487 cycles

FLOORBOARD SUPPORT HAT CHANNEL CORRODED. REPLACED FLOOR SUPPORT HAT CHANNEL IAW SRM 53-10-51-01.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,238 hrs

DFW - EMERGENCY LIGHTS AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,238 hrs

DFW - EMERGENCY LIGHT AT SEAT 12ABC BULLNOSE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 12ABC BULLNOSE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,238 hrs

DFW - EMERGENCY LIGHTS AT SEAT ROWS 7DEF TO 15DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 7DEF TO 15DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (CABIN) · airframe 51,238 hrs

DFW - EMERGENCY EXIT SIGN LIGHT AT FORWARD LAVATORY SIDEWALL INOPERATIVE. REPLACED MODULE FOR EMERGENCY EXIT SIGN LIGHT AT FORWARD LAVATORY SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,238 hrs

DFW - EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,071 hrs

MIA - EMERGENCY LIGHTS AT SEAT ROWS 9 TO 15 INOPERATIVE. REPLACED BATTERY PACK AT RIGHT NUMBER TWO DOOR FOR EMERGENCY LIGHTS AT SEAT ROWS 9 TO 15. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (STAB TRIM)

DEN INFLIGHT T2209/16DEC DFW TO EGE, HORIZONTAL STABILIZER ASYMMETRY STATUS MESSAGE ILLUMINATED AT CRUISE. LANDED DEN WITHOUT INCIDENT. REPLACED STABILIZER TRIM AILERON CONTROL MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)

LAX - EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. SECURED LOOSE CONNECTION FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 36D INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 36D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 15D INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA - EMERGENCY LIGHTS AT SEATS 11D AND 15D INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT SEATS 11D AND 15D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY PATH LIGHTS AT SEAT 16D INOPERATIVE. REPLACED FORWARD EMERGENCY ESCAPE PATH LIGHT ON SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CABLE — ODOR (CABIN)

INFLIGHT ELECTRICAL SMELL IN COCKPIT, SMELL & SMOKE HAZE IN CABIN. DISSIPATED AFTER TURNING OFF POWERPORTS, OVENS, OVERHEAD LIGHTS, AND WORK LIGHTS. STANDBY ALTIMETER C/B POPPED DURING FLIGHT. LANDED WITHOUT INCIDENT. SMELL REOCCURED WITH POWERPORT SWITCH ACTIVATION. PLACARDED POWERPORT SYS INOP. REINSTATED STANDBY ALTIMETER C/B. SYS GROUND CHECKED NORMAL OPERATION. DFW PERFORMED VISUAL INSPECTION OF ALL INSEAT POWER SUPPLY UNITS AND UNDER LOWER SIDEWALL PANELS, SIDEWALL TO PASSENGER SEAT POWERPORT CABLES, UNDER SEAT POWERPORT WIRING. POWERPORT POWER RELAY K9701 AND ALL POWER PORT OUTLETS FOR SIGNS OF OVERHEATING, ARCING, OR CHAFED WIRES. NO FAULTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER MOD M10798 FOR FORWARD CABIN EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS IN THE AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AND CHARGER MOD M00737 FOR EMERGENCY LIGHTS IN THE AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

BOS - FOUND ROW 15-24 SEAT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK OVER ROW 19 IAW MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY LIGHT AT OVERWING EXIT INOPERATIVE. REPLACED FORWARD OVERWING EMERGENCY EXIT LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE FLOOR PATH LIGHT STRIP AT COFFEE BAR INOPERATIVE. REPLACED 2 BAD JUMPER WIRES. SYSTEM GROUND CHECK NORMAL OPERATION. (M)