N173AN

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,027 hrs · 15,998 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS EMERGENCY LIGHTS INOP AT SEATS 16DEF TO 24DEF. REPLACED EMERGENCY LIGHTS BATTERY M10953 IAW AMM 33-51-07. TEST NORMAL.

Part: FUEL TANK — LEAKING (RT WING) · airframe 56,730 hrs · 15,898 cycles

AIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS FUEL LEAK AT R WING FWD SEEM OUTBD OF NO. 2 PYLON. MAINTENANCE ISOLATED LEAK @ STRINGER (L-10) JUST INBOARD OF (WS369.50). REMOVED SEALANT PREPPED AND APPLIED NEW SEALANT IAW B757 AMM 28-11-00-206-001. LEAK CHECK GOOD, NO LEAKS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,507 hrs · 15,834 cycles

AIRCRAFT WAS NOT GROUNDED: R2 EMERGENCY SLIDE LIGHT INOPERATIVE. MAINTENANCE REPLACED SLIDE LIGHT PER AMM 33-51-06.

Part: PITOT HEAD — UNRELIABLE (PITOT/STATIC SYS) · airframe 56,094 hrs · 15,718 cycles

AIRCRAFT WAS GROUNDED: CREW REPORTED A HIGH SPEED ABORTED TAKE-OFF DUE TO AIRSPEED DISAGREE. STANDBY AIRSPEED INDICATOR WAS 15KTS OFF CAS & FOS. MAINTENANCE REMOVED AND REPLACED AUX 1 PITOT TUBE IAW AMM 34-11-01-024-041, ALL TEST GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 56,083 hrs · 15,714 cycles

AIRCRAFT NOT GROUNDED: R3 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED R3 DOOR EXT SLIDE LIGHT IAW AMM 33-51-06.

Part: LIGHT — BROKEN (CABIN) · airframe 56,083 hrs · 15,714 cycles

AIRCRAFT NOT GROUNDED: R2 DOOR FWD EXIT IDENTIFIER LIGHT ASSY BROKEN. REPLACED R2 DOOR FWD EXIT IDENTIFIER LIGHT ASSY IAW AMM 33-51-10.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 56,083 hrs · 15,714 cycles

AIRCRAFT NOT GROUNDED: 34D SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. SECURED SEAT CONNECTOR ON SEAT 34D EMERGENCY LIGHTS IAW AMM 33-51-11.

Part: COMPUTER — FAILED (FLT CONTROL) · airframe 55,843 hrs · 15,649 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS STAB TRIM EICAS AFTER TAKE OFF QRH PROC. COMPLETED. RETURNED TO MIA. STAB TRIM LIGHT REMAINED ON TILL TOUCHDOWN. MAINTENANCE FOUND LEFT FCC FAILED. REMOVED AND REPLACED LEFT FCC IAW AMM 22-11-01. PERFORMED LAND TEST 40. ALL TESTS CHECK NORMAL.

Part: LENS — MISSING (CABIN) · airframe 55,644 hrs · 15,588 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHT ON WALL AFT OF GALLEY WAS MISSING COVER, LENS. MAINTENANCE REPLACED LIGHT ASSEMBLY PER AMM 33-50-00.

Part: VALVE — STUCK (LT FUEL) · airframe 55,179 hrs · 15,456 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS FUEL IS OUT OF BALANCE WITH LEFT FUEL VALVE STUCK CLOSED. MAINTENANCE TRANSFERED FUEL FROM CENTER WING TO OUTER WING IAW AMM 28-26-00. OK FOR SERVICE. RE-CYCLED L/H FUEL VALVE. OPS CHECKS GOOD.

Part: MODULE — MALFUNCTIONED (RUDDER SYS) · airframe 55,076 hrs · 15,431 cycles

AIRCRAFT WAS GROUNDED: PILOT DECLARED EMERGENCY ON ACCOUNT OF THE RUDDER RATIO LIGHT CAME ON AFTER TAKE OFF. MAINTENANCE ACCOMPLISHED RUDDER RATIO MODULE RESET. NO FAULTS NOTED. A/C OK FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (L1 DOOR AREA) · airframe 53,074 hrs · 14,867 cycles

L1 FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED THE FLASHLIGHT IAW AMM 25-64-00.

Part: ENGINE — ODOR (RIGHT) · airframe 52,167 hrs · 14,630 cycles

FLT 203 EN-ROUTE AMS - PHL. THE AIRCRAFT WAS GROUNDED. ODOR IN CABIN (FWD) AND FLIGHT DECK. RAN FUMES CHECK LIST. PULLED IFE C/B- UTILITY BUSES OF- LEFT RECIRCULATION OFF-EQUIP COOLING ALTN- RT PAC OFF. WHEN PAC OFF ODOR WENT AWAY. RECEIVED FORM 8533. ACCOMPLISHED J/C 05-96-70 AND 05-96-71. FOUND TO BE RIGHT ENGINE AT FAULT. REMOVED AND REPLACED RT ENG IAW J/C NO. 74-94-01. OPERATIONAL AND LEAK CK SATISFACTORY.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 51,639 hrs · 14,504 cycles

AIRCRAFT WAS NOT GROUNDED: EXIT SIGN ON 2R DOOR FELL OFF. MAINTENANCE INSTALLED NEW LENS COVER OVER 2R EMERGENCY EXIT DOOR PER IPC 33-51-11 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: TRANSMITTER — FAULTY (EPR) · airframe 51,282 hrs · 14,404 cycles

AIRCRAFT WAS GROUNDED. PHL-AMS RETURNING TO PHL ACCOUNT ENGINE TRUST ASYMMETRY ISSUE. EMERGENCY DECLARED. AT FL 35.0 PILOT REPORTS LEFT ENGINE LOW POWER DUE TO HIGH EPR. LEFT HAND ENGINE EPR: 1.96, N1: 74.4, EGT: 474, N2: 74, N3: 77, F/F: 2.6. R/H ENG EPR:1.76, N1: 95.5, EGT: 648, N2: 88, N3: 86, F/F 5.4, TROUBLESHOOTING IN PROGRESS. REPLACED EPR TRANSMITTER HOSE AND 3-WAY VALVE PER AMM 77-11-01. (SEE NON-ROUTINE MIC 20558640 FOR CHAFED TRANSMITTER HOSE, REPLACED PER AMM 77-11-01 AND 20558642 FOR LEAKING 3-WAY ADAPTER TUBE AND VALVE ASSEMBLY REPLACED PER AMM 77-11-00-735-019-R00. PERFORMED P1 SYSTEM PRESSURE TEST PER CARD #4227.) POWER ASSURANCE CHECK OK PER 71-00-00.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 51,212 hrs · 14,387 cycles

EMERGENCY LIGHT LENS AT SEAT 2E FOUND MISSING. REPLACED THE LENS IAW AMM 33-20.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 51,212 hrs · 14,387 cycles

EMERGENCY LIGHT LENS AT SEAT 1E MISSING. REPLACED THE LENS IAW AMM 33-20.

Part: POWER SUPPLY — DEFECTIVE (CABIN) · airframe 51,110 hrs · 14,356 cycles

THE AIRCRAFT WAS GROUNDED. FOUND EMERGENCY PATH LIGHTING FROM ROW 9D THRU 15D VERY DIM. REMOVED AND REPLACED EMERGENCY PATH LIGHTING POWER SUPPLY AND BATTERY PACK PER MM 33-51-07. ALL OPERATIONS AND INDICATIONS NOW TEST NORMAL.

Part: CAP — MISSING (CABIN) · airframe 51,108 hrs · 14,355 cycles

THE AIRCRAFT WAS GROUNDED. SEAT 3EF AND EMERGENCY LIGHT CAP MISSING AFT OF SEAT. REPLACED LIGHT CAP AFT OF SEAT 3E AF F GROUND CHECK OK PER 33-51-00.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 51,111 hrs · 14,356 cycles

FOUND EMERGENCY LIGHTS FROM ROWS 9D TO 15D VERY DIM, REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-07. OPS TESTED NORMAL.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 51,111 hrs · 14,356 cycles

FOUND THE EMERGENCY LIGHTS FROM ROWS 9D TO 15D VERY DIM. REMOVED AND REPLACED THE POWER SUPPLY M10952 IAW AMM 33-51-07, OPS TESTED NORMAL.

Part: GIRT BAR — OUT OF POSITION (R1 DOOR SLIDE) · airframe 50,916 hrs · 14,298 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR 1R HARD TO ARM AND DISARM ACCORDING TO CABIN CREW. DURING INSPECTION, AMM TASK 52-11-20-825-001, FOUND RING TO GIRT OUT OF POSITION CAUSING IMPROPER ARMING. OPERATIONAL CHECKS SMOOTHLY.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,911 hrs · 14,294 cycles

AIRCRAFT NOT GROUNDED. DOOR L4 ARM LIGHT INOPERATIVE. REMOVED AND REPLACED BULB AT L4 DOOR SLIDE. INDICATOR OPERATIONAL CHECK GOOD PER AMM 33-13-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,911 hrs · 14,294 cycles

AIRCRAFT NOT GROUNDED. L4 DOOR ARM LIGHT INOPERATIVE. REPLACED BULB AT L4 DOOR SLIDE INDICATOR PER AMM 33-13-00.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 50,560 hrs · 14,189 cycles

THE AIRCRAFT WAS GROUNDED. TRAILING EDGE FLAP ASYMMETRY WHEN SELECTING FLAPS 5 ON DOWNWIND, THE FLIGHT DECLARED AN EMERGENCY AND PERFORMED QRH PROCEDURES. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO HEAVY BRAKING, NORMAL TOUCHDOWN. VERIFIED NO MESSAGE ON EICAS, ACCOMP OPS CHECK OF THE TEAM FLAP SYS IAW MM 27-51-00. OPS CKS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 50,362 hrs · 14,135 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT SEAT (L1) FLASHLIGHT INOPERATIVE . REPLACED FLASHLIGHT BATTERY AT FLIGHT ATTENDANT SEAT (L1) IAW AMM 25-64-00.

Part: TACH GENERATOR — FLUCTUATES (NR 2 ENGINE) · airframe 50,035 hrs · 14,055 cycles

EMERGENCY DECLARED. FLIGHT RETURNED TO DEPARTURE DUE TO A NR 2 ENGINE SPEED CARD FAILED. LANDING UNEVENTFUL. REMOVED AND REPLACED RIGHT ENGINE N3 TACHOMETER GENERATOR TRANSMITTER IAW AMM 77-12-02. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: SEAL — BINDING (L1 DOOR SLIDE) · airframe 49,596 hrs · 13,948 cycles

L1 DOOR SLIDE COVER LOWER SEAL IS BINDING, CAUSING THE SLIDE COVER TO BE LOOSE. TRIMMED EXCESS SEAL MATERIAL BELOW SLIDE COVER TO ELEVIATE BINDING. OPERATIONAL CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 49,290 hrs · 13,875 cycles

AIRCRAFT WAS NOT GROUNDED. LEFT AFT FLIGHT ATTENDANT EVACUATION LIGHT HAS A MISSING LENS COVER. **SUPPLEMENTAL - 06/17/17 - INSTALLED LENS COVER IAW AMM 33-50-51. OPERATIONAL CHECK GOOD. (CLOSED)

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 49,152 hrs · 13,839 cycles

SEAT MOUNTED EMERGENCY LIGHT AT ROW 18 DEF IS INOPERATIVE. RESET LOOSE SIDEWALL CONNECTOR IAW AMM 33-51-11. OPS CHECKED GOOD.

Part: FITTING — CORRODED (BS 1712) · corrosion level 2 · airframe 48,754 hrs · 13,734 cycles

AFT GALLEY FLOORBEAM MOUNT FITTING CORRODED AT BS 1712, LBL 51. REMOVED AND REPLACED THE FITTING ASSEMBLY IAW SRM 51-40-02.

Part: FITTING — CORRODED (BS 1688) · corrosion level 2 · airframe 48,754 hrs · 13,734 cycles

AFT GALLEY FLOOR BEAM CENTER MOUNT FITTING CORRODED AT BS 1688, BL 0. REMOVED AND REPLACED THE FITTING ASSEMBLY IAW SRM 51-40-02.

Part: FITTING — CORRODED (BS 327) · corrosion level 2 · airframe 48,754 hrs · 13,734 cycles

FORWARD GALLEY FLOOR BEAM MOUNT FITTING CORRODED AT BS 327, RBL 42. REMOVED AND REPLACED FITTING ASSEMBLY IAW 51-00-05-1.

Part: FITTING — CORRODED (BS 1687) · corrosion level 2 · airframe 48,754 hrs · 13,734 cycles

AFT GALLEY FLOOR BEAM MOUNT FITTING CORRODED AT BS 1687, RBL 52. REMOVED AND REPLACED THE FITTING ASSEMBLY IAW SRM 51-40-02.

Part: FITTING — CORRODED (BS 1713) · corrosion level 2 · airframe 48,754 hrs · 13,734 cycles

AFT GALLEY FLOOR BEAM MOUNT FITTING CORRODED AT BS 1713, RBL52. REMOVED AND REPLACED THE FITTING ASSEMBLY IAW SRM 51-40-02.

Part: CONTROL MODULE — FAILED (CABIN) · airframe 48,347 hrs · 13,632 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGNS AT L1/R1 DOORS AND FIRST CLASS SEAT MOUNTED EMERGENCY LIGHTS ARE VERY DIM. REMOVED AND REPLACED CONTROL MODULE AND BATTERY PACK AT M10798 IAW AMM 33-51-07. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,347 hrs · 13,632 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGNS AT L1/R1 DOORS AND FIRST CLASS SEAT MOUNTED EMERGENCY LIGHTS ARE VERY DIM. REMOVED AND REPLACED CONTROL MODULE (AALA20170201018) AND BATTERY PACK AT M10798 IAW AMM 33-51-07. OPERATIONAL CHECK GOOD.

Part: VALVE — FAULTY (ZONE 400) · airframe 48,112 hrs · 13,568 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. BHX-JFK FLIGHT DIVERTED TO LHR ACCOUNT LEFT ENGINE HIGH STAGE WARNING INDICATION. OVERWEIGHT LANDING UNEVENTFUL. REMOVED AND REPLACED LEFT HIGH STAGE PILOT VALVE IAW AMM 36-11-08(AALA20170103002) AND LEFT HIGH PRESSURE SHUTOFF VALVE IAW AMM 36-11-07. OPERATIONAL CHECK GOOD.

Part: VALVE — FAULTY (ZONE 400) · airframe 48,112 hrs · 13,568 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. BHX-JFK FLIGHT DIVERTED TO LHR ACCOUNT LEFT ENGINE HIGH STAGE WARNING INDICATION. OVERWEIGHT LANDING UNEVENTFUL. REMOVED AND REPLACED LEFT HIGH STAGE PILOT VALVE IAW AMM 36-11-08 AND LEFT HIGH PRESSURE SHUTOFF VALVE IAW AMM 36-11-07(AALA20170106005). OPERATIONAL CHECK GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 47,893 hrs · 13,503 cycles

AIRCRAFT NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTING RIGHT SIDE ROW 18 IS INOPERATIVE. SECURED LOOSE CONNECTOR IAW AMM 33-51-00. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,016 hrs · 13,013 cycles

AIRCRAFT WAS NOT GNDED. R1 DOOR EXIT IDENTIFIER, L1 DOOR EXIT IDENTIFIER & FIRST CLASS RT SIDE EMER PATH LIGHTS ARE INOPERATIVE. R & R CONTROL MODULE ASSEMBLY IAW AMM 33-51-11 & BATTERY PACK IAW AMM 33-51-07. OPERATIONAL CHECKED NORMAL. SEE ALSO AALA 20160518001.

Part: CONTROL MODULE — FAULTY (CABIN) · airframe 46,016 hrs · 13,013 cycles

AIRCRAFT WAS NOT GNDED. R1 DOOR EXIT IDENTIFIER, L1 DOOR EXIT IDENTIFIER & FIRST CLASS RT SIDE EMER PATH LIGHTS ARE INOPERATIVE. R & R CONTROL MODULE ASSEMBLY IAW AMM 33-51-11 & BATTERY PACK IAW AMM 33-51-07. OPERATIONAL CHECKED NORMAL. SEE ALSO AALA 20160518002.

Part: OVEN — CONTAMINATED (GALLEY) · airframe 45,285 hrs · 12,838 cycles

DURING FLIGHT, WHILE USING THE OVENS, A GRAY SMOKE ALONG WITH A STRONG, ACRID ODOR BECAME PRESENT. THE FLIGHT ATTENDANT TURNED OFF THE OVENS & THE SMOKE DISSIPATED. THE FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. CLEANED OVENS. PERFORMED OPERATIONS CHECK IAW AMM 25-31-00. THE ACFT WAS NOT GNDED.

Part: BOTTLE — MALFUNCTIONED (EVAC SLIDE) · airframe 44,038 hrs · 12,568 cycles

LEFT OVERWING SLIDE FAILED TO UNLOCK & DEPLOY. INSTALLED 8130 BOTTLE IAW MM 25-65-02. LEFT OVERWING SLIDE DEPLOYED CORRECTLY IAW PC 2905.

Part: SENSOR — FAULTY (LT MLG) · airframe 41,249 hrs · 11,897 cycles

LANDING GEAR DOOR LIGHT ILLUMINATED AFTER GEAR RETRACTION. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. PLACARDED LG DOOR SENSOR S10076 IAW MEL 32-18D. FLIGHT CONTINUED TO DESTINATION. REPLACED SENSOR ON 10/15/2014. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: WIRE — DAMAGED (CABIN) · airframe 40,840 hrs · 11,796 cycles

ESCAPE PATH LIGHT WIRING AT SEAT 13DEF WAS DAMAGED. REPAIRED WIRING FOR ESCAPE PATH LIGHT AT SEAT 13DEF. OPERATIONS CHECKED NORMAL.

Part: PAN — WORN (DOOR) · airframe 40,148 hrs · 11,610 cycles

HANDLE PAN ON THE OUTSIDE OF DOOR WORN AT TOP CTR & LOWER CTR NEXT TO CAM BASKET. INSTALLED NEW HANDLE PAN IAW AARD 51-00-05-1.

Part: PRESSURE SWITCH — FAILED (OIL SYSTEM) · airframe 39,926 hrs · 11,553 cycles

MIA CREW REPORTED LT HAND OIL FILTER EICAS ILLUMINATED ON CLIMB OUT INTERMITTENTLY. EMER DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. R & R THE PRESS OIL FILTER DIFFERENTIAL PRESS SWITCH & THE SCAVENGE OIL FILTER DIFFERENTIAL PRESS SWITCH. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,802 hrs · 11,519 cycles

FORWARD CARGO COMPARTMENT, DOORWAY TRANSITION PANEL FROM STATIONS 580 TO 645 HAS SCATTERED SURFACE CORROSION. REMOVED CORROSION & REPLACED TRANSITION PANEL.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,802 hrs · 11,519 cycles

FORWARD CARGO COMPARTMENT, DOOR SILL SUPPORT STRUCTURE CORRODED FROM FRAME STATIONS 560 TO 620. REMOVED CORROSION & REPLACED TRANSITION PANEL.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 39,802 hrs · 11,519 cycles

MAIN CABIN SEAT TRACK GOUGED AT BS 870 & RBL 25. R & R SECTION OF SEAT TRACK IAW SRM 53-00-52.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,802 hrs · 11,519 cycles

AFT LOWER CARGO DOOR SILL UPPER FLOOR SUPPORT CHANNEL IS CORRODED UNDERNEATH AT SEVERAL NUTPLATES & ON TOP. REMOVED CORROSION & REPLACED SIDE PANEL.

Part: DOUBLER — GOUGED (R1 DOOR) · airframe 39,802 hrs · 11,519 cycles

RIGHT NR 1 DOOR INNER DOUBLER IS GOUGED UNDER UPPER HINGE ARM TORQUE TUBE FROM STATIONS 338 TO 302. ACCOMPLISHED REPAIR IAW ESO 90284 PG 1 STEP 1 1 1 12.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,802 hrs · 11,519 cycles

FORWARD CARGO COMPARTMENT, DOOR SILL SUPPORT STRUCTURE UNDERSIDE CORRODED AT NUTPLATES FROM FRAME STATIONS 560 TO 620. REMOVED CORROSION & REPLACED TRANSITION PANEL FROM STATIONS 560 TO 645.

Part: TRANSITION PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 39,802 hrs · 11,519 cycles

FORWARD CARGO COMPARTMENT, RT FLOOR TRANSITION PANEL CORRODED FROM FRAME STATIONS 646 TO 666. REMOVED CORROSION & REPAIRED RT FLOOR TRANSITION PANEL.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 39,802 hrs · 11,519 cycles

AFT CARGO PIT, NR 1 FLOOR PANEL UNDERSIDE HAS CORROSION AROUND MOST SCREW HOLES. REMOVED CORROSION & INSTALLED NEW PANEL IAW AARD 51-20-00-1.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,802 hrs · 11,519 cycles

STATION 1635 AT RBL 20 FLOOR SUPPORT INTERCOSTAL CORRODED. R & R INTERCOSTAL IAW AARD 51-00-05.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 39,802 hrs · 11,519 cycles

G4B GALLEY RT SECTION COFFEE MAKER MOUNTING PLATE IS CORRODED. R & R COFFEE MAKER MOUNTING PLATE IAW AARD 25-30-00-8 PAGES 1 - 2.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 39,802 hrs · 11,519 cycles

STATION 1640 FLOORBEAM TEE CAP CORRODED AT RBL 18. REPAIRED 1640 FLOORBEAM FROM LBL 14 TO RBL 36 IAW SRM 53-00-51 REPAIR 10.

Part: FLOOR SUPPORT — CORRODED (BS 1635) · corrosion level 2 · airframe 39,802 hrs · 11,519 cycles

FLOOR SUPPORT BS 1635 & LBL 20 CORRODED. R & R FLOOR SUPPORT IAW SRM 51-40-02.

Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 39,802 hrs · 11,519 cycles

CORROSION ON LT NR 4 DOOR CUT OUT, LOWER SILL, UPPER SURFACE, AT AFT END. R & R ANGLE IAW SRM 51-40-02.

Part: BRACKET — CORRODED (LAV DOOR) · corrosion level 2 · airframe 39,802 hrs · 11,519 cycles

LAVATORY K DOOR BRACKET CORRODED. R & R BRACKET IAW CMM 25-40-85 PG 706.

Part: MOUNT — CORRODED (AFT GALLEY) · corrosion level 2 · airframe 39,802 hrs · 11,519 cycles

AFT GALLEY, THE RT AFT GALLEY MOUNT IS CORRODED. R & R GALLEY MOUNT IAW AARD 51-00-05.

Part: ANGLE — CORRODED (BS 365) · corrosion level 2 · airframe 39,802 hrs · 11,519 cycles

MAIN CABIN BS 365, RT NR 1 LOWER SILL ANGLE CORRODED. R & R ANGLE IAW SRM 51-40-02.

Part: SUPPORT — CORRODED (BS 330) · corrosion level 2 · airframe 39,802 hrs · 11,519 cycles

MAIN CABIN BS 330, RT NR 1 DOOR DRAIN PAN SUPPORT CORRODED. R & R DRAIN PAN SUPPORT IAW SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 39,802 hrs · 11,519 cycles

AFT CARGO PIT, CABIN UNDERFLOOR INTERCOSTAL CRACKED IN UPPER FLANGE FROM STATIONS 1580 TO 1600, BL 0. R & R THE CRACKED INTERCOSTAL IAW SRM 51-40-02.

Part: ACCESS PANEL — WORN (NR 2 PYLON) · airframe 39,802 hrs · 11,519 cycles

NR 2 PYLON ACCESS PANEL 443 - FRAME HAS A WORN EDGE. FABRICATED & INSTALLED PANEL IAW AARD 20-00-00-1.

Part: FILTER — DEFECTIVE (LT ENGINE) · airframe 39,465 hrs · 11,455 cycles

MIA CREW REPORTED INTERMITTENT LT HAND ENG OIL FILTER EICAS MESSAGE. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. REPLACED LT HAND ENG OIL SYS PRESS, SCAVENGE FILTER & OIL FILTER DIFFERENTIAL PRESS SWITCH. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: DOOR FRAME — CORRODED (R1 DOOR) · airframe 38,116 hrs · 11,119 cycles

CORROSION FOUND ON AFT FRAME FACE UNDER ASSIST HANDLE ON RT NR 1 DOOR. ACCOMPLISHED REPAIR IAW B757-52-031230.

Part: PRESSURE SWITCH — INOPERATIVE (RT ENGINE) · airframe 38,049 hrs · 11,096 cycles

CCS CREW REPORTED RT ENGINE SHUTDOWN ON DESCENT, SINGLE ENGINE TIME TWO MINUTES. EMERGENCY DECLARED FLIGHT LANDED CCS WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RT ENGINE TRANSIENT PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 37,229 hrs · 10,900 cycles

SEAT 4E, EMERGENCY LIGHT INOPERATIVE. RESEATED CONNECTER FOR SEAT 4E EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,229 hrs · 10,900 cycles

RIGHT NR 3 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RT NR 3 DOOR EXTERIOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 35,823 hrs · 10,577 cycles

SEAT NUMBER 4E EMERGENCY EXIT LIGHT INOPERATIVE. RE-SEATED CONNECTOR FOR SEAT 4E EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,672 hrs · 10,546 cycles

EMERGENCY EXIT LIGHT AT 36DEF BULL-NOSE INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT LIGHT AT 36DEF. OPS CHECK NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 35,672 hrs · 10,546 cycles

EMERGENCY EXIT LIGHT AT SEAT 36DEF INOPERATIVE. SECURED LOOSE CONNECTOR. OPS CHECK NORMAL.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 34,524 hrs · 10,294 cycles

ROW 32 EMERGENCY EGRESS LIGHT INOPERATIVE. RECONNECTED CONNECTOR AT SIDEWALL. OPS CHECK NORMAL.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 34,524 hrs · 10,294 cycles

LEFT NUMBER 1 DOOR EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT BATTERY AT LEFT NUMBER 1 DOOR LOCATION. OPS CHECK GOOD.

Part: SPLICE — LOOSE (EMERGENCY LIGHTS) · airframe 33,544 hrs · 10,088 cycles

EMERGENCY EXIT LIGHT AT SEAT 16D WAS INOPERATIVE DUE TO A WIRE SPLICE COMING LOOSE. RECRIMPED NEW SPLICE FOR EMERGENCY EXIT LIGHT AT SEAT 16D. OPS CHECK NORMAL.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,526 hrs · 9,886 cycles

CORROSION AFT PRESSURE DECK CABIN FLOOR STATIONS 1718 TO 1719 AND LEFT BUTTLINES 48 TO 51. CUT OUT DAMAGED SECTION AND INSTALLED DOUBLER REPAIR PER SRM 53-60-51-2R REPAIR 2 AND EA B757-53-022045.

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 32,526 hrs · 9,886 cycles

CORROSION ON REAR SPAR AT DEFUEL VALVE IRSS 206.75. REMOVED CORROSION PER SRM 51-10-02. REPAIRED PER EA B757-57-021959.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,526 hrs · 9,886 cycles

CABIN FLOOR AFT PRESSURE DECK TOP FLOORBEAM DOUBLER CORRODED STATION 1640 LEFT BUTTLINES 2 TO 10. INSTALLED DOUBLER PER SRM 53-60-51-2R.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 32,526 hrs · 9,886 cycles

FLOORBEAM UPPER TEE CORRODED AT BS 1640 AND RBL 56 TO 59. REPAIRED FLOORBEAM PER EA B757-53-021911.

Part: SEAL — DAMAGED (AILERON) · airframe 29,243 hrs · 9,280 cycles

LHR - INFLIGHT CDG-JFK. CREW REPORTED LEFT HYDRAULIC QUANTITY LOSS AND PRESSURE PROBLEMS. EMEREGNCY DECLARED FLIGHT DIVERTED LHR LANDED WITHOUT INCIDENT. FOUND RIGHT OUTBOARD AILERON PCA SEAL DAMAGED. REPLACED SEAL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: MODULE — LEAKING (STAB CONTROL) · airframe 27,413 hrs · 8,882 cycles

BOS - CREW REPORTED AIRCRAFT LOSING RIGHT HYDRAULIC QUANTITY. EMERGENCY DECLARED RETURNED BOS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEAK ON STAB CONTROL MODULE. REPLACED MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FSEU — FAULTED (TE FLAP) · airframe 25,514 hrs · 8,485 cycles

JFK - CREW REPORTED TRAILING EDGE FLAP DISAGREE MESSAGE ON APPROACH. QRH PROCEDURE ACCOMPLISHED. EMERGENCY DECLARED LANDED JFK WITHOUT INCIDENT. FOUND FLAP SLAT ELECTRONIC UNIT AT FAULT. REPLACED UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DIRTY (CABIN) · airframe 23,679 hrs · 8,011 cycles

SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 36D INOPERATIVE. CLEANED AND RESEATED CONNECTOR.

Part: CONNECTOR — DIRTY (CABIN) · airframe 23,679 hrs · 8,011 cycles

SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 4E INOPERATIVE. CLEANED AND RESEATED CONNECTOR.

Part: CONNECTOR — LOOSE (CABIN) · airframe 23,580 hrs · 7,993 cycles

EMERGENCY LIGHTS AT SEAT 18DEF INOPERATIVE. SECURED LOOSE CONNECTOR UNDER SEAT 18F EMERGENCY LIGHTS. OPS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,731 hrs

SJU EMERGENCY LIGHTS FROM ROWS 16D TO 25D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM ROWS 16D TO 25D.

Part: CIRCUIT BREAKER — TRIPPED (FUEL SYSTEM) · airframe 22,124 hrs · 7,500 cycles

TPA - INFLIGHT DFW-MIA - LEFT FUEL VALVE MESSAGE LIGHT ON. LANDED TPA WITHOUT INCIDENT. FOUND LEFT SPAR VALVE CIRCUIT BREAKER OUT. RESET BREAKER AND OPERATED LEFT SPAR VALVE NUMEROUS TIMES AND NO FAULTS NOTED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: DUCT — LEAKING (NR 1 ENGINE) · airframe 20,876 hrs

LAX - ON CLIMB THROUGH 1000 OVERHEAT LIGHT ILLUMINATED. CREW TURNED OFF ENGINE BLEED SYSTEM AND LIGHT EXTINGUISHED. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. ON LANDING FOUND NUMBER ONE ENGINE ACCESS PANELS OPEN. REPLACED NUMBER ONE ENGINE HIGH PRESSURE NUMBER 6 DIFFUSER DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT AT SEAT ROW 26D INOPERATIVE. REPLACED BATTERY PACK M100801 FOR EMERGENCY LIGHT AT SEAT ROW 26D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PLACARD — LOOSE (EMERGENCY EXIT)

MIA - EMERGENCY LIGHT AT FORWARD LEFT WING EXIT SIGN AT SEAT BOTTOM LEVEL HAS DIRECTIONAL DECAL FALLING OFF. REPLACED DECAL FOR EMERGENCY LIGHT AT FORWARD LEFT WING EXIT SIGN AT SEAT BOTTOM LEVEL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SIGN — BROKEN (EMERGENCY LIGHT)

MIA - OVERHEAD EMERGENCY EXIT LIGHT SIGN AT LEFT NUMBER THREE DOOR FELL OFF. REINSTALLED OVERHEAD EMERGENCY EXIT SIGN AT LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: RELAY — INOPERATIVE (MLG)

MIA - AFTER GEAR RETRACTION, GOT NOSE AIR GROUND DISAGREE STATUS MESSAGE. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED SYSTEM ONE AIR GROUND RELAY K177. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (CABIN)

MIA NO TRIP/30 DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING SEAT 3JH INOPERATIVE. FOUND SIDEWALL PLUG DISCONNECTED AND RECONNECTED. SYSTEM GROUND CHECKED NORMAL OPERATION.