N656AA

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 69,997 hrs · 24,306 cycles

LEFT NR 1 DOOR EXTERIOR EMER LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 1 DOOR EXTERIOR EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,177 hrs · 24,026 cycles

CORROSION ON INNER CHORD FROM STATION 560 TO 620 & WL 208.10. INSTALLED INNER CHORD & TWO SPLICES IAW AARD 53-30-13-1A.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,177 hrs · 24,026 cycles

CORROSION ON WEB ABOVE FWD CARGO DOOR CUT OUT AT BS 590. REMOVED FLOOR PANEL STATION 560 - 620, RBL 46-64, REMOVED CORRODED WEB & INSTALLED NEW WEB.

Part: CONNECTOR — BROKEN (CABIN) · airframe 69,177 hrs · 24,026 cycles

RIGHT ROW 28 EMERGENCY LIGHT CONNECTOR BROKEN. REPLACED RT ROW 28 EMERGENCY LIGHT CONNECTOR, OPERATIONS CHECKED NORMAL.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,177 hrs · 24,026 cycles

BS 1020 RT WING UPPER WING TO BODY PANEL ATTACH ANGLE CORRODED. R & R FILLER IAW AARD 51-20-00-1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,177 hrs · 24,026 cycles

STATION 1680 AT LBL 12 T CAP HAS CORROSION UNDER METAL CLIP. FLOORBEAM FOUND TO BE OUT OF LIMITS AFTER CORROSION REMOVED. REPAIRED FLOORBEAM IAW SRM 53-60-51.

Part: SKIN — DENTED (BS 570-577) · airframe 69,177 hrs · 24,026 cycles

LEFT EXTERIOR FUSELAGE SKIN DENTED FROM BS 570 TO 577 & STRINGERS 16 TO 17 LT. REMOVED DAMAGE, INSTALLED DOUBLER & FILLER IAW SRM 53-00-02.

Part: STRAP — CORRODED (BS 1680) · corrosion level 2 · airframe 69,177 hrs · 24,026 cycles

NUTPLATE & METAL STRAP IS CORRODED ON T CAP AT BS 1680 AT LBL 12. R & R NUTPLATE & METAL STRAP ON T CAP AT IAW AARD 51-00-05 REPAIR 1.

Part: INTERCOSTAL — CORRODED (ZONE 200) · corrosion level 2 · airframe 69,177 hrs · 24,026 cycles

CORROSION ON INTERCOSTAL INBD OF RT NR 1 DOOR SILL FROM BS 324 TO 365. R & R INTERCOSTAL IAW RD 51-00-05.

Part: ATTACH ANGLE — DAMAGED (BS 1100) · airframe 69,177 hrs · 24,026 cycles

KEEL BEAM ATTACH ANGLE AT STATION 1100 HAS ELONGATED HOLES. INSTALLED NEW KEEL ANGLE IAW SRM 51-40-02.

Part: MOUNT — CORRODED (LAVATORY) · corrosion level 2 · airframe 69,177 hrs · 24,026 cycles

AFT RT LAVATORY THE INBD AFT MOUNT PAD IS CORRODED. R & R MOUNT PAD IAW SRM 51-40-02.

Part: NUT PLATE — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 69,177 hrs · 24,026 cycles

NR 1 PYLON AFT FAIRING MATTING SURFACES TO STRINGER PANEL NUTPLATE CORRODED THROUGHOUT ON BOTH SIDE. R & R 17 NUTPLATES IAW SRM 51-40-02.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,843 hrs · 23,917 cycles

EMERGENCY AISLE LIGHT SEAT MOUNTED FROM STATIONS 430 TO 625 INOPERATIVE. REPLACED BATTERY PACK M10798, OPERATIONS CHECKED NORMAL.

Part: WIRE — PULLED (CABIN) · airframe 67,922 hrs · 23,578 cycles

EMERGENCY PATHWAY LIGHT AT SEAT 28D DID NOT ILLUMINATE WHEN SWITCH WAS TURNED ON. WIRE PULLED OUT AT SIDEWALL PANEL TO E&E CONNECTOR. RE-CONNECTED WIRE. OPERATIONS CHECKED NORMAL

Part: WIRE — PULLED (CABIN) · airframe 67,922 hrs · 23,578 cycles

EMERGENCY EXIT LIGHT AT SEAT 28D INOPERATIVE. FOUND WIRE PULLED FROM SIDEWALL TO SEAT EE LIGHTS CONNECTOR. REPINNED CONNECTOR FOR SEAT 28A. OPERATIONS CHECKED NORMAL

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,941 hrs · 23,240 cycles

EMERGENCY LIGHT AT ROW 10 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT ROW 10. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,941 hrs · 23,240 cycles

EMERGENCY LIGHT AT ROW 15 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT ROW 15. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,941 hrs · 23,240 cycles

EMERGENCY LIGHT AT ROW 26 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT ROW 26. OPS CHECK NORMAL.

Part: IDG — FAILED (ZONE 100) · airframe 65,305 hrs · 22,656 cycles

EWR - INFLIGHT BGI-JFK CREW REPORTED LEFT AC BUSS FAILED. EMERGENCY DECLARED FLIGHT DIVERTED EWR LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED INTEGRATED DRIVE GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,070 hrs · 22,570 cycles

STRINGER 25 LEFT CORRODED AT STATION 1713. INSTALLED STRINGER SPLICE REPAIR PER EA B757-53-026932.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 3 · airframe 65,070 hrs · 22,570 cycles

THE BELLFRAME CORRODED AT STATION 1660 BETWEEN STRINGERS 29 AND 28 RIGHT. INSTALLED BELLFRAME REPAIR PER EA B757-53-026955.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 65,070 hrs · 22,570 cycles

SHEAR TIE CORRODED AT STATION 1660, BETWEEN STRINGERS 29 AND 28 RIGHT. INSTALLED NEW SHEAR TIE PER EA B757-53-026955.

Part: PRESSURE DECK — CORRODED (FUSELAGE) · corrosion level 3 · airframe 65,070 hrs · 22,570 cycles

CORROSION AT RIGHT WHEEL WELL PRESSURE DECK FROM STATIONS 1121 AND 1135, RIGHT BUTTLINE 65. REMOVED CORROSION PER SRM 51-10-02 0G AND REPAIRED PER EA B757-53-026902.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,665 hrs · 22,424 cycles

EMERGENCY LIGHTS AT AFT CARGO DOOR, ABOVE ROW 27, SIGN ABOVE OVERWING EMERGENCY EXITS INOPERATIVE. REPLACED BATTERY PACK M10699. OPS CHECK NORMAL.

Part: ANTI-SKID VALVE — INOPERATIVE (NR 3) · airframe 64,069 hrs · 22,212 cycles

VVI - INFLIGHT MIA-LPB. CREW REPORTED ANTI-SKID LIGHT ILLUMINATED. FLIGHT DIVERTED VVI LANDED WITHOUT INCIDENT. DEFERRED ANTI SKID SYSTEM INOPERATIVE PER MEL 32-4A. REPLACED NUMBER 3 ANTI SKID VALVE ON 05/07/2012 AT SFO. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,450 hrs · 21,241 cycles

STATION 1690 STRINGER 29 RIGHT CORRODED. ACCOMPLISHED REPAIR PER SRM 53-00-03-2R-1.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,450 hrs · 21,241 cycles

STATION 1692 STRINGER 29 RIGHT HAS CORROSION. INSTALLED STRINGER 29 RIGHT DOUBLER APPROXIMATELY STATION 1685 TO 1692 AND REINSTALLED WEB AT STRINGER 29 RIGHT STATION 1680 TO 1700 PER EA B757-53-017678.

Part: PLATE — CORRODED (DEFUEL VALVE) · corrosion level 2 · airframe 61,450 hrs · 21,241 cycles

LEFT DEFUEL VALVE ACTUATOR ADAPTER PLATE FAILED RESISTANCE CHECK PER CARD F1553AD. INSTALLED LEFT DEFUEL VALVE PER M/M 28-22-01. INSTALLED DEFUEL VALVE ACTUATOR PER ECO F1553AD.

Part: SKIN — DENTED (FUSELAGE) · airframe 61,450 hrs · 21,241 cycles

DENT ON THE RIGHT FUSELAGE LOCATED AT STATION 480. INSTALLED DOUBLER USING PER SRM 53-00-01-2R 2 AND EA 757-53-017663.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,450 hrs · 21,241 cycles

INTERCOSTAL AT STATIONS 1440 TO 1460 STRINGER 27 RIGHT HAS CORROSION ON FORWARD END OF WEB. REPLACED WEB AS PER SRM 51-10-02-0G.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,450 hrs · 21,241 cycles

CORROSION ON AFT TOP DECK. INSTALLED DOUBLER REPAIR PER EA B757-53-017440 AND SRM 53-60-51-2R.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 61,450 hrs · 21,241 cycles

FLOORBEAM STATION 1702 TO 1721 RIGHT BUTTLINE 39.5 DAMAGED. REPLACED FLOORBEAM PER SRM 51-10-02 OG.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 61,450 hrs · 21,241 cycles

FLOORBEAM STATION 1702 TO 1721 RIGHT BUTTLINE 15 DAMAGED. REPLACED FLOORBEAM PER SRM 51-10-02-OG.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 61,450 hrs · 21,241 cycles

FLOORBEAM STATION 1702 TO 1720 DAMAGED. REPLACED FLOORBEAM PER SRM 51-10-02-OG.

Part: DOOR FRAME — CRACKED (R2 DOOR) · airframe 61,450 hrs · 21,241 cycles

CRACK IN INNER CHORD, AT DOOR UPPER HINGE CUTOUT, LOCATED AT NUMBER 3 DOOR STOP, RIGHT NUMBER 2 PASSENGER/SERVICE ENTRY DOOR. ROUTED OUT THE DAMAGE AND INSTALLED A DOUBLER REPAIR AS PER EA COMP-52-17430 AT THE UPPER HINGE CUTOUT OF THE RIGHT NUMBER 2 DOOR.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,450 hrs · 21,241 cycles

CORROSION ON AFT GALLEY MOUNT LUGS LEFT BUTTLINE 51.1. INSTALLED G4 GALLEY FORWARD LEFT FLOOR FITTING IAW SRM 51-10-02-0G.

Part: SKIN — DENTED (CARGO DOOR) · airframe 61,450 hrs · 21,241 cycles

FORWARD CARGO DOOR SKIN DENTED 9 INCHES FROM FORWARD EDGE AND 11 INCHES FROM BOTTOM. INSTALLED EXTERNAL DOUBLER ON OUTER SKIN IAW SRM 52-30-01-2R 4.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,450 hrs · 21,241 cycles

CORROSION ON UPPER SILL PLATE FROM STATIONS 1380 1440. REMOVED AND REPLACED UPPER T-CHORD FOR AFT CARGO DOOR THRESHOLD FROM STATIONS 1360 TO 1460 PER SRM 51-10-02-0G.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,450 hrs · 21,241 cycles

INTERCOSTAL AT STATIONS 1440 TO 1460 STRINGER 27 HAS CORROSION ON FORWARD END OF WEB. WEB AND ALL FASTENERS ARE INSTALLED PER SRM 51-10-02-G10.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,450 hrs · 21,241 cycles

CORROSION ON GALLEY MOUNT LUGS AT STATION 1680 BUTTLINE 0. INSTALLED G4 GALLEY FORWARD CENTER FLOOR FITTING IAW SRM 51-10-02-0G.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,450 hrs · 21,241 cycles

FOUND CORROSION ON FORWARD END OF WEB AT STATION 1380. REMOVED AND REPLACED WEB BETWEEN STATIONS 1380 TO 1440 STRINGER 26 RIGHT PER SRM 51-10-02-0G.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,450 hrs · 21,241 cycles

HEAVY CORROSION ON LEFT WEB AT OUTBOARD CREASE ANGLE JUST AFT OF STATION 940. INSTALLED NEW WEB PER SRM 51-10-02-0G AND EA B757-53-017446.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,450 hrs · 21,241 cycles

CORROSION AT WEBBING, RIGHT CREASE ANGLE BETWEEN STATIONS 980 AND 1000. REPLACED CREASE ANGLE FROM FRAME STATIONS 900 TO 1040, RIGHT BUTTLINES 63 TO 64, WATERLINE 208 AT THE CABIN FLOOR PER SRM 51-10-02-0G.

Part: BEAM — DAMAGED (CARGO DOOR) · airframe 61,450 hrs · 21,241 cycles

NUMBER 2 CARGO DOOR LOWER EDGE BEAM IS DENTED AND HAS DAMAGE. INSTALLED NEW EDGE BEAM PER ESO 90121.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,450 hrs · 21,241 cycles

WEB CORRODED FROM STATIONS 1400 TO 1420. REPLACED WEB PER SRM 51-10-02-0G.

Part: SKIN — DENTED (LE SLAT) · airframe 61,450 hrs · 21,241 cycles

LEFT WING AT NUMBER 2 SLAT, UPPER SKIN, 42 INCHES FROM OUTBOARD END 7 INCHES FROM LEADING EDGE DENT IN SKIN. CUT OUT DENT AND CORROSION THEN INSTALLED FLUSH DOUBLER PER AARD 57-43 00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 61,450 hrs · 21,241 cycles

CORROSION AROUND FASTENER ON TOP 57 INCHES FROM INBOARD END. REMOVED CORROSION FROM TOP SKIN 57 INCHES FROM END AND INSTALLED DOUBLER PER AARD 57-43-00-1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 61,450 hrs · 21,241 cycles

LEFT WING, AT NUMBER 3 SLAT, 35 INCHES FROM INBOARD END, TOP SKIN, 8 INCHES FROM LEADING EDGE SKIN CORRODED. INSTALLED FLUSH SKIN REPAIR ON NUMBER 3 SLAT PER AARD 57-43-01.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 61,450 hrs · 21,241 cycles

NUMBER 10 SLAT UPPER SKIN 67 INCHES FROM INBOARD END HAS CORRODED FASTENER. FABRICATED DOUBLERS AND FILLER REPAIR PER AARD 57-43-001.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,450 hrs · 21,241 cycles

INTERCOSTAL AT STATIONS 1360 TO 1380 4 INCHES OUTBOARD OF STRINGER 27 HAS CORROSION ON WEB AND FOOT OF WEB. REPLACED INTERCOSTAL PER SRM 51-10-02-G-9.

Part: SKIN — DEBONDED (LE SLAT) · airframe 61,450 hrs · 21,241 cycles

RIGHT WING NUMBER 9 SLAT HAS DENT WITH DISBOND INDICATIONS ON TOP AND BOTTOM SKINS 43 INCHES INBOARD OF OUTBOARD END. REMOVED DAMAGED AREA AND INSTALLED EXTERNAL HOT BOND DOUBLER REPAIR PER SRM 51-70-10-2R.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 61,450 hrs · 21,241 cycles

RIGHT WING NUMBER 7 SLAT LEADING EDGE HAS SKIN CORROSION, ADJACENT TO A FASTENER LOCATION ON THE LEADING EDGE SKIN SURFACE APPROX 2.5 FEET INBOARD OF THE OUTBOARD EDGE. CORROSION BLENDED TO FINAL SKIN THICKNESS OF .023 INCH. CUT OUT DAMAGE PER AARD. FABRICATED AND INSTALLED REPAIR DOUBLERS PER AARD 57-43-01.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 61,450 hrs · 21,241 cycles

NUMBER 8 SLAT CORROSION AROUND FASTENER APPROXIMATELY 2 INCH FROM OUTBOARD END OF SLAT IN UPPER SKIN ALONG TRAILING EDGE. REMOVED CORROSION PER AARD PER 57-43-00-3 ON OUTBOARD AFT UPPER END OF SLAT SKIN. INSTALLED DOUBLER PER AARD 57-43-00-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,450 hrs · 21,241 cycles

INTERCOSTAL CRACKED AT STATIONS 1580 TO 1600 BUTTLINE 0. INSTALLED DOUBLER IAW SRM 51-70-13-0G.

Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 61,710 hrs · 21,334 cycles

RIGHT WING UNDER DEFUEL VALVE ADAPTER SHAFT PLATE HAS PITTING CORROSION. REPAIRED PER EA B757-57-017276 DATED 06-23-11.

Part: PROBE — FAILED (TAT) · airframe 60,911 hrs · 21,050 cycles

MIA - CREW REPORTED LOSS OF TOTAL AIR TEMPERATURE PROBE, AUTO THROTTLE, AUTOPILOT, AND SOME NAVIGATIONAL CAPABILITIES. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED TAT PROBE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: OVEN — DIRTY (GALLEY) · airframe 59,709 hrs · 20,604 cycles

JFK INFLIGHT BOS-MIA - FLIGHT ATTENDANTS REPORTED SMOKE COMING FROM INSIDE FIRST CLASS GALLEY OVEN. EMERGENCY DECLARED FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. FOUND FOOD BURNED ON HEATING ELEMENT OF OVEN CAUSING SMOKE. REPLACED OVEN. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,172 hrs · 19,662 cycles

DENT IN FUSELAGE STATION 1681 TO STATION 1701 AND STRINGER 19 LEFT. INSTALLED DOUBLERS PER SRM 53-00-01-2R2 AND SRM 53-00-03-2R1.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,172 hrs · 19,662 cycles

FLOORBEAM CRACKED AT STATION 700 AT BUTTLINE 24 LEFT TO 48 LEFT. REPAIRED FLOORBEAM PER AARD 53-30-51-2R2, SRM 53-00-51-2R3, ENGINEERING AUTHORIZATION B757-51-007981 AND ESO 90309.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 57,172 hrs · 19,662 cycles

LEFT WING NUMBER 2 SLAT HAS CORROSION ON INBOARD TRAINING EDGE LOWER SURFACE 2 INCHES FROM AFT EDGE. INSTALLED 350 DEGREE HOT BOND REPAIR PER SRM 51-70-10-2R 4.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - LEFT FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT FORWARD OVERWING EMERGENCY LIGHT.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT 35 INOPERATIVE. REPLACED CONNECTOR AT WALL FOR SEAT 35.

Part: LAMP — BROKEN (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHTS AT ROW 25 INOPERATIVE. REPLACED LAMP AT ROW 25 EMERGENCY LIGHTS.

Part: NUT — LOOSE (OXYGEN MASK) · airframe 54,066 hrs

MCI INFLIGHT SFO TO STL - CREW REPORTED OXYGEN BOTTLE PRESSURE LOW. LANDED MCI WITHOUT INCIDENT. FOUND CAPTAINS MASK COMPARTMENT LEAKING. TIGHTEN B NUT AT CAPTAINS MASK COMPARTMENT. REPLACED CREW OXYGEN BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACTUATOR — INOPERATIVE (RT MLG DOOR)

SEA INFLIGHT T1603/09AUG - RIGHT MAIN GEAR DOOR REMAINED OPEN ON GEAR EXTENSION. DOOR WARNING AND GEAR DOOR EICAS MESSAGE ILLUMINATED. LANDED SEA WITHOUT INCIDENT. REPLACED RIGHT MAIN GEAR DOWN LOCK ACTUATOR LINE AND HYDRAULIC EXTENSION AND RETRACTOR FUSES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 4E INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 4E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 28D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 28D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 24D INOPERATIVE. REINSTALLED EMERGENCY LIGHT PLUG FOR SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT AT FORWARD RIGHT OUTSIDE OVERWING INOPERATIVE. REPLACED EMERGENCY LIGHT AT FORWARD RIGHT OUTSIDE OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT AT RIGHT AFT SIDEWALL OVERWING INOPERATIVE. REPLACED EMERGENCY LIGHT AT RIGHT AFT SIDEWALL OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FITTING — OVERSIZED (BULKHEAD)

TUL - OUTBOARD LOWER FORWARD HOLE OVERSIZED WHEN CRACK REMOVED AT NR 1 MID BULKHEAD FITTING. AREA IS 0.640 BY 0.640 WITH A DEPTH OF 0.250. FABRICATED BUSHING AND INSTALLED PER ESO 90309. 757 SRM 54-50-02, 51-20-07, 757 AARD 54-50-003, SERVICE BULLETIN 757-54-A0039, FCD FF0377G, AND BOEING COMMUNICATION AAL-TUL-04-00172F FOR OUTBOARD LOWER FORWARD HOLE AT NR 1 MID BULKHEAD FITTING.

Part: TRANSMISSION — MALFUNCTIONED (T/E FLAP)

MIA T921/21 EN ROUTE MCO-MIA TRAILING EDGE FLAP DISAGREE. FLAPS INDICATED 20 DEGREES WITH HANDLE AT 25 DEGREE POSITION. LEFT HAND OUTBOARD GEAR BOX TRANSMISSION POPPED. RESET INDICATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 18D INOPERATIVE. RECONNECTED EMERGENCY EXIT ILGHT WIRE AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONTROLLER — FAILED (E/E BAY)

SJU - FLT 1013 - EN ROUTE BOS-AUA - UNABLE TO CONTROL COCKPIT OR CABIN TEMPERATURE IN MANUAL OR AUTOMATIC MOD. ALL 3 ZONE TEMPERATURE CONTROL VALVE CIRCUIT BREAKERS POPPED. AIR INTERRUPTED AND LANDED SJU WITHOUT INCIDENT. REPLACED CABIN ZONE TEMPERATURE CONTROLLER PER MM. CLEANED THREE CABIN TEMPERATURE SENSORS. OPERATIONS CHECKED ALL THREE ZONE TEMPERATURES AND FOUND WORKING. RESET ZONE TEMPERATURE CIRCUIT BREAKERS. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN FIRST CLASS AND FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN FIRST CLASS AND FORWARD GALLEY. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN MID-GALLEY AREA INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: FLOOR BEAM — GOUGED (BS 405)

AFW - FOUND BLENDED GOUGE ON FLOOR BEAM IS BEYOND SRM LIMITS. (M)

Part: RIB — CORRODED (BS 817)

AFW - AFTER REMOVING CORROSION, FOUND REMAINING METAL BEYOND SRM LIMITS ON RIB. REPAIR PER MRB 757-916. (M)

Part: FLOOR BEAM — CORRODED (BS 377)

AFW - AFTER REMOVING CORROSION, REMAINING METAL IS BEYOND SRM LIMITS ON FLOOR BEAM. REPAIR PER MRB 757-914. (M)

Part: FLOOR BEAM — CORRODED (BS 365)

AFW - BLENDED CORROSION, REMAINING METAL IS BEYOND SRM LIMITS ON FLOOR BEAM. REPAIR PER MRB 757-915. (M)

Part: STRUCTURE — CORRODED (BS 370)

AFW - AFTER REMOVING CORROSION, FOUND REMAINING METAL IS BEYOND SRM LIMITS. REPAIR PER MRB 757-913. (M)

Part: SILL — CORRODED (L2 DOOR)

AFW - AFTER REMOVING CORROSION, FOUND REMAINING MATERIAL BEYOND SRM LIMITS ON LOWER L2 DOOR SILL. REPAIR PER MRB 757-919. (M)

Part: DOOR PAN — GOUGED (CABIN)

AFW - FOUND L4 DOOR PAN HAS GOUGE BEYOND SRM LIMITS. REPAIR PER MRB 757-921. (M)

Part: BLKHD STIFFENER — CORRODED (BS 1180)

AFW - FOUND BLENDED CORROSION BEYOND SRM LIMITS ON BULKHEAD STIFFENER. REPAIR PER MRB 757-917. (M)

Part: KEEL BEAM — CORRODED (BS 1170)

AFW - FOUND KEEL BEAM HORIZONTAL WEB HAS CORROSION. PER MRB 757-747. (M)