N690AA

Part: TRANSMITTER — FAILED (ENGINE TACH) · airframe 76,787 hrs · 21,398 cycles

DURING TAKEOFF CREW REPORTED RT ENGINE N3 INDICATION WAS ERRATIC. DURING CLIMB RT ENG BLEED VALVE WAS CYCLING OFF & ON, ACFT DID NOT PRESSURIZE. CREW TURNED OFF RT ENG BLEED & ACFT BEGAN TO PRESSURIZE. RETURNED TO DEPARTURE & EMERGENCY DECLARED. LANDING UNEVENTFUL. REMOVED AND REPLACED RIGHT ENGINE N3 TACH TRANSMITTER IAW AMM 77-12-02 AND CONNECTOR BACKSHELL IAW WDM 71-51-22. ACCOMPLISHED RIGHT ENGINE RUN. SYSTEM CHECKED NORMAL IAW AMM 71-00-00.

Part: TRANSMITTER — DEFECTIVE (LT ENGINE) · airframe 76,787 hrs · 21,398 cycles

AIR INTERRUPT, RETURNED & EMER NOT DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB THE LT ENG BLEED OFF & LT PACK OFF INDICATORS ILLUMINATED. AT THE SAME TIME, THE RT CTR FUEL PUMP LOW PRESS LIGHT FLICKERED ON & OFF. R & R ENG SPEED CARD M10298 IAW AMM 77-12-03. R & R N3 TACHOMETER TRANSMITTER IAW AMM 77-12-13. PERFORMED ENG RUN & LEAK CHECKED IAW AMM 71-00-00. SYS CHECKED NORMAL.

Part: TACH GENERATOR — FAILED (LT ENGINE) · airframe 76,491 hrs · 21,331 cycles

RETURNED & EMER DECLARED. LANDING UNEVENTFUL. ACFT WAS OVERWEIGHT. DURING INITIAL CLIMB OUT AT 500 FEET LT ENG BLEED OFF FOLLOWED BY LT PACK OFF. FOLLOWED QRH PROCEDURES. THIS WAS FOLLOWED BY THE RT ENG BLEED & RT PACK CYCLING ON & OFF WITH THE RT CTR FUEL PUMP CYCLING ON & OFF. PERFORMED FIM 36-10-00-815-820 & 77-22-00-815-R00. REPLACED LT ENG N3 TACH GENERATOR. PERFORMED LT & RT ENG HIGH POWER RUNS. SYS CHECKED NORMAL.

Part: PRESSURE SWITCH — INOPERATIVE (FUEL SYSTEM) · airframe 75,827 hrs · 21,172 cycles

RIGHT CTR FUEL BOOST PUMP LOW PRESS LIGHT ON OVERHEAD & DISPLAYED ON EICAS. EMER DECLARED FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT CTR FUEL LOW PRESS SWITCH. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 72,214 hrs · 20,275 cycles

LT INBD AFT FLAP HAD PUNCTURE DAMAGE TO THE UPPER SURFACE WEDGE. ACCOMPLISHED REPAIR IAW EA B757-57-031577.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 3 · airframe 72,214 hrs · 20,275 cycles

AFT CARGO DOOR FORWARD FS FRAME AT STATION 1380 & STRINGER 25 RT CORRODED AT AREA OF CARGO DOOR DOWN SWITCH. ACCOMPLISHED REPAIR IAW SRM 53-00-07-2R-2.

Part: TRANSITION PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 72,214 hrs · 20,275 cycles

AFT CARGO RT TRANSITION PANEL HAS CORROSION BETWEEN BS 1360 & 1380. CORROSION REMOVED & ACCOMPLISHED REPAIR IAW EA 757-53-031551.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 72,214 hrs · 20,275 cycles

LT INBD MAIN FLAP UPPER ACCESS PANEL BETWEEN MAIN FRAME STA 215.67 TO 227.62 HAS THREE SMALL SPOTS OF CORROSION. REMOVED CORROSION & ACCOMPLISHED REPAIR IAW EA B757-57-031570.

Part: SKIN — DENTED (RT HORIZ STAB) · airframe 72,214 hrs · 20,275 cycles

DENT IN THE LOWER SKIN OF THE RT HORIZONTAL STABILIZER TORQUE BOX, APPROXIMATELY 3 INCHES FROM THE INBD END. ACCOMPLISHED REPAIR IAW EA B757-55-031555.

Part: SKIN — DENTED (FUSELAGE) · airframe 72,214 hrs · 20,275 cycles

FOUND TWO DENTS FROM STATIONS 600 TO 620, & STRINGERS 15 & 16 LT. INSTALLED DOUBLER IAW SRM 53-00-01-2R-3.

Part: IDG — FAILED (LT ENGINE) · airframe 69,648 hrs · 19,631 cycles

LAX - CREW REPORTED LEFT GENERATOR DRIVE LIGHT ILLUMINATED DURING TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT INTEGRATED DRIVE GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CHARGER — DISCHARGED (CABIN) · airframe 67,373 hrs · 19,077 cycles

AFT COACH SECTION EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER FOR AFT COACH SECTION EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,133 hrs · 19,005 cycles

ROWS 26 TO 36 SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK FOR ROWS 26 TO 36 SEAT EMERGENCY LIGHTS, OPS CHECK NORMAL.

Part: CHECK VALVE — DEFECTIVE (FUEL SYSTEM) · airframe 66,577 hrs · 18,818 cycles

LAX - CREW REPORTED UNWANTED FUEL TRANSFER FROM CENTER TANK TO RIGHT TANK. FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT MAIN TANK FORWARD AND AFT BOOST PUMP DISCHARGE CHECK VALVES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,437 hrs · 18,766 cycles

CORROSION ON TOP OF FRAME AT BS 1360 STRINGER 27 RIGHT. INSTALLED DOUBLER REPAIR PER EA B757-53-021729.

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,437 hrs · 18,766 cycles

CORROSION ABOVE KEEL BEAM AT BS 1120. ACCOMPLISHED SPLICE REPAIR PER EA B757-53-021490.

Part: FASTENER — DEBONDED (ZONE 200) · airframe 66,437 hrs · 18,766 cycles

FASTENER DISBONDED AT BS 1600 BETWEEN STRINGERS 1 AND 2. INSTALLED NEW FASTENERS PER EA B757-53-021495.

Part: DOOR FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,437 hrs · 18,766 cycles

CORROSION ON FORWARD LOWER CORNER OF AFT CARGO DOOR FRAME UNDER NET TIEDOWN FITTING. REMOVED CORROSION AND OVERSIZED TIEDOWN FITTING HOLES PER EA.

Part: BEAM — DAMAGED (CARGO DOOR) · airframe 66,437 hrs · 18,766 cycles

FORWARD CARGO DOOR BOTTOM EDGE BEAM IS DENTED AND GOUGED. REMOVED DAMAGED EDGE BEAM AND INSTALLED NEW EDGE BEAM PER ESO 90114.

Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 66,437 hrs · 18,766 cycles

FORWARD CARGO DOOR LOWER SEAL LANDING CORNER IS DAMAGED. REMOVED DAMAGED LOWER FORWARD SEAL LANDING CORNER AND INSTALLED NEW SEAL LANDING CORNER PER ESO 90114.

Part: SKIN — DAMAGED (CARGO BAY) · airframe 66,437 hrs · 18,766 cycles

NUMBER 2 CARGO DOOR OUTER SKIN HAS DAMAGED AT FORWARD LOWER CORNER AROUND 8 INCHES FROM FORWARD EDGE AND 2 INCHES FROM BOTTOM EDGE. TRIMMED OUT THE DAMAGED SECTION OF SKIN AND INSTALLED A DOUBLER REPAIR AT THE LOWER FORWARD CORNER OF THE NUMBER 2 CARGO DOOR PER SRM 52-30-01-2R 4.

Part: SLAT — CORRODED (LT WING) · corrosion level 2 · airframe 66,437 hrs · 18,766 cycles

CORROSION AROUND FASTENER 29 INCHS FROM INBOARD END ON BOTTOM SIDE. REMOVED CORROSION AND INSTALLED DOOUBLER PER AARD 57-43-00-1.

Part: SLAT — CORRODED (LT WING) · corrosion level 2 · airframe 66,437 hrs · 18,766 cycles

LEFT WING NUMBER 1 SLAT OUTBOARD END HAS CORROSION AROUND FASTENER. REMOVED BLENDED AREA AND INSTALLED DOUBLER PER AARD 57-43-00-1.

Part: SLAT — CORRODED (LT WING) · corrosion level 2 · airframe 66,437 hrs · 18,766 cycles

CORROSION AROUND FASTRNER 44 INCHES FROM OUTBOARD END ON BOTTOM SIDE ON NUMBER 1 SLAT. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 57-43-00-1.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,437 hrs · 18,766 cycles

RIGHT NUMBER 4 DOOR GUTTER SUPPORT CORRODED BETWEEN STATIONS 1640 TO 1660. INSTALLED RIGHT NUMBER 4 DRAIN SUPPORT FROM STATIONS 1640 TO 1660 PER SRM 51-10-02-OG.

Part: SLAT — CORRODED (LT WING) · corrosion level 2 · airframe 66,437 hrs · 18,766 cycles

LEFT WING NUMBER 3 SLAT - CORROSION AROUND FASTENER AT APPROXIMATE STATION 530. REMOVED CORROSION AND INSTALLED FLUSH DOUBLER PER AARD 57-43-00-1.

Part: SKIN — DENTED (FUSELAGE) · airframe 66,437 hrs · 18,766 cycles

FUSELAGE DENT WITH GOUGE AT STATION 760 STRINGER 15 LEFT. HFEC CHECKED AREA NO CRACKS FOUND. INSTALLED RIVET PER SRM 53-00-01-2R SECTION I PARAGRAPH 3.

Part: DOOR — DENTED (CABIN) · airframe 66,437 hrs · 18,766 cycles

LEFT NUMBER 1 DOOR IN WHITE STRIPE AREA HAS DENT. INSTALLED REPAIR DOUBLER PER SRM 52-10-01-2R 7.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 66,437 hrs · 18,766 cycles

NUMBER 2 CARGO DOOR OUTER SKIN HAS DAMAGED AT FORWARD LOWER CORNER AROUND 8 INCHES FROM FORWARD EDGE AND 2 INCHES FROM BOTTOM EDGE. TRIMMED OUT THE DAMAGED SECTION OF SKIN AND INSTALLED A DOUBLER REPAIR AT LOWER FORWARD CORNER OF THE NUMBER 2 CARGO DOOR PER SRM 52-30-01-2R4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,437 hrs · 18,766 cycles

CORROSION ON FLOORBEAM AT STATION 1660 RIGHT BUTTLINE 52. REPLACED T-CAP PER EA B757-53-021507AND AARD 51-10-05-1.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 66,437 hrs · 18,766 cycles

CORROSION ON FLOORBEAM AT STATION 1640 RIGHT BUTTLINE 54 JUST OUTBOARD OF DOUBLER. ACCOMPLISHED SPLICE REPAIR PER EA B757-53-021501.

Part: PANEL — CORRODED (NLG WW) · corrosion level 2 · airframe 64,537 hrs · 18,298 cycles

NOSE LANDING GEAR WHEEL WELL LEFT SIDE PANEL LOWER CHORD AT STATION 352 CORRODED. ACCOMPLISHED REPAIR PER EA NUMBER B757-53-017907.

Part: FILTER — DIRTY (CABIN) · airframe 61,742 hrs · 17,625 cycles

LAX - CREW REPORTED ELECTRICAL ODOR IN CABIN DURING CLIMBOUT. CAPTAIN TURNED OFF RIGHT PACK AND ISOLATION VALVE AND SMELL WENT AWAY. EMERGENCY DECLARED RETURNED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT AND RIGHT RECIRCULATION FILTERS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PRESSURE PANEL — CORRODED (RT MLG WW) · corrosion level 2 · airframe 61,492 hrs · 17,568 cycles

THE RIGHT WHEEL WELL UPPER PRESSURE DECK HAD CORROSION AT STATION 1160. REPAIRED PER EA B757-53-013113.

Part: PUMP — FAILED (LT ENGINE) · airframe 60,613 hrs · 17,362 cycles

HNL - INFLIGHT LIH-LAX. CREW REPORTED LEFT ENGINE HYDRAULIC PUMP FAILED. EMERGENCY DECLARED LANDED HNL WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT ENGINE DRIVEN PUMP AND CASE DRAIN FILTERS. CLEANED POWER TRANSFER UNIT INPUT PRESSURE SWITCHES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PRESSURE SWITCH — INOPERATIVE (FUEL SYSTEM) · airframe 60,442 hrs · 17,319 cycles

LAX - CREW REPORTED CENTER FUEL BOOST PUMP LIGHT FLICKERING DURING FLIGHT. FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE AND FERRIED TO TUL FOR FURTHER MAINTENANCE DUE TO REPEATS OF ISSUE. REPLACED PRESSURE SWITCH AND K10399 RELAY. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: RELAY — FAILED (FUEL SYSTEM) · airframe 60,427 hrs · 17,313 cycles

LAX - CREW REPORTED CENTER FUEL BOOST PUMP LOW PRESSURE LIGHT ILLUMINATED DURING FLIGHT. FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RELAYS K9902 AND KI10012. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (EXTERIOR)

DFW - RIGHT NUMBER 2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 DOOR EXTERIOR EMERGENCY EXIT LIGHT.

Part: CONNECTOR — LOOSE (CABIN)

DFW - EMERGENCY EXIT LIGHT AT SEAT 34D INOPERATIVE. SECURED LOOSE CONNECTOR BELOW SEAT 34D.

Part: LIGHT — INOPERATIVE (EXTERIOR)

DFW - LEFT NUMBER ONE DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER ONE DOOR EXTERIOR EMERGENCY EXIT LIGHT.

Part: CONNECTOR — LOOSE (ZONE 200)

DFW EMERGENCY LIGHT AT SEAT 34D INOPERATIVE. FOUND LOOSE CONNECTION. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 34D.

Part: PROBE — DAMAGED (NR 1 ENGINE) · 55,099 cycles

LAX INFLIGHT T824/22SEP. CREW REPORTED NR 1 ENGINE PRESSURE RATIO PROBLEMS AFTER TAKEOFF. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. FOUND PROBE MOUNT FLANGE BROKEN AND PNEUMATIC TUBE AND MOUNT BROKEN. ALSO FOUND NOSE COWL CRACKED. REPLACED PROBE SENSOR AND MOUNTING PLATE, PNEUMATIC TUBE AND MOUNT, AND NOSE COWL. SYSTEM GROUND CHECKED NORMAL OPS.

Part: GOVERNOR — INOPERATIVE (NR 1 ENGINE)

LAX INFLIGHT T285/20SEP. AT ABOUT 18000 FT ACFT YAWED TO THE LT AND ENGINE INSTRUMENTS SHOWED REDUCED POWER ON NR 1 ENGINE. FUEL FLOW WAS 3000 LBS. LESS ON NR 1 ENGINE. NR 1 ENGINE WOULD NOT PRODUCE FULL POWER WITH LT THROTTLE PUSHED TOWARDS FULL FORWARD. CREW COULD NOT CONTROL YAW. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED FUEL FLOW GOVERNOR FOR NR 1 ENGINE. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LIGHT — DAMAGED (LT OVERWING)

DFW - EMERGENCY LIGHT PLACARD AT LEFT HAND FORWARD OVERWING DAMAGED. REPLACED PLACARD FOR EMERGENCY LIGHT AT LEFT HAND FORWARD OVERWING. SYSTEM GROUND CHECK NORMAL OPERATION. (A)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHTS AT BULLNOSE SEAT 23ABC INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT BULLNOSE SEAT 23ABC. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,184 hrs

MIA - EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BLEED VALVE — LEAKING (RT ENGINE) · airframe 53,095 hrs

MIA INFLIGHT T725/09MAR - DURING CLIMB CREW RECEIVED RIGHT ENGINE OVERHEAT INDICATION. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED HIGH STAGE PNEUMATIC VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT FORWARD LEFT OVERWING INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT FORWARD LEFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS)

MIA - EMERGENCY FLASHLIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRAP — MISSING (FLASHLIGHT)

MIA - EMERGENCY FLASHLIGHT AT LEFT NUMBER TWO FLIGHT ATTENDANT SEAT HAS MISSING STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT LEFT NUMBER TWO FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRAP — MISSING (FLASHLIGHT)

MIA - EMERGENCY FLASHLIGHT AT LEFT NUMBER ONE DOOR MISSING HOLD DOWN STRAP. REPLACED HOLD DOWN STRAP FOR EMERGENCY FLASHLIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DFW - FOUND EMERGENCY LIGHT AT R4 DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)

DFW EMERGENCY LIGHT AT SEAT ROW 34 INOPERATIVE. FOUND CONNECTOR LOOSE AT SEAT ROW 34D. RESECURED CONNECTOR AT 34D FOR INOPERATIVE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR INOPERATIVE EMERGENCY LIGHTS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: LENS — MISSING (EMERGENCY LIGHT)

EMERGENCY PATH LIGHT LENS AND BULBS AT SEAT ROW 15 MISSING. REPLACED LENS AND BULBS AT SEAT ROW 15 FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT AT SEAT 23D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LAX - SEAT MOUNTED EMERGENCY EXIT LIGHTS STARTING AT ROW 9 AND LOWER EXIT LIGHTS AT 2 RIGHT AND 2 LEFT INOPERATIVE. REPLACED BATTERY PACK MODULE M10799 FOR SEAT MOUNTED EMERGENCY EIXT LIGHTS STARTING AT ROW 9 AND LOWER EXIT LIGHTS AT 2 RIGHT AND 2 LEFT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SIGN — INOPERATIVE (CABIN)

LAX - EMERGENCY EXIT SIGN AFT ROW ON RIGHT SIDE INOPERATIVE. REPLACED EMERGENCY EXIT ARROW SIGN AT AFT ROW ON RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

DFW SEAT MOUNTED ESCAPE PATH LIGHTING AT SEAT 23D INOPERATIVE. RESECURED CONNECTOR FOR SEAT MOUNTED ESCAPE PATH LIGHTING AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

DFW SEAT MOUNTED EMERGENCY PATH LIGHT AT SEAT 31D INOPERATIVE. RESECURED CONNECTOR FOR SEAT MOUNTED EMERGENCY PATH LIGHT AT SEAT 31D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER)

LEFT THRUST REVERSER AMBER LIGHT CAME ON DURING CLIMB-OUT AT FL170. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, AFT SEAT MOUNTED EMERGENCY EXIT PATH LIGHT AT 16D INOPERATIVE. REPLACED AFT SEAT MOUNTED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WARNING LIGHT — ILLUMINATED (LT REVERSER)

HNL - ON CLIMB-OUT, LEFT ENGIE REVERSE AMBER LOCK LIGHT. LEFT REVERSER PLACARDED INOPERATIVE PER MEL. ENTERED IN MIC MPM 78-01 COMPLIED WITH. REINSTALLED NUT PLUS WASHER FOR MECHANICAL LINKAGE COMMON TO OUTBOARD PROXIMITY SWITCH. OPS CHECK GOOD CLEARED MIC SHEET PLUS MEL. (M)

Part: SMOKE — DETECTED (CABIN)

ELECTRICAL SMOKE AREA SEATS 9 THROUGH 13 AREA, REQUEST INSPECTION. INSPECT INSEAT HARNESSES, POWERPORTS, LIGHT BALLASTS IN AREA. PERFORM OPERATION CHECK OF SYSTEMS PER MM. REPAIR FOR FINDINGS. ELECTRICAL SMOKE AREA SEATS 9-13, ACC CABIN FIRE/SMOKE CHECKLIST SMOKE STOPPED. VISUAL INSPECTED ALL ELECTRICAL WIRE CABLE ROWS 9 THROUGH13 LEFT AND RIGHT CHECK ALL NORMAL. NO VISUAL EVIDENCE IF SMOKE AND ELECTRICAL ODOR. (M)

Part: ACM — FAILED (A/C BAY)

AFTER TAKEOFF, A/C COCKPIT TEMP UNCONTROLLABLE ON COLD SIDE, AND EXTREMELY NOISY TO THE POINT CREW COULD NOT HEAR EACH OTHER. REMOVED AND REPLACED LEFT PACK ACM. FOUND IT FROZEN WOULD NOT SPIN. REPLACED LEFT ACM PER MM REQUIRES OPS AND LEAK CHECK EMP 486492. LEAK CHECK AND OPS CHECK OK. (M)

Part: WINDOW — CRACKED (R1 DOOR)

SJC - FOUND 1R ENTRY DOOR WINDOW CRACKING AND CRAZED. INSPECTED 1R WINDOW FOUND SUPERCICIAL SCRATCHES ON OUTER SURFACE OK FOR SERVICE PER MM 56-31-02-6. (M)

Part: BATTERY — SHORTED (RT WING)

MIA - DURING OVERNIGHT MAINTENANCE, NR 1 RIGHT AFT OVERWING EMERGENCY EXIT LIGHT SHORTING. REPLACED RIGHT EMERGENCY AFT OVERWING BATTERY PACK AND CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — BROKEN (R4 DOORWAY)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R4 DOOR INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT SOCKET AT R4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (MID GALLEY)

DFW - DURING OVERNIGHT CHECK, MID GALLEY EMERGENCY EXIT FLOOR LIGHT INOPERATIVE. REPLACED LIGHT STRIP AT MID GALLEY EMERGENCY EXIT FLOOR. SYSTEM GROUD CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT FIRST CLASS GALLEY FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT FIRST CLASS GALLEY. SYSTEM FOUND CHECKED, NORMAL OPERATION. (X)

Part: SLIDE — LOOSE (L1 DOOR)

ORD - FLT 1700 - DURING CRUISE L1 DOOR EMERGENCY ESCAPE SLIDE IS LOOSE FROM DOOR AND SLIDE PACKAGE COVER. CAPTAIN DECLARED AN EMERGENCY AND LANDED ORD AND WITHOUT FURTHER INCIDENT. INSPECTED L1 DOOR SLIDE ASSEMBLY AND SECURED SLIDE AND COVER. (M)