N352AA

Part: WIRE — DAMAGED (CABIN) · airframe 109,372 hrs · 18,068 cycles

EMERGENCY LIGHT ON G2 GALLEY HAS DAMAGED WIRES. R & R EMER LIGHT EXIT MARKER & WIRES ON G2 GALLEY IAW AMM 33-60-98. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 109,372 hrs · 18,068 cycles

G5 MID GALLEY LT AFT WALL EMER LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW AMM 33-60-98. SYS CHECKED GOOD.

Part: WIRE — DAMAGED (CABIN) · airframe 109,372 hrs · 18,068 cycles

A6 LAVATORY RT AFT EMER LIGHT INOPERATIVE. REPAIRED WIRING IAW SWPM 20-10-13. SYS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 109,372 hrs · 18,068 cycles

R1 DOOR OUTSIDE EMER LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-51-03. SYS CHECKED GOOD.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 109,022 hrs · 18,016 cycles

LEFT MID GALLEY EMER LIGHT INTERMITTENT. WIRING CONNECTIONS SECURED FOR LT MID GALLEY EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 108,628 hrs · 17,950 cycles

CORROSION ON FUSELAGE SKIN AT STATION 1275 & STRINGER 36 LT. INSTALLED DOUBLER REPAIR IAW SRM 53-00-01-2R-12.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 108,628 hrs · 17,950 cycles

FUSELAGE SKIN AT STATION 1710 & STRINGER 30 RT DAMAGED. R & R SKIN DOUBLER IAW EA B767-53-036375.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 108,628 hrs · 17,950 cycles

CORROSION ON SKIN JUST AFT OF STATION 1241 BETWEEN STRINGERS 39 LT & 39 RT. COMPLETED INSTALLATION OF TEAR STRAP, FILLER, DOUBLER, TRIPLER & SHEAR TIE IAW EA B767-53-036369 & SRM 53-00-01 REPAIR 29.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 108,628 hrs · 17,950 cycles

SHEAR TIE CORRODED AT STATION 1219 BETWEEN STRINGER 37 & 38 LT. R & R SHEAR TIE IAW AARD 51-00-05-1.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 108,628 hrs · 17,950 cycles

STRINGER CAP SPLICE CORRODED AT STATION 1220 & STRINGER 34 LT. REPLACED STRINGER CAP IAW AARD 51-00-05-1.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 108,628 hrs · 17,950 cycles

EMERGENCY LIGHTS AT 6HJ INOPERATIVE. RE-SEATED EMER LIGHTS CONNECTOR AT 6HJ. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 108,032 hrs · 17,863 cycles

EMERGENCY LIGHT AT LT FUSELAGE INBD TE. REPLACED LAMP FOR EMER LIGHT AT LT FUSELAGE INBD TE. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 107,151 hrs · 17,717 cycles

EMERGENCY LIGHT AT SEAT 3B INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 3B, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 105,806 hrs · 17,497 cycles

LT SIDE, FUSELAGE MOUNTED NR 5 EMERGENCY ESCAPE PATH ILLUMINATION LIGHT INOPERATIVE. REPLACED LAMP FOR LT SIDE, FUSELAGE MOUNTED NR 5 EMERGENCY ESCAPE PATH ILLUMINATION LIGHT. OPERATIONS CHECKED NORMAL

Part: PRESSURE SWITCH — MALFUNCTIONED (HYDRAULIC SYS) · airframe 105,751 hrs · 17,485 cycles

JFK CENTER HYDRAULIC SYSTEM PRESSURE MESSAGE & LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED S35 HYDRAULIC PRESSURE SWITCH, SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: WIRE — BROKEN (CABIN) · airframe 105,352 hrs · 17,422 cycles

EMERGENCY LIGHT CAPSULE BELOW CLOSED FORWARD OF SEAT 2H HAS A WIRE BROKEN OFF & EMERGENCY LIGHT IS INOPERATIVE. REPLACED SEAT 2H EMERGENCY LIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 104,795 hrs · 17,330 cycles

ESCAPE PATH LIGHT AT SEAT 13A INOPERATIVE. SECURED FLOOR WIRING CONNECTION FOR ESCAPE PATH LIGHT AT SEAT 13A. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 104,795 hrs · 17,330 cycles

ESCAPE PATH LIGHT AT SEAT 22H INOPERATIVE. REPLACED LAMP FOR SEAT 22H ESCAPE PATH LIGHT. OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 104,795 hrs · 17,330 cycles

ESCAPE PATH LIGHT AT SEAT 12A INOPERATIVE. SECURED FLOOR WIRING CONNECTION FOR ESCAPE PATH LIGHT AT SEAT 12A. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 104,795 hrs · 17,330 cycles

SEAT 12H ESCAPE PATH LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 12H ESCAPE PATH LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 104,795 hrs · 17,330 cycles

SEAT 25A ESCAPE PATH LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 25A ESCAPE PATH LIGHT. OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 104,795 hrs · 17,330 cycles

ESCAPE PATH LIGHT AT SEAT 11A INOPERATIVE. SECURED FLOOR WIRING CONNECTION FOR SEAT 11A ESCAPE PATH LIGHT. OPERATIONS CHECKED NORMAL.

Part: SKIN — DAMAGED (TE FLAP) · airframe 104,519 hrs · 17,288 cycles

TWO AREAS OF IMPACT DAMAGE TO LOWER SURFACE OF RT INBD FLAP, APPROXIMATELY 20 INCHES FROM OTBD END. REPAIRED WITH BONDED DOUBLER IAW SRM 57-53-01-2R-1, 51-70-10-2R-3, 51-70-10-2R, 57-53-01-2R-1, 57-53-01-0I-1, 51-70-03-0G, 51-70-14 & ESO 9284.

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 104,519 hrs · 17,288 cycles

WEB SUPPORT BEAM IS CRACKED. INSTALLED NEW WEB SUPPORT BEAM IAW SRM 53-60-53-1.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 104,384 hrs · 17,265 cycles

LT SIDE OF FUSELAGE AFT OF THE WING EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT ON LT SIDE AFT OF THE WING. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 103,044 hrs · 17,056 cycles

CEILING EMERGENCY LIGHT AT ROW 11G INOPERATIVE. CLEANED SOCKET AND REPLACED LAMP FOR CEILING EMERGENCY LIGHT AT ROW 11G. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 103,044 hrs · 17,056 cycles

CEILING EMERGENCY LIGHT AT ROW 11G INOPERATIVE. CLEANED SOCKET AND REPLACED LAMP FOR CEILING EMERGENCY LIGHT AT ROW 11G. OPS CHECK NORMAL.

Part: CONTROL PANEL — MALFUNCTIONED (AUTOPILOT SYS) · airframe 100,409 hrs · 16,644 cycles

IAD - INFLIGHT JFK-PAP. CREW REPORTED FLIGHT DIRECTOR FAILED, FOLLOWED BY FAILURE OF AUTO THROTTLES AND VERTICAL NAVIGATION. EMERGENCY DECLARED FLIGHT DIVERTED IAD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED MODE CONTROL PANEL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ALTIMETER — FAILED (COCKPIT) · airframe 100,320 hrs · 16,631 cycles

MAD - CREW REPORTED CAPTAINS ALTIMETER FAILED IN CLIMBOUT. FLAG IN VIEW AND NO HEIGHT INDICATION. EMERGENCY DECLARED FLIGHT RETURNED MAD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CAPTAINS ALTIMETER. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)

Part: SLAT — DEBONDED (LT WING) · airframe 98,777 hrs · 16,379 cycles

LEFT WING NUMBER 4 SLAT DISBONDED. ACCOM[PLISHED DOUBLER REPAIR PER AARD 57-43-00-01.

Part: SKIN — GOUGED (FUSELAGE) · airframe 98,777 hrs · 16,379 cycles

SKIN AT STATION 1200 BETWEEN STRINGERS 29 AND 30 RIGHT GOUGED. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-00-01-2R.

Part: WIRE — DAMAGED (CABIN) · airframe 98,544 hrs · 16,342 cycles

EMERGENCY LIGHTS ON LEFT SIDE AT ROWS 32 TO 41 INOPERATIVE. FOUND AFFECTED LIGHTS BATTERY PACK WITH BLOWN FUSE. INSPECTED AND REPAIRED WIRING TO SEVERAL SEAT LIGHT ASSEMBLIES AND REPOSITIONED POSSIBLE PINCHED WIRING UNDER FLOOR. REPLACED BATTERY PACK. OPS CHECK NORMAL.

Part: CONTROL PANEL — FAILED (AUTOPILOT SYS) · airframe 98,126 hrs · 16,279 cycles

MXP - CREW REPORTED ON TAKEOFF ROLL, FIRST OFFICER OBSERVED LOSS OF BOTH FLIGHT DIRECTORS. AFTER TAKEOFF COMMAND AIRSPEED BUGS ALSO NOTED MISSING FROM BOTH SIDES. AUTOPILOT MODE CONTROL PANEL LOCKED UP. NO WARNING INDICATIONS OR EICAS MESSAGES. EMERGENCY DECLARED FLIGHT RETURNED MXP. AIRCRAFT REMOVED FROM SERVICE. REPLACED AUTOPILOT MODE CONTROL PANEL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ACTUATOR — INOPERATIVE (RUDDER TRIM) · airframe 96,830 hrs · 16,081 cycles

MIA - CREW REPORTED RUDDER TRIM INOPERATIVE DURING FLIGHT. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RUDDER TRIM ACTUATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ALTIMETER — FAILED (COCKPIT) · airframe 95,956 hrs · 15,942 cycles

BOS - CREW REPORTED CAPTAINS ALTIMETER FAILED DURING CLIMB. FLIGHT RETURNED BOS LANDED WITHOUT INCIDENT. REPLACED CAPTAINS ALTIMETER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONNECTOR — LOOSE (AC PACK) · airframe 95,050 hrs · 15,794 cycles

LAX - INFLIGHT DFW-HNL. CREW REPORTED LEFT PACK INOPERATIVE WITH CRUISE POWER SET AT CRUISE ALTITUDE. EMERGENCY DECLARED FLIGHT DIVERTED LAX LANDED WITHOUT INCIDENT. MAINTENANCE RE-SECURED LEFT PACK VALVE CONNECTOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: GUARD — BROKEN (CABIN) · airframe 94,888 hrs · 15,766 cycles

SEAT 21B EMERGENCY LIGHT GUARD BROKEN. REPLACED GUARD FOR SEAT 21B EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 94,888 hrs · 15,766 cycles

SEAT 20B EMERGENCY LIGHTS INOPERATIVE. REPLACED BROKEN WIRE AT CONNECTOR UNDER SEAT 20B. OP CHECK NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 94,236 hrs · 15,645 cycles

EMERGENCY LIGHTS INOPERATIVE AT ROW 24. REPAIRED LOOSE CONNECTOR AT SEAT 24B.

Part: ANTENNA — FAILED (WEATHER RADAR) · airframe 93,884 hrs · 15,589 cycles

GIG - CREW REPORTED WEATHER RADAR FAILED INFLIGHT. EMERGENCY DECLARED RETURNED GIG LANDED WITHOUT INCIDENT. REMOVED AND REPLACED WEATHER RADAR ANTENNA. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FRAME — DENTED (FUSELAGE) · airframe 93,445 hrs · 15,508 cycles

FUSELAGE FRAME STATION 500 INNER CHORD BETWEEN STRINGERS 30 AND 31 LEFT DAMAGED. ACCOMPLISHED REPAIR PER EA B767-53-011677.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,445 hrs · 15,508 cycles

FORWARD CARGO DOOR LOWER SILL INNER CHORD FAILSAFE STRAP STATION 505 AND 569 CORRODED. ACCOMPLISHED REPAIR PER EA B767-53-011906.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 93,445 hrs · 15,508 cycles

FUSELAGE FRAME LOWER LOBE WEB AT STATION 566 AND RIGHT BUTTLINE 14 DAMAGED. ACCOMPLISHED REPAIR PER EA B767-53-011825.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 93,445 hrs · 15,508 cycles

STATION 347 FLOORBEAM BETWEEN RIGHT AND LEFT BUTTLINE 27 CRACKED. ACCOMPLISHED REPAIR PER EA B767-53-011744.

Part: WIRE — BROKEN (CABIN) · airframe 92,713 hrs · 15,385 cycles

SEAT 39B EMERGENCY LIGHT INOPERATIVE. REPINNED BROKEN WIRE TO PLUG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 91,757 hrs · 15,208 cycles

EMERGENCY LIGHT AT OVERHEAD SEAT 10B INOPERATIVE. REPLACED LAMP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 91,757 hrs · 15,208 cycles

EMERGENCY LIGHT AT OVERHEAD SEAT 23H INOPERATIVE. REPLACED LAMP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 91,757 hrs · 15,208 cycles

EMERGENCY LIGHT AT LEFT OVERWING CENTER EXTERIOR INOPERATIVE. REPLACED LAMP.

Part: CONNECTOR — DAMAGED (CABIN`) · airframe 91,757 hrs · 15,208 cycles

EMERGENCY LIGHT AT SEAT 29B INOPERATIVE. REPAIRED CONNECTOR AT SEAT 29B.

Part: SIGN — DAMAGED (CABIN) · airframe 91,757 hrs · 15,208 cycles

EMERGENCY LIGHT EXIT SIGN AT RIGHT NUMBER ONE DOOR DAMAGED. REPLACED EXIT SIGN ASSEMBLY AT RIGHT NUMBER ONE DOOR.

Part: FAN — FAULTY (CABIN) · airframe 91,465 hrs · 15,151 cycles

ON DESCENT INTO MIA A STRONG ACRID SMELL WAS IN THE COCKPIT. FLIGHT ATTENDANTS REPORTED STRONG BURNING ELECTRIC WIRE SMELL IN CABIN. THE ODORS DISSIPATED ON DESCENT. REPLACED LEFT RECIRCULATION FAN AND FILTER.

Part: PROCESSOR — INOPERATIVE (TCAS) · airframe 88,133 hrs · 14,607 cycles

MIA - EMERGENCY DECLARED, RETURNED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. AIR COLLISION AVOIDANCE SYSTEM INOPERATIVE. REPLACED PROCESSOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LENS — MISSING (CABIN)

JFK - EMERGENCY LIGHT AT LT NR FOUR DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LT NR FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: SHUTOFF VALVE — LEAKING (HYDRAULIC SYS) · airframe 85,064 hrs

DFW INFLIGHT T2473/11MAR - RIGHT HYDRAULIC SYSTEM FLUID LOSS DURING CLIMB. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT HAND WING LATERAL CONTROL SHUT OFF VALVE AND SERVICED HYDRAULIC RESERVOIR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BEZEL — INOPERATIVE (CABIN)

SFO - EMERGENCY LIGHT AT RIGHT AFT GALLEY INOPERATIVE. REPLACED BEZEL FOR EMERGENCY LIGHT AT RIGHT AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

SFO - EMERGENCY LIGHT AT RIGHT AFT GALLEY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PRESSURE SWITCH — INOPERATIVE (LT ENGINE)

YYR INFLIGHT T88/02NOV ORD TO BRU - LEFT ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. CREW SHUT DOWN LEFT ENGINE. LANDED YYR WITHOUT INCIDENT. SINGLE ENGINE TIME SIX MINUTES. REPLACED OIL SCAVENGE FILTER. NO DEBRIS FOUND ON OIL SCAVENGE FILTER. REPLACED OIL FILTER DIFFERENTIAL PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)

JFK - EMERGENCY LIGHT AT SEATS 20AB INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEATS 20AB. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SLIDE — UNWANTED DEPLOY (RT OVERWING)

DFW INFLIGHT T102/01JUN - RIGHT OVERWING SLIDE DEPLOYED DURING FLIGHT. AIRCRAFT REMOVED FROM SERVICE TO EVALUATE DAMAGE. REPLACED RIGHT OVERWING SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: OVEN — DIRTY (GALLEY)

CDG - FIRST CLASS OVEN NUMBER ONE HAD FOOD SPILL CAUSING SMOKE IN GALLEY. CLEANED OVEN NUMBER ONE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT AT SEATS 39AB INOPERATIVE. REPAIRED CONNECTOR AT SEAT 39A FOR EMERGENCY LIGHTS AT SEATS 39AB. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

CDG - EMERGENCY EXIT SIGN AT 4L AND 4R INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN AT 4L AND 4R. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — CRACKED (FUSELAGE)

AFW - FUSELAGE SKIN AT STATION 1582 AT 539L ON THE FORWARD SIDE OF PRODUCTION SPLICE HAS CORROSION. THE AREA OF CORROSION IS 8 INCHES BY 3 AND .75 INCH AND THE CRACK LENGTH IS APPROXIMATELY 0.75 INCH. REMOVED AREA OF SKIN DAMAGE PER SRM 53-00-01 AND REPAIRED USING STACKED DOUBLERS PER THE SRM. REPAIR FASTENERS IN NEW LOCATIONS ARE .1875 INCH STAINLESS SHEAR HEAD HI-LOKS.

Part: PUMP — INOPERATIVE (FUEL BOOST)

LAX INFLIGHT T283/31, AT CRUISE ALTITUDE TURNED ON CENTER PUMPS. BOTH PUMPS FAILED TO OPERATE. RETURNED TO LAX. LANDED WITHOUT INCIDENT. REPLACED LEFT AUXILLARY TANK OVERRIDE BOOST PUMP PER MM 28-22-05. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUSHROD — OUT OF ADJUST (PAX DOOR)

AIRCRAFT CLIMB-OUT FROM EZE CREW OBSERVED L1 DOOR AIR LEAK. LANDED EZE WITH IN NORMAL WEIGHT LIMITS. ACCOMPLISHED OVERCENTER PUSHROD MECHANISM ADJUSTMENT TO L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHTING AT 23B INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTING WALL TO SEAT HARNESS CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

STL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 23B INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT AT SEAT 23B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, SEAT 31B EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE CONNECTORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 35H INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT CONNECTOR AT 35H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 26 A/B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 26 A/B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — FAULTY (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTS AT SEAT 29 A/B INOPERATIVE. REPLACED WALL CONNECTOR AT SEAT 29 A/B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PIN — LOOSE (CONNECTOR)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 22H INOPERATIVE. REPINNED EMERGENCY EXIT LIGHT AT SEAT 22H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONTROL PANEL — FAILED (COCKPIT)

WEATHER RADAR UNUSABLE ON 20-40 MILE RANGES ALL RED PLUS SHOWING NO RETURNS, BOTH CAPTAINS AND FIRST OFFICERS. REMOVED AND REPLACED WEATHER RADAR CONTROL PANEL PER MM AND CHECK OPERATION FUNCTION PER MM SYSTEM OK FOR SERVICE. (M)

Part: SOCKET — DIRTY (L4 DOOR)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L4 DOOR INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT SOCKET AT L4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHT SEAT 29H INOPERATIVE. RESEATED CONNECTOR TO EMERGENCY ESCAPE PATH LIGHT SEAT 29H. SYTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTS SEAT 17H THROUGH 23H INOPERATIVE. RESEATED CONNECTOR TO BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — INOPERATIVE (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 29H INOPERATIVE. RE-PINNED EMERGENCY EXIT LIGHT WIRE AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 39H INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 39H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 38H, 25B, 2B, 3B, 7B AND 8B INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 38H AND 25B. REPAIRED CONNECTOR AT 2B AND 3B, 7B AND 8B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: OVEN — DEFECTIVE (NR 2 GALLEY)

LHR - FLT 91 - EN ROUTE LHR-ORD, DETECTED SMOKE AT NR 2 GALLEY. NR 2 OVEN CIRCUIT BREAKER PULLED. LANDED ORD WITHOUT FURTHER INCIDENT. REPLACED NR 2 GALLEY OVEN AND RESET CIRCUIT BREAKER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT ESCAPE PATH LIGHT AT SEAT 31A INOPERATIVE. REPAIRED WIRA AT SEAT 31A. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHT AT SEAT 37B INOPERATIVE. REPAIRED BROKEN WIRE AT SEAT 37B. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: UNKNOWN — ODOR (LAVATORY)

PHX - FLT 2238 - DURING FLIGHT, STRONG ELECTRICAL BURNING ODOR IN LEFT BUSINESS CLASS M1 LAVATORY. REMOVED AND CLEANED SEALANT FROM M1 LAVATORY DOOR SEAL. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — BROKEN (ROW 28H)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 28H INOPERATIVE. REPAIRED WIRE ON EMERGENCY EXIT SEAT LIGHT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: FRAME — CORRODED (BS 1219)

AFW - AFT CARGO FRAME (J-CAP) AT STATION 1219 RBL 42 HAD CORROSION. REMOVED CORROSION UNDER NUTPLATE, ALODINED, PRIMED AND REINSTALLED NUTPLATES. (M)

Part: STRINGER — CORRODED (BS 444)

AFW - FOUND STRINGER 37L CORRODED AT APPROX STATION 444. REMOVE CORRODED PIECE OF STRINGER. REPLACE WITH SIMILAR LONGER SPLICE WITHOUT A JOGGLE. USE SHIMS AND FILLERS. REPAIR PARTS AND BARE SURFACES FINISHED WITH ALODINE AND PRIMER. (M)

Part: STRINGER — CORRODED (BS 444)

AFW - STRINGER 37L CORRODED AT APPROX STATION 444. REMOVED CORRODED PIECE. INSTALLED SIMILAR PIECE FASTENERS AND STRINGER CLIP, TREATED AND PRIMED SURFACE. (M)

Part: SILL — CORRODED (BS 625)

AFW - LOWER AUXILIARY SILL INNER CHORD RBL 30, STATION 625 HAD CORROSION BLENDED ON LOWER SURFACE BEYOND SRM LIMITS. REPAIRED PER MRB 767-7818. (M)

Part: FLOORBEAM — CORRODED (BS 1480)

AFW - FLOORBEAM AT STATION 1480 HAS CORROSION REMOVAL AS SHOWN ON SKETCH. ALODINED AND PRIMED STATION 1480 LBL 50-51. REPAIRED IAW MRB 767-1810. (M)

Part: SILL — CORRODED (CARGO DOORWAY)

AFW - OUTER CHORD ON LOWER MAIN SILL HAS CORROSION REMOVAL ON VERTICAL LEG INNER SURFACE AS SHOWN. REPAIRED IAW MRB 767-1819, DATED 11 FEB 99. (M)

Part: FLOORBEAM — CRACKED (BS 783)

AFW - FOUND SMALL CRACK IN VERTICAL LEG OF FLOORBEAM AT STATION 783 RBL 11.06 AND LBL 11.06. REMOVED DAMAGED SECTION OF FLOORBEAM. SPLICED IN NEW SECTION OF FLOORBEAM. INSTALLED ALL REPAIR PARTS WET WITH BMS 5-95. (M)

Part: FRAME — CORRODED (BS 1197)

AFW - FUSELAGE FRAME INNER CHORD HAS CORROSION REMOVAL ON LOWER SURFACE AS SHOWN MATERIAL REMAINING IS BEYOND SRM 53-00-07-1 LIMITS. BLENDED CORROSION IAW MRB 767-1816 DATED FEB 09, 1999. (M)

Part: WIRE — FAILED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEAT ROW 24AB INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT ROW 24AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: IDG — FAILED (LT ENGINE)

GRU - FLT 920 - ON LEFT ENGINE START GEN DRIVE LIGHT FAILED TO EXTINGUISH. DEFERRED LT ENGINE IDG AS PER MEL REF MIC SHEET AND PLACARDED. PERFORMED AND SERVICED OIL LEVEL RT/LT AND APU GENERATOR AS REQUIRED PER MPM 24-01. REPLACED LT ENG IDG REQUIRES OPS CHECK LEAK CHECK DFRL.4. REPLACED NR 1 IDG AND SERVICED WITH OIL. LEAK CHECK AND OPS CHECK OK. REMOVED PLACARD AND CLEARED MIC SHEET. (M)

Part: IDG — FAILED (RT GEN)

MAD - FLT 0069 - RT IDG PLAC INOP AS MEL 24-01 AUTH 4-32-9DC-B NO TIME AT MAD NO PARTS ENTERED MICS MEL PROCEDURES C/W ENG APU. COWLINGS CLOSED BOTH IDG AND APU SERVICED TO PROPER LEVEL. R/R RT IDG PER MM LEAK CK NO LEAKS NOTED. OPS CHECK THRU ALL OPERATIONS CKS NORMAL. NOTE: EXTENDED RANGE EVENT REPORT (ER) NR AFW777. (X)

Part: CONNECTOR — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 24 AB FOUND INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 24 AB. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 40H INOPERATIVE. REPLACED BROKEN EMERGENCY EXIT LIGHT ASSEMBLY AT PASSENGER SEAT 40H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: IDG — MALFUNCTIONED (LT ENGINE)

GRU - FLT 951 - LEFT GENERATOR FAILED IN FLT. DEFERRED THE LEFT ENG GEN DRIVE INOP, AS PER MEL REF ACCOMPLISHED MPM CHECK 24-01 AND OIL SERVICED BOTH IDGS PER MM 12-13-03. PLACARD AND MIC SHEET ENTERED. MEL REF 24-01 AUTH NR 06-0288DC-B. REMOVED AND REPLACED LEFT ENGINE GENERATOR DRIVE UNIT AS PER MM SERVICED IDG, RUN UP OK. DISCONNECTED IDG AND RECONNECTED AND RECHECKED ON RUN UP. ALL CHECKS OK. REMOVED MEL 06--0288DC-B AND CLEARED MIC SHEET. (M)

Part: IDG — FAILED (LT ENGINE)

JFK - FLT 0016 - IN-FLIGHT FLICKERING LEFT GENERATOR DRIVE LIGHT ON WITH LEFT EICAS IDG TEMP SENSOR LIGHT. GENERATOR OFF LIGHT CAME ON INTERMITTENTLY. LEFT IDG WAS DISCONNECTED. REPLACED LT IDG. RAN ENGINE, ALL PARAMETERS CK NORMAL. RECONNECTED IDG. LEAK CK OK. (X)

Part: CONNECTOR — LOOSE (CABIN)

SFO - EMERGENCY EXIT LIGHT AT SEAT 27B INOPERATIVE. RECONNECTED LOOSE CONNECTOR AND SECURED AT SEAT 27B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PIN — BROKEN (PAX SEAT)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 27B INOPERATIVE. REPLACED BROKEN PIN ON SEAT MOUNTED EMERGENCY EXIT LIGHT AT PASSENGER SEAT 27B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING ON RIGHT SIDE OF FIRST CLASS AND BUSINESS CLASS FOUND INOPERATIVE. RESECURED LOOSE CONNECTOR IN FIRST CLASS, RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS AT 9-12AB, 25-31AB, AND 7-12HJ INOPERATIVE. RESECURED CONNECTORS AT SAME LOCATIONS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTORS — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS FROM PAX SEAT ROWS 8B TO 12B AND 7H TO 12H INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTORS AT PAX SEATS 8B TO 12B AND 7H TO 12H. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)

Part: EEL ASSY — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 22B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT PAX SEAT 22B. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS BETWEEN PASSENGER SEAT ROWS 9B THROUGH 12B INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR BY PASSENGER SEAT ROW S12B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL ASSY — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, LEFT SIDE EMERGENCY EXIT LIGHT IN BUSINESS CLASS CABIN INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSY AT LEFT SIDE IN BUSINESS CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS BETWEEN PASSENGER SEAT ROWS 7H THROUGH 12H INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR BY PASSENGER SEAT ROW 7H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE ON RIGHT SIDE OF BUSINESS CLASS. RESECURED LOOSE EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR AT 12HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT RT AISLE OF BUSINESS CLASS INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT AFT AREA OF RT AISLE BUSINESS CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS BETWEEN PAX SEAT ROWS 7H AND 12H INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT ROW 7H. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)

Part: EEL — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT RT AISLE BETWEEN PAX SEAT ROWS 7 AND 12 INOPERTIVE. REPLACED EMERGENCY FLOOR LIGHTS ASSEMBLIES AT RT AISLE BETWEEN PAX SEAT ROWS 7 AND 12. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT AT LEFT AISLE BETWEEN PAX SEAT ROWS 8 AND 12 INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT LEFT AISLE BY PAX SEAT ROW 12. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)