N383AN

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 96,255 hrs · 15,598 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT THE L4 DOOR IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT PER AMM 25-64-00. OPERATIONAL CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 96,255 hrs · 15,598 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT THE L2 DOOR IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT PER AMM 25-64-00. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 96,226 hrs · 15,590 cycles

AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT THE FORWARD WALL RIGHT JUMPSEAT IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY PER AMM 25-63-00. OPERATIONAL CHECK GOOD.

Part: TERMINAL — LOOSE (EMERGENCY LIGHT) · airframe 95,274 hrs · 15,408 cycles

EMERGENCY EXIT SIGN ON LEFT FORWARD INTERIOR OVERWING HATCH IS INOPERATIVE. SECURED LOOSE TERMINAL AT L322 ON LIGHT ASSEMBLY IAW WDM 33-51-14. OPERATIONAL CHECKED GOOD.

Part: UNKNOWN — INOPERATIVE (LIGHTS) · airframe 95,274 hrs · 15,408 cycles

OVERWING EMERGENCY ESCAPE HATCH INTERIOR LIGHTS FORWARD AND AFT, LEFT AND RIGHT ARE INOPERATIVE. RESET SYSTEM LIGHTS IAW AMM 33-51-00. OPERATIONAL CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 95,274 hrs · 15,408 cycles

SEAT MOUNTED AND OVERHEAD AISLE EMERGENCY EXIT LIGHTS IN ROWS 11H THROUGH 31H ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT ROW 24HJ IAW AMM 33-51-07. OPERATIONAL CHECKED GOOD.

Part: CLAMP — FAILED (PNEUMATIC SYS) · airframe 95,209 hrs · 15,397 cycles

EMERGENCY DECLARED. RETURNED TO DEPARTURE DUE TO A LEFT ENGINE WARNING INDICATIONS FOR FIRE LOOP, N2, AND CENTER FUEL BOOST PUMP. AIRCRAFT WAS GROUNDED. MAINTENANCE DETERMINED DIFFICULTY WAS THE PNEUMATIC DUCT CLAMP FAILED. REMOVED AND REPLACED THE CLAMP IAW AMM 36-11-01. OPS CHECKED GOOD.

Part: SENSING ELEMENT — SHORTED (RT NACELLE) · airframe 95,029 hrs · 15,359 cycles

FIRE/OVERHEAT INDICATION RECEIVED DURING CLIMB. ACCOMPLISHED CHECKLIST AND LIGHT EXTINGUISHED. NORMAL FLIGHT CONTINUED. INSPECTED RIGHT ENGINE FIRE/OVERHEAT DETECTION SYSTEM AND FOUND SENSING ELEMENT GROUNDING TO SUPPORT TUBE ON UPPER AFT ENGINE FIRE LOOP. ADJUSTED SENSING ELEMENT IAW AMM 26-11-00. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 94,809 hrs · 15,322 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT RIGHT SIDE AFT OF TRAILING EDGE FLAP IS INOPERATIVE. SECURED LIGHT ASSEMBLY IAW AMM 33-50-00. OPERATIONAL CHECK GOOD.

Part: GIRT BAR — OUT OF POSITION (R1 DOOR) · airframe 94,809 hrs · 15,322 cycles

AIRCRAFT WAS NOT GROUNDED. R1 DOOR EMERGENCY EVACUATION SLIDE GIRT BAR IS OUT OF POSITION. SECURED GIRT BAR IAW AMM 25-66-05. OPERATIONAL CHECK GOOD.

Part: CYLINDER — LOW PRESSURE (EVAC SLIDE) · airframe 94,508 hrs · 15,246 cycles

AIRCRAFT WAS NOT GROUNDED. L4 DOOR EMERGENCY EVACUATION SLIDE CYLINDER PRESSURE IS LOW. REMOVED AND REPLACED SLIDE IAW AMM 25-66-01. OPERATIONAL CHECK GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 94,283 hrs · 15,182 cycles

SEAT MOUNTED EMERGENCY LIGHT AT ROW 2 LEFT HAS A MISSING LENS. INSTALLED A NEW LENS IAW AMM 33-51-05. OPS CHECKED GOOD.

Part: LENS — MISSING (EXIT SIGN) · airframe 94,228 hrs · 15,171 cycles

AIRCRAFT NOT GROUNDED. EMERGENCY EXIT SIGN AT SEAT 21J IS MISSING LENS COVER. INSTALLED LENS COVER IAW AMM 33-51-09. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 94,050 hrs · 15,135 cycles

AIRCRAFT NOT GROUNDED. SEAT MOUNTED EMERGENCY EXIT LIGHTS AT ROWS 32H THROUGH 41H ARE INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY AT SEAT 41H IAW AMM 33-51-10. OPERATIONAL CHECK GOOD.

Part: CHARGER — NO TEST (EMERGENCY LIGHTS) · airframe 93,912 hrs · 15,107 cycles

SEAT MOUNTED EMERGENCY LIGHTING DOES NOT ILLUMINATE DURING TEST AT SEATS 32H THROUGH 41H. REMOVED AND REPLACED BATTERY CHARGER ASSEMBLY AT ROW 41H. OPERATIONAL CHECKED GOOD.

Part: CHARGER — NO TEST (EMERGENCY LIGHTS) · airframe 93,912 hrs · 15,107 cycles

SEAT MOUNTED EMERGENCY LIGHTING DOES NOT ILLUMINATE DURING TEST AT SEATS 32H THROUGH 42H. REMOVED AND REPLACED BATTERY CHARGER ASSEMBLY AT ROW 42H. OPERATIONAL CHECKED GOOD.

Part: WEB — CRACKED (BS 1153) · airframe 92,700 hrs · 14,848 cycles

FUSELAGE FRAME BS 1153 WEB IS CRACKED AT LBL 24 AND RBL 21. REPAIRED WEB IAW SRM 51-70-13 AND EA #261117

Part: SKIN — DAMAGED (BS 1720) · airframe 92,700 hrs · 14,848 cycles

FUELAGE SKIN IS DAMAGED AT APPROXIMATELY BS 1720, S30R. REPAIRED SKIN IAW SRM 53-00-01, REPAIR 14 AND EA 261141.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 92,700 hrs · 14,848 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. S30R IS DAMAGED AT APPROXIMATELY FUSELAGE STA 1720. R & R STRINGER SECTION IAW AARD 51-00-05-1, EA 261532 AND EA 261534.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 92,700 hrs · 14,848 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. S32R IS DAMAGED AT APPROXIMATELY FUSELAGE STA 1720. R & R STR SECTION IAW AARD 51-00-05-1 AND EA 261534.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 92,700 hrs · 14,848 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. LEFT WING SKIN AT OVERWING FILL PORT IS CORRODED. REPAIRED SKIN IAW NR 260987.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 92,700 hrs · 14,848 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. AFT CARGO FLOOR WEB SUPPORT ANGLE AT RBL 40 AND FUSELAGE STA 1277 IS CORRODED. R & R ANGLE IAW SRM 51-10-02-0G.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 92,700 hrs · 14,848 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. AFT CARGO COMPARTMENT FLOOR PANEL SUPPORT AT RBL 38 BETWEEN FUSELAGE STA 1263 AND STA 1285 IS CRACKED. R & R SUPPORT IAW SRM 51-10-02-0G.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 92,700 hrs · 14,848 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. AFT CARGO COMPARTMENT TRACK 6 SUPPORT ANGLE AT FS 1263 IS CORRODED. R & R SUPPORT ANGLE IAW SRM 51-10-02-0G.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 92,700 hrs · 14,848 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CABIN FLOORBEAM AT FUSELAGE STA 347 IS CORRODED ON LOWER SURFACE OF TEE CAP BETWEEN LBL 28 AND LBL 47. REPAIRED FLOORBEAM IAW SRM 53-00-51-2R AND EA 261119.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 91,827 hrs · 14,665 cycles

L2 DOOR AFT FLIGHT ATTENDANT SEAT, FLASHLIGHT FAILED OPERATIONAL CHECK, NO GREEN LIGHT. REPLACED FLASHLIGHT. THE ACFT WAS NOT GNDED.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 91,639 hrs · 14,630 cycles

AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING FLIGHT A CLICKING NOISE WAS IN OVERHEAD, FOLLOWED BY FLUCTUATING FLAP INDICATION & LE SLAT ASYMMETRY & LE LIGHT WARNINGS. MAINTENANCE REMOVED AND REPLACED FLAP INDICATOR IAW AMM REF 27-58-02 AND ACCOMPLISHED OPERATIONAL CHECKS IAW AMM REF 27-58-00 WITH NO FAULTS, MESSAGES OR LIGHTS. SYSTEM CHECKS NORMAL.

Part: CHARGER — FAULTY (CABIN) · airframe 89,871 hrs · 14,294 cycles

L1 & R1 DOORS, EMER EXIT SIGNS INOPERATIVE. R & R POWER SUPPLY M1208 CHARGER AT L1 DOOR. PERFORMED OPERATIONAL CHECK. SYS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 89,871 hrs · 14,294 cycles

L1 DOOR EMER EXIT SIGN INOPERATIVE. R & R POWER SUPPLY M1208 BATTERY IAW 33-51-07. PERFORMED OPERATIONAL CHECK, SYSTEM CHECKED NORMAL.

Part: TEST PANEL — FAULTY (ZONE 200) · airframe 89,775 hrs · 14,278 cycles

WHILE PERFORMING SQUIB TEST 2, LT & RT OVERWING SQUIBS ILLUMINATE INTERMITTENTLY. R & R SQUIB TEST PANEL. PERFORMED OPERATIONAL CHECK IAW AMM 26-21-04. SYS CHECKED NORMAL.

Part: BATTERY PACK — FAULTY (ZONE 500) · airframe 89,775 hrs · 14,278 cycles

WHILE PERFORMING SQUIB TEST 1, LT OVERWING ESCAPE SLIDE SQUIB DOES NOT ILLUMINATE. R & R SQUIB BATTERY & PERFORMED OPERATIONAL CHECK IAW AMM 26-21-04. SYS CHECKED NORMAL.

Part: TIRE — OUT OF ROUND (NLG) · airframe 89,719 hrs · 14,266 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING TAKEOFF, NOSE GEAR HAD ABNORMAL VIBRATION & WOBBLE BUT RETRACTED SUCCESSFULLY. ON EXTENSION AT NOSE GEAR APPEARED TO HAVE SLAMMED DOWN & FLIGHT ATTENDANT REPORTED GRINDING NOISE. PERFORMED FIM 32-51-00 & FOUND NOSE GEAR TIRE ASSEMBLY OUT OF ROUND & PRESS LOW. R & R TIRE ASSEMBLY IAW NIC 32-96-51. OPERATIONAL TEST IAW 32-3400. SYS CHECKED NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 88,006 hrs · 13,964 cycles

EMERGENCY EXIT IDENTIFIERS AT L1 & R1 DOORS DO NOT TEST. REPLACED POWER SUPPLY CHARGER & TESTED IAW AMM 33-51-07. LIGHTS OPERATIONS NORMAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 87,611 hrs · 13,889 cycles

DENT BETWEEN FUSELAGE STATIONS 1219 & 1241 AT STRINGER 29 RT IS BEYOND SRM 53-00-01-1A LIMITS. PERFORMED EXTERNAL DOUBLE REPAIR IAW SRM 53-00-01-2R-1.

Part: LIGHT — INOPERATIVE (ZONE 100) · airframe 87,516 hrs · 13,872 cycles

NUMBER 6 RT SLIDE ILLUMINATION LIGHT INOPERATIVE. REPLACED LAMP. OPERATIONS CHECKED NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 87,516 hrs · 13,872 cycles

LEFT & RT NR 1 DOOR EMER EXIT SIGNS INOPERATIVE. R & R BATTERY PACK & CHARGER ASSEMBLY. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 87,516 hrs · 13,872 cycles

NUMBER 5 RT SLIDE ILLUMINATION LIGHT INOPERATIVE. REPLACED LAMP. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (ZONE 100) · airframe 87,516 hrs · 13,872 cycles

LEFT SLIDE ILLUMINATION LIGHT NR 5 INOPERATIVE. REPLACED LAMP. OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 86,693 hrs · 13,731 cycles

SEAT 2HJ EMER LIGHT INOPERATIVE. CONNECTED LOOSE CONNECTOR & REPLACED LAMP FOR EMER LIGHT AT SEAT 2HJ. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 86,200 hrs · 13,654 cycles

LEFT NR 1 DOOR UPPER FWD EMER EXIT SIGN INOPERATIVE. REPLACED LAMP FOR LT NR 1 DOOR UPPER FWD EMER EXIT SIGN. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 86,072 hrs · 13,634 cycles

NOSE WHEEL NOT EXTENDED INDICATION. RETRACTED GEAR WITH NO CHANGE. TOWER CONFIRMED NOSE GEAR WAS EXTENDED. EMER DECLARED FLIGHT LANDED WITHOUT INCIDENT. REPLACED LAMP FOR NOSE LANDING GREEN INDICATOR LIGHT. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,930 hrs · 13,611 cycles

FORWARD SEAT MOUNTED EMERGENCY ESCAPE LIGHT AT 5B INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR 5B FWD SEAT MOUNTED EMERGENCY ESCAPE. OPERATIONS CHECKED NORMAL.

Part: SIGN — CRACKED (CABIN) · airframe 85,685 hrs · 13,575 cycles

EMER EXIT SIGN CRACKED. REPLACED LENS FOR EMER EXIT SIGN. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 85,685 hrs · 13,575 cycles

LEFT AFT FUSELAGE GND SCAN EMER LIGHT INOPERATIVE. REPLACED LAMP FOR LT AFT FUSELAGE GND SCAN EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,685 hrs · 13,575 cycles

EMERGENCY LIGHT AT SEAT 12B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 12B. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 85,685 hrs · 13,575 cycles

LOWER FWD EMERGENCY EXIT SIGN AT RT NR 1 DOOR INOPERATIVE. REPLACED LAMP FOR LOWER FWD EMERGENCY EXIT SIGN. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,255 hrs · 13,509 cycles

RT NR 2 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RT NR 2 DOOR EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: SENSOR — INOPERATIVE (LE SLAT) · airframe 84,829 hrs · 13,442 cycles

MIA CREW REPORTED FLAP SLAT DISAGREE. EMERGENCY DECLARED FLIGHT RETURNED MIA & LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED S278 NR 3 SLAT SENSOR. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: SHROUD — MISSING (CABIN) · airframe 83,952 hrs · 13,310 cycles

SEAT EMERGENCY LIGHT HAS BACK UP SHROUD MISSING AT SEAT 22B. INSTALLED SHROUD FOR EMERGENCY LIGHT AT SEAT 22B. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 83,952 hrs · 13,310 cycles

RT SIDE FUSELAGE MOUNTED NR 7 EMERGENCY EXIT ILLUMINATION LIGHT INOPERATIVE. REPLACED LAMP FOR RT SIDE NR 7 EXTERIOR EMERGENCY EXIT ILLUMINATION LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 83,035 hrs · 13,158 cycles

RT NR 2 DOOR EMERGENCY SIGN LOWER PORTION LIGHTS INOPERATIVE. REPLACED LAMPS FOR RT NR 2 DOOR EMERGENCY EXIT SIGN LOWER PORTION LIGHTS. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 83,035 hrs · 13,158 cycles

LT NR 2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 2 DOOR EXTERIOR EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: SENSOR — INOPERATIVE (LE SLAT) · airframe 82,204 hrs · 13,033 cycles

LEADING EDGE SLAT ASYMMETRY & LEADING EDGE LIGHT DISPLAYED DURING NORMAL FLAP EXTENSION & RETRACTION AT FLAP 1. FOUND FAULT ON SLAT SENSOR S302. REPLACED WITH SERVICEABLE SENSOR AT NR TEN INBOARD POSITION. SYSTEM GROUND CHECKED NORMAL.

Part: MOTOR — FAILED (LE SLAT) · airframe 82,203 hrs · 13,032 cycles

"LEADING EDGE SLAT ASYMMETRY" EICAS MESSAGE. EMERGENCY DECLARED FLIGHT RETURNED TUL LANDED WITHOUT INCIDENT. REPLACED INBOARD SLAT PDU MOTOR. SYSTEM GROUND CHECKED NORMAL.

Part: SLIDE — UNWANTED DEPLOY (CABIN) · airframe 80,014 hrs · 12,692 cycles

RIGHT OVERWING ESCAPE SLIDE WAS BEING DE-ACTIVATED WHEN IT ACCIDENTALLY DEPLOYED. REPLACED RIGHT OVERWING SLIDE ASSEMBLY.

Part: SKIN PANEL — DAMAGED (LT ELEVATOR) · airframe 79,393 hrs · 12,588 cycles

HAIL DAMAGE TO UPPER SKIN PANEL OF LEFT ELEVATOR. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-04.

Part: SKIN — PUNCTURED (LT ELEVATOR) · airframe 79,393 hrs · 12,588 cycles

LEFT OUTBOARD ELEVATOR UPPER SKIN HAS PUNCTURE 125 INCHES FROM OUTBOARD AND 17 INCHES FROM TRAILING EDGE. ACCOMPLISHED BONDED REPAIR PER SRM 51-71-04.

Part: STRUCTURE — DAMAGED (RT ELEVATOR) · airframe 79,393 hrs · 12,588 cycles

RIGHT ELEVATOR UPPER 59 INCHES FROM OUTBOARD AND 25 INCHES FROM TRAILING EDGE. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-04.

Part: SKIN — PUNCTURED (LT ELEVATOR) · airframe 79,393 hrs · 12,588 cycles

LEFT OUTBOARD ELEVATOR UPPER SKIN PUNCTURED 11 INCHES FROM OUTBOARD AND 22 INCHES FROM TRAIILNG EDGE. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-04.

Part: STRUCTURE — DAMAGED (RT ELEVATOR) · airframe 79,393 hrs · 12,588 cycles

RIGHT ELEVATOR UPPER HAS DAMAGE 5.5 INCHES FROM OUTBOARD AND 12 INCHES FROM TRAILING EDGE. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-04.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 79,393 hrs · 12,588 cycles

LEFT OUTBOARD ELEVATOR UPPER SKIN 11 INCHES FROM OUTBOARD AND 16 INCHES FROM TRAILING EDGE DAMAGED. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-04.

Part: STRUCTURE — DAMAGED (LT ELEVATOR) · airframe 79,393 hrs · 12,588 cycles

LEFT OUTBOARD ELEVATOR UPPER HAS PUNCTURE 31 INCHES FROM OUTBOARD AND 25 INCHES FROM TRAILING EDGE. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-04.

Part: STRUCTURE — DAMAGED (RT ELEVATOR) · airframe 79,393 hrs · 12,588 cycles

RIGHT ELEVATOR UPPER HAS DAMAGE 36 INCHES FROM OUTBOARD AND 11.5 FROM TRAILING EDGE. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-04.

Part: STRUCTURE — DAMAGED (LT ELEVATOR) · airframe 79,393 hrs · 12,588 cycles

LEFT OUTBOARD ELEVATOR UPPER HAS DAMAGE 64 INCHES FROM OUTBOARD AND 30.5 INCHES FROM TRAILING EDGE. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-04.

Part: SKIN — PUNCTURED (LT ELEVATOR) · airframe 79,393 hrs · 12,588 cycles

LEFT OUTBOARD ELEVATOR HAS PUNCTURE IN UPPER SKIN 108 INCHES FROM OUTBOARD AND 14 INCHES FROM TRAILING EDGE. ACCOMPLISHED BONDED REPAIR SRM 51-70-04.

Part: STRUCTURE — DAMAGED (LT ELEVATOR) · airframe 79,393 hrs · 12,588 cycles

LEFT OUTBOARD ELEVATOR UPPER HAS DAMAGE 52.5 INCHES FROM OUTBOARD AND 16 INCHES FROM TRAILING EDGE. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-04.

Part: FLAP — PUNCTURED (LT WING) · airframe 79,393 hrs · 12,588 cycles

PUNCTURE ON LEFT OUTBOARD FLAP TRAILING EDGE 108 INCHES FROM OUTBOARD AND 17 INCHES FROM TRAILING EDGE. ACCOMPLISHED BONDED REPAIR PER SRM 57-53-01.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 79,393 hrs · 12,588 cycles

RIGHT OUTBOARD ELEVATOR UPPER SKIN 71.5 INCHES FROM OUTBOARD AND 15 INCHES FROM TRAILING EDGE. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-04.

Part: STRUCTURE — DAMAGED (LT ELEVATOR) · airframe 79,393 hrs · 12,588 cycles

LEFT OUTBOARD ELEVATOR UPPER HAS DAMAGE 46 INCHES FROM OUTBOARD AND 7 INCHES FROM TRAILING EDGE. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-04.

Part: SKIN PANEL — DAMAGED (RT ELEVATOR) · airframe 79,393 hrs · 12,588 cycles

HAIL DAMAGE TO UPPER SKIN PANEL OF RIGHT ELEVATOR. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-04.

Part: STRUCTURE — DAMAGED (LT ELEVATOR) · airframe 79,393 hrs · 12,588 cycles

LEFT OUTBOARD ELEVATOR UPPER HAS DAMAGE 58 INCHES FROM OUTBOARD AND 28 INCHES FROM TRAILING EDGE. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-04.

Part: STRUCTURE — DAMAGED (LT ELEVATOR) · airframe 79,393 hrs · 12,588 cycles

LEFT OUTBOARD ELEVATOR UPPER HAS DAMAGE 43.5 INCHES FROM OUTBOARD AND 23 INCHES FROM TRAILING EDGE. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-04.

Part: STRUCTURE — DAMAGED (LT ELEVATOR) · airframe 79,393 hrs · 12,588 cycles

LEFT OUTBOARD ELEVATOR UPPER HAS PUNCTURE 97 INCHES FROM OUTBOARD AND 32 INCHES FROM TRAILING EDGE. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-04.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 79,393 hrs · 12,588 cycles

RIGHT ELEVATOR UPPER SIDE DAMAGED 108 INCHES FROM OUTBOARD AND 15.5 FROM TRAILING EDGE. ACCOMPLISHED BONDED REPAIR SRM 51-70-04.

Part: SKIN — PUNCTURED (LT ELEVATOR) · airframe 79,393 hrs · 12,588 cycles

LEFT OUTBOARD ELEVATOR UPPER SKIN HAS PUNCTURE 51 INCHES FROM OUTBOARD AND 25.5 INCHES FROM TRAILING EDGE. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-04.

Part: ELEVATOR — DAMAGED (LEFT) · airframe 79,393 hrs · 12,588 cycles

LEFT OUTBOARD ELEVATOR UPPER 43.5 INCHES FROM OUTBOARD AND 23 INCHES FROM TRAILING EDGE. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-04.

Part: SKIN PANEL — DAMAGED (AILERON) · airframe 79,393 hrs · 12,588 cycles

HAIL DAMAGE TO UPPER SKIN PANEL OF RIGHT OUTBOARD AILERON. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-05.

Part: SKIN PANEL — DAMAGED (NR 12 SPOILER) · airframe 79,393 hrs · 12,588 cycles

HAIL DAMAGE TO UPPER SKIN PANEL OF NUMBER 12 SPOILER. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-05.

Part: SKIN — DAMAGED (LT AILERON) · airframe 79,393 hrs · 12,588 cycles

HAIL DAMAGE ON TOP SURFACE OF LEFT WING OUTBOARD AILERON AT TWO LOCATIONS. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-05.

Part: SPOILER — DAMAGED (LT WING) · airframe 79,393 hrs · 12,588 cycles

HAIL DAMAGE TO NUMBER 6 SPOILER. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-5.

Part: SKIN — DAMAGED (NR 2 SPOILER) · airframe 79,393 hrs · 12,588 cycles

HAIL DAMAGE TO THE LEFT NUMBER 2 SPOILER. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-5.

Part: STRUCTURE — DAMAGED (LT ELEVATOR) · airframe 79,393 hrs · 12,588 cycles

LEFT OUTBOARD ELEVATOR UPPER HAS DAMAGE 58.5 INCHES FROM OUTBOARD AND 12 INCHES FROM TRAILING EDGE. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-04.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 73,945 hrs · 11,716 cycles

LEFT NUMBER 4 DOOR EMERGENCY LIGHT EXTERIOR INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 4 DOOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: UNKNOWN — ODOR (CABIN) · airframe 72,904 hrs · 11,544 cycles

MXP - STRONG ELECTRICAL BURNING SMELL BETWEEN ROWS 17 AND 30 (AB SIDE). SMELL WENT AWAY IMMEDIATELY WHEN POWERPORTS WERE TURNED OFF. FLIGHT LANDED MXP WITHOUT INCIDENT. RESET CIRCUIT BREAKER AND CHECKED POWERPORT FROM 17AB TO 30AB AND NO BURNING SMELL NOTED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 71,555 hrs · 11,311 cycles

FOUND THAT THE EXTERNAL DOUBLER WAS KNIFE EDGED BY THE TENSION HEAD LOCK FASTENERS INSTALLED IN THE EXTERNAL DOUBLER. REPAIRED PER EA B767-53-011770 AFW CHOSE TO COMPLETELY TRIM OUT THE DAMAGED SKIN AND TEAR STRAP AND ACCOMPLISH AN SRM REPAIR AND TEAR STRAP SPLICE WITH TITANIUM DOUBLERS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 71,555 hrs · 11,311 cycles

CORROSION WAS FOUND AT STATION 325 FLOOR BEAM AT LEFT BUTTLINE 2 AND RIGHT BUTTLINE 4. A REPAIR STRAP WAS INSTALLED OVER THE TWO BLENDS TO RESTORE LOST STRENGTH. REMOVED CORROSION PER SRM STANDARD PRACTICES, DO NOT EXCEED 0.063 INCH MINIMUM REMAINING. FABRICATED PARTS AND REPAIRED PER EA B767-53-011627.

Part: FSEU — INOPERATIVE (TE FLAP) · airframe 71,430 hrs · 11,291 cycles

DFW - CREW REPORTED FLAPS WOULD NOT RETRACT AFTER TAKEOFF. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLAP SLAT ELECTRONIC UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONTROLLER — FAILED (BLEED AIR SYS) · airframe 70,027 hrs · 11,054 cycles

KIN - INFLIGHT SCL-MIA. CREW REPORTED LEFT AND RIGHT HIGH PRESSURE SHUT OFF VALVE LIGHTS ILLUMINATED. EMERGENCY DECLARED, DIVERTED KIN LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE HIGH PRESSURE CONTROLLER AND HIGH STAGE VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,223 hrs

MIA RIGHT HAND CEILING AT CENTER GALLEY EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT HAND CEILING AT CENTER GALLEY.

Part: CONTACT — DIRTY (EMERGENCY LIGHT) · airframe 26,223 hrs

MIA RIGHT SIDE AFT OVERWING EMERGENCY LIGHT INOPERATIVE. FOUND LAMP CONTACT DIRTY...CLEANED CONTACT.

Part: LENS — MISSING (CABIN) · airframe 26,223 hrs

MIA EMERGENCY LIGHT AT SEAT 23B MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 23B.

Part: CONNECTOR — LOOSE (CABIN) · airframe 26,223 hrs

MIA EMERGENCY LIGHT AT SEAT 31H DIM. SECURED LOOSE CONNECTOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,223 hrs

MIA LEFT HAND AISLE CEILING EMERGENCY LIGHT OVER ROW 4B INOPERATIVE. REPLACED LAMP AT LEFT HAND AISLE CEILING FOR EMERGENCY LIGHT OVER ROW 4B.

Part: LIGHT — INOPERATIVE (CABIN)

DFW EMERGENCY LIGHT AT SEAT 24B INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 24B. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LIGHT — INOPERATIVE (SEAT 20B) · 65,421 cycles

MIA EMERGENCY LIGHT AT FORWARD SEAT 20B INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FORWARD SEAT 20B. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHT AT LEFT AFT DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PSEU — INOPERATIVE (SLATS)

LAX INFLIGHT T5/03DEC DFW TO HNL - LEADING EDGE SLAT ASYMMETRY MESSAGE ILLUMINATED WITH AURAL WARNING HORN. LANDED LAX WITHOUT INCIDENT. REPLACED PROXIMITY SWITCH ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

DFW - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — CHAFED (LEFT ENGINE)

MIA INFLIGHT T963/26OCT DFW TO GRU - LEFT ENGINE PRESSURE RELIEF VALVE EICAS STATUS MESSAGE ILLUMINATED AT FLIGHT LEVEL 300. LANDED MIA WITHOUT INCIDENT. FOUND GROUND WIRE CHAFING WITH STUDS AT NUMBER ONE ENGINE PRESSURE RELIEF VALVE. REPLACED GROUNDING WIRE AND PRESSURE RELIEF VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS)

JFK - EMERGENCY LIGHT AT MID GALLEY RIGHT MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT MID GALLEY RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 26B BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 26B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHT AT SEAT 3B MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 3B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — MISSING (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT 34H HAS MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 34H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 34H HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 34H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS)

MIA - EMERGENCY EXIT LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HEAT EXCHANGER — CRACKED (LEFT)

DFW INFLIGHT T963/04MAY - AT CRUISE LEFT BLEED DUCT OVERHEAT INDICATIONS. RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. RESEATED DUCT LEAK CONTROL CARD AND REPLACED CRACKED LEFT HEAT EXCHANGER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TERMINAL — BROKEN (REGULATOR VALVE)

LIM INFLIGHT T912/02APR SCL TO MIA - CREW REPORTED A LEFT ENGINE BLEED DUCT LEAK INDICATION. LANDED LIM WITHOUT INCIDENT. FOUND BROKEN TERMINAL AT LEFT PRESSURE REGULATOR VALVE AT POINT ONE. REPLACED TERMINAL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LAX - EMERGENCY LIGHTS AT OVERHEAD SEAT 26A INOPERATIVE. REPLACED BATTERY PACK AT SEAT 23A FOR EMERGENCY LIGHTS AT OVERHEAD SEAT 26A. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FLUID — LEAKING (HYDRAULIC SYSTEM)

DFW - HYDRAULIC LEAK (VISIBLE FLUID LEAK) NOTED STREAMING OVER LEFT OUTBOARD AILERON INFLIGHT. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. RAN HYDRAULIC SYSTEM AND FOUND NO LEAKS. FOUND EVIDENCE OF FUEL IN AREA. RAN FUEL PUMPS AND BITE CHECKED ALL TANK SENSORS. NO LEAKS NOTED. FUEL IN TANK WAS 39500 AT TIME. SYSTEM GROUND CHECKED NORMAL OPERATION. ETOPS AIRCRAFT. ER INCIDENT REPORT 1841 DATED 23 NOV 2006.

Part: SIGN — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE AT DOOR R1. REPLACED EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 32B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 32B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 36H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 36H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 35B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 35B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (COCKPIT)

DFW - DURING OVERNIGHT MAINTENANCE, COCKPIT EMERGENCY EXIT LIGHT DIM WHEN TESTED. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 24B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 24B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING SEAT 34H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 34H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE HARNESS — DAMAGED (LT ENGINE)

BOS - FLT 156 - LEFT GEN FAILED WOULD NOT RESET. REPLACE IDG AND TRIED GCU, NO HELP. SERVICED IDGS AND APU PER MPM24-01. IDG DISCONNECTED. BPCU FAULTS CT LOOP GND DP TRIP. MAIN BUS OVER LAP. GEN IFDR. REPAIRED T1/T2/AND T3 IDG LEADS WITH SPLICES AS EPR WIRING REPAIR DOCUMENT INSTALLED ALL LEADS TO IDG TO BE OPS CHECKED. ACCOMPLISHED OPS CHECK OF LEFT ENGINE GENERATOR. (M)

Part: WIRE — BROKEN (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY PATH LIGHTING AT 32HJ INOPERATIVE. REPAIRED BROKEN WIRE AND BATTERY PACK FOR EMERGENCY PATH LIGHTING AT SEAT 32HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TERMINAL — BROKEN (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHT AT SEAT 31H INOPERATIVE. REPLACED BROKEN TERMINAL AT CONNECTOR EMERGENCY ESCAPE PATH LIGHT AT SEAT 31H. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: TERMINAL — BROKEN (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHT AT SEAT 29B INOPERATIVE. REPLACED BROKEN TERMINAL AT CONNECTOR EMERGENCY ESCAPE PATH LIGHT AT SEAT 29B. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: IDG — FAILED (LT ENGINE)

GRU - FLT 999 - LEFT GEN LIGHT FLICKERED ON/OFF FOR 1 HOUR BEFORE STAYING ON. DISCONNECTED GEN DRIVE. REMOVED AND REPLACED LEFT IDG DUE NOTED OIL LEAKAGE AS PER MM. ACCOMPLISHED LEAKAGE AN DOPS TEST AS REQUIRED. OK FOR SERVICE. (M)

Part: WIRE — BROKEN (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT 39H INOPERATIVE. REPAIRED EMERGENCY EXIT WIRE AT SEAT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — SHORTED (CABIN)

SFO - DURING OVER-NIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS AT SEATS 24A AND 24B INOPERATIVE. REPAIRED WIRE AT ROW 20. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — DEFECTIVE (ROW 38H)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT 38H INOPERATIVE. FOUND BROKEN WIRE AT CONNECTOR TO EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT 38J. REPLACED CONNECTOR AND CONNECTOR PINS TO EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 39J. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (BS 385)

AFW - FLOORBEAM AT STA 385 RBL 34 HAD CORROSION BLENDED TOP AND LOWER SURFACE BEYOND SRM LIMITS. BLENDED CORROSION FROM FLOORBOARD HOLES. ALODINED AND PRIMED. TST: 26,387 HOURS. CYCLES: 4,095. (X)

Part: RETAINER — CRACKED (NR 5 LE SLAT)

AFW - NR 5 SLAT HAS A SMALL CRACK ON THE INBOARD EDGE AT SEAL RETAINER. INSTALLED AN EXTERNAL DOUBLER AND FILLER. INSTALLED ALL REPAIR PARTS WET WITH BMS5-95. CHAMFER EDGES, ALODINED AND PAINTED.

Part: SEAT TRACK — CORRODED (BS 347)

AFW - SEAT TRACK AT STA 347 LBL 22 HAD CORROSION BLEND FROM OUTBOARD. REPAIRED IAW MRB 767-1824. TST: 26,387 HOURS. CYCLES: 4,095. (X)

Part: FLOORBEAM — CORRODED (BS 325)

AFW - FLOORBEAM AT STA 325 RBL 34 HAD CORROSION BLENDED. FLOORBEAM AT STA 325 RBL 34 HAD CORROSION BLENDED, TOP AND LOWER SURFACE. TST: 26,387 HOURS. CYCLES: 4,095. (X)

Part: CONNECTOR — FAILED (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PROXIMITY LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PROXIMITY CONNECTOR AT CABIN FLOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: IDG — FAILED (RT ENGINE)

LAX - FLT 999 - CHECKED AND PLACARDED LT GEN SYSTEM INOP AS PER MEL MAN ACCOMPD REQUIRED MPM AS PER MEL MAN CHECKED AND SERVICED LT. RT ENG 'IDG' AND APU IDG ENTERED IN MIC. REPLACED 1 ENG IDG ENG GROUND RUN UP OK. LEAK CHECK OK REMOVED PLACARD 2-37DC-B CLEARED MIC. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY EXIT LIGHT AT PASSENGER SEAT 38HJ INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 38HJ. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: IDG — FAILED (RT ENGINE)

GIG - FLT 0905 - RIGHT GENERATOR DRIVE AND RIGHT GENERATOR OFF LIGHT AND EICAS MESSAGE. RIGHT GENERATOR DISCONNECTED FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED RIGHT IDG PER MM 24-11-01-4-1, PAGES 401 THROUGH 413. OPS CHECK OK. RAN ENGINE PER MM. OPS CHECK OF RT IDG OF REMOVED PLACARD AND CLEARED MIC SHEET. RT IDG OK FOR SERVICE. (X)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 22HJ FOUND INOPERATIVE. RECONNECTED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 22HJ. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: IDG — FAILED (LT ENGINE)

ORY - LEFT GEN DRIVE LIGHT FLICKERED INTERMITTENLY DURING LAST 2 HRS OF FLT. REMOVED AND REPLACED LEFT ENG IDG PER MM ACCOMPLISHED SPLICE REPAIR TO T1 CABLE TO IDG. INSTALLED TERMINAL HOT AND COLD SHRINK TO T1 CABLE NR 1 IDG NR 1 IDG OPS AND LEAKS CHECKED NORMAL. REMOVED PLACARD. (M)

Part: CSD — REQUIRED SERVICE (NR 1 ENGINE)

SCL - FLT 2101 - LEFT GENERATOR DRIVE LIGHT FLICKERS WITHOUT ANY OTHER INDICATIONS. SERVICED NR 1 ENGINE CSD TO PROPER LEVEL. RUN-UP ENGINE OK. AIRCRAFT OK FOR SERVICE. (X)

Part: FIRE LOOP — FAILED (NR 2 ENGINE)

MAD - FLT 68 - LEFT ENGINE FIRE LOOP 2 DISPLAYED ON EICAS. RESEATED LEFT ENGINE FIRE LOOP 2 CONTROL CARD M682 AT P54 AND PERFORMED BITE PER MM ALL IND NORMAL. NO MSGS DISPLAYED ACCESS SECURED CLOSED. (M)

Part: SKIN — CRACKED (FUSELAGE)

SFO - FLT 1539 - DURING A RE-INSPECT OF PREVIOUS FUSELAGE SKIN DAMAGE OF A SCRATCH TWO FEET BELOW AFT RIGHT SERVICE DOOR. PERFORMED EDDY CURRENT INSPECTION THAT REVEALED TWO SKIN CRACKS IN AREA. ONE CRACK WAS A QUARTER INCH AND THE OTHER A .375 INCH CRACK. PERFORMED SHEET METAL REPAIR PER SRM 53-00-01-2, 'FUSELAGE SKIN REPAIR, SMALL HOLE EXTERNAL REPAIR.' REPAIR IS ALL RIGH TFOR A MAXIMUM OF 2500 FLIGHTS OR UNTIL NEXT SCHEDULED C-CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT ON PAX SEAT 9AB INOPERATIVE. REPLACED BROKEN EMERGENCY EXIT LIGHT CONNECTOR ON PAX SEAT 9AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PINS — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PASSENGER SEATS 10B AND 11B FOUND INOPERATIVE. RESEATED LOOSE EMERGENCY EXIT LIGHT PINS AT PASSENGER SEATS 10B AND 11B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS FROM ROW 27 TO ROW 40 FOUND INOPERATIVE. SECURED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR AT SEAT 40 AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)