N371AA

Part: WINDOW — OPEN (COCKPIT) · airframe 95,194 hrs · 15,146 cycles

ABORTED TAKEOFF BETWEEN 70 & 75 KNOTS FOR COCKPIT SLIDING WINDOW OPENED ON TAKEOFF ROLL. NO DEFECTS NOTED WITH THE WINDOW, OPERATES NORMALLY. PERFORMED HIGH ENERGY STOP INSPECTION WITH NO DEFECTS NOTED.

Part: O-RING — TORN (HYDRAULIC SYS) · airframe 93,349 hrs · 14,833 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. AT TOP OF DESCENT RECEIVED, C HYD QTY EICAS MSG. QTY CONTINUED TO DECREASE TO .15 DURING FINAL APPROACH. PRESS NEVER INDICATED LOW. FOUND LEAK AT CTR HYD SYS CASE DRAIN DIFFERENTIAL PRESS INDICATOR AT PRESSURIZATION MODULE DUE TO TORN O RING. R & R INDICATOR IAW AMM 29-11-19. PERFORMED LEAK & OPERATIONAL CHECKS. SYSTEM CHECKED NORMAL.

Part: COMPUTER — FAILED (ZONE 200) · airframe 93,074 hrs · 14,789 cycles

AIR INTERRUPT, RETURNED & EMER NOT DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB BOTH FLIGHT MANAGEMENT COMPUTERS FAILED. R & R LT FLIGHT MANAGEMENT COMPUTER IAW AMM 34-61-00. SYS CHECKED NORMAL.

Part: PSEU — FAULTY (LE SLAT) · airframe 92,884 hrs · 14,753 cycles

LEADING EDGE SLAT ASSYM MSG ON CLIMB OUT. FLAP NEEDLES FLUCTUATED BETWEEN 0 & 1. ON ARRIVAL AT JFK, BITE OF PSEU SHOWS CARD FAULT 10 & LE SLAT TARGET FAULT 297. R & R PSEU IAW AMM 32-09-04 & ALTERNATE OTBD SLAT EXT RELAY K221 IAW AMM 27-81-00-735-277.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 92,615 hrs · 14,701 cycles

EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. LE SLAT ASYMMETRY MSG ILLUMINATED AFTER TAKEOFF. LANDED 20 DEGREE FLAPS USING FLAP HANDLE. ACCOMPLISHED FIM 27-81-00. CYCLED SLATS ELECTRICALLY & HYDRAULICALLY MULTIPLE TIMES. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 91,688 hrs · 14,540 cycles

LEFT NR 2 DOOR EXTERNAL EMER LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 2 DOOR EXTERNAL EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 90,659 hrs · 14,382 cycles

FUSELAGE SKIN AT STATION 1460 & STRINGER 28 RT DAMAGED. ACCOMPLISHED REPAIR IAW EA B767-53-035130.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 90,659 hrs · 14,382 cycles

CRACKS FOUND IN OUTER CORD AT RT STATION 1725.5. ACCOMPLISHED REPAIR IAW SRM 53-80-01 REPAIR 5, FIGURE 201 DETAIL 3 & EA B767-53-035085.

Part: FRAME — CRACKED (NR 2 PYLON) · airframe 90,659 hrs · 14,382 cycles

NUMBER 2 PYLON FRAME CHORD AT STATION 285.450 OTBD SIDE CRACKED AT BOTTOM. REPLACED CHORD IAW SRM 51-10-02 & DWG 311T2400.

Part: FRAME — CRACKED (RT PYLON) · airframe 90,659 hrs · 14,382 cycles

RIGHT PYLON FRAME CHORD AT STATION 285.450 INBD SIDE CRACKED AT BOTTOM. REPLACED CHORD IAW B767-300 SRM 51-10-02 & DWG 311T2400.

Part: STIFFENER — CRACKED (RT PYLON) · airframe 90,659 hrs · 14,382 cycles

RIGHT PYLON STIFFENER CRACKED 2 INCHES AFT OF INBD FRAME CHORD AT STATION 285.450. R & R STIFFENER IAW SRM 51-10-02-0G, 51-40-02-0G & DWG 311T2400.

Part: SOCKET — DIRTY (EXTERIOR LIGHT) · airframe 90,659 hrs · 14,382 cycles

EXTERIOR EMERGENCY LIGHT AFT OF LT NR 4 DOOR INOPERATIVE. CLEANED LIGHT SOCKET & REPLACED LIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL.

Part: SKIN — DAMAGED (ZONE 100) · airframe 90,243 hrs · 14,311 cycles

FUSELAGE SKIN DAMAGED FROM BS 1390 - 1480 BETWEEN STRINGERS 27 & 28 RT. INSTALLED EXTERNAL REPAIR IAW EA B767-53-034141.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 89,724 hrs · 14,217 cycles

LT NR 4 EXIT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 4 EXIT EXTERIOR EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 89,724 hrs · 14,217 cycles

OVERWING LIGHT WAS DIM. REPLACED LAMP FOR OVERWING LIGHT. OPERATIONS CHECKED NORMAL.

Part: CONTROLLER — INOPERATIVE (BLEED AIR SYS) · airframe 88,970 hrs · 14,090 cycles

GIG CREW REPORTED DUAL BLEED FAULTS & RT HIGH PRESSURE SHUTOFF VLV EICAS MESSAGE WITH WARNING LIGHT & LT PRESSURE RELIEF VLV MESSAGE DISPLAYED. EMERGENCY DECLARED FLIGHT RETURNED GIG LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED HIGH PRESSURE COMPRESSOR CONTROLLER. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: CHARGER — FAILED (MAIN BATTERY) · airframe 87,135 hrs · 13,799 cycles

CREW REPORTED MULTIPLE ELECTRICAL FAULTS AND MAIN BATTERY CHARGER MESSAGE. EMERGENCY DECLARED FLIGHT RETURNED LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED MAIN BATTERY CHARGER AMD RELAY K102. SYS GROUND CHECK NORMAL OPERATION.

Part: WIRE HARNESS — FAULTY (RT WING) · airframe 85,885 hrs · 13,583 cycles

JFK - INFLIGHT ORD-LHR. CREW REPORTED RIGHT ENGINE HP BLEED AIR *HPSOV* LIGHT ILLUMINATED DURING FLIGHT. FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE WIRE HARNESS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 85,005 hrs · 13,439 cycles

HORIZONTAL STABILIZER CENTER BOX UPPER SKIN FROM STRINGERS 3 TO 2, LEFT BUTTLINE 1.75. INSTALLED DOUBLER PER EA B767-55-027021.

Part: ANGLE — CRACKED (RT PYLON) · airframe 85,005 hrs · 13,439 cycles

RIGHT PYLON CLOSE OUT ANGLE CRACKED. REPLACED ANGLE PER SRM 51-00-05-1.

Part: STRUCTURE — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 85,005 hrs · 13,439 cycles

CORROSION FOUND ON TOP OF HORIZONTAL STABILIZER BOX. REPAIRED CORROSION ON STABILIZER BOX PER EA B767-55-026959.

Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 85,005 hrs · 13,439 cycles

HORIZONTAL STABILIZER CENTER BOX UPPER SKIN FROM STRINGER 1 TO REAR SPAR, RIGHT BUTTLINE 2.75. INSTALLED DOUBLER PER EA B767-55-027021.

Part: STRUCTURE — CRACKED (HORIZ STAB) · airframe 85,005 hrs · 13,439 cycles

RIGHT STATION 1809.5 OUTER CHORD CRACK. ACCOMPLISHED SPLICE REPAIR PER ECO C1945DN.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 85,005 hrs · 13,439 cycles

RIGHT WING OUTBOARD FLAP LOWER SKIN SURFACE DELAMINATED. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-07.

Part: SLAT — DEBONDED (LT WING) · airframe 85,005 hrs · 13,439 cycles

NUMBER 5 LEADING SLAT STARTING TO DISBOND. ACCOMPLISHED BONDED REPAIR PER SRM 57-43-02-01.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 82,561 hrs · 13,054 cycles

SEAT 37H OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 37H OVERHEAD LIGHT. OPS CHECKED NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 82,561 hrs · 13,054 cycles

RIGHT NUMBER 2 DOOR EMERGENCY EXIT LIGHT UPPER INTERIOR LOWER SECTION INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 DOOR EMERGENCY EXIT LIGHT. OPS CHECKED NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 82,561 hrs · 13,054 cycles

L2 DOOR EMERGENCY EXIT LIGHT. REPLACED LAMP FOR L2 EMERGENCY EXIT LIGHT. OPS CHECKED NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 82,561 hrs · 13,054 cycles

MID GALLEY OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR MID GALLEY OVERHEAD EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 82,561 hrs · 13,054 cycles

OVERHEAD EMERGENCY LIGHT AT SEAT 34B INOPERATIVE. REPLACED LAMP FOR OVERHEAD EMERGENCY LIGHT AT SEAT 34B. OPS CHECKED NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 82,561 hrs · 13,054 cycles

OVERHEAD EMERGENCY LIGHT AT SEAT 43C INOPERATIVE. REPLACED LAMP FOR OVERHEAD EMERGENCY LIGHT AT SEAT 43C. OPS CHECKED NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 82,561 hrs · 13,054 cycles

RIGHT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT AFT OVERWING EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 82,561 hrs · 13,054 cycles

FORWARD GALLEY OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR FORWARD GALLEY OVERHEAD EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LENS — LOOSE (CABIN) · airframe 82,059 hrs · 12,973 cycles

EMERGENCY EXIT LIGHT LENS COVER AT RIGHT NUMBER 4 DOOR LOOSE. SECURED LENS COVER FOR RIGHT NUMBER 4 DOOR. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 81,955 hrs · 12,955 cycles

LEFT AFT EXTERIOR EMERGENCY LIGHT NEAR LEFT NUMBER 2 DOOR INOPERATIVE. REPLACED LAMP FOR LEFT AFT EXTERIOR EMERGENCY NEAR LEFT NUMBER 2 DOOR. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 81,955 hrs · 12,955 cycles

RIGHT EXTERIOR EMERGENCY LIGHT NEAR AFT CARGO DOOR INOPERATIVE. REPLACED LAMP FOR RIGHT EXTERIOR EMERGENCY LIGHT NEAR AFT CARGO DOOR. OPS CHECK NORMAL.

Part: BRAKE — OVERHEATED (MLG) · airframe 79,177 hrs · 12,498 cycles

DFW - CREW REPORTED TAIL STRIKE ON TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. BRAKES OVERHEATED UPON LANDING CAUSING ALL MAIN LANDING GEAR TIRES TO DEFLATE. AIRCRAFT REMOVED FROM SERVICE. REPLACED ALL MAIN LANDING GEAR TIRES AND BRAKES. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 78,807 hrs · 12,441 cycles

UPON LANDING RIGHT AFT LAVATORY SMOKE DETECTOR WENT OFF. NO GREEN LIGHT ON. CHECKED LAVATORY FOR SMOKE AND FIRE NONE NOTED. REPLACED SMOKE DETECTOR. OPS CHECK NORMAL.

Part: TRANSFORMER — FAILED (ELECTRICAL SYS) · airframe 78,794 hrs · 12,439 cycles

LHR - INFLIGHT CDG-JFK. CREW REPORTED RIGHT AC BUSS OFF LIGHT WITH CORRESPONDING ELECTRICAL BUS FAILURE. EMERGENCY DECLARED FLIGHT DIVERTED LHR LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CURRENT TRANSFORMER T113. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: STRUCTURE — CRACKED (STABILIZER) · airframe 74,926 hrs · 11,763 cycles

FOUND CRACK INDICATION AT STATION 1809.5 RIGHT FORWARD CHORD FASTENER HOLE. THE HOLE WAS OVERSIZED TO 0.2782 INCH IN ORDER TO REMOVE ANY CRACK INDICATIONS. BOEING REQUIRED AN INSURANCE CUT OF AT LEAST 0.030 INCH. THE INSURANCE CUT RESULTED IN A FINAL HOLE SIZE OF 0.3245 INCH. REPAIRED UNDER ENGINEERING AUTHORIZATION B767-53-008500 N/R 1268153.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,680 hrs · 11,708 cycles

FRAME AT STATION 522 IN THE FORWARD CARGO BETWEEN STRINGER 30 LEFT AND 31 LEFT WERE FOUND DAMAGED. THE SUBJECT DAMAGE IS LIMITED TO THE FRAME INNER CHORD BETWEEN STRINGER 30 LEFT AND 31 LEFT APPROXIMATELY 6 INCHES IN LENGTH. REPAIRED UNDER ENGINEERING AUTHORIZATION B767-53-008462.

Part: STRUCTURE — CRACKED (STABILIZER) · airframe 74,680 hrs · 11,708 cycles

FOUND CRACK INDICATION AT STATION 1809.5 LEFT FORWARD CHORD FASTENER HOLE. THE HOLE WAS OVERSIZED TO 0.2636 INCH IN ORDER TO REMOVE ANY CRACK INDICATIONS. BOEING REQUIRED AN INSURANCE CUT OF AT LEAST 0.030 INCH. THE INSURANCE CUT RESULTED IN A FINAL HOLE SIZE OF 0.341 INCH. REPAIRED UNDER ENGINEERING AUTHORIZATION B767-53-008500 N/R 1268153.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,680 hrs · 11,708 cycles

FRAME AT STATION 500 IN THE FORWARD CARGO BETWEEN STRINGER 30 LEFT AND 31 LEFT WERE FOUND DAMAGED. THE SUBJECT DAMAGE IS LIMITED TO THE FRAME INNER CHORD BETWEEN STRINGER 30 LEFT AND 31 LEFT APPROXIMATELY 6 INCHES IN LENGTH. REPAIRED UNDER ENGINEERING AUTHORIZATION B767-53-008462.

Part: TORQUE BOX — CRACKED (LT PYLON) · airframe 74,680 hrs · 11,708 cycles

FOUND SEVERAL CRACKS AROUND THE LEFT PYLON STRUT TORQUE BOX FORWARD UPPER WEB POWER FEEDER CABLE CUTOUT. REPAIRED UNDER ENGINEERING AUTHORIZATION B767-54-008424 NR 1267610.

Part: SKIN PANEL — DAMAGED (RT WING) · airframe 74,680 hrs · 11,708 cycles

FIVE UPPER SKIN PANEL 666KT FASTENER HOLES ON THE RIGHT OUTBOARD TRAILING EDGE FLAP WERE DAMAGED DURING MAINTENANCE. REPAIRED UNDER ENGINEERING AUTHORIZATION COMP-57-008495.

Part: SKIN — DAMAGED (TE FLAP) · airframe 74,680 hrs · 11,708 cycles

ONE UPPER SKIN PANEL 666JT FASTENER HOLE ON THE RIGHT OUTBOARD LEADING EDGE FLAP WAS DAMAGED DURING MAINTENANCE. REPAIRED UNDER EA COMP-57-008495.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 74,430 hrs · 11,660 cycles

LEFT HAND MID FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY IN FLASHLIGHT.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

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

Part: SKIN — GOUGED (BS 883-873)

AFW - FUSELAGE SKIN BETWEEN STATION 883.5 AND STATION 873 BETWEEN STRINGER 1 RIGHT AND STRINGER 2 RIGHT IN AN AREA OF 1 INCH BY 0.5 INCH WITH AT DEPTH OF .0.76 INCH HAD GOUGES. BLENDED GOUGES PER SRM 530001 FIGURE 101 AND PERFORMED HIGH FREQUENCY EDDY CURRENT INSPECTION FOR CRACKS AND ALODINED.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DFW - NUMBER ONE SLIDE EMERGENCY LIGHT INOPERATIVE. RELAMPED NUMBER ONE SLIDE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT LOWER LEFT OVERWING EXIT SIGN LOWER INOPERATIVE. RELAMPED EMERGENCY LIGHT AT LOWER LEFT OVERWING EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DFW - EMERGENCY FLOOD LIGHT AT AFT RIGHT DOOR INOPERATIVE. RELAMPED EMERGENCY FLOOD LIGHT AT AFT RIGHT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS)

ORD - SEAT MOUNTED EMERGENCY LIGHTS AT FIRST CLASS LEFT HAND SEATS INOPERATIVE. AIRCRAFT OUT OF SERVICE FOR EVALUATION. FOUND SHORTED WIRES AT SIDEWALL CONNECTOR OF SEAT 6AB. REPAIRED WIRES AND REPLACED BATTERY PACK M735 FOR INOPERATIVE SEAT MOUNTED EMERGENCY LIGHTS AT FIRST CLASS LEFT HAND SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS)

MIA - EMERGENCY LIGHT AT SEAT 35H MISSING LENS. REPLACED EMERGENCY LIGHT LENS AT SEAT 35H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT AT OUTSIDE WALL OF LAVATORY INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT OUTSIDE WALL OF LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — DISCONNECTED (CABIN)

LAX - EMERGENCY LIGHT AT SEAT 22B INOPERATIVE. RECONNECTED CONNECTOR AT SIDEWALL FOR INOPERATIVE EMERGENCY LIGHT AT SEAT 22B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW OVERWING EMERGENCY LIGHT FORWARD EXTERNAL INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR OVERWING EMERGENCY LIGHT FORWARD EXTERNAL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

SFO - WITH ALL POWER REMOVED FROM AIRCRAFT COCKPIT OVERHEAD EMERGENCY LIGHT ILLUMINATES. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SILL — CORRODED (FUSELAGE)

AFW - LOWER MAIN SILL OUTER CHORD HAS CORROSION REMOVAL ON VERTICAL LEG INBOARD SURFACE. AREA IS 1.6 INCH BY 3.2 INCH WITH A DEPTH OF 0.039 INCH. BLENDED OUT CORROSION. NO CRACKS FOUND ON HIGH FREQUENCY EDDY CURRENT. REFINISHED THE BLENDED AREA PER SRM. ENSURED SURFACE WAS FLAT FOR PROPER FASTENER INSTALLATION. RETURNED TO SERVICE WITH NOTED CONDITION.

Part: ENGINE — MALFUNCTIONED (LEFT)

MAN - CLIMBING AT FL280 LEFT ENGINE EXPERIENCED TWO COMPRESSOR STALLS. INDICATION ACCOMPANIED WITH HIGH VIBRATION. N2 VIBRATIONS WERE FIVE UNITS. ENGINE POWER WAS REDUCED TO IDLE FOR DESCENT AND LANDING. EVENT RECORD SWITCH PRESSED AT IDLE POWER. LATER ON DECENT EICAS MESSAGE CAME ON LEFT WING ANTI-ICE. REPLACED LEFT ENGINE PER WORK CARD 71 93 01. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY FLOOR PATH LIGHTING AT 22, 23, AND 24HJ, INOPERATIVE. REPLACED BATTERY PACK M732 FOR 22, 23, AND 24HJ EMERGENCY FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (L4 EXTERIOR)

DFW EXTERIOR EMERGENCY LIGHT AT L4 IS INOPERATIVE. RECLAMPED AND SECURED EXTERIOR EMERGENCY LIGHT ASSEMBLY AT L4. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: IDG — MALFUNCTIONED (RT ENGINE)

SFO - FLT 310 - RIGHT IDG DRIVE LIGHT FLICKERED ALMOST CONSTANTLY. IN CLIMB, EICAS GEN DRIVE LIGHT FLASHED ON SEVERAL TIMES BUT ALWAYS WENT OUT PRIOR TO IDG DISCONNECT. PROBLEMS SEEMED OT BE ASSOCIATED WITH HIGHER CLIMB POWER SETTINGS AT CRUISE, ALL SYSTEMS NORMAL. REMOVED AND REPLACED GARLOCK SEAL. REMOVED AND REPLACED RIGHT IDG PER MM 24-11-01-4. LEAK AND OPS CHECK NORMAL LIGHT CHECKS NORMAL. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT PATH LIGHTING AT SEATS 24H AND 29H INOPERATIVE. RESEATED LOOSE CONNECTORS AT SEATS 24H AND 29H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, RIGHT AFT OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERIES FOR RIGHT AFT OVERHEAD EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL. (M)

Part: HARNESS — DEFECTIVE (LT ENGINE)

GIG - FLT 904 - DURING CLIMB-OUT AT FL280, NR 1 ENGINE FIRE STATUS MESSAGE ILLUMINATE. CREW RAN CHECKLISTS AND RETARDED NR 1 ENGINE AND STATUS MESSAGE QUIT. STATUS MESSAGE WAS INTERMITTENT WHILE DUMPING FUEL. FLIGHT RETURNED GIG AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED REQUIRED CHECKS AND PLCARDED NR 1 ENGINE FIRE LOOP. DURING OVERNIGHT MAINTENANCE, NR 1 ENGINE FIRE LOOP DETECTION FAULTED DURING TEST. REPLACED NR 1 ENGINE FIRE LOOP HARNESS. REQUIRED CHECKS PRODUCED NO FAULTS. PLACARD WAS REMOVED AND MIC SHEET CLEARED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (BS 764)

AFW - FLOORBEAM HAS CORROSION ON UPPER SURFACE. REMOVED ALL CORROSION. REFINISHED PER SRM 53-00-01. FILLED BLENDS WITH BMS5-92. TST: 27,711.57 HOURS. CYCLES: 4,361. (X)

Part: FLOORBEAM — CORRODED (BS 347)

AFW - FLOORBEAM AT STA 347 RBL 46 HAD CORROSION BLENDED BEYOND SRM LIMITS. ALODINED THE BLENDED AREA, FABRICATED STRAP FROM 0.50301-1/2 HARD STEEL. APPLIED TWO COATS OF PRIMER TO THE STRAP AND FLOORBEAM. FILLED THE BLENDED AREA WITH BMS5-92 TYPE NRS 1 AND 3. TST: 27,711.57 HOURS. CYCLES: 4,361. (X)

Part: EFIS PANEL — MALFUNCTIONED (LT COCKPIT)

BOS - FLT 70 - CAPTAINS EFIS CONTROL PANEL CIRCUIT BREAKER POPS IN FLIGHT. ONE RESET WAS ATTEMPTED. REMOVED AND REPLACED EFIS CONTROL PANEL OPERATIONAL CHECKS NORMAL. (M)

Part: IDG — FAILED (LT ENGINE)

ORY - FLT 0044 - LEFT GENERATOR DRIVE AND CONTROL OFF ILLUMINATED STEADILY AFTER 5 HOURS FLIGHT WITH ASSOCIATED POWER SHIFT INDICATIONS. LEFT IDG REPLACED AND TESTED IAW MM 24-11-01. ALL OPS CHECK OK. (X)

Part: CONNECTOR — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 35H INOPERATIVE. REPLACED BROKEN EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 35H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PAX SEAT 26H INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 26H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CHAFED (TE AFT FLAP)

AFW - FLAP NOSE SKIN IS CHAFED BEYOND SRM LIMITS IN TWO AREAS. BLENDED SHARP EDGES, EDDY CURRENT CHECKED FILLED WITH BMS 5078 TYPE 3 AND ADJUSTED SEAL RETAINER PER ENGINEERING MRB 767-100. (M)

Part: SKIN — CHAFED (TE AFT FLAP)

AFW - FLAP NOSE SKIN IS CHAFED BEYOND SRM LIMITS IN TWO AREAS. BLENDED SHARP EDGES, EDDY CURRENT CHECKED, FILLED WITH BMS 5-28 TYPE 3 AND ADJUSTED SEAL RETAINER PER ENGINEERING MRB 767-100. (M)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS ON PASSENGER SEAT 20HJ INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CABIN SIDEWALL CONNECTOR BY PASSENGER SEAT 20HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)