N321AA

Part: SIGN — INOPERATIVE (COCKPIT) · airframe 98,470 hrs · 18,507 cycles

COCKPIT EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. REPLACED COCKPIT EMERGENCY EXIT SIGN. OPS CHECK NORMAL.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,134 hrs · 18,037 cycles

RIGHT KEEL BEAM CHORD OUTBOARD SPLICE FITTING CORRODED. BLENDED PER 767 SRM 51-10-02 AND GENERAL DAMAGE REMOVED. BLENDED AREA AFTER REWORK MEASURES 2 INCHES (FWD/AFT) BY 0.6 INCH HIGH WITH A MIN REMAINING THICKNESS OF 0.288 AND DOES NOT AFFECT FASTENER HOLES. MAJOR EA B767-53-015202 SUBMITTED FOR REMAINING THICKNESS.

Part: SPAR — CRACKED (LT PYLON) · airframe 96,134 hrs · 18,037 cycles

FOUND 1.5 INCH CRACK IN THE LEFT PYLON STRUT FORWARD UPPER SPAR WEB AROUND THE POWER FEEDER CABLE CUTOUT. TRIMMED IT OUT (1.0€ RADIUS) PER BOEING SB 767-54-0090 REV 2 DATED JAN 28, 2010 AND EA B767-54-015200.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 95,080 hrs · 17,829 cycles

EMERGENCY EXIT SIGNS AT LEFT NUMBER 1 AND RIGHT NUMBER 1 DOORS DO NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE TURNED ON. REPLACED BATTERY POWER SUPPLY PACK AT LEFT NUMBER 1 DOOR POSITION. OPS CHECKS NORMAL.

Part: SWITCH — LOOSE (ZONE 200) · airframe 93,057 hrs · 17,410 cycles

EMERGENCY LIGHT SWITCH LOOSE. SECURED EMERGENCY LIGHT SWITCH. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 92,592 hrs · 17,311 cycles

THREE EXTERIOR EMERGENCY LIGHTS ON LEFT AFT FUSELAGE FOUND INOPERATIVE. FOUND BATTERY PACK MODULE M00738 LOCATED BY SEAT 36AB SIDEWALL PANEL DEFECTIVE. REPLACED BATTERY PACK. OPS CHECK NORMAL.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 91,433 hrs · 17,080 cycles

DURING HOLDING FOR JFK WITH ONE CABIN AUTO CONTROLLER INOPERATIVE. CREW REPORTED LOSS OF NUMBER 2 CABIN PRESSURE CONTROLLER. LANDED JFK WITHOUT INCIDENT. REPLACED OUTFLOW VALVE, CABIN ALTERNATE CONTROL PANEL AND NUMBER 2 PNEUMATIC PRESSURE CONTROLLER.

Part: LIGHT — INOPERATIVE (CABIN)

JFK - EMERGENCY EXIT FLOOD LIGHT ASSEMBLY BENEATH LEFT NUMBER 2 FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT FLOOD LIGHT ASSEMBLY BENEATH LEFT NUMBER 2 FLIGHT ATTENDANT SEAT.

Part: CONNECTOR — LOOSE (CABIN)

JFK - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 38H INOPERATIVE. RESECURED LOOSE CONNECTOR AT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY.

Part: FITTING — CORRODED (CARGO BAY) · corrosion level 2 · airframe 85,722 hrs · 15,902 cycles

AFW - CORROSION FOUND UNDER CARGO FITTING AT STATION 612 FORWARD CARGO DOOR CUTOUT. ADDITIONAL CORROSION FOUND IN TWO HOLES JUST AFT OF STATION 612. REPAIRED IN ACCORDANCE WITH SRM 53-00-015 FIG 101 AND MRB 767-3154.

Part: LIGHT — BROKEN (ZONE 200) · airframe 89,505 hrs

LAX - AFT AISLE AT FLOOR EMERGENCY LIGHT HAS ONE SIDE OUT. REPLACED LIGHT ASSEMBLY.

Part: SHROUD — DAMAGED (EMERGENCY LIGHT) · airframe 86,463 hrs

LAX - EMERGENCY LIGHT AT SEAT 20B SHROUD DAMAGED. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 20B. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,463 hrs

LAX - EXTERIOR EMERGENCY LIGHT AT LEFT NR ONE DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LT NR ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LAMP — MISSING (EMERGENCY LIGHT) · airframe 86,463 hrs

LAX - EMERGENCY LIGHT AT SEAT 20B MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 20B. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 86,463 hrs

LAX - EMERGENCY LIGHT AT SEAT 20B MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20B. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 86,238 hrs

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

Part: SKIN — DAMAGED (BS 437) · airframe 85,722 hrs · 15,902 cycles

AFW - FUSELAGE SKIN AT STATION 437 STRINGER 32 RIGHT HAD DAMAGE. AREA OF DISCREPANCY WAS 13.2 INCHES BY 2.2 INCHES. REPAIRED PER SRM 53 00 01 2R AND MRB 767 3160.

Part: SHEAR TIE — CORRODED (FUSELAGE)

MCI - FOUND CORROSION ON SHEAR TIE AT STATION 720 BETWEEN STRINGER 39 LEFT AND 38 LEFT. REPLACED SHEAR TIE AT STATION 720 BETWEEN STRINGER 39 LEFT AND 38 LEFT.

Part: SHEAR TIE — CORRODED (BS 698)

MCI - CORROSION FOUND ON SHEAR TIE AT STATION 698 (FORWARD CARGO BIN) BETWEEN STRINGER 39 LEFT AND 39 RIGHT. REPLACED SHEAR TIES AT STATION 698 BETWEEN STRINGERS 39 LEFT AND 39 RIGHT.

Part: STRINGER — CORRODED (BS 419 S36L)

MCI - FOUND CORROSION ON STRINGER 36 LEFT AT STATION 419 (FORWARD CARGO BIN). REPLACED STRINGER AT 36 LEFT AT STATION 419. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRINGER — CORRODED (BS 454 S35L)

MCI - FOUND CORROSION ON STRINGERS 35 LEFT AT STATION 454. INSTALLED NEW STRINGERS AT 35 LEFT AT STATION 454.

Part: STRINGER — CORRODED (FUSELAGE)

MCI - CORROSION FOUND ON STRINGER 34 LEFT AT STATION 416. REPLACED STRINGER 34 LEFT FROM STATION 393 TO 440. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — CORRODED (FUSELAGE)

MCI - FOUND CORROSION AT AIRCRAFT SKIN BELOW STRINGER 35 LEFT AT STATION 446 TO 451. INSTALLED SKIN REPAIR DOUBLER AT STRINGER 35 LEFT FROM STATION 446 TO 451 PER STRUCTURAL REPAIR MANUAL 53-00-01 AND AA REPAIR DOCUMENT 53 00 01 5. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FLOORBEAM — CORRODED (FUSELAGE)

MCI - FLOORBEAM AT STATION 1329 TO 1351 RIGHT BUTT LINE 16 HAD CORROSION ON BOTTOM SIDE NUT PLATE AREA. REPLACED FLOOR SUPPORT AT STATION 1329 TO 1351 RIGHT BUTT LINE 16.

Part: KEELBEAM — CORRODED (FUSELAGE)

MCI - HEAVY CORROSION ON INBOARD AFT CORNER OF RIGHT HAND PACK AREA ON KEEL BEAM AT STATION 955. INSTALLED NET FIT FILLER IN REWORKED AREA. REINSTALLED FASTENERS PER STRUCTURAL REPAIR MANUAL 53-50-12 AND MRB 767 2874 DATED 06 SEP 2006.

Part: CHANNEL — CRACKED (RT WING)

MCI - RIGHT AND INBOARD WING PANEL SUPPORT U-CHANNEL CRACKED AT AFT INBOARD SIDE OF FALSE SPAR TRAILING EDGE (WING BUTT LINE 110). FABRICATED AND INSTALLED REPAIR L-ANGLE PER SRM 57-51-02 AND MRB 767 2878 DATED 31 AUGUST 2006.

Part: STRINGER — CORRODED (BS 419 S35L)

FOUND CORROSION ON STRINGERS 35 LT AT STA 419 (FORWARD CARGO BIN). REPLACED STRINGERS 35 AT STA 419. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: BEAM — CORRODED (CARGO DOOR)

MCI - FOUND CORROSION ON CARGO DOOR NUMBER TWO INNER CHORD BEAM NUMBER THREE. INSTALLED NEW INNER CHORD BEAM NUMBER THREE ON CARGO DOOR NUMBER TWO.

Part: MOUNT BRACKET — CORRODED (UHF ANTENNA)

MCI - UHF ANTENNA MOUNT BRACKET BELOW CARGO BIN FLOOR AT STATION 1317 HAD CORROSION BETWEEN STRINGER 39 LEFT AND 39 RIGHT. REPLACED UHF ANTENNA MOUNT BRACKET AT STATION 1317 BETWEEN STRINGER 39 LEFT AND 39 RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRINGER — CORRODED (FUSELAGE)

MCI - FOUND CORROSION ON STRINGER 33 LEFT AT STATION 415 (FORWARD CARGO BIN). REPLACED SECTION OF STRINGER FROM STATION 400 TO 434 AT STRINGER 33 LEFT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRINGER — CORRODED (FUSELAGE)

MCI - FOUND CORROSION ON STRINGER 32 LEFT BETWEEN STATIONS 447 AND 453. REPLACED STRINGER 32 LEFT FROM STATION 428 TO 471.

Part: SHEAR TIE — CORRODED (FUSELAGE)

MCI - FOUND CORROSION ON SHEAR TIE AT STATION 356 LEFT BUTT LINE 29 TO LEFT BUTT LINE 34. INSTALLED NEW SHEAR TIE AT STATION 356 LEFT BUTT LINE 29 TO LEFT BUTT LINE 34.

Part: SHEAR TIE — CORRODED (BS 676 S37-38L)

MCI - CORROSION FOUND ON SHEAR TIE AT STATIONS 676 (FORWARD CARGO BIN) BETWEEN STRINGER 37 LEFT AND 38 LEFT. REPLACED SHEAR TIES AT STATIONS 676 BETWEEN STRINGERS 37 LEFT AND 38 LEFT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRINGER — CORRODED (BS 454 S39L)

MCI - FOUND CORROSION ON STRINGER 39 LEFT AT STATION 454. INSTALLED NEW STRINGER AT 39 LEFT AT STATION 454.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - EMERGENCY OVERWING EXIT SIGNS ABOVE HATCH ON RIGHT AND LEFT HAND SIDES INOPERATIVE. REPLACED BATTERY PACK M1209 FOR EMERGENCY OVERWING EXIT SIGNS ABOVE HATCH ON RIGHT AND LEFT HAND SIDES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

AFW BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS ON RIGHT HAND SIDE FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS ON RIGHT HAND SIDE FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — FAILED (HYD SYSTEM)

MCI - INFLIGHT T003 FROM JFK TO LAX LOST CENTER HYDRAULIC SYSTEM QUANTITY APPROXIMATELY TWO HOURS INTO FLIGHT. LANDED MCI WITHOUT INCIDENT. REPLACED HYDRAULIC MODULE AND DELTA P O-RINGS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW RIGHT HAND OVERWING EMERGENCY LIGHTS AND RIGHT HAND FORWARD SLIDE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT HAND OVERWING EMERGENCY LIGHTS AND RIGHT HAND FORWARD SLIDE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

DURING OVERNIGHT MAINTENANCE EMERGENCY ESCAPE PATH LIGHTING SEATS 20H THROUGH 29H FADE/EXTINGUISHED AFTER 1MIN 10 SEC. REPLACED EMERGENCY ESCAPE PATH LIGHTING BATTERY ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SIGN — INOPERATIVE (CABIN)

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

Part: COMPUTER — FAULTY (COCKPIT)

JFK - FLT 52 - NO CAPTAIN FLT DIR, NO AIRSPEED SALMON BUG ON LEFT AUTO PILOT. ACCOMPLISHED MCDP FAUCT FLIGHT REVIEW FAULTED LFCC COMPUTER REPLACED L FCC COMPUTER ACCOMPLISHED ALL REQUIRED TESTS PER MM ALSO ACCOMPLISHED LAND TEST 40 AN CKS NORMAL PER MM. (M)

Part: IDG — FAILED (LT ENGINE)

LHR - FLT 121 - LEFT GENERATOR FAILED ONE HOUR INTO FLIGHT ATTEMPTED ONE RESET UNABLE TO RESET STARTED APU. REPLACED LEFT GCU AND LEFT IDG. ACCOMPLISHED ENGINE RUN AND LEAK CHECK ALL OPS NORMAL. (M)

Part: HARNESS — CONTAMINATED (IDG)

LHR - FLT 121 - LEFT GENERATOR FAILED 10 MINUTES AFTER TAKEOFF, UNABLE TO RESET. STARTED APU RETURNED TO LHR TAXI TIME PRIOR TO TAKEOFF WAS 18 MIN. LEFT IDG/GCU WIRING TROUBLESHOOT IAW B767 FIM 24-20-00-1. ALL FOUND TO BE OK. LEFT IDG ENGINE HARNESS INSPECTED FOR CHAFING. ALL OK. IDG HARNESS FOUND TO HAVE OIL INGRESS FROM PREVIOUS OIL LEAK. IDG HARNESS AND C/P CLEANED ALL OIL REMOVED. C/P RECONNECTED. LEFT ENGINE GROUND RUN FOR 40 MINUTES WITH NUMEROUS ELECTRICAL LOAD CHANGES. ALL OPS AND IND NORMAL. NO REPEAT OF FAULT ON THE GROUND. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 37B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 37B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DAMAGED (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 30H INOPERATIVE. REPAIRED EMERGENCY EXIT WIRE AT SEAT 30H. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 30H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: OVEN — DIRTY (AFT GALLEY)

LAX - FLT 34 - EN ROUTE LAX-JFK - DETECTED FOUL ODOR AT AFT GALLEY. RETUNED LAX AND LANDED WITHOUT FURTHER INCIDENT. CLEANED AFT GALLEY OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: OVEN — DEFECTIVE (F/C GALLEY)

CCS - FLT 935 - EN ROUTE JFK-CCS, DETECTED SMOKE AT FIRST CLASS GALLEY OVEN. LANDED SCS WITHOUT FURTHER INCIDENT. REPLACED FIRST CLASS GALLEY OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, MID-GALLEY RIGHT SIDE EMERGENCY EXIT FLOOR LIGHTING INOPERATIVE. REPLCED EMERGENCY EXT FLOOR LIGHT ASSEMBLY AT RIGHT SIDE OF MID-GALLEY. SYSTEM GORUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — SHORTED (ROW 31 H)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS FROM SEAT 31H TO AFT OF AIRCRFT INOPERATIVE. REPAIRED WIRE IN EMERGENCY EXIT SEAT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: OVEN — DIRTY (GALLEY)

LHR - FLT 0092 - DURING CRUISE, FIRST CLASS RIGHT SIDE NR 2 OVEN SMOKED WHEN OVEN ON. DISCONTINUED USE OF OVEN. LANDED LHR WITHOUT INCIDENT. CLEANED FIRST CLASS RIGHT SIDE NR 2 OVEN. GROUND CHECKED, NORMAL OPERATION. (X)

Part: WINDOW — DEFECTIVE (COCKPIT)

JFK - FLT 142 - DURING CRUISE, FLIGHT CREW NOTICED AN ELECTRICAL SMELL IN THE COCKPIT. FLIGHT AIR INTERRUPTED AND RETURNED JFK AND LANDED WITHOUT FURTHER INCIDENT. REPLACED CAPTAINS NR 1 WINDOW DUE TO TERMINAL BLOCK ARCHING. WINDOW HEAT CHECKED NORMAL WITH NO ELECTRICAL SMELL NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEATS 22HJ, 25AB, AND 33HJ WERE FOUND INOPERABLE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEATS 22HJ, 25AB, AND 33HJ. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT MID-RIGHT HAND GALLEY FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AT MID-RIGHT HAND GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: IDG — FAILED (LT ENGINE)

LEFT GENERATOR DRIVE LIGHT DID NOT EXTINGUISH DURING ENGINE START. ACCOMPANIED BY EICAS MSG. LEFT ENG IDG BPCU BITE CARRIED OUT SHOWS LOW OIL PRESS ON LEFT IDG NL SPARES AT GLA ITEM DEFERRED RIGHT IDG AND APU OIL SERVICE CARRIED OUT. TEST OK ITEM TRANSFERRED TO MIC. REMOVED AND REPLACED LEFT IDG PER MM CHECK LEAK AND OPS CHECK GOOD. REMOVED MEL 10-259DC-13 MIC. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 25B FOUND INOPERATIVE. RE-SECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR UNDER PASSENGER SEAT 25B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 25AB FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR ON PASSENGER SEAT 25AB. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 25B FOUND INOPERATIVE. RE-SEATED LOOSE EMERGENCY EXIT LIGHT CONNECTOR ON PASSENGER SEAT 25B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: SKIN — CORRODED (BS 434)

AFW - FOUND AND BLENDED OUT DAMAGE ON THE EXTERNAL SURFACE AT THE FUSELAGE SKIN. THE BLEND OUT WAS FOUND TO EXCEED SRM LIMITS. REFINISHED THE BLENDED AREA. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB767-1421. (M)

Part: IDG — REQ'D SERVICE (RT ENGINE)

JFK - FLT 0099 - AT 5 HRS 15 MINS INTO FLIGHT, RIGHT GEN DRIVE LIGHT CAME ON STEADY WITH ASSOCIATED EICAS MESSAGE. RIGHT GENERATOR CONTROL OFF LIGHT CAME ON BEFORE DISCONNECTING GENERATOR. RIGHT GEN DRIVE DISCONNECT SWITCH WAS PRESSED PER OM PROCEDURE. DEFERED NR 2 RT GENERATOR INOP PER MEL. CKD AND SERVICED BOTH IDG ENG AND APU OILS TO FULL. ENTERED IN MIC SHEET. REMOVED AND REPLACED RT ENGINE IDG. OPS CHK OFF IDG GOOD PER MM ON ENG RUN. REMOVED MEL 2-114DC-B. CLEARED MIC SHEET. (X)

Part: CONNECTOR — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PAX SEATS 25B AND 27B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AND CONTACT AT PAX SEAT 27B AND RESECURRED EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 25B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PAX SEATS 31B AND 37H INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTORS AT PAX SEATS 31B AND 37H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WING SKIN — CORRODED (FS 955)

AFW - FOUND WING BOX SKIN UPPER SURFACE HAS CORROSION BEYOND SRM LIMITS AFTER BLEND OUT. REPAIRED 'T' CHORD USING SRM 51-70-12 AS A GUIDE PER ENGINEERING MRB 767-1027. (M)

Part: FLOOR BEAM — DENTED (BS 478)

AFW - FOUND FLOOR BEAM LOWER FLANGE AND BOTTOM OF WEB ARE DENTED. INSTALLED 0.080 BY 2.5 BY 13 INCH 7075-0 REPAIR ANGLE PER ENGINEERING MRB 767-1025. (M)

Part: TRUNNION — CORRODED (RT MLG)

AFW - BLENDED LOCAL CORROSION IN AFT TRUNNION BORE PER BOEING SB 767-3240148. BLENDED AREA PER BOEING SB 767-3740148 AND ENGINEERING MRB 767-1099. (M)

Part: FRAME — CORRODED (BS 676)

AFW - FOUND AREA ON FORWARD CARGO FRAME UPPER CHORD BEYOND SRM LIMITS AFTER BLEND OUT. VOIDS FILLED WITH BMS5-25. CHORD IS SATISFACTORY FOR CONTINUED SERVICE WITH NOTED CONDITION PER ENGINEERING MRB 767-1092. (M)

Part: FLOOR BEAM — CORRODED (BS 950)

AFW - FLOOR BEAM HAS CORROSION BEYOND SRM LIMITS AFTER BLEND OUT. FLOOR BEAM IS ACCEPTABLE FOR CONTINUED SERVICE WITH NOTED CONDITION PER ENGINEERING MRB 767-1093. (M)

Part: TRUNNION — CORRODED (LT MLG)

AFW - FOUND LOCAL CORROSION IN AFT TRUNNION BORE. BLENDED AREA PER BOEING SB 767-3240148 AND ENGINEERING MRB 767-100. (M)

Part: EEL CONNECTOR — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY SEAT LIGHTS ON LEFT SIDE OF ROW 31 FOUND INOPERATIVE. REPLACED CONNECTOR AT SEAT ROW 33. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: EEL LAMP — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, SEAT MOUNTED EMERGENCY FLOOR LIGHTS AT SEATS 8B AND 9B FOUND INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY FLOOR LIGHTS AT SEATS 8B AND 9B. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)