N324AA

Part: FRAME — CORRODED (FUSELAGE) · airframe 100,253 hrs · 19,160 cycles

FUSELAGE FRAME AT STATION 977 CORRODED. ACCOMPLISHED NESTED REPAIR ANGLE PER EA B767-53-014290 REVISION B.

Part: SPAR — CRACKED (PYLON) · airframe 100,253 hrs · 19,160 cycles

PYLON STRUT FORWARD UPPER SPAR WEB CRACKED AT POWER FEEDER CABLE PASS THROUGH. REMOVED DAMAGE AND INSTALLED DOUBLER PER AARD 54-52-01-1.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 97,703 hrs · 18,644 cycles

EMERGENCY LIGHTS IN FIRST CLASS LEFT SIDE WILL NOT TURN OFF AFTER TEST. REPLACE BATTERY PACK FOR FIRST CLASS LEFT SIDE EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 97,703 hrs · 18,644 cycles

EMERGENCY LIGHTS WILL NOT TURN OFF AFTER TEST. REMOVED AND REPLACED BATTERY PACK.

Part: CIRCUIT BREAKER — DEFECTIVE (GALLEY) · airframe 97,609 hrs · 18,624 cycles

ORD - INFLIGHT JFK-SFO. CREW REPORTED FAINT BURNING ODOR IN COCKPIT AND CABIN. EMERGENCY DECLARED FLIGHT DIVERTED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT SIDE 15 AMP CIRCUIT BREAKER FOR CHILLER IN AFT GALLEY. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,913 hrs · 18,076 cycles

CORROSION ON THE FUSELAGE STATION 977 FRAME OUTER CHORD AT RIGHT BUTTLINE 95 BETWEEN WATERLINES 183 TO 187. INSTALLED L ANGLE PER EA B767-53-014290.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 93,118 hrs · 17,707 cycles

HNL - INFLIGHT KOA-LAX. CREW REPORTED CENTER HYDRAULIC SYSTEM QUANTITY LOSS. QUANTITY INDICATION WENT TO ZERO. EMERGENCY DECLARED DIVERTED HNL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND FLEX HOSE ON C2 ELECTRIC PUMP LEAKING. REPLACED PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION (CLOSED) / FLEX HOSE REF 20-10-4, OPS AND LEAK CHECK GOOD. RE-SERVICED HYD QTY TO FULL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 92,701 hrs · 17,621 cycles

SEAT AISLE LIGHTS DIM FROM SEAT 7HJ TO 17HJ. REPLACED BATTERY PACK FOR SEAT AISLE LIGHTS. OPS CHECK NORMAL.

Part: MODULE — INOPERATIVE (CABIN) · airframe 91,210 hrs · 17,325 cycles

EMERGENCY AISLE LIGHT AT LEFT COACH INOPERATIVE. REPLACED MODULE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 91,210 hrs · 17,325 cycles

EMERGENCY LIGHT SEATS IN LEFT COACH SECTION INOPERATIVE. REPLACED BATTERY PACK M9032.

Part: COMPRESSOR BLADE — DAMAGED (LT ENGINE) · airframe 90,014 hrs · 17,085 cycles

JFK - INFLIGHT EWR-LAX. AIRCRAFT HAD BIRD STRIKE TO LEFT ENGINE AND LEFT ENGINE VIBRATIONS ON TAKEOFF. LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED BOROSCOPE INSPECTION AS PER MM 72-00-00-6. NO DISCREPANCIES NOTED. REMOVED AND REPLACED FAN BLADES NUMBER 3, 4, 5, 6 AND 7 AS PER BOEING 767 MM 72-31-02-4. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (CABIN) · airframe 89,112 hrs

JFK - EMERGENCY LIGHTS AT SEAT 7B INOPERATIVE. REPAIRED BROKEN WIRES AT SIDEWALL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 89,077 hrs

JFK - ROWS 10, 11, 17 AND 19 EMERGENCY EXIT FLOOR LIGHTING FLICKERED DURING FLIGHT. REPLACED BATTERY PACK.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 89,077 hrs

JFK - ROWS 10, 11, 17, AND 19 EMERGENCY EXIT FLOOR LIGHTING FLICKERED ON AND OFF DURING FLIGHT. REPLACED EMERGENCY LIGHT POWER SUPPLY M9030.

Part: LENS — MISSING (CABIN) · airframe 89,066 hrs

JFK - EMERGENCY LIGHT ON RIGHT SIDE FORWARD IN FIRST CLASS AFT OF RIGHT NUMBER ONE DOOR MISSING LENS. REPLACED LENS.

Part: ANTI-SKID SYS — INOPERATIVE (MLG) · airframe 88,804 hrs · 16,835 cycles

JFK CREW RECIEVED AN ANTI-SKID MESSAGE WITH THE LEFT THRUST REVERSER INOPERATIVE. EMERGENCY DECLARED LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CHAFFING WIRING ON LEFT ENGINE HARNESS AND REPLACED THE ANTISKID/AUTOBRAKE CONTROL UNIT. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)

Part: ENGINE — SHUTDOWN (NR 1) · airframe 85,968 hrs

JFK INFLIGHT T20/11JUN. AT FLIGHT LEVEL 230 NR ONE ENGINE UNCOMMANDED SHUT DOWN. LANDED JFK WITHOUT INCIDENT. SINGLE ENGINE TIME 20 MINUTES. REPLACED NR ONE ENGINE ON 11JUN AT JFK. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: METERING VALVE — DEFECTIVE (NLG STEERING) · airframe 85,505 hrs

JFK INFLIGHT T686/25APR - DURING TAKEOFF AIRCRAFT PULLED TO LEFT. REQUIRED .75 RUDDER PEDAL TO KEEP AIRCRAFT ON CENTERLINE. AFTER TAKEOFF ANOTHER AIRCRAFT REPORTED SMOKE FROM NOSE TIRES AND OBSERVED NOSE WHEEL TURNED LEFT OF CENTER. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR STEERING METERING VALVE AND BOTH NOSE GEAR TIRE WHEEL ASSEMBLIES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — CORRODED (BS 412-434 S37L) · airframe 84,775 hrs · 15,991 cycles

AFW - FUSELAGE SKIN HAS CORROSION ON INNER SURFACE AT STATION 412 TO 434 UNDER S37L. BLENDED OUT CORROSION USING A MINIMUM TAPER RATIO OF 20 TO 1. VISUALLY CONFIRMED NO FURTHER CORROSION. PERFORMED HIGH FREQUENCY EDDY CURRENT ON BLENDED AREAS AND HOLES SURROUNDING BLENDS. TREATED BLENDED AREAS WITH ALODINE AND TWO COATS PRIMER AND FILLED WITH BMS595 SEALANT.

Part: SKIN — CORRODED (BS 1081-1087) · airframe 84,775 hrs · 15,991 cycles

AFW - FUSELAGE SKIN AT STATION 1081 TO 1087 BETWEEN S39R AND S39L HAD CORROSION BLENDED ON INNER SURFACE BEYOND SRM LIMITS. BLENDED CORROSION FROM PARENT THICKNESS OF 0.316 INCH WITH REMAINING THICKNESS NO LESS THAN 0.252 INCH AND 0.233 INCH. INSPECTED BLENDED AREA TO CONFIRM COMPLETE REMOVAL OF DAMAGE PER 767 200 SRM 51 10 02 06. ACCOMPLISHED EDDY CURRENT INSPECTION TO ENSURE NO CRACKING AT BLENDED AREAS.

Part: SKIN — NONE · airframe 84,775 hrs · 15,991 cycles

AFW - FUSELAGE SKIN AT STATION 1582 HAD A TEMPORARY REPAIR. AREA OF DISCREPANCY IS 3.8 INCH BY 2.7 INCH. ACCOMPLISHED PERMANENT REPAIR FOR FUSELAGE SKIN AT STATION 1582 STRINGER 25L.

Part: STRINGER — CORRODED (BS 1300 S37L) · airframe 84,775 hrs · 15,991 cycles

AFW - STRINGER 37L AT STATION NUMBER 1300 WAS CORRODED JUST FORWARD OF A PRODUCTION SPLICE. FABRICATED AND INSTALLED EXTENDED SPLICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

JFK - EMERGENCY LIGHTS AT SEAT ROWS 10 AND 11 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 10 AND 11. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

JFK - EMERGENCY LIGHT AT SEAT ROW 19B INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 22D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

JFK - EMERGENCY LIGHTS FROM SEATS ROWS 10AB TO 11AB INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT ROWS 10AB TO 11AB. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

JFK - EMERGENCY LIGHT AT SEAT 19B INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 19B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

JFK - EMERGENCY LIGHT AT SEAT 27B MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 27B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — DAMAGED (LT PYLON)

AFW - LEFT AND RIGHT PYLON OUTBOARD SKIN AT STATION 250 HAD GROOVE WORN FROM THRUST REVERSER SEAL RETAINER. AREA WAS 6 INCHES BY .7 INCH WITH A DEPTH OF .125 INCH AND WAS SIX INCHES LONG. DAMAGE WAS BLENDED PER SRM. A HIGH FREQUENCY EDDY CURRENT INSPECTION WAS ACCOMPLISHED AND AREA REFINISHED.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

LAX - SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 31 TO 40AB INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK MODULE FOR SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 31 TO 40AB. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — PINCHED (EMERGENCY LIGHT)

LAX - EMERGENCY LIGHTS AT SEATS 10, 11 AND 17HJ WILL NOT EXTINGUISH AT END OF LIGHT TEST. FOUND MID GALLEY FLOOD LIGHT WIRES PINCHED BENEATH GALLEY FLOOR. REPLACED MID GALLEY FLOOD LIGHT ASSEMBLY WIRES FOR EMERGENCY LIGHTS AT SEATS 10, 11 AND 17HJ. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COMPRESSOR — STALLED (ZONE 600)

ORD - DURING CRUISE AT FL370 EXPERIENCED THREE COMPRESSOR STALLS. ALL ENGINE INDICATIONS REMAINED NORMAL, NO VARIATIONS. FLIGHT ATTENDANTS REPORTED SPARKS COMING OUT OF RIGHT HAND ENGINE. SPARKS CONTINUED INTERMITTANTLY DURING DECENT WHENEVER POWER WAS CHANGED. REPLACED RIGHT HAND ENGINE PER WORKCARDS 71-94-01 AND 71-95-18 AND ALL ATTACHMENTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DAMAGED (EMERGENCY LIGHT)

JFK LT MID GALLEY CROSS AISLE EMERGENCY LIGHT INOPERATIVE. FOUND HIGH RESISTANCE AT L9072 GROUND SPLICE. RESPLICED AT L9072 GROUND SPLICE FOR LEFT HAND MID GALLEY CROSS AISLE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PLATE — CORRODED (FUSELAGE)

DURING REMOVAL OF H-11 BOLTS THROUGHT THE SPLICE PLATE PER SB 767-57A0046, TWO HOLES WERE FOUND CORRODED AND REQUIRED OVERSIZING THE HOLES WERE COMMON TO THE HORIZONTAL FLANGES OF THE CENTER WING SPAR CHORD AND THE OUTBOARD WING SPAR CHORD. REMOVED HOLE BORE CORROSION DAMAGE BY REAMING THE OUTBOARD HOLE TO THE SECOND OVERSIZE AND THE INBOARD HOLE TO THE NEXT FULL DIAMETER.875 INCH. HFEC INSPECTION BOTH HOLES TO ENSURE A CORROSION AND CRACK FREE CONDITION. REFINISH RE-WORKED AREA PER SRM AND INSTALL A BACB300S14RK .875 INCH AND BACB3OUS12KY, 2ND OVERSIZE .75 INCH BOLTS IN THE APPLICABLE HOLE INSTEAD OF THE NOMINAL BACB3OUS12K .75 INCH BOLTS SEAL THE FASTENERS PER SB 767-57A0046. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

AFW - FOUND FLOORBEAM AT BL33 LEFT AND RIGHT STATION 890 AND STATION 933 HAD CORROSION BLEND FROM TOP SURFACE BEYOND SRM LIMITS. SEE ATTACHED DRAWINGS. REQUEST ENG APPROVAL TO SHOT-PEEN, ALODINE, 2 COATS OF PRIMER AND SEAL W/BMS 5-95. REMOVED CORROSION PER REF 1A1. ROTO-PEEN BLENDED AREA. REFINISHED BLENDED AREAS WITH ALODINE AND 2 COATS PRIMER. FILL BLENDS W/BMS5-95 SEALANT. (M)

Part: SLIDE — INOPERATIVE (R1 DOOR)

LAX - FLT 3 - UPON ARRIVAL, R1 DOOR INADVERTENTLY DEPLOYED. SLIDE PARTIALLY DEPLOYED. REPLACED R1 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — BROKEN (MID GALLEY)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT MID GALLEY BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS AT SEAT 28H INOPERATIVE. REPLACED CONNECTOR AT SEAT 28H. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: MANIFOLD — DEFECTIVE (RT ENGINE)

GIG - FLT 972 - ON INITIAL ENGINE START UP ON RAMP DURING PUSH OUT, FUEL LEAK NOTED FROM RIGHT ENGINE. ENGINE WAS SHUTDOWN WITHOUT FURTHER INCIDENT. FOUND RIGHT ENGINE UPPER FUEL NOZZLE MANIFOLD LEAKING. REPLACED RIGHT ENGINE UPPER FUEL NOZZLE MANIFOLD AND SEALS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, BOTH OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. RESEATED CONNECTOR TO BATTERY PACK MODULE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: VALVE — CLOGGED (LT ENGINE)

SFO - FLT 682 - AFTER TAKEOFF SFO, EN ROUTE TO ORD SMOKE AND FUMES NOTED IN THE CABIN. RETURNED TO SFO AND LANDED WITHOUT INCIDENT. REPLACED 8TH STAGE CHECK VALVE AND DUCTING TO PRE-COOLER DUE TO LINE BEING PLUGGED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — CORRODED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, LEFT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED CORROSION FROM LEFT FORWARD EMERGENCY EXIT LIGHT SOCKET AND RELAMPED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — CHAFED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, RIGHT HAND EMERGENCY EXIT PATH LIGHTS FROM SEAT ROW 31H AFT INOPERATIVE. REPAIRED WIRE AT AFT RIGHT EMERGENCY EXIT DOOR SIGN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — DEFECTIVE (CABIN)

JFK - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT AFT RIGHT LAVATORY FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AT AFT RIGHT LAVATORY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: MODULE — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS ON LEFT SIDE OF FIRST CLASS AND BUSINESS CLASS SEATS AND UNDER FORWARD FLIGHT ATTENDANT SEATS FOUND INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT MODULE AT SEAT 3A. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)

Part: WIRE — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT LIGHT AT SEAT 27H INOPERATIVE. REPAIRED BROKEN WIRE AT SEAT 27H CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT LIGHT AT SEAT 17 H/J INOPERATIVE. REPAIRED PIN THAT WAS PUSHED BACKED AND RESEATED CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PROCESSING UNIT — FAILED (LT FUEL TANK)

JFK - LEFT TANK FUEL QTY INDICATOR INTERMITTENTLY GOES BLANK. TOTALIZER GOES BLANK ALSO. BITE OF FQI BOX SHOWS FAULT CODE C1 51 5355 56 57 58 59 AND 60 TSM POINTS TO LT TANK UNITS AND OR WIRING DEFER L MAIN TANK FUEL TANK TO QTY INOP AS PER MEL 28-11A ENT IN MIC AUTH 11-120DC-C DFRL. REPLACED FQIS PROCESSOR UNIT. PERFORMED REQUIRED TESTS. NO FAULTS OPS CHECK GOOD. (M)

Part: GCU — FAILED (E/E COMPT)

GEN DRIVE LIGHT RIGHT SIDE DISCONNECTED IDG. PLACARD RT IDG INOP IAW MEL SERVICED LEFT AND RIGHT IDGS TO FULL SERVICED APU TO FULL. NO RESCENT HISTORY. NO FAULT FOUND ON LEFT IDG OR APU. ENTERED ITEM ONTO MIC SHEET. REPLACED RT GEN CONTROL UNIT OPS CHECKED NORMAL PER MM ON RUN UP, REMOVED MEL 7 172 DC B CLRD MIC. (M)

Part: LIGHT — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT OVER COCKPIT DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LGHT OVER COCKPIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: IDG — FAILED (LT ENGINE)

LT GEN DRIVE DISC LIGHT ON OVERHEAD PANEL ILLUMINATED. LT GEN DRIVE ON EICAS ILLUMINATED. DISCONNECTED LT GEN DRIVE FOR REMAINDER OF FLT. REMOVED AND REPLACED LT IDG PE MM 24-11-01, NEEDS OPS AND LEAK CHECK. PERFORMED OPERATIONAL AND LEAK CHECK OF LT IDG. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 29H INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 29H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 24B INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 24B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONTACT — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 30H INOPERATIVE. REPLACED BROKEN EMERGENCY EXIT LIGHT CONTACT AT PASSENGER SEAT 30H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 33H INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 33H. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)

Part: FLOOR BEAM — CORRODED (FS 287)

AFW - FLOOR BEAM HAS CORROSION ON UPPER CHORD. FABRICATE A REPAIR STRAP FROM .050 INCH 301 1/2 HARD STAINLESS STEEL AND INSTALL WET WITH BMS 5-25 SEALANT. ALODINED, PRIMED AND PAINTED PER ENGINEERING MRB 767.

Part: SKIN — CORRODED (FS 956)

AFW - HEAVY CORROSION ON CENTER WING UPPER SKIN AT AFT DRAIN. FABRICATE A REPAIR STRAP FROM .100 THICK 7075-T6 ALUMINUM AND INSTALL WET WITH BMS 5-25. SEALANT FLAPPER PEEN, ALODINED, PRIMED AND PAINTED PER ENGINEERING MRB B767-858.

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 8H THROUGH 11H INOPERATIVE. RECONNECTED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT 8H. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)

Part: EEL WIRE — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT RT AISLE IN BUSINESS CLASS AND MAIN CABIN FOUND INOPERATIVE. REPAIRED EMERGENCY FLOOR LIGHT WIRE SPLICES IN BUSINESS CLASS AND MAIN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)

Part: EEL WIRE — FAILED (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT PAX SEAT ROWS 7H AND 8H INOPERATIVE. REPAIRED DEFECTIVE WIRE SPLICE BY PAX SEAT 7H. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)