N302AA

Part: LIGHT — DIRTY (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, AFT 'IN SEAT' EMERGENCY LIGHT AT SEAT 11H INOPERATIVE. CLEANED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — SHORTED (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS AT SEATS 9H THROUGH 19H INOPERATIVE. REPAIRED WIRE AT SEAT 19H. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: NOZZLE FEEDER — DAMAGED (NR 2 ENGINE)

ORD - FLT 180 - DURING FLIGHT, AIRCRAFT YAWED AND CREW NOTED N1 EGT AND N2 WINDING DOWN. SHUTDOWN ENGINE. ATTEMPTED INFLIGHT START NO SUCCESS. DIVERTED AND LANDED ORD WITHOUT INCIDENT. REPLACED DAMAGED FUEL NOZZLE FEEDER MANIFOLDS AT POSITIONS 10:00 O'CLOCK, 11:00 O'CLOCK, 12:00 O'CLOCK AND 2:00 O'CLOCK. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (ROWS 9-19)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS FROM 9H TO 19H ON RIGHT SIDE OF AIRCRAFT INOPERATIVE. SECURED POWER SUPPLY CONNECTOR TO EMERGENCY EXIT SEAT LIGHTS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: SKIN — CORRODED (WS 798.2)

AFW - RIGHT WING UPPER SURFACE SKIN HAS CORROSION AND INTERGRANULAR CORROSION AT FASTENER LOCATION. REPAIRED PER MRB 767-1960. DRILLED OUT THE CORRODED FASTENERS AND BLENDED OUT CORROSION ON WING SKIN SURFACE. ALODINED ALL BARE ALUMINUM. INSTALLED FREEZE PLUG WET WITH BMS 5-95. INSTALLED STRAP/WASHER 7075T-56 MINIMUM OVERLAP OF .125 INCH PAST THE FREEZE PLUG.

Part: SKIN — CORRODED (BS 718-712)

AFW - FUSELAGE SKIN AT S2R STA 718 HAD CORROSION BLENDED BEYOND LIMITS. REPAIRED PER MRB 767-1962. REMOVED CORROSION PER 767-200 SRM 53 FIG 101. REPLACED FASTENERS IN BLENDED AREA WITH BACR15FV6KE RIVETS. APPLIED ALODINED 1000 TO BLENDED AREA. TST: 56,505 HOURS. CYCLES: 16,666. (X)

Part: FLOORBEAM — CORRODED (BS 286)

AFW - FLOORBEAM AT STA 286 RBL 49 HAD CORROSION BLENDED ON TOP SURFACE BEYOND SRM LIMITS. REPAIRED PER MRB 767-1959. FABRICATED STRAP OUT OF 301 1/2H 55 .050 INCH THICK. ALODINED ALL BARE ALUMINUM PRIME PARTS WITH 2 COATS BMS 10-11 PRIMER FILLED BLENDS WITH BMS 5-92. INSTALLED STRAP BELT WITH BMS 5-92 SEALANT. TST: 56,505 HOURS. CYCLES: 16,666. (X)

Part: WIRE — LOOSE (ROW 24B)

SFO - DURING MAINTENANCE, EMERGENCY EXIT PATH LIGHTS AT SEAT ROW 24B INOPERATIVE. REPAIRED EMERGENCY EXIT WIRING AT SEAT ROW 24B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SWITCH — FAILED (LT WING)

LAX - FLT 10 - AFTER TAKEOFF LAX, AIR INTERRUPTURED WITH LEFT WING EVACUATION SLIDE EICAS MESSAGE. RETURN AND LANDED LAX WITHOUT INCIDENT. REPLACED AND ADJUSTED BOTH PROXIMITY SWITCHES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRINGER — CORRODED (BS 1307)

AFW - FUSELAGE STRINGER AT STATION 1307 HAS CORROSION. FABRICATED NEW STRINGER SPLICE AND INSTALLED PER SRM. (M)

Part: SPLICE — CORRODED (BS 1298)

AFW - STRINGER AND STRINGER SPLICE AT 537L HAD CORROSION. FABRICATED AND REPLACEMENT STRINGER SPLICE FROM .071 INCH THICK 7075-T6 ALCLAD. INSTALLED PER SRM 51-40-02 AND 51-40-03. APPLIED ALODINE AND TWO COATS PRIMER. (M)

Part: FRAME — CORRODED (BS 1175)

AFW - FUSELAGE FRAME AT CAP UPPER SURFACE HAS CORROSION. BLENDED AND REFINISHED PER SRM 53-00-07 FIGURE 101. (M)

Part: KEEL BEAM — CORRODED (BS 800)

AFW - LEFT KEEL BEAM OUTER FLANGE HAD SEVERE CORROSION. CUT OUT CORRODED AREA. FABRICATED A FILLER PIECE FROM 7075-T6 AND A STIFFENING ANGLE FROM 7075-T6 AND INSTALLED PER SRM. (M)

Part: FRAME — CORRODED (BS 1346)

AFW - FAIL/SAFE CHORD HAS CORROSION. FABRICATE A REPAIR ANGLE FROM 7075T6 USING BAC1503400141 THE CORNER OF THE ANGLE SHOULD BE CHAMFERED TO ALOOW PROPER NESTING IN THE EXISTING CHORD. (M)

Part: FRAME — CORRODED (FUSELAGE)

AFW - WHILE IN FOR MBV, MAINTENANCE FOUND AN AREA OF CORROSION ON THE FWD FACE OF THE VERTICAL FLANGE OF THE INNER CHORD ABOVE STRINGER 33R. ENSURE BLENDOUT IS FLAT IN AREA OF THE FASTENER. REFINISH THE BLENDED AREA PER REF SRM. (M)

Part: SKIN — CORRODED (BS 587.5)

AFW - AREA OF CORROSION IN FORWARD CARGO AT ALTIMETER ANTENNA AT STATION 587.5, JUST LEFT OF BL 0. ENSURE THE BLENDOUT IS FLAT IN AREA OF NUTPLATE FOR PROPER RESEATING WHEN REINSTALLED, REFINISH THE BLENDED OUT AREA PER REF SRM. (M)

Part: FIRE SEAL — WORN (LT PYLON)

AFW - FOUND WEAR ON INBOARD AND OUTBOARD OF LEFT PYLON FIRE SEAL AND 2 GAUGES ON PYLON AFT OF PNL 416BR. BLENDED DAMAGED AREA PER SRM, VERIFIED NO CRACKS AND REFINISH PER SRM. (M)

Part: STRINGER — CORRODED (BS 1314-1299)

AFW - STRINGER SPLICE AND STRINGER HAD CORROSION. FABRICATE A REPLACEMENT STRINGER SPLICE FROM .071 THICK 7075-T6. (M)

Part: SENSOR — DEFECTIVE (EMERGENCY EXIT)

ABQ - FLT 0076 - EN ROUTE LAX/IAD DURING CRUISE, RIGHT WING SLIDE DEPLOYMENT LIGHT ON UPPER EICAS SCREEN ILLUMINATED. FOLLOWED ABNORMAL PROCEDURES AND DIVERTED TO ABQ. LANDED WITHOUT INCIDENT, MESSAGE EXTINGUISHED UPON LANDING. REPLACED RIGHT WING SLIDE DOOR, CLOSED SENSOR S219. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: HYD SYSTEM — REQ SERVICE (CENTER HYD SYS)

ORD - FLT 177 - EN ROUTE JFK-ORD, DURING CRUISE, CENTER HYDRAULIC SYSTEM LOW QTY MESSAGE. ACCOMPLISHED ALTERNATE LANDING GEAR AND ALTERNATE FLAP PROCEDURES AND AIRCRAFT LANDED ORD WITHOUT INCIDENT. SERVICED CENTER HYDRAULIC SYSTEM. ACCOMPLISHED LEAK AND GROUND CHECKED WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NROMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (FS 325 LBL 23)

AFW - FLOORBEAM CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND PRIMED BLENDED AREAS. APPROVED FOR CONTINUED SERVICE IN NOTED CONDITION BY ENGINEERING PER MRB 767-953. TST 41,966.02. CYCLES, 13,544. (X)

Part: FLOORBEAM — CORRODED (BS 325 RBL 57)

AFW - FLOORBEAM CORRODED. AFTER BLENDING, FOUND DAMAGE BEYOND SRM LIMITS. ALODINED AND FILLED BLENDED AREAS. FABRICATED AND INSTALLED A REPAIR STRAP USING .050 INCH 301 HALF-HARD STAINLESS STEEL. PRIMED AND PAINTED. REPAIR ACCOMPLISHED. APPROVED BY ENGINEERING PER MRB 767-954. TST 41,944.02. CYCLES, 13,544. (X)

Part: FLOORBEAM — CORRODED (FS 303)

AFW - FLOORBEAM CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND FILLED BLENDED AREAS. FABRICATED AND INSTALLED REPAIR STRAP USING .050 INCH 301 HALF-HARD STAINLESS STEEL. PRIMED REPAIR STRAP. APPROVED BY ENGINEERING PER MRB 767-955. TST 41,966.02. CYCLES, 13,544. (X)

Part: FRAME — CORRODED (FS 1307)

AFW - FOUND AND BLENDED OUT CORROSION ON AFT CARGO FRAME WEB JUST BELOW INNER CHORD AT LBL 32. BLEND OUT GOES ALL OF THE WAY THROUGH THE WEB. FABRICATED AND INSTALLED REPAIR STRAP USING .040 INCH 7075-T6 ALUMINUM PRIMED REPAIR STRAP. APPROVED BY ENGINEERING AND ACCOMPLISHED PER MRB 767-966. TST 41,966.02. CYCLES, 13,544. (X)

Part: FITTING — CORRODED (CARGO DOOR)

AFW - FOUND INTERNAL CORROSION ON THE TEE FITTING LOCATED NEXT TO THE AFT FASTENER HOLE. TRIMMED OUT DISCREPANT AREA. APPLIED ALODINE AND PRIMED. FABRICATED AND INSTALLED FILLER, SHIM, AND STRAP USING 7075-T6 ALUMINUM. PRIMED AND PAINTED. ACCOMPLISHED AND APPROVED BY ENGINEERING PER MRB 95C062. TST 41,966.02. CYCLES, 13,544. (X)

Part: SKIN — CORRODED (FS 1314)

AFW - LOWER FUSELAGE SKIN OUTER SURFACE UNDERNEATH VHF ANTENNA CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. REINSTALLED ANTENNA WITH NEW FASTENERS. APPROVED BY ENGINEERING PER MRB 767-967. TST 41,944.02. CYCLES, 13,544. (X)

Part: STRAP — CORRODED (FS 1270)

AFW - FAIL SAFE STRAP LOCATED ON THE FORWARD SIDE OF THE AFT CARGO DOOR CUT-OUT CORRODED JUST BELOW 533R AND JUST BELOW 532R. BOTH EXCEEDED SRM LIMITS AFTER BLENDING. ROTOPEENED, PRIMED, AND PAINTED BLENDED AREAS. APPROVED FOR CONTINUED SERVICE BY ENGINEERING WITH NOTED CONDITION PER MRB 767-960. TST 41,944.02. CYCLES, 13,544. (X)

Part: SKIN STRAP — CORRODED (FS 1540)

AFW - TEAR STRAP CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND PRIMED BLENDED AREA. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-963. TST 41,966.02. CYCLES, 13,544. (X)

Part: DOOR FRAME — CORRODED (FS 1270)

AFW - FOUND CORROSION ON THE FORWARD SIDE OF THE VERTICAL LEG OF THE INNER CHORD. ALODINED BLENDED AREA AND REINSTALLED FASTENERS. APPROVED FOR CONTINUED SERVICE BY ENGINEERING PER MRB 767-958. TST 41,966.02. CYCLES, 13,544. (X)

Part: SILL — CORRODED (BS 1270)

AFW - INNER CHORD CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. REINSTALLED FASTENERS WITH SHIM AS REQUIRED AFTER ALODING BLENDED AREAS. APPROVED BY ENGINEERING WITH NOTED CONDITION PER MRB 767-959. TST 41,966.02. CYCLES, 13,544. (X)

Part: FLOORBEAM — CORRODED (FS 347)

AFW - FLOORBEAM CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED BLENDED AREAS. FABRICATED AND INSTALLED REPAIR STRAP USING .050 INCH 301 HALF-HARD STAINLESS STEEL. PRIMED AREA. APPROVED BY ENGINEERING PER MRB 767-956. TST 41,966.02. CYCLES, 13,544. (X)

Part: SEAT TRACK — CORRODED (BS 788)

AFW - FOUND CORROSION ON THE SEAT TRACK OUTBOARD FLANGE AT LBL 11 AND ON THE INBOARD FLANGE AT RBL 11. FLAP PEENED BLENDED AREAS. PRIMED BLENDED AREAS. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-957. TST 41,944.02. CYCLES, 13,544. (X)

Part: STRINGER — CORRODED (FS 1263-1285)

AFW - STRINGER CORRODED AROUND FASTENER HOLES. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND PRIMED BLENDED AREAS. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-961. TST 41,966.02. CYCLES, 13,544. (X)