N301AA

Part: LIGHT — DISCONNECTED (CABIN)

JFK - FLT 182 - AFTER LANDING BEFORE NEXT FLIGHT EMERGENCY LIGHT IN CEILING PANEL BETWEEN 26G AND 26H DISCONNECTED. LIGHT WOULD NOT STAY IN PLACE. REPLACED LIGHT SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE SEAT PATH LIGHT AT SEAT 7G INOPERATIVE. CONNECTED LOOSE CONNECTOR AT SEAT 7G. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — SHORTED (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS FROM SEAT 31 TO LEFT AFT LAVATORY INOPERATIVE. REPLACED SHORTED WIRE HARNESS UNDER SEAT 35A. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — SHORTED (CABIN CEILING)

JFK - FLT 1262 - AFTER LANDING AND SHUTDOWN SMOKE APPEARED IN AFT CABIN CEILING AREA NEAR LIGHTS. REPAIRED SHORT IN WIRE 122-12 FROM K172 RELAY TO M598 BLOWER MOTOR. ALSO REPAIRED BURNED/DAMAGED PIN IN CONNECTOR D1266. SYSTEM GROUND CHECK NORMAL OPERATION. REPLACED LOGIC CONTROL MODULE AS PRECAUTION. (M)

Part: LIGHT — DEFECTIVE (L2 DOOR)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT LOWER LEFT OF L2 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY BY LOWER LEFT L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LINE — LEAKING (E/E COMPT)

JFK - FLT 0160 - AFTER TAKEOFF, FLIGHT CREW NOTICED AN ELECTRICAL SMELL IN COCKPIT AND FORWARD GALLEY AREA. AIRCRAFT AIR INTERRUPTED AND RETURNED JFK WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND HYDRAULIC FLUID LEAKING FROM GEAR UP LINE. REPAIRED HYDRAULIC GEAR UP LINE PER MM PROCEDURES. SYSTEM LEAK AND OPERATIONS CHECKED OK. SYSTEM GROUND CHECKED, NORMAL OPERATIONS. (X)

Part: AIR DIST — ODOR (CABIN)

ORD - FLT 0003 - EN ROUTE JFK-LAX, A SMOKE SMELL IN CABIN THAT POSSIBLE SMELLED LIKE ELECTRICAL. AIRCRAFT AIR INTERRUPTED AND LANDED ORD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND GROUND RAN ENGINES WITH PACKS BEING CYCLED. UNABLE TO DUPLICATE SMELL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FUSE — TRIPPED (CTR HYD SYST)

ORD - FLT 0177 - EN ROUTE JFK-SFO - CENTER HYDRAULIC QTY EICAS MESSAGE ILLUMINATED IN FLIGHT. ALL PUMPS WERE TURNED OFF WITH QTY STOPPING AT 46. LOWEST FLUID WAS 20. DECLARED EMERGENCY, AIR INTERRUPTED AND LANDED ORD WITHOUT INCIDENT. REPLACED CENTER HYDRAULIC FUSE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FRAME — CORRODED (BS 456/478)

AFW - J-CAP AT STATION 456 ABOVE STRINGER 332 AND J-CAP AT STATION 478 ABOVE LBL 43 HAVE CORROSION. BLEND CORROSION. PLUG EXISTING NUTPLATE. ALODINE ALL BARE ALUMINUM. PLACED ANGLE IN REPAIR AREA TO ENSURE FIT. INSTALL NUTPLATES, SHIM ALL GAPS, FILL ALL VOIDS. (M)

Part: FLOORBEAM — CORRODED (BS 325)

AFW - FLOORBEAM AT STATION 325 RBL 20 HAD CORROSION. REMOVED ALL CORROSION IAW REF C ALODINE, FINISH WITH 2 COATS OF BMS10-11. (M)

Part: SPLICE — CORRODED (BS 434)

AFW - STRINGER 32L HAD SECTION REMOVED DUE TO CORROSION NEAR A PRODUCTION SPLICE AT STATION 434. REMOVE CORRODED PIECE OF STRINGER. REPLACE WITH SIMILAR LONGER SPLICE WITHOUT JOGGLE. ALODINE AND APPLY 2 COATS PRIMER SURFACE SEAL WITH BMS5-95. (M)

Part: FLOORBEAM — CORRODED (BS 325)

AFW - FLOORBEAM AT STAITON 325 RBL 20 HAD CORROSION BLENDED BEYOND LIMITS. REMOVED ALL CORROSION IAW REF C ALODINE, FINISH WITH TWO COATS FO BMS10-11, FILL WITH BMS 5-95. (M)

Part: FRAME — CORRODED (BS 368)

AFW - FOUND CORROSINO ON 'J' CAP BLENDED BEYOND LIMITS AT STATION 368 LBL 36. TRIM FLANGE AS SHOWN IN ATTACHED FIGURE AND ENSURE ALL CORROSION IS REMOVED. FABRICATED REPAIR ANGLE AND FILLER PER SKETCH. FINISH REPAIR ANGLE AND FILLER PER 767 SRM 53-00-07 FIG 101. INSTALLED REPAIR ANGLE PER SKETCH. (M)

Part: SKIN — CORRODED (BS 609)

AFW - FOUND CORROSION BLENDED BEYOND SRM LIMITS, PARENT MATERIAL .260, AREA BLENDED 20 TO 1 MIN .219. PARENT MATERIAL .260, AREA BLENDED 20 TO 1 MINUTE .219. REMOVE CORROSION AND BLEND IAW REFERENCE B ALODINE AND APPLY TWO COATS OF PRIMER. (M)

Part: STRINGER — CORRODED (BS 774)

AFW - FOUND CORROSION BLENDED BEYOND SRM LIMITS ON STRINGER 37L - STATION 774. BLENDOUT CORROSION AND MAKE SURE NO CRACKS EXIST. REFINISH THE BLENDED AREA PER THE REF. ALL FASTENERS COMMON TO THE CORROSION BLENDS ARE .0156 OVERSIZE, USING THE SAME TYPE AS FASTENERS REMOVED. THE SKIN BLEND REPAIR IS SATISFACTORY FOR CONTINUED SERVICE WITH NOTED CONDITION. (M)

Part: FRAME — CORRODED (CARGO DOOR)

AFW - FOUND CORROSION OUT OF SRM LIMITS ON TEE-INNER CHORD, ONE AREA BLENDED. SECOND AREA CORROSION CUT OUT. INSTALLED FILLER OF .125 7075T6 ALUM IN CUTOUT. INSTALLED REPAIR STRAP OF .125 7075T6 ALUM INSTALLED WET W/BMS 5.95 USING BACB30NW6K FASTENERS. BLEND ALL CORROSION. TRIM AREA AS NOTED ON SKETCH, FABRICATE FILLER FROM 7075-T6. FABRICATE REPAIR STRAP FROM .125 7075T6. ALODINE ALL BARE ALUMINUM, APPLY TWO COATS BM510-11 PRIMER. INSTALL STRAP AND FILLER IAW ATTACHED USING BACB30NW6K FASTENERS IAW SRM. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE LIGHT AT SEAT ROW 27H WOULD NOT ILLUMINATED. REPLACED EMERGENCY ESCAPE LIGHT ASSEMBLY AT SEAT ROW 27H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DIRTY (FUSELAGE)

SFO - DURING OVERNIGHT MAINTENANCE, EXTERIOR EMERGENCY EXIT LIGHT FORWARD OF AFT CARGO DOOR INOPERATIVE. CLEANED AND RESEATED CONNECTORS ON EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: KEEL BEAM — CORRODED (BS 795)

AFW - FOUND CORROSION ON KEEL BEAM BEYOND SRM LIMITS AFTER BLEND OUT. FLAP PEENED AND REFINISHED AREA. KEEL BEAM IS SATISFACTORY FOR CONTINUED SERVICE WITH NOTED CONDITION PER MRB 767-1105. (M)