N305AA

Part: LIGHT — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE FOUND CENTER GALLEY EMERGENCY ESCAPE PATH LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY ESCAPE PATH LIGHT CENTER GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SEQUENCE VALVE — INOPERATIVE (MLG)

JFK - EN ROUTE JFK-MIA, LEFT MAIN LANDING GEAR COMES DOWN WHEN GEAR HANDLE IS PLACED IN OFF POSITION. RETURNED TO JFK LANDED WITHOUT INCIDENT. REPLACED LEFT MAIN GEAR DOOR LATCH AND GEAR OPERATED SEQUENCE VALVE. PERFORMED OPS AND LEAK CHECK PER MM REF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CORRODED (LT/RT WING)

AFW - LEFT AND RIGHT WING UPPER SURFACE HAS CORROSION REMOVAL AS SHOWN ON SKETCH. BLEND OUT CORROSION. PERFORMED HFEC BLENDED AREA FOR CRACKS, ROTO PEEN PER SRM. APPLY ALODINE AND PRIMER TO REWORKED AREA. (M)

Part: STRAP — CORRODED (DOOR FRAME)

AFW - AFT CARGO DOOR FRAME FAIL/SAFE STRAP HAD CORROSION BLEND ON TOP SURFACE. BLEND ALL CORROSION, ROTO PEEN AREA AND REFINISH IAW TO SRM REQUIREMENTS. (M)

Part: STRINGER — CORRODED (BS 434)

AFW - AFT END OF 38L AT STATION 434 WAS BADLY CORRODED. REMOVED CORRODED PIECE OF STRINGER. REPLACED WITH SIMILAR LONGER SPLICE WITHOUT A JOGGLE. (M)

Part: SPLICE — CORRODED (BS 434)

AFW - STRINGER 33R WAS BADLY CORRODED, AFT OF STATION 434. REMOVE CORRODED PIECE OF STRINGER. REPLACE WITH SIMILAR LONGER SPLICE WITHOUT A JOGGLE. (M)

Part: FRAME — CRACKED (BS 1087)

AFW - FOUND CRACK IN THE 146T1501-3 FRAME AND THE 146T1352-14 ANGLE ON THE FRAME. THE CRACK RUNS FROM THE CUTOUT IN THE FRAME AND ANGLE TO A FASTENER HOLE ABOVE THE CUTOUT. REMOVED CRACKED AREA. REMOVED FASTENERS AS REQUIRED. TREATED AND PRIMED AREA OVERSIZED HOLES AND INSTALLED CRES TENSION HEAD HI-LOKS, APPROVED BY ENGINEERING PER MRB 767-1015. (M)

Part: FAIL SAFE STRAP — CORRODED (BS 5395)

AFW - FOUND AND BLENDED OUT CORROSION IN FWD LOCATIONS ON THE UPPER SURFACE OF THE FAIL SAFE CHORD. REFINISHED AND INSTALLED SHIMS AS REQUIRED UNDER STRINGER APPROVED BY ENGINEERING PER MRB 767-1014. (M)

Part: FLOOR BEAM — CORRODED (BS 325)

CORROSION FOUND ON FLOOR BEAM. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND FILLED BLENDED AREA. FABRICATED AND INSTALLED REPAIR STRAP USING .050 INCH 301 HALF HARD STAINLESS STEEL. APPROVED BY ENGINEERING PER MRB767-1009. (M)

Part: SKIN — CORRODED (BS 439)

AFW - FOUND AND BLENDED OUT DAMAGE ON THE INNER SURFACE OF FUSELAGE SKIN. THE BLEND OUT IS APPROXIMATELY 1 INCH BY 2 INCHES WITH APPROX .050 MATERIAL REMAINING. THE DAMAGE IS UNDERNEATH STRINGER 38L. REFINISHED AND INSTALLED A FILLER. APPROVED BY ENGINEERING PER MRB767-1016. (M)

Part: SPLICE — CORRODED (BS 1307)

AFW - FOUND CORROSION ON STRINGER SPLICE, STRINGER 35L WAS TRIMMED BACK 1.5 INCHES TO REMOVE THE CORRODED AREA. FABRICATED AND INSTALLED A NEW SPLICE PIECE IDENTICAL TO OLD USING THE SAME MATERIAL TYPE AND SHAPE EXCEPT THAT NEW PIECE IS LONGER BY THE AMOUNT REMOVED FROM THE STRINGER END. APPROVED BY ENGINEERING PER MRB 767-1013. (M)

Part: SKIN — CORRODED (CTR WING)

AFW - CORROSION REMOVED FROM CENTER WING UPPER SKIN. AFTER BLENDING, FOUND BEYOND LIMITS. REMOVED FASTENERS IN CORRODED AREAS. EDDY CHECKED FASTENER HOLES AND SPOTFACED. SHOT PEENED AND ALODINED AREAS. APPLIED BMS 10-11 SEALANT AND APPLIED FUEL BARRIER TOP COAT. APPROVED BY ENGINEERING PER MRB 767-1012. (M)