N713AX

Part: LIGHT — DEFECTIVE (CABIN) · airframe 71,612 hrs · 21,993 cycles

EMERGENCY LIGHT ASSEMBLY AT MAIN ENTRY DOOR INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY IAW B767 AMM CHAPTER 33. OPS CHECKED GOOD.

Part: PANEL — MISSING (RT PYLON) · airframe 70,924 hrs · 21,724 cycles

ON WALKAROUND, MAINTENANCE FOUND NR 2 ENGINE INBOARD PYLON PANEL MISSING. DEFERRED 57076. C/W REA B654-56397, APPLIED SPEED TAPE. DEFERRED IAW REA B654-56397 AND GMM CHAPTER 1, SECTION 7.04 FOR MX TRACKING. CLEARED: DI 57076, INSTALLED NEW PANEL 446BL IAW B767 SRM 51-40-02.

Part: SLIDE — UNWANTED DEPLOY (PAX DOOR) · airframe 70,579 hrs · 21,562 cycles

FIRST OFFICER DEPLOYED SLIDE INADVERTANTLY. REMOVED AND REPLACED MAIN ENTRY DOOR SLIDE IAW B767 AMM 21-58-1-1.

Part: DOUBLER — CRACKED (NR 2 NACELLE) · airframe 70,525 hrs · 21,539 cycles

NR 2 PYLON INTERIOR DOUBLER CRACKED AT AFT LOWER EDGE OF OUTBOARD STRUT DOOR. REMOVED AND REPLACED DOUBLER IAW B767 SRM.

Part: INTERCOSTAL — CORRODED (BS 368) · airframe 70,525 hrs · 21,539 cycles

LEVEL I CORROSION ON SUBFLOOR STRUCTURES AT FLOORBEAM BS 368 AND 9G ATTACH POINT CUTOUTS. REMOVED AND REPLACED FITTING IAW B767 SRM 51-10-02.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 70,525 hrs · 21,539 cycles

FORWARD LOWER CARGO DOOR JAMB AFT SILL MOUNTED BASE FITTING WAS CRACKED. REMOVED AND REPLACED FORWARD LOWER CARGO DOOR JAMB AFT SILL MOUNTED BASE SIDE GUIDE RAIL IAW B767 SRM 51-40-02.

Part: FITTING — CRACKED (CARGO DOORWAY) · airframe 70,525 hrs · 21,539 cycles

AFT LOWER CARGO DOOR JAMB FORWARD SILL MOUNTED BASE FITTING CRACKED. REMOVED AND REPLACED FITTING IAW B767 SRM 51-40-02.

Part: STRUT — CRACKED (NR 2 NACELLE) · airframe 70,525 hrs · 21,539 cycles

INTERIOR STRUCTURE CRACKED STRUT TRAILING EDGE ASSEMBLY 447DB. REMOVED AND REPLACED CRACKED STRUCTURE IAW B767 SRM.

Part: BEAM — CORRODED (AFT CARGO DOOR) · airframe 70,525 hrs · 21,539 cycles

HORIZONTAL BEAM ON AFT CARGO DOOR HAD CORROSION AROUND 1 NUT PLATE JUST AFT OF CENTER OF BEAM. REPAIRED AFT LOWER CARGO DOOR BEAM CORROSION IAW B767 SRM 51-70-12.

Part: LIGHT — SHORTED (COCKPIT) · airframe 70,300 hrs · 21,446 cycles

AFTER LANDING, WHEN TURNING OFF 22R ONTO A3 TAXIWAY, STA ILN, THE WHEEL WELL FIRE WARNING LIGHT CAME ON ALONG WITH MASTER WARNING LIGHT. EMERGENCY DECLARED. SHUT DOWN AIRCRAFT ON A3 AND EVACUATED AIRCRAFT. DEPLOYED SLIDE FOR EVACUATION. VERIFIED PROBLEM. FOUND RIGHT GEAR DOWNLOCK GREEN LIGHT ASSEMBLY SHORTED IN IT'S SOCKET, CAUSING A SHORT TO GROUND AND ILLUMINATING MASTER WARNING WHEEL WELL FIRE AND OTHER LIGHTS. REPLACED RIGHT GEAR DOWNLOCK LIGHT ASSEMBLY IAW B767 AMM CH 33. OPS CHECKED GOOD. REPLACED/INSTALLED SLIDE ASSEMBLY IAW B767 AMM 25-66-01. SLIDE REMOVED - P/N: 101623-303, S/N: PB0422.

Part: PUMP — BURNED (HYD SYSTEM) · airframe 69,661 hrs · 21,187 cycles

PERFORM FOLLOW-UP OF C1 ACMP LOW PRESSURE LIGHT ILLUMINATED. C1 PUMP BREAKER PULLED. INSPECTED AREA, FOUND CONNECTOR 0482 TO C1 ACMP BURNT AND WELDED TO SOCKET. REPLACED CONNECTOR IAW BOEING SB 777-29-0029 AND WDM 29-11-31. FOUND PINS ON C1 ACMP BURNT. REMOVED AND REPLACED HYDRAULIC PUMP IAW B767 AMM 29-11-02-4. LEAK AND OPS CHECKED GOOD AT THIS TIME.

Part: ROLLER — LACK OF LUBE (COCKPIT SEAT) · airframe 69,486 hrs · 21,122 cycles

FIRST OFFICER'S SEAT, VERTICAL ADJUSTMENTS, UNEXPECTANTLY DROP TO NEXT LOWER POSITION WHEN TO HIGH HIGHEST POSITION. LUBRICATED ROLLERS AND GEARS. OPS CHECKED GOOD IAW MM.

Part: CONTROL WHEEL — BINDING (COCKPIT) · airframe 69,486 hrs · 21,122 cycles

CAPTAIN AND FIRST OFFICER'S AILERON CONTROL WHEEL BINDS. LUBRICATED LOAD FEEL AND CENTERING MECHANISM. AILERONS OPS CHECKED GOOD IAW B767 AMM 27-11-00-5.

Part: BUSHING — CORRODED (RT MLG TRUNNION) · airframe 68,650 hrs · 20,803 cycles

LEFT AND RIGHT MAIN LANDING GEAR TRUNNION BUSHINGS CORRODED WITH AREAS OF DEEP PITTING. REMOVED AND REPLACED BUSHINGS IAW BOEING CMM 57-54-13.

Part: SLAT — MISSING (RT WING L/E) · airframe 68,093 hrs · 20,598 cycles

DURING INSPECTION OF AIRCRAFT AT ILN, FOUND RIGHT WING NR 12 LEADING EDGE SLAT OUTER SKIN MISSING. HONEYCOMB EXPOSED AT UPPER INBOARD SIDE, APPROXIMATELY 9.5 WIDE AND 11.0 LENGTH. REMOVED AND REPLACED NR 12 LEADING EDGE SLAT IAW B767 MM 27-81-02-4.

Part: WINDOW — DEFECTIVE (COCKPIT) · airframe 67,805 hrs · 20,474 cycles

L2 WINDOW WOULD NOT LOCK SHUT. REMOVED AND REPLACED L2 WINDOW IAW BOEING MM.

Part: DOOR — INOPERATIVE (COCKPIT) · airframe 63,397 hrs · 18,904 cycles

COCKPIT DOOR WOULD NOT OPEN, BINDED ON CEILING UNHINGED DOOR. REINSTALLED COCKPIT DOOR AND ADJUSTED TABS IAW B767 MM. COCKPIT DOOR OPS CHECKED GOOD.

Part: TERMINAL BLOCK — BURNED (NOSE E&E BAY) · airframe 63,165 hrs · 18,824 cycles

WHILE PERFORMING ROUTINE MAINTENANCE AT ILN, MAINTENANCE FOUND WIRING BURNED OFF STUDS 5 AND 6, STA. 172 IN NOSE. STUD 4 HAD DAMAGE ALSO. REMOVED AND REPLACED TERMINAL BLOCK 5020, REPAIRED WIRES IAW WDM 24-51-11, SHEET 2.

Part: WIRE — CHAFED (FUEL TANK PROBE) · airframe 60,042 hrs · 17,705 cycles

LEFT WING FUEL QUANTITY PROBE WIRING AT ACCESS PANEL 531BB WAS CHAFED DOWN TO BARE WIRE. MAINTENANCE INSPECTED AND REPLACED THE LEFT AUX FUEL QUANTITY WIRING HARNESS.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,042 hrs · 17,705 cycles

CORROSION WAS FOUND ON THE FWD PIT FRAME AT BS 764, LBL 8. MAINTENANCE INSPECTED AND REPAIRED THE FRAME IAW B767 SRM 53-00-07 AND 51-20-01.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,042 hrs · 17,705 cycles

CORROSION WAS FOUND ON STRINGER 39R AT THE AFT END BETWEEN BS 456 AND 478. MAINTENANCE INSPECTED AND REPLACED THE STRINGER IAW BOEING DRAWING 143T3220 AND B767 SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 60,042 hrs · 17,705 cycles

CORROSION WAS FOUND ON STRINGER 35L AT THE AFT BULK PIT BS 1461-1480 FRAME 636. MAINTENANCE INSPECTED AND REPLACED THE STRINGER IAW B767 SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,042 hrs · 17,705 cycles

STRINGER 19 WAS FOUND TO BE CRACKED AT STA 390L FRAME 481. MAINTENANCE INSPECTED AND REPLACED THE STRINGER IAW B767 SRM.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,042 hrs · 17,705 cycles

STRINGER 39R AT BS 1373 IN AFT LOWER CARGO AREA FRAME 400 WAS FOUND TO BE CORRODED. MAINTENANCE INSPECTED AND REPLACED THE STRINGER IAW B767 SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,042 hrs · 17,705 cycles

CORROSION WAS FOUND ON FLOORBEAM CAP AT STATION 303 RBL 63. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW BOEING DRAWING 141T5112 AND B767 SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,042 hrs · 17,705 cycles

CORROSION WAS FOUND ON TOP LEG OF FLOOR BEAM FRAME 207, STATION 1518 LBL 25. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW ABX REA B653-39290-MR.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,042 hrs · 17,705 cycles

STRINGER SPLICE FITTING 25R AT STATION 434 FRAME 111 WAS FOUND TO BE CORRODED. MAINTENANCE INSPECTED AND REPLACED THE FITTING IAW B767 SRM.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,042 hrs · 17,705 cycles

STRINGER SPLICE FITTING 31L STATION 434, FRAME 110 WAS FOUND TO BE CORRODED. MAINTENANCE INSPECTED AND REPLACED THE FITTING IAW BOEING DRAWING 140T115 AND B767 SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,042 hrs · 17,705 cycles

CORROSION WAS FOUND ON BEAM CAP AT STATION 287 BL 0- RBL 70. MAINTENANCE REPLACED THE CAP IAW B767 SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,042 hrs · 17,705 cycles

CORROSION WAS FOUND ON THE TOP OF FLOORBEAM CAP AT FRAME 087, STA 287, LBL 0 THROUGH LBL 20. MAINTENANCE INSPECTED AND REPLACED THE CAP IAW BOEING DRAWING 141T5111 AND B767 SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,042 hrs · 17,705 cycles

CORROSION WAS FOUND ON T-CAP AT STA 632, RBL 20. MAINTENANCE REPLACED THE T-CAP IAW B767 SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,042 hrs · 17,705 cycles

CORROSION WAS FOUND ON T-CAP AT STA 434 RBL 44. MAINTENANCE REPLACED THE T-CAP IAW B767 SRM.