N655GT

Part: FIRE DETECTOR — FAILED (RT ENGINE) · airframe 78,955 hrs · 26,234 cycles

RIGHT ENGINE FIRE LOOP 1 STATUS MESSAGE. REMOVED AND REPLACED NR 2 ENGINE UPPER AFT DETECTOR IAW B767 AMM 26-11-02. NO EICAS MESSAGE PRESENT. PERFORMED ENGINE FIRE DETECTION TEST, OPS CHECKED GOOD. THIS CLEARS MDDR 122671.</P>)

Part: INERTIA REEL — UNWANTED DEPLOY (MAIN DECK) · airframe 78,955 hrs · 26,234 cycles

MAIN DECK DESCENT DEVICE "C" DEPLOYED. REMOVED AND REPLACED DESCENT DEVICE IAW CMM 25-61-03. NO FURTHER DEFECTS NOTED.

Part: BULKHEAD — CRACKED (NR 1 PYLON) · airframe 77,589 hrs · 25,420 cycles

NR 1 PYLON BULKHEAD WEB DAMAGED INBD SIDE, AT THE HYD BULKHEAD FITTING FDR PANEL 431BT. FABRICATED A NEW WEB IAW BDEW 313T3104. REVAP LEAK CHECK OF HYDRAULIC LINES GOOD IAW AMM 29-11-00-796-053.

Part: STIFFENER — CRACKED (NLG WW BULKHEAD) · airframe 77,589 hrs · 25,420 cycles

FUSELAGE SECTION 41.5, BS 287, LBL 25, NOSE WHEEL WELL BUCKHEAD VERTICAL STIFFENER CRACKED DURING EA 6753A027. REPAIRED THE NOSE WHEEL WELL VERTICAL STIFFENER IAW SRM 51-71-12-06-0.

Part: SMOKE DETECTOR — DEFECTIVE (CARGO BAY) · airframe 77,589 hrs · 25,420 cycles

CARGO SMOKE DETECTION AIR SAMPLE TUBES FAILED LEAK CHECK, TROUBLESHOOTING REQUIRED. TROUBLESHOT CARGO SMOKE DETECTION AIR SAMPLE SYSTEM. FOUND LEAKS IN THE SYSTEM AND DAMAGED TUBES TIGHTENED THE SEAL ON THE HOSES AND REPLACED THE DAMAGED HOSES. IAW AMM TLS 0633TIC9-2-B(USE OF STANDARD INDUSTRY PRACTICES) AND SPECIAL FREIGHTER MMS 26-14-005. PERFORMED OPS CHECK. OPS CHECK GOOD.

Part: STRAP — NOT REPORTED (FUSELAGE) · airframe 77,589 hrs · 25,420 cycles

4H FAIL SAFE 12 STRAP FAILED OPEN OPEN HOCK INSPECTION. REPAIRED LT FAIL SAFE STRAP AT SSTA 955 IAW S/B 76753A0100 REV 3 & EA 6753A070 REVII.

Part: BULKHEAD — DAMAGED (NR 1 PYLON) · airframe 77,589 hrs · 25,420 cycles

NR 1 PYLON BULKHEAD WEB DAMAGED INBD SIDE AT HYD BULKHEAD FITTING FDR PANEL 431 BT. FORMED NEW WEB IAW BDEW 313T3104 REV AP LEAK CHECK OF HYDRAULIC LINES IAW AMM 29-11-00-796 -053.

Part: BRACKET — CRACKED (NR 2 PYLON) · airframe 77,589 hrs · 25,420 cycles

NR 2 PYLON FWD AREA PANEL 441BT, FWD ANGLE BRACKET OTBD LOWER WEB CORNER HAS A CRACK. REMOVED AND REPLACED THE PYLON FWD AREA BARRIER ASSY WITH WEB IAW SRM 51-40-02.

Part: BRACKET — BROKEN (LIGHT PANEL) · airframe 77,589 hrs · 25,420 cycles

L1 DOOR LIGHT PANEL INTERNAL LIGHT BRACKET BROKEN. REMOVED AND REPLACED L1 DOOR EXIT LIGHT PANEL IAW SFMMS 33-51-01-022-802 AND 33-51-01-402-803. OPS CHECKED MC28893 18MAY18 EXIT SIGN IAW SFMMS 33-51-01-712-013 OPS CHECK GOOD.

Part: STRAP — NOT REPORTED (FUSELAGE) · airframe 77,589 hrs · 25,420 cycles

RT FAIL SAFE STRAP FAILED OPEN HOCK INSPECTION. REPAIRED RT FAIL STRAP AT STA 955 IAW S/B 53A0100 REV 3 & EA6753A070 REVII.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 77,589 hrs · 25,420 cycles

EMERGENCY LIGHT IN THE GALLEY AREA WAS FOUND INOPERATIVE. THE EMERGENCY LIGHT FOUND TO HAVE A LOOSE CONNECTION ON THE LIGHT ASSY. TIGHTENED IAW AMM 33-22-01, OPS CHECKED GOOD IAW AMM 33-22-01.

Part: FIRE DETECTOR — MALFUNCTIONED (AFT CARGO) · airframe 77,589 hrs · 25,420 cycles

AFT CARGO FIRE DETECTION SYSTEM FAILED A SMOKE TEST. TROUBLESHOT, PERFORMED AN OP CHECK OF AFT LOWER CARGO COMPARTMENT SMOKE DETECTION SYSTEM, CHECKED GOOD IAW AMM 26-16-001735-399. PERFORMED LOWER COMPARTMENT SMOKE DETECTION SYSTEM BITE PROCEDURE,BIT PROCEDURE SYSTEM TEST GOOD IAW B767 FIM 26-16-FAULT TREE 806.

Part: BRACKET — CRACKED (NR 2 PYLON) · airframe 77,589 hrs · 25,420 cycles

NR 2 PYLON FWD AREA PANEL 441 BT FWD ANGLE BRACKET OB LOWER WEB CORNER HAS A CRACK. REMOVED AND REPLACED NR 2 PYLPON FWD AREA BARRIER ASSY WITH WEB IAW SRM 51-40-02.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 77,589 hrs · 25,420 cycles

EMERGENCY LIGHT IN GALLERY AREA INOPERATIVE. THE EMERGENCY LIGHT WAS FOUND TO HAVE A LOOSE CONNECTION. TIGHTENED IAW AMM 33-22-01. OPS CHECKED GOOD IAW AMM 33-22-01.

Part: HOSE — DAMAGED (CARGO) · airframe 77,589 hrs · 25,420 cycles

CARGO SMOKE DETECTION AIR SAMPLE TUBES FAILED A LEAK CHECK. TROUBLESHOT THE CARGO SMOKE DETECTING AIR SAMPLE SYSTEM AND FOUND LEAKS AND DAMAGED TUBES TIGHTENED THE HOSES AND REPLACED THE DAMAGED HOSES IAW AMM 0633T1C9-2-B AND MM 26-14-005. OPS CHECKED GOOD.

Part: FAILSAFE — DAMAGED (BS 955) · airframe 59,931 hrs · 42,599 cycles

RT SAFE STRAP AT BS 955 FAILED AN OPEN HOLE INSPECTION. REPAIRED THE FAILSAFE STRAP IAW 53A0100, REV 3, & EA 6753A070, REVII.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 77,589 hrs · 25,420 cycles

EMERGENCY LIGHT BY THE L1 DOOR WAS FOUND INOPERATIVE. EMERGENCY LIGHT OUTSIDE L1 DOOR WAS FOUND TO HAVE A BULB NOT INSTALLED PROPERLY. INSTALLED THE BULB CORRECTLY IAW AMM 33-51-06-902-082, OPS CHECK GOOD IAW 33-51-06 B62-083.

Part: BULKHEAD — CRACKED (NLG WW) · airframe 77,589 hrs · 25,420 cycles

FUSELAGE-SECTION 41 STATION 287 BL25 NOSE WHELL WELL LT BUCKHEAD VERTICAL CHORD HAS CRACK FOUND ON PART 1. STEP ON EA 6753A027. REPAIRED NOSE WHEEL WELL IAW SRM 51-71-12-06-0 OPS CHECK GOOD.

Part: BULB — UNSECURE (EMERGENCY LIGHT) · airframe 77,589 hrs · 25,420 cycles

EXTERIOR EMERGENCY LIGHT BY THE L1 DOOR WAS FOUND INOPERATIVE. THE EMERGENCY LIGHT WAS FOUND TO HAVE BULB NOT INSTALLED PROPERLY. INSTALLED THE BULB CORRECTLY IAW AMM 33-51-06-902-082, OPS CHECKED GOOD IAW 33-51-06 862-083.

Part: BRACKET — BROKEN (PANEL) · airframe 77,589 hrs · 25,420 cycles

L1 DOOR LIGHT PANEL INTERNAL LIGHT BRACKET BROKEN. REMOVED AND REPLACED L1 DOOR EXIT LIGHT PANEL IAW 33-57-01-022-802, AND 33-51-01-402-808. OPS CHECKED THE EXIT SIGN IAW MM 33-51-01-712-013, CHECKED GOOD.

Part: FAILSAFE — DAMAGED (BS 955) · airframe 77,589 hrs · 25,420 cycles

LEFT FAILSAFE STRAP AT BS 955 FAILED OPEN HOLE INSPECTION. REPAIRED THE FAILSAFE STRAP IAW 53A0100 REV3 & EA 6753A070, REV II.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 77,043 hrs · 25,059 cycles

EMERGENCY LIGHTS AT CREW SERVICE AREA 2 OUT OF 5 INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY M736 AND M735 IAW AMM 33-51-00. OPS CHECKED NORMAL.

Part: THRUST REVERSER — DAMAGED (NR 2 ENGINE) · airframe 75,972 hrs · 24,304 cycles

ON MAINTENANCE WALK AROUND FOUND NR 2 ENGINE THRUST REVERSER AT AROUND 2 O`CLOCK POSITION IS DAMAGED. INSPECTED AND REPAIRED IAW SRM 54-02-22-1.

Part: ESCAPE ROPE — UNSERVICEABLE (L1 DOOR) · airframe 75,912 hrs · 24,263 cycles

L1 DOOR ENTRY AREA DESCENT DEVICES D & E ARE UNRAVELED. R & R DESCENT DEVICES D & E FROM CONTAINER AT L1 DOOR IAW AMM 25-61-03-422-801 AND 25-61-03-422-802.

Part: CABLE — UNSERVICEABLE (CABIN) · airframe 75,082 hrs · 23,715 cycles

FOUR EACH MAIN DECK EMER DESCENT DEVICES FOUND TO BE UNSERVICEABLE CONDITION WITH CABLES EXTENDED. R & R 4 EA MAIN DECK EMER DESCENT DEVICES IAW AMM 25-61-03.

Part: FITTING — DAMAGED (TE FLAP) · airframe 75,082 hrs · 23,715 cycles

LEFT WING FLAP SUPPORT RIB INBD FITTING, OTBD HOLE HAS DAMAGE, NICK IN HOLE. REAMED OTBD HOLE TO .875. CONFIRMED DAMAGE REMOVAL BY NDT REAMED INBD HOLE TO .875 IAW MSG PMO-TLS-15-0013-02B OF SR 4-2892244521.

Part: SEAL DEPRESSOR — DAMAGED (FUSELAGE) · airframe 75,082 hrs · 23,715 cycles

MAIN DECK CARGO DOOR CUT OUT FWD UPPER SECTION OF SEAL DEPRESSOR IS DAMAGED. REPAIRED SEAL DEPRESSOR AS REQUIRED IAW SRM 53-00-15 REPAIR 1 & FORM 8110-.3 APPROVAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 75,082 hrs · 23,715 cycles

MULTIPLE DENTS AT RT FUSELAGE SKIN AFT OF AFT CARGO DOOR, STATION 1340 - 1355. REPAIRED AREA OF DENTS ON RT FUSELAGE AS REQUIRED IAW INSTRUCTIONS PROVIDED IN SR 4-2890259542.

Part: MECHANISM — OUT OF ADJUST (CARGO DOOR) · airframe 75,082 hrs · 23,715 cycles

RED INDICATION SHOW IN VIEW PORTS WHEN MAIN CARGO DOOR IS CLOSED & LOCKED. ADJUSTED PRESS DOOR MECHANISM, RELOCATED SWITCH S9028 & SUPPORT. ACCOMPLISHED OPERATIONS CHECKED GOOD IAW SF MM 52-32-00, 52-71-09, 52-32-22 & EO6752A023.

Part: SKIN — DENTED (FUSELAGE) · airframe 75,082 hrs · 23,715 cycles

DENT IN LT FUSELAGE SKIN 20" FWD OF OUT FLOW VLV STATION 1520 APPROX. REMOVED DAMAGE & ACCOMPLISHED REPAIR IAW SRM 53-00-01 FIG 201 REPAIR 14. SUPPLEMENTAL INSPECTION REQUIRED IAW TABLE V.

Part: SKIN — DENTED (TE FLAP) · airframe 74,255 hrs · 23,066 cycles

NUMEROUS SMALL DENTS ON RT INBD AFT FLAP UPPER SURFACE. REPAIRED IAW SRM 51-70-10, REPAIR 2 & EO1957A139 FOR PROXIMITY DEVIATIONS & TIME LIMITED REPAIR. PERMANENT REPAIR ON OR BEFORE NEXT C CHECK.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 74,255 hrs · 23,066 cycles

SMALL GOUGE NOTED FWD OF FWD CARGO DOOR CUTOUT AT STATION 539 & ABOVE STRINGER 32R. REWORKED DAMAGE, DVI, HFEC & OPEN HOLE ROTO PROBE INSPECTED DAMAGE & SURROUNDINGS AREA & RESTORED FINISH AS INSTRUCTED IN BOEING SR 3-2638596022-8100-9 RECIEVED FOR APPROVAL.

Part: SKIN — DENTED (TE FLAP) · airframe 74,255 hrs · 23,066 cycles

NUMEROUS SMALL DENTS ON LT INBD AFT FLAP UPPER SURFACE. REPAIRED IAW SRM 51-70-10, REPAIR 2 AN ATLAS AIR EO 1957A138 FOR PROXIMITY DEVIATIONS & TIME LIMITED REPAIR. PERMANENT REPAIR ON OR BEFORE NEXT "C" CHECK.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 74,228 hrs · 23,039 cycles

FLIGHT DECK FLASHLIGHT NOT CHARGING. R & R FLASH LIGHT IAW MM 25-63-00.

Part: WIRE — BURNED (ELECTRICAL BAY) · airframe 74,171 hrs · 22,977 cycles

ON ARRIVAL, OBSERVED ONE EXT/APU POWER BOTH AVAILABLE, EXT ON, 2 SIGNIFICANT WATER AT ENTRY WAY DUE TO OPEN 1L DOOR. ACFT SUBSEQUENTLY LOST POWER AND UNABLE TO RECONNECT ELECTRICAL POWER. MX OBSERVED APPROXIMATE .5" WATER IN ELECTRICAL EQUIPMENT BAY AND SMOKE FROM UNDERTERMINED SOURCE. REPAIRED BURNED AND BROKEN WIRES ON THE BACK OF THE MEC RACK IAW SWPM 20-30-12.

Part: FIRE WARNING — INTERMITTENT · airframe 73,575 hrs · 22,688 cycles

DURING CLIMB AND FIRST HOUR OF FLIGHT ALL MAIN DECK CARGO FIRE LIGHTS AND MASTER FIRE LIGHT ILLUMINATED INTERMITTENTLY WITH CHIME SOUNDING. CHECKED SYS IAW FIM 26-14-00 ALL SYSTEMS TESTED NORMAL INCLUDING LIGHTS AND ALARM, PRESSURIZED EJECTOR , NO LEAKS NOTED. ALL OTHER SYSTEMS AND LIGHTS CHECKED NORMAL. SYS OK FOR SERVICE.