N632GT

Part: UNKNOWN — MALFUNCTIONED (COCKPIT TEMP) · airframe 76,502 hrs · 9,432 cycles

COCKPIT TEMP CONTROL GOES FULL HOT & FULL COLD, AUTO REGULATION INOPERATIVE. PERFORMED TEMP CONTROL SYS ADJUSTMENT AND TEST, SYS FUNCTIONS NORMAL IAW AMM 21-61-00/501.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENGINE) · airframe 76,449 hrs · 9,416 cycles

RT ENGINE CONTROL EICAS MESSAGE. TROUBLESHOT IAW FIM 73-21 TR 878, RT PIMU HAD EEC / PIMU MODE DISAGREE, CLEARED THE MESSAGE & RAN BOTH ENGINES IAW FIM. MESSAGE CLEARED. OPS CHECKED GOOD.

Part: VALVE — MALFUNCTIONED (LT A/C PACK) · airframe 76,428 hrs · 9,410 cycles

LT PACK BITE MESSAGE FAULT LT LOW LIMIT VALVE. REMOVED AND REPLACED LT PACK LOW LIMIT VALVE PER AMM 21-51-11 OPS CHECKED OK.

Part: CONTROLLER — MALFUNCTIONED (RT ENGINE) · airframe 76,263 hrs · 9,361 cycles

DURING DESCENT, AN EICAS MESSAGE FOR THE RT ENGINE HPSOV REPLACED HPC CONTROLLER IAW AMM 36-11-08, OPS OK,

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI ICE SYS) · airframe 76,260 hrs · 9,360 cycles

DURING DESCENT, ENGINE ANTI-ICE EICAS RT HPSOV WENT AWAY AFTER A COUPLE OF MINUTES STATUS MSG R ENG HPSOV CLEARED MESSAGE PERFORMED BITE TEST NO FAULTS NOTED , GROUND TEST OK IAW AMM 36-11-00.

Part: VALVE — INOPERATIVE (NR 1) · airframe 76,229 hrs · 9,354 cycles

ENGINE NR 1 PRV INOPERATIVE. NR 1 PRV REPLACED IAW MM 36-11-18/401.

Part: FITTING — DAMAGED (MLG) · airframe 76,229 hrs · 9,354 cycles

COCKPIT FLOOR LANDING GEAR ALTERNATE EXTEND QUADRANT FITTING DAMAGED. THE FITTING WAS REPLACED IAW AMM 32-35-13-404-015.

Part: HINGE — WORN (NACELLE) · airframe 76,229 hrs · 9,354 cycles

NR 1 ENGINE FAN HOLD OPEN ROD PIVOT HINGE HAS EXCESSIVE PLAY. REPLACED IAW AMM 71-11-04..

Part: TUBE — CRACKED (LT A/C PACK) · airframe 76,229 hrs · 9,354 cycles

ACFT LEFT COOLING PACK TUBING IS CRACKED. COOLING TUBING REPLACED IAW AMM 21-51-52.

Part: SHAFT — TORN (THRUST REVERSER) · airframe 76,229 hrs · 9,354 cycles

NR 1 ENGINE THRUST REVERSER COWL FOUND FLEX SHAFT BETWEEN CDU AND LOWER GEARBOX TORN. SERVICEABLE FLEX SHAFT INSTALLED IAW AMM 78-31-18.

Part: CONTROLLER — DAMAGED (NR 1) · airframe 76,229 hrs · 9,354 cycles

NR 1 ENGINE PRV CONTROLLER DAMAGED. THE NR 1 PRV CONTROLLER REPLACED IAW MM 36-11-19/401.

Part: TANK — ABNORMAL (FUEL SYSTEM) · airframe 76,229 hrs · 9,354 cycles

HIGH RESISTANCE BETWEEN LT MAIN TANK OVER-WING FILL PORT TO STRUCTURE. LT OVER-WING FILL PORT REMOVED & ALL MATING SURFACES CLEANED. FILL PORT REINSTALLED IAW AMM 28-11-04-404-019 REV 119. ELECTRICAL BONDING RESISTANCE MEASURED FOUND WITHIN LIMITS.

Part: JUMPER — TORN (OUTFLOW VALVE) · airframe 76,229 hrs · 9,354 cycles

CABIN OUT FLOW VALVE JUMPER TORN. THE JUMPER WAS REPLACED IAW AMM 21-32-01.

Part: IDG — INOPERATIVE (NR 1 GENERATOR) · airframe 76,229 hrs · 9,354 cycles

NR 1 ENGINE LEFT GENERATOR INOPERATIVE. NR 1 ENGINE IDG REPLACED IAW MM 24-11-01/401.

Part: CABLE — TWISTED (THRUST REVERSER) · airframe 76,229 hrs · 9,354 cycles

DURING REVIEWING INSPECTION, FOUND LT ENGINE INBD THRUST REVERSER CABLE SHAFT TO LOWER ANGLE GEAR BOX TWISTED.

Part: SKIN — CHAFED (NR 1 PYLON) · airframe 76,229 hrs · 9,354 cycles

NR 1 PYLON INBD UPPER RUB STRIP SKIN CHAFED RT SIDE. REPLACED IAW SRM 51-40-02

Part: VALVE — ABNORMAL (FUEL SHUTOFF) · airframe 76,229 hrs · 9,354 cycles

HIGH RESISTANCE FROM APU FUEL SHUTOFF TO STRUCTURE. CLEANED THE MATING SURFACE IAW AMM 28-25-02.

Part: TUBE — DAMAGED (FUEL HEATER) · airframe 76,229 hrs · 9,354 cycles

NR 2 ENGINE FUEL HEATER TUBE DAMAGED. REPLACED THE TUBE IAW MM 79-21-01.

Part: HOSE — DAMAGED (NR 2 PYLON) · airframe 76,229 hrs · 9,354 cycles

NR 2 PYLON ANTI-ICE HOSE AND UNION DAMAGED. HOSE ASSY REPLACED IAW AMM 30-11-02/401.

Part: LINE — DAMAGED (FUEL SYSTEM) · airframe 76,229 hrs · 9,354 cycles

FUEL LINE DAMAGED. REPLACED THE FUEL LINE IAW MM 28-25-22/201.

Part: SKIN — CHAFED (NR 2 PYLON) · airframe 76,229 hrs · 9,354 cycles

NR 2 PYLON SKIN CHAFING LT SIDE. SKIN REPLACED IAW SRM 51-40-02.

Part: TUBE — DENTED (EXTINGUISHER) · airframe 76,229 hrs · 9,354,262 cycles

AFT CARGO BAY FIRE EXTINGUISHER SYSTEM TUBE IS DENTED. REPLACED IAW AMM 26-23-11.

Part: BOLT — WORN (NR 1 ENGINE) · airframe 76,229 hrs · 9,354 cycles

NR 1 ENGINE 6 SLING MOUNTING BOLTS ARE WORN. REPLACED IAW AMM 71-11-04.

Part: CAP — CORRODED (RESERVOIR) · airframe 76,229 hrs · 9,354 cycles

RIGHT PYLON HYD RESERVOIR CAP CORRODED. REPLACED THE CAP IAW MM 20-30-83.

Part: TANK — ABNORMAL (FUEL SYS) · airframe 76,229 hrs · 9,354 cycles

HIGH RESISTANCE BETWEEN RT MAIN TANK OVER-WING FILL PORT TO STRUCTURE. RT OVER-WING FILL PORT REMOVED AND ALL MATING SURFACES CLEANED. FILL PORT REINSTALLED IAW AMM 28-11-04-404-019 REV 119. ELECTRICAL BONDING RESISTANCE MEASURED FOUND WITHIN LIMITS..

Part: FITTING — DAMAGED (RT WING TE FLAP) · airframe 76,229 hrs · 9,354 cycles

RIGHT WING INBD FLAP FOUND DAMAGED ON CONNECTION FITTING BETWEEN AFT FLAP AND MID FLAP. REPLACED NEW CONNECTION FITTING BETWEEN AFT FLAP AND MID FLAP IAW 27-51-06- PB 401 REV. 119 2.

Part: VALVE — ABNORMAL (LT WING) · airframe 76,229 hrs · 9,354 cycles

LEFT WING T/E THE 3 FUELING SHUTOFF VALVES FOUND WITH HIGH BONDING RESISTANCE. CLEANED MATING SURFACE IAW AMM 28-21-02.

Part: SLEEVE — DENTED (EXHAUST) · airframe 79,229 hrs · 9,354 cycles

NR 2 ENGINE EXHAUST SLEEVE DENT. REPLACED THE SLEEVE IAW MM 78-11-01.

Part: SLEEVE — CORRODED (LT BOOST PUMP) · airframe 76,229 hrs · 9,354 cycles

LEFT FWD BOOST PUMP SHUTOFF SLEEVE FOUND WITH A HOLE ON SLEEVE STRUT OUTSIDE OF THE LIMITS DUE TO EROSION. THE SLEEVE REPLACED IAW MM 28-22-03.