N901RA

Part: WIRE — DISCONNECTED (CABIN)

SNA-CCI - AFT EMERGENCY LIGHT ASSY INOPERATIVE. FOUND WIRES DISCONNECTED TO EMERGENCY LIGHT ASSY, REATTACHED WIRES. OPS CHECK GOOD. (M)

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

SFO - DURING TAKEOFF AT 60 KNOTS, TAILCONE LIGHT ILLUMINATED AND CAPTAIN ABORTED TAKEOFF. RESET TAILCONE LOCK SWITCH PIN AND LANYARD AND CLEARED UNSAFE ANNUNCIATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SNA - MAIN ENTRANCE EMERGENCY EXIT SIGN LIGHT OUT, BATTERY CHARGER INOPERATIVE. REPLACED BATTERY PACK POWR SUPPLY. OPS CHECK NORMAL. (M)

Part: CHARGER — FAILED (CABIN)

SNA - 1ST CLASS FLOOR E-LIGHTS INOPERATIVE. REMOVED AND REPLACED E-PACK CHARGING UNIT. OPS CHECK GOOD. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE IN FIRST CLASS. REPLACED B5-240 POWER SUPPLY, CHECK GOOD. (M)

Part: WIRE — PINCHED (CABIN)

OKC - EMERGENCY FLOOR TRACK LIGHTING FAILED STEP H 1. REPAIRED PINCHED WIRE IN FLOOR TRACK SYSTEM. OPS CHECK NORMAL IAW MD-90 MM 20-10-03. OPS CHECK GOOD IAW C-CHECK CARD 1C-114 STEP H. 1. (M)

Part: WIRE — BROKEN (ROW 1)

OKC - EMERGENCY FLOOR TRACK LIGHTING FAILED STEP B.1 WIRES BROKEN AT LIGHT ASSY ROW 1 FORWARD LIGHT. REPLACED BULB AND REPAIRED BROKEN WIRES IAW MD-90 MM 20-50-01. OPS CHECK GOOD IAW C-CHECK CARD NR 1C-114 STEP B.1. (M)

Part: WIRE — BROKEN (ROW 31)

RNO - EMERGENCY PATH LIGHT AT ROW 33 IS INOPERATIVE. REPLACED BROKEN WIRE ON ROW 31 EMERGENCY EXIT LIGHT SYSTEM, OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (BS 402)

SJC - FOUND EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IW 33-5117. OPS CHECK GOOD. (M)

Part: VALVE — FAILED (LT ENGINE)

SJC - ABORTED TAKEOFF, ON TAKEOFF ROLL, LEFT PNEUMATIC SYSTEM FAULT ON EOAP THROUGH 80 KNOTS. REMOVED AND REPLACED LEFT PRESSURE REGULATING PILOT SHUTOFF VALVE IAW MM 36-12-03. OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (ROW 5)

IN SJC, EMERGENCY FLOOR LIGHTS INOPERATIVE FOR ROWS 6-20. REMOVED AND REPLACED BATTERY PACK AT ROW 5, OPS CHECK GOOD. (M)

Part: CONTROLLER — MALFUNCTIONED (PNEUMATIC SYSTEM)

IN RNO - AFTER TAKEOFF, ROLL 6 FT PNEU SYSTEM FAULT REJECTED TAKEOFF RETURN TO GATE. RAN BIT TEST ON PNEU SYSTEM CONTROLLER, NO FAULTS NOTED SYSTEM FAULT CLEARED MESSAGE CLEARED. (M)

Part: CONTROL UNIT — FAILED (MLG)

AT RENO, ANTI-SKID FAULT. REMOVED AND REPLACED BRAKE CONTROL UNIT IAW MM 32-00. MAINTENANCE TAXI TEST FOUND NO FAULTS OR DISCREPANCIES. SYSTEM OPS CHECK NORMAL AND OK FOR SERICE. REF ORJA98215. (M)

Part: BRACKET — DAMAGED (NR 1 ENGINE)

SJC - MAINTENANCE DISCOVERED ON NR 1 ENGINE, THE UPPER AND LOWER C-DUCTS DELAMINATED AND DISBONDED BEYOND LIMITS. AIRCRAFT FERRIED TO RENO FOR REPAIR. MAINT DISCOVERED THE FOLLOWING FUEL NOZZLE BRACKETS LOOSE DUE TO ELONGATION OF THE BOLT HOLES IN THE BRACKET CAUSING HOT AIR LEAKAGE AT NR 18, NR 17 FUEL NOZZLE BRACKETS. MAINT REPLACED THE UPPER C-DUCT AND PERFORMED AN INTERIM REPAIR IN THE LOWER C-DUCT IAW ROHR NR 98VN515. A PERMANENT REPAIR WILL BE PERFORMED AT C-CHECK (7-98). AIRCRAFT WAS RETURNED TO SERVICE. NOTE: FUEL NOZZLES HAVE NEVER BEEN REPLACED. (X)

Part: BRACKET — DAMAGED (NR 2 ENGINE)

SJC - MX DISCOVERED NR 2 ENG AFT COWL LATCH DOOR HAS EVIDENCE OF HEAT DAMAGE. NR 2 ENG UPPER AND LOWER C-DUCTS HAVE DELAMINATION AND ARE DISBONDED BEYOND LIMITS. AIRCRAFT WAS FERRIED TO RENO FOR REPAIR. UPON FURTHER INVESTIGATION, MAINTENANCE DISCOVERED THAT THE FOLLOWING FUEL NOZZLE BRACKETS SHOW EVIDENCE OF HOT AIR LEAKAGE DUE TO ELONGATION OF THE BOLT HOLES IN THE BRACKET ASSY (BRACKET POSITIONS 14, 16 AND 19). MX PERFORMED AN INTERIM REPAIR TO THE UPPER AND LOWER C-DUCTS AND THE AFT COWL LATCH DOOR IN ACC W/ROHR ENG, DOCUMENT NR 98VN515. THIS REPAIR WILL BE PERMANENT AT C-CHECK (JULY 98). MAINTENANCE REMOVE AND REPLACED DEFECTIVE FUEL NOZZLE BRACKETS. FUEL NOZZLES HAVE NEVER BEEN REPLACED. (M)

Part: BRACKET — DAMAGED (NR 2 ENGINE)

SJC - MX DISCOVERED NR 2 ENG AFT COWL LATCH DOOR HAS EVIDENCE OF HEAT DAMAGE. NR 2 ENG UPPER AND LOWER C-DUCTS HAVE DELAMINATION AND ARE DISBONDED BEYOND LIMITS. A/C WAS FERRIED TO RENO FOR REPAIR. UPON FURTHER INVESTIGATION, MX DISCOVERED THE FOLLOWING FUEL NOZZLE BRACKETS SHOW EVIDENCE OF HOT AIR LEAKAGE DUE TO ELONGATION OF THE BOLT HOLES IN THE BRACKET ASSEMBLY (BRACKET POSITIONS 14, 16 AND 19). MX PERFORMED AN INTERIM REPAIR TO THE UPPER AND LOWER C-DUCTS AND THE AFT COWL LATCH DOOR IN ACC WITH ROHR ENG DOCUMENT NR 98VN515. THIS REPAIR WILL BE PERMANENT AT C-CHECK. MX REMOVED AND REPLACED DEFECTIVE FUEL NOZZLE BRACKETS. FUEL NOZZLES HAVE NEVER BEEN REPLACED. (M)

Part: BRACKET — DAMAGED (NR 2 ENGINE)

SJC - MAINTENANCE DISCOVERED NR 2 ENGINE AFT COWL LATCH DOOR HAS EVIDENCE OF HEAT DAMAGE. NR 2 ENGINE UPPER AND LOWER C-DUCTS HAVE DELAMINATION AND ARE DISBONDED BEYOND LIMITS. AIRCRAFT 901RA WAS FERRIED TO RENO FOR REPAIR. UPON FURTHER INVESTIGATION, MAINTENANCE DISCOVERED THAT THE FOLLOWING FUEL NOZZLE BRACKETS SHOW EVIDENCE OF HOT AIR LEAKAGE DUE TO ELONGATION OF THE BOLT HOLES IN THE BRACKET ASSEMBLY (BRACKET POSITIONS 14, 16 AND 19) MAINTENANCE. PERFORMED AN INTERMIM REPAIR TO THE UPPER AND LOWER C-DUCTS AND THE AFT COWL LATCH DOOR IN ACC WITH ROHR ENG DOCUMENT NR 98VN515. THIS REPAIR WILL BE PERMANENT AT C-CHECK (JULY 98). MAINTENANCE REMOVED AND REPLACED DEFECTIVE FUEL NOZZLE BRACKETS. FUEL NOZZLE

Part: GASKET — DAMAGED (NR 1 ENGINE)

SJC - MAINTENANCE DISCOVERED ON THE NR 1 ENGINE, THE UPPER AND LOWER C-DUCTS WERE DELAMINATED AND DISBONDED BEYOND LIMITS. AIRCRAFT FERRIED TO RENO FOR REPAIRS. MAINT DISCOVERED THAT 2 EACH GASKETS (FUEL NOZZLE BRACKET GASKET) WERE DEFECTIVE AT THE NR 17 AND NR 18 POSITIONS. MAINT REPLACED THE UPPER C-DUCT AND REPAIRED THE LOWER C-DUCT IAW ROHR ENGINE DOCUMENT 98VN515. THIS IS AN INTERIM REPAIR WHICH WILL BE PERMANENTLY REPAIRED AT C-CHECK (7-98). MAINT REPLACED THE 2 EACH DEFECTIVE GASKETS. AIRCRAFT RETURNED TO SERVICE. NOTE: FUEL NOZZLES HAVE NEVER BEEN REPLACED. (X)

Part: BRACKET — DAMAGED (NR 1 ENGINE)

SJC - MAINTENANCE DISCOVERED ON NR 1 ENGINE, THE UPPER AND LOWER C-DUCTS DELAMINATED AND DISBONDED BEYOND LIMITS. AIRCRAFT FERRIED TO RENO FOR REPAIR. MAINT DISCOVERED THE FOLLOWING FUEL NOZZLE BRACKETS LOOSE DUE TO ELONGATION OF THE BOLT HOLES IN THE BRACKET CAUSING HOT AIR LEAKAGE AT NR 18, NR 17 FUEL NOZZLE BRACKETS. MAINT REPLACED THE DEFECTIVE FUEL NOZZLE BRACKETS. MAINT REPLACED THE UPPER C-DUCT AND PERFORMED AN INTERIM REPAIR ON THE LOWER C-DUCT IAW ROHR NR 98VN515. A PERMANENT REPAIR WILL BE PERFORMED AT C-CHECK (7-98). AIRCRAFT RETURNED TO SERVICE. NOTE: FUEL NOZZLES HAVE NEVER BEEN REPLACED. (X)

Part: BRACKET — DAMAGED (NR 2 ENGINE)

SJC MAINTENANCE DISCOVERED NR 2 ENGINE AFT COWL LATCH DOOR HAS EVIDENCE OF HEAT DAMAGE. NR 2 ENGINE UPPER AND LOWER C-DUCTS HAVE DELAMINATION AND ARE DISBONDED BEYOND LIMITS. AIRCRAFT FERRIED TO RENO FOR REPAIR. MAINT DISCOVERED THE FOLLOWING FUEL NOZZLE BRACKETS SHOW EVIDENCE OF HOT AIR LEAKAGE DUE TO ELONGATION OF THE BOLT HOLES IN THE BRACKET ASSY (BRACKET POSITIONS 14, 16, AND 19). MAINT PERFORMED AN INTERIM REPAIR TO THE UPPER AND LOWER C-DUCTS AND THE AFT COWL LATCH DOOR IAW W/ROHR ENG DOCUMENT NR 98VN515. THIS REPAIR WILL BE PERMANENT AT C-CHECK (7-98). MAINT REMOVED AND REPLACED DEFECTIVE FUEL NOZZLE BRACKETS. NOTE: FUEL NOZZLES HAVE NEVER BEEN REPLACED. (X)

Part: BRACKET — DAMAGED (NR 2 ENGINE)

SJC - MAINTENANCE DISCOVERED NR 2 ENGINE AFT COWL LATCH DOOR HAS EVIDENCE OF HEAT DAMAGE. NR 2 ENG UPPER AND LOWER C-DUCTS HAVE DELAMINATION AND ARE DISBONDED BEYOND LIMITS. ACFT FERRIED TO RENO FOR REPAIR. UPON FURTHER INVESTIGATION, MAINT DISCOVERED THE FOLLOWING FUEL NOZZLE BRACKETS SHOW EVIDENCE OF HOT AIR LEAKAGE DUE TO ELONGATION OF THE BOLT HOLES IN THE BRACKET ASSY (BRACKETS 14, 16, AND 19). MAINT PERFORMED INTERIM REPAIR TO UPPER AND LOWER C-DUCTS AND AFT COWL LATCH DOOR IAW ROHR ENG DOC NR 98VN515. THIS REPAIR WILL BE PERMANENT AT C-CHECK (7-98). MAINT REMOVED AND REPLACED DEFECTIVE FUEL NOZZLE BRACKETS. NOTE: NOZZLES HAVE NEVER BEEN REPLACED. (X)

Part: BRACKET — DAMAGED (NR 1 ENGINE)

SJC - MAINTENANCE DISCOVERED ON NR 1 ENGINE, THE UPPER AND LOWER C-DUCTS DELAMINATED AND DISBONDED BEYOND LIMITS. AIRCRAFT FERRIED TO RENO FOR REPAIR. UPON FURTHER INVESTIGATION, MAINT DISCOVERED THE FOLLOWING FUEL NOZZLE BRACKETS LOOSE DUE TO ELONGATION OF THE BOLT HOLES IN THE BRACKET CAUSING HOT AIR LEAKAGE AT NR 18, NR 17 FUEL NOZZLE BRACKETS. MAINT REPLACED THE DEFECTIVE FUEL NOZZLE BRACKETS. MAINT REPLACED THE UPPER C-DUCT AND PERFORMED AN INTERIM REPAIR ON THE LOWER C-DUCT IAW ROHR NR 98VN515. A PERMANENT REPAIR WILL BE PERFORMED AT C-CHECK (7-98). AIRCRAFT WAS RETURNED TO SERVICE. NOTE: FUEL NOZZLES HAVE NEVER BEEN REPLACED. (X)

Part: BRACKET — DAMAGED (NR 1 ENGINE)

SJC - MAINTENANCE DISCOVERED ON NR 1 ENGINE, THE UPPER AND LOWER C-DUCTS DELAMINATED AND DISBONDED BEYOND LIMITS. AIRCRAFT FERRIED TO RENO FOR REPAIR. MAINTENANCE DISCOVERED THE FOLLOWING FUEL NOZZLE BRACKETS LOOSE DUE TO ELONGATION OF THE BOLT HOLES IN THE BRACKET CAUSING HOT AIR LEAKAGE AT NR 18, NR 17 FUEL NOZZLE BRACKETS. MAINT REPLACED THE UPPER C-DUCT AND PERFORMED AN INTERIM REPAIR ON THE LOWER C-DUCT IAW ROHR NR 98VN515. A PERMANENT REPAIR WILL BE PERFORMED AT C-CHECK (7-98). AIRCRAFT WAS RETURNED TO SERVICE. NOTE: FUEL NOZZLES HAVE NEVER BEEN REPLACED. (X)

Part: BRACKET — DAMAGED (NR 1 ENGINE)

SJC - MAINTENANCE DISCOVERED ON NR 1 ENGINE, THE UPPER AND LOWER C-DUCTS DELAMINATED AND DISBONDED BEYOND LIMITS. AIRCRAFT FERRIED TO RENO FOR REPAIR. MAINT DISCOVERED THE FOLLOWING FUEL NOZZLE BRACKETS LOOSE DUE TO ELONGATION OF THE BOLT HOLES IN THE BRACKET CAUSING DEFECTIVE FUEL NOZZLE BRACKETS. MAINTENANCE REPLACED THE UPPER C-DUCT AND PERFORMED AN INTERIM REPAIR ON THE LOWER C-DUCT IAW ROHR NR 98VN515. A PERMANENT REPAIR WILL BE PERFORMED AT C-CHECK (7-98). AIRCRAFT RETURNED TO SERVICE. NOTE: FUEL NOZZLES HAVE NEVER BEEN REPLACED. (X)

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY FLOOR TRACK LIGHT AT ROW 2 IS INOPERABLE. REMOVED AND REPLACED 2 EMERGENCY PATH LIGHT ASSEMBLIES. OPS CHECK GOOD. (X)

Part: WIRE — FAILED (CABIN)

EMERGENCY FLOOR TRACK LIGHTING ONE LAMP INOP AT ROW 8. FOUND BROKEN WIRE. RECONNECTED, OPS CHECK GOOD. (M)

Part: LAMP — INOPERATIVE (CABIN)

FLOOR EMERGENCY LIGHT AT ROW 30 FAIL TO ILLUMINATE. INSTALLED LAMP HOLDER ASSY AT ROW 30 EMERGENCY LIGHT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

OVERWING EMERGENCY LIGHT WILL NOT COME ON. REMOVED AND REPLACED OVERWING EMERGENCY LGHT BATTERY. OPS CHECK GOOD. (M)

Part: LOCK CABLE — DISCONNECTED (TAIL CONE)

TAIL CONE UNSAFE LIGHT ON. RE-CONNECTED LOCK CABLE TO TURN OFF UNSAFE LIGHT. (X)

Part: CONNECTOR — LOOSE (NLG)

AFTER TAKEOFF AND GEAR RETRACTION, RED 'NOSE GEAR UNSAFE LIGHT' ILLUMINATED. COCKPIT NOISE LEVEL INORDINATELY HIGH. FOUND CANNON PLUG LOOSE ON UPLOCK TARGET. SECURED CANNON PLUG AND SWUNG NOSE GEAR PER MD90 MM 32-20-00. OPS CHECK NORMAL. (X)

Part: CABLE — DISCONNECTED (TAIL CONE)

TAIL CONE UNSAFE LIGHT. PERFORMED CHECK OF TAIL CONE JETISON SYSTEM. FOUND EXT HANDLE CABLE BALL END OUT OF RECEPTICLE. RE-ATTACHED CABLE EXTINGUISHING UNSAFE LIGHT PER MM 53-53-00. (X)

Part: SENSOR LINKAGE — DISCONNECTED (RT MLG)

SJC - AFTER GEAR EXTENSION, RIGHT MAIN AND RED UNSAFE LIGHT. CYCLED GEAR AND ON SECOND EXTENSION, SAME INDICATION. PULLED RED MANUAL EXTENSION HANDLE AND GOT THREE GREEN INDICATIONS. LANDED STRAIGHT AHEAD WITH GEAR DOORS FLYING. FOUND UPLOCK PROXIMITY-SENSOR LINKAGE DISCONNECTED. RECONNECTED LINKAGE. OPS CHECK GOOD. PERFORMED A FUNCTIONAL TEST OF THE LANDING GEAR POSITION INDICATING AND WARNING SYSTEMS PER MM 32-60-00. (X)

Part: WIRE — BROKEN (LT ENGINE)

LEFT ENGINE B-LOOP WILL NOT TEST. REPAIRED BROKEN GROUND WIRE ON LEFT ENGINE. (X)

Part: CONNECTOR — DIRTY (APU)

APU B-LOOP WILL NOT TEST. CLEANED CANNON PLUG ON FIRE LOOP AMP. (X)