N205AA

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, FOUND CEILING EMERGENCY LIGHTS AT ROWS 21D INOPERATIVE. REPLACED BATTERY/CHARGER ASSEMBLY FOR CEILING EMERGENCY LIGHTS AT ROW 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OVERWING SIGN AT ROW 21 INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND SKIN CRACKED AT STATION 1380 ABOVE LONGERON 14L AT SHEAR TIE FASTENERS. INSTALLED DOUBLER, PER SRM 53-01-00, PAGE 1 AARD 53-30-00-02 PAGE 1. (M)

Part: SKIN — CRACKED (VERTICAL STAB)

TUL - FOUND VERTICAL STAB SKIN CRACKED RIGHT UPPER CORNER OF AIR INLET, FS 1388. INSTALLED DOUBLER REPAIR PER SRM 55-01-00 FIG 2 SHEET 2. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND SKIN STATION 1380 ABOUT L14R HAS CRACK. INSTALLED DOUBLER PRE SRM 53-01 FIG 2 AND AARD 53-30-00-02. (M)

Part: ACM — MALFUNCTIONED (A/C BAY)

RDU - FLT 735 - EN ROUTE RDU-ORD, CLIMBING THROUGH 27,000 FEET TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. LIGHT EXTINGUISHED AFTER ACCOMPLISHING CHECKLIST AFTER APPROXIMATELY 1 MINUTE LIGHT ILLUMINATED AGAIN. RETURNED RDU AND LANDED WITHOUT INCIDENT. REPLACED RIGHT ACM AND AUGMENTATION VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 89 BROKEN. REPLACED EMERGENCY EXIT LIGHT AT SEAT 8D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PUMP — MALFUNCTIONED (AFT FUEL TANK)

DFW - FLT 1725 - EN ROUTE AUS-LAX, SHORTLY AFTER TAKEOFF DETECTED ALL THREE CENTER TANK FUEL BOOST PUMP CIRCUIT BREAKERS POPPED AND WOULD NOT RESET. AIR INTERRUPTED, DIVERTED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED AFT CENTER FUEL BOOST PUMP. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BUNGEE CYLINDER — DEFECTIVE (NLG)

SJC - FLT 2468 - AFTER TAKEOFF, NOSE GEAR FAILED TO RETRACT. RETURNED AND LANDED SJC WITHOUT INCIDENT. REPEAT ON T2721 AND T9670/26 AUGUST. REPLACED BUNGEE CYLINDER SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD OVERWING EXIT EMERGENCY EXIT FLOOR PATH LIGHT EXIT MARKER INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

DTW - FLT 1363 - ON TAKEOFF, AFTER GEAR HANDLE RAISED RED NOSE GEAR LIGHT ILLUMINATED. EXTENDED GEAR WITH NORMAL INDICATIONS. RETURNED AND LANDED DTW WITHOUT INCIDENT. ACCOMPLISHED INSPECTION AND GEAR SWING. UNABLE TO DUPLICATE. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: OUTFLOW VALVE — MALFUNCTIONED (FUSELAGE)

DFW - FLT 1618 - AFTER TAKEOFF FLOW LIGHT AND CABIN DESCENT OF 300 FEET PER MINUTE DURING CLIMB AT 31,000 FEET POP AND NOISE UNDER FIRST CLASS CABIN REPORTED BY FLIGHT ATTENDANT. RETURNED AND LANDED DFW WITHOUT FURTHER INCIDENT. DURING DESCENT FLOW LIGHT EXTINGUISHED. REPLACED OUTFLOW VALVE ACTUATOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CONTROLLER — MALFUNCTIONED (ACM BAY)

DFW- FLT 1969 - ON TAKEOFF CABIN RATE OF CLIMB SHOWED DESCENT OF 600 FEET PER MINUTE FOR APPROXIMATELY TWO MINUTES, TRANSFER LOCKOUT ILLUMINATED. PUSHED RESET LOCKOUT AND LIGHT REMAINED ON. RETURNED AND LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED STANDBY PRESSURE CONTROLLER AND PRESSURE TRANSFER RELAY R2-258. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS FROM FORWARD BULKHEAD TO FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTS FROM FORWARD BULKHEAD TO FORWARD GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: SENSOR — NEEDED ADJUSTING (LT MLG DOOR)

DFW - FLT 1122 - DURING CLIMB-OUT, GDL-DFW, MAIN LANDING GEAR DOOR OPEN LIGHT ILLUMINATED AND THEN WENT OUT. CONTINUED TO DFW AND LANDED WITHOUT INCIDENT. ADJUSTED LEFT MAIN LANDING GEAR DOOR UPLOCK TARGET. CYCLED LANDING GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LINE — LEAKING (MLG)

DFW - FLT 2066 - ON APPROACH TO DFW, RIGHT HYDRAULIC QTY SHOWED 1 QT AND PRESSURE VARIED BETWEEN 1,000-1,500 PSI. RAN QRH PROCEDURES FOR LOSS OF RIGHT HYDRAULIC FLUID AND EXTENDED THE GEAR USING ALTERNATE PROCEDURE. LANDED DFW WITHOUT INCIDENT. REPLACED HYDRAULIC LINE TO RUDDER CONTROL, BOTH MLG DOORS, AND WATER SEPARATOR BAGS. ACCOMPLISHED PACK BURNOUT AND GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR LIGHTS INOPERATIVE AT FORWARD GALLEY. REPLACED EMERGENCY EXIT FLOOR LIGHT STRIP AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SERVICE DOOR INOPERATIVE. REPAIRED WIRE AT CONNECTOR FOR CHARGER/BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: COFFEE MAKER — DEFECTIVE (GALLEY)

DFW-SJC - FLT 1967 - DURING CRUISE, FLT ATTENDANTS REPORTED A STRONG ELECTRICAL BURNING SMELL IN THE AFT GALLEY. THE SMELL WENT AWAY WHEN GALLEY POWER WAS TURNED OFF. LANDED SJC WITHOUT INCIDENT. REPLACED NR 4 COFFEE MAKER, ACCOMPLISHED SNIFF CHECK. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M)

Part: CONTROLLER — DEFECTIVE (AFT FUSELAGE)

DFW - FLT 1617 - DURING CRUISE LGA/DFW FL 280, FLOW LIGHT ILLUMINATED WITH ANTI-ICE ON. CREW ACCOMPISHED RAPID DECOMPRESSION/EMERGENCY DESCENT PROCEDURES AND DEPLOYED PASSENGER OXYGEN MASKS. CABIN DECOMPRESSED ALONG WITH A TEMPERATURE CHANGE IN CABIN. AIRCRAFT LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED BOTH CABIN PRESSURE CONTROLLERS. REPLACED ALL PASSENGER OXYGEN CANISTERS AND REPACKED MASKS. RAN ENGINES AND PACKS ON THE GROUND WITH NO ABNORMAL INDICATION NOTED. AIRCRAFT WAS FLOWN ON FUNCTIONAL CHECK FLIGHT AND PRESSURIZATION CHECKS NORMAL IN ALL PHASES OF FLIGHT WITH ANTI-ICE ON OR OFF. AIRCRAFT WAS RELEASED INTO SERVICE. SYSTEM GROUND AND LEAK CHECKED, NORMAL OPERATION. REF: OPER CNTRL NR AALA9

Part: CONTROLLER — DEFECTIVE (AFT FUSELAGE)

DFW - FLT 1617 - DURING CRUISE LGA/DFW FL 280, FLOW LIGHT ILLUMINATED WITH ANTI-ICE ON. CREW ACCOMPISHED RAPID DECOMPRESSION/EMERGENCY DESCENT PROCEDURES AND DEPLOYED PASSENGER OXYGEN MASKS. CABIN DECOMPRESSED ALONG WITH A TEMPERATURE CHANGE IN CABIN. AIRCRAFT LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED BOTH CABIN PRESSURE CONTROLLERS. REPLACED ALL PASSENGER OXYGEN CANISTERS AND REPACKED MASKS. RAN ENGINES AND PACKS ON THE GROUND WITH NO ABNORMAL INDICATION NOTED. AIRCRAFT WAS FLOWN ON FUNCTIONAL CHECK FLIGHT AND PRESSURIZATION CHECKS NORMAL IN ALL PHASES OF FLIGHT WITH ANTI-ICE ON OR OFF. AIRCRAFT WAS RELEASED INTO SERVICE. SYSTEM GROUND AND LEAK CHECKED, NORMAL OPERATION. REF OPER CNTRL NR 98ZZZX

Part: ANGLE — CORRODED (BS 207-218)

TUL - CORROSION ON CUSP ANGLE LONGERON 18L. INSTALLED DOUBLER PER ESO 80559, DATE 11-14-96. (M)

Part: ANGLE — CORRODED (BS 160-205)

TUL - CUSP T-ANGLE AND CUSP MEMBRANE CORRODED STATION 160-205, JUST INBOARD OF FORWARD SERVICE DOOR. INSTALLED NEW SECTION OF CUSP ANGLE STATION 165-205 PER SRM 53-05 FIG 55, INSTALLED NEW SECTION OF CUSP STATION 175-200 PER SRM 53-01 FIG 2. TREATED AND PRIMED BARE METAL PER SRM 51-10-3. (M)

Part: LONGERON — CORRODED (BS 1060)

TUL - CORROSION INSIDE GOUGE L-28 RIGHT BLENDED BEYOND LIMITS. REPAIRED PER ESO 80559, DATED 11-7-96. INSTALLED STRAP DOUBLER INSIDE LONGERON CHANNEL. (M)

Part: LONGERON — CORRODED (BS 1078)

TUL - FOUND CORROSION INSIDE GOUGE L-27 RIGHT BLENDED TO BEYOND LIMITS. REPAIRED PER ESO 80559, DATED 11-7-96. INSTALLED STRAP DOUBLER INSIDE LONGERON CHANNEL. (M)

Part: BRACKET — CORRODED (BS 1309)

TUL - CORROSION ON PULLEY BRACKET. BRACKET REPLACED. (M)

Part: BRACKET — CORRODED (BS 1309)

TUL - CORROSION ON PULLEY BRACKET. BRACKET REPLACED. (M)