N133DN

Part: SKIN — DENTED (BS 336, S37R) · airframe 48,451 hrs · 22,952 cycles

DENTS IN FUSELAGE SKIN REQUIRING CUTOUT AND REINFORCEMENT VIA TWO EXTERNAL REPAIR DOUBLERS. CORRECTIVE ACTION PER ERA 456425-14 REV A

Part: GASPER FAN — OVERHEATED (CABIN) · airframe 47,287 hrs · 22,464 cycles

TAXI OUT, 5 MINS AFTER NR 2 ENG WAS STARTED ODOR ALL OVER CABIN. RETURNED TO GATE. SMELL HAD DISSIPATED UPON RETURN TO GATE. FOUND GASPAR FAN INOP. RAN BOTH ENGS AND PACKS, NO SMELL NOTED. REPLACED GASPER FAN.

Part: COFFEEMAKER — ARCED (FWD GALLEY) · airframe 46,751 hrs · 22,245 cycles

1RT GALLEY G1A COFFEEMAKER MAKES ELEC ARCING SOUND WHEN TURNED ON. REPLACED SAME.

Part: HOUSING — FRACTURED (SPOILER ACTUATOR) · airframe 43,462 hrs · 20,816 cycles

CENTER HYD SYSTEM FAILURE ON TAKEOFF. QUANTITY ZERO RETURNED. FOUND NBR 6 SPOILER ACTUATOR HOUSING CRACKED. REPLACED NR 6 SPOILER PCA IAW MM 27-61-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,705 hrs · 20,431 cycles

FUSELAGE SKIN CRACKED AT STA 1197+100 AND BL 0 AT LOWER VHF ANTENNA. AREA REPAIR IAW ERA 091394-14.

Part: PIN — DAMAGED (RT MLG) · airframe 42,097 hrs · 20,080 cycles

WHILE WORKING A AIR GROUND DISAGREE PROBLEM. JACKED THE A/C PER THE SETUP AND FOUND THE RIGHT MAIN GEAR SWAYED FROM SIDE TO SIDE WHEN PUSHED INBOARD TO OUTBOARD. FOUND THE BOGIE PIN DAMAGED AND THE RIGHT TRUCK BUSHINGS WORN AND CRACKED. ALSO FOUND THE BOGIE BEAM BUSHINGS DAMAGED AND CRACKED.

Part: FLASHLIGHT — UNSERVICEABLE (CABIN) · airframe 41,613 hrs · 19,817 cycles

DURING MEDICAL EMERGENCY, EEMK, WALKAROUND 02 BOTTLE, FLASHLIGHT, AND BIOHAZARD KIT WERE USED. REPLACED EEMK O2 BOTTLE FLASHLIGHT BIOHAZARD KIT AND EMK. OK CONTINUED SERVICE.

Part: ODOR — DETECTED (CABIN) · airframe 40,555 hrs · 19,304 cycles

IRREG/ LIGHT OUTSIDE MID LAV (AREA 215) ELECTRICAL BURNING/ BALLAST ODOR. INSPECTED BALLASTS IN AREA AND IFE SYSTEM, NO ELECTRICAL BURNING ODOR. LIGHTS AND IFE SYS OPS OK. NO ODOR IN AREA UPON ARRIVAL. CHECKED ACOVE CEILING PANELS IN AREA AND IN LAV. ALL OK.

Part: WIRE HARNESS — DAMAGED (LE FLAP SENSOR) · airframe 39,853 hrs · 18,968 cycles

LEADING EDGE FLAP LIGHT AND EICAS MSG WHEN FLAPS WERE PUT TO 20 DEGREES. REPAIRED S301 SENSOR WIRING.

Part: INDICATOR — INOPERATIVE (TE FLAPS) · airframe 39,765 hrs · 18,928 cycles

AT FL350 FLAP INDICATOR NEEDLES JUMPED TO .5 DEG AND FLUCTUATED TO 0 AND BACK L/E ASSY LIGHT AND MESSAGE. BIT PSEU/FSEU FAULTS NBR 11 I/B SLAT SENSOR..301.. CKD GAPS AND SENSORS W/ELDEC CKS GOOD. RESET PSEU AND OP FLAPS SEV TIMES. NO FAULTS. REPLACED FSEU MM OK FOR SERVICE.

Part: GASKET — LEAKING (NR 1 ENGINE) · airframe 35,852 hrs · 16,958 cycles

LEFT ENGINE FAILED IN FLT ON DESCENT INTO MCO. POM PROCEDURES FOLLOWED, ONLY ABNORMAL INDICATION WAS HIGH FUEL FLOW, COMPARED TO THE RIGHT ENGINE. ON ARRIVAL FOUND LEFT ENGINE IDG FUEL/OIL COOLER GASKET CUT AND LEAKING. REPLACED SAME. FULL POWER RUN UP PER PFHB PERFORMED. LEAK CHECK OK.

Part: FUEL LINE — LEAKING (NR 2 ENGINE) · airframe 35,703 hrs · 16,892 cycles

FOUND FUEL LEAK ON RT ENGINE WHEN OPENED FOR MTC, POSSIBLE FIRE CONDITION EXISTED. FOUND FUEL LINES LEAKING. REPLACED FLEX FUEL LINES FROM FUEL FILTER TO DIFF PRESSURE SWITCH AND TO HEAT EXCHANGER, LEAK CHECK FOUND OK.

Part: LIGHT — INOPERATIVE (AFT DOOR) · airframe 34,495 hrs · 16,318 cycles

LT AFT DOOR EXT EMERGENCY LIGHT INOP RELAMPED. CKS OK.

Part: CIRCUIT BOARD — FALSE INDICATION (FIRE DETECTION) · airframe 31,362 hrs · 14,825 cycles

APPROX 90 KNOTS ON T/O FIRE BELL SOUNDED . T/O REJECTED AT 100 KNOTS NO LIGHT ASSOC WITH BELL. REPLACED CIRCUIT CARDS M1000 AND M618.

Part: FAN — INOPERATIVE (COCKPIT)

AT CRZ FLT FL390, CREW NOTED AN ELECT ODOR. CREW PERFORMED SMOKE IDENTIFICATION/REMOVAL CHECKLIST. ODOR WAS ELIMINATED, C/B H-21 ON P6-4 PANEL WAS POPPED. FWD EXHAUST EQUIPT FAN. NO OTHER SMELLS NOTED FOR REMAINDER OF FLT. REPLACED FAN.

Part: BOTTLE — LOW PRESSURE (RT EMER EXIT)

RIGHT OVERWING SLIDE BOTTLE PRESSURE LOW ALMOST EMPTY.

Part: SKIN — CRACKED (BS 436)

THE FUSELAGE SKIN AT FS 436, STRG 33R TO 34R, WAS DENTED BY GROUND EQUIPMENT. THE AFT EDGE OF THE UNDERLYING SKIN SPLICE STRAP WAS CRACKED AT A FASTENER LOCATION. THE DENTED SKIN AND CRACKED AREA OF THE STRAP WERE TRIMMED OUT AND AN EXTERNAL ALUMINUM REPAIR DOUBLER WAS INSTALLED TO REPAIR THE DAMAGE. THE REPAIR WAS ACCOMPLISHED PER ER/A 364759-14, REV A.

Part: TRANSMITTER — INOPERATIVE (OIL QTY)

CENTER SYSTEM RESVR LIGHT ON OVERHEAD PANEL ILLUMINATED. STATUS PAGE SHOWED CENTER SYSTEM QUANTITY AT ZERO. VERIFIED THAT SYSTEM QUANTITY WAS OK. REPLACED OIL QUANTITY TRANSMITTER, SYSTEM OPS CHECKS NORMAL.

Part: CLAMP — LOOSE (NR 1 ENGINE)

AIRCRAFT 133 EXPERIENCED AN IN FLIGHT SHUTDOWN DUE TO A LEFT ENGINE FIRE WARNING ON CLIMBOUT FROM PDX. PILOTS FOLLOWED POM PROCEDURES. MAINTENANCE FOUND A LOOSE HIGH PRESSURE VALVE INBOAD CLAMP AFTER BACK PRESSURIZING USING APU. RESECURED CLAMP AND RELEAK CHECKED VALVE, ALL NORMAL. RAN NR 1 ENGINE AT TAKEOFF POWER AND NO WARNING NOTED.

Part: COFFEEMAKER — FAILED (GALLEY)

ELECTRICAL BURNING SMELL COMING FROM MID GALLEY AREA WHEN COFFEE MAKER IS USED. REPLACED COFFEEMAKER.

Part: BULB — FAILED (CABIN)

R-3 DOOR EMER EXIT LIGHT INOP. RELAMPED RT OVERWING MOST AFT EMER LIGHT.