N366PX

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 31,270 hrs · 26,692 cycles

DURING CAPACITY INSPECTION IN MSP, BATTERY SUPPLY P/N 61-0478-9, S/N ELB136 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACITY CHECK FAILED. MAINTENANCE REPLACED CELL PACK P/N 549-1324-06 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/16/04.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,137 hrs · 26,529 cycles

DURING CAPACITY INSPECTION IN MSP, EMERGENCY LIGHT POWERED BY POWER SUPPLY P/N 60-1321-1, S/N 14587, SQUAWKED INOP. MAINTENANCE DEEP CYCLED & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/6/04.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,137 hrs · 26,529 cycles

EMERGENCY LIGHTS 3LN, 4LN, AND 42LN INOPERATIVE. (LT AND RT EXTERIOR LIGHTS AND RT AFT COVE LIGHT) MAINTENANCE REMOVED AND REPLACED 24LN EMERGENCY POWER SUPPLY IAW SMM 33-50-10. P/N ON/OFF 60-1321-1. S/N ON 18225 S/N OFF 14587.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

BATTERY PACK P/N 61-0478-9, S/N ELB109 WAS REMOVED FOR SCHEDULED CAPACITY CHECK. CAPACITY CHECK FAILED. MAINTENANCE REPLACED CELL PACK P/N 55-2198-1. UNIT PASSED CMM CHECK AND WAS RETURNED TO SERVICE 6/4/04.

Part: TRANSDUCER — MALFUNCTIONED (HYD PRESSURE) · airframe 30,327 hrs · 25,695 cycles

SHORTLY AFTER T/O CLIMBING THROUGH ABOUT 6000 FT GOT HYD CAUTION LIGHT ON CWP TURNED PUMP OFF NOTICED MAIN WAS NORMAL EMERG WAS LOW DOWN TO ALMOST 0 QTY AND O/B INDICATORS WAS NORMAL ABOUT A MIN TO 90 SEC IT STARTED TO PUMP BACK UP JUMPING UP NAD DOWN THEN BACK TO NORMAL. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED EMERG ACC PRESSURE TRANSDUCER IAW AMM 29-32-05-4 OPS CHECKS GOOD PN IPT61-1000-3000SG SN OFF 645-8-175 SN ON 560-7-264.

Part: FIRE DETECTOR — FAULTY (LT ENGINE) · airframe 30,199 hrs · 25,541 cycles

AFTER ENGINE START, LEFT ENGINE FIRE WARNING ON CWP AND LEFT FIRE HANDLE ILLUMINATED, ALONG WITH FIRE BELL. LIGHTS AND WARNING WERE ON BRIEFLY, THEN EXTINGUISHED. TESTED THE LEFT FIRE SYSTEM ON TEST PANEL, TEST GOOD. THEN THE FIRE INDICATION OCCURRED AGAIN. MAINTENANCE REMOVED AND REPLACED FIRE DETECTOR P/N 899052-02, S/N ON 0840, S/N OFF 0620, AND WEU P/N 006W00, S/N ON 1581, S/N OFF 1623, IAW AMM 31-50-05 AND 26-11-10. OPS CHECK GOOD.

Part: DOOR — OPEN (RT NACELLE) · airframe 30,044 hrs · 25,376 cycles

RIGHT COWLING POPPED OPEN INFLIGHT. AIR RETURN TO MEM. REPLACED LEFT AND RIGHT FWD COWLINGS ON RIGHT ENGINE WITH SERVICEABLE UNITS. RIGHT P/N 7271110-271, LEFT P/N 7271110-269. GOOD FOR SERVICE.

Part: ENGINE — SURGES (LEFT)

DURING FLT, SHORTLY AFTER T/O, LT ENGINE SURGED TO OVER 100 PERCENT TORQUE, THEN BACK TO 80 PERCENT. ITT FOLLOWED SAME TREND. PERFORMED ERRATIC. ENGINE QRH INFLIGHT AND LOCKED OUT TORQUE MOTOR, ENGINE AND INDICATIONS STABILIZED EXCEPT FOR TORQUE. TORQUE GAUGE CONTINUED TO BOUNCE 20 PERCENT ON TAXI IN, POWER LEVERS AT GROUND IDLE TORQUE IND WAS AT 0-20 PERCENT. AIR RETURN TO MSP. MAINTENANCE REPLACED LT ENGINE P/N CT7-9B IAW JOB CARD 7100-301 AND PROP P/N R390/4-123-F/27 IAW JOB CARD 6110-303 ENG S/N ON GE-E785734 PROP S/N ON DAP0192, ALL OPS CHECKS GOOD. CREW MUST ESTABLISH NEW BASE LINE FOR DDT.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,861 hrs · 24,077 cycles

DURING 4K INSPECTION IN CWA, LT CENTER FWD SEAT TRACK ASSEMBLY HAS CORROSION OUT OF LIMITS. MAINTENANCE REPAIRED DAMAGED SECTION OF SEAT TRACK IAW EO NR S53060 LBL 18.5 AT STA 297 TO STA 329. A/C RELEASE DATE IS 8/11/03. REFER TO 409 NR 192875 FOR DETAIL.

Part: SKIN — DENTED (TAIL CONE) · airframe 28,862 hrs · 24,078 cycles

DURING 4K INSPECTION IN CWA, RT TAIL CONE UPPER SKIN 1050 HAS A DEEP DENT, 1 DIA AT RT STA 828.25, 20.5 INCH, ABOVE SL1614. MAINTENANCE REPAIRED DAMAGE IAW EO NR S53176.

Part: B-NUT — LOOSE (MLG)

DURING APPROACH ON FLIGHT NR 3268, ON SHORT FINAL WITH GEAR AND FLAPS DOWN, HYDRAULIC CAUTION LIGHT ILLUMINATED. WENT AROUND BUT GEAR AND FLAPS REMAINED DOWN. HYDRAULIC QUANTITY AND MAIN PRESSURE INDICATED ZERO. LOST HYDRAULIC AND PRESSURE. GEAR WAS SELECTED DOWN ALREADY BEFORE QUANTITY STARTED GOING DOWN. MAINTENANCE FOUND HYDRAULIC FLUID COMING FROM THE GEARWELL. FOUND B-NUT LOOSE ON RETRACTION ACTUATOR ON AFT LINE. MAINTENANCE RETORQUED LINE. FLUID STOPPED. SERVICED HYDRAULIC IAW SF340 AMM 29-10-29 PERFORMED LEAK AND OPS CHECK ON RETRACTION ACTUATOR . OPS CHECK GOOD. NO LEAKS AT THIS TIME.

Part: BOLT — BROKEN (MLG)

RT SEPARATION BOLT (ON MAIN LANDING GEAR) BROKE. MAINTENANCE REPAIRED WIRING AT CONNECTOR GB602-20 AND WIRE GB604-20 IAW SAAB WM 20-20-35. REFER LOG PAGE 177372 FOR DETAIL.

Part: CONTROLLER — FAILED (WINDSHIELD HEAT)

DURING FLIGHT 3082 LT FRONT WIND SHIELD LIGHT ILLUMINATED 3 TIMES IN 10 MINUTES. FOLLOWED QRH, COMES ON AGAIN. AIR RETURN TO MSP. MAINTENANCE COMPLETED 409 CARD 144349 REPLACED LT WINDSHIELD HEAT CONTROLLER. SEE CONTINUATION CARD 144349 FOR DETAILS. OPS CHECK GOOD.

Part: CONTROL UNIT — FAULTY (BLEED AIR SYS)

INFLIGHT 3054, HAD A LT BLD AIR LEAK LIGHT. PERFORMED QRH LIGHT WENT OUT. AIR RETURN TO DTW. MAINTENANCE REPLACED BLEED LEAK DETECTION CONTROL UNIT (3WU) IAW MM 36-23. OPS CHECKS GOOD.

Part: POWER SUPPLY — LOOSE (E/E BAY)

DURING FLIGHT 2756 EMERGENCY POWER SUPPLY CAUTION LIGHT ILLUMINATED. AIR TURNBACK TO MSP. MAINTENANCE RESECURED EMERGENCY POWER SUPPLY (JET PACK) IN AVIONICS RACK. OPS CHECK GOOD.

Part: FIRE DETECTOR

BEFORE FLIGHT #3255, CARGO SMOKE NOT TESTING IN BJI. FERRIED AC TO MSP. MAINTENANCE REPAIRED BROKEN WIRE COMMON TO FWD CARGO SMOKE DETECTOR CONNECTOR. COMPLETED OPERATIONAL TEST IAW SF340 AMM 26-13-00-5 OPS CHECK GOOD.

Part: PCU — SURGED (LT ENGINE)

ABORTED TAKEOFF, APPEARED THAT LEFT ENGINE TORQUE SURGED AND CAUSED AIRCRAFT TO YAW TO RIGHT. REMOVED AND REPLACED LEFT PCU. PERFORMED GROUND RUNS. OPS CHECK GOOD. (M)

Part: VALVE — FAILED (RT ENGINE)

RIGHT ENGINE VIBRATES AND SOUNDS SIMILAR TO COMPRESSOR STALL. ALL OTHER INDICATIONS NORMAL. AFTER INSPECTION OF RIGHT ENGINE AND GROUND RUNS IN SEVERAL DIFFERENT POWER SETTINGS, NO DEFECTS NOTED. SWAPPED ANTI-ICING BLEED VALVE FOR TROUBLESHOOTING GROUND RUNS AND CHECKS. FOUND NO DEFECTS. (X)

Part: AC GENERATOR — FAILED (LT ENGINE)

LEFT AC GENERATOR FAILED ON TAXI. REMOVED AND REPLACED LEFT GENERATOR. (M)

Part: ENGINE — OVERTEMP (RIGHT)

ABORTED TO RIGHT ENGINE REACHED 936 ITT. DEFERRED AND PLACARDED PER MEL 77-20-01. (M)

Part: CONNECTOR — LOOSE (RIGHT COCKPIT)

SMOKE IN COCKPIT WHILE ON GROUND, WITH L/R AVIONICS SWITCHES ON. RT EFI TUBES WERE BLACK. FOUND RIGHT DISPLAY CONTROL PANEL ELECTRICAL CONNECTOR LOOSE. TIGHTENED LOOSE CONNECTOR. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: FIRE WARNING — ACTIVATED (CARGO COMPT)

CARGO SMOKE IN CWP. CAPTAIN BLEW FIRE BOTTLE AND RETURNED TO LITTLE ROCK. NO EVIDENCE OF FIRE. REMOVED AND REPLACED SMOKE DETECTOR AND FIRE EXTINGUISHER CONTAINER BOTTLE. (M)

Part: HOSE — BROKEN (NLG WW)

ON TAXIING, LOST HYDRAULIC QUANTITY 2 CWP, LEAK ON MAIN RESERVE IN NOSE WHEEL COMPARTMENT. REMOVED AND REPLACED UPPER HYDRAULIC PUMP RETURN LINE IAW AMM CHAPTER 29. NO LEAKS NOTED. ACFT OK FOR SERVICE. (X)

Part: CLEVIS ASSEMBLY — BROKEN (LT BRAKE PEDAL)

CAPTAIN'S LEFT BRAKE RUDDER PEDAL BROKE. REMOVED AND REPLACED CAPTAIN'S LEFT FOOT PEDAL BRAKE CABLE ASSY IAW AMM CHAPTER 32. (X)