N367PX

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,376 hrs · 25,000 cycles

DURING 4Y/2Y INSPECTION IN BNA, GALLEY SEAT TRACK P/N 7253721-459 CORRODED. MAINTENANCE REMOVED AND REPLACED. AIRCRAFT RETURNED TO 11/23/04.

Part: FRAME — CHAFED (FUSELAGE) · airframe 29,376 hrs · 25,000 cycles

DURING 4Y/2Y INSPECTION IN BNA, FRAME CHAFED ON RT SIDE AT FS 686.888 WAS REPAIRED IAW EO S53261. AIRCRAFT RETURNED TO 11/23/04.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT)

DURING CAPACITY CHECK, BATTERY PACK P/N 61-0478-9, S/N ELB502 FAILED SCHEDULED CAPACITY CHECK. REPLACED BATTERY ASSEMBLY P/N 55-2198-1. UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 11/13/04.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,789 hrs · 26,983 cycles

DURING CAPACITY INSPECTION IN MSP, POWER SUPPLY P/N 61-0478-9, S/N 9903018 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACITY CHECK FAILED. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 55-2198-1 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/11/04.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,789 hrs · 26,983 cycles

DURING CAPACITY INSPECTION IN MSP, BATTERY PACK P/N 61-0478-9, S/N 9804449 REMOVED FOR SCHEDULED CAPACITY CHECK, CAPACITY CHECK FAILED. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 55-2198-1 & UNIT PASSES CMM CHECKS. RETURNED TO SERVICE 10/4/04.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,091 hrs · 26,200 cycles

BATTERY PACK P/N 61-0478-9, S/N ELB052 FAILED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 55-2198-1, PASSES CMM CHECKS. A/C RETURNED TO SERVICE 6/13/04.

Part: BATTERY PACK — SMOKE (EMERGENCY LIGHT)

BATTERY PACK P/N 61-0478-9, S/N 19881 STARTED SMOKING WHEN INSTALLED INTO POWER SUPPLY. MAINTENANCE REPLACED BATTERY PACK P/N 55-2198-1. UNIT PASSED CMM CHECKS, RETURNED TO SERVICE 12/12/04.

Part: PROPELLER — FAULTY (LT ENGINE) · airframe 30,852 hrs · 25,939 cycles

LEFT PROP DEICE ANNUNCIATION ILLUMINATES IN NORM AND MAX INFLIGHT. AIR RETURN TO MEM. MAINTENANCE REMOVED & REPLACED LEFT PROP IAW JC 6110-303. P\N OFF R390/4-123/F27. P\N ON R389/4-123/F26. S/N ON DAP0199, S/N OFF DAP/0003/92. ALL CHECKS GOOD.

Part: CONTROL VALVE — FAILED (TE FLAPS) · airframe 30,495 hrs · 25,580 cycles

LANDING IN DTW CREW REPORTED FLAPS WOULD NOT EXTEND. COMPLETED ALL FLAPS LANDING. FLAPS WILL NOT EXTEND DN FLAPS 0 AT DTW ALL CB IN. REMOVED AND REPLACED FLAP CONTROL VALVE S/N ON 1168, S/N OFF 1588 IAW SAAB MM CHAP 27 SEE 409 CARD FOR DEATILS, ALL CHECKS GOOD.

Part: SWITCH — CONTAMINATED (MLG)

AFTER GEAR RETRACTION ON TAKEOFF THE GEAR INTRANSIT LIGHT REMAINED ILLUMINATED. MAINTENANCE REMOVED ICE FROM SWITCHES ON MLG & CLEANED SWITCHES, OPS CHECK GEAR IAW 32-30-00-5 ALL CHECKS GOOD.

Part: CONTROL QUADRANT — DAMAGED (ENGINE)

AFTER TAKEOFF, WHEN GEAR WAS SELECTED UP, THE F1 STOP OPEN LIGHT ILLUMINATED. AIR RETURN TO MEM. MAINTENANCE REPLACED CONTROL QUADRANT IAW TASK CARD 761002. ALL SYSTEM CHECKS NORMAL SEE CONTINUATION CARD 039947, 040855 FOR DETAILS. DISC NR 1 REMOVED ALL CENTER CONSOLE TO FACILITATE FO MX/CA NR 1 INSTALLED EVERYTHING IN CENTER CONSOLE AS REQUIRED. ALL CHECK GOOD. DISC NR 2 PANEL ON SIDE OF CENTER CONSOLE REMOVED AND INSTALLED PANELS. DISC NR 3 DURING ENGINE RUNS FOR QUADRANT CHANGE, AUTOCOURSEN, APR AND CTOT INOP. MX FOUND RELAY 44KA BAD, REPLACED RELAY ALL SYSTEMS CHECK NORMAL. PN 6106-27-023.

Part: STRUCTURE — DENTED (FUSELAGE)

RT FUSELAGE HAS 2 DENTS AT STA 315, BETWEEN SL1615 AND SL1617. MAINTENANCE COMPLETED REPAIR IAW EO S53143.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,740 hrs · 22,469 cycles

DURING 4K INSPECTION IN CWA, CENTER AISLE SEAT TRACK BL 0 HAS CORROSION IN CARGO AREA. MAINTENANCE REMOVED CORROSION IN CARGO AREA, COMPLETED REPAIR IAW MAL EO S53060. A/C RELEASE DATE 11/6/02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,740 hrs · 22,469 cycles

DURING 4K INSPECTION IN CWA, RT SEAT TRACK IN CARGO AREA HAS CORROSION. MAINTENANCE COMPLETED REPAIR IAW MAL EO S53060. A/C RELEASE DATE 11/6/02.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT)

DURING TAXI OUT OF FLIGHT NR 3154, RUDDER LIMITER LIGHT ILLUMINATED. RETURNED A/C TO GATE. MAINTENANCE ADVISED OF PROBLEM AFTER GATE RETURN. MAINTENANCE T/S SYSTEM IAW SAAB AMM 27-21-45. ALL CHECKS GOOD, COULD NOT DUPLICATE.

Part: ACTUATOR — DAMAGED (MLG)

ON APPROACH TO YNG RT MLG LIGHT DID COME ON AFTER SELECTING GEAR DOWN/TRANSIT LIGHT STILL ON. FOLLOWED QRH WHEN RECYCLED THE GEAR UP, THEN DOWN, THE RIGHT GEAR MADE A LARGE CLUNK NOISE. GEAR DOWN W/T 2/3 SECONDS THEN LT AND NLG SHOWED DOWN. ON POST FLIGHT NOTED GEAR DOOR DAMAGE. MAINTENANCE INSPECTED RT GEAR, FOUND RETRACT ACTUATOR BROKE AND MINOR SHEETMETAL DAMAGE TO GEAR DOOR. FERRIED A/C TO DTW FOR REPAIRED.

Part: BLEED VALVE — MALFUNCTIONED (LT ENGINE)

DURING FLIGHT 2789, LT AIR VALVE LIGHT ILLUMINATED IN ICING CONDITIONS. LT AIR VALVE LIGHT CAME ON AT 16,000 FT MSL FOLLOWED QRH AND RESET SWITCH. LIGHT STAYED ON OPERATED LEFT ENGINE BELOW 86 PERCENT NG UNTIL CLEAR OF ICING CONDITIONS AS PER QRH. AIR RETURN TO MSP. MAINTENANCE REPLACED THE LT AIR VALVE IAW GE MM 75-00-00. ALL CHECKS GOOD.

Part: INDICATOR — DEFECTIVE (COCKPIT)

DURING FLIGHT 3036 WHILE CRUISING, FLIGHT AT 22,000 FT AND -20 DEGREES CELSIUS THE F/O AIRSPEED INDICATOR INCREASED SLOWLY TO 350 KIAS NO OVERSPEED WARNING WAS TRIGGERED, CAPT AND STBY AIRSPEED INDICATOR OPERATES NORMALLY. AIR RETURN TO MSP. MAINTENANCE DRAINED AND PURGED W/DRY NITROGEN NR 2 PITOT SYSTEM, REMOVED AND REPLACED NR 2 ASI. NR 2 PITOT STATIC SYSTEM AND NR 2 ASI TEST GOOD IAW SF340 MM CHAP 34. PITOT HEAT TEST GOOD.

Part: MOTOR — OVERHEATED (AIR CONDITIONING)

SMOKE IN CABIN. REMOVED AND REPLACED AFT FREON COMPRESSOR MOTOR. (M)

Part: SWITCH — FAILED (HYDRAULIC SYSTEM)

PILOT REPORTED LOSS OF HYDRAULIC PRESSURE. PERFORMED EMERGENCY EXTENSION OF THE LANDING GEAR AND DECLARED AN IN-FLIGHT EMERGENCY. REMOVED AND REPLACED THE HYDRAULIC PRESSURE SWITCH. REMOVED AND REPLACED THE EXPLOSIVE BOLTS ON LEFT AND RIGHT MLG DOORS AND PERFORMED FUNCTIONAL/OPERATIONAL CHECK OF LANDING GEAR. SYSTEM CHECKED GOOD. (X)

Part: GENERATOR — FAILED (RIGHT)

RIGHT GENERATOR IS INOP. REMOVED AND REPLACED RIGHT GENERATOR AND REPAIRED ALL WIRES ON TERMINAL BLOCK. OPS CHECK GOOD. (M)

Part: ANTENNA — FAILED (RADAR)

WEATHER RADAR POINTS ECHOES ON OPPOSITE SIDE OF DISPLAY KNOWN. ECHOES TO RIGHT OF AIRCRAFT PAINT ON LEFT SIDE OF DISPLAY. REMOVED AND REPLACED THE WEATHER RADAR ANTENNA. (M)

Part: LIMITER UNIT — INOP (RUDDER)

RUDDER WOULD NOT TRAVEL FREELY WITH GUST LOCK REMOVED UNTIL RUDDER LIMITER WAS PLACED IN OVERRIDE. REMOVED AND REPLACED THE RLU IAW AMM CH27. (M)

Part: HYDRAULIC PUMP — FAILED (FWD FUSELAGE)

HYDRAULIC PUMP FAILURE. REMOVED AND REPLACED MAIN HYDRAULIC PUMP IAW AMM OPERATIONAL CHECK OF SYSTEMS GOOD. OK FOR SERVICE. (X)

Part: STARTER/GEN — FAILED (RIGHT)

RIGHT GENERATOR FELL OFF-LINE. REMOVED AND REPLACED STARTER GENERATOR. (X)