N365PX

Part: LAMP — INOPERATIVE (LIGHT SWITCH) · airframe 46,042 hrs · 37,186 cycles

LAMP IN F/A EMERGENCY LIGHT SWITCH IS OUT. INSTALLED NEW LAMP.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 45,779 hrs · 36,954 cycles

INDICATION OF LAVATORY SMOKE. INDICATION ONLY LASTED FOR A FEW SECONDS AND THEN EXTINGUISHED. LAVATORY WAS CHECKED AND NO INDICATION OF A FIRE WAS PRESENT. SMOKE WARNING CAME ON A SECOND TIME AND WENT OFF. CIRCUIT BREAKERS PULLED IAW THE CHECKLIST AND RECIRCULATION FAN WAS TURNED OFF. RETURNED TO PQI.

Part: PUMP — MALFUNCTIONED (HYDRAULIC SYS)

DURING THE ARRIVAL INTO ANC THE HYDRAULIC WARNING LIGHT ILLUMINATED, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT.

Part: DETECTOR — MALFUNCTIONED (LT TAIL PIPE)

ON JUNE 22, 2008, THE FLIGHT CREW HAD A LEFT TAIL PIPE HOT LIGHT, AN INFLIGHT ENGINE SHUTDOWN WAS MADE, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT MADE AN UNEVENTFUL LANDING AT DEPARTURE AIRPORT. THE LIGHT WENT OUT A FEW MINUTES BEFORE LANDING, AND THE TOTAL FLIGHT TIME WAS 23 MINUTES. MAINT REPLACED ALL THREE HEAT DETECTORS AFTER TROUBLESHOOTING THE SYSTEM, THE SYSTEM CHECKED NORMAL AND THE AC WAS RETURNED TO SERVICE. THE FLIGHT WAS BEING OPERATED UNDER FLIGHT NR 245. (K)

Part: CONDITION LEVER — FAILED (LT PROPELLER) · airframe 33,785 hrs · 29,190 cycles

NO CONTROL OF LT PROP RPM IN FLIGHT CONDITION LEVER MOVES FREELY WITH NO CHANGE IN RPM. ALL OTHER PARAMETERS NORMAL ENGINE WOULD NOT SHUT DOWN AT GATE. PULLED FIRE HANDLE. REMOVED AND REPLACED LT CONDITION CABLE. PERFORMED ALL RUNS AND OPS CHECK IAW SAAB AMM 76-10-46.

Part: ACM — ODOR (LEFT) · airframe 33,061 hrs · 28,367 cycles

AIR RETURN TO RHI FOR BURNING ODOR, MAINLY IN FLT DECK. REPLACED LEFT ACM.

Part: RADIO — MALFUNCTIONED (COCKPIT) · airframe 32,861 hrs · 28,117 cycles

DURING CLIMBOUT FROM DTW INTERCOM STATIC BECAME SEVERE, STATIC OVER SPEAKERS WITH ALL VOLUMNS OFF. RETURNED TO DTW. REMOVED AND REPLACED REU AND F/O'S ACP. OPS CHECK GOOD.

Part: BATTERY — FAILED (EMERGENCY LIGHT)

BATTERY POWER SUPPLY FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY. UNIT PASSES CMM CHECKS. AIRCRAFT RETURNED TO SERVICE 12/26/04.

Part: BATTERY PACK — FAILED (EMERGECNY LIGHT)

BATTERY PACK FAILED SCHEDULED CAPACITY CHECK. MAINTENANCE DEEP CYCLED UNIT PASSES CMM CHECKS. AIRCRAFT RETURNED TO SERVICE 12/23/2004.

Part: RELAY — INOPERATIVE (EMERGNECY LIGHT)

BATTERY POWER SUPPLY P/N 61-1321-1, S/N OFF 18522 REPORTED TO NEED BENCH CHECK. MAINTENANCE FOUND WHITE ARM SWITCH ON LIGHT DOES NOT LIGHT. MAINTENANCE REPLACED C4, C5, Q1, Q5 AND SCR1. UNIT PASSES CMM CHECKS. A/C RETURNED TO SERVICE 1/21/04.

Part: GALLEY TRACK — CORRODED (FUSELAGE) · airframe 32,040 hrs · 27,220 cycles

DURING 4Y/2Y INSPECTION IN BNA, NOTED GALLEY FLOOR TRACK CORRODED. MAINTENANCE REPLACED TRACK.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,040 hrs · 27,220 cycles

DURING 4Y/2Y INSPECTION IN BNA, NOTED CORROSION ON FRAME STA 258.0 FLANGE. REPAIRED PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,178 hrs · 26,324 cycles

UNIT WAS REMOVED FOR MISSING CAMLOCK, P/N 61-0478-9, S/N ELB082. WHILE UNDERGOING BENCH CHECK, UNIT FAILED CAPACITY CHECK. REPLACED CELL PACK P/N 55-219801 AND UNIT PASSED CMM CHECKS. RETURNED TO SERVICE 5/27/04.

Part: BATTERY — FAILED (CABIN) · airframe 31,083 hrs · 26,244 cycles

POWER SUPPLY PN 501-1712-02 SN 2065, WAS REMOVED FOR SCHEDULED DISCHARGE CHECK, UNIT FAILED DISCHARGE CHECK. BATTERY ASSEMBLIES (2 EA) PN 549-1324-06 WERE REPLACED AND UNIT PASSED ALL CMM CHECKS. UNIT WAS RETURNED TO SERVICE 5/13/04. FOR ADDITIONAL INFORMATION REFER TO WO#366903.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,968 hrs · 26,125 cycles

DURING CAPACITY CHECK BATTERY PACK P/N 61-0478-9, S/N 9712219 REMOVED FOR SCHEDULED CAPACITY CHECK ON 4/16/04 & 4/21/04 UNIT FAILED TO PASS CAPACITY CHECK. REPLACED CELL PACK P/N 55-2198-1 AND CHARGED AND CAPACITY CHECK WAS GOOD. UNIT CHARGED AND RETURNED TO SERVICE ON 4/25/04.

Part: ACM — SEIZED (LEFT)

POST FLIGHT OF NR 3084, LT ACM BURNING ODOR. SECONDARY INDICATION OF INMINENT LT ACM FAILURE, BURNING ODOR GRINGING NOSIES LT SIDE MIDSECTION. MAINTENANCE FOUND BURNING ODOR FROM RT ACM, FOUND RT ACM SEIZED. REPLACED RT ACM PN 776910-6 SEE 409 NR 071530 FOR DETAILS. OPS CHECKS OF BOTH ACMS GOOD. RT AUTO TEMP CONTROL INOPERATIVE REPLACED AIR CONDITIONING PANEL PN 7739019-505 OPS CHECK GOOD.

Part: ACTUATOR — FAILED (AIRSTAIR)

LEFT FWD EMERGENCY EXIT AIRSTAIRS WILL NOT EXTEND. INSPECTED AND FOUND STAIRS WILL NOT COME DOWN. STAIRS WILL EXTEND, INSPECTED AND FOUND NO DAMAGE, PUT STAIRS IN THE STOWED POSITION. INSPECTED A/C AND FOUND SAFE FOR SAFE FOR FERRY FLIGHT FROM FNT TO DTW. MAINTENANCE REMOVED AND REPLACED AIRSTAIRS KICK OUT ACTUATOR P/N 900050, IAW SF340 MM CHAP 52. ALL CHECKS GOOD.

Part: SELECTOR — LEAKING (OXYGEN CYLINDER)

DURING FLIGHT NR 2735 FROM LOG PAGE: OXYGEN LIGHT ILLUM. GAUGE IND 750 PSI, 1700 PSI AT ACCEPTANCE OF AIRCRAFT. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED LT AND RT AFT OXYGEN CYLINDERS (DUE TO LEAKING AT ON/OFF SELECTOR) & REPLACED BROKEN PRESSURE INDICATING CAPILLARY LINE. LEAK CHECKS GOOD.

Part: PEDAL — FROZEN (RUDDER)

DURING APPROACH ON FLIGHT 2906, RUDDER PEDALS CONTROL ALMOST COMPLETELY UNMOVABLE (FELT AS IF GUST LOCK WAS ENGAGED). FLT CONTROLS FREE AND FULL ON GROUND W/ GUST LOCK DISENGAGED YAW DAMPER AP OFF. INSPECTED RUDDER & ATTACHMENTS FOR CONDITION AND SECURITY, ALL CHECKS GOOD. MAINTENANCE COULD NOT DUPLICATE. FROM LOG PAGE 1212595, COMPLETED FUNCTIONAL AND SYSTEM SELF TEST IAW 27-21-45 AMM OF RUD LIM SYS. CHECK GOOD. INSPECTED RUDDER PEDALS, TAIL COMPARTMENT RUDDER CONTROL AND RUDDER ASSY. NO DEFECTS NOTED. COMPLETED OPERATIONAL CHECKS OF RUDDER GUST LOCK AND YAW DAMPER/AUTOPILOT CONTROL IAW SF 340 MM. ALL CHECKS GOOD AT THIS TIME. MXC NOTIFIED. REMOVED FROM DMR.

Part: SPAR — CRACKED (LT TE FLAP) · airframe 29,176 hrs · 24,258 cycles

DURING 4K INSPECTION IN CWA, LT FLAP REAR SPAR CRACKED AT WS 142. MAINTENANCE COMPLETED REPAIR IN REAR SPAR AT WS 142 IAW EO 57007. A/C RELEASE DATE 6/19/03. REF TO 409 NR 179691 FOR DETAIL.

Part: SPAR — CRACKED (TE FLAP) · airframe 29,176 hrs · 24,258 cycles

DURING 4K INSPECTION IN CWA, RT FLAP REAR SPAR CRACKED AT WS 142. MAINTENANCE COMPLETED REPAIR ON REAR SPAR IAW EO S57007. REF NR 179683 FOR INFORMATION. A/C RELEASE DATE IS 6/19/03.

Part: ICE SHIELD — DENTED (FUSELAGE) · airframe 29,176 hrs · 24,258 cycles

DURING 4K INSPECTION IN CWA, DENT FOUND UNDER RT ICE SHIELD FWD OF STA 319, BETWEEN SL1618 AND SL1620. MAINTENANCE COMPLETED DOUBLER REPAIR IAW EO NR 53005. REF TO 409 NR 179654 FOR DETAIL. A/C RELEASE DATE 6/19/03.

Part: SKIN — DENTED (FUSELAGE) · airframe 29,176 hrs · 24,258 cycles

DURING 4K CHECK IN CWA, RT FUSELAGE CABIN SKIN HAS .039 INCH DEEP DENT, 1.25 INCH AT STA 340.5, 2.5 INCH BELOW SL 1615. MAINTENANCE REPAIRED RT CABIN SKIN DENT IAW EO S53009. A/C RELEASE DATE 6/19/03. REF 409 NR 179659 FOR DETAIL.

Part: DOWNLOCK SWITCH — DIRTY (MLG)

CREW ON FLIGHT 3110, REPORTED THE RT GEAR GREEN LIGHT DID NOT ILLUMINATE WHEN GEAR IS SELECTED DOWN. MAINTENANCE CLEANED AND LUBED DOWNLOCK ACTUATOR SWITCH, PERFORMED GEAR SWINGS. ALL CHECKS GOOD IAW SF340 AMM CHAP 32-30-00-5.

Part: BRAKE — DRAGGING (LT MLG)

DURING TAKEOFF ROLL, THE LEFT BRAKE SEEMED TO START DRAGGING OR APPLY ITSELF. REMOVED FOOT FROM THE PEDAL AND A/C CONTINUED TO PULL LEFT. MORE PRONOUNCED AFTER 40 KNOTS. MAINTENANCE NOTICED LEFT OUTBOARD BRAKE TO BE HOTTER THAN OTHER BRAKES. MAINTENANCE INSTALLED 4 BRAKE TEST GAUGES ON BRAKES. ALL INPUT PRESSURES ARE NORMAL. REF AMM 324003 INSPECTED BRAKE CONTROL VALVE. NO OBVIOUS DEFECTS OR BINDING NOTED. PERFORMED HIGH SPEED TAXI, COULD NOT FEEL ANY DRAGGING TO LEFT. REPLACED BRAKE AS A PRECAUTION PER JC 3240-301. (M)

Part: VSI INDICATOR — SHORTED (RT COCKPIT)

FIRST OFFICER'S VSI/TCAS INOP. REMOVED AND REPLACED VSI/TCAS IND IAW AMM. PERFORMED PITOT/STATIC LEAK CHECK IAW AMM. OPS CHECK AND LEAK CHECK GOOD. OK FOR SERVICE. (M)

Part: GEARBOX — FAILED (LT ENGINE)

SHUT DOWN LEFT ENGINE IN FLIGHT, DUE TO PROP GEARBOX FAILURE. INSTALLED SERVICEABLE PGB IAW GE MM. (M)

Part: LIGHT BULB — FAILED (CABIN)

WINDOW LIGHTS 8C NEON LIGHT STRIP SHORT CIRCUITED. AREA AROUND PLUG IN LOOKS BURNED. DEFERRED IAW MEL 33-20-1 AUTHORIZATION NR 10029. (M)

Part: SEAT TRACK — CORRODED (FS 638)

LAV CENTER SEAT TRACK FS 638 HAS MAJOR CORROSION DAMAGE LOWER FLANGE. CUT CENTER TRACK AT FS 620 REMITTING BACK TO FS 686 DRILLED UP NEW SEAT TRACK SECTION AND DOUBLER AND INSTALLED REPAIR PART IAW SRM 53-70-60. (Z)