N207SW

Part: BOOT — TORN (LT H/S DEICE SYS) · airframe 27,452 hrs · 33,827 cycles

RIGHT AND LEFT OUTBOARD STAB AND VERT FIN BOOTS INOP AFTER 28 SECONDS ON TIMERS 1 & 2. RETURNED TO DEN. REPLACED LEFT HORIZONTAL STAB DEICE BOOT IAW MM CHAPTER 30-10-01. OPS CHECK GOOD.

Part: RIB — DAMAGED (RUDDER) · airframe 27,155 hrs · 33,476 cycles

RIB IN RUDDER 1 DAMAGED JUST BELOW GREEN RUDDER ACTUATOR ATTACH POINT. DISCOVERED DURING C-CHECK. REPLACED DAMAGED RIB IAW 120 SRM 51-10-02.

Part: SENSOR — MALFUNCTIONED (ELEVATOR) · airframe 26,680 hrs · 32,875 cycles

TAKEOFF TRIM AURAL WARNING FAILURE. ABORTED TAKEOFF. REPLACED BOTH LEFT AND RIGHT ELEVATOR TRIM SENSORS. RAN BOTH ENGINES TO TAKEOFF POWER SETTINGS AND ALL TRIM SETTINGS IN GREEN BAND. OPS CHECK GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,708 hrs · 31,723 cycles

CRACK IN SKIN AROUND FWD CORNER OF RT SIDE COCKPIT SIDE WINDOW. DISCOVERED DURING ROUTINE LINE INSPECTION. INSTALLED REPAIR DOUBLER PER SB 120-053-0010.

Part: ACTUATOR — FAILED (T/E FLAP) · airframe 25,540 hrs · 31,522 cycles

AFTER TAKEOFF A FLAP DISAGREEMENT OCCURRED. TWO SEGMENTS OF THE INBOARD PAIR WERE ILLUMINATED AND 1 BAR OF THE NACELLE AND OUTBOARD PAIR FLASHED. DISAGREEMENT CLEARED AFTER SELECTING 15 DEGREES UP, BUT THEN AN INVALID ANALOG IND WAS DISPLAYED. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR IAW 27-50-08. OPS CHECK GOOD AT THIS TIME.

Part: SELECTOR SWITCH — MALFUNCTIONED (TE FLAPS) · airframe 24,958 hrs · 30,837 cycles

FLAPS WILL NOT MOVE WHEN 45 DEGREES IS SELECTED.REMOVED AND REPLACED FLAP SELECTOR LEVER IAW MM 27-50-01. OPS CHECK GOOD IAW 27-50-00.

Part: SWITCH — OUT OF ADJ (ENTRY DOOR) · airframe 23,885 hrs · 29,525 cycles

ON TAKEOFF FORWARD DOOR LIGHT BLINKED ON WITH WARNING. ADJUSTED THE MICROSWITCH FOR THE FORWARD DOOR LIGHT. OPS CHECK GOOD.

Part: PROXIMITY SENSOR — FAILED (ELEVATOR TRIM) · airframe 23,844 hrs · 29,479 cycles

ELEVATOR TRIM AURAL WARNING CONTINUOUS IN OR OUT OF TRIM. REMOVED AND REPLACED LEFT ELEVATOR TRIM PROXIMITY SENSOR WITH NEW IAW EMB MM 27-32-00. P/N 922AA2Y-A6P-Z722. ADJUSTED AND OPS CHECK GOOD.

Part: SPRING — LACK OF LUBE (ELEVATOR) · airframe 23,587 hrs · 29,150 cycles

ELEVATOR MOVEMENT PRODUCES ABNORMAL SOUNDS, SOUNDS LIKE CABLES PRANGING. LUBED ELEVATOR RETURN SPRING FWD ATTACH POINT. SYSTEM CHECK OK.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 23,274 hrs · 28,709 cycles

DESCENDING FROM FLIGHT LEVEL 260 CABIN ALTITUDE LIGHT ILLUMINATED ON THE MAP. LOST CONTROL OF CABIN ALTITUDE IN BOTH AUTO AND MANUAL MODES. MASKS DROPPED. PRESSURIZED AIRCRAFT ON GROUND IN MANUAL MODE. COULD NOT PRESSURIZE IN AUTO MODE. REMOVED AND REPLACED ELECTRONIC CONTROLLER IAW MM 21-30-01. OPS CHECKS GOOD. PN ON: 22201T011400 SNON: 493 SNOFF: 530

Part: SEQUENCE VALVE — FAILED (LT MLG) · airframe 23,162 hrs · 28,579 cycles

LEFT LANDING GEAR WOULD NOT RETRACT. REMOVED AND REPLACED LEFT MAIN GEAR OUTBOARD SEQUENCE VALVE IAW MM 32-32-07. CYCLED GEAR SEVERAL TIMES. OPS CHECK GOOD. P/N 120-32443-001

Part: WARNING SYSTEM — ACTIVATED (TAKEOFF TRIM) · airframe 23,162 hrs · 28,579 cycles

TAKEOFF TRIM ALARMED, ABORTED TAKEOFF. RAN BOTH ENGINES TO TEST TAKEOFF TRIM ALARM. TAKEOFF TRIM OPS CHECK GOOD. COULD NOT DUPLICATE DISCREPANCY.

Part: LANDING GEAR — CONTAMINATED (LEFT) · airframe 23,114 hrs · 28,523 cycles

LEFT LANDING GEAR WOULD NOT RETRACT. RETURNED TO COD. INSPECTED LEFT LANDING GEAR. CLEANED OFF SNOW AND ICE. SWUNG LANDING GEAR OVER 10 TIMES IAW 32-30-00. LANDING GEAR OPS CHECK GOOD AT THIS TIME.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 22,977 hrs · 28,362 cycles

ON CLIMBOUT CLACKER WARNING ACTIVATED FOR DURATION OF FLIGHT. RETURNED TO SLC. REPLACED STALL WARNING COMPUTER AND TESTED IAW MM 27-34-02. REPLACED STALL PANEL PER 27-34-00. OPS CHECKS GOOD. NO FAULTS FOUND. S/N ON: 489T, S/N OFF: 686. STALL PANEL S/N ON: MC 27-34-00.

Part: REGULATOR — FAILED (DEICE SYSTEM) · airframe 22,977 hrs · 28,362 cycles

RIGHT DUCT LEAK LIGHT ON INFLIGHT. FOLLOWED QRH AND LIGHT DID NOT GO OUT AFTER 3 MINUTES. SHUT DOWN RIGHT ENGINE AND RETURNED TO SLC. TROUBLESHOOT RIGHT BLEED AIR SYSTEM. REMOVED THE RIGHT DEICE AIR PRESSURE REGULATOR AND INSTALLED A SERVICEABLE REGULATOR. OPERATIONAL CHECKS OK IAW MM 30-10-06. P/N ON: 38E96-6A S/N: B2358.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 22,400 hrs · 27,701 cycles

DURING TAKEOFF ROLL, RECEIVED T6 WARNING BEFORE V1. ABORTED TAKEOFF. PERFORMED STATIC RUN UP AND RECEIVED T6 WARNING ON RIGHT ENGINE AT 90 PERCENT TORQUE WITH BLEEDS CLOSED. REMOVED AND REPLACED RIGHT ENGINE MM 71-00-00 RII 72-301. P/N ON: PW118B, S/N: 115714, S/N OFF: 115161.

Part: CONTROL BOX — FAILED (MLG) · airframe 22,296 hrs · 27,583 cycles

RED A SYSTEM GEAR LIGHTS ILLUMINATED DURING FLIGHT WITH GEAR UP. RETURNED TO SLC. REPLACED GEAR CONTROL BOX WITH SERVICEABLE ASSY, OPS CHECK GOOD IAW 32-60-00.

Part: SWITCH — FAILED (FUEL DOOR)

SERVICE DOOR LIGHT ILLUMINATED IN FLIGHT. RETURNED TO PSP. INSPECTED FUEL DOOR SWITCH, AVIONICS BAY SWITCH AND RIGGING DOOR SWITCH. ALL SWITCHES CHECK GOOD. COULD NOT DUPLICATE DISCREPANCY.

Part: SWITCH — DAMAGED (HYD SYSTEM)

GREEN SYSTEM MAIN PUMP LOW PRESSURE LIGHT AND LOW LEVEL LIGHT ILLUMINATED WITHIN A FEW SECONDS OF EACH OTHER. QUANTITY INDICATOR FOR GREEN SYSTEM INDICATED EMPTY. RETURNED TO SALT LAKE, LEFT HYDRAULIC PRESSURE SWITCH FOUND BLOWN APART. REMOVED AND REPLACED PRESSURE SWITCH IAW SMB120 MM 293006. OPS AND LEAK CHECK GOOD.

Part: FILTER — DIRTY (RIGHT)

RIGHT HYDRAULIC FILTER LIGHT ILLUMINATED. RETURNED TO SLC. REPLACED HIGH AND LOW PRESSURE FILTERS ON RIGHT PACK. OPS AND LEAKS CHECK GOOD.

Part: HYD SYST — REQD SERVICE (LT HYD SYST)

SHORTLY AFTER TAKEOFF REACHING CRUISE ALTITUDE THE LEFT HYDRAULIC RESERVOIR LOW PRESSURE LIGHT CAME ON AND WAS ACCOMPANIED BY A FLUID QUANTITY INDICATION IN MID GREEN ARC. WITHIN 5 MINUTES THE RIGHT LOW PRESS CAME ON. BOTH REMAINED TO 15,000 FEET. INSPECTED BOTH HYDRAULIC GREEN AND BLUE. FOUND FLUID QUANTITY IN GREEN SERVICED IAW 12-13-01 AND PURGE IAW 29-12-00. BOTH OPS CHECK GOOD AT THIS TIME.

Part: ACTUATOR — FAILED (RT TE FLAP)

NACELLE FLAP DISAGREEMENT AT 2 BARS ON DEPARTURE. RETURNED TO SLC. REPLACED RIGHT NACELLE FLAP ACTUATOR IAW MM 27-50-08 AND OPS CHECKS GOOD.

Part: ACTUATOR — MALFUNCTIONED (RT TE FLAP)

UNABLE TO RETRACT FLAPS, DISAGREEMENT. RETURNED TO SLC. REMOVED AND REPLACED RIGHT WING INBOARD FLAP ACTUATOR, OPS CHECKS GOOD.

Part: TQ SENSOR — MALFUNCTIONED (RT ENGINE)

AFTER TAKEOFF RIGHT TORQUE GAUGE OSCILLATED BETWEEN 40 PERCENT AND 100 PERCENT AND THEN FEATHERED INADVERTENTLY. RETURNED TO FIELD, REMOVED AND REPLACED TORQUE SENSOR ON RIGHT ENGINE, IAW EMB MM 76-11-02. REMOVED AND REPLACED RIGHT ENGINE HMU IAW MM 73-21-00 AND RII 73-301-IAW. OPS CHECK AND LEAK CHECK GOOD.

Part: AHRS COMPUTER — MALFUNCTIONED (NR 1)

CAPTAINS ATTITUDE DISPLAY FAILED. RETURNED TO FIELD. REPLACED NR 1 AHRS COMPUTER. OPS CHECKS GOOD.

Part: CLAMP — LOOSE (RT ENGINE)

RIGHT ENGINE AIR INLET DE-ICE INOP. RETURNED TO FIELD AFTER TAKEOFF. TIGHTENED CLAMP ON RIGHT ENGINE INLET DE-ICE BOOT SUPPLY LINE, OPS CHECKS GOOD.

Part: HOSE — CHAFED (RT OIL COOLER)

AT CRUISE ALTITUDE, RIGHT OIL PRESSURE DROPPED TO 40 PSI. PERFORMED PRECAUTIONARY ENGINE SHUT DOWN ON RIGHT ENGINE. REMOVED AND REPLACED UPPER HOSE ASSY ON RIGHT OIL COOLER. OPS CHECK AND LEAK CHECKS GOOD AT THIS TIME.

Part: SEAL — LOOSE (CARGO DOOR)

CLIMBING THROUGH 24,000 FEET, CABIN ALTITUDE LIGHT CAME ON. TESTED ALTITUDE WARNING SWITCH SYSTEM IAW MM 21-30-08. SYSTEM OPERATION CHECKS GOOD. FOUND CARGO DOOR SEAL PULLED OUT. REINSTALLED SEAL AS NEEDED. PRESSURIZED AIRCRAFT. CARGO DOOR LEAK CHECK GOOD.

Part: BLADE TIP — DAMAGED (RT PROP)

VIBRATION ON CLIMB-OUT FROM SLC, FOUND RT PROPELLER DAMAGED, ALL ENGINE PARAMETERS WERE NORMAL FOR TAKEOFF AND CLIMB. FOUND DAMAGED TO NR TWO BLADE TIP. PROPELLER REMOVED FROM SERVICE.

Part: OIL SYST — REQD SERVICE (RT ENGINE)

AFTER ROTATION, RT OIL PRESSURE FLUCTUATED TO AROUND 40 PSI AND OIL AURAL WARNING SOUNDED. OIL PRESSURE IMMEDIATELY RETURNED AND MAINTAINED NORMAL PSI. SERVICED RT ENGINE OIL, 3 QTS. INSPECTED ENGINE, NO LEAKS FOUND. FILTER BYPASS PINS NOT POPPED, TRANSMITTER WIRING AND CANNON PLUG OK. PERFORMED ENGINE RUN UP, OIL PRESSURE INDICATION NORMAL.

Part: REG VLV GASKET — FAILED (RT DE-ICE)

FIVE MINUTES AFTER TAKEOFF USING ONLY APU BLEED X FEED TO BOTH PACS, RT DUCT LEAK LIGHT, ILLUMINATED, TURNED OFF X FEED AND RT PAC, STARTED TIME AS PER CHECK LIST, AFTER 3 MINUTES BEGAN PRECAUTIONARY ENGINE SHUT DOWN CHECK LIST WITH ENGINE AT FLIGHT IDLE AS RT ENGINE PROP WAS FEATHERED, DUCT LIGHT WENT OUT. TROUBLESHOT SYSTEM, FOUND GASKET FOR RT DEICE PRESSURE REGULATING VALUE BLOWN, INSTALLED NEW GASKET, RAN ENGINE, OPS CKS GOOD.

Part: HYD PUMP — FAILED (RT ENGINE)

LOST ALL HYDRAULIC PRESSURE IN FLIGHT, LOW PRESSURE ELECTRICAL STANDBY FAILED TO OPERATE. REPLACED A BROKEN RETURN LINE AT ENGINE PUMP IN THE LEFT HYDRAULICS BAY. REMOVED AND REPLACED RIGHT ENGINE HYDRAULIC PUMP. OPERATIONALLY AND LEAK CHECKS GOOD. DECONTAMINATION COMPLIED WITH IN ACCORDANCE WITH EMB 120 MM 20-00-02. ALL SYSTEMS OPERATIONALLY CHECK GOOD ON BLUE HYDRAULIC SYSTEM.

Part: WHEEL — CRACKED (MLG)

NR 1 MAIN WHEEL CRACKED. REMOVED AND REPLACED NR 1 MAIN WHEEL ASSY. SEE FL 73942 FOR MECH SIGN OFF.