N214SW

Part: ACTUATOR — MALFUNCTIONED (RUDDER) · airframe 30,424 hrs · 39,557 cycles

RT RUDDER JAMMED AFTER TAKEOFF. REPLACED BOTH RUDDER ACTUATORS IAW MM 27-22-02. OPERATIONAL CHECK GOOD, PN 308140-1003, SN/OFF 0165 SN/OFF 0671.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAP) · airframe 29,741 hrs · 38,739 cycles

ABOVE 160 KTS DURING FLAP RETRACTION OUTBOARD FLAPS DISAGREE (FLAP ON MAP, DISAGREEMENT ON OVERHEAD). REPLACED FLAP CONTROL UNIT IAW A/C MM 27-50-06, OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAP) · airframe 29,716 hrs · 38,708 cycles

FLAP CONTROL FAULT ON CLIMB-OUT. REPLACED THE FLAP CONTROL UNIT. OPERATIONAL CHECK GOOD IAW MM 27-50-00.

Part: ANNUNCIATOR — MALFUNCTIONED (TE FLAPS) · airframe 29,614 hrs · 38,587 cycles

ON CLIMB-OUT, GOT A FLAP DISAGREEMENT INDICATION. REPLACED FLAP ANNUNCIATOR PANEL IAW EMB 120 MM 27-50-00. OPERATIONAL CHECK GOOD, PN ON 306900-1017; PN OFF 347100-1001; SN ON 0015; SN OFF 0089.

Part: SIGN — INOPERATIVE (CABIN) · airframe 28,999 hrs · 37,853 cycles

RED EMERGENCY FLOOR LIGHTS IN GALLEY INOPERATIVE. REPLACED RED EMERGENCY SIGN AT THE GALLEY FLOOR. OPERATIONAL CHECK GOOD.

Part: DOOR — BINDING (MAIN PAX) · airframe 28,684 hrs · 37,438 cycles

MAIN CABIN DOOR VERY HARD TO OPEN AND CLOSE. ADJUSTED AND RIGGED PAX DOOR BACKSTOP SHIMS IAW EMB 120 MM 52-11-00.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 28,684 hrs · 37,438 cycles

AFT SECTION EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED LIGHT BATTERY PACK FOR AFT SECTION. OPERATIONAL CHECK GOOD.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 29,078 hrs · 37,956 cycles

THERE IS CORROSION ON BUTT STRAP JUST AFT OF PAX DOOR ENTRANCE. ITEM FOUND AT C-CHECK INSPECTION. REPLACED AFFECTED BUTT STRAP AND SECURED SAME IAW EMB 120 MM 51-10-02 PG 3 SEC 3A.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,979 hrs · 36,500 cycles

PASSENGER ENTRY OVERHEAD EMERGENCY LIGHT DOES NOT ILLUMINATE. RELAMPED PASSENGER ENTRY OVERHEAD EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 27,523 hrs · 35,902 cycles

LT STALL WARNING LIGHT CAME ON IN FLIGHT. REMOVED AND REPLACED LT NR 1 STALL WARNING COMPUTER. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 27,220 hrs · 35,521 cycles

AFTER LANDING SELECTED FLAPS UP, RECEIVED A CONTROL FAULT ON OUTBOARD FLAPS. REMOVED AND REPLACED FLAP ACTUATOR IAW AMM 27-50-00. REPAIRED PIN 4 AT CONNECTOR P1867. REMOVED AND REPLACED FCU IAW 27-50-00 AND OPERATIONAL CHECKED GOOD IAW 27-50-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,100 hrs · 35,375 cycles

FORWARD EMERGENCY RED LIGHT STRIP ON FLOOR INOP. REPLACED FORWARD EMERGENCY LIGHT STRIP ON FLOOR WITH SERVICEABLE UNIT. OPS CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 27,100 hrs · 35,375 cycles

LEFT CAPTIANS SIDE WINDOW CRACKED ON GROUND. REMOVED AND REPLACED LEFT SIDE WINDSHIELD IAW MM 56-10-01. PN: NP151311-1, S/N OFF: 00108.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,887 hrs · 35,113 cycles

EMERGENCY LIGHT AT PAX DOOR CEILING IS INOP. REMOVED AND REPLACED LAMP. OPS CHECK GOOD. P/N: 209.

Part: CONTROL PANEL — MALFUNCTIONED (STALL WARNING) · airframe 26,603 hrs · 34,765 cycles

STALL WARNING LIGHT ILLUMINATES ON THE MAP. REMOVED AND REPLACED STALL PANEL. OPS CHECKS GOOD.

Part: SWITCH — FAILED (CABIN PRESSURE) · airframe 26,406 hrs · 34,528 cycles

DURING CRUISE FLIGHT AT 27,000 FT, HAD A PRESSURE POP AND THEN A CABIN ALT WITH TRIPLE CHIME. PERFORMED PRECAUTIONARY EMERGENCY DESCENT TO 10,000 FT AT THAT POINT, WENT TO QRH. FOLLOWED PROCEDURE FOR LOSS OF CABIN PRESSURE. WENT TO MANUAL MODE ON PRESSURIZATION CONTROL AND WAS ABLE TO CONTROL CABIN. CONTINUED TO SLC AND LANDED WITHOUT INCIDENT. REPLACED AUTO-MAN DAMP SWITCH. OPS CHECK GOOD IAW 20-13-03 AND 21-30-00.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 25,501 hrs · 33,396 cycles

FORWARD EMERGENCY LIGHT (INOPERATIVE). RECONNECTED BOTH POWER LEADS AT FORWARD (EXIT) SIGN. OPS CHECK GOOD.

Part: CHANNEL — CRACKED (LT NACELLE) · airframe 25,501 hrs · 33,396 cycles

LT MLG INSIDE WELL FORWARD OUTBOARD CRACK ON NACELLE. (DISCOVERED DURING C-CHECK INSPECTION) LT MLG OUTBOARD CHANNEL REPLACED SRM120 51-10-02.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 25,298 hrs · 33,113 cycles

EMERGENCY LIGHTS IN ROW 9 COME ON MOMENTARILY AND THEN GO OUT. REMOVED AND REPLACED EMERGENCY BATTERY PACK NR 4 IAW MM 33-50-02. OPS CHECK GOOD.

Part: CHANNEL — CRACKED (T/E FLAP) · airframe 25,075 hrs · 32,851 cycles

AFTER DEPARTURE THE FLAPS WOULD NOT RETRACT PAST APPROXIMATELY 10 DEGREES. RECEIVED FLAP DISAGREEMENT WITH THE OUTBOARD FLAPS INDICATING APPROXIMATELY 10 DEGREES. FOUND THE LEFT OUTBOARD FLAP LOWER CHANNEL CRACKED AT INBOARD END [ROLLER BRACKET ATTACH POINT]. REMOVED CHANNEL AND REPAIRED IAW 51-70-02. REINSTALLED CHANNEL, RAN FLAPS. OPS CHECK GOOD.

Part: PANEL — MALFUNCTIONED (FLAP ANNUNCIATOR) · airframe 25,040 hrs · 32,807 cycles

AFTER TAKEOFF, OUTBOARD FLAPS WOULD NOT COMPLETELY RETRACT AND FLAP DISAGREEMENT INDICATED. QRH, RECYCLED AND WOULD NOT CORRECT. FLAPS CAME DOWN FINE BUT WILL NOT RETRACT IN AIR. ON GROUND THEY RETRACT COMPLETELY. REMOVED AND REPLACED FLAP ANNUNCIATOR PANEL WITH SERVICEABLE UNIT IAW MM 27-50-05. OPS CHECKS GOOD.

Part: FLAP TRACK — DAMAGED (TE FLAPS) · airframe 25,010 hrs · 32,765 cycles

AFTER DEPARTURE FLAPS WOULD NOT RETRACT PAST 10 DEGREES. FLAP DISAGREEMENT WITH THE OUTBOARD FLAPS INDICATING 10 DEGREES. RETURNED TO FIELD. REPLACED RIGHT OUTBOARD FLAP INNER FIXED TRACK IAW EMB MM 57-53-03. INSTALLED SERVICEABLE TRACK ON RIGHT WING, OUTBOARD FLAP AT OUTBOARD POSITION.

Part: SWITCH — STUCK (AUTOFEATHER SYS) · airframe 25,007 hrs · 32,761 cycles

PILOT REPORTS THAT RIGHT ENGINE AUTO FEATHERED ON TAKEOFF ROLL WITH LT ENGINE TQ FLUCTUATION, BUT ENGINE DID NOT FOLLOW FLUCTUATION. FOUND LEFT ENGINE AUTO FEATHER TEST SWITCH STUCK IN THE TEST POSITION. REMOVED AND REPLACED SWITCH. RAN A/C, OPS CHECKED GOOD.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 24,981 hrs · 32,731 cycles

FLAPS WILL NOT RETRACT FULLY. OUTBOARD FLAPS REMAIN AT ABOUT 10 DEGREES. RETURNED TO SLC. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR WITH SERVICEABLE PART IAW MM 27-50-09. OPS AND LEAK CHECK GOOD.

Part: STRINGER — CRACKED (LEFT WING) · airframe 24,980 hrs · 32,730 cycles

CRACKED STRINGER LEFT INBOARD WING LOWER SURFACE AFT OF INBOARD FUEL CELL ACCESS PANEL. FOUND DURING A CHECK INSPECTION. COMPLIED WITH WING STRINGER REPAIR AT LEFT INBOARD WING LOWER SURFACE STRINGER NR 8 AT RIB NR 5 PER SRM 57-20-03.

Part: FLAP TRACK — WORN (RT WING) · airframe 24,868 hrs · 32,588 cycles

FLAP DISAGREEMENT AFTER TAKEOFF. OUTBOARD PAIR WOULD NOT RETRACT TO LESS THAN 10 DEGREES, OTHER PAIRS RETRACTED PROPERLY. APPLIED QRH PROCEDURE 3 TIMES, FAILED ALL 3 TIMES. FLAPS EXTENDED TO 25 DEGREES PROPERLY FOR LANDING, THEN RETRACTED PROPERLY TO 0 DEGREES AFTER LANDING. REMOVED AND REPLACED RIGHT OUTBOARD FLAPS OUTBOARD MOVEABLE TRACK AND ROLLERS. OPS CHECK GOOD IAW MM 27-50-02.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 24,857 hrs · 32,576 cycles

IN FLIGHT CLIMBING THROUGH 7,000 FEET, THE FLAP DISAGREEMENT LIGHT ILLUMINATED. COULD NOT CLEAR VIA QRH. RETURNED TO SLC. INSPECTED FLAPS. NO DEFECTS FOUND. PERFORMED FLAP FUNCTIONAL CHECKS IAW MM 27-50-00. OPERATIONAL CHECKS SATISFACTORY. NO DEFECTS NOTED AT THIS TIME.

Part: CONNECTOR — CONTAMINATED (TE FLAPS) · airframe 24,661 hrs · 32,344 cycles

FLAP DISAGREEMENT ON FLAP RETRACTION ON TAKEOFF, OUTBOARD FLAPS. RETURNED TO SLC. INSPECTED OUTBOARD FLAPS CONNECTORS, FOUND GLYCOL IN LEFT OUTBOARD CONNECTOR. CLEANED LEFT OUTBOARD CONNECTOR AND RAN FLAPS 10 CYCLES. OPS CHECK GOOD. NO FAULTS AT THIS TIME.

Part: CONNECTOR — WORN (LEFT OB FLAP) · airframe 24,387 hrs · 32,006 cycles

FLAPS WOULD NOT RETRACT, DISAGREEMENT WITH THE OUTBOARD PAIRS, WOULD NOT CORRECT. FOUND LEFT OUTBOARD FLAP CONNECTOR TO HAVE FLUID INSIDE AND WORN BACKSHELL. REPLACED CANNON PLUG AND BACKSHELL. APPLIED SUPER CORR-B TO CANNON PLUG AND CONNECTORS. OPS CHECK OF FLAP SYSTEM GOOD IAW 20-50-00 AND 27-50-00.

Part: SIGNAL COND UNIT — MALFUNCTIONED (RT ENGINE) · airframe 24,186 hrs · 31,777 cycles

NR 2 PROPELLER FEATHERED WHEN TAKEOFF POWER APPLIED. TORQUE REACHED 125 PERCENT INSTANTANEOUSLY. NP 18.9 PERCENT WHEN POWER BROUGHT BACK TO IDLE. REPLACED RIGHT ENGINE TORQUE SIGNAL CONDITIONER IAW EMB MM 77-11-01. OPERATIONAL CHECKS GOOD. REPLACED NR 2 ENGINE PROP ASSEMBLY IAW EMB 120 MM 61-10-03.

Part: CONNECTOR — CONTAMINATED (LT TE FLAP ACT) · airframe 24,186 hrs · 31,777 cycles

AFTER TAKEOFF, RECEIVED A FLAP DISAGREEMENT WITH 2 BARS ON OUTBOARD FLAPS, AND ALL LIGHTS ON THE 10 DEGREE LINE FLASHING. RESET AS PER QRH. RESET NOT SUCCESSFUL. RETURNED TO LAX. FOUND LT OUTBOARD FLAP ACTUATOR CONNECTOR PLUG CONTAMINATED WITH MOISTURE. CLEANED AND DRIED AS NEEDED. OPERATED FLAPS AND GROUND CHECKS GOOD.

Part: CONNECTOR — CONTAMINATED (FLAP ACTUATOR) · airframe 24,089 hrs · 31,629 cycles

FLAP DISAGREEMENT THAT WOULD NOT CLEAR AFTER TAKEOFF. RETURNED TO SLC. DEICE FLUID FOUND IN OUTBOARD FLAP ACTUATOR CONNECTOR PLUGS. CLEANED CONNECTOR PLUGS. OPS CHECK GOOD AT THIS TIME.

Part: ANNUNCIATOR — MALFUNCTIONED (TE FLAPS) · airframe 24,075 hrs · 31,611 cycles

FLAP DISAGREEMENT ON TAKEOFF. RECYCLED 3 TIMES - UNSUCCESSFULLY. FLAP DISAGREEMENT ON OUTBOARD PAIR DURING RETRACTION. RETURNED TO DEN. CLEANED AND INSPECTED FLAP TRACKS AND RERACKED FCU. INSTALLED SERVICEABLE FLAP ANNUNCIATOR. OPERATED FLAPS SEVERAL TIMES. NO DEFECTS NOTED. OPS CHECK GOOD.

Part: GCU — MALFUNCTIONED (NR 1) · airframe 23,871 hrs · 31,371 cycles

CAPTAIN'S EHSI WENT BLANK ON TAXI OUT. REPLACED GCU NR 1 (AUX GEN NR 1) IAW MM 24-30-02. CHECKED OPERATION OF POWER TRANSFER AT NP 70 PERCENT WITHOUT OBSERVING ANY ANOMALIES ON EHSI NR 1. CHECKS GOOD. PARALLELED AUX GEN'S IAW MM 24-30-02 ALL OPS CHECK GOOD AT THIS TIME.

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 23,871 hrs · 31,371 cycles

FO'S EHSI FAILED DURING TAXI AND IN FLIGHT. EHSI SHOWS YELLOW FAIL FLAG AND HEADING FLAG. SUCCESSFULLY RESET BOTH TIMES. REPLACED FO'S HDG74. OPERATIONAL CHECK OF EHSI GOOD.

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 23,804 hrs · 31,276 cycles

CAPT'S EHIS FAILED AFTER TAKEOFF. RETURNED TO FIELD. REMOVED AND REPLACED THE NR 1 HPU WITH A SERVICEABLE UNIT. OPS CHECK GOOD.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 23,497 hrs · 30,889 cycles

RIGHT ENGINE AUTO FEATHERED ON THE TAKEOFF ROLL. ABORTED THE TAKEOFF. PERFORMED TWO TAKEOFF POWER RUNS, ALL CHECKS NORMAL.

Part: CONNECTOR — LOOSE (STICK SHAKER) · airframe 23,254 hrs · 30,624 cycles

FIRST OFFICER'S STICK SHAKER NOT WORKING ON FIRST FLIGHT OF THE DAY CHECK. FOUND CONNECTOR LOOSE ON SHAKER UNIT. TIGHTENED CONNECTOR. OPS CHECK PER 27-60-00 GOOD.

Part: FLAP — MALFUNCTIONED (WING) · airframe 23,190 hrs · 30,544 cycles

FLAP DISAGREEMENT IN FLIGHT. RETURNED TO SLC. PERFORMED OPS CHECKS IAW 27-50-00. COULD NOT DUPLICATE DISCREPANCY.

Part: RELAY — FAILED (AUTO FEATHER) · airframe 23,210 hrs · 30,571 cycles

UPON ADDING POWER ON TAKEOFF, LEFT TORQUE GAUGE WOULD NOT GO ABOVE 75PERCENT, THEN AURAL AUTO FEATHER WARNING SOUNDED AND THE RIGHT ENGINE FEATHERED. UPON PULLING BACK POWER TO GROUND IDLE BOTH SIDES (ABORT), LEFT TORQUE GAUGE REMAINED AT 75 PERCENT AND RIGHT PROPELLER REMAINED FEATHERED. AFTER TURNING OFF AUTO FEATHER SWITCH, BOTH TORQUE INDICATORS NORMAL AND RIGHT PROP ON FEATHER. FDR DOWNLOAD INFORMATION INDICATED THE LEFT ENGINE AUTO FEATHER WAS STUCK IN THE TEST MODE, KEEPING LEFT TORQUE INDICATING 75 PERCENT AND RIGHT ENGINE PROPELLER IN FEATHER. REMOVED AND REPLACED AUTO FEATHER TEST RELAY M8353616-022M. OPS CHECKS GOOD.

Part: INDICATOR — ERRATIC (COCKPIT) · airframe 23,190 hrs · 30,544 cycles

LEFT ENGINE T6 GAUGE ERRATIC. RETURNED TO DEN. REPLACED LEFT T6 GAUGE. OPS CHECK GOOD.

Part: FASTENER — LOOSE (FUEL DOOR) · airframe 22,897 hrs · 30,202 cycles

ABORTED TAKEOFF AT 60 KIAS DUE TO A MAP RED DOOR LIGHT ILLUMINATING. FOUND CAMLOCK ON FUEL SERVICE DOOR UNSECURED. SECURED CAMLOCK ON FUEL DOOR. OPS CHECK GOOD. ALL PANELS SECURED.

Part: ACTUATOR — LEAKING (PAX DOOR) · airframe 22,599 hrs · 29,852 cycles

AT 1000 FT AGL AND 10 DEGREES BANK TO THE RIGHT (AFTER TAKEOFF), THE GREEN SYSTEM RESERVOIR LOW LEVEL LIGHT ILLUMINATED WITH HYD ON MAP. THE FLUID QUANTITY NEEDLE REGISTERED IN THE YELLOW ARC. THE LIGHTS EXTINGUISHED SOON AFTER WINGS LEVELED AND THE FLUID QUANTITY NEEDLE STABILIZED JUST ABOVE THE YELLOW ARC FOR THE REMAINDER OF THE FLIGHT. THE GEAR WAS UP AND FLAPS AT 15 DEGREES WHEN AMBER LIGHTS FIRST ILLUMINATED. RETURNED TO DEN. FOUND THE FORWARD PASSENGER DOOR FORWARD ACTUATOR LEAKING. REMOVED AND REPLACED WITH SERVICEABLE UNIT. OPS CHECKS GOOD.

Part: DETECTOR — MALFUNCTIONED (ICE PROTECTION) · airframe 22,599 hrs · 29,852 cycles

ICE MONITOR FAILED INFLIGHT. RETURNED TO DEN. CYCLED CIRCUIT BREAKER. OPS CHECKED GOOD.

Part: WIRE HARNESS — DEFECTIVE (RT MLG) · airframe 22,376 hrs · 29,581 cycles

RT MAIN LANDING GEAR -A- DISAGREEMENT LIGHT ILLUMINATED DURING FLIGHT. ALL -B- LIGHTS FUNCTION NORMAL. REMOVED AND REPLACED -A- UPLOCK HARNESS WITH SERVICEABLE HARNESS. OPS CHECKS GOOD.

Part: TARGET — OUT OF ADJUST (RT MLG) · airframe 22,348 hrs · 29,550 cycles

RIGHT GEAR LIGHTS RED A & B WOULD NOT EXTINGUISH WHEN GEAR RETRACTED. CYCLED 3 TIMES. INSPECTED RT MAIN GEAR. FOUND UPLOCK HOOK ADJUSTED OUT, PLUS ICE BUILD UP ON HOOK. ADJUSTED UPLOCK PROX TARGET. C/W GEAR SWING. OPS CHECKS GOOD.

Part: CONNECTOR — CONTAMINATED (T/E FLAP) · airframe 22,304 hrs · 29,499 cycles

ON TAKEOFF, DURING FLAP RETRACTION, RECEIVED A FLAP DISAGREEMENT. FOLLOWED QRH AND FLAPS RETRACTED NORMALLY. COULD NOT DUPLICATE ON GROUND. INSPECTED FLAPS, TRACKS, ACTUATORS AND FOUND LEFT OUTBOARD FLAP CANNON PLUG WET. CLEANED AND RESECURED. OPS CHECKS GOOD WITH NO DISCREPANCIES.

Part: FRAME — CRACKED (LT & RT NACELLE) · airframe 21,601 hrs · 28,698 cycles

RIGHT AND LEFT NACELLE NR 1 FRAMES CRACKED. REPLACED BOTH NACELLE NR 1 FRAMES IAW EMB120 SRM 51-10-02 AND SB 120-54-0036.

Part: FCU — MALFUNCTIONED (T/E FLAP) · airframe 21,594 hrs · 28,688 cycles

ON CLIMBOUT RECEIVED A FLAP DISAGREEMENT AND FLAPS WOULD NOT FULLY RETRACT. RETURNED TO FAT. AIRCRAFT IN FOR C CHECK INSPECTION. DETAILS FORTHCOMING. UPDATE: PULLED FCU, MEGGED WIRES TO BOTH INBOARD FLAP ACTUATORS. NO DEFECTS NOTED. CHECKED ANNUNCIATORS FOR ANY FAULT CODES. RERACKED FCU. OPS CHECKED FLAP WITH NO FURTHER FAULTS NOTED AT THIS TIME.

Part: EEC — MALFUNCTIONED (LT ENGINE) · airframe 21,537 hrs · 28,613 cycles

ABORTED TAKEOFF IN WYS DUE TO LEFT ENGINE SURGE +/- 45 PERCENT. PERFORMED ENGINE RUNS. DEFERRED LEFT EEC.RAN LEFT ENGINE TO TAKEOFF POWER WITH NO FLUCTUATIONS NOTED. ALL CHECKS GOOD AT THIS TIME.

Part: INDICATOR — MALFUNCTIONED (TE FLAPS) · airframe 21,537 hrs · 28,613 cycles

WHEN RETRACTING FLAPS AFTER DEPARTURE FROM EKO GOT A FLAP DISAGREEMENT. THE PROBLEM CORRECTED ITSELF BUT TOOK ABOUT TWO MINUTES.CLEANED TRACKS. OPERATED FLAPS SEVERAL TIMES. ALL INDICATIONS NORMAL. FLAPS OPS CHECK GOOD.

Part: WARN PANEL — MALFUNCTIONED (COCKPIT) · airframe 19,960 hrs · 26,762 cycles

ON TAKEOFF ROLL RECEIVED HIGH SPEED AURAL WARNING THROUGH 80 KNOTS. ABORTED TAKEOFF. PERFORMED INSULATION TEST ON ALL WIRES IN HIGH SPEED WARNING SYSTEM. WIRES CHECK GOOD. REMOVED AND REPLACED AURAL WARNING UNIT WITH SERVICEABLE UNIT IAW 31-53-02. HIGH SPEED WARNING ONLY SOUNDS AT PROPER SPEED. OPS CHECK GOOD. P/N: 80-0557-11, S/N ON: 0472, S/N OFF: 0405.

Part: WARNING SYSTEM — FALSE INDICATION (PITOT STATIC) · airframe 19,900 hrs · 26,694 cycles

HIGH SPEED AURAL WARNING UPON APPLICATION OF TAKEOFF POWER. PRESSURIZED PITOT STATIC SYSTEM USING TEST BOX THROUGH ENTIRE AIRSPEED RANGE IAW MM 34-17-01. AURAL WARNING OPS CHECKS GOOD. RAN BOTH ENGINES AT TAKEOFF POWER IN TAKEOFF CONFIGURATION WITH NO HIGH SPEED WARNINGS. AURAL WARNING SYSTEM OPS CHECKS GOOD.

Part: PROBE — MALFUNCTIONED (LEFT ENGINE) · airframe 19,426 hrs · 26,128 cycles

LEFT TORQUE GAUGE FLUCTUATES BOTH ANALOG AND DIGITAL. RETURNED TO FIELD. REMOVED AND REPLACED LEFT ENGINE TORQUE PROBE. P/N 3116942-01, S/N ON MM1660 OFF MM 1751. ALSO REMOVED AND REPLACED THE LEFT ENGINE TORQUE INDICATOR. P/N SEDL-OC2R, S/N ON: 918, S/N OFF: 1094. WORK PERFORMED IAW P&W MM 77-00-00. OPS CHECKS GOOD.

Part: ACTUATOR — MALFUNCTIONED (RUDDER) · airframe 17,569 hrs · 23,995 cycles

AFTER TAKEOFF ABOVE 120 KIAS, FOUND RUDDER UNPOWERED AND NO RUDDER INOP LIGHTS WERE ILLUMINATED, NO MAP LIGHT EITHER. RETURNED TO LAX. REPLACED RELAY K0318, GROUND TESTED RUDDER, OPS CHECKS GOOD.

Part: SWITCH — OUT OF ADJUST (FUEL DOOR)

SERVICE DOOR LIGHT INFLIGHT. RETURNED TO LAX. ADJUSTED FUEL DOOR MICROSWITCHES. OPS CHECKS GOOD.

Part: AIRSPEED IND — STUCK (RIGHT COCKPIT)

FIRST OFFICER'S AIRSPEED INDICATOR STUCK AT 64 KNOTS. RETURNED TO LAX. REPLACED FIRST OFFICER'S AIRSPEED INDICATOR. OPS AND LEAK CHECK GOOD.

Part: OIL SYST — REQD SERVICE (LT & RT ENGINE)

OIL AURAL WARNING AT V1 FOLLOWED WITHIN 30 SECONDS BY OIL PRESSURE FLUCTUATION BELOW GREEN ON RIGHT ENGINE. RETURNED TO FIELD. SERVICED BOTH ENGINES WITH 2 QUARTS OIL EACH. PERFORMED ENGINE RUN ON BOTH ENGINES. OIL PRESSURE INDICATION STEADY.

Part: SWITCH — FAILED (LT DEICE BOOT)

CLIMBING THROUGH 5,000 FEET, LEFT OUTBOARD AND MIDDLE LEADING EDGE DE-ICE FAILURE. RECYCLED PER QRH BETWEEN TIMER 1 AND 2 WITH 5 SECONDS DELAY. THEN FAILURE OF LEFT OUTBOARD LEADING EDGE AND VERTICAL FIN DEICE. RETURNED TO FIELD. REPLACED LEFT MIDDLE AND LEFT OUTBOARD DE-ICE BOOT PRESSURE SWITCHES. OPS CHECKS GOOD.

Part: DUCT LIGHT — ILLUMINATED (LT ENGINE)

LEFT ENGINE BLEED DUCT LEAK ON IN FLIGHT. SCENARIO B IN QRH LEFT ENGINE SHUTDOWN IN FLIGHT. PERFORMED LEAK CHECK OF LEFT ENGINE BLEED AIR SYSTEM WITH ENGINE AND SHOP AIR. COULD NOT DUPLICATE PROBLEM. OPS CHECK GOOD.

Part: FILTERS — DIRTY (TE FLAPS)

AFTER TAKEOFF, WE HAD A FLAP DISAGREEMENT LIGHT. PERFORMED ABNORMAL CHECKLIST AND RETURNED TO LAX. INSPECTED AND CLEANED OUTBOARD FLAP ACTUATOR LINE FILTERS (BOTH LEFT AND RIGHT). PERFORMED OPS CHECKS OF FLAP SYSTEM. OPS CHECKS GOOD.

Part: CONNECTORS — DIRTY (TE FLAPS)

AFTER TAKEOFF, ATTEMPTED FLAPS UP. DISAGREEMENT FLAP LIGHT ILLUMINATED (OUTBOARD WAS AGREEING BUT NOT THE NACELLE AND INBOARD). REFERED TO QRH HOWEVER UNSUCCESSFUL. RETURNED TO LAX. CLEANED CANNON PLUGS ON OUTBOARD FLAPS AND RECHECKED FLAP CONTROL UNIT. OPERATED FLAPS NUMEROUS TIMES. OPS CHECKS GOOD.

Part: HYD PUMP — FAILED (LT ENGINE)

AFTER TAKEOFF DURING GEAR RETRACTION, LEFT MAIN HYDRAULIC PUMP FAILED. RETRY FAILED. RETURNED AND LANDED AT SLC. REMOVED AND REPLACED LEFT ENGINE DRIVEN HYDRAULIC PUMP. CHANGED HYDRAULIC FILTER ON LEFT PACK, FOUND NO CONTAMINATION. OPS CHECKS AND LEAKS CHECKS GOOD IAW MM 29.

Part: LUMINAIRE — BURN DAMAGE (LAMP HOLDER)

ULTRALIGHT LIGHTING SYSTEM FROM SKYWEST RETURNED FOR 'BROKEN END'. BURN DAMAGE AT LAMP HOLDER NOTED AT INITIAL INSP.

Part: CONTROL BOX — FAILED (LANDING GEAR)

LANDING GEAR WOULD NOT RETRACT. REPLACED LANDING GEAR CONTROL BOX, DID SEVERAL GEAR SWINGS AND OPS CHECK GOOD.

Part: IND BULBS — FAILED (NLG)

NO GREEN LIGHTS ON NOSE GEAR ILLUMINATED WITH GEAR HANDLE DOWN. REPLACED BULBS IN NOSE DOWN INDICATOR LIGHTS AND A AND B CHECKS GOOD.

Part: BLEED AIR LINE — LOOSE (LT ENGINE)

LT DUCT LEAK LIGHT CAME ON AND WOULD NOT EXTINGUISH, SHUTDOWN LT ENGINE AND RETURNED TO LAX. FOUND BLEED AIR LOOSE ON 18 PSI REGULATOR. TIGHTENED LINE, PERFORMED ENGINE POWER, OPS CKS GOOD AND NO LEAKS NOTED.

Part: CONTROL PANEL — DIRTY (STALL WARNING)

AFTER T/O, INADVERTENT STICK SHAKER, TURNED OFF NR 2 SYSTEM AND RETURNED TO LAX. FOUND SYSTEM NR 2 TEST TO BE STICKING. REMOVED, CLEANED AND REINSTALLED STALL WARNING CONTROL PANEL. OPS CK GOOD.

Part: LOCKPIN — BENT (LT MLG DOOR)

LEFT MAIN GEAR OUTBD GEAR DOOR WILL NOT REMAIN LATCHED WHILE IN FLIGHT. FOUND GEAR DOOR LATCH LOCK PIN BENT. REPAIRED LOCK RETAINER PIN. OPERATIONALLY CHECKS GOOD.