N223SW

Part: ACTUATOR — OUT OF ADJUST (RT MLG) · airframe 42,006 hrs · 59,926 cycles

THE RT MAIN GEAR WOULD NOT RETRACT. FLT 5503 ADJUSTED THE RT MAIN GEAR ACTUATOR.

Part: ACTUATOR — OUT OF ADJUST (RT MLG) · airframe 42,021 hrs · 59,942 cycles

THE RT MLG DID NOT RETRACT. FLT 5503 ADJUSTED RT MLG RETRACTION ACTUATOR IAW AMM.

Part: LANDING GEAR — MALFUNCTIONED (RT MLG) · airframe 42,021 hrs · 59,942 cycles

THE RT MLG DID NOT RETRACT. FLT 6452 REPLACED RT MLG RETRACTION IAW AMM. PN ON 19595-000-8 SN ON 169 PN OFF 19595-000-07 SN OFF 815.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,893 hrs · 59,768 cycles

OVERHEAD EMERGENCY LIGHT AT FLIGHT ATTENDANT JUMPSEAT IS BURNED OUT. FLT 6302 RELAMPED.

Part: PANEL — MALFUNCTIONED (COCKPIT) · airframe 41,196 hrs · 58,746 cycles

STRONG ELECTRICAL BURNING ODOR IN COCKPIT. FLT#6479 REPLACED BACKLIGHTING PANEL FOR EMERGENCY BACKUP BATTERY. RAN AIRCRAFT, NO SMELL DETECTED. OPERATIONS CHECKED GOOD.

Part: POWERPACK — FAILED (CABIN) · airframe 40,641 hrs · 57,956 cycles

INTERIOR EMERGENCY LIGHTS DO NOT ILLUMINATE. (SERVICE) REPLACED THE AFT CABIN EMERGENCY BATTERY POWER PACK IAW AMM. P/N D366-04-001 S/N ON 915/03-91 S/N OFF 710-03/90

Part: ACTUATOR — FAILED (RT MLG) · airframe 40,452 hrs · 57,676 cycles

RIGHT MAIN GEAR WOULD NOT RETRACT, CYCLED HANDLE AND GEAR CAME UP. (FLT 5646) REPLACED RIGHT MLG RETRACT ACTUATOR IAW AMM. OPS CHECK GOOD. P/N ON: 19595-000-7 S/N ON: 652 P/N OFF: 19595-000-8 S/N OFF: B105

Part: ACTUATOR — DISCONNECTED (TE FLAP) · airframe 40,438 hrs · 57,659 cycles

AIRCRAFT ROLLS APPROXIMATELY 20 DEGREE DEFLECTION TO RIGHT IN LEVEL FLIGHT, WITH ALL TRIMS NEUTRAL, ROLL BECAME MORE AGGRESSIVE AS AIRSPEED INCREASED. (FLT 5576 RECONNECTED RIGHT O/B FLAP ACTUATOR TO FLAP IAW. ALL OPERATIONAL AND TRAVEL CHECKS GOOD.

Part: SEQUENCE VALVE — DIRTY (RT MLG DOOR) · airframe 40,416 hrs · 57,624 cycles

RIGHT MAIN GEAR WOULD NOT RETRACT UNTIL ABOUT 20 SEC AFTER SELECTING THE GEAR UP. (FLT 6359) CLEANED EXCESSIVE DEBRIS FROM RIGHT MAIN LANDING GEAR DOOR SEQUENCE VALVES AND PERFORMED GEAR SWINGS. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,372 hrs · 57,553 cycles

AFT CENTER AISLE EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 5360) RELAMPED AFT EMERGENCY CEILING LIGHT, OPS CHECKS GOOD.

Part: SEQUENCE VALVE — FAILED (LT MLG) · airframe 40,231 hrs · 57,357 cycles

LEFT MAIN GEAR DOES NOT RETRACT. (FLT 1352) REPLACED LEFT MAIN GEAR INBOARD SEQUENCE VALVE IN REFERENCE TO AMM. PN: 120-32943-001 SN: UNKNOWN.

Part: RIB — CRACKED (RT WING) · airframe 40,165 hrs · 57,268 cycles

RIGHT WING RIB AT YA4945 BETWEEN AUXILIARY SPAR AND FRONT SPAR CRACKED AT TOP. (C-CHECK) REPAIRED NOSE RIB AT YA4945 BETWEEN AUXILIARY SPAR AND FRONT SPAR IAW ETD.

Part: MECHANISM — LACK OF LUBE (CABIN DOOR) · airframe 39,845 hrs · 56,809 cycles

MAIN CABIN DOOR VERY DIFFICULT TO OPEN. (FLT 5491) LUBRICATED LATCH MECHANISM AND ROLLERS ON PASSENGER DOOR.

Part: BRAKE — LOCKED (LT MLG) · airframe 39,775 hrs · 56,713 cycles

LEFT MAIN INBOARD TIRE IS FLAT AND BRAKES ARE SMOKING. (FLT 5392) FOUND NR 2 BRAKE LOCKED UP. REPLACED THE NR 2 BRAKE AND THE NR 1 AND NR 2 WHEEL AND TIRE ASSEMBLIES IN REFERENCE TO MM. P/N: 3-1544 S/N OFF: 02491; P/N: 3-1544 S/N OFF: 1615; / P/N: 2-1661 S/N OFF: 1661.

Part: HYDRAULIC LINE — FAILED (RT NACELLE) · airframe 39,439 hrs · 56,239 cycles

LOST BLUE HYDRAULIC FLUID DURING CLIMBOUT. (FLT 5371) REPLACED HYDRAULIC LINE AT RIGHT NACELLE ABOVE OIL COOLER.

Part: BRAKE — WORN (NR 1) · airframe 39,388 hrs · 56,165 cycles

BRAKES LOCKED UP. (FLT 6282) FOUND NR 1 BRAKE WORN & HARD TO MOVE WITH HYDRAULICS ON. REPLACED THE NR 1 BRAKE ASSEMBLY. P/N: 2-1661, S/N OFF: 0475A

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,323 hrs · 56,077 cycles

ONE WHITE EMERGENCY FLOOR LIGHT AT ROW 6 IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: PROXIMITY SENSOR — OUT OF ADJUST (RT MLG) · airframe 39,305 hrs · 56,048 cycles

ON GEAR RETRACTION, LEFT AND NOSE GEAR RETRACTED NORMALLY BUT THE RIGHT MAIN'S RED POSITION DISAGREEMENT LIGHTS (A&B) REMAINED ILLUMINATED. (FLT 6287) ADJUSTED A AND B RIGHT MLG DOWNLOCK PROXIMITY SENSORS IN REFERENCE TO AMM.

Part: MODULE — FAILED (GEAR HANDLE) · airframe 39,253 hrs · 55,971 cycles

DOWNLOCK RELEASE REQUIRED TO RAISE LANDING GEAR. (FLT 6489) REPLACED LANDING GEAR HANDLE MODULE PER MM. P/N OFF: 120-38594-501 S/N OFF: 120293.

Part: CABLE — OUT OF ADJUST (BRAKE SYSTEM) · airframe 39,141 hrs · 55,802 cycles

THE BRAKES SLOWLY LOCKED UP STOPPING THE AIRCRAFT COMPLETELY. (FLT 5416) ADJUSTED INBOARD BRAKE CONTROL VALVE CABLES.

Part: LIGHT — BROKEN (CABIN) · airframe 38,062 hrs · 54,308 cycles

EMERGENCY EXIT LIGHT AT MCD DOOR IS BROKEN. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,062 hrs · 54,308 cycles

EMERGENCY LIGHT BY MAIN CABIN DOOR IS OUT. (FLT 5547) RELAMPED EMERGENCY LIGHT.

Part: RELAY — FAILED (CABIN) · airframe 37,601 hrs · 53,679 cycles

EMERGENCY CABIN LIGHTS WILL NOT TURN OFF WHEN COMMANDED. (SERVICE) REPLACED RELAYS K519 AND K0201.

Part: PROFILE — CRACKED (FUSELAGE) · airframe 36,546 hrs · 52,224 cycles

VERTICAL STAB TO FUSELAGE LEFT "L" PROFILE CRACKED FROM ONE HI-LOK. (C-CHECK) REPLACED FORWARD SECTION OF LEFT VERTICAL STAB TO FUSELAGE "L" PROFILE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,546 hrs · 52,224 cycles

CORROSION ON STRINGER 18L, 19L AND 20R NEAR CABIN PAX ENTRANCE BELOW FLOOR. (C-CHECK) REPAIRED STRINGER 18L, 19L AND 20R PER SRM.

Part: SMOKE DETECTOR — INTERMITTENT (CARGO BAY) · airframe 35,186 hrs · 50,341 cycles

CARGO SMOKE/FIRE LIGHT ILLUMINATED INTERMITTENTLY. (FLT 6964) REPLACED FORWARD AND AFT CARGO SMOKE DETECTORS.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,319 hrs · 49,102 cycles

LOWER FUSELAGE FRAME 9 AND DOUBLER PLATE CORRODED. (SVC CK) REPAIRED PER ETD2010 -120/01820 AND SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 34,696 hrs · 49,654 cycles

CORROSION AT FRAMES 8 THROUGH 14 ON STRINGERS 20R TO 20L. (C CHECK) REPAIRED PER SRM.

Part: MECHANISM — LACK OF LUBE (PAX DOOR) · airframe 33,647 hrs · 48,165 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6814) LUBRICATED DOOR MECHANISM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,069 hrs · 47,326 cycles

REAR OVERHEAD CABIN EMERGENCY LIGHT INOP. (FLT 6318) RELAMPED EMERGENCY LIGHT.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,985 hrs · 47,200 cycles

CORROSION ON FRAME 23. (C CHECK) REPAIRED PER SRM.

Part: STRINGER — CRACKED (LT NACELLE) · airframe 32,985 hrs · 47,200 cycles

LEFT NACELLE STRINGER AT FRAME 10 CRACKED. (C CHECK) REPLACED PER SRM.

Part: FRAME — CRACKED (NACELLE) · airframe 33,355 hrs · 47,736 cycles

LEFT NACELLE O/B FWD COWL DOOR, FWD LWR NACELLE FRAME CRACKED. (C-CHECK) DRILLED OUT CRACKED FRAME ON LT NACELLE FWD LWR CORNER WHERE FWD COWL O/B DOOR LATCHES, INSTALLED SERVICEABLE FRAME PIECE.

Part: BRACKET — CRACKED (HYDRAULIC PACK) · airframe 33,069 hrs · 47,326 cycles

LEFT HYDRAULIC PACK LOWER MOUNT CRACKED. (C CHECK) REPLACED BRACKET PER SRM.

Part: FRAME — CRACKED (LT NACELLE) · airframe 32,985 hrs · 47,200 cycles

LEFT NACELLE FRAME 8 CRACKED. (C CHECK) REPLACED PER SRM.

Part: LAMP — BURNED OUT (EMERGENCY LGIHTS) · airframe 32,100 hrs · 45,990 cycles

FLT 5719 - MOST FORWARD FLOOR PROXIMITY EMERGENCY LIGHT BURNED OUT. RELAMPED.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 30,398 hrs · 43,715 cycles

FLT 5712 - EXIT LIGHT ON OVERHEAD BIN AT ROW 9 IS INOP. REPAIRED WIRING TO EMERGENCY LIGHT ON OVERHEAD BIN.

Part: ACTUATOR — LEAKING (TE FLAPS) · airframe 30,113 hrs · 43,327 cycles

FLT 5423 - WHEN FLAPS WERE SELECTED TO 25 DEGREES, RECEIVED A FLAPS MESSAGE FOLLOWED BY LOSS OF BLUE HYDRAULIC SYSTEM FLUID. REPLACED THE RIGHT NACELLE ACTUATOR IAW AMM 27-50-08. OPS AND LEAK CHECKS GOOD, P/N: 343100-1001 S/N OFF: 0200.

Part: A/C PACK — SMOKE (RIGHT) · airframe 29,329 hrs · 42,272 cycles

FLT 5706 - RIGHT PACK FAIL LIGHT CAME ON INFLIGHT AND LAV SMOKE ALARM SOUNDED WITH ASSOCIATED SMELL OF SMOKE. RAN AIRCRAFT AND RIGHT PACK ON BOTH ENGINE AND APU BLEEDS AND IN AUTO AND MANUAL MODES. NO DISCREPANCIES NOTED. OPS CHECK GOOD.

Part: SIGN — MISSING (EMERGENCY EXIT) · airframe 29,145 hrs · 42,026 cycles

FLT 5446 - EMERGENCY EXIT SIGN MISSING FROM 6A. INSTALLED NEW EMERGENCY LIGHT FIXTURE AT 6A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,145 hrs · 42,026 cycles

FLT 5491 - WHITE FLOOR EMERGENCY LIGHT IS INOP. REPLACED LIGHT ASSEMBLY ON FLOOR TRACK.

Part: TAB — CORRODED (AILERON) · airframe 29,385 hrs · 42,341 cycles

LEFT AILERON TRIM TABS HAVE SURFACE CORROSION. REPLACED LEFT AILERON TRIM TAB OUTBOARD CONTROL ROD IAW EMB 120 MM 27-12-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,385 hrs · 42,341 cycles

LEFT FORWARD SMALL SEAT TRACK SECTION IS CORRODED. REPLACED SEAT TRACK IAW AMM 53-01-05.

Part: SKIN — CORRODED (FUSELAGE) · airframe 28,672 hrs · 41,352 cycles

BELLY FUSELAGE SKIN IS CRACKED AND CORRODED BY FRAME 22. REPAIRED DAMAGED AREA PER EMB APPROVED REPAIR IC2007-120/00663 AND SRM 53-00-03.

Part: LIGHT — DISLODGED (EMERGENCY EXIT) · airframe 27,768 hrs · 40,092 cycles

EMERGENCY EXIT PLACARD OVER SEATS 9BC CAME OFF. REPLACED EMERGENCY EXIT SIDEWALL LIGHT AT 9BC. OPERATIONAL CHECKS GOOD.

Part: ACTUATOR — JAMMED (RT RUDDER) · airframe 27,582 hrs · 39,836 cycles

RIGHT RUDDER JAMMED AFTER TAKEOFF. REPLACED BLUE SYSTEM RUDDER ACTUATOR IAW MM 27-22-02. OPERATIONAL CHECKS GOOD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 26,698 hrs · 38,510 cycles

OVERWING EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED CENTER ELBP IAW MM 33-50-02. OPERATIONAL CHECKS GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 25,588 hrs · 36,851 cycles

A 4 FLOOR LEVEL EMERGENCY LIGHTS INOP. RESET PINS ON CONNECTOR UNDER FLOOD LIGHT. OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 25,565 hrs · 36,812 cycles

EMERGENCY FLOOR LIGHT OUT 5A. REPLACED EMERGENCY LIGHT 5A PER MM 33-51-01. OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 25,418 hrs · 36,609 cycles

EMERGENCY FLOOR LIGHTS 7A INOP. RELAMPED EMERGENCY LIGHTING AT SEAT 7A FLOOR. OPERATIONAL CHECK GOOD.

Part: RELAY — MALFUNCTIONED (TRIM SYSTEM) · airframe 25,408 hrs · 36,587 cycles

TRIM ON F/O SIDE FAILED FFOD TEST. REPLACED F/O'S TRIM SWITCH AND TRIM PRIORITY RELAY K0393. OPERATIONAL CHECK GOOD PER MM 22-11-00 AND MM 27-31-00.

Part: SIGN — BROKEN (EMERGENCY EXIT) · airframe 24,587 hrs · 35,336 cycles

EMERGENCY EXIT SIGN, FLOOR LEVEL AT 6A IS BROKEN. REPAIRED E-EXIT SIGN AT 6A. OPERATIONAL CHECK GOOD.

Part: SIGN — BROKEN (ROW 9C) · airframe 24,555 hrs · 35,282 cycles

LOWER EXIT SIGN AT ROW 9C BROKEN. REPLACED LOWER EXIT SIGN. OPERATIONAL CHECK GOOD.

Part: PRESSURE VALVE — MALFUNCTIONED (LT A/C PACK) · airframe 24,438 hrs · 35,106 cycles

LEFT PACK FAIL AND DUCT LEAK MSG, AND COCKPIT FILLED WITH SMOKE. INSTALLED PRESSURE REGULATOR SHUT OFF VALVE, OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,845 hrs · 31,166 cycles

FIRST 2 EMERGENCY OVERHEAD LIGHT PODS ARE INOP. REPLACED 1ST EMERGENCY OVERHEAD LIGHT POD WITH A SERVICEABLE UNIT. SECOND OVERHEAD EMERGENCY LIGHT OPERATES NORMALLY. OPS CHECK GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 21,845 hrs · 31,166 cycles

LEFT FORWARD FLOOR SEAT TRACK SMALL 3 HOLE PIECE IS CORRODED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED LEFT FORWARD SEAT TRACK IAW 53-01-05.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 21,845 hrs · 31,166 cycles

LEFT HYDRAULIC BAY SHEET METAL CRACKED AT BULKHEAD. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CRACKED BULKHEAD IAW 120 SRM 51-10-02 PAGE 2, PAR 2B.

Part: STICK SHAKER — MALFUNCTIONED (COCKPIT) · airframe 21,276 hrs · 30,278 cycles

F/O'S STICK SHAKER INOP. REPLACED RIGHT STICK SHAKER. OPS CHECKS GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,558 hrs · 29,193 cycles

EMERGENCY LIGHTS BEHIND ROW 8 WOULD NOT ILLUMINATE. COCKPIT AND FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCHES BOTH TESTED. REPLACED AFT BATTERY. ALL EMERGENCY LIGHTS OPS CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (T/E FLAP) · airframe 20,268 hrs · 28,743 cycles

OUTBOARD FLAPS CONTROL FAULT FOR ABOUT 30 SECONDS WHEN RETRACTING FROM 15 DEGREES. REPLACED FCU WITH SERVICEABLE UNIT. SYSTEM OPS CHECKS OKAY.

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAP) · airframe 19,584 hrs · 27,682 cycles

NACELLE FLAPS DROP SLIGHTLY (UNCOMMANDED). REPLACED LEFT NACELLE FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-00. OPS CHECK GOOD. NO HYDRAULIC LEAKS NOTED. S/N OFF: 0187.

Part: FLOW DIVIDER — MALFUNCTIONED (LT ENGINE) · airframe 18,939 hrs · 26,716 cycles

ON TAKEOFF ROLL BELOW 80 KTS, THE LT ENGINE SHUT DOWN. ABORTED THE TAKEOFF. REMOVED AND REPLACED LT ENGINE FLOW DIVIDER. RAN ENGINE. SYSTEM OPS CHECK AND LEAK CHECK GOOD IAW EMB120 MM 73-14-00 & P&W MM.

Part: ODOR — DETECTED (COCKPIT) · airframe 18,830 hrs · 26,555 cycles

ON TAKEOFF ROLL, WITH POWER SET AT APPROXIMATELY 90 PERCENT TORQUE, THE FLIGHT DECK STARTING TO FILL WITH UNIDENIFIED VAPOR. CABIN ALSO BEGAN TO FILL WITH VAPOR. ABORTED TAKEOFF. PERFORMED ENGINE RUNS. FOUND TO BE WATER VAPOR IN THE AIR CONDITIONING SYSTEM. RAN PACKS FOR 15 MINUTES TO CLEAR. OPS CHECK GOOD.

Part: APU — SMOKE (APU BAY) · airframe 18,794 hrs · 26,505 cycles

RT PACK BLOWS HOT AIR AND SETS OFF LAV SMOKE DETECTOR WITH PROMINENT PACK BURNING ODOR. RAN BOTH ENGINES WITH RT PACK ON. FOUND LAV SMOKE DETECTOR NOT GOING OFF. RAN APU WITH THE RT PACK ON. FOUND THAT THE APU BLEEDS SMOKE INTO THE CABIN. SUPPLEMENTAL REPORT FORTHCOMING.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 18,575 hrs · 26,172 cycles

AUTOPILOT AND TRIM FAILURE MAP LIGHTS ILLUMINATED ON TAKE OFF ROLL. ABORTED TAKE OFF. INSTALLED SERVICEABLE FO'S A/P COMPUTER. AUTO PILOT SELF DIAGNOSTIC AND OPS CHECKS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 18,416 hrs · 25,927 cycles

EMERGENCY LIGHTS WOULD NOT ILLUMINATE IN THE LAST THREE ROWS OF THE AIRCRAFT. REPLACED AFT EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD.

Part: WIRE HARNESS — FAULTY (RT MLG) · airframe 18,196 hrs · 25,573 cycles

THE CABIN PRESSURE DROPPED BELOW LEVEL WITH AUTO MODE, IDLE NR 1 & 2 UNLK LIGHTS CAME ON AND DOWNLOCK RELEASE WAS REQUIRED TO PUT THE GEARS UP. REMOVED AND REPLACED RT MLG HARNESS ASSY WITH SERVICEABLE PART. PERFORMED OPS CHECK FOR DISCREPANCIES. NO DEFECTS NOTED AT THIS TIME.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,165 hrs · 25,525 cycles

C-CHECK, LEFT SIDE UPPER SEAT RAIL CORROSION FOUND IN 28 LOCATIONS. INSTALLED LEFT SIDE UPPER SEAT RAIL IAW 53-01-05.

Part: FRAME — CRACKED (RT NACELLE) · airframe 18,165 hrs · 25,525 cycles

RIGHT NACELLE FRAME 1 CRACKED AT O/B TOP TORQUE MOUNT BOLT WEB. REMOVED AND REPLACED FRAME 1 IAW SB 120-54-0036 REV 02, 09 JUN 99.

Part: FRAME — CRACKED (NACELLE) · airframe 18,165 hrs · 25,525 cycles

RIGHT AND LEFT NACELLE, ABOVE WING, I/B & O/B SIDE, BENEATH EXHAUST PIPE MOUNT, CRACKS IN FRAMES. STOP-DRILLED CRACKS AND INSTALLED REPAIR DOUBLERS ON THE FRAMES IAW EMB SRM 51-70-05.

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 17,619 hrs · 24,716 cycles

AFTER TAKEOFF RECEIVED CONTROL SINK, TERRAIN AND CONTINUOUS PULL UP WARNINGS UNTIL 50 FT AGL. RETURNED TO FAT. REPLACED GPWS COMPUTER. OPS CHECK GOOD IAW MM 34-44-00.

Part: INVERTER — MALFUNCTIONED (NR 2) · airframe 17,228 hrs · 24,139 cycles

ON INITIAL TAKEOFF ROLL, INVERTER NR 2 INOP LIGHT CYCLES ON AND OFF TWICE WITH NO INDICATIONS OF AN INVERTER NR 2 FAILURE. TAKEOFF WAS ABORTED. REPLACED NR 2 INVERTER WITH SERVICEABLE ASSEMBLY FOR TROUBLESHOOTING. OPS CHECK GOOD AT THIS TIME.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 17,228 hrs · 24,139 cycles

UPON ADVANCING POWER LEVERS FOR TAKEOFF, PRESSURIZATION VSI WENT TO 2000 FPM DOWN. ABORTED TAKEOFF AND RETURNED TO GATE. REPLACED ELECT. ALTITUDE PRESSURE CONTROLLER. PERFORMED OPS CHECK. OPS CHECK GOOD. S/N OFF: 153.

Part: CONNECTOR — DIRTY (T/E FLAP) · airframe 16,741 hrs · 23,410 cycles

WHEN FLAPS 45 SELECTED DISAGREEMENT ON OUTBOARD FLAPS, 2 BARS DIFFERENCE. CLEANED OUTBOARD FLAP ACTUATOR CANNON PLUGS. CLEANED FLAP TRACKS AND ROLLERS. CYCLED FLAPS 2 DOZEN TIMES. CLEARED COMPUTER FAULTS. OPS CHECK GOOD.

Part: SWITCH — FAILED (RT STAB)

OUTBOARD RIGHT STABILIZER INOP, LIGHT ILLUMINATED IN FLIGHT. CYCLED THROUGH BOTH TIMERS AS WELL AS HEAVY AND LIGHT MODES. DIVERTED FROM MCE TO FAT. REPLACED RIGHT OUTBOARD STABILIZER DEICE PRESSURE SWITCH AND INSTALLED THREE DEICE PATCHES, OPS CHECKS GOOD.

Part: SWITCH — MALFUNCTIONED (LEFT MLG)

DEPARTED LAS, LEFT MAIN SYSTEM A GREEN LIGHT REMAINED ILLUMINATED. FOLLOWED QRH PROCEDURE, CYCLED GEAR HANDLE. GEAR WOULD NOT CYCLE DOWN. AFTER LEVEL OFF, LIGHT EXTINGUISHED. CONTINUED TO FAT. USED EMERGENCY GEAR EXTENSION PROCEDURES AND GEAR EXTENDED. REPLACED LEFT GEAR SYSTEM A GREEN PROX HARNESS AND SWITCH IAW EMB 120 MM 32-61-01, OPS CHECK GOOD.

Part: ENGINE — OVERTEMP (LT & RT)

ON APPROACH INTO JAC, ENCOUNTERED SEVERE TURBULENCE AND WINDSHEAR. MAXIMUM POWER WAS REQUIRED AND T6 EXCEEDED 900 DEG. AIRCRAFT NEEDS SEVERE TURBULENCE INSPECTION. DID NOT LAND IN JAC BUT RETURNED TO SLC. COMPLIED WITH SEVERE TURBULENCE INSPECTION WITH NO DEFECTS NOTED. REPLACED BOTH ENGINE ASSEMBLIES AND INSPECTED BOTH PROPS IAW MM 61-10-00.

Part: CIRCUIT BREAKER — TRIPPED (E & E COMPT)

ON TAKEOFF, FIRST OFFICERS EHSI AND NAV NUMBER TWO WENT INOPERATIVE. RETURNED TO LAX. NORMAL POWER RETURNED TO BOTH UNITS AFTER LANDING. FOUND NUMBER TWO EMERGENCY BUS CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER. RAN ENGINE AND ALL CHECKS GOOD.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR)

CARGO DOOR LIGHT CAME ON AFTER V1 DURING TAKEOFF. RETURNED FOR LANDING AND VERIFIED DOOR PROPERLY CLOSED. ADJUSTED CARGO DOOR MICRO SWITCH, OPS CHECKS GOOD ON GROUND.

Part: TORQUE MONITOR — MALFUNCTIONED (LT ENGINE)

LEFT ENGINE FAILED AFTER TAKEOFF AT 600 FT. RETURNED TO FIELD. DETERMINED LEFT ENGINE HAD AN AUTO FEATHER WITHOUT ENGINE SHUT DOWN. REPLACED LEFT ENGINE TORQUE PROBE WITH SERVICEABLE UNIT. ALL GROUND CHECKS GOOD IAW MM 73.

Part: LATCH — FAILED (LT MLG DOOR)

AFTER DEPARTURE WITH GEAR UP AND LOCKED, NOTICED LEFT MAIN OUTBOARD GEAR DOOR WAS STILL DOWN. RETURNED AND LANDED AT EKO. REPLACED LEFT OUTBOARD GEAR DOOR LATCH AS REQUIRED, OPS CKS GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (TE FLAPS)

FLAP CONTROL FAULT. FAULT WILL NOT RESET. REMOVED AND REPLACED FLAP CONTROL UNIT WITH SERVICEABLE UNIT. OPERATIONALLY CHECKS GOOD.

Part: CONNECTOR — DIRTY (FLAP CONTROL)

NUMEROUS FLAP CONTROL FAULTS ENROUTE. CONTROL FAULTS RESET EACH TIME. CLEANED FLAP ACTUATOR CANNON PLUGS. RERACKED FLAP CONTROL BOX. ALL CHECKS GOOD AT THIS TIME.