N217SW

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 43,373 hrs · 57,186 cycles

AIRPLANE WOULD NOT HOLD PRESSURIZATION AT ALTITUDE. (FLT 5356) REPLACED PRESSURIZATION CONTROLLER IAW AMM. OPS CHECKS GOOD. PRESSURIZED A/C ON GROUND NO DEFECTS NOTED. P/N: 22201T011400, S/N ON: 153, SN OFF: 520

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,243 hrs · 57,035 cycles

EMERGENCY LIGHTS DO NOT ILLUMINATE. (FLT 7405) REPLACED NR 2 EMERGENCY LIGHTING BATTERY PACK IAW AMM. P/N: D366-04-001 S/N ON: 242 S/N OFF: 1022

Part: SOLENOID VALVE — FAILED (NLG DOOR) · airframe 42,885 hrs · 56,577 cycles

NOSE WHEEL WOULD NOT RETRACT, RECEIVED A GEAR UP INDICATION. (FLT 7446) REPLACED NOSE GEAR DOOR SOLENOID VALVE IAW AMM. P/N-SV14H1100-4 S/N ON-N64481 S/N OFF-N92770

Part: MONITOR — DEFECTIVE (DE-ICE SYSTEM) · airframe 42,596 hrs · 56,218 cycles

DEICE MONITOR TEST LIGHT BURNED OUT. (FLT 6246) REPLACED DE-ICE MONITOR. P/N: D552-01-001 S/N ON: 078/04-87 S/N OFF: 362/04-91.

Part: WIRE — UNSECURE (CABIN) · airframe 42,448 hrs · 56,027 cycles

FORWARD DOOR OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RE-SECURED WIRING AT OVERHEAD MAIN CABIN DOOR LIGHT.

Part: LIGHT — UNSECURE (CABIN) · airframe 42,415 hrs · 55,990 cycles

EMERGENCY OVERHEAD LIGHT AT 6C AND AFT OVERHEAD EMERGENCY LIGHT ARE BOTH INOPERATIVE. (FLT 6491) RE-SECURED OVERHEAD EMERGENCY LIGHT AT SEAT 6C AND AFT OVERHEAD EMERGENCY LIGHT.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 42,448 hrs · 56,027 cycles

FUSELAGE FRAME NR 13 CRACKED IN TWO PLACES BETWEEN 1ST AND 2ND DOOR FUSELAGE STOPS. (C-CHECK) REPAIRED IN REFERENCE TO EMB SRM.

Part: SPAR — CRACKED (LT WING) · airframe 42,448 hrs · 56,027 cycles

LEFT WING LOWER SPAR CRACKED BETWEEN RIBS 16 AND 18. (C-CHECK) REPAIRED IN REFERENCE TO EMB SRM.

Part: FUSE — NOT SEATED (EMERGENCY LIGHTS) · airframe 42,363 hrs · 55,917 cycles

FOUR WHITE AND ONE RED LIGHT OUT IN FLOOR EMERGENCY LIGHTING. (FLT 5367) RE-SEATED INTERIOR EMERGENCY LIGHT FUSE F0032 AT FRAME 24 IN REFERENCE TO AMM.

Part: DUCT — FAILED (BLEED AIR SYS) · airframe 42,124 hrs · 55,629 cycles

AFTER TAKEOFF WHEN CHANGING BLEEDS TO AUTO AND PACKS TO NORMAL HEARD A LOUD BANG FOLLOWED BY A DUCT LEAK ON BOTH RIGHT & LEFT PACKS. LIGHTS WENT OUT AFTER TURNING BLEEDS OFF. (FLT 7782) REPLACED BLEED AIR DUCT TUBE ASSEMBLY. P/N: 120-24937-011

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,994 hrs · 55,466 cycles

EXIT ROW EMERGENCY LIGHT IS OUT. (FLT 7780) REPLACED NR 2 ELBP. P/N: D366-04-001, S/N OFF: 1088

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,775 hrs · 55,226 cycles

EMERGENCY LIGHTS IN CABIN ARE INOPERATIVE. (FLT 5478) REPLACED AFT ELBP. PN: D366-04-001 SN OFF: 874

Part: STRINGER — CORRODED (FUSELAGE) · airframe 41,712 hrs · 55,132 cycles

LOWER AFT FUSELAGE STRINGERS 20L AND 20R HAS CORROSION. (C-CHECK) REPLACED STRINGERS 20R AND 20L IN REFERENCE TO SRM 120.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,712 hrs · 55,132 cycles

CORROSION FOUND AT LEFT CENTER FLOOR SUPPORT BRACKET AT FRAME 16. (C-CHECK) REPLACED LEFT CENTER FLOOR SUPPORT BRACKET AT FRAME 16 IN REFERENCE TO 120 SRM.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 41,712 hrs · 55,132 cycles

CENTER FORWARD BUTTSTRAP CORRODED AT FRAME 16. (C-CHECK) REPLACED CENTER FORWARD BUTTSTRAP IN REFERENCE TO 120 SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,712 hrs · 55,132 cycles

CORROSION ON LEFT OMEGA BEAM NEAR PASSENGER DOOR ENTRANCE. (C-CHECK) REPLACED LEFT OMEGA BEAM IN REFERENCE TO EMB 120 SRM.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 41,712 hrs · 55,132 cycles

SURFACE CORROSION ON LEFT CABIN BUTT STRAP NEAR PASSENGER DOOR ENTRANCE. (C-CHECK) REPLACED AFFECTED BUTT STRAP IN REFERENCE TO EMB 120 SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 41,712 hrs · 55,132 cycles

CORROSION FOUND UNDER FRAME 38 JUST OUTBOARD OF STRINGER 21R AFT LOWER FUSELAGE. (C-CHECK) REPAIRED DAMAGED AREA AT FRAME 38 JUST OUTBOARD OF STRINGER 21R.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 41,712 hrs · 55,132 cycles

CORROSION UNDER FRAME 36 JUST OUTBOARD OF STRINGER 21L AFT LOWER FUSELAGE. (C-CHECK) REPAIRED DAMAGED AREA AT FRAME 36 JUST AFT OF LOWER FUSELAGE.

Part: WIRE — BROKEN (CABIN) · airframe 41,298 hrs · 54,548 cycles

NR 2 EMERGENCY FLOOR LIGHT ON THE LEFT SIDE IS OUT. (FLT 5479) REPAIRED BROKEN WIRE.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 40,910 hrs · 54,052 cycles

FLOOR LEVEL EMERGENCY LIGHT AT 3A IS OUT. (FLT 6339) RE-SECURED CONNECTOR ON FLOOR EMERGENCY LIGHT NEAR ROW 3.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,469 hrs · 53,496 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6191) RELAMPED EMERGENCY LIGHT.

Part: TRIM SWITCH — DEFECTIVE (AUTOPILOT SYS) · airframe 40,362 hrs · 53,371 cycles

PITCH TRIM RUNAWAY ON LANDING. (FLT 5341) REPLACED BOTH PITCH TRIM SWITCHES, BOTH AUTOPILOT COMPUTERS AND ELEVATOR SERVO.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,257 hrs · 53,236 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 5 IS OUT. (FLT 5359) REPLACED NR 2 ELBP. P/N D366-04-001, S/N OFF 1006.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 39,411 hrs · 52,227 cycles

FORWARD OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 6446) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,306 hrs · 52,099 cycles

FIRST RED LIGHT ON EMERGENCY EXIT FLOOR LIGHTS INOPERATIVE. (FLT 6237) RELAMPED EMERGENCY LIGHT.

Part: STARTER GEN — CORRODED (APU) · airframe 38,383 hrs · 50,975 cycles

APU STARTER GENERATOR AIRFRAME GROUND CORRODED. (A CHECK) REPAIRED PER EMB SRM.

Part: WIRE — DAMAGED (CABIN) · airframe 38,158 hrs · 50,717 cycles

RED EMERGENCY LIGHT MAIN CABIN ENTRY INOP. (FLT 6654) REPAIRED WIRE AND RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,038 hrs · 50,566 cycles

CENTER OVERHEAD EMERGENCY LIGHT INOP. (FLT 7778) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — NOT SEATED (CABIN) · airframe 37,788 hrs · 50,271 cycles

EMERGENCY CEILING LIGHT ABOVE 9B & 9C INOP. (FLT 1001) RESEATED LIGHT BULB.

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 36,880 hrs · 49,081 cycles

EMERGENCY LIGHTS CIRCUIT BREAKER A30 TRIPPED IN FLIGHT. (FLT 6232) RESET C/B ON GROUND, OPERATIONAL CHECKS NORMAL.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 36,285 hrs · 48,293 cycles

FLT 6809 - MID CABIN OVERHEAD EMERGENCY LIGHT INOP. REPAIRED BROKEN WIRE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 36,175 hrs · 48,130 cycles

FLT 6232 - FORWARD CABIN EMERGENCY FLOOR LIGHT INOP. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,124 hrs · 48,064 cycles

FLT 5875 - FORWARD MOST FLOOR LEVEL RED EMERGENCY LIGHT INOP. REPLACED LIGHT ASSEMBLY.

Part: LANDING GEAR — INTERMITTENT (LEFT) · airframe 36,109 hrs · 48,042 cycles

FLT 6909 - LEFT MAIN GEAR SLOW TO COME DOWN. OPERATED GEAR SEVERAL TIMES, OPS CHECKS GOOD.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 36,499 hrs · 48,588 cycles

C-CHECK, BUTTSTRAP AND STRINGERS BETWEEN FRAME 13 AND 19 LOWER FUSELAGE CORRODED. REPAIRED PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 35,720 hrs · 47,523 cycles

FLT 5473 - EXIT LIGHT AT ROW 6CDE BROKEN. REPLACED LIGHT ASSEMBLY.

Part: RIB — CRACKED (RT WING) · airframe 35,457 hrs · 47,176 cycles

SVC CHECK, RIGHT WING LEADING EDGE, INBOARD RIB ASSEMBLY IS CRACKED IN TWO PLACES. REPLACED PER SRM.

Part: ACTUATOR — JAMMED (RUDDER) · airframe 34,986 hrs · 46,571 cycles

ON CLIMB, RIGHT RUDDER WAS JAMMED AFTER ABOUT 1 INCH OF TRAVEL. REPLACED BLUE RUDDER ACT PER MM 27-22-00, P/N: 308140-1003, S/N ON, 0153 S/N OFF, 0494.

Part: BEAM — CORRODED (PAX DOORWAY) · airframe 34,805 hrs · 46,333 cycles

PAX DOOR HINGE BEAM HAS AREAS OF CORROSION WHERE BUSHINGS ARE INSTALLED FOR FWD AND AFT HINGES. REPLACED PAX DOOR HINGE BEAM IAW SRM 51-25-00, 51-22-00, 51-40-02, 51-40-04, AND 51-40-07.

Part: BUSHING — WORN (PAX DOOR) · airframe 34,805 hrs · 46,333 cycles

MAIN CABIN DOOR IS HARD TO CLOSE AND OPEN. REPLACED PAX DOOR BUSHINGS AND BOLTS IAW AMM 20-10-00 AND INSTALLED DOOR IAW AMM 52-10-00. OPS CHECK GOOD.

Part: APU — ODOR · airframe 34,356 hrs · 45,740 cycles

FUEL SMELL IN THE CABIN WHILE APU IS RUNNING. REPLACED APU IAW EMB 120 MM 49-00-01. OPS CHECK GOOD, P/N 3800376-2, S/N OFF P-322.

Part: SIGNAL COND UNIT — MALFUNCTIONED (LT PROPELLER) · airframe 33,813 hrs · 45,027 cycles

LEFT PROP AUTO FEATHERED UNCOMMANDED WHILE EXITING THE RUNWAY, FLIGHT NR 3715. REPLACED TORQUE SIGNAL CONDITIONER IAW EMB MM 77-12-00, PN 30005-0000-52, SN OFF 2229.

Part: CONTACTOR — DAMAGED (EMERGENCY BUSS) · airframe 29,761 hrs · 39,714 cycles

EMERGENCY LIGHTS FAIL TO TEST PROPERLY. REPLACED EMERGENCY BUSS CONTACTOR NR 2 (K0519) IAW MM 24-52-03. OPERATIONAL CHECK OK.

Part: SERVO — BINDING (RUDDER) · airframe 29,082 hrs · 38,831 cycles

CAPTAINS RUDDER PEDALS BINDING. REPLACED RUDDER SERVO. OPERATIONAL CHECK GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,354 hrs · 39,197 cycles

PAX SEAT TRACK CORRODED FWD LT SIDEWALL, ITEM FOUND AT C-CHECK INSPECTION. REPLACED PAX SEAT TRACK FWD LT SIDEWALL IAW EMB120 MM 53-01-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,354 hrs · 39,197 cycles

PAX SEAT TRACK CORRODED RT AFT FLOOR, ITEM FOUND AT C-CHECK INSPECTION. REPLACED PAX SEAT TRACK RT AFT FLOOR IAW EMB120 MM 53-01-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,354 hrs · 39,197 cycles

FWD LT FLOOR TRACK CORRODED, GALLEY FLOOR ANCHOR, ITEM FOUND AT C-CHECK INSPECTION. REPLACED FORWARD LT INBOARD SEAT TRACK.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 28,423 hrs · 37,947 cycles

EMERGENCY LIGHT UNDER F/A'S SEAT INOP. INSTALLED NEW BULB IN EMERGENCY LIGHT UNDER F/A'S SEAT, OPERATIONAL CHECK GOOD.

Part: DOOR — LACK OF LUBE (MAIN CABIN) · airframe 28,394 hrs · 37,896 cycles

MAIN CABIN DOOR HARD TO OPEN AND CLOSE. LUBRICATED CABIN DOOR LINKAGE. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (RUDDER CONTROL) · airframe 28,361 hrs · 37,839 cycles

RT RUDDER PEDAL JAMMED EN ROUTE. R & R RUDDER PCU, GREEN HYD SYSTEM RUDDER ACTUATOR, AND BLUE HYD SYSTEM RUDDER ACTUATOR IAW AMM 27-22-20; 27-22-02; 27-22-01. OPS CHECK GOOD,

Part: SMOKE — DETECTED (CABIN) · airframe 26,308 hrs · 35,159 cycles

SMELLED SMOKE IN COCKPIT ON GROUND. RAN BOTH PACKS. NO DEFECTS NOTED.

Part: PUMP — MALFUNCTIONED (HMU) · airframe 26,116 hrs · 34,928 cycles

DURING CLIMB RIGHT ENGINE LOST POWER INDICATING ABOUT 15 PERCENT TQ, T6 450, DECREASING FUEL FLOW 250, DECREASING NP 100 PERCENT. REMOVED AND REPLACED HMU FUEL PUMP. OPERATIONAL CHECK GOOD. P/N: 786390-10, S/N OFF: F10376, P/N: 5006488G, S/N OFF: 2178.

Part: COMPUTER — MALFUNCTIONED (AUTO PILOT) · airframe 25,684 hrs · 34,377 cycles

DURING FLIGHT, CAPTAIN'S ADI AND FLIGHT DIRECTOR WERE ERRATIC CAUSING A COMPUTER FAILURE AND THE A/P TO DISENGAGE. INSTALLED SERVICEABLE APC-65B ON THE CAPTAIN'S SIDE IAW EMB 120 MM CHAPTER 22-10-02. OPS CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAP) · airframe 25,294 hrs · 33,918 cycles

CREW REPORTED FLAP DISAGREE ALARM WHEN RETRACTING FLAPS. LEFT NACELLE FLAP SLOW TO ACTUATE IN OVERRIDE UP. REPLACED LEFT FLAP ACTUATOR WITH SERVICEABLE UNIT IAW EMB MM 27-50-08. OPS CHECKS GOOD.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 24,944 hrs · 33,498 cycles

FO SIDE AUTOPILOT CAUSES CONTROL WHEEL TO SHAKE. REMOVED AND REPLACED NR 2 APC COMPUTER WITH A SERVICEABLE UNIT. OPS CHECKS GOOD.

Part: FUSE — BLOWN (BATTERY PACK) · airframe 24,766 hrs · 33,225 cycles

EMERGENCY LIGHTS NOT WORKING CENTER SECTION. REPLACED BLOWN FUSE AT NR 1 ELBP, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,480 hrs · 32,836 cycles

AFT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK GOOD IAW 33-50-02.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,286 hrs · 32,603 cycles

EMERGENCY LIGHTS INOPERATIVE, IN CABIN. RESECURED CENTER LIGHTS BATTERY PACK CONNECTOR PLUG. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: ACTUATOR — FAILED (NACELLE FLAP) · airframe 24,234 hrs · 32,543 cycles

SHORTLY AFTER SELECTING FLAPS 15 DEGREES FOR LANDING, RECEIVED A FLAP DISAGREEMENT ON THE INBOARD & NACELLE FLAPS. WITHIN A FEW SECONDS, LOST THE ENTIRE BLUE HYD SYSTEM AS NOTED BY NO FLUID QUANTITY AND SUBSEQUENT WARNING LIGHTS. INSTALLED SERVICEABLE HYD ACTUATOR ON RT NACELLE FLAP. OPS CHECK AND LEAK CHECKS GOOD IAW 27-50-00.

Part: CONTROL HANDLE — OBSTRUCTED (FLAP CONTROL) · airframe 24,090 hrs · 32,345 cycles

FLAPS WILL NOT GO TO THE 45 DEGREE POSITION. COMMAND BARS SHOW CORRECTLY, BUT THE FLAPS WILL NOT GO PAST 25 DEGREES. REMOVED DEBRIS OBSTRUCTING FLAP HANDLE MOVEMENT TO 45 DEGREES. CYCLED FLAPS. OPS CHECK GOOD, NO DEFECTS NOTED.

Part: WYE DUCT — DAMAGED (ENGINE) · airframe 23,642 hrs · 31,793 cycles

ON TAKEOFF ROLL RIGHT T6 GAP WENT TO 300 DEGREES IN BOTH DIGITAL AND ANALOG WITH NO POWER LOSS TO THE ENGINE. ABORTED TAKEOFF. FOUND BLEED AIR DUCT ON TOP OF T6 PROBE RING TOUCHING BOTH RINGS. REMOVED AND REPLACED BLEED AIR WYE OFF OF ENGINE, TIGHTENED CLAMPS, AND ADJUSTED WHEEL WELL FEED THROUGH TUBE CLAMP AND BRACKET.

Part: WINDOW — CRACKED (COCKPIT) · airframe 23,656 hrs · 31,809 cycles

RIGHT SIDE DV WINDOW CRACKED AT FORWARD BOTTOM CORNER. REMOVED AND REPLACED RIGHT SIDE DV WINDOW.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 23,526 hrs · 31,661 cycles

EN ROUTE AT 11500 FT, RECEIVED A 'CABIN ALT' LIGHT ON THE MAP WITH MASTER WARNING AND TRIPLE CHIME. QRH PROCEDURE FOLLOWED, UNABLE TO CONTROL CABIN PRESSURE IN MANUAL MODE. RETURNED TO SBA. REPLACED PRESSURE CONTROLLER. PRESSURIZED AIRCRAFT, OPS CHECK GOOD.

Part: CONTROL HANDLE — MALFUNCTIONED (COCKPIT) · airframe 22,882 hrs · 30,882 cycles

LANDING GEAR WOULD NOT EXTEND WHEN SELECTING GEAR DOWN. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE. CYCLED GEAR 6 TIMES W/ONE EMERGENCY FREE FALL. OPS CHECK GOOD AT THIS TIME.

Part: COMPARATOR — MALFUNCTIONED (NR 1) · airframe 22,882 hrs · 30,882 cycles

CAPTAIN'S AUTOPILOT WENT INTO UNCOMMANDED CLIMB. REPLACED NR 1 AHC IAW MM 34-21-01. AHRS OPS CHECK GOOD IAW MM 34-21-00. AUTOPILOT OPS CHECK GOOD IAW MM 22-10-00.

Part: FUEL LINE — CRACKED (RT ENGINE) · airframe 22,114 hrs · 29,972 cycles

AFTER TAKEOFF FUEL DISCOVERED LEAKING FROM RIGHT ENGINE. ENGINE SHUTDOWN AND AIRCRAFT RETURNED TO THE FIELD. FOUND CRACKED FUEL LINE AT HMU. REPLACED LINE. LEAK CHECK GOOD. REMOVED AND REPLACED HMU FUEL RETURN HOSE IAW EMB POWERPLANT BUILDUP 71-00-00. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,114 hrs · 29,972 cycles

COCKPIT ENTRY RED FLOOR LEVEL EMERGENCY LIGHTING INOP. REMOVED AND REPLACED COCKPIT FLOOR LEVEL LIGHTS. OPS CHECK GOOD.

Part: SKIN — CRACKED (T/E FLAP) · airframe 22,083 hrs · 29,933 cycles

LEFT NACELLE FLAP CRACKED ON LOWER SIDE. REINFORCEMENT ADDED OVER AFFECTED AREA IAW EMB120 51-10-02.

Part: FRAME — CORRODED (PAX DOOR) · airframe 21,679 hrs · 29,435 cycles

INTERGRANULAR CORROSION FOUND IN FORWARD TOP INTERNAL AREA ACCESS HOLE ON PASSENGER DOOR. REMOVED AND REPLACED THE CORRODED FRAME IAW EMB SRM 51-40-02 AND 51-00-00.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 20,714 hrs · 28,264 cycles

NR 2 ENGINE T6 INDICATOR FLUCTUATES AT TAKEOFF POWER SETTINGS. CAUSED ABORTED TAKEOFF. REPLACED RT ENGINE T-6 INDICATOR AND REPOSITIONED THE RIGHT ENGINE BLEED AIR LINE. OPS CHECK GOOD.

Part: ACTUATOR — OUT OF ADJ (NLG) · airframe 19,434 hrs · 26,489 cycles

DURING CRUISE AT FL 260 NOSE GEAR RED A LIGHT ILLUMINATED. WHEN LANDING GEAR WAS RECYCLED IT EXTENDED NORMALLY; HOWEVER, WHEN RETRACTED BOTH RED A & B LIGHTS REMAINED ILLUMINATED AND VIBRATION AND NOISE WERE NOTICEABLE. GEAR EXTENDED NORMALLY. ADJUSTED NOSE LANDING GEAR ACTUATING CYLINDER IAW EMB120 MM 32-32-11. PERFORMED OPERATIONAL CHECK IAW EMB120 MM 32-30-00. OPS CHECK GOOD.

Part: ACTUATOR — FAILED (RUDDER) · airframe 19,261 hrs · 26,230 cycles

ON LANDING APPROACH AT APPROXIMATELY 130 KNOTS WITH THE YAW DAMPER OFF, UNABLE TO MOVE THE RIGHT RUDDER PEDAL TO THE RIGHT PAST APPROX .25 TRAVEL. NO ASSOCIATED RUDDER LIGHTS ILLUMINATED. REPLACED BLUE SYSTEM RUDDER LINEAR ACTUATOR. S/N IN 0142, S/N OUT 611 RUDDER SYSTEM CHECKED GOOD WITH NO LEAKS.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 19,075 hrs · 25,981 cycles

WHEN SELECTING FLAPS 45 DEGREES, GET DISAGREEMENT. OUTBOARD INDICATING LIGHTS FLASHING. CLEANED FLAP TRACKS AND OPERATED FLAPS. COULD NOT DUPLICATE. OPS CHECK GOOD.

Part: CONNECTOR — CONTAMINATED (TE FLAP SYSTEM) · airframe 18,987 hrs · 25,871 cycles

FLAP DISAGREEMENT AFTER TAKEOFF WHEN RETRACTING FLAPS TO 0 DEGREES. QRH PROCEDURES COMPLIED WITH AND DISAGREEMENT REMAINED. RETURNED TO SLC. CLEANED GLYCOL FROM OUTBOARD FLAP CANNON PLUGS. CYCLED FLAPS SEVERAL TIMES, INDICATION AND OPS CHECK GOOD.

Part: STRIKER — OUT OF ADJ (MLG DOOR)

AFTER TAKEOFF, THE RIGHT LANDING GEAR WOULD NOT RETRACT, TRIED CYCLING THE GEAR BUT STILL WOULD NOT RETRACT. RETURNED TO PSP. ADJUSTED RIGHT OUTBOARD FOWARD GEAR DOOR SEQUENCE VALVE STRIKER THREE TURNS. SWUNG GEAR, OPS CHECKS GOOD.

Part: CLAMP — LOOSE (RT PACK)

INFLIGHT RIGHT DUCT LEAK LIGHT ILLUMINATED. COMPLIED WITH QUICK REFERENCE HANDBOOK AND LIGHT EXTINGUISHED JUST PRIOR TO ENGINE SHUTDOWN. THE RIGHT BLEED WAS NOT IN USE. REPLACED CLAMP TO RIGHT COOLING TURBINE. RAN PACK AND NO LEAKS WERE NOTED. SYSTEM OPS CHECK GOOD.

Part: VALVE — FAILED (LT ENGINE)

INFLIGHT LEFT ENGINE INLET DEICE FAIL. FOLLOWED QRH. RETURNED TO FAT. REPLACED LEFT INLET EJECTOR VALVE AND SERVICED DEICE SYSTEM WITH ALCOHOL LUBE MIX.

Part: DEICE — FAILED (LT ENGINE INLET)

IN FLIGHT LEFT ENGINE INLET DEICE FAILED, FOLLOWED QRH. RETURNED TO FAT. REPLACED FLEX HOSE TO LEFT ENGINE INLET DEICE BOOT. RAN ENGINES, COULD NOT DUPLICATE FAILURE. SWAPPED PRESSURE SWITCHES RIGHT TO LEFT INLETS FOR TROUBLESHOOTING.

Part: TIMER — FAILED (LT ENGINE)

LEFT ENGINE INLET FAILED 3 TIMES. RESET PER QRH AND AFTER 5 SECONDS KEPT ON FAILING. RETURNED TO FAT. REPLACED LEFT ENGINE INLET DEICE TIMER IAW MM 30-60-01, OPS CHECKS GOOD.

Part: UPLOCK HOOK — OUT OF ADJUST (RT MLG)

RIGHT MAIN GEAR ABNORMAL INDICATION UPON RETRACTION. THE RED A,B SYSTEM LIGHT WOULD NOT EXTINGUISH WITH GEAR HANDLE IN THE UP POSITION. RETURNED TO SLC. ADJUSTED LEFT AND RIGHT MAIN UPLOCK HOOK IAW MM 32-32-09. CHECKED ADJUSTMENT OF GEAR INDICATION IAW MM 32-61-01. CHECKED FREE FALL AND ELECTRIC OVERRIDE AND CYCLED GEAR 20 TIMES. ALL CHECKS GOOD.

Part: ANTENNA — CORRODED (RADIO ALT)

FORWARD RADIO ALTIMETER ANTENNA NEEDS REPLACEMENT FOR CORROSION. REMOVED AND REPLACED FORWARD RADIO ALTIMETER ANTENNA IAW MM 34-42-00.

Part: ACTUATOR — DIRTY (LT TE FLAP)

AFTER TAKEOFF ON FLAP RETRACTION, OUTBOARD FLAP DISAGREEMENT. RETURNED TO FIELD. CLEANED DE-ICE FLUID OUT OF OUTBOARD FLAP LEFT SIDE ACTUATOR, INSPECTED RIGHT OUTBOARD ACTUATOR, SWUNG GEAR NUMEROUS TIMES, WITH NO OTHER PROBLEMS.

Part: CONNECTOR — CONTAMINATED (TE FLAPS)

FLAPS DID NOT RETRACT AFTER TAKEOFF, HAD DISAGREEMENT WITH OUTBOARD PAIR. RETURNED TO FIELD. FOUND FLUID ON CANNON PLUG FOR LEFT OUTBOARD FLAP. CLEANED CANNON PLUG ON OUTBOARD FLAPS ON LEFT AND RIGHT SIDES, OPS CHECKS GOOD.

Part: TEST RELAY — MALFUNCTIONED (BLUE HYD SYST)

BLUE HYDRAULIC SYSTEM FLUID OVERHEAT LIGHT CAME ON DURING THE FLIGHT. DIVERTED TO FAT. REPLACED TEST RELAY K45. ALL TESTS AND CHECKS FOUND GOOD.

Part: DN LOCK ACT — MALFUNCTIONED (RT MLG)

AFTER TAKEOFF, RT MAIN GEAR STAYED DOWN, RETURNED FOR LANDING AT LAX. REPLACED RT GEAR SEQUENCE VALUE, LEAK AND OPS CKS GOOD. FAILED TEST FLIGHT, FOUND RT DOWN LOCK ACTUATOR SLOW TO UNLOCK GEAR. INSTALLED SERVICEABLE UNIT AND OPS CKS GOOD. CYCLED LANDING GEAR ON TEST FLIGHT, ALL SYST EMS NORMAL.

Part: ACTUATOR — OUT OF ADJUST (RT MLG)

RT MLG WOULD NOT RETRACT, CYCLED 3 TIMES. ADJUSTED RT MLG ACTUATOR IAW MM 32-32-10.

Part: RETRACT MECH — LACK OF LUBE (RT MLG)

RT MAIN WOULD NOT RETRACT, CYCLED 3 TIMES. LUBRICATED RT MLG MAIN BRAKE ATTACH POINTS, SWUNG GEAR SEVERAL TIMES AND OPS CKS GOOD.

Part: VALVE — MIS INSTALLED (RT ENGINE)

AFTER TAKEOFF, THE RIGHT RED DUCT LIGHT ILLUMINATED. COMPLETED CHECK LISTS AND SHUTDOWN THE RIGHT ENGINE, AIRCRAFT RETURNED TO AIRPORT. FOUND THE RIGHT DE-ICE PRESSURE REGULATING VALVE INSTALLED BACKWARDS, CAUSING BLEED AIR TO VENT INFO FWD WING BOOT FAIRING AREA. REMOVED AND REPLACED VALVE WITH SERVICEABLE UNIT IAW MM 30-10-06. OPERATED DE-ICING SYSTEM, OPS CHECKS GOOD. DUCT LEAK LIGHT DID NOT ILLUMINATE DURING GROUND RUNS.

Part: AURAL WARNING — ACTIVATED (COCKPIT)

UPON STARTING TAKEOFF ROLL, TRIM AURAL WARNING WENT OFF. RETURNED TO GATE AFTER ABORTING TAKE OFF. COULD NOT DUPLICATE PROBLEM. CYCLED TRIM AND POWER LEVER SWITCHES. OPS CKS GOOD. POWERED AIRCRAFT DOWN AND UP.