N190SW

Part: SELECTOR — FAULTY (COCKPIT) · airframe 41,760 hrs · 51,119 cycles

WHEN FLAP LEVER WAS MOVED, CONTROL FAULT MESSAGE. REMOVED AND REPLACED FLAP SELECTOR IAW EMB MM 22-50-01. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAP) · airframe 41,707 hrs · 51,059 cycles

RECEIVED CONTROL FAULT ON APPROACH WHEN SELECTING FLAPS 25 DEGREES. REMOVED AND REPLACED RIGHT INBOARD, RIGHT NACELLE, AND RIGHT OUTBOARD FLAP ACTUATORS IAW EMB MM 27-50-00. OPERATIONAL CHECK GOOD. P/N 308200-1005, S/N 0091 AND S/N 0834, P/N 320300-1007, S/N 0036.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 41,209 hrs · 50,484 cycles

FRONT CABIN EXIT LIGHT NEAR MAIN CABIN DOOR IS INOPERATIVE. RELAMPED AS REQUIRED, OPERATIONAL CHECK GOOD.

Part: DUCT — LOOSE (A/C PACK) · airframe 40,937 hrs · 50,149 cycles

LEFT PACK MAKES A SQUEALING SOUND WITH LOW SELECTED. IN FLIGHT, PACK CREATES A HOT, SMOKEY SMELL UNTIL TURNED OFF. TIGHTENED CLAMPS AT LEFT PACK. COULD NOT DUPLICATE SMELL. OPERATIONAL CHECK GOOD.

Part: SIGNAL COND UNIT — MALFUNCTIONED (RT ENGINE) · airframe 40,789 hrs · 49,983 cycles

ON T/O ROLL, RIGHT ENGINE AUTO-FEATHERED DURING POWER LEVER ADVANCEMENT. REMOVED AND REPLACED RIGHT HAND ENGINE TORQUE SIGNAL CONDITIONER IAW MM 77-11-01. OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 40,714 hrs · 49,895 cycles

EMERGENCY LIGHT ON OVERHEAD BIN ROW 9 DOESN'T ILLUMINATE. REPAIRED WIRING TO EMERGENCY LIGHT ON OVERHEAD BIN. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,269 hrs · 49,347 cycles

REAR SECTION EMERGENCY LIGHTS DOES NOT ILLUMINATE. REPLACED AFT ELBP WITH A SERVICEABLE UNIT. OPS CHECK GOOD. P/N 17366-04-001, S/N OFF 397.

Part: ANNUNCIATOR — MALFUNCTIONED (TE FLAPS) · airframe 40,254 hrs · 49,320 cycles

ON THE GROUND WITH FLAP LEVER AT UP POSITION, CONTROL FAULT, FLAP AND ADVANCED SWS APPEAR INTERMITTENTLY. REPLACED FLAP ANNUNCIATOR IAW MM 20-21-00, MM 27-50-05. S/N OFF: 2151. REPAIRED AND REPOSITIONED WIRE W110-2909-2H WHICH WAS CHAFING AND SHORTING ON FLAP ANNUNCIATOR CASE IN OVERHEAD PANEL.

Part: FRAME — CRACKED (NR 1 NACELLE) · airframe 39,925 hrs · 48,939 cycles

CHANNEL CRACKED FORWARD OF FRAME NR 1 ON RIGHT ENGINE NACELLE AT TOP INBOARD SIDE AT UPPER NUT PLATE STRIP. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INBOARD SECTION OF CHANNEL FORWARD OF FRAME NR 1 ON RIGHT NACELLE IAW SRM 54-10-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 39,925 hrs · 48,939 cycles

UNDER FLOOR PANEL 243 DF BRACKET BUCKLED AND CRACKED. DISCOVERED DURING C-CHECK INSPECTION. FITTED AND INSTALLED NEW FLOOR SUPPORT BRACKET. P/N: 120-14243-001.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,925 hrs · 48,939 cycles

CRACK ON CENTER FRAME RIB BELOW E-BRAKE VALVE BOX INBOARD SIDE. DISCOVERED DURING C-CHECK INSPECTION. PERFORMED REPAIR ON CENTER FRAME RIB BELOW E-BRAKE VALVE BOX INBOARD SIDE IAW SRM 51-70-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,832 hrs · 48,823 cycles

ENTRY EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BULB IN ENTRYWAY. OPS CHECKS GOOD.

Part: SELECTOR — MALFUNCTIONED (TE FLAPS) · airframe 39,772 hrs · 48,729 cycles

ON DESCENT INTO SGU- LOW SPEED ALARM WENT OFF AND WOULD NOT STOP DESPITE NO ICING CONDITIONS AND ONLY STANDARD ICE ON. LANDED IN SGU WITHOUT INCIDENT AND WHEN THE ALARM STOPPED, THE SMOKE STOPPED. REMOVED AND REPLACED FLAP SELECTOR PANEL IAW MM 27-50-01. S/N OFF: 120131, OPS CHECK GOOD IAW MM 27-50-00. REPLACED LOW SPEED ALARM PANEL IAW MM 30-90-01. LOW SPEED ALARM OPS CHECK GOOD IAW MM 30-90-00. P/N: 120-64199-001, S/N ON: 1209998612, S/N OFF: 1209994742.

Part: WIRE HARNESS — FAULTY (RT MLG) · airframe 39,429 hrs · 48,280 cycles

WHEN SELECTING THE GEAR DOWN, ONLY THE RIGHT MAIN EXTENDED. RIGHT GREEN B-LIGHT AND ALL DISAGREEMENTS ILLUMINATED. THE ELECTRICAL OVER RIDE PROCEDURE IN THE QRH WAS CONDUCTED, RESULTING IN A SUCCESSFUL EXTENSION. REMOVED & REPLACED RIGHT MAIN GEAR SYSTEM-A PROX SENSOR HARNESS WITH A SERVICEABLE PART PER MM 32-61-01 401. CHECKS NORMAL.

Part: APU — LEAKING · airframe 39,216 hrs · 48,003 cycles

CAPT REPORTS SMOKE IN COCKPIT FROM AIR CONDITIONING SYSTEM. BOTH LT AND RT AIR CONDITIONING PACKS ARE COVERED IN OIL. APU BLEED SYSTEM IS PUTTING OIL INTO PACKS. REMOVED AND REPLACED THE APU IAW RII 49-301. OPS AND LEAK CHECKS GOOD.

Part: SERVO — MALFUNCTIONED (AUTOPILOT SYS) · airframe 39,079 hrs · 47,843 cycles

WITH AUTOPILOT ENGAGED ON EITHER C/A OR F/O SIDE, AP MAKES UNCOMMANDED SLOW ROLL LEFT OR RIGHT. AUTOPILOT FAIL LIGHT ON MAP DOES NOT ILLUMINATE. REMOVED AND REPLACED THE AILERON AUTOPILOT SERVO IAW EMB120 MM 27-00-03. AUTOPILOT OPS CHECK GOOD IAW MM 22-10-00.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 38,751 hrs · 47,455 cycles

WHITE EMERGENCY TRACK LIGHTING A-BEAM GALLEY INOP, SINGLE LIGHT. INSPECTED AND FOUND BROKEN WIRE. REPAIRED BROKEN WIRE ON WHITE EMERGENCY LIGHT TRACK A-BEAM GALLEY IAW EMB120 WM 20-21-00. OPS CHECK GOOD.

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 38,221 hrs · 46,778 cycles

FLAP CONTROL FAULT FOR INBOARD FLAPS UPON RETRACTING FLAPS AFTER LANDING. REMOVED AND REPLACED FLAP ANNUNCIATOR PANEL AND FCU FOR TROUBLESHOOTING. RAN FLAPS UP AND DOWN SEVERAL TIMES. OPS CHECK GOOD AT THIS TIME.

Part: CONNECTOR — DAMAGED (TE FLAP ACTUATOR) · airframe 38,217 hrs · 46,769 cycles

FLAP CONTROL FAULT INDICATED FOR INBOARD FLAPS. FLAPS WOULD NOT RETRACT ON THE GROUND. REMOVED AND REPLACED CONNECTOR FOR LEFT INBOARD FLAP ACTUATOR WITH A NEW PART. OPS CHECK OF FLAPS PERFORMED SATISFACTORY. P/N ON MS3476L12-10S.

Part: BUSHING — LACK OF LUBE (A/C PACK) · airframe 38,042 hrs · 46,531 cycles

BOTH AIR CONDITIONING PACKS FAILED IN THE NORMAL POSITION. SMOKE FILLED THE CABIN AND COCKPIT. VERY LIMITED AIRFLOW IN LOW/LOW CONFIGURATION. LUBRICATED LEFT AND RIGHT ACTUATOR PIVOT BUSHINGS, CLEANED OIL FROM CONNECTORS. FREED RIGHT RAM AIR CHECK VALVE FROM OBSTRUCTION. OPS CHECK GOOD. RAN AIR CONDITIONING EXTENSIVELY, NO FURTHER PACK FAILURES NOTED.

Part: WIRE HARNESS — MALFUNCTIONED (LT MLG) · airframe 37,785 hrs · 46,151 cycles

ON TAKEOFF COULDN'T GET THE LANDING GEAR TO GO UP. ALL THE LIGHTS WOULD BE ON BUT THE LEFT RED A. RETURNED TO FAT. REMOVED AND REPLACED LEFT MAIN GEAR A-PROXIMITY HARNESS IAW 32-61-01. OPS CHECK GOOD, LEAK CHECK OF VALVE IS GOOD.

Part: PUMP — FLUCTUATES (RT ENGINE) · airframe 37,496 hrs · 45,728 cycles

AUX FEATHER PUMP BROKEN, RT ENGINE TORQUE FLUCTUATES 3 PERCENT TO 4 PERCENT AT CRUISE. REMOVED AND REPLACED AUX FEATHER PUMP.

Part: TERMINAL BLOCK — LOOSE (AHAR) · airframe 37,473 hrs · 45,703 cycles

MULTIPLE FAILURES ASSOCIATED WITH THE AHAR: HSI ROTATES 60 DEGREES-BOTH SIDES THEN CENTERS ADI-COMPUTER FAILURE LT SIDE ASSOCIATED WITH A GYRO FLAG RIGHT SIDE COMPUTER FAILURE-NO GYRO FLAG.FOUND SEVERAL NUTS ON TB0033 LOOSE AND RUBBER NIPPLE ON W138-0001-2 MISSING. INSTALLED WASHERS AND TIGHTENED NUTS ON TB0033. INSTALLED RUBBER NIPPLE ON WIRE W138-0001-2. INSTALLED RUBBER NIPPLE ON W158-0001-2 AND REPLACED ALL TERMINAL ENDS ON WIRES THAT ATTACH TO STUD NR 2 AND TIGHTENED ALL NUTS ON TB0034 IAW EMB WM 20-00-00. OPERATIONAL CHECKS GOOD AT THIS TIME.

Part: CONTROL UNIT — MALFUNCTIONED (PROPELLER) · airframe 37,473 hrs · 45,703 cycles

DURING CLIMB, RIGHT NP DROPPED TO 96 PERCENT. TURNED OFF EEC WITH POWER LEVER AT FLIGHT IDLE AND CL MAX T6 780, TORQUE 97 PERCENT AND NP 56 PERCENT. WE FEATHERED THE ENGINE PER QRH PRECAUTIONARY ENGINE SHUT DOWN AND DIVERTED TO CYS. REPLACED RT ENGINE PCU IAW MM 61-21-00. OPS CHECK GOOD. TRANSFER TUBE REMOVAL AND REINSTALLATION DONE PER 61-10-00. NO LEAKS NOTED.SN OFF 1213.

Part: RECEIVER — FAILED (ADF) · airframe 37,050 hrs · 45,210 cycles

WHILE HOLDING AT WYS, ADF FAILED IN FLIGHT. DIVERTED TO IDA. REPLACED ADF RECEIVER. OPS CHECKS GOOD IAW MM 34-53-00.

Part: BRAKE — SEIZED (RT MLG) · airframe 36,947 hrs · 45,091 cycles

ON TAXI OUT THE OUTBOARD RIGHT MAIN TIRE POPPED. FOUND NR 4 BRAKE LOCKED UP. REMOVED AND REPLACED NR 4 BRAKE IAW MM 32-41-05. LEAK CHECKS GOOD.

Part: SERVO — BINDING (AUTOPILOT SYS) · airframe 36,822 hrs · 44,948 cycles

RUDDER PEDALS FEEL LIKE RUDDERS ARE BINDING UP. INSTALLED SERVICEABLE SVO65 AUTOPILOT SERVO. OPS CHECKS GOOD.

Part: COMPUTER — MALFUNCTIONED (E/E BAY) · airframe 36,689 hrs · 44,795 cycles

AUTOPILOT/YAW FAILURE IN FLIGHT. INSTALLED SERVICEABLE AHC85 COMPUTER. OPS CHECKS GOOD. CAPTAIN'S COMPUTER AND GYRO FLAGS ARE INTERMITTENT IN FLIGHT. INSTALLED SERVICEABLE AHC85 COMPUTER. OPS CHECKS GOOD.

Part: ACTUATOR — FAILED (T/E FLAP) · airframe 36,410 hrs · 44,493 cycles

IN CRUISE FLIGHT, FLAP LIGHT ON MAP PANEL ILLUMINATED ALONG WITH ADVANCED SWS LIGHT. FLAP INBOARD LIGHTS WERE ILLUMINATED. COMPLIED WITH QRH PROCEDURES. FLAPS WOULD NOT RESET. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR. REPLACED ACTUATOR CANNON PLUG. OPERATED FLAPS SEVERAL TIMES, OPS CHECK GOOD.

Part: COMPUTER — FAULTY (NR 2) · airframe 36,358 hrs · 44,424 cycles

FIRST OFFICER'S EHSI TURNED 30-40 DEGREES RIGHT WHILE CLIMBING STRAIGHT OUT. FIRST OFFICER'S RMI HEADING INFORMATION MATCHES CAPTAIN'S EHSI, RMI AND MAGNETIC COMPASS. RESET FIRST OFFICER'S HEADING BY SWITCHING FIRST OFFICER'S COMPASS COMPENSATOR MOMENTARILY TO DG MODE. NO ASSOCIATED FLAGS OR WARNINGS. REPLACED NR 2 AHRS COMPUTER AND PERFORMED ORIENTATION. OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 36,389 hrs · 44,467 cycles

DURING CLIMBOUT, FIRST OFFICER'S HEADING INDICATOR STARTED STICKING WITH A 30 DEGREE DIFFERENCE BETWEEN HI'S WITH NO ASSOCIATED FLAGS OR ALARMS. AFTER TURNING BACK TOWARD DEN, THE GYRO BEGAN WORKING PROPERLY. FIRST OFFICER RECEIVED COMPUTER FLAG DURING TAXI IN. RERACKED HEADING COMPUTER. OPS CHECK GOOD ON GROUND.

Part: WIRE — LOOSE (CABIN) · airframe 36,129 hrs · 44,166 cycles

EMERGENCY LIGHTS IN FLOOR TRACK WILL NOT ILLUMINATE. SECURED LOOSE WIRE AT CONNECTION BELOW FLOOR AT ROW 3. EMERGENCY LIGHTS, OPS CHECK OK.

Part: CONTROL CABLE — CORRODED (ELEVATOR) · airframe 36,129 hrs · 44,166 cycles

RIGHT OUTBOARD AFT ELEVATOR CABLE AND RIGHT AND LEFT AFT ELEVATOR TRIM CABLES SHOWING SIGNS OF WEAR AND CORROSION. REPLACED RIGHT OUTBOARD AFT ELEVATOR CABLE AND RIGHT AND LEFT AFT ELEVATOR TRIM CABLES IAW EMB120 MM 27-00-01.

Part: CONTROL CABLE — CORRODED (RUDDER) · airframe 36,129 hrs · 44,166 cycles

LEFT RUDDER AFT OUTBOARD AND INBOARD CABLES SHOW SIGNS OF CORROSION. REPLACED LEFT RUDDER AFT OUTBOARD AND INBOARD CABLES IAW EMB120 MM 27-00-01.

Part: ANNUNCIATOR — FAULTY (COCKPIT) · airframe 36,076 hrs · 44,093 cycles

FLAPS INOP - ALL CONTROL FAULT, DISAGREEMENT AND ASYMMETRY LIGHTS ON. COULD NOT CLEAR ANY OF THE FAULT LIGHTS. FLAP CONTROL PANEL FLAP PORTION INDICATOR (ALL) INDICATED FLAPS UP WHEN FLAPS WERE 15 DEGREES, 25 DEGREES OR 45 DEGREES POSITION PHYSICALLY. CONDITION WAS INTERMITTENT ON TAXI BACK. REMOVED AND REPLACED FLAP CONTROL UNIT AND FLAP ANNUNCIATOR ASSEMBLY. OPS CHECK GOOD IAW 27-50-00.

Part: TAIL CONE — OUT OF POSITION (FUSELAGE) · airframe 35,952 hrs · 43,932 cycles

CONTROL YOKE BINDS ABOUT HALFWAY THROUGH FORWARD AND AFT TRAVEL WITH ELEVATOR TRIM IN THE GREEN ARC. BIND IS LESS WITH ELEVATOR TRIM FULL FORWARD AND GOES AWAY COMPLETELY WITH TRIM FULL AFT. REPOSITIONED TAIL CONE TO PREVENT RUBBING ON ELEVATOR. OPS CHECK GOOD. NO FURTHER DEFECTS FOUND.

Part: TIMER — MALFUNCTIONED (LT ENGINE) · airframe 35,529 hrs · 43,433 cycles

LEFT ENGINE AIR INLET FAILED 14 MINUTES INTO FLIGHT PASSING THROUGH FL180. TURNED OFF FOR A FEW MINUTES AND THEN ON FOR ANOTHER 14 MINUTES DURING RETURN TO SLC AND IT DID NOT FAIL AGAIN. REMOVED AND REPLACED LEFT ENGINE DEICE TIMER IAW MM 30-20-05. REMOVED AND REPLACED DEICE MONITOR IAW MM 30-00-01. OPS CHECK GOOD. DE-ICE MONITOR P/N 0552-01-001, S/N OFF 132/10-87.

Part: HARNESS — FAULTY (RT MLG) · airframe 35,508 hrs · 43,409 cycles

AFTER GEAR RETRACTION, RIGHT MAIN GEAR B-GREEN LIGHT REMAINS ILLUMINATED WITH ALL OTHER LIGHTS OUT. RECYCLED GEAR WITH SAME RESULT. B-GREEN LIGHT DID FINALLY GO OUT 10 MINUTES AFTER SECOND GEAR RETRACTION. REPLACED RIGHT MLG PROXIMITY HARNESS-B IAW 32-61-01. GEAR CYCLED THREE TIMES. OPS CHECK GOOD. P/N: 120-22622-501, S/N ON: T02148, S/N OFF: A005710710.

Part: ACTUATOR — FAILED (T/E FLAP) · airframe 35,471 hrs · 43,366 cycles

CONTROL FAULT WOULD NOT RESET PER QRH. INBOARD FLAPS SHOWED 10 DEGREES. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR PER MM 27-50-00. OPS CHECK, LEAK CHECKS GOOD.

Part: ROLLER — WORN (T/E FLAP) · airframe 35,446 hrs · 43,333 cycles

CONTROL FAULT ON INBOARD FLAPS. FOUND CONTAMINATION IN INBOARD ACTUATOR CANNON PLUGS. ALSO FOUND WORN ROLLERS ON LEFT INBOARD FLAP. CLEANED CANNON PLUGS AND REMOVED AND REPLACED ROLLER LEFT INBOARD FLAP. REINSTALLED PANELS. OPS CHECK GOOD. ROLLER P/N: PE61026-1.

Part: DOOR — MISSING (LT HYDRAULIC) · airframe 35,508 hrs · 43,409 cycles

LEFT HYDRAULIC DOOR MISSING. (DISCOVERED ON WALK AROUND INSPECTION.) FIT AND INSTALLED A NEW LEFT HYDRAULIC BAY DOOR IAW EMB SRM 51-00-00 AND 51-40-02.

Part: ACTUATOR — FAILED (T/E FLAP) · airframe 35,348 hrs · 43,227 cycles

CONTROL FAULT ON FLAPS ON TAKEOFF. REPLACED INBOARD FLAP ACTUATOR IAW MM 27-50-00. OPS AND LEAK CHECK GOOD.

Part: SWITCH — INOPERATIVE (COCKPIT) · airframe 35,348 hrs · 43,227 cycles

FIRST OFFICER'S PTT SWITCH INOP. RETURNED TO SLC. INSTALLED NEW SWITCH. FIRST OFFICER'S PTT OPS CHECK GOOD.

Part: PROXIMITY SENSOR — FAILED (ELEVATOR TRIM) · airframe 35,258 hrs · 43,121 cycles

ABORTED TAKEOFF WHEN WE BROUGHT THE POWER UP DUE TO TAKEOFF TRIM WARNING. TRIM CONFIRMED SET AT 4 IN THE GREEN BAND.REMOVED AND REPLACED LEFT TRIM PROXIMITY SENSOR. OPS CHECK GOOD. P/N: ATG120TR

Part: EEC — MALFUNCTIONED (LEFT ENGINE) · airframe 35,224 hrs · 43,083 cycles

LEFT EEC WENT TO MANUAL ON TAKEOFF POWER UP. ABORTED TAKEOFF.RESET LEFT EEC. OPS CHECK GOOD.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 35,206 hrs · 43,061 cycles

BLUE HYDRAULIC FILTER LIGHT ILLUMINATED , THEN MAIN PUMP LOW PRESSURE LIGHT ILLUMINATED WHEN TRIED FLAPS 15 DEGREES LOST ALL BLUE HYDRAULIC LEVEL AND PRESSURE. HYD FLUID LEAKING FROM R MAIN GEAR BAY.REPAIRED BROKEN HYDRAULIC LINE, CHANGED ENGINE DRIVEN PUMP, PERFORMED HYDRUALIC FLUSH AND CHANGED ALL FILTERS IAW MM 29-00-00 OPS AND LEAK CHECK GOOD PN ON PV3-022-29 SN MX-490588 SN MX-523017

Part: INDICATOR — INOPERATIVE (RADAR SYSTEM) · airframe 35,091 hrs · 42,928 cycles

RADAR DISPLAY + TCAS DISPLAY WXR-270 MADE A BRIGHT FLASH AND WENT INOP. REMOVED & REPLACED RADAR TRANSCEIVER WTX-250B, RADAR/TCAS INDICATOR IND-270, AND RADAR ANTENNA ANT-318 IAW AMM 34-41-00. OPS CHECK GOOD. ANT-318 PN ON 622-2504-001

Part: ANNUNCIATOR — FAULTY (COCKPIT) · airframe 4,013 hrs · 4,594 cycles

FLAP ASYMMETRY, CONTROL FAULT, DISAGREEMENT LIGHTS AND MAP FLAP AND ADVANCED SWS LIGHTS ILLUMINATED BRIEFLY INFLIGHT AS AIRCRAFT LEVELED IN CRUISE FLIGHT. REMOVED AND REPLACED FLAP ANNUNCIATOR IAW 27-50-00. OPERATED FLAPS THROUGH RANGE OF TRAVEL SEVERAL TIMES. OPS CHECK GOOD. S/N OFF: 0200

Part: HOSE — FAILED (LT ENG DEICE SYS) · airframe 34,696 hrs · 42,455 cycles

LEFT ENGINE AIR INLET FAILED. RETURNED TO THE FIELD. REPLACED HOSE TO LEFT ENG INLET DEICE. OPS CHECKS GOOD.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 3,840 hrs · 4,388 cycles

WHEN SELECTING GEAR UP ON TAKEOFF, EXPERIENCED COMPLETE LOSS OF HYDRAULIC GREEN SYSTEM. RETURNED TO SLC. REPLACED FLEX LINE LEFT GEAR OUTBOARD LINE OVER DRAG BRACE.

Part: CARBON SEAL — LEAKING (LT ENGINE) · airframe 34,641 hrs · 42,388 cycles

LEFT ENGINE INBOARD NACELLE HAS LEAK (APPEARS TO BE FUEL). PERFORMED NECESSARY SHUT DOWN AND RETURNED TO SLC. REMOVE AND REPLACE LEFT ENGINE BREATHER CARBON SEAL IAW 72-30-00. LEAK CHECK GOOD.

Part: ACTUATOR — FAILED (T/E FLAP) · airframe 34,355 hrs · 42,064 cycles

FLAP CONTROL FAULT INTERMITTENT IN FLIGHT. TROUBLESHOT SYSTEM IAW EMB FAULT ISOLATION MANUAL 27-50-00. FOUND RIGHT OUTBOARD FLAP ACTUATOR BAD. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR IAW EMB MM 27-50-09 AND RII 27-307. SYSTEM OPS CHECK GOOD. P/N: 320300-1007, S/N ON: 1212, S/N OFF: 0026A.

Part: CONTROL HANDLE — FAULTY (COCKPIT) · airframe 34,312 hrs · 42,017 cycles

CONTROL FAULT AT FLAPS 15 DEGREES. REMOVE AND REPLACE FLAP CONTROL HANDLE IAW 27-50-01. OPS CHECK GOOD. P/N ON: 120-42642-001, S/N ON: 120128, P/N OFF: 120-42642-507, S/N OFF: 120-283.

Part: ACTUATOR — FAILED (LT FLAP) · airframe 34,279 hrs · 41,980 cycles

INBOARD FLAPS FAILED TO RETRACT UPON LANDING. REMOVE AND REPLACE LEFT INBOARD FLAP ACTUATOR IAW MM 27-50-00. REPLACED BOTH INBOARD ROLLERS AND MOVEABLE OUTBOARD ROLLER ON LEFT INBOARD FLAP IAW 27-50-12. OPS AND LEAK CHECK GOOD.

Part: PROXIMITY SENSOR — FAULTY (LT MLG) · airframe 34,103 hrs · 41,772 cycles

ON TAKEOFF THE LEFT LANDING GEAR FAILED TO RETRACT. UPON RECYCLING, THE GEAR WOULD NOT EXTEND. RETURNED TO SLC. REMOVED AND REPLACED A SYSTEM DOWNLOCK PROX SENSOR AND B-SYSTEM DOWNLOCK PROX SENSOR AND CANNON PLUG AT P0136 WITH SERVICEABLE UNIT IAW EMB 120 MM 32-61-01, OPS CHECK GOOD.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 33,789 hrs · 41,403 cycles

APU DUCT LEAK ILLUMINATED INFLIGHT WITH APU NOT OPERATING AND BLEEDS CLOSED. RETURNED TO SLC. CHECKED ALL DUCT LEAK SENSORS FOR APU BLEEDS IAW MM 36-20-00. RAN APU BLEEDS TO CHECK FOR LEAKS, NO LEAKS NOTED. DUCT LEAK SENSORS ALL OPS CHECK GOOD. NO FAULTS DETECTED. UNABLE TO DUPLICATE SQUAWK.

Part: PROXIMITY SWITCH — OUT OF ADJ (MLG) · airframe 33,698 hrs · 41,296 cycles

ON CLIMBOUT AFTER TAKEOFF RED B-RIGHT GEAR LIGHT CAME ON. CYCLED GEAR PER QRH ON GEAR RETRACTION RT MAIN DID NOT FULLY COME UP. EXTENDED GEAR AND GOT GOOD 3 GREEN INDICATION. RETURNED TO SLC. REPLACED TIGHT GEAR UPLOCK B-SYSTEM PROXIMITY SWITCH IAW 32-61-01. ADJUSTED RIGHT MAIN LANDING GEAR ACTUATOR IAW 32-30-00. CYCLED GEAR SEVERAL TIMES, FOUND TO OPERATE NORMAL.

Part: TAB — BINDING (ELEVATOR TRIM) · airframe 33,648 hrs · 41,238 cycles

INFLIGHT WITH F/O AUTOPILOT ENGAGED THE AIRCRAFT LEVELED OFF TO CATCH THE COURSE AND FELT A VIBRATION LIKE TENSION BEING RELEASED ON THE CABLES TO THE AILERON. THE YOKE VIBRATED LEFT AND RIGHT, THEN EVERYTHING RETURNED TO NORMAL. DISENGAGED AUTOPILOT, TESTED AILERON/ELEVATOR TRAVEL, SEEMED OK. FOUND LEFT AILERON TRIM TAB BINDING AND POPPING. INSTALLED NEW TRIM TAB, BEARINGS AND REINSTALLED TRIM TAB IAW EMB MM 22-12-02. OPS CHECK GOOD.

Part: SERVO — MALFUNCTIONED (AUTOPILOT) · airframe 33,619 hrs · 41,204 cycles

WHILE PERFORMING FLIGHT CONTROL TEST ON TAXI CHECK, THE ELEVATOR CONTROL SEEMED TO SNAG OR CATCH ON SOMETHING MIDWAY OF TRAVEL. RETURNED TO GATE. REMOVED AND REPLACED ELEVATOR AUTO PILOT SERVO IAW MM 27-00-03. OPS CHECKS GOOD. P/N ON: 622-5734-002, S/N ON: 5371, S/N OFF: 3893.

Part: ACTUATOR — FAILED (FLAP) · airframe 33,475 hrs · 41,049 cycles

INBOARD FLAP CONTROL FAULT INFLIGHT. NO FLAP HANDLE MOVEMENT. REMOVED AND REPLACED INBOARD FLAP ACTUATOR. CYCLED FLAPS NUMEROUS TIMES OPS CHECKS GOOD. RII 27-307PN ON 320300-1005 SN ON 0030 SN OFF 0421

Part: CONNECTOR — CONTAMINATED (TE FLAP ACTUATOR) · airframe 33,416 hrs · 40,987 cycles

CONTROL FAULT ON FLAPS WHILE TAXIING AIRCRAFT. FOUND INBOARD AND OUTBOARD FLAP ACTUATOR CANNON PLUGS FULL OF DEICE FLUID. CLEANED CANNON PLUGS, OPERATED FLAPS NUMEROUS TIMES IN HANGER AND NO PROBLEMS NOTED.

Part: CONNECTOR — DIRTY (FLAP ACTUATOR) · airframe 33,475 hrs · 41,049 cycles

FLAP CONTROL FAULT WHEN SELECTING FLAPS 45 DEGREES, INBOARD PAIR FLASHING. CLEANED BOTH INBOARD FLAP ACTUATORS CANNON PLUGS WITH CONTACT CLEANER. CYCLED FLAPS THROUGH 4 COMPLETE FAULT FREE CYCLES. OPS CHECK NORMAL.

Part: WIRE — BROKEN (FLAP CONTROL) · airframe 33,475 hrs · 41,049 cycles

FLAP CONTROL FAULT ON LANDING, UNABLE TO RESET. REPAIRED BROKEN WIRE ON LEFT INBOARD FLAP CANNON PLUG. CYCLED FLAPS SEVERAL TIMES. OPS CHECK GOOD.

Part: EJECTOR VALVE — FAILED (DEICE BOOT) · airframe 33,109 hrs · 40,648 cycles

LEADING EDGE DEICE BOOT (MIDDLE/BOTH WINGS) INOP IN FLIGHT. RETURNED TO SLC. WORKS FINE ON GROUND. REMOVED AND REPLACED WING MIDDLE DEICE EJECTOR VALVE GROUND. RAN AIRCRAFT AT LOW AND HIGH PRESSURE AND ALL BOOTS OPS AND LEAK CHECKS OK.

Part: EJECTOR VALVE — FAILED (WING DEICE SYS) · airframe 33,013 hrs · 40,538 cycles

LOSS OF OUTBOARD LEADING EDGE WING DEICE. RETURNED TO SLC. REMOVED AND REPLACED OUTBOARD WING EJECTOR VALVE WITH SERVICEABLE UNIT IAW MM 30-20-04. OPS CHECKS GOOD. P/N ON: 3D237606, S/N: PJ334, S/N OFF: N3517.

Part: CONNECTOR — DAMAGED (AILERON CONTROL) · airframe 32,966 hrs · 40,488 cycles

CONT DISENGAGE LIGHT CAME ON, ON TAKEOFF ROLL. ABORTED TAKEOFF. FOUND BROKEN WIRE AT AILERON DISCONNECT CANNON PLUG BACKSHELL. REMOVED AND REPLACED PINS AT CANNON PLUG IAW MM 20-50-01. CONTROL DISENGAGE INDICATION OPS CHECKS GOOD.

Part: BULB — WRONG PART (ROW 9) · airframe 32,814 hrs · 40,314 cycles

EXIT SIGN ABOVE ROW 9 IN OVERHEAD BIN IS INOP. INSTALLED CORRECT LIGHT BULBS. OPS CHECKS GOOD IAW 33-51-02.

Part: DOWNLOCK SENSOR — FAILED (MLG) · airframe 32,632 hrs · 40,109 cycles

LEFT MAIN SYSTEM ''''A'''' GREEN LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. FOLLOWED QRH WHICH HAD US ATTEMPT TO CYCLE GEAR DOWN. WITH GEAR LEVER DOWN, NO ACTION WITH GEAR AND ALL GEAR LIGHTS EXCEPT LEFT MAIN ''''A'''' RED LIGHT ILLUMINATED. PERFORMED ELECTRICAL OVER RIDE PER QRH AND GEAR EXTENDED, NORMALLY WITH NORMAL INDICATIONS. REPLACED DOWNLOCK A PROX SENSOR IAW MM 32-61-00. OPS CHECKS GEAR IAW MM 32-00-00 GOOD.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 32,519 hrs · 39,979 cycles

AIRCRAFT WOULD NOT PRESSURIZE. RETURNED TO SLC. REMOVED AND REPLACED MANUAL CONTROLS FOR PRESSURIZATIONS. OPS CHECKS GOOD. P/N ON: 912R0201, S/ NON: 762, S/N OFF: 308.

Part: CONTROL BOX — MALFUNCTIONED (MLG) · airframe 32,394 hrs · 39,820 cycles

WHEN LANDING GEAR HANDLE WAS POSITIONED DOWN ALL RED SYSTEM LIGHT LIT UP AND THEN LEFT MAIN GEAR A GREEN LIGHT LIT UP, BUT NONE OF THE GEAR EXTENDED ELECTRICAL OVERIDE PROCEDURE WAS USED, GEAR EXTENDED. REPLACED LANDING GEAR CONTROL BOX WITH SERVICEABLE UNIT IAW MM 323000, OPS CHECKS GOOD. P/N ON: 12038594001, S/N: 12004JR, S/N OFF: 120151.

Part: SENSOR — FAILED (LT MLG) · airframe 32,394 hrs · 39,820 cycles

WHEN PUTTING GEAR DOWN THE LEFT MAIN GREEN A LIGHT WAS THE ONLY GEAR INDICATION THAT CAME ON AND GEAR DID NOT COME DOWN. USED ELECTRICAL OVERRIDE TO GET GEAR DOWN. REPLACED LEFT MLG DOWNLOCK A PROXIMITY SENSOR IAW 326101. ALL GEAR SWINGS CHECK GOOD IAW 323000.

Part: FUEL FILTER — FAILED (FUEL SYSTEM) · airframe 31,745 hrs · 39,074 cycles

FUEL LIGHT ON MAP ON FUEL LIGHT (FILTER LIGHT) ON FUEL PANEL ON AFTER TAKEOFF. RETURNED TO SLC. INSTALLED LEFT LOW AND HIGH PRESS FUEL FILTERS AND NEW NUTS. RAN ENGINE 930 PPH, OPS AND LEAK CHECK GOOD.

Part: SELECTOR KNOB — FAILED (TE FLAP) · airframe 31,643 hrs · 38,956 cycles

FLAP CONTROL FAULT AFTER TAKEOFF FOLLOWED QRH BUT WAS UNABLE TO CORRECT. RETURNED TO SLC. REMOVED FLAP SELECTOR AND INSTALLED SERVICEABLE UNIT, IAW MM 275100, OPS CHECKS GOOD. (P/N 12002642) (S/N 120283) ON, (S/N 120060).

Part: BOOT — INOPERATIVE (RT WING DE ICE)

RIGHT INBOARD WING DE-ICE BOOT INOP. RETURNED TO SLC. FOUND SPLIT IN LEFT INBOARD DE-ICE BOOT. REMOVED BOOT, INSTALLED NEW DE-ICER ON LEFT INBOARD LEADING EDGE.

Part: UPLOCK — OUT OF ADJUST (RT MLG)

RIGHT RED A LIGHT STAYS ON AFTER RETRACTION. RETURNED TO SLC. ADJUSTED RIGHT MLG UPLOCK ROLLER AND UPLOCK PROXIMITY SENSORS IAW EMB 120 MM 32-61-01. OPS CHECK GOOD UPON RETRACTION.

Part: RELAY — FAILED (LANDING GEAR)

LANDING GEAR FAILED TO COME DOWN NORMALLY, HAD TO DROP IT BY ELECTRICAL OVERRIDE. REMOVED AND REPLACED LANDING GEAR RELAY BOX. GEAR SWING OPS CHECKS GOOD.

Part: LINE — CHAFED (LT HYD SYST)

NORMAL HYDRAULIC OIL LEVEL ON GROUND, BUT RIGHT AFTER TAKEOFF LOW PRESSURE LIGHT CAME ON FOLLOWED BY LOW OIL LEVEL AND MAIN PUMP LOW PRESSURE LIGHTS CAME ON. TRIED TO BALANCE RIGHT SYSTEM OIL WITH LEFT BUT IT WOULD ONLY MAINTAIN FOR 30 SECONDS. RETURNED TO SLC. REPLACED CHAFED HYDRAULIC PRESSURE LINE FROM LEFT ENGINE DRIVEN PUMP TO HYDRAULIC PACK. OPS AND LEAK CHECKS GOOD.

Part: WIRE — FAILED (RT MLG)

ON GEAR RETRACTION, RIGHT MAIN SYSTEM B LIGHT DID NOT ILLUMINATE. GREEN LIGHT SYSTEM REMAINED ILLUMINATED THE ENTIRE TIME. DID NOT EXTINGUISH AFTER RETRACTION. RETURNED TO SLC. REMOVED AND REPLACED B WIRE HARNESS ON RIGHT MLG IAW EMB MM 32-61-01, OPS CHECK GOOD.

Part: RETRACT MECH — ICED UP (LANDING GEAR)

GEAR WOULD NOT EXTEND USING NORMAL PROCEDURES. CYCLED 3 TIMES TO GET THE GEAR DOWN AND LOCKED. DEICED NOSE GEAR AND CYCLED LANDING GEAR SEVERAL TIMES. ALL INDICATION AND OPERATION NORMAL. ALL LOCKING MECHANISM CLEARED OF ICE.

Part: SWITCH — FAILED (LT WIND DEICE)

MIDDLE LEFT WING DEICE INOP WITH TIMER 1 AND TIMER 2 SELECTED. RETURNED TO SLC. MEGGED OUT WIRES FOR LEFT, RIGHT AND MIDDLE BOOT PRESSURE SWITCHES FOUND OK. CHECKED BOTH PRESSURE SWITCHES, FOUND LEFT OK. FOUND RIGHT SET TOO HIGH. REMOVED AND REPLACED RIGHT MIDDLE PRESSURE SWITCH. CYCLED BOOTS FOR 30 MINUTES, OPS CHECKS GOOD.

Part: VALVE — FAILED (RT ENG BLEED AIR)

MIDDLE LEFT WING DEICE FAILS IN BOTH TIMER POSITIONS AND BOTH HEAVY AND LIGHT POSITIONS. RETURNED TO SLC. REMOVED AND REPLACED THE RIGHT BLEED AIR SHUT OFF VALVE IAW EMB 120 MM 36-10-00. RAN THE AIRCRAFT DEICE SYSTEM IN ALL CONFIGURATIONS, CHECKS GOOD. ALSO, RAN WITH SHOP AIR FOR 45 MINUTES. SYSTEM OPS CHECKS GOOD.

Part: DEICE BOOT — FAILED (LT & RT WING)

ON CLIMB, OUTBOARD WING BOOTS FAILED BOTH TIMERS, BOTH CYCLES. RETURNED TO FIELD. REMOVED AND REPLACED OUTBOARD WING DEICE BOOT IAW MM.

Part: VALVE — FAILED (LT & RT WING)

LEADING EDGE DEICE OUTBOARD LEFT AND RIGHT FAILED BOTH TIMERS IN HEAVY AND LIGHT CYCLES AFTER APPROX 6-8 SECONDS. RETURNED TO FIELD. REPLACED OUTBOARD BOOT DEICE EJECTOR VALVE. GROUND RAN 15 MINUTES, CHECKS GOOD.

Part: ENGINE — FAILED (LEFT)

APPROXIMATELY 5 MINUTES AFTER TAKEOFF, LEFT T6 INCREASED TO CONTINUOUS LIMIT. REDUCED POWER TO CLIMB POWER SETTING, T6 STILL INCREASING. REDUCED POWER TO 60 PERCENT TQ. AT THAT POINT SEVERAL LOUD ENGINE NOISES HEARD AND AIRCRAFT YAWED. PERFORMED PRECAUTIONARY ENGINE SHUT DOWN AND RETURNED TO WYS. REMOVED AND REPLACED LEFT ENGINE IAW MM 71-00-00. OPS CHECKS GOOD. NO LEAKS NOTED.

Part: TRANSPONDER — FAILED (NR 1)

DEPARTING SAN, LOCAL APPROACH REPORTED THAT THE 3RD DIGIT ON NR 1 TRANSPONDER WAS SHOWING A DIFFERENT NUMBER THAN WAS ASSIGNED. TRIED NR 2 TRANSPONDER AND IT WAS TOTALLY INOPERABLE. WAS TOLD BY DISPATCH TO DIVERT TO LAX. INSTALLED NEW CONTROL HEAD CTRL 92 AT NR 1 TRANSPONDER. PERFORMED TRANSPONDER TEST SEQUENCE WITH TEST BOX AND PITOT STATIC CHECK FOR ALTITUDE READ OUT. ALL CHECKS GOOD.

Part: WIRING HARNESS — FAILED (LANDING GEAR)

AFTER TAKEOFF, PUT GEAR HANDLE UP AND GEAR SEEMED TO RETRACT NORMALLY BUT LEFT GREEN A LIGHT STAYED ON. CYCLED GEAR HANDLE AND WITH HANDLE DOWN GOT 3 RED B LIGHTS WITH NOSE AND RIGHT MAIN RED A LIGHTS ON CONTINUOUSLY, GEAR WOULD NOT EXTEND AND HYDRAULICS WERE NORMAL. USED ELECTRONIC OVER RIDE PROCEDURE AND RETURNED TO LAX. REPLACED LEFT GEAR A SYSTEM WIRING HARNESS AND BOTH PROX SENSORS. SWUNG GEAR AND OPS CHECKS GOOD.

Part: PROX SWITCH — FAILED (LT MLG)

LANDING GEAR HAD TO BE EXTENDED MANUALLY. LEFT GEAR A SYSTEM INOP. REPLACED LEFT A DOWNLOCK PROXIMITY SWITCH IAW MM 32-61-1. OPERATIONAL CHECK OF GEAR IAW MM 32-30-00. OPS CHECKS GOOD.

Part: COALESCER BAG — CONTAMINATED (LEFT)

LEFT DUCT LEAKAGE LIGHT ILLUMINATED DURING FLIGHT. FOLLOWED QRH BUT LIGHT DID NOT EXTINGUISH AFTER 3 MIN. PERFORMED PRECAUTIONARY ENGINE SHUT DOWN AND RETURNED TO PSP. REPLACED LEFT WATER SEPARATOR. RAN LEFT ENGINE WITH POWER, CHECKS GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE)

LEFT FORWARD OMEGA BEAM CORRODED THROUGH TOP SIDE. REPLACED LEFT FORWARD OMEGA BEAM WITH NEW ONE.

Part: STRAP — CORRODED (BS 4410-6467)

LEFT FORWARD BUTT STRAP BETWEEN STATION 4410 AND 6467 HAS CORROSION PITS. REPLACED LEFT FORWARD BUTT STRAP WITH NEW ONE.

Part: FUEL PUMP — MALFUNCTIONED (LT ENGINE)

LEFT ENGINE FAILED ON TAKEOFF ROLL. REJECTED TAKEOFF, RETURNED TO GATE. REMOVED AND REPLACED LEFT ENGINE FUEL PUMP WITH SERVICEABLE UNIT. WORK PERFORMED IAW MM 77-01-40, OPS CKS GOOD, NO LEAKS.

Part: DOOR STOP — FAILED (PAX DOOR)

AT 25,000 FEET, HEARD A BIG BANG. FLIGHT ATTENDANT REPORTED THAT ONE OF THE LATCHES ON THE FORWARD DOOR BROKE OFF. LANDED AT SBA. REPLACED UPPER FORWARD ENTRY DOOR BACKSTOP AND ADJUSTED BOTH UPPER DOOR BACKSTOPS PER MM 52-11-00, CHECKS GOOD.

Part: CONNECTOR — MISWIRED (RT MLG)

RIGHT MAIN GEAR -A+ LIGHT DIDN'T EXTINGUISH AND NO OTHER GEAR LIGHTS WOULD ILLUMINATE WITH GEAR HANDLE DOWN. USED EMERGENCY GEAR EXTENSION PRECEDURE TO PUT GEAR DOWN. REPLACED RIGHT GEAR -A+ SYSTEM PROX WIRE HARNESS. AFTER CONNECTING PROX SENSOR, RIGHT RED -A+ LIGHT STAYS ON. TROUBLESHOT TO RIGHT UPLOCK CAM CANNON PLUG FOR PROX SENSOR WIRED INCORRECTLY. SWAPPED WIRES IN CANNON PLUG FOR -A+ SYSTEM AND -B+ SYSTEMS IN RIGHT WHEEL WELL FOR A LIGHT INDICATIONS. GROUND OPS CHECK GOOD.

Part: ROD END — FAILED (NLG)

AFTER TAKEOFF, COULD NOT RETRACT NOSE GEAR. NOSE GEAR INTRANSIT LIGHT REMAINS ILLUMINATED WITH A STRONG VIBRATION. REMOVED AND REPLACED UP ACTUATOR ROD END AT GEAR NOSE, SWUNG GEAR AND OPS CKS GOOD IAW MM 32-32-11.

Part: RELAY — FAILED (AUTO FEATHER SYS)

RT PROP FEATHERED ON TAKEOFF ROLL. REMOVED AND REPLACED K0039 AND K0161 RELAYS WITH A NEW UNIT, AUTO FEATHER TESTS GOOD, GROUND RAN ENGINE TO TAKEOFF POWER, OPS CKS NORMAL.

Part: CONNECTOR — DIRTY (TE FLAPS)

SHORTLY AFTER TAKEOFF WITH FLAPS SET 15 DEGREES, A FLAP ASYMMETRY OCCURRED, OUTBD FLAPS. CLEANED OUTBD FLAPS CANNON PLUG CONNECTION AND RERACKED FLAP COMPUTER. OPS CKS GOOD ON GROUND.

Part: CONTL MECH — OUT OF ADJUST (TE FLAPS)

ON DEPARTURE AFTER GEAR UP SELECTED AND NORMAL GEAR RETRACTOR LIGHT SEQUENCES, LOUD RUMBLING SOUND FROM FRONT OF PLANE OCCURRED DUE TO GEAR DOORS NOT CLOSING. RETURNED TO FIELD. REPLACED RELAY BOX, CYCLED GEAR 25 TO 30 TIMES, AND IT FUNCTIONED PROPERLY.

Part: RELAY BOX — FAILED (LT MLG DOORS)

LT MAIN GAP DOORS WOULD NOT CLOSE AFTER TAKEOFF, RECYCLED 4 TIMES, BOTH REQUIRED LIGHTS ON WITH GEAR HANDLE IN UP POSITION. REPLACED LDG RELAY BOX SWING GEAR SEVERAL TIMES, OPS CKS GOOD.

Part: ROLLER — FAILED (LT TE FLAP)

ON DEPARTURE, THE OUTBOARD FLAPS WOULD NOT RETRACT PAST 6 DEGREES. REPLACED THE ROLLER (INBOARD ROLLER) ON THE LEFT OUTBOARD MOVEABLE FLAP. OPS CHECKS OK.

Part: SIG COND — MALFUNCTIONED (RT ENGINE)

ABORTED TAKEOFF. FLIGHT 242 LAX. TORQUE ON RIGHT ENGINE WENT TO 107 PERCENT AND NP DROPPED TO 17.1 PERCENT ON APPLICATION OF TAKEOFF POWER. REPLACED RIGHT TORQUE SIGNAL CONDITIONER. GROUND RUN AND OPS CKS GOOD. SEE FL 75611 FOR MECH SIGN OFF.

Part: DOOR — NOT CLOSED (AVIONICS BAY)

SERVICE DOOR WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL. ABORTED TO. RETURNED TO GATE. FOUND SERVICE DOOR NOT FULLY CLOSED. RESECURED AVIONICS BAY SERVICE DOOR. LIGHT EXTINGUISHED. OPS CHECKS GOOD. SEE FL 75608.