N561SW

Part: WIRE HARNESS — FAULTY (LT MLG) · airframe 31,810 hrs · 45,059 cycles

GEAR DOWN LOCK DID NOT RELEASE. OVERRIDE WAS USED TO RAISE THE GEAR. FLT 5398 REPLACED LT MLG SQUAT SWITCH HARNESS ASSEMBLY. CW LANDING GEAR SWINGS IAW AMM, PN TDQ120-20509-01.

Part: LIGHT — LOOSE (CABIN) · airframe 31,576 hrs · 44,731 cycles

FORWARD FLOOR EMERGENCY RED LIGHTS ASSEMBLY IS LOOSE. FLT#5331 REWIRED FORWARD FLOOR EMERGENCY RED LIGHTS ASSEMBLY IAW WM.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 31,323 hrs · 44,367 cycles

3RD WHITE FLOOR EMERGENCY LIGHT IS DIM. FLT#5439 RECONNECTED LIGHT ASSEMBLY.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 31,116 hrs · 44,095 cycles

SURFACE CORROSION ON FIRST BUTT STRAP AT PASSENGER DOOR ENTRANCE. C-CHECK CUT OUT THE DAMAGED BUTT STRAP AT PASSENGER DOOR ENTRANCE & SPLICED IN A NEW PIECE IAW EST & SRM.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 31,116 hrs · 44,095 cycles

RT WING FIRST FUEL ACCESS PANEL OTBD OF NACELLE AT RIB 15 LOWER SKIN CLIP JUST FWD OF ACCESS PANEL CRACKED AFT RIVET HOLE. C-CHECK REPLACED LOWER SKIN SUPPORT CLIP ON RT WING FIRST FUEL ACCESS PANEL OTBD OF NACELLE AT RIB 15 LOWER SKIN CLIP JUST FWD OF ACCESS PANEL IAW SRM.

Part: STRINGER — CRACKED (LT WING) · airframe 31,116 hrs · 44,095 cycles

LT STRINGER IN DRY BAY IS CRACKED THROUGH THE OTBD RIVET OF THE ANTISKID BOX SUPPORT BRACKET. C-CHECK REPLACED LT WING STRINGER 10 FROM RIB 6 TO FS CENTER LINE IAW SRM & AMM.

Part: FUSE — BLOWN (CABIN) · airframe 30,899 hrs · 43,777 cycles

AFT EXTERIOR EMERGENCY LIGHTS DO NOT ILLUMINATE. (SERVICE) REPLACED FUSE AT SEAT 9 B/C.

Part: CONNECTOR — LOOSE (SMOKE DETECTOR) · airframe 30,383 hrs · 43,059 cycles

GALLEY SMOKE ALARM IS ANNUNCIATING WITH NO VISABLE SIGNS OF SMOKE OR FLAMES PRESENT. (FLT 7386) FOUND CONNECTOR ON LAV SMOKE DETECTOR WAS LOOSE. RE-SECURED CONNECTOR. OPS CHECKS GOOD.

Part: GROUND WIRE — UNSECURE (CABIN) · airframe 30,261 hrs · 42,915 cycles

NR 1 RED EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE. (FLT 5397) SECURED GROUND WIRE.

Part: CONTROL UNIT — FAILED (ANTI-SKID SYS) · airframe 30,031 hrs · 42,575 cycles

FAILED TO STOP AFTER FULL BRAKE APPLICATION, STOPPED AFTER ENGAGING EMERGENCY BRAKE. (FLT 5331) REPLACED ANTI SKID CONTROL UNIT IAW AMM. P/N 42-687-1 S/N ON: 228 S/N OFF: 480

Part: WINDSHIELD — DEFECTIVE (COCKPIT) · airframe 30,031 hrs · 42,575 cycles

MILD ELECTRICAL ODOR WHEN WIND SHIELD HEAT WAS TURNED ON. (FLT 5424) REPLACED RIGHT WINDSHIELD IAW AMM. P/N: NP-151311-2 S/N ON: 06114H2739 S/ N OFF: 03078119092

Part: SIGN — MISSING (CABIN) · airframe 30,031 hrs · 42,575 cycles

EMERGENCY EXIT LOWER SIGN AT ROW 9 B/C MISSING. (FLT 5440) REPLACED EMERGENCY EXIT LOWER LIGHT ASSEMBLY AT ROW 9 B/C.

Part: UNKNOWN — SMOKE (CABIN) · airframe 29,762 hrs · 42,204 cycles

RIGHT PACK FAILS WITH SMOKE IN THE CABIN. (SERVICE) RIGHT GROUND COOLING FAN CIRCUIT BREAKER POPPED AND THE CIRCUIT BREAKER WAS RESET.

Part: HYDRAULIC LINE — LEAKING (GREEN SYSTEM) · airframe 29,722 hrs · 42,145 cycles

UPON RAISING THE LANDING GEAR MOST HYDRAULIC FLUID IN THE GREEN SYSTEM WAS LOST. (FLT 5647) FOUND SMALL PINHOLE LEAK ON GREEN SYSTEM. REPLACED GREEN GSE PRESSURE LINE FROM MULE CONNECTOR TO RESERVOIR IN REFERENCE TO AMM.

Part: RELAY — FAILED (COCKPIT) · airframe 29,571 hrs · 41,945 cycles

AN UNUSUALLY HIGH LOAD ON VOLTMETER, APU GENERATOR SIDE, AND RECEIVED A SMOKE SMELL IN THE COCKPIT. THE FIRST OFFICER'S SIDE PANEL WAS HOT TO TOUCH. (FLT 5447) REPLACED APU FEEDER PROTECTION RELAY IN RIGHT SIDE CONSOLE.

Part: SIGN — MISSING (CABIN) · airframe 29,117 hrs · 41,281 cycles

FLOOR LEVEL EXIT SIGN AT 6-C IS MISSING. (FLT 7758) REPLACED EXIT SIGN AT 6C FLOOR LEVEL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,981 hrs · 39,835 cycles

LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 7802) RELAMPED EMERGENCY LIGHT.

Part: SEQUENCE VALVE — FAILED (RT MLG) · airframe 27,939 hrs · 39,780 cycles

RIGHT MAIN GEAR WOULD NOT RETRACT AFTER TAKEOFF. (FLT 7800) REPLACED RIGHT OUTBOARD SEQUENCE VALVE AND FORWARD OUTBOARD GEAR DOOR ACTUATOR. NR 1 PN: 120-32943-001 S/N OFF: 1916. NR 2 P/N 120-32943-001 S/N OFF 1916

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,384 hrs · 39,117 cycles

1 RED FLOOR LEVEL EMERGENCY LIGHT BURNED OUT AT ROW 9. (FLT 5556) RELAMPED EMERGENCY LIGHT.

Part: ROLLER — OUT OF ADJUST (CABIN DOOR) · airframe 26,777 hrs · 38,382 cycles

MAIN CABIN DOOR DIFFICULT TO CLOSE. (FLT 6373) ADJUSTED PAX DOOR UPPER AFT ROLLER.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 26,658 hrs · 38,216 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6505) LUBED MAIN CABIN DOOR ROLLERS.

Part: SIGN — MISSING (CABIN) · airframe 26,282 hrs · 37,693 cycles

FORWARD EMERGENCY EXIT SIGN MISSING. (FLT 7811) INSTALLED FORWARD EMERGENCY "EXIT" SIGN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,245 hrs · 36,364 cycles

PASSENGER ENTRY DOOR EMERGENCY LIGHT INOP. (FLT 7757) RELAMPED EMERGENCY LIGHT.

Part: STRUCTURE — LACK OF LUBE (CABIN DOOR) · airframe 25,086 hrs · 36,192 cycles

MAIN CABIN DOOR HARD TO OPEN. (FLT 6232) CLEANED AND LUBRICATED MULTIPLE POINTS ON MAIN CABIN DOOR.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,000 hrs · 36,095 cycles

AFT SECTION OF CABIN EMERGENCY LIGHTING INOP. (FLT 7790) REPLACED AFT EMERGENCY LIGHT BATTERY PACK. P/N D366-04-001 S/N OFF 1184/12-95.

Part: PAD — CORRODED (RT ENGINE) · airframe 24,973 hrs · 36,062 cycles

RIGHT ENGINE TORQUE PAD SPIGOT BORE CORRODED. (ENG CHG) REPLACED ENGINE.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 24,318 hrs · 35,305 cycles

CABIN PRESSURIZATION LOST IN BOTH AUTO AND MANUAL MODES AT ALTITUDE. (FLT 7761) REPLACED ELECTRONIC ALTITUDE CONTROLLER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 24,276 hrs · 35,256 cycles

STRINGERS 18 AND 19 AT PASSENGER DOOR CORRODED. (C CHECK) REPAIRED PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 24,276 hrs · 35,256 cycles

PASSENGER DOOR LOWER THRESHOLD ANGLE CORRODED. (C CHECK) REPLACED ANGLE PER SRM.

Part: SPLICE — OVERHEATED · airframe 24,276 hrs · 35,256 cycles

WIRE SPLICE SPBG57 HAS SIGNS OF OVERHEATING. (C CHECK) REPAIRED WIRE SPLICE PER WMM.

Part: UNKNOWN — MALFUNCTIONED (PROP REVERSERING) · airframe 23,977 hrs · 34,877 cycles

AFTER LANDING, WAS UNABLE TO GET POWER LEVERS INTO REVERSE. APPLIED BRAKES AND BLEW NR 1 AND NR 3 TIRES. (FLT 7772) REPLACED ALL MAIN WHEEL ASSYS IAW EMB MM 32-44-02. PERFORMED FUNCTIONAL CHECK OF PROPELLER REVERSE SYSTEM IAW EMB MM 61-20-00, NO FAULTS FOUND.

Part: PULLEY — BINDING (RT AILERON) · airframe 23,674 hrs · 34,482 cycles

FLIGHT CONTROLS STIFF IN RIGHT TURNS. (FLT 100) REPLACED THREE PULLEYS IN RIGHT AILERON CONTROL CIRCUIT.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 23,527 hrs · 34,299 cycles

EMERGENCY EXIT SIGN FORWARD OF RIGHT OVERWING EXIT HAS "EXIT" PLACARD MISSING. (FLT 7802) REPLACED COVER.

Part: HMU — POWER LOSS (ENGINE) · airframe 23,339 hrs · 34,064 cycles

FLT 6297 - POWER LOSS ON CLIMB. REPLACED HMU AND FUEL PUMP.

Part: PROPELLER — SURGES (RIGHT) · airframe 22,330 hrs · 32,792 cycles

FLT 7802 - RIGHT PROP NP ABOVE TOLERANCES ON CLIMB-OUT. RAN ENGINES, UNABLE TO DUPLICATE.

Part: STRINGER — CRACKED (RT WING) · airframe 21,322 hrs · 31,426 cycles

STRINGER NR 10 ON RIGHT WING BETWEEN RIBS NR 8 AND NR 9 IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH MAJOR REPAIR ON RIGHT WING PER SRM 57-20-03.

Part: SUPPORT — CORRODED (BS 4992-5100) · airframe 21,322 hrs · 31,426 cycles

LEFT FLOOR AND SIDEWALL SUPPORT IS CORRODED AT FS 4992 TO FS 5100, FOUND AT C-CHECK. COMPLIED WITH REPLACEMENT AND REPAIR PER EMB 120 SRM 51-30-10 AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 5118-6653) · airframe 21,322 hrs · 31,426 cycles

FLOOR SUPPORT RAIL AND WEB ON THE LEFT SIDE OF FS 5118 TO FS 6653 IS CORRODED. FOUND AT C-CHECK. REPLACED CORRODED PARTS PER EMB 120 SRM 51-40-02.

Part: WIRE — CORRODED (BUSS BAR) · airframe 21,322 hrs · 31,426 cycles

WIRE TERMINAL CONNECTED TO BUSS BAR IN RIGHT AFT CONSOLE IS CORRODED, FOUND AT C-CHECK. REPLACED TERMINAL ON WIRE. OPS CHECKS GOOD.

Part: WIRE — DAMAGED · airframe 21,322 hrs · 31,426 cycles

WIRE AT TB0122 IN LEFT, FORWARD CONSOLE SHOWS SIGNS OF OVERHEATING, FOUND AT C-CHECK. REPLACED WIRE AT TB0122 AS REQUIRED.

Part: DOOR — LACK OF LUBE · airframe 20,866 hrs · 30,851 cycles

FLT 3699 - MAIN CABIN DOOR IS DIFFICULT TO OPEN AND CLOSE. CLEANED AND LUBED DOOR. OPS CHECKED GOOD.

Part: COVER — BROKEN (EMERGENCY LIGHTS) · airframe 20,866 hrs · 30,851 cycles

FLT 3691 - EMERGENCY LIGHT COVER NEAR MAIN CABIN DOOR IS BROKEN. REPLACED LIGHT ASSEMBLY NEAR THE MAIN CABIN DOOR. OPS CHECK GOOD.

Part: BLADE — CRACKED (LT PROPELLER) · airframe 20,791 hrs · 30,756 cycles

LEFT PROP NR 1 BLADE APPEARS TO BE CRACKED. REPLACED NR 1 BLADE ASSY WITH SERVICEABLE UNIT. NO LEAKS NOTED, PN RFC11M1R6AD4E2, SN OFF 880331.

Part: CONTACTOR — BURNED (UNKNOWN) · airframe 20,711 hrs · 30,633 cycles

ELECTRICAL ODOR COMING FROM FLIGHT DECK, FLIGHT NR 5539. REPLACED CONTACTOR K0519 WITH SERVICEABLE UNIT. OPS CHECKED GOOD.

Part: FLEX DRIVE — BINDING (POWER LEVER) · airframe 20,574 hrs · 30,470 cycles

FLT 3730 - RIGHT POWER LEVER IS DIFFICULT TO MOVE. REPLACED AND RIGGED FLEX CABLE AND HOUSING, IAW 76-10-02. OPS CHECKS GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 20,467 hrs · 30,356 cycles

FLT 3716 - CAPTAINS SIDE WINDOW IS CRACKED. REPLACED CAPTAINS SIDE DIRECT VISION WINDOW IAW AMM 56-11-01.

Part: A/C PACK — SMOKE · airframe 19,880 hrs · 29,618 cycles

RECEIVED "SMOKE" WARNING AND FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN, FLIGHT NR 5429. THAWED OUT FROZEN PACK AND OPS CHECK GOOD AT THIS TIME.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 19,824 hrs · 29,542 cycles

EMERGENCY LIGHT OVER ROW 3 IS INOP, FLIGHT NR 5578. REPLACED BLOWN FUSE. OPS CHECKS GOOD.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 19,360 hrs · 28,883 cycles

UPON ESTABLISHING APU BLEEDS, CABIN AND FLIGHT DECK FILLED WITH SMOKE. RAN BOTH PACKS ON APU BLEED FOR 1.5 HOURS. NO SMOKE NOTED IN CABIN OR COCKPIT. COULD NOT DUPLICATE. SYSTEM CHECKS GOOD.

Part: LATCH — MALFUNCTIONED (MLG DOOR) · airframe 18,264 hrs · 27,496 cycles

RIGHT INBOARD WHEEL WELL DOOR OPENED INFLIGHT WITH LANDING GEAR RETRACTED.INSPECTED DOOR LATCH FOR INTEGRITY AND APPLIED POWER TO DOORS WITH NO DEFECTS NOTED. DOOR IS SECURE IAW EMB 120 MM 22-10-00. UNABLE TO DUPLICATE.

Part: ACTUATOR — OUT OF ADJUST (NLG) · airframe 17,648 hrs · 26,713 cycles

NORMAL EXTENSION OF GEAR NOT POSSIBLE. DROPPED GEAR MANUALLY WITH BAR.ADJUSTED NOSE LANDING GEAR ACTUATOR. OPERATIONAL CHECKS GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 17,696 hrs · 26,799 cycles

LATERAL FLOOR SUPPORTS (2) AT FRAME 16, RIGHT SIDE, CORRODED ON TOP SIDE BEYOND LIMITS, DISCOVERED DURING C-CHECK INSPECTION. REPLACED LATERAL FLOOR SUPPORTS (2) AT FLOOR LINE OF FRAME 16, RIGHT SIDE PER SRM 51-40-02.

Part: STRINGER — CRACKED (LT WING) · airframe 17,696 hrs · 26,799 cycles

LEFT INBOARD WING NR 8 STRINGER CRACKED BETWEEN NR 8 AND NR 9 RIB, DISCOVERED DURING C-CHECK INSPECTION. REPAIRED NR 8 STRINGER BETWEEN NR 8 AND NR 9 RIBS ON LEFT INBOARD WING IAW SRM 57-20-03, RII 57-900-1000.

Part: MODULE — MALFUNCTIONED (MLG) · airframe 17,185 hrs · 26,078 cycles

GEAR DID NOT COME DOWN, RECYCLED PER QRH. GEAR CAME DOWN SECOND TRY. REPLACED SELECTOR HANDLES IAW EMB 120 32-31-07. OPERATIONAL CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 17,016 hrs · 25,842 cycles

STALL WARNING TEST WILL NOT TEST. REPLACED NR 1 SWS COMPUTER. OPERATIONAL CHECK GOOD, PN C-81806-1, SN OFF 842.

Part: RELAY — ODOR (COCKPIT) · airframe 16,910 hrs · 25,688 cycles

BURNING ODOR COMING FROM FO'S SIDE PANEL. REPLACED FEEDER PROTECTION RELAY KO542 IN RT AUX RELAY PANEL.

Part: ODOR — DETECTED (COCKPIT) · airframe 16,838 hrs · 25,596 cycles

A BURNING SMELL WAS OBSERVED COMING FROM FO'S SIDE PANEL AREA WITH POWER TO THE AIRCRAFT. SECURED APU STARTER/GENERATOR TERMINAL. OPERATIONAL CHECK GOOD, NO BURNING SMELL WAS OBSERVED.

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAPS) · airframe 16,824 hrs · 25,574 cycles

FLAP DISAGREEMENT ON OUTBD PAIR DURING RETRACTION. REPLACED FLAP CONTROL UNIT; FLAP ANNUCICATOR UNIT AND REPLACED LT NACELLE FLAP ACTUATOR. OPERATIONAL CHECK GOOD, PN ON 347200-1001, OFF 0194 PN ON 347100-1001 OFF 230 PN ON 343100-1001, OFF 0141.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,392 hrs · 24,910 cycles

FLOOR LEVEL EMERGENCY LIGHT AT SEAT 3A INOP. REPLACED EMERGENCY LIGHT LAMP ASSY AT SEAT 3A. OPERATIONAL CHECK GOOD.

Part: ENGINE — SEIZED (LEFT) · airframe 16,387 hrs · 24,905 cycles

LT ENG WILL NOT ROTATE. REPLACED LEFT ENG WITH SERVICABLE UNIT IAW MM 71-00-00, P/N: PW118B S/N OFF: 115664.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 15,775 hrs · 23,992 cycles

EMERGENCY STRIP LIGHTS ADJACENT TO GALLEY INOP. REPLACED FORWARD EMERGENCY BATTERY PACK. OPERATIONAL CHECK GOOD.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 15,262 hrs · 23,208 cycles

LOWER LEFT EXIT EMERGENCY LIGHT 6C BROKEN. REPLACED EMERGENCY EXIT SIGN ASSY AT 6C. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAP) · airframe 15,110 hrs · 22,977 cycles

"FLAP DISAGREEMENT" WHEN PLACING FLAP LEVER FROM 45 DEGREES TO 0 DEGREES. REPLACED RIGHT NACELLE FLAP ACTUATOR IAW EMB MM 27-50-08. REPLACED FLAP SELECTOR HANDLE IAW 27-50-01. OPERATIONAL CHECK GOOD.

Part: SELECTOR — MALFUNCTIONED (TE FLAP) · airframe 15,085 hrs · 22,937 cycles

WHILE ENROUTE AT FL240, RECEIVED SEVERAL CONTROL FAULT WARNINGS ACCOMPANIED BY "AWS" AND FLAP WARNINGS ON MAP. REPLACED FLAP SELECTOR LEVER. CLEARED ALL FAULTS FROM FCU. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAP) · airframe 15,066 hrs · 22,908 cycles

FLAP CONTROL FAULT WHILE DROPPING THE FLAPS. REPLACED FCU AND RIGHT OUTBOARD FLAP ACTUATOR PER MM 27-50-00. OPERATIONAL CHECK GOOD.

Part: ANNUNCIATOR — MALFUNCTIONED (TE FLAPS) · airframe 14,967 hrs · 22,758 cycles

RETRACTED FLAPS AND RECEIVE A FLAP AND ADVANCED SWS ON MAP. REMOVED AND REPLACED THE FLAP ANNUNCIATOR IAW AMM 27-50-05. OPERATIONAL CHECK GOOD. P/N 347100-1001, S/N OFF 0214.

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAP) · airframe 14,235 hrs · 21,637 cycles

FLAP RETRACTION GENERATES A DISAGREEMENT ON TAXI. REPLACED LEFT NACELLE FLAP ACTUATOR IAW MM 27-50-00.

Part: WIRE — BROKEN (AILERONS) · airframe 13,564 hrs · 20,586 cycles

CONTROLS DISENGAGE LIGHT ON MAP COMES ON INTERMITTENTLY. REPAIRED BROKEN WIRE NEAR AILERON DISCONNECT IAW 20-00-00, OPERATIONAL CHECK GOOD.

Part: COMPUTER — WILL NOT TEST (STALL WARNING) · airframe 13,547 hrs · 20,564 cycles

STALL WARNING SYSTEM WILL NOT TEST. REPLACED NR 1 AND NR 2 STALL WARNING COMPUTERS. OPERATIONAL CHECK GOOD. P/N: C-81806-1, S/N OFF: 724.

Part: ACM — MALFUNCTIONED (AIR CONDITIONER) · airframe 13,134 hrs · 19,923 cycles

UNABLE TO COOL COCKPIT WITH ENGINE OR APU BLEED, LOW OR NORM SELECTED ON GROUND. SMOKE IN COCKPIT ASSOCIATED WITH DUCT OVERHEAT LIGHT. REPLACED AIR CYCLE MACHINE IAW MM 21-50-05, OPS CHECK GOOD.

Part: SPRING — FAILED (ELEVATOR) · airframe 13,020 hrs · 19,747 cycles

FLIGHT CONTROLS FOR ELEVATOR FEEL EXCEPTIONALLY LITE. REPLACED FIRST OFFICER'S ELEVATOR RETURN SPRING WITH SERVICEABLE UNIT. OPS CHECKS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,776 hrs · 19,366 cycles

EMERGENCY EXIT SIGN LIGHTS WILL NOT ILLUMINATE DURING TEST. REPLACED MIDDLE ELBP WITH SERVICEABLE UNIT. OPS CHECK GOOD.

Part: ACTUATOR — FAILED (FLAPS) · airframe 12,416 hrs · 18,806 cycles

ON TAXI OUT HAD LOSS OF HYDRAULIC PRESSURE ON BLUE SYSTEM. RETURNED TO GATE. REPLACED RIGHT NACELLE FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-00 AND RII 27-307. OPS AND LEAK CHECKS GOOD.

Part: ACTUATOR — MALFUNCTIONED (LINEAR) · airframe 11,927 hrs · 18,066 cycles

INFLIGHT, MOMENTARILY WAS NOT ABLE TO GET MORE THAN 1 INCH TRAVEL OUT OF RIGHT RUDDER PEDAL. RAN QRH, CYCLED BLUE RUDDER SYSTEM AND PROBLEM COMPLETELY ELIMINATED WITH NO FURTHER PROBLEMS. REMOVED AND REPLACED BLUE HYD SYSTEM RUDDER ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-22-02. OPS CHECK GOOD.

Part: WARNING LIGHT — ILLUMINATED (STAB TRIM) · airframe 11,315 hrs · 17,109 cycles

ON TAKEOFF ROLL, GOT A ''TRIM WARNING''. ABORTED TO AND RETURNED TO THE BOX.FOUND AURAL WARNING CB'S POPPED. RESET CB'S AND ALL TEST GOOD.

Part: SQUAT SWITCH — FAULTY (MLG) · airframe 11,315 hrs · 17,109 cycles

AFTER T.O GEAR WOULD NOT RETRACT,. USED ''DOWNLOCK RED BUTTON'' TO RETRACT THE GEAR. ''IDLE AND UNLOCK'' LIGHT ILLUMINATED, AUTO PRESSURIZATION WOULD NOT PRESSURIZE, TCAS REMAINED ON.TROUBLESHOT SYSTEM. FOUND RIGHT LANDING GEAR WEIGHT ON WHEELS SWITCH FAULTY. REPLACED WEIGHT ON WHEELS SWITCH WITH SERVICEABLE UNIT. CYCLED GEAR. OPS CHECK GOOD.

Part: PLUNGER — OUT OF ADJUST (MLG) · airframe 9,998 hrs · 15,041 cycles

DEPARTING LAX ON GEAR RETRACTION, HAD INDICATION DISAGREEMENT. ALL GREEN LIGHTS OUT THEN ALL RED LIGHTS ON, THEN BOTH A&B LIGHT ON LEFT GEAR (RED) AND -B- ON RT GEAR WOULD NOT EXTINGUISH. COMPLIED WITH QRH. NO CHANGE & GEAR CYCLED DOWN WITH 3 GREEN. RETURNED TO LAX. FOUND BOTH MAIN GEAR UPLOCK PLUNGERS OUT OF ADJUSTMENT. ADJUSTED PLUNGERS. SWUNG GEAR NUMEROUS TIMES. ALL CHECKS GOOD.

Part: ACTUATOR — FAILED (T/E FLAP) · airframe 9,838 hrs · 14,790 cycles

LEFT INBOARD FLAP WILL NOT RETRACT EVEN WITH OVERRIDE. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-07. OPS CHECKS GOOD.

Part: EEC — MALFUNCTIONED (RT ENGINE) · airframe 9,515 hrs · 14,308 cycles

ON CLIMBOUT, THE RIGHT ENGINE STARTED TO SURGE WITH THE EEC ON AND OFF. RETURNED TO SAN. INSPECTED RIGHT ENGINE EEC & HMU FOR CONDITION. RAN LEFT AND RIGHT ENGINES THROUGH VARIOUS CONFIGURATIONS, WITH THE RIGHT ENGINE EEC ON THE ENGINE SURGES. INSPECTED EEC CANNON PLUG, CLEANED AND DID AN OHM CHECK. NO DEFECTS NOTED. OPERATIONAL CHECK GOOD IAW EMB 73-22-00.

Part: SWITCH — OUT OF ADJ (DOOR) · airframe 8,581 hrs · 12,858 cycles

FORWARD DOOR LIGHT CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF. ADJUSTED FORWARD DOOR MICROSWITCH. OPS CHECK GOOD.

Part: CONTROL VALVE — FAILED (APU) · airframe 7,172 hrs · 10,866 cycles

ON THE GROUND W/APU RUNNING, CABIN SMOKE DETECTOR IS ACTIVATED. ISOLATED SOURCE TO BE LEFT PACK. APU LOAD CONTROL VALVE CLOSED LIGHT ILLUMINATES WITH SWITCH IN OPEN POSITION. UPON TROUBLESHOOTING, FOUND VENTURI TUBE ASSEMBLY CRACKED. REMOVED AND REPLACED WITH SERVICEABLE UNIT. WASHED HEAT EXCHANGERS, RAN COOLING FAN FOR 30 MINS, RAN AIRCRAFT. DISCREPANCIES STILL EXISTS. P/N 120-50481-001. ISOLATED SOURCE TO APU. REPLACED APU LOAD CONTROL VALVE AND RAN APU. OPS CHECK GOOD. P/N ON 109812-1, S/N ON P-112C, P/N OFF 109812-9, S/N OFF 2276.

Part: EJECTOR VALVE — MALFUNCTIONED (DEICE SYSTEM) · airframe 6,889 hrs · 10,459 cycles

AFTER TAKEOFF INBOARD LEFT AND RIGHT STAB AND INBOARD LEFT AND RIGHT WING DEICE LIGHT CAME ON BOTH TIMERS IN HEAVY AND LIGHT CYCLE. RETURNED TO LAX. INSTALLED SERVICEABLE RIGHT FOWARD EJECTOR VALVE FOR BOOTS IAW 30-10-00. RAN ENGINE AND OPS CHECK GOOD. REINSTALLED PANEL AND ALL CHECKS OK AT THIS TIME. S/N ON P1263, S/N OFF N1671.

Part: REGULATOR — LOOSE (PNEUMATIC SYSTEM)

ON TAKEOFF DURING CLIMBOUT DUCT LEAK LIGHT CAME ON BUT WENT OFF WHEN RESPECTIVE BLEED WAS CLOSED. RETURNED TO LAX. LIGHT CAME BACK ON DURING APPROACH. LIGHT WENT OFF AFTER ENGINE WAS SHUTDOWN DURING TAXI. FOUND PRESSURE REGULATOR OVERBOARD DRAIN OFF OF LEFT SIDE. REPOSITIONED PRESSSURE REGULATOR AND REPLACED CLAMP. RAN ENGINE AND NO LEAKS WERE NOTED.