N582SW

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 32,177 hrs · 44,138 cycles

MULTIPLE FLOOR EMERGENCY LIGHTS INOPERATIVE DURING TEST. REPLACED EMERGENCY LIGHTING BATTERY PACK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,911 hrs · 43,759 cycles

AFT SECTION OF EMERGENCY LIGHTS INOPERATIVE. C-CHECK, REPLACED AFT ELBP IAW AMM.

Part: RIB — CRACKED (FUSLEAGE) · airframe 31,911 hrs · 43,759 cycles

LEFT UPPER FUSELAGE BEHIND CAPTAIN`S DV WINDOW RIB IS CRACKED. C-CHECK, R & R RIB AT LT UPPER FUSELAGE BEHIND CAPTS DV WINDOW IAW SRM.

Part: FRAME — CRACKED (PAX DOOR) · airframe 31,911 hrs · 43,759 cycles

PAX DOOR INTERNAL FRAME AT BAY 15 IS CRACKED. C-CHECK, R & R PAX DOOR INTERNAL FRAME ASSY IAW SRM.

Part: CLEAT — CRACKED (LT WING) · airframe 31,911 hrs · 43,759 cycles

LEFT WING ABOVE NR 5 FUEL FWD OF ACCESS PANEL HAS A CRACKED SKIN CLEAT . C-CHECK, REPLACED FWD MOST, SKIN TO RIB CLEAT, AT LT WING RIB 21 IAW SRM.

Part: ROLLER — STIFF (PAX DOOR) · airframe 31,823 hrs · 43,635 cycles

MAIN CABIN DOOR IS HARD TO OPEN. INSPECTED MAIN CABIN DOOR AND FOUND LOWER FORWARD DOOR ROLLER STIFF AND HARD TO ROTATE. CLEANED AND LUBED MAIN CABIN DOOR LOWER FORWARD DOOR ROLLER IAW AMM.

Part: A/C PACK — FAILED (RIGHT) · airframe 31,616 hrs · 43,321 cycles

AFTER TAKEOFF SELECTED RT PACK. SMALL AMOUNTS OF SMOKE IN CABIN FOLLOWED BY RT PACK FAILED.

Part: ACTUATOR — FAILED (RAM AIR DOOR) · airframe 31,701 hrs · 43,455 cycles

AFTER TAKEOFF, SELECTED RT PACK TO AUTO LOW. SMALL AMOUNT OF SMOKE IN COCKPIT. RECEIVED A RT PACK FAIL. RAN QRH, FAILED TO RESET. AT SEVERAL MINUTES LATER THE LT PACK FAILED. RAN QRH PROCEDURE, PACK RESET, FAILED AGAIN A FEW MINUTES LATER. PACKS WERE LT IN CLOSED FOR SHORT DURATION OF FLIGHT. FOR TROUBLESHOOTING REPLACED LT AND RT HEAT EXCHANGERS. FURTHER INSPECTION FOUND RT RAM AIR DOOR ACTUATOR INOPERATIVE IN THE CLOSED POSITION. R & R RAM RT AIR ACTUATOR.

Part: ACM — ODOR (RIGHT) · airframe 31,358 hrs · 42,933 cycles

WITH THE TORQUE AT 65 PERCENT, RECEIVED A VERY STRONG ODOR, NO SMOKE NOTED . ODOR PERSISTED FOR DURATION OF FLIGHT. REPLACED RT ACM AND RT TIC VALVE IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,810 hrs · 42,219 cycles

WHITE FLOOR EMERGENCY LIGHT AT ROW 8A IS BURNED OUT. FLT 5376 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,772 hrs · 42,167 cycles

LAST FLOOR EMERGENCY WHITE LIGHT IS BURNED OUT. FLT 6264 RELAMPED.

Part: ACTUATOR — FAILED (NLG) · airframe 30,127 hrs · 41,234 cycles

ON DEPARTURE NOSE GEAR WOULD NOT RETRACT. RE-CYCLED & WOULD STILL NOT RETRACT. ASSOCIATED RED LIGHTS REMAINED ON WITH GEAR HANDLE SELECTED UP WHILE LT & RT EXTINGUISHED. FLT#6329 REPLACED NLG RETRACT ACTUATOR IAW AMM. PN 20605-000-05, SN ON B37 & SN OFF B31.

Part: WIRE — DISCONNECTED (CABIN) · airframe 30,014 hrs · 41,081 cycles

ONE FLOOR-LEVEL EMERGENCY LIGHT DOES NOT ILLUMINATE FLT#6310 REATTACHED WIRE TO THE FLOOR-LEVEL EMERGENCY LIGHT AT ROW 5.

Part: BALLAST — DEFECTIVE (LAVATORY) · airframe 29,932 hrs · 40,943 cycles

LAVATORY LIGHT HAS A BURNING SMELL. FLT#5476 REPLACED THE LAVATORY LIGHT BALLAST.

Part: SOCKET — FAILED (CABIN) · airframe 29,882 hrs · 40,876 cycles

EMERGENCY FLOOR LIGHT AT 5A DOES NOT ILLUMINATE. FLT#5428 REPLACED SOCKET FOR EMERGENCY LIGHT ON FLOOR NEAR SEAT 5A & CHANGED EMERGENCY LIGHT BATTERIES USING GPU, PN: 10-1307-3.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 29,816 hrs · 40,771 cycles

APU BLEED PACKS LOW, STARTED TO GET SMOKE SMELL. SWITCHED TO ENGINE BLEEDS & SMELL WENT AWAY. FLT#5304 REPLACED APU ASSEMBLY IAW AMM. PN: 3800376-2 SN ON: P-401 SN OFF: P-421.

Part: WIRE — BROKEN (CABIN) · airframe 29,671 hrs · 40,601 cycles

NR 1 RED EMERGENCY FLOOR LIGHT DOES NOT ILLUMINATE. REPAIRED BROKEN WIRE ON FORWARD RED EMERGENCY FLOOR LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,171 hrs · 39,882 cycles

THE CEILING EMERGENCY LIGHT OVER 6A IS BURNED OUT. (FLT 5476) RELAMPED EMERGENCY LIGHT.

Part: BLEED VALVE — FAILED (BLEED AIR SYS) · airframe 29,171 hrs · 39,882 cycles

SMOKE IN COCKPIT THROUGH VENTS WHEN POWER WAS PULLED BACK TO APPROX 50% TORQUE. (FLT 5654) REPLACED LEFT ENGINE HIGH PRESSURE P3 BLEED VALVE, IAW AMM 36-10-03. P/N-979626-6 S/N ON-2239 S/N OFF-1344

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,192 hrs · 39,914 cycles

AFT OVERHEAD EMERGENCY ENTRANCE LIGHT BURNED OUT. (FLT 5346) RELAMPED EMERGENCY LIGHT.

Part: SHUTOFF VALVE — FAILED (AC BAY) · airframe 29,112 hrs · 39,794 cycles

FAILURE TO PRESSURIZE AIRCRAFT ADEQUATELY AND NOT HOLDING PRESSURE. (FLT 5387) REPLACED LT PACK PRSOV. P/N-3214414-3 S/N ON-1044 S/N OFF-895

Part: DOOR SEAL — OUT OF POSITION (CARGO DOOR) · airframe 29,091 hrs · 39,755 cycles

CABIN ALTITUDE WARNING MESSAGE. CABIN ALTITUDE EXCEEDED 10,000 FT. WE DID AN EMERGENCY DESCENT TO 10,000 FT AND RAN QRH PROCEDURE, CABIN BEGAN TO SLOWLY PRESSURISE AGAIN. (FLT 6329) INSPECTED AND FOUND TOP AFT CORNER CARGO DOOR SEAL POPPED OUT OF RETAINER. RE-INSTALLED SEAL INTO RETAINER AND PERFORMED PRESSURIZATION CHECK IAW AMM.

Part: UNKNOWN — SMOKE (COCKPIT & CABIN) · airframe 29,091 hrs · 39,755 cycles

SMOKE IN COCKPIT AND CABIN IN FLIGHT, SMOKE CLEARED WHEN PACKS WERE TURNED OFF. (FLT 5640) RAN BOTH ENGINES. ISOLATED BOTH BLEED SOURCES. NO DEFECTS NOTED. OPERATED AND ISOLATED EACH PACK. RT PACK HAS NO COLD AIR FLOW. FOUND NO SMOKE WHILE OPERATING FOR 30 MINUTES. PERFORMED ENGINE RUN AND APU RUN BLEED SOURCES FOR BOTH PACKS, SYSTEM OPERATES NORMAL IN ALL MODES AND COLD AND HOT TEMP SELECTIONS, NO DEFECTS NOTED NO SMOKE OR ODOR SMELL. ALL CHECKS GOOD. RETURNED SYSTEM TO NORMAL OPERATION.

Part: UNKNOWN — ODOR · airframe 29,091 hrs · 39,755 cycles

DURING DESCENT, STRONG BURNING ODOR FROM LEFT PACK WHILE PACK IS IN LOW. (FLT 5504) PERFORMED OPS CHECK ON LEFT PACK USING APU BLEED AND BOTH ENGINE BLEED SOURCES COULD NOT DUPLICATE ON GROUND, NO SMOKE OR BURNING ODOR OF ANY KIND, OPS CHECK GOOD.

Part: COOLING FAN — FAULTY (AC SYSTEM) · airframe 28,824 hrs · 39,388 cycles

SMOKE IN COCKPIT AND CABIN WHEN PACKS SELECTED TO NORMAL WHILE ON GROUND WITH APU ON. (FLT 1356) REPLACED GROUND COOLING FAN. P/N: EVAC 2322C2 S/N ON: 302 S/N OFF: 507

Part: WIRE — DISCONNECTED (CABIN) · airframe 28,507 hrs · 38,929 cycles

OVERHEAD EMERGENCY LIGHT INOP. (FLT 5308) RECONNECTED WIRES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,507 hrs · 38,929 cycles

EMERGENCY PATH LIGHT AT ROW 8 BURNED OUT. (FLT 5427) REPLACED LIGHT ASSEMBLY.

Part: SPAR — CRACKED (RT WING) · airframe 28,519 hrs · 38,950 cycles

RIGHT WING FORWARD LOWER AUXILIARY SPAR OUTBOARD OF NACELLE CRACKED IN 2 LOCATIONS. (C-CHECK) REPAIRED LOWER AUXILIARY SPAR.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 28,028 hrs · 38,282 cycles

LOST CABIN PRESSURE. (FLT 6453) REPLACED ELECTRONIC CONTROLLER. P/N 22201T011400, S/N OFF 465

Part: STRINGER — CRACKED (RT WING) · airframe 26,532 hrs · 36,190 cycles

RIGHT WING LOWER STRINGER FORWARD OF NR 1 FUEL PANEL STRINGER NR 10 CRACKED. (C-CHECK) REPAIRED PER SRM.

Part: ACTUATOR — FAILED (RT MLG) · airframe 25,786 hrs · 35,102 cycles

RIGHT MLG WOULD NOT RETRACT. (FLT 6269) REPLACED RIGHT MLG ACTUATOR. P/N 19595-000-8, S/N OFF T98141.

Part: SIGN — MISSING (CABIN) · airframe 25,136 hrs · 34,192 cycles

EXIT ROW SIGN AT ROW 9 IS MISSING. (FLT 6886) RELAMPED EXIT SIGN.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,015 hrs · 32,645 cycles

EMERGENCY LIGHTS AT ROW 6 WILL NOT COME ON. (FLT 6419) REPLACED EMERGENCY BATTERY PACK.

Part: BEAM — CRACKED (LT NACELLE) · airframe 21,792 hrs · 29,422 cycles

LEFT NACELLE HYDRAULIC BAY DOOR CUTOUT OUTBOARD BEAM CRACKED. (C CHECK) REPLACED BEAM PER SRM.

Part: STRINGER — CRACKED (LT WING) · airframe 21,792 hrs · 29,422 cycles

LEFT INBOARD WING LOWER STRINGER 10 IS CRACKED AT RIB 6. (C CHECK) REPAIRED PER SRM.

Part: BALLAST — ODOR (CABIN LIGHTS) · airframe 21,165 hrs · 28,533 cycles

SMOKE AND STRONG ELECTRICAL ODOR FROM THE OVERHEAD ABOVE 3A. REPLACED BALLAST.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 20,854 hrs · 28,139 cycles

FLT 7802 - EMERGENCY LIGHTS ON FLOOR INOP. REPLACED NR 1 ELBP PN D366-04-001, SN OFF 1231/06-96.

Part: COVER — BROKEN (EMERGENCY LIGHTS) · airframe 20,814 hrs · 28,093 cycles

FLT 7793 - ROW 9 LOWER EXIT LIGHT COVER IS BROKEN. REPLACED SIGN.

Part: RELAY — BURNED · airframe 20,805 hrs · 28,083 cycles

FLT 7816 - FEEDER PROTECTION RELAY AND SUPPORT ARE BURNED UP. REPLACED FEEDER PROTECTION RELAY, SUPPORT AND TWO EACH BUSS BARS.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 20,686 hrs · 27,948 cycles

FLT 5672 - EMERGENCY LIGHT IN MID CABIN INOP. REPLACED BATTERY PACK PN D366-04-001.

Part: MOUNT — CRACKED (LT MLG HYD PACK) · airframe 20,075 hrs · 27,144 cycles

LEFT MLG HYDRAULIC PACK LOWER O/B MOUNT CRACKED. C-CHECK, REPLACED MOUNT.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 19,809 hrs · 26,786 cycles

AFT EMERGENCY LIGHTS INOP. REPLACED THE AFT EMERGENCY LIGHT BATTERY PACK, PN D366-04-001, SN ON 1195, SN OFF 551.

Part: PROPELLER — MALFUNCTIONED (LEFT) · airframe 19,691 hrs · 26,615 cycles

PERFORMED GO-AROUND WHEN ENGINES WOULD NOT GO INTO GROUND IDLE. PERFORMED OPERATIONAL TEST OF FLIGHT IDLE STOP SYSTEM IAW AMM 76-13-00 WITH NO FAULTS. REPLACED LEFT PROP ASSEMBLY WITH SERVICEABLE UNIT IAW MM 61-10-00 DUE TO TORQUE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 18,709 hrs · 25,342 cycles

FLT 5544 - EMERGENCY LIGHTS ARE INOP. REPLACED BATTERY PACK. OPS CHECKS GOOD.

Part: SEAL — LEAKING (CARGO DOOR) · airframe 18,594 hrs · 25,191 cycles

FLT 5758 - LOST CABIN PRESSURE AND OXYGEN MASKS DEPLOYED. REPAIRED UPPER CARGO DOOR SEAL. PRESSURIZATION CHECKS GOOD IN AUTO AND MANUAL MODES.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 18,312 hrs · 24,775 cycles

FLT 5712 - DURING CLIMB, OXYGEN MASKS DROPPED. REPLACED ELECTROPNEUMATIC OUTFLOW VALVE IAW MM 21-30-03. OPS CHECK GOOD AT THIS TIME.

Part: STRINGER — CRACKED (RT WING) · airframe 18,365 hrs · 24,860 cycles

RIGHT WING NR 2 FUEL PANEL STRINGER IS CRACKED ALONG AFT SIDE, FOUND AT C-CHECK. REPAIRED STRINGER IAW SRM 120 57-20-03 PG 206-211 FIG 202.

Part: STRINGER — DAMAGED (RT WING) · airframe 18,074 hrs · 24,450 cycles

RIGHT DEFUEL PANEL HAS ONE RIVET LEAKING FUEL. ACCOMPLISHED REPAIR TO NR 8 STRINGER IAW SRM 57-20-03.

Part: SWITCH — DIRTY (PAX DOOR) · airframe 17,964 hrs · 24,306 cycles

FLT 3681 - CABIN DOOR WOULD NOT OPEN FOR DEPLANEMENT. CLEANED THE DOOR "CLOSE" SWITCH. OPS CHECK GOOD.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 17,734 hrs · 24,048 cycles

LOWER FORWARD STRINGER IN LEFT WING ACCESS PANEL INBOARD OF NACELLE IS CRACKED. FOUND AT C-CHECK, REPAIRED LEFT WING STRINGER IAW SRM 57-20-103 PG 203.

Part: WIRE — CORRODED (DOOR WARNING) · airframe 17,514 hrs · 23,715 cycles

LEFT TANK DOES NOT ACCEPT PRESSURE REFUELING. REPLACED CORRODED SPLICES FOUND ON FUEL SERVICE DOOR MICROSWITCH WIRING. OPS CHECK GOOD AT THIS TIME.

Part: WINDSHIELD — CRACKED · airframe 17,168 hrs · 23,286 cycles

LEFT DIRECT VISION WINDOW IS CRACKED. REPLACED LEFT DIRECT VISION WINDOW IAW 56-11-01.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 16,204 hrs · 22,021 cycles

FOUR CONSECUTIVE WHITE EMERGENCY LIGHTS ARE INOP ON LEFT SIDE. REPLACED CENTER ELBP. OPERATIONAL CHECKS GOOD IAW 3-50-00.

Part: UNKNOWN — ODOR (CABIN) · airframe 15,848 hrs · 21,522 cycles

IN FLIGHT DETECTED AN ODOR OF SMOKE. INSPECTED A/C AND OPERATED PACKS. NO EVIDENCE OF FIRE OR SMOKE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 14,507 hrs · 19,728 cycles

FOUND EMERGENCY EXIT LIGHT OVER ROW 9 INOP. RELAMPED EMERGENCY EXIT LIGHT OVER ROW 9, OPERATIONAL CHECK GOOD.

Part: PCU — LEAKING (RUDDER) · airframe 13,914 hrs · 18,834 cycles

BLUE HYD RESERVOIR LOW LEVEL LIGHT CAME ON INFLIGHT. REPLACED RUDDER PCU PER EMB 120 MM 27-22-01, OPERATIONAL CHECK GOOD.

Part: RELAY — DEFECTIVE (EMERGENCY LIGHTS) · airframe 13,108 hrs · 17,751 cycles

EMERGENCY LIGHTS WILL NOT EXTINGUISH WHEN POWER REMOVED FROM AIRCRAFT. REPLACED RELAY IAW WM 20-00-02. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,758 hrs · 17,262 cycles

ONE RED EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE AT FORWARD DOOR. REPLACED SECOND FLOOR RED EMERGENCY LIGHT ASSY AT PAX DOOR. OPERATIONAL CHECK GOOD.

Part: LIGHT — SMOKE (CABIN) · airframe 12,726 hrs · 17,217 cycles

AISLE LIGHT AT 10A HAD SMOKE COMING OUT OF IT. REPLACED CEILING LIGHT FIXTURE AT 10A. OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (WARNING SYSTEM) · airframe 12,247 hrs · 16,596 cycles

TAKEOFF TRIM AURAL WARNING WHEN TRIM IS IN THE GREEN BAND. A BROKEN WIRE WAS REPAIRED. OPERATIONAL CHECK GOOD REFERENCING 27-00-00.

Part: FLAP TRACK — WORN (TE FLAPS) · airframe 11,361 hrs · 15,411 cycles

AFTER TAKEOFF SELECTED FLAPS UP AND RECEIVED FLAP DISAGREEMENT. REMOVED AND REPLACED RT IB FLAP OB TRACK AND ALL ROLLERS ON RT IB FLAP IAW 27-50-02, OPERATIONAL CHECKS GOOD.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT) · airframe 11,061 hrs · 14,978 cycles

WHEN EMERGENCY LIGHT TESTED, MIDDLE ROW DOES NOT TURN ON. WHEN EMERGENCY LIGHT TURNED OFF AND AC POWER OFF, MIDDLE ROW LIGHTS TURN ON. REPLACED AND SECURED FORWARD CABIN EMERGENCY BATTERY PACK. OPERATIONAL CHECK GOOD.

Part: COMPUTER — FAULTY (STALL WARNING) · airframe 10,649 hrs · 14,401 cycles

LEFT STALL TEST LIGHT ILLUMINATES INTERMITTENTLY ON GROUND DURING TAXI. STALL TEST ON POWER UP IS SATISFACTORY. REPLACED NR 1 STALL WARNING COMPUTER WITH SERVICEABLE UNIT AS REQUIRED. SYSTEM OPS CHECK GOOD IAW EMB 120 MM 27-34-00.

Part: LIGHT — BROKEN (ROW 6A) · airframe 10,543 hrs · 14,258 cycles

EMERGENCY SIDEWALL LIGHT AT 6A BROKEN. REPLACED LIGHT FIXTURE. OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (ATTITUDE) · airframe 10,373 hrs · 14,038 cycles

IN FLIGHT, AUTOPILOT FAILED ON CAPTAIN'S SIDE. AHRS FLAGS ATT, HDG, AND FD. CYCLED ON AND OFF. F/O'S AUTOPILOT OPERATES NORMAL. INSTALLED NEW SERVICEABLE AHRS COMPUTER ON CAPTAIN'S SIDE. SYSTEM OPS CHECKS GOOD AND AUTOPILOT OPS CHECKS GOOD IAW MM 34-21-00.

Part: UPLOCK — OUT OF RIG (RT MLG) · airframe 7,959 hrs · 10,994 cycles

RIGHT MAIN LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO DRO. RUNNING GEAR UP AND DOWN, FOUND THE UPLOCK HOOK TO BE OUT OF RIG. ADJUSTED UPLOCK HOOK ACTUATOR ROD PER MM CHAPTER 32-32-09. OPS CHECK GOOD.

Part: WIRE — BROKEN (FIRE WARNING SYS) · airframe 7,914 hrs · 10,944 cycles

INTERMITTENT INDICATIONS OF BAGGAGE COMPARTMENT SMOKE/FIRE OCCURRED. COMPLIED WITH MEMORY ITEM & QRH BY ACTUATING FIRE EXTINGUISHERS. REMOVED AND REPLACED BOTH SMOKE DETECTORS IN CARGO BAY IAW MM 26-15-0. REPAIRED BROKEN WIRES W11-5695-22 AND W110-5700-22 AT TEST PANEL. INSPECTED CARGO COMPARTMENT SMOKE DETECTORS WIRING HARNESS AND CANNON PLUGS. FOUND NO DEFECTS. PERFORMED CARGO COMPARTMENT FIRE/SMOKE WARNING TEST, OPS CHECK GOOD AT THIS TIME.

Part: BEAM — CORRODED (FUSELAGE) · airframe 7,541 hrs · 10,452 cycles

EXCESSIVE CORROSION ON BEAM IN FRONT OF LAV BETWEEN FRAMES 38 AND 40. REMOVED AND REPLACED BEAM AND RIVETED IAW ASM 51-40-02.

Part: FRAME — CRACKED (LT NACELLE) · airframe 7,541 hrs · 10,452 cycles

LEFT NACELLE OUTBOARD AND INBOARD FRAME NR 17 CRACKED. INSTALLED REPAIR DOUBLER ON FRAMES IAW EMB SRM 51-70-05 AND 51-40-02.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 7,541 hrs · 10,452 cycles

FRAME 13 RIGHT SIDE CRACKED ON INSIDE AND OUTSIDE OF VERTICAL BRACE, AT COCKPIT DOOR OPENING. REMOVED AND REPLACED INSIDE L-BRACKET AND FABRICATED AND INSTALLED DOUBLER IAW SRM 51-70-05 AND 51-40-02.

Part: RELAY — FAILED (NLG STEERING) · airframe 7,103 hrs · 9,908 cycles

AIRCRAFT PULLS LEFT ON TAKEOFF ROLL AT 80 KNOTS. REMOVED AND REPLACED NOSE WHEEL STEERING RELAY WITH SERVICEABLE UNIT IAW MM 32-50-00. OPS CHECK GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 6,283 hrs · 8,912 cycles

ON TAKEOFF, AUTO FEATHER AURAL WARNING SOUNDED WITH SWITCH IN THE ON POSITION AND SYSTEM ARMED. AUTO FEATHER SYSTEM OPS CHECK GOOD DURING TEST. POWERED DOWN AND BACK UP. PERFORMED HIGH SPEED TAXI. OPS CHECK GOOD.

Part: CONTROL BOX — MALFUNCTIONED (E/E BAY) · airframe 6,257 hrs · 8,877 cycles

AFTER TAKEOFF, DOWNLOCK RELEASE NEEDED FOR GEAR RETRACTION. FLIGHT IDLE UNLOCK LIGHTS ILLUMINATED ON GLARESHIELD. AUTO PRESSURIZATION UNABLE TO CONTROL CABIN ALTITUDE. REMOVED AND REPLACED LANDING GEAR RELAY BOX. LANDING GEAR RETRACTION, OPS CHECKS GOOD AT THIS TIME AND FLIGHT IDLE STOP UNLOCK LIGHTS OPS CHECKS GOOD AT THIS TIME. OPS CHECK GOOD AT THIS TIME.

Part: ENGINE — FLUCTUATES (RIGHT) · airframe 5,987 hrs · 8,621 cycles

ON TAKEOFF ROLL RIGHT NP DID NOT REACH 100 PERCENT AND FLUCTUATED BETWEEN 96 AND 98.5 PERCENT. TAKEOFF WAS ABORTED. PERFORMED ENGINE RUNS AND OPS CHECKED PROP SYNC. SIMULATED TAKEOFF ROLL. NO FAULTS NOTED. COULD NOT DUPLICATE ERROR. ALL ENGINE PARAMETERS NORMAL. ALSO CHECKED RIGHT ENGINE PROP SYNC CANNON PLUG (CLEANED AND OHMED). NO FAULTS. CHECKED PROP SYNC GAP. ALL CHECKS GOOD. OPS CHECK GOOD.

Part: SERVO — DEFECTIVE (RUDDER) · airframe 4,058 hrs · 5,878 cycles

RUDDER HAS CLICK IN TRAVEL AS IT IS MOVED THROUGH FULL TRAVEL. INSPECTED AND DETERMINED RUDDER TRIM SERVO TO BE CAUSE OF CLICKING. INSTALLED SERVICEABLE SERVO FOR RUDDER TRIM IAW MM 27-00-00. RUDDER OPS CHECK GOOD. SMOOTH THROUGH FULL TRAVEL. P/N: 622-5734-002 S/N ON: 6060 S/N OFF: 10359

Part: HARNESS — LOOSE (T6 INDICATOR) · airframe 4,371 hrs · 6,223 cycles

DURING CLIMB NUMBER ONE T6 INDICATOR (BOTH ANALOG & DIGITAL) FLUCTUATED CONTINUOUSLY +/- 200 DEGREES. OTHER ENGINE INDICATIONS NORMAL. PROBLEM CONTINUED FOR 20-25 MINUTES, THEN T6 INDICATIONS STABILIZED DURING DESCENT, AFTER POWER REDUCTION. REPLACED WIRES FROM T6 PROBE HARNESS TO TERMINAL BLOCK. WIRE WAS LOOSE IN TERMINAL CONNECTION. RAN ENGINE, T6 INDICATION NORMAL, BOTH ANALOG AND DIGITAL. NO FLUCTUATIONS AS PREVIOUSLY INDICATED. OPS CHECKS GOOD.

Part: PROXIMITY SENSOR — FAILED (ELEVATOR TAB) · airframe 3,827 hrs · 5,417 cycles

RECEIVED TRIM WARNING DURING TAKEOFF ROLL WITH TRIM SET IN GREEN BAND. ABORTED REMOVED AND REPLACED LEFT TRIM TAB PROXIMITY SENSOR (ELEVATOR) IAW EMB120 MM 27-32-05. SYSTEM OPS CHECK GOOD. RIGGED RIGHT HAND TRIM TAB IAW 27-32-00. P/N: ATG120TR.

Part: SERVO — FAILED (ELEVATOR) · airframe 3,717 hrs · 5,276 cycles

DURING DESCENT INTO SEA AT 220 IAS, 13000 FT THE AIRCRAFT MADE AN UNCOMMANDED NOSE PITCH UP TO 15 DEGREES AND AUTOPILOT DISENGAGED. THERE WAS NO FORWARD TRIM AVAILABLE AFTER THAT. FORWARD YOKE PRESSURE WAS NEEDED UNTIL LANDING TO MAINTAIN PITCH CONTROL. INSPECTED CABLES, PULLEYS, ELEVATOR HINGE POINTS, ELEVATOR TRIM TAB. PERFORMED FREEDOM OF MOVEMENT CHECK. OPS CHECKED AUTOPILOT SERVOS. CHECKED RIGGING OF ELEVATOR AND ELEVATOR TRIM. REMOVED AND REPLACED ELEVATOR SERVO IAW MM 22-10-05 AND REMOVED AND REPLACED APP-65 IAW MM 22-10-04. OPS CHECK GOOD. P/N SERVO: 622-5734-002, S/N ON: 2667, S/N OFF: 10433.

Part: LENS — BROKEN (EXIT SIGN) · airframe 2,841 hrs · 4,010 cycles

FLOOR LEVEL MAIN CABIN EXIT SIGN BROKEN INSTALLED NEW MAIN CABIN ENTRANCE FLOOR LEVEL LENS (EXIT) SIGN.