N564SW

Part: COVER — MISSING (EXIT SIGN) · airframe 32,817 hrs · 44,849 cycles

RT SIDE OVERWING EXIT EMERGENCY LIGHT COVER MISSING. FLT 5646 REPLACED EMERGENCY EXIT LIGHT COVER FOR RT SIDE LOWER SIGN.

Part: CONNECTOR — DISCONNECTED (LT MLG) · airframe 32,738 hrs · 44,756 cycles

LANDING GEAR SYS DISAGREE WHEN SELECTING GEAR DOWN. LT MAIN RED B LIGHT, L MAIN GRN A LIGHT, ALL OTHER INDICATIONS NORMAL. VISUAL GEAR DOWN THROUGH CABIN WINDOW. FLT 5363 RECONNECTED CANNON PLUG ON LT MLG DOWN & LOCKED PROX SENSOR B. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,162 hrs · 44,010 cycles

MAIN CABIN DOOR EMERGENCY LIGHT WILL NOT ILLUMINATE. FLT#7425 REPLACED ENTRY LIGHT FIXTURE ASSEMBLY IAW AMM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 32,162 hrs · 44,010 cycles

FWD EMERGENCY LIGHT BATTERY PACK IS INOPERATIVE. FLT#7425 REPLACED FWD EMERGENCY POWER BATTERY LIGHT PACK IAW AMM. PN: D366-04-001, SNON: 234 & SNOFF: 213

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,785 hrs · 43,566 cycles

EMERGENCY LIGHT ABOVE F/A SEAT IS BURNED OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,332 hrs · 43,001 cycles

EMERGENCY OVERHEAD LIGHT AT MAIN CABIN DOOR DOES NOT ILLUMINATE. (FLT 6309) RELAMPED EMERGENCY LIGHT.

Part: WINDOW — LACK OF LUBE (COCKPIT) · airframe 29,791 hrs · 41,131 cycles

UNABLE TO OPEN FIRST OFFICER'S DIRECT VISION WINDOW. (FLT 5487) LUBRICATED FIRST OFFICER'S DIRECT VISION WINDOW.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 29,230 hrs · 40,402 cycles

AUTO PRESSURE FAILED AND DEPRESSURIZED AT 5,000'. (FLT 6198) REPLACED ELECTRONIC PRESSURE CONTROLLER & PRESSURIZED AIRCRAFT. P/N: 22201T011400 S/N OFF: 512.

Part: CAM — OUT OF ADJUST (CABIN DOOR) · airframe 28,672 hrs · 39,647 cycles

MAIN CABIN DOOR IS HARD TO OPEN. (FLT 7811) ADJUSTED MAIN CABIN DOOR FORWARD LOCK CAM.

Part: MECHANISM — LACK OF LUBE (CABIN DOOR) · airframe 28,536 hrs · 39,472 cycles

MCD IS HARD TO OPEN. (FLT 6309) LUBRICATED PAX DOOR LATCHING MECHANISM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,292 hrs · 39,186 cycles

FLOOR LEVEL EMERGENCY LIGHT NEAR MCD IS OUT. (FLT 6506) RELAMPED EMERGENCY LIGHT.

Part: TRANSMITTER — FAULTY (OIL SYSTEM) · airframe 26,298 hrs · 36,732 cycles

NR 2 ENGINE OIL PRESSURE SPIKED TO 80 PSI. ENGINE SHUT DOWN. (FLT 7772) REPLACED PRESSURE TRANSMITTER P/N APT-79-1000-80D, S/N OFF 4703-3-258.

Part: SPLICE — OVERHEATED (ICE/RAIN PROTECT) · airframe 25,830 hrs · 36,161 cycles

SPLICE SPBK38 DISCOLORED. (C CHECK) REPLACED SPLICE SPBK38.

Part: MOUNT FITTING — CRACKED (FUSELAGE) · airframe 25,830 hrs · 36,161 cycles

LEFT MOUNT CLIP AFT OF DV WINDOW FRAME 13 CRACKED. (C CHECK) REPAIRED PER SRM.

Part: SKIN — CRACKED (FLAP) · airframe 25,830 hrs · 36,161 cycles

RIGHT NACELLE FLAP LOWER SKIN CRACKED. (C CHECK) REPLACED FLAP PER AMM.

Part: MECHANISM — LACK OF LUBE (CABIN DOOR) · airframe 25,639 hrs · 35,919 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6642) LUBED DOOR MECHANISM.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 24,625 hrs · 34,636 cycles

HYDRAULIC FUMES IN COCKPIT. (FLT 7774) REPAIRED RUDDER HYDRAULIC LINE AT AFT BULKHEAD PER AMM.

Part: SIGN — BROKEN (CABIN) · airframe 24,224 hrs · 34,121 cycles

AFT LOWER EMERGENCY EXIT SIGN BROKEN. (FLT 6457) REPLACED LIGHT ASSEMBLY.

Part: CABIN PRESSURE — FAILED · airframe 23,892 hrs · 33,657 cycles

FLT 6388 - CABIN LOST PRESSURE. SYSTEM CHECKS ACCOMPLISHED AND CHECK NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 23,854 hrs · 33,605 cycles

FLT 5761 - EXIT ROW 6A EMERGENCY LIGHT BROKEN. REPLACED EXIT LIGHT ASSEMBLY.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 23,799 hrs · 33,531 cycles

FLT 5574 - EXIT SIGN ON MAIN CABIN DOOR BROKEN. REPLACED SIGN.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 23,665 hrs · 33,377 cycles

C-CHECK, STRINGER 18L BETWEEN FRAME 13 AND 14 CORRODED, MAJOR REPAIR. REPAIRED PER EMB SRM 53-10-03.

Part: CONNECTOR — BURNED (BEACON) · airframe 23,633 hrs · 33,341 cycles

FLT 7760 - ROTATING BEACON CONNECTOR BURNED. REPLACED BEACON ASSEMBLY AND CONNECTOR.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 23,633 hrs · 33,341 cycles

FLT 7759 - "EXIT" LIGHT COVER AT SEAT 6 C IS MISSING. REPLACED LIGHT ASSEMBLY.

Part: UNKNOWN — SMOKE (CABIN) · airframe 23,160 hrs · 32,753 cycles

FLT 5734 - AFTER POWER REDUCTION IN DESCENT, AIRCRAFT FILLED WITH SMOKE. SMOKE LIGHT ON MAP ASSOCIATED WITH LAV DETECTOR. INSPECTED RT AND LT ENGINES, RT AND LT PACKS, APU, NO DEFECTS FOUND. RAN ENGS AND APU IN MULTIPLE BLEED CONFIGURATIONS, COULD NOT DUPLICATE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,846 hrs · 32,352 cycles

FORWARD EMERGENCY LIGHT INOP. (FLT 5464) ALL FORWARD EMERGENCY LIGHTS CHECK NORMAL.

Part: BUSS BAR — BURNED (APU RELAY) · airframe 22,761 hrs · 32,228 cycles

FOUND BUSS BARS IN APU RELAY BOX BURNED. C-CHECK, INSTALLED NEW SERVICABLE BUSS BARS.

Part: CONTACTOR — BURNED (APU RELAY) · airframe 22,761 hrs · 32,228 cycles

FOUND CONTACTOR IN APU AUX RELAY BOX BURNED. C-CHECK, REPLACED APU CONTACTOR IN APU AUX RELAY SHELF.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 22,761 hrs · 32,228 cycles

JUMP SEAT FLOORBOARD, LT AND RT FLOOR PROP ANGLES ARE CRACKED. C-CHECK, REPLACED RT FLOOR PROP ANGLES.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 22,761 hrs · 32,228 cycles

AFT SUPPORT ANGLE IS CRACKED IN FRONT OF PAX DOOR. C-CHECK, REPLACED AFT SUPPORT ANGLE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 22,761 hrs · 32,228 cycles

RT FLOOR PROP CRACKED AT FRAME 13. C-CHECK, INSTALLED FILLER AND DOUBLER.

Part: FRAME — CRACKED (RT NACELLE) · airframe 22,761 hrs · 32,228 cycles

RT NACELLE O/B WHEEL WELL FRAME IS CRACKED. C-CHECK, INSTALLED REPAIR DOUBLER TO NR 2 NACELLE WHEEL WELL INNER WEB SUPPORT INTERCOSTAL O/B SIDE.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 21,736 hrs · 30,866 cycles

FLOOR EMERGENCY EXIT SIGN IS BROKEN. REPLACED EMERGENCY EXIT SIGN. OPS CHECK GOOD.

Part: ROLLER — BINDING (PAX DOOR) · airframe 20,512 hrs · 29,186 cycles

MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN, FLIGHT NR 5752. LUBED ROLLERS AS REQUIRED. OPS CHECK GOOD AT THIS TIME.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 20,377 hrs · 29,019 cycles

SEVERAL EMERGENCY LIGHTS ARE INOP, FLIGHT NR 3684. REPLACED CENTER EMERGENCY LIGHT BATTERY IAW MM 33-50-02. OPS CHECK GOOD.

Part: WIRE — LOOSE (PACK SWITCH) · airframe 19,060 hrs · 27,403 cycles

RIGHT PACK PRODUCES OVERHEATED SMELL. RESECURED WIRE TO RIGHT PACK SWITCH, OPERATIONAL CHECKS GOOD.

Part: WIRE — LOOSE (RT A/C PACK) · airframe 19,146 hrs · 27,527 cycles

RIGHT PACK PRODUCES OVERHEATED ODOR. SECURED WIRE TO RIGHT PACK SWITCH "LOW". OPS CHECKED GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 19,102 hrs · 27,475 cycles

RIGHT SIDE FLOORBEAM AT FRAME 40 FLOOR REQUIRES REPLACEMENT DUE TO CORROSION, DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT SIDE FLOORBEAM AT FRAME 40 PER SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 19,102 hrs · 27,475 cycles

CENTER RIB FRAME 13 BEHIND PILOTS AFT DV POST IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CENTER SUPPORT BRACKET (RIB) AT FRAME 13 BEHIND PILOTS AFT DV POST PER SRM 51-40-02 AND SEE RII 53-800-1000.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 19,102 hrs · 27,475 cycles

RIGHT SIDE FLOORBEAM AT FRAME 39 REQUIRES REPLACEMENT DUE TO CORROSION, DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT SIDE FLOORBEAM AT FRAME 39 PER 51-40-02.

Part: UNKNOWN — FUMES (COCKPIT & CABIN) · airframe 18,279 hrs · 26,360 cycles

WHEN THE BLEEDS ARE SWITCHED FROM ENGINE TO APU IN FLIGHT, OIL FUMES ARE SMELLED IN THE COCKPIT AND CABIN. COULD NOT DUPLICATE.

Part: GCU — MALFUNCTIONED (APU) · airframe 17,961 hrs · 25,935 cycles

AFTER APU SHUTDOWN SMOKE FILLED THE COCKPIT. REPLACED APU GCU. REPLACED APU STARTER/GEN AND REPLACED FEEDER PROTECTION RELAY. OPERATIONAL CHECKS GOOD, PN23080-013 SN/OFF 2364, PN2903-0002-001.

Part: SERVO — MALFUNCTIONED (AILERONS) · airframe 17,577 hrs · 25,370 cycles

ON PREFLIGHT OF FLIGHT CONTROLS. NOTICED RESISTANCE IN AILERON CIRCUIT. REPLACED AILERON SERVO IAW MM 22-10-05, OPERATIONAL CHECK GOOD.

Part: SERVO — MALFUNCTIONED (ELEVATOR) · airframe 16,495 hrs · 24,034 cycles

BINDING AND FRICTION FELT IN ELEVATOR MOVEMENT. REPLACED ELEVATOR SERVO IAW EMB 120 MM 22-10-05. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 16,332 hrs · 23,837 cycles

THREE EMERGENCY LIGHTS DO NOT TEST. REPLACED FORWARD EMERGENCY LIGHT BATTERY PACK IAW 73-00-00. OPERATIONAL CHECK GOOD, P/N: D366-04-001, S/N ON: 1139 S/N OFF: 1130.

Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 15,955 hrs · 23,314 cycles

LT OVERWING EXIT (6A) SIGN FELL OFF. REINSTALLED EXIT SIGN AS REQUIRED.

Part: LIGHT — UNSECURE (CABIN) · airframe 14,942 hrs · 22,004 cycles

ROW 6 EXIT PLACARD FELL OFF. INSTALLED NEW EMERGENCY LIGHT FIXTURE. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 14,863 hrs · 21,907 cycles

FOUR FLOOR LEVEL EMERGENCY LIGHTS AND BOTH PAIRS OF OVERWING EMERGENCY EXIT LIGHTS ARE INOPERATIVE. INSTALLED SERVICEABLE EMERGENCY LIGHT BATTERY PACK, OPERATIONAL CHECK GOOD.

Part: CARBON SEAL — LEAKING (RT ENGINE) · airframe 14,112 hrs · 20,944 cycles

OIL PRESSURE 50 PSID IN RIGHT ENGINE. PERFORMED QRH FOR LOW OIL PRESSURE 40-55 PSID. OIL PRESSURE WENT UP TO 60 PSID. INSTALLED NEW CARBON SEAL AND CENTRIFUGAL BREATHER GEAR SHAFT IAW P&W MM 3034622 72-20-00 PARA (2) (D) AND (10) (F). OPERATIONAL CHECK GOOD. P/N 3121371-01, 3037223.

Part: PANEL — MALFUNCTIONED (STALL WARNING) · airframe 13,719 hrs · 20,385 cycles

STALL WARNING TEST, RED LIGHTS REMAIN ILLUMINATED AFTER TEST. REPLACED STALL WARN TEST PANEL PER MM 27-34-08, OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (RUDDER TRIM) · airframe 12,816 hrs · 19,078 cycles

UNABLE TO USE RUDDER TRIM AT HIGH ALTITUDES AND COLD TEMP. REMOVED AND REPLACED RUDDER TRIM ACTUATOR IAW EMB 120 MM 27-23-02. OPS CK GOOD.

Part: SERVO — MALFUNCTIONED (AUTOPILOT SYS) · airframe 12,718 hrs · 18,920 cycles

AUTOPILOT WILL NOT CAPTURE OR HOLD ALTITUDE USING EITHER LEFT OR RIGHT FLIGHT DIRECTOR. FLIGHT DIRECTORS APPEAR TO WORK, BUT AP WANDERS OFF. REPLACED ELEVATOR SERVO WITH SERVICEABLE UNIT. BOTH APS & CPS CHECKED GOOD IAW MM 22-11-00.

Part: CONTROL PANEL — MALFUNCTIONED (AUTOPILOT) · airframe 12,614 hrs · 18,737 cycles

NEITHER CAPTAIN NOR F/O'S AUTOPILOT WILL CAPTURE AND FOLLOW THE COMMAND BARS, NOR WILL IT CAPTURE AN ALTITUDE. REMOVED AND REPLACED APP-65A AUTOPILOT CONTROL PANEL AND REPLACED ELEVATOR SERVO IAW EMB 120 MM 22-10-04. OPS CHECK GOOD. SERVO P/N: 622-5734-002, S/N OFF: 8426.

Part: PLUNGER — DAMAGED (SEQUENCE VALVE) · airframe 12,460 hrs · 18,493 cycles

DURING GEAR RETRACTION, LEFT MAIN LANDING GEAR WOULD NOT RETRACT. CYCLED LANDING GEAR 6-7 TIMES WITH SAME RESULT. RETURNED TO AIRPORT WITH NO FURTHER PROBLEM. REPLACED LEFT OUTBOARD MLG DOOR BEARING AND ADJUSTED LEFT OUTBOARD SEQUENCE VALVE PLUNGER IAW MM 32-32-04. OPS CHECK GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 11,902 hrs · 17,647 cycles

OVERHEAD EMERGENCY LIGHT GOING ON/OFF INTERMITTENTLY WHILE FA TESTED SWITCH. REPAIRED BROKEN WIRE TO ROW 9 OVERHEAD BIN EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: BRACKET — CRACKED (TE FLAP ROLLER) · airframe 11,305 hrs · 16,756 cycles

LT INBOARD FLAP BUTE DOOR INBOARD ROLLER BRACKET CRACKED. REPLACED ROLLER BRACKET ON LEFT INBOARD FLAP BUTE DOOR INBOARD POSITION.

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 10,969 hrs · 16,232 cycles

ABORTED TAKEOFF AT 70 KTS DUE TO TRIPLE CHIME WARNING, WITHOUT ANY OTHER ANNUNCIATIONS ACCOMPANYING IT. ALL TAKEOFF PARAMETERS WERE SET. RESET AURAL WARNING COMPUTER AND CHECK ALL WARNING SYSTEM. OPS CHECK GOOD ON GROUND.

Part: MONITOR — FAILED (COCKPIT) · airframe 10,508 hrs · 15,498 cycles

DEICE MONITOR INOP. RESET CB'S A5/A6 PER MX CONTROL, WITH NO CHANGE. SMELL OF BURNED WIRING, WAITED 20 MINUTES FOR SMELL TO CLEAR, NO CHANGE. BOTH CB'S POPPED ON THEIR OWN AFTER 5 MINUTES, WILL NOT RESET. REMOVED AND REPLACED DEICE MONITOR WITH SERVICEABLE UNIT. MONITOR CHECKS GOOD. ALL PANELS SECURED.

Part: WARNING SYSTEM — MALFUNCTIONED (ICE PROTECTION) · airframe 8,652 hrs · 12,635 cycles

WHILE EN ROUTE, CRUISE THE ICE PROTECTION MONITOR FAILED. FLIGHT RETURNED TO SFO. RESET DEICE MONITOR CB'S AND PERFORMED AN A/C POWER DOWN TO RESET SYSTEM. OPS CHECK GOOD AT THIS TIME.

Part: STRUT — OVERSERVICED (RT MLG) · airframe 8,348 hrs · 12,209 cycles

AT 80 KTS AIRCRAFT VEERED HARD LEFT. ABORTED TAKEOFF.FOUND RIGHT MAIN LANDING GEAR OVERSERVICED. RETURNED RIGHT MAIN LANDING GEAR TO PROPER POSITION.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 8,348 hrs · 12,209 cycles

PRESSURIZATION CABIN WOULD NOT PRESSURIZE IN AUTO. REFERRED TO QRH AND WENT TO MANUAL CONTROL. IN MANUAL CONTROL RATE SEEMED VERY SLOW, IT TOOK AROUND 2 MINUTES FOR THE CABIN TO START DOWN FROM 5000 FT TO 200 FT. RETURNED TO PSP. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER WITH A SERVICEABLE UNIT. OPS CHECK GOOD.

Part: PROXIMITY SWITCH — FAILED (NLG STRUT) · airframe 8,289 hrs · 12,105 cycles

AIRCRAFT RUNS TO LEFT ON TAKEOFF ROLL WITH FULL RIGHT RUDDER. ABORTED TAKEOFF.REMOVED AND REPLACED THE NOSE STRUT PROXIMITY SWITCH. ALSO REMOVED AND REPLACED THE FEEDBACK POT HARNESS. P/N: 20540-001-01

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 8,307 hrs · 12,141 cycles

LEFT AFT FLOOR SEAT TRACK CORRODED LAST SIX FEET.REMOVED AND REPLACED LEFT AFT FLOOR SEAT TRACK.

Part: CONTROL CABLE — WORN (AILERON) · airframe 8,307 hrs · 12,141 cycles

RIGHT AND LEFT UPPER AND LOWER AILERON CABLES WORN. REPLACED RIGHT AND LEFT UPPER AILERON AND LOWER CABLES.

Part: CONTROL CABLE — WORN (ELEVATOR TRIM) · airframe 8,307 hrs · 12,141 cycles

ELEVATOR TRIM OUTBOARD AND INBOARD CABLES WORN. REPLACED OUTBOARD AND INBOARD ELEVATOR TRIM CABLES.

Part: CONTROL CABLE — WORN (RUDDER) · airframe 8,307 hrs · 12,141 cycles

RIGHT MID INBOARD AND OUTBOARD RUDDER CABLES WORN. RIGHT AFT INBOARD AND OUTBOARD RUDDER CABLES WORN. REPLACED RIGHT MID INBOARD, OUTBOARD AND AFT INBOARD, OUTBOARD RUDDER CABLES.

Part: PULLEY — NICKED (RUDDER) · airframe 8,307 hrs · 12,141 cycles

AFT RUDDER RIGHT INBOARD CABLE PULLEY HAS NICK. REPLACED RIGHT AFT INBOARD CABLE AFT PULLEY.

Part: WARNING HORN — FALSE ACTIVATION (COCKPIT) · airframe 7,981 hrs · 11,630 cycles

INTERMITTENT FIRE BELL DURING GOUND OPERATIONS. NO LIGHTS SUPPORTING INDICATION. REPLACED AURAL WARNING UNIT. OPS CHECK GOOD.

Part: SQUAT SWITCH — FAILED (NLG) · airframe 6,884 hrs · 10,016 cycles

DURING CLIMBOUT 2000 FEET AURAL WARNING TAKEOFF CONTINOUSLY SOUNDED. ONCE POWER LEVERS PULLED BACK WARNING WENT AWAY. RETURNED TO AIRPORT. REPLACED LANDING GEAR RELAY BOX. P/N ON: 1201110-001, S/N ON: 125399-305, OFF: 120-339. REPLACED RELAY K0122 FOR OPERATIONAL CHECK. FAILED TEST FLIGHT. FOUND NOSE GEAR SQUAT SWITCH BAD. REMOVED AND REPLACED NOSE GEAR SQUAT SWITCH IAW EMB 120 MM 32-01-01. FUNCTIONAL CHECK OF AURAL WARNING SYSTEM WORKS NORMALLY. OPS CHECK GOODP/N ON: 25-00417-02. FOUND BAD FEMALE PIN AT RELAY K0194 RECEPTACLE. REPLACED FEMALE PIN. GROUND OPS CHECKS GOOD.

Part: AHARS — FAILED (LT& RT)

AFTER TAKEOFF ROLL, HSI/EADI PILOT AND COPILOT AHARS FAILED. RETURNED TO MRY. RERACKED AHARS COMPUTER. OPS CHECK GOOD.

Part: POWER LEVER — JAMMED (RT ENGINE)

RIGHT POWER LEVER STUCK AT 85 PERCENT TQ INFLIGHT. UNABLE TO RETARD POWER LEVER. SHUT ENGINE DOWN. FOUND BONDING STRAP HOOKED ON RIGHT POWER LEVER FLIGHT IDLE SOLENOID HOOK ON BELLCRANK. REMOVED BONDING STRAP AND INSTALLED SHORTER STRAP. MOVED POWER LEVER THROUGH FULL RANGE AND CHECKED CLEARANCE. OPS CHECKS GOOD.

Part: RMI — FAILED (NR 2)

AFTER TAKEOFF, SMOKE IN THE COCKPIT THAT APPEARED TO COME FROM RMI NUMBER 2. SMOKE STOPPED WHEN RADIO MASTER NORMAL SWITCH WAS TURNED OFF. AIRCRAFT RETURNED TO SBA. REPLACED NUMBER 2 RMI. ALSO, INSPECTED ALL WIRES AND OTHER INSTRUMENTS. NO DISCREPANCIES OR DEFECTS NOTED. OPS CHECK GOOD.