N580SW

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 32,424 hrs · 43,971 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 9 IS BURNED OUT. REPLACED LAMP.

Part: COMPUTER — FAILED (AUTOPILOT) · airframe 32,150 hrs · 43,626 cycles

UNCOMMANDED RT BANK WITH THE NR 1 AUTOPILOT ENGAGED. FLT 5303 REPLACED THE AILERON AUTOPILOT SERVO & NR 1 AUTOPILOT COMPUTER.

Part: SPLICE — DAMAGED (CABIN) · airframe 31,882 hrs · 43,261 cycles

FLOOR LEVEL EMERGENCY WHITE LIGHT OUT AT SEAT 3A. FLT#6487 REPLACED SPLICE IN WIRE AFT OF THE WHITE EMERGENCY LIGHT AT SEAT 3A.

Part: COVER — MISSING (CABIN) · airframe 31,882 hrs · 43,261 cycles

EMERGENCY LIGHT COVER MISSING ON 6A. FLT#5426 REPLACED EMERGENCY LIGHT COVER ASSEMBLY ON 6A SEAT.

Part: COMPUTER — FAILED (AUTOPILOT SYS) · airframe 30,324 hrs · 41,051 cycles

UNCOMMANDED ROLL IN FLIGHT, AUTO PILOT WAS HARD TO DISENGAGE. (FLT 6327) REPLACED THE A/P COMPUTER.

Part: LIGHT — BROKEN (CABIN) · airframe 30,304 hrs · 41,015 cycles

FLOOR LEVEL EMERGENCY EXIT AT 6A IS BROKEN. (FLT 5615) REPLACED EMERGENCY EXIT LIGHT AT 6A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,146 hrs · 40,799 cycles

FLOOR LEVEL EMERGENCY LIGHT STRIP LIGHT AT 11A INOPERATIVE. (SERVICE) INSTALLED NEW WHITE FLOOR LEVEL EMERGENCY LIGHT AT ROW 11.

Part: LIGHT — MISSING (CABIN) · airframe 29,847 hrs · 40,356 cycles

EMERGENCY LIGHT ON FLOOR NEXT TO SEAT 11A IS MISSING. (FLT 6329) INSTALLED SERVICEABLE LIGHT.

Part: CONTROL VALVE — DEFECTIVE (AC BAY) · airframe 29,600 hrs · 39,997 cycles

FLIGHT ATTENDANT SMELLED A PACK BURNING IN CABIN DURING FLIGHT. ON THE GROUND FLIGHT DECK BECAME SMOKEY WITH PACKS ON. (FLT 6238) REPLACED TEMP CONTROL VALVE IN REFERENCE TO EMB 120 MM. P/N: 979990-1 S/N OFF: 2081

Part: DOUBLER — CHAFED (FUSELAGE) · airframe 29,519 hrs · 39,878 cycles

LEFT LOWER FUSELAGE SKIN DOUBLER CHAFED AT HEAT EXCHANGER AREA. (C-CHECK) REPLACED DOUBLER ON LEFT FUSELAGE BEHIND HEAT EXCHANGER IN REFERENCE TO SRM.

Part: DOUBLER — CHAFED (FUSELAGE) · airframe 29,519 hrs · 39,878 cycles

RIGHT LOWER FUSELAGE SKIN DOUBLER CHAFED AT HEAT EXCHANGER LOCATION. (C-CHECK) REPLACED DOUBLER ON RIGHT FUSELAGE BEHIND HEAT EXCHANGER IN REFERENCE TO SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 29,302 hrs · 39,572 cycles

STRINGER 18L FORWARD END HAS CORROSION BY FORWARD PAX DOOR ACTUATOR. (C-CHECK) REPLACED FORWARD END OF STR 18L AND INSTALLED OVERLAPPING REINFORCING SECTION IN REFERENCE TO EMB 120 SRM.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 29,335 hrs · 39,621 cycles

CABIN BUTT STRAP BELOW FLIGHT ATTENDANT'S SEAT HAS CORROSION. (C-CHECK) REPLACED CABIN BUTT STRAP BELOW FLIGHT ATTENDANT'S SEAT IN REFERENCE TO EMB-120 SRM.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 28,747 hrs · 38,791 cycles

OVERHEAD STRIP LIGHTING ABOVE SEAT 5A BEGAN EMITTING SMOKE. (FLT 5388) REPLACED LIGHTING ASSEMBLY AT SEAT 5A.

Part: ROLLER — BROKEN (TE FLAP) · airframe 28,201 hrs · 38,058 cycles

FLAP DISAGREEMENT. (FLT 5339) REPLACED BROKEN ROLLER ASSEMBLY FOR RIGHT OUTBOARD FLAPS.

Part: SIGN — BROKEN (CABIN) · airframe 26,635 hrs · 35,924 cycles

FLOOR LEVEL EMERGENCY EXIT SIGN BROKEN. (FLT 6318) RE-SECURED FLOOR LEVEL EXIT SIGN.

Part: SIGN — MISSING (CABIN) · airframe 26,034 hrs · 35,079 cycles

FLOOR LEVEL EMERGENCY EXIT SIGN AT SEAT 6A MISSING. (FLT 6480) RE-SECURED "EXIT" SIGN AT SEAT 6A.

Part: STRINGER — CRACKED (RT WING) · airframe 26,236 hrs · 35,368 cycles

RIGHT WING STRINGER NR 10 CRACKED BETWEEN RIBS NR 7 & NR 9. (C-CHECK) REPAIRED RIGHT WING STRINGER NR 10 BETWEEN RIBS NR 7 & NR 9 PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,588 hrs · 31,553 cycles

MOST AFT OVERHEAD CEILING EMERGENCY LIGHT INOP. (FLT 6489) RELAMPED OVERHEAD CEILING EMERGENCY LIGHT.

Part: WIRE — DAMAGED (APU) · airframe 23,122 hrs · 30,902 cycles

SMOKE IN COCKPIT FROM APU BLEED SOURCE. (FLT 5258) REPLACED POWER WIRE AND TERMINAL IN APU RELAY BOX.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,811 hrs · 30,441 cycles

CEILING EMERGENCY LIGHT INOP. (FLT 6230) RELAMPED EMERGENCY LIGHT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,533 hrs · 30,033 cycles

RIGHT EXTERNAL FRAME 24 UPPER CORNER CRACKED. (C CHECK) REPAIRED PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 22,533 hrs · 30,033 cycles

STRINGER 19 FORWARD OF PASSENGER DOOR CORRODED. (C CHECK) REPAIRED PER SRM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,160 hrs · 29,521 cycles

FLT 6282 - CABIN DOOR EMERGENCY FLOOR LIGHT INOP. RELAMPED.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 19,806 hrs · 26,397 cycles

FLT 5485 - SEVERAL EMERGENCY FLOOR LIGHTS AND BOTH OVERWING EXIT LIGHTS ARE INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 19,179 hrs · 25,646 cycles

FLT 5473 - "EXIT" SIGN MISSING ON EMERGENCY EXIT DOOR AT ROW 6 BC. REPLACED EXIT LIGHT ASSEMBLY AT 6BC. OPS CHECK GOOD.

Part: CONTROL CABLE — CORRODED (LT AILERONS) · airframe 18,668 hrs · 24,908 cycles

LEFT LOWER AILERON CABLE CORRODED AT PULLEY, DISCOVERED AT C-CHECK. REPLACED LEFT LOWER AILERON CABLE IAW AMM 27-00-01.

Part: RIB — CRACKED (PAX DOOR) · airframe 18,668 hrs · 24,908 cycles

PAX DOOR, AFT MID INTERNAL RIB IS CRACKED, FOUND AT C-CHECK. NEW RIB INSTALLED IAW SRM 120 51-10-02 PG 3 SEC 3A.

Part: RVDT — BINDING (AILERONS) · airframe 18,551 hrs · 24,749 cycles

ON TAXI CHECK, YOKE ONLY DEFLECTS APPROX 1/3 OF THE WAY TO FULL RIGHT AILERON. REPLACED NR 1 AILERON RVDT AND ALIGNED IAW MM 31-30-00.

Part: WIRE — BURNED (COFFEEMAKER) · airframe 18,049 hrs · 24,063 cycles

LEFT HOT JUG IS NOT HEATING. REPLACED BURNED WIRE LEAD AND CONNECTOR. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — JAMMED (RUDDER) · airframe 17,116 hrs · 22,880 cycles

RUDDER PEDALS JAMMED ON LANDING ROLL. REPLACED THE RUDDER PCU IAW MM 27-22-01 AND RII 27-300-1006. OPERATIONAL CHECKS GOOD, SN/OFF 0121.

Part: COFFEEMAKER — OVERHEATED (GALLEY) · airframe 17,098 hrs · 22,858 cycles

FA REPORTS AN ODOR OF OVERHEATING NEAR THE COFFEE POT. REPLACED AFT HOT JUG DUE TO LEAKING SEAL. OPS CHECK GOOD REF 25-00-00.

Part: ACTUATOR — MALFUNCTIONED (RUDDER) · airframe 16,923 hrs · 22,653 cycles

RIGHT RUDDER PEDAL WOULD NOT MOVE WITH BOTH RUDDER SWITCHES ON. REPLACED BLUE HYDRAULIC RUDDER ACTUATOR IAW AMM 27-22-02. OPERATIONAL CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,218 hrs · 21,794 cycles

EMERGENCY EXIT ROW LIGHT AT SEAT 6AB IS INOP. REPLACED LAMP ASSEMBLY IAW 33-50-00. OPERATIONAL CHECKS GOOD, P/N:10-1301-15.

Part: SELECTOR — MALFUNCTIONED (COCKPIT) · airframe 15,570 hrs · 20,920 cycles

DURING LANDING FLAPS WOULD NOT GO TO 45 DEG. REPLACED FLAP SELECTOR LEVER ASSY IAW EMB 120 MM 27-50-01. OPERATIONAL CHECK GOOD. PN ON 120-64207-165, OFF 120186.

Part: WIRE — BROKEN (CABIN) · airframe 15,570 hrs · 20,920 cycles

BROKEN WIRE AT FWD MOST EMERGENCY LIGHT ON FLOOR. REPAIRED BROKEN WIRE AT EMERGENCY FLOOR LIGHT. OPERATIONAL CHECK GOOD.

Part: BUSHING — WORN (PAX DOOR) · airframe 15,362 hrs · 20,676 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. REPLACED PAX DOOR BUSHING AND HARDWARE. RIGGED PAX DOOR IAW AMM 52-11-00. OPERATION CHECK GOOD.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,326 hrs · 19,355 cycles

EMERGENCY FLOOR LEVEL LIGHT INOPERATIVE ABEAM 2A. REPLACED ONE LIGHT FIXTURE EMERGENCY FLOOR LIGHTS. REPLACED FUSE IN RIGHT OVERHEAD PANEL. OPS CHECK GOOD.

Part: SIGN — DISLODGED (EMERGENCY EXIT) · airframe 13,948 hrs · 18,839 cycles

EXIT SIGN NEAR MAIN CABIN DOOR FELL OFF. REPLACED EXIT SIGN BY PAX DOOR IAW MM 33-40-00 . OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 13,842 hrs · 18,701 cycles

ONE OF TWO RED EMERGENCY FLOOR PATH LIGHTING ARE INOPERATIVE AT THE FORWARD DOOR. RELAMPED FORWARD RED EMERGENCY FLOOR PATH LIGHTING. OPERATIONAL CHECK GOOD.

Part: TERMINAL — LOOSE (EMERGENCY LIGHT) · airframe 13,776 hrs · 18,612 cycles

ONE OF TWO RED LIGHTS EMERGENCY FLOOR PATH LIGHTING ARE INOPERATIVE AT THE FORWARD DOOR. FOUND LOOSE TERMINAL CONNECTING THE BULB TO THE CIRCUIT. RESECURED LOOSE BULB, OPERATIONAL CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 13,635 hrs · 18,425 cycles

ONE EMERGENCY LIGHT OUT. RELAMPED INOPERATIVE LIGHT ASSEMBLY ON THE FLOOR EMERGENCY STRIP, OPERATIONAL CHECK GOOD.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,472 hrs · 18,195 cycles

AFT WHITE EMERGENCY FLOOR LIGHT IS INOPERATIVE. REPLACED AFT WHITE EMERGENCY FLOOR LIGHT SOCKET ASSY. OPERATIONAL CHECK GOOD. REF 33-50-02.

Part: MECHANISM — LACK OF LUBE (PAX DOOR) · airframe 13,472 hrs · 18,195 cycles

PAX DOOR HARD TO OPEN. REMOVED PAX DOOR TRIM, CLEANED AND LUBED DOOR MECHANISMS, RE-INSTALLED DOOR TRIM, OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAP) · airframe 13,472 hrs · 18,195 cycles

ON GROUND WHEN FLAPS ARE RETRACTED FROM 45 DEGREES TO UP NACELLE FLAPS ARE SLOWER THAN OTHER SEGMENTS RESULTING IN DISAGREEMENT. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR PER EMB 120 MM 27-50-00. OPERATIONAL CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 13,416 hrs · 18,120 cycles

FLOOR EMERGENCY LIGHTING, FIRST WHITE LIGHT INOPERATIVE. REPLACED LAMP FIRST WHITE FLOOR EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 13,416 hrs · 18,120 cycles

APU BLEED AIR CAUSING SMOKE IN CABIN WITH PACKS ON. REPLACED APU ASSEMBLY IAW EMB 120 MM 49-00-01 OPERATIONAL CHECK GOOD. P/N 3800376-1, S/N P-449.

Part: RUDDER PEDAL — MISINSTALLED (COCKPIT) · airframe 13,299 hrs · 17,963 cycles

FO'S LEFT RUDDER PEDAL STUCK ON PEDESTAL TRIM PANEL. REINSTALLED RUDDER PEDALS CORRECTLY IAW MM 27-21-00. OPERATIONAL CHECK GOOD.

Part: SENSOR — MALFUNCTIONED (DUCT LEAK) · airframe 13,212 hrs · 17,836 cycles

RECEIVED ENGINE DUCT LEAK WARNING DURING FLIGHT. COMPLIED WITH QRH WARNING WOULD NOT EXTINGUISH; FOLLOWED QRH WHICH LED TO PRECAUTIONARY ENGINE SHUTDOWN. REPLACED THE SENSOR OVER THE PRESSURE REGULATOR ON THE LT SYSTEM. OPERATION CHECK GOOD.

Part: PRESSURE SWITCH — MALFUNCTIONED (HYD SYSTEM) · airframe 12,945 hrs · 17,467 cycles

RUDDER SPEED SWITCH LIGHT ILLUMINATED ON MAP. REPLACED BOTH RUDDER GREEN SYSTEM AND BLUE SYSTEM HYDRAULIC PRESSURE SWITCHES WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (RUDDER) · airframe 12,438 hrs · 16,774 cycles

COULD NOT PUSH RIGHT RUDDER PEDAL AFTER TAKEOFF. REPLACED RUDDER PCU PER MM 27-27-01. OP AND LEAK CHECK OK PER RII 27-312.

Part: SOCKET — DAMAGED (EMERGENCY LIGHT) · airframe 12,106 hrs · 16,352 cycles

1ST 3 LIGHTS OF THE FLOOR LEVEL EMERGENCY EXIT LIGHTS ARE NOT ILLUMINATING. INSTALLED INSULATING BOOT ON E-LIGHT SOCKET OVER PAX DOOR ENTRANCE. EMERGENCY LIGHTS OPS CHECK NORMAL. ALL PANELS AND ITEMS REMOVED FOR ACCESS SECURED.

Part: CLIP — CRACKED (RT WING) · airframe 12,106 hrs · 16,352 cycles

MIDDLE LOWER SKIN CLIP CRACKED AT RIB 16, RIGHT WING. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED MIDDLE LOWER SKIN CLIP AT RIB 16 ON RIGHT WING WITH SERVICEABLE UNIT IAW SRM 57-20-07.

Part: SUPPORT BRACKET — CRACKED (WINDOW) · airframe 12,079 hrs · 16,315 cycles

SUPPORT BRACKET AFT CENTER OF PILOT'S DV WINDOW CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED SKIN SUPPORT BRACKET, AFT CENTER OF PILOT'S DV WINDOW PER SRM 51-40-02 AND RII 53-301.

Part: CLIP — CRACKED (RT WING) · airframe 12,106 hrs · 16,352 cycles

2 ND FROM AFT LOWER SKIN CLIP CRACKED AT RIB 15, RIGHT WING. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED 2ND FROM AFT LOWER SKIN CLIP AT RIB 15 ON RIGHT WING WITH SERVICEABLE UNIT IAW SRM 57-20-07.

Part: CLIP — CRACKED (RT WING) · airframe 12,079 hrs · 16,315 cycles

MIDDLE LOWER SKIN CLIP CRACKED AT RIB 15, RIGHT WING. DISCOVERED DURING C-CHECK INSPECTION. REPLACED MIDDLE LOWER SKIN CLIP AT RIB 15 ON RIGHT WING WITH SERVICEABLE UNIT IAW SRM 57-20-07.

Part: SERVO — WILL NOT TEST (STICK SHAKER) · airframe 11,991 hrs · 16,198 cycles

STALL STICK SHAKER NR 1 WON'T TEST. REMOVED AND REPLACED NR 1 STICK SHAKER. OPS CHECK GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,983 hrs · 11,248 cycles

LT AFT-MOST SEAT TRACK SECTION CORRODED IN AREAS AS MARKED. REMOVED AND REPLACED PASSENGER SEAT TRACK LT AFT. NO OTHER DEFECTS NOTED.

Part: PRESSURE SWITCH — FAILED (RT ENGINE) · airframe 7,927 hrs · 11,164 cycles

RIGHT ENGINE AIR INLET DEICE BOOT FAILED IN FLIGHT AT FL240, -19 DEGREES C, 36 MINUTES AFTER DEPARTURE. RETURNED TO SLC. LEAK CHECKED RIGHT INLET DEICE SYSTEM FROM EJECTOR VALVE TO BOOTS AND FOUND NO LEAKS. REMOVED AND REPLACED RIGHT INLET BOOT PRESSURE SWITCH. OPS CHECKS GOOD.

Part: ANNUNCIATOR — FAULTY (COCKPIT) · airframe 7,642 hrs · 10,814 cycles

AFTER TAKEOFF, ATTEMPTED TO RAISE FLAPS AND RECEIVED A FLAP DISAGREEMENT ON THE OUTBOARD PAIR. RAN QRH PROCEDURE WITH NO CHANGE. RETURNED TO DEN. REMOVED AND REPLACED FLAP ANNUNCIATOR PANEL. CLEANED FLAP TRACKS AND CANNON PLUGS AND RAN SYSTEM DIAGNOSTICS. RAN FLAPS NUMEROUS TIMES. OPS CHECK GOOD IAW MM 27-00-00.

Part: OUTFLOW VALVE — DIRTY (CABIN PRESSURE) · airframe 7,422 hrs · 10,565 cycles

AIRCRAFT WILL NOT PRESSURIZE, MANUAL OR AUTO. WARMED AIRPLANE, CLEANED OUTFLOW VALVES. TEST RUN AND OPS CHECKED GOOD.

Part: ACTUATOR — FAILED (LT MLG) · airframe 6,875 hrs · 9,894 cycles

LEFT MAIN GEAR WOULD NOT RETRACT AT ALL. RETURNED TO SEA. REMOVED AND REPLACED LEFT MAIN GEAR ACTUATOR IAW EMB 120 MM 32-32-10. OPS CHECK GOOD. S/N OFF T86691.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 6,762 hrs · 9,712 cycles

DURING CLIMB OUT CABIN PRESSURE BEGAN TO OSCILLATE +/- 2000 FPM. SELECTED MANUAL MODE IAW QRH AND PRESSURE HELD NORMALLY. REPLACED ELECTRONIC PRESSURE CONTROLLER. OPS CHECK GOOD.

Part: CONNECTING ROD — BROKEN (RT AILERON) · airframe 5,210 hrs · 7,427 cycles

AFTER SHUTDOWN, AILERON CONTROL WHEEL WOULD NOT MOVE LEFT OR RIGHT WITHOUT EXCESSIVE FORCE. INSPECTED LEFT AND RIGHT AILERON CABLE ROUTING. NO DEFECTS NOTED. AILERONS HAVE FREE MOVEMENT. PSP MX REQUEST CHECK LEFT AND RIGHT RVIT (AILERON) FOR CONDITION. CHECK OF LEFT RVIT, FOUND TO BE OK. CHECK OF RIGHT RVIT FOUND SUPPORT (P/N 120-63140-001) BENT. FOUND CONNECTING ROD (P/N 120-63143) BROKEN. FOUND BELLCRANK (P/N 123-82549-007) FOR RUDDER INSTALLED. REMOVED AND REPLACED BELLCRANK. OPS CHECK GOOD. BELLCRANK (P/N: 123-82549-009).

Part: INDICATOR — FAILED (COCKPIT) · airframe 4,707 hrs · 6,695 cycles

NUMBER TWO ADI FAILED ON SHORT FINAL FOLLOWED BY HEADING CARD SPIN AND AUTO PILOT FAIL. REMOVED AND REPLACED NUMBER TWO AHC85 IAW MM 34-25-00. OPS CHECK GOOD. PN ON: 622-6190-204

Part: INDICATOR — FAILED (COCKPIT) · airframe 4,707 hrs · 6,695 cycles

ADI MALFUNCTIONS SHOWING PIT AND ROL FLAGS, FIRST OFFICERS SIDE SHOWS 4 DEGREE PITCH LOW. FIRST OFFICERS COMMAND BARS OFFSET LOW WHILE CAPTAINS COMMAND BARS OFFSET HIGH. RETURNED TO SFO. TOOK OFF AND RETURNED SECOND TIME WITH SAME MALFUNCTIONS. REPLACED AHRS COMPUTER. PN 622-6190-204 SN 1981 UNABLE TO DUPLICATE SQUAWK SECOND TIME. REPLACED DPU FOR TROUBLESHOOTING. OPS CHECKS GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 3,953 hrs · 5,588 cycles

ON PREFLIGHT FOUND EMERGENCY EXIT SIGNS ON ROW SIX AND OVERHEAD EMERGENCY FLOOD LIGHT TO BE INOP. USING FLIGHT DECK SWITCH AND/OR FLIGHT ATTENDANT LIGHT SWITCH HAD NO EFFECT. REMOVED AND REPLACED CENTER ELBP IAW MM 33-50-02, OPS CHECKS GOOD. P/N ON: D366-04-001, S/N: 489, S/N OFF: 1089.

Part: HARNESS — DAMAGED (MLG) · airframe 3,873 hrs · 5,491 cycles

UPON GEAR RETRACTION GREEN ''''B'''' LIGHT REMAINED ILLUMINATED WITH ''''A'''' RED LIGHT ILLUMINATED. RETURNED TO PSP. REPLACED ''''A'''' DOWNLOCK HARNESS ASSEMBLY. OPS CHECK GOOD. (P/N 120-41125-001) ON, (S/N T97557) ON, (S/N 2498) OFF.

Part: AHRS — TRIPPED (E & E COMPT)

INFLIGHT RECEIVED A PIT FLAG ON BOTH EADI'S WITH THE FO'S EADI SHOWING 10 DEGREES LOWER. RESET BOTH AHRS NR 2 CIRCUIT BREAKERS WITHOUT ANY CHANGE. QRH PROCEDURES WERE FOLLOWED WITHOUT ANY RESULTS. RETURNED TO SBA. PERFORMED AHRS INITIALIZATION AND ORIENTATION TEST PER AND AHRS OPERATES NORMAL.

Part: SOLENOID — FAILED (FLIGHT IDLE STOP)

THE IDLE 2 UNLK LIGHT ILLUMINATED IN FLIGHT. AS PER FLIGHT OPS BULLETIN B-12, DATED NOV 24,1998, THERE IS NO QRH PROCEDURE ASSOCIATED WITH ILLUMINATION OF THE LIGHT. RETURNED TO LAX. INSTALLED NEW FLIGHT IDLE STOP SOLENOID IAW 76-10-00. GROUND OPS CHECK GOOD.