N292SW

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,339 hrs · 55,519 cycles

EMERGENCY LIGHT AT ROW 9 IS BURNED OUT. FLT 5344 RELAMPED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,908 hrs · 53,534 cycles

DAMAGE AT FS STA 15370.0 LEFT FUSELAGE EXTERNAL SKIN BELOW AND AFT OF CARGO DOOR CUT OUT AREA, CRACKED. (C-CHECK) REPAIRED FUSELAGE REINFORCEMENT AND SKIN BY MEANS OF INSTALLING FILLERS AND A EXTERNAL DOUBLER AT LEFT FS 15370.0 BETWEEN STR 19L AND 18L IAW ETD.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 36,548 hrs · 53,008 cycles

DEPARTING PDX ALL 3 LANDING GEAR DID NOT RETRACT UNTIL 2400 FT. AT THAT TIME GEAR RETRACTED NORMALLY. (FLT 5379) PERFORMED SEVERAL GEAR SWINGS WITH NO DEFECTS NOTED. ALL LANDING GEAR PERFORMED NORMAL.

Part: UNKNOWN — ODOR · airframe 36,057 hrs · 52,308 cycles

BURNT PACK SMELL ON ENGINE BLEED. (FLT 5405) INSPECTED LEFT PACK, NO DEFECTS NOTED. RAN LEFT PACK, NO SMELL NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,512 hrs · 51,517 cycles

FLOOR LEVEL EMERGENCY LIGHT NEAR MAIN CABIN DOOR OUT. (FLT 5293) RELAMPED EMERGENCY LIGHT.

Part: SEQUENCE VALVE — FAILED (RT MLG) · airframe 35,458 hrs · 51,455 cycles

THE RED IN TRANSIT LIGHTS REMAINED ON WHEN LANDING GEAR LEVER WAS PLACED IN THE UP POSITION AND THE RIGHT MAIN GEAR DOWN AND LOCKED. (FLT 5616) REPLACED RIGHT OUTBOARD SEQUENCE VALVE IN REFERENCE TO AMM. P/N: 120-32943-001, S/N: 2254.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,348 hrs · 48,465 cycles

FORWARD CABIN EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: SIGN — BROKEN (CABIN) · airframe 33,073 hrs · 48,072 cycles

EMERGENCY EXIT SIGN AT RIGHT SIDE OF ROW 6 BROKEN. (FLT 6379) REPLACED EMERGENCY LIGHT ASSEMBLY.

Part: WIRE — LOOSE (CABIN) · airframe 32,230 hrs · 46,888 cycles

EMERGENCY FLOOR RED LIGHT NOT WORKING AT ROW 1. (FLT 6818) RE-SECURED WIRE AT FLOOR LEVEL EMERGENCY LIGHT.

Part: HOT WATER POT — SMOKE (GALLEY) · airframe 32,075 hrs · 46,662 cycles

AFT HOT JUG PRODUCING SMOKE. (FLT 6181) REPLACED HOT LIQUID CONTAINER.

Part: REGULATOR — FAILED (DE-ICE SYSTEM) · airframe 31,073 hrs · 45,250 cycles

LEFT ENGINE SHUT DOWN DUE TO BLEED LEAK INDICATION. (FLT 6687) REPLACED DE-ICE SYSTEM PRESSURE REGULATOR. P/N 38E96-6A, S/N OFF RF-1888.

Part: SPLICE — BURNED (COCKPIT) · airframe 29,867 hrs · 43,507 cycles

COCKPIT LEFT SIDE CURRENT SENSOR SPLICE BURNT. (C-CHECK) REPAIRED SPLICE PER WMM.

Part: RIB — CRACKED (NACELLE) · airframe 29,867 hrs · 43,507 cycles

RIB CRACKED AT RIGHT INBOARD AND OUTBOARD UPPER NACELLE. (C-CHECK) REPLACED RIBS PER SRM.

Part: FITTING — CRACKED (RT NACELLE) · airframe 29,867 hrs · 43,507 cycles

RIGHT NACELLE WHEEL WELL INBOARD AREA VERTICAL FRAME FITTING CRACKED. (C-CHECK) REPLACED FITTING PER SRM.

Part: SPAR CAP — CRACKED (LT WING) · airframe 29,867 hrs · 43,507 cycles

LEFT WING FORWARD UPPER AUX SPAR CAP CRACKED. (C-CHECK) REPAIRED PER ETD.

Part: WIRE — BURNED (ELECTRICAL SYS) · airframe 29,867 hrs · 43,507 cycles

WIRE FROM CONTACTOR K0027 TO RCCB BURNT. (C-CHECK) REPLACED WIRE PER WMM.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 29,867 hrs · 43,507 cycles

PASSENGER DOOR FRAME CRACKED. (C-CHECK) REPLACED FRAME PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 29,867 hrs · 43,507 cycles

ANGLE CRACKED AT LEFT SIDE OF COCKPIT, BELOW FLOOR. (C-CHECK) REPLACED ANGLE PER SRM.

Part: FITTING — CRACKED (LT NACELLE) · airframe 29,867 hrs · 43,507 cycles

LEFT NACELLE WHEEL WELL INTERNAL VERTICAL FITTING CRACKED. (C-CHECK) REPLACED FITTING PER SRM.

Part: CHANNEL — CRACKED (RT NACELLE) · airframe 29,867 hrs · 43,507 cycles

RIGHT NACELLE CHANNEL CRACKED. (C-CHECK) REPLACED CHANNEL PER SRM.

Part: FRAME — CRACKED (LT NACELLE) · airframe 29,867 hrs · 43,507 cycles

LEFT NACELLE FRAME 1 INBOARD SIDE CRACKED. (C-CHECK) REPLACED LEFT NACELLE FRAME PER SRM.

Part: BELLCRANK — CORRODED (AILERON) · airframe 29,867 hrs · 43,507 cycles

RIGHT AILERON BELLCRANK CORRODED. (C-CHECK) REPLACED RIGHT AILERON BELLCRANK PER AMM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 29,867 hrs · 43,507 cycles

FUSELAGE STRINGERS 18 AND 19 CORRODED. (C-CHECK) REPAIRED AND REPLACED PER SRM.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 29,767 hrs · 43,366 cycles

OVERHEAD EMERGENCY LIGHT ABOVE 9C INOP. (FLT 6254) REPAIRED BROKEN WIRE.

Part: SIGNAL COND UNIT — FAULTY (LT ENGINE) · airframe 29,539 hrs · 43,041 cycles

LEFT PROP AUTO-FEATHERED UNCOMMANDED. (FLT 6181) REPLACED LEFT ENGINE TORQUE SIGNAL CONDITIONER.

Part: SIGNAL COND UNIT — FAULTY (LT ENGINE) · airframe 29,492 hrs · 42,975 cycles

LEFT PROP AUTO-FEATHERED UNCOMMANDED. (FLT 6192) REPLACED TORQUE SIGNAL CONDITIONER.

Part: WIRE — BROKEN (CABIN) · airframe 29,462 hrs · 42,934 cycles

EMERGENCY LIGHTS EXIT SIGN INOP. (FLT 6110) REPAIRED BROKEN WIRE.

Part: HMU — OUT OF RIG (LEFT) · airframe 29,421 hrs · 42,871 cycles

LEFT PROPELLER SPEED INCREASED UNCOMMANDED ON TAXI. (FLT 6630) RIGGED LEFT HMU.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 29,288 hrs · 42,665 cycles

MAIN CABIN DOOR HARD TO OPEN. (FLT 6357) INSPECTED AND LUBED MAIN CABIN DOOR.

Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 28,883 hrs · 42,138 cycles

FLT 6232 - EMERGENCY LIGHT AT THE FORWARD DOOR INOP. REPOSITIONED BULB.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 28,883 hrs · 42,138 cycles

FLT 6249 - MULTIPLE EMERGENCY EXIT SIGN LIGHTS OUT IN MAIN CABIN. REPLACED FORWARD EMERGENCY BATTERY PACK.

Part: SOCKET — FAILED (EMERGENCY LIGHTS) · airframe 28,445 hrs · 41,549 cycles

FLT 5406 - FORWARD FLOOR RED EMERGENCY LIGHT STRIP INOP. REPLACED SOCKET.

Part: ROD END — WORN (LT MLG) · airframe 28,341 hrs · 41,400 cycles

FLT 1005 - LEFT MAIN GEAR DID NOT RETRACT ON CLIMB UNTIL CYCLED A SECOND TIME. INSTALLED NEW ROD END AND LEVER ASSEMBLY ON LEFT MAIN GEAR ACTUATOR, P/N 19502-000-01.

Part: BULB — BROKEN (EMERGENCY LIGHT) · airframe 27,602 hrs · 40,395 cycles

FLT 5557 - EXIT SIGN AT MAIN CABIN DOOR, COVER MISSING AND BULBS BROKEN. REPLACED EXIT SIGN.

Part: BUTTSTRAP — CORRODED (FLOORBEAM) · airframe 27,028 hrs · 39,617 cycles

BUTT STRAP UNDER LAV IS CORRODED. (FOUND AT C-CHECK) REPLACED BUTT STRAP IAW EMB 120, SRM 51-10-02, PAGE 3 AND 51-40-02.

Part: ROD END — CORRODED (ELEVATOR) · airframe 27,028 hrs · 39,617 cycles

LT AND RT ELEVATOR UPPER BELLCRANK ROD ENDS SHOW SIGNS OF CORROSION. (FOUND AT C-CHECK) REPLACED THE LT AND RT ELEVATOR ROD END ASSEMBLIES IAW AMM 27-00-00.

Part: RCCB — MALFUNCTIONED (COCKPIT) · airframe 26,353 hrs · 38,725 cycles

FLT 5742 - SMOKE IN COCKPIT WHILE AT THE GATE. REPLACED RCCB FOR LEFT GROUND COOLING FAN. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,771 hrs · 37,892 cycles

EMERGENCY LIGHT OVER PAX DOOR IS INOP. REPLACED EMERGENCY LIGHT. OPS CHECKS GOOD.

Part: BULB — ODOR (EMERGENCY LIGHTS) · airframe 25,393 hrs · 37,357 cycles

FLT 5592 - THE ODOR OF SMOKE FILLED THE COCKPIT AND C/B A30 POPPED. REPLACED COURTESY LIGHT BULB. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 23,706 hrs · 34,996 cycles

ALL EMERGENCY LIGHTS AFT OF ROW 8 INOP. REPLACED THE AFT EMERGENCY LIGHT BATTERY IAW AFM 33-50-02. OPERATIONAL CHECKS GOOD.

Part: SIGN — DEFECTIVE (CABIN) · airframe 22,476 hrs · 33,220 cycles

LIGHTED EXIT SIGN AT FLOOR LEVEL SEAT 6C CAME APART. REPLACED EMERGENCY EXIT SIGN FIXTURE AT ROW 6. OPERATIONAL CHECKS GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,324 hrs · 32,996 cycles

FOUND CORROSION IN LEFT FLOOR SEAT TRACK. REMOVED AND REPLACED SECTIONS OF LEFT FLOOR SEAT TRACKS IAW 53-20-10 SRM AND 51-21-04 CPM.

Part: RIB — CRACKED (LT NACELLE) · airframe 22,324 hrs · 32,996 cycles

CRACK FOUND AT LEFT NACELLE INBOARD UPPER RIB BELOW EXHAUST MOUNT. REPLACED LEFT NACELLE INBOARD UPPER RIB IAW SRM 120 51-10-02 PG 3 SEC 3A.

Part: STRINGER — CRACKED (RT WING) · airframe 22,324 hrs · 32,996 cycles

RIGHT INBOARD WING, LOWER FRONT STRINGER FORWARD OF NR 2 FUEL PANEL CRACKED. REPAIRED STRINGER FORWARD OF NR 2 FUEL PANEL AT RIGHT INBOARD WING IAW SRM120 57-20-03, ALSO RII 57-900-1000.

Part: WINDSHIELD — UNKNOWN (COCKPIT) · airframe 22,228 hrs · 32,860 cycles

LOST PRESSURIZATION IN FLIGHT, DIVERTED TO FRESNO. REMOVED AND REPLACED LEFT WINDSHIELD IAW EMB MM 56-10-01 AND RII 56-200-1000. FUNCTIONAL CHECKS GOOD.

Part: LIGHT — BURNED (CABIN) · airframe 21,379 hrs · 31,576 cycles

OVERHEAD AISLE LIGHT OVER SEAT 10A MELTING HEAD LINER AND CAUSES LARGE BURN MARKS AND SMOKE (VERY FAINT). REPLACED CABIN LIGHT FIXTURE ASSEMBLY FOR SEAT 10A. OPERATIONAL CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 19,360 hrs · 28,580 cycles

EMERGENCY LIGHT OVER PAX DOOR INOPERATIVE. REPLACED BULB IN EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAP) · airframe 18,864 hrs · 27,844 cycles

FLAP DISAGREEMENT ON RETRACTION. REMOVED AND REPLACED NACELLE FLAP ACTUATOR IAW MM 27-50-00. OPERATIONAL CHECKS GOOD.

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAP) · airframe 18,858 hrs · 27,832 cycles

FLAP DISAGREEMENT ON RETRACTION. REPLACED LEFT NACELLE FLAP ACTUATOR WITH A SERVICEABLE UNIT IAW MM 27-50-00. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN FLOOR) · airframe 17,684 hrs · 25,973 cycles

FORWARD CABIN EMERGENCY EXIT LIGHT INOP. REPLACED FORWARD CABIN EMERGENCY EXIT LIGHT ASSEMBLY WITH SERVICEABLE UNIT. OPS CHECK GOOD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 17,536 hrs · 25,744 cycles

MID SECTION OF EMERGENCY LIGHTS FAILED TO TEST. REPLACED AND SECURED MID CABIN EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 17,471 hrs · 25,644 cycles

CAPTAIN SIDE FCP HAS A RED TRIM WARNING ACCOMPANIED WITH COMPUTER FLAG ON ADI. REPLACED LEFT APC65 WITH SERVICEABLE UNIT. ALL FUNCTIONAL CHECKS FOUND GOOD. P/N: 622-8315-402, S/N ON: 2470, S/N OFF: 1641.

Part: SERVO — MALFUNCTIONED (ELEVATOR) · airframe 16,140 hrs · 23,569 cycles

CAPTAIN'S AND F/O'S YOKE TRIM SWITCHES FAIL TO MOVE TRIM WHEEL. TRIM FAIL APPEARS ON MAP AFTER THE YOKE TRIM SWITCHES ARE PUSHED. ALSO, TRIM ILLUMINATES ON AUTOPILOT PANEL. REPLACED ELEVATOR TRIM SERVO. OPS CHECK GOOD. UPDATE 5/24/03 FAILURE REPEATED. REPLACED TRIM SERVO RELAY K0463. BOTH AUTOPILOT TRIM SWITCHES OPS CHECK GOOD IAW MM 22-10-00. P/N M83536/6-022M.

Part: WIRE HARNESS — SHORTED (MLG) · airframe 15,623 hrs · 22,777 cycles

UPON GEAR RETRACTION, GREEN AND RED -A- SYSTEM NOSE WHEEL LIGHTS STAY ILLUMINATED. FOUND A DOWN HARNESS TO BE GROUNDED OUT. REPLACED A DOWN HARNESS. PERFORMED GEAR OPERATIONAL SWINGS AND NOSE GEAR INDICATION OPS CHECK GOOD.

Part: ACTUATOR — LEAKING (RT NACELLE FLAPS) · airframe 15,511 hrs · 22,606 cycles

ON SHORT FINAL RECEIVED A FLAP DISAGREE MESSAGE ON THE NACELLE FLAPS AFTER SELECTING FLAPS 45 (ABOUT 125 KTS). THEN LOST RT HYD PRESSURE. REMOVED AND REPLACED LEAKING RIGHT NACELLE FLAP ACTUATOR PER EMB MM 27-50-08. GROUND OPS CHECK AND LEAK CHECK COMPLIED WITH. NO DEFECTS NOTED.

Part: RIB — CRACKED (RT WING) · airframe 15,133 hrs · 21,995 cycles

RT INBOARD LEADING EDGE RIB IS CRACKED. CRACKED AREA STOP-DRILLED AND DOUBLER ADDED TO DAMAGED AREA IAW EMB120 SRM 51-10-02.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 15,133 hrs · 21,995 cycles

RIVET HEAD SHEARED OFF BRACKET BETWEEN CAPTAIN'S DV WINDOW AND PASSENGER DOOR, COCKPIT INTERIOR. FOUND BRACKET TO BE CRACKED. NEW BRACKET INSTALLED IAW SRM120 51-10-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 15,133 hrs · 21,995 cycles

FOUND CRACKED ANGLE INSIDE COCKPIT BELOW FLOOR AT FRAME 11, RT SIDE.APPLIED DOUBLER IAW SRM120 51-10-02.

Part: SWITCH — LOOSE (FUEL DOOR) · airframe 13,845 hrs · 19,986 cycles

SERVICE DOOR LIGHT ILLUMINATED PASSING 10,000 FT. RETURNED TO MFR. LIGHT EXTINGUISHED ON SHORT FINAL. FOUND BOTH MICROSWITCHES ON REFUELING DOORS LOOSE. SECURED BOTH MICROSWITCH ASSEMBLIES AS NEEDED. OPS CHECK GOOD AT THIS TIME.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 13,624 hrs · 19,670 cycles

DURING CLIMBOUT, NOTICED NH GAUGE FLUCTUATING RAPIDLY +/- 10 PERCENT. REDUCED POWER AND SELECTED NR 1 EEC TO MANUAL. NH GAUGE STILL FLUCTUATED. ALL OTHER ENGINE PARAMETERS NORMAL. INSTALLED NH SENSOR FOR TROUBLESHOOTING. DURING ENGINE RUNS NH/NL (LT) START FLUCTUATING AT GROUND IDLE. SWAPPED GAUGES. PROBLEM FOLLOWED. INSTALLED SERVICEABLE NH/NL GAUGE (LT). RAN ENGINES. OPS CHECK GOOD. P/N: SEDL-0C29M, S/N ON: 174A, S/N OFF: 180.

Part: WARNING LIGHT — FALSE INDICATION (COCKPIT) · airframe 11,821 hrs · 17,015 cycles

CARGO DOOR LIGHT ILLUMINATED IN FLIGHT AND RETURNED TO FIELD. VISUALLY CHECKED CARGO DOOR UPON ARRIVAL AND FOUND TO BE SECURED. VERIFIED DOOR WARNING WORKS. PERFORMED INSPECTION ON CARGO DOOR LIGHT SWITCHES AND PERFORMED NUMEROUS CYCLES ON CARGO DOOR. COULD NOT DUPLICATE FAILURE. OPS CHECK GOOD.

Part: DAMPER — MALFUNCTIONED (AUTOPILOT) · airframe 11,821 hrs · 17,015 cycles

YAW DAMPER ENGAGED ON TAXI, WILL NOT DISCONNECT. REMOVED AND REPLACED APP65A WITH SERVICEABLE UNIT. OPS CHECK GOOD. P/N: 622-6684-006, S/N ON: 2614, S/N OFF: 344.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 11,799 hrs · 16,983 cycles

ON TAKEOFF ROLL HEARD TRIPLE CHIME AURAL WARNING FOR TRIM. RESET AURAL WARNING UNIT. PERFORMED OPS CHECK OF TRIM SEVERAL TIMES. OPS CHECK NORMAL. COULD NOT DUPLICATE PROBLEM ON GROUND.

Part: INDICATOR — FAILED (COCKPIT) · airframe 11,746 hrs · 16,909 cycles

CAPTAIN HDG 70 DEGREES FROM FO EHSI FAIL AND HDG FLAGS DISPLAYED AS WELL AS COMP FLAG CAPTAIN ADI AND FAIL FLAG FO RMI 2/23/01. RETURNED TO FAT. COULD NOT DUPLICATE COMPLAINT. REPLACED K0395 AND K0397 TO TROUBLESHOOTING. SYSTEM OP CHECKS GOOD IAW MM 34-21-00.

Part: COMPARATOR — FAILED (COCKPIT) · airframe 11,705 hrs · 16,849 cycles

NUMBER ONE EHSI RED HDG FLAG AND HDG FAILURE DURING FLIGHT. RETURNED TO PDX. REPLACED NUMBER ONE AHC85 AND INITIALIZATION PROCEDURE WAS PERFORMED. SYSTEM OPS CHECK GOOD. ALL PANELS SECURE. P/N: 622-6190-204, S/N ON: 1121, S/N OFF: 1059.

Part: RELAY — FAILED (AUTOFEATHER SYS) · airframe 11,341 hrs · 16,359 cycles

WHEN CLEARED FOR TAKEOFF, SET CONDITION LEVERS TO MAXIMUM, AUTO FEATHER AURAL WARNING SOUNDED. ABORTED TAKEOFF. WHEN T/O POWER SET FIRST OFFICER NOTICED RIGHT NP DID NOT SPOOL UP TO 65 PERCENT. REPLACED REVERSION (EEC) RELAYS K0059, K0060 PER WM 20-00-00, AND PERFORMED ENGINE TRIM PER PWC MM 72-00-00. REPLACED K0161 AUTO FEATHER SYSTEM ARM RELAY AS A PRECAUTION PER WM 20-00-00. RAN ENGINES AT TAKEOFF POWER WITH MATCHED POWER LEVERS, ALL PARAMETERS AND INDICATIONS CHECKED NORMAL. PERFORMED AUTO FEATHER CHECK PER MM 61-10-00, ALL CHECKS GOOD.

Part: FASTENER — LOOSE (FUEL DOOR) · airframe 10,902 hrs · 15,718 cycles

ON TAKEOFF, RED ''DOOR'' MAP WITH SERVICE DOOR ON OVERHEAD PANEL. ONE OF THE FUEL DOOR FASTENERS WAS LOOSE. RESECURED THE FASTENER AND FUEL DOOR, OPS CHECK GOOD.

Part: WARNING LIGHT — ILLUMINATED (FUEL DOOR) · airframe 10,360 hrs · 14,937 cycles

SERVICE DOOR LIGHT CAME ON DURING CLIMBOUT. RETURNED TO SBA. CHECKED FUEL DOOR LATCHES. OPS CHECKS GOOD.

Part: FUEL FILTER — FAILED (RT ENGINE) · airframe 10,173 hrs · 14,666 cycles

DURING CLIMBOUT (APPROXIMATELY 11,000 FEET) FUEL LIGHT ON MAP ILLUMINATED WITH FILTER ON NUMBER TWO ENGINE. RETURNED TO LAX. REMOVED AND REPLACED RIGHT ENGINE FUEL FILTERS. RAN ENGINE. OPS CHECKS AND LEAK CHECKS GOOD.

Part: CONTROL BOX — MALFUNCTIONED (MLG)

RED B LANDING GEAR LIGHTS WOULD NOT EXTINGUISH WHEN LANDING GEAR HANDLE RAISED IN UP POSTION (CYCLED GEAR TWICE). RETURNED TO PDX. REPLACED LANDING GEAR CONTROL BOX, OPS CHECK GOOD IAW MM CH 22. (P/N 12038544501), (S/N 120009R) ON, (S/N 120085) OFF.

Part: DOOR — NOT LATCHED (RT EMER EXIT)

UNABLE TO PRESSURIZE CABIN. RETURNED TO SLC. LATCHED RIGHT FOWARD EMERGENCY EXIT. EXIT NOW SECURE. NO OTHER PRESSURIZATION PROBLEMS.

Part: AHRS — FAILED (COCKPIT)

TOTAL AHRS FAILURE EHSI, EADI. DIVERTED TO PSP. REPLACED RELAYS K0395, K0397, K0394 AND K0396. TESTED AHRS IAW MM 34-21-00 AND PERFORMED OPERATIONAL TEST OF 70 PERCENT SWITCHING RELAYS, TEST GOOD. BACK UP BATTERY TEST GOOD IAW MM 24-00-00.

Part: CONTROLLER — MALFUNCTIONED (CABIN)

AT 11,400 CABIN ALTITUDE MAP ILLUMINATED. RETURNED TO FAT. CLEANED AND INSPECTED PUMP, SWITCH, MANUAL CONTROLLER AND THE INDICATOR. CLEANED DOOR SEALS AND PNEUMATIC VALVE. NO DEFECTS NOTED. REPLACED AUTO ELECTRIC CONTROLLER.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR)

CARGO DOOR WARNING LIGHT IS ON. RETURNED TO FIELD. MEL 52-70-1. ADJUSTED CARGO DOOR WARNING LIGHT MICRO SWITCH, OPS CHECKS GOOD.

Part: STRAP — CORRODED (LAVATORY)

CENTER CABIN FLOOR BUTT STRAP FRAME 38 AFT (NEAR LAVATORY) HAS CORROSION. REMOVED AND REPLACED CENTER CABIN FLOOR BUTT STRAP AT FRAME 38, IAW SRM 51-40-02.

Part: BOLT — LOOSE (PAX DOOR)

CORROSION AND LOOSENESS IN ATTACH BOLT, LOWER END OF LOWER AFT HANDRAIL SUPPORT ARM. REPLACED HARDWARE, IAW MM 52-10-00.

Part: BOLT — LOOSE (PAX DOOR)

CORROSION AND LOOSENESS IN LOWER ATTACH BOLT LOWER HALF FWD HANDRAIL SUPPORT ARM, CABIN DOOR. REPLACED HARDWARE IAW MM 52-10-00.

Part: CONTROL BOX — FAILED (LANDING GEAR)

AFTER TAKEOFF WITH GEAR UP TAKEOFF WARNING CONTINUED TRIM, FLAPS, AUTO FEATHER. REPLACED GEAR CONTROL BOX, OPS CHECKS GOOD AT THIS TIME.

Part: HANDLE — OUT OF POSITION (GEAR DOORS)

GEAR DOORS WOULD NOT CLOSE AFTER RETRACTION OF LANDING GEAR. RETURNED TO FIELD, CYCLED OPERATION MAINTENANCE HANDLE. DOORS SELECTED TO OPERATION AND ALL CHECKS GOOD.

Part: ACTUATOR — OUT OF ADJUST (RT MLG)

RIGHT MAIN GEAR DOORS WOULD NOT CLOSE, CYCLED SEVERAL TIMES. ADJUSTED RIGHT MAIN LANDING GEAR ACTUATOR HALF TURN IAW MM 32-32-10, OPS CKS GOOD.