N38537

Part: PRESSURE SWITCH — MALFUNCTIONED (FEATHERING SYS) · airframe 32,353 hrs · 39,488 cycles

PILOT REPORTS, ON APPROACH, RT PROPELLER CYCLES IN AND OUT OF AUTOFEATHER. REPLACED RT AUTOFEATHER LOW PRESSURE SWITCH.

Part: RADIO — SHORTED (HF SYSTEM) · airframe 32,254 hrs · 39,325 cycles

NR 2 COMM FAILED ACCOMPANIED BY SMOKE. INSPECTED WIRING BEHIND RADIO PANEL, NO DEFECTS NOTED. REPLACED COMM NR 2 RADIO, RAN UNIT FIFTEEN MINUTES, NO DEFECTS NOTED.

Part: PROPELLER — MALFUNCTIONED · airframe 32,030 hrs · 39,020 cycles

DURING APPROACH RT ENG CYCLED BETWEEN 700 AND 1200 POUNDS OF TORQUE WITH ASSOCIATED RT AUTO FEATHER LIGHT. CHECKED AUTO FEATHER SWITCH SETTINGS AND PERFORMED MULTIPLE AUTOFEATHER TEST OPS CHECK NORMAL.

Part: SPAR CAP — CORRODED (RT WING) · airframe 31,902 hrs · 38,877 cycles

DURING SCHEDULED X RAY INSP DISCOVERED RT WING CORROSION AT LOWER FWD SPAR CAP NEAR FUEL DRAIN. REMOVED CORROSION FROM RIGHT WING LOWER FORWARD SPAR CAP COMPLIED WITH FLOURESCENT INSPECTION ON BLEND OUT AREA NO SIGNS OF CORROSION FOUND,ALL AREAS WITHIN LIMITS.

Part: STRINGER — CORRODED (RT WING) · airframe 31,902 hrs · 38,877 cycles

DURING SCHEDULED X RAY INSP DISCOVERED RT WING CORROSION IN RT COLLECTOR TANK 1ST STRINGER AFT OF SPAR BPTH SIDES OF FLANGE 4 INCHES TO 6 INCHES FROM INBD RIB. REMOVED CORROSION INSTALLED REPAIR STRINGER AND DOUBLER REPAIRS TO FORWARD AND AFT FLANGES.

Part: SPAR CAP — CORRODED (LT WING) · airframe 31,902 hrs · 38,877 cycles

DURING SCHEDULED X-RAY INSP DISCOVERED LT WING CORROSION AT LOWER FWD SPAR CAP NEAR FUEL DRAIN WS 125.5. REMOVED CORROSION FROM LEFT WING AT LOWER FORWARD SPAR CAP NEAR FULE DRAIN WS 125.5 AND INSTALLED AN EXTERNAL DOUBLER REPAIR.

Part: HANDLE — BINDING (EMERGENCY EXIT) · airframe 31,747 hrs · 38,703 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED RT FWD EMERGENCY EXIT HANDLE DIFFICULT TO OPERATE. ADJUSTED UPPER STRIKER PLATES AND LOWER LUGS, OPS CHECK GOOD. ACFT DOWN FOR STRUCTURAL INSP.

Part: SKIN — CHAFED (BS 259-281) · airframe 31,747 hrs · 38,703 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED LT EXTERNAL SKIN CHAFE, APPROX AT FS 259-281 WS 30. REPAIRED LT EXTERNAL SKIN CHAFE INSTALLED EXTERNAL DOUBLER 1.5 X 22 INCHES COVER PATCH.

Part: DOOR FRAME — CRACKED (CARGO DOORWAY) · airframe 31,747 hrs · 38,703 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED UPPER AFT CARGO DOOR FRAME HAS A 2.0 INCH CRACK APPROX AT FS 509.5, STRINGER 14L. REPAIRED CRACKED "L" ANGLE BY REMOVING 47.0 INCHESS OF ANGLE AND INSTALLING INSERTION OF THE SAME MATERIAL AND A 9.5 INCH REINFORCEMENT ANGLE AND 129-440046-23, 129-440046-25 SKIN REPAIRS.

Part: SWITCH — INOPERATIVE (LANDING GEAR) · airframe 31,688 hrs · 38,633 cycles

PILOT REPORTED LANDING GEAR HAD TO BE RETRACTED BY BYPASSING THE "J" HOOK. REPLACED LANDING GEAR SWITCH OPS CHECK SATISFACTORY.

Part: ANNUNCIATOR — INTERMITTENT (MLG) · airframe 31,422 hrs · 38,356 cycles

PILOT REPORTED CTR LANDING GEAR DOWN GREEN LIGHT INTERMITTENT. REPLACED CENTER LANDING GEAR DOWN GREEN LIGHT ANNUNCIATOR. OPS CHECK NORMAL.

Part: TORQUE TUBE — CORRODED (LT ELEVATOR) · airframe 31,246 hrs · 38,168 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED LT ELEVATOR TORQUE TUBE HAS CORROSION. REPLACED LT ELEVATOR TORQUE TUBE.

Part: ALTIMETER — READS LOW · airframe 30,973 hrs · 37,875 cycles

FLIGHT: 9174 AFTER TAKEOFF CAPTAINS ALTIMETER HAD A 300 FT SPLIT AT 11,000 FT AND 240 FT SPLIT ON LANDING. DECLARED AN EMERGENCY RETURNED TO TPA LANDED WITHOUT INCIDENT. REPLACED CAPTAINS ALTIMETER.

Part: ACCESS PANEL — DELAMINATED (LT WING) · airframe 30,916 hrs · 37,807 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED LT WING FUEL ACCESS PANEL 542CB LEAKS. REPAIRED DELAMINATED SKIN AT WING ACCESS PANEL 542CB.

Part: PANEL — DEBONDED (WING) · airframe 30,705 hrs · 37,584 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED LT AND RT INTERNAL DOUBLERS FOR FUEL PANEL 532DB, 532FB, 631DB AND 642FB DEBONDED. REBONDED RING DOUBLERS AT FUEL PANELS 532DB, 532FB, 631DB AND 642FB.

Part: SWITCH — INTERMITTENT (MLG WARNING) · airframe 30,627 hrs · 37,501 cycles

PILOT REPORTED GEAR WARNING SILENCE BUTTON DOES NOT SILENCE THE GEAR WARNING HORN. REPLACED GEAR WARNING SILENCE SWITCH, OPS CHECK GOOD.

Part: WARNING HORN — MALFUNCTIONED (MLG) · airframe 30,585 hrs · 37,454 cycles

PILOT REPORTED GEAR WARNING HORN STILL SOUNDS OCCASIONALLY WITH SILENCE BUTTON DEPRESSED. CLEANED AND RERACKED PCB CONNECTOR P273 OPS CHECK NORMAL.

Part: SKIN — PUNCTURED (RT WING) · airframe 30,230 hrs · 37,074 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED RT STUB WING TOP OF L/E HAS A DENT AND PUNTURED. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR.

Part: LINE — LEAKING (FUEL SYSTEM) · airframe 29,730 hrs · 36,496 cycles

PILOT REPORTED VERY STRONG CHEMICAL ODOR INSIDE PLANE. REPLACED RT ENGINE PRESSURE FUEL LINE, OPS CHECK OK.

Part: INTAKE — CONTAMINATED (RT ENGINE) · airframe 29,729 hrs · 36,495 cycles

PILOT REPORTED CHEMICAL ODOR COMING FROM RT BLEED. FOUND RESIDUAL OIL AT RT ENG INTAKE. CLEANED AREA OF OIL.

Part: INTAKE — CONTAMINATED (RT ENGINE) · airframe 29,729 hrs · 36,495 cycles

PILOT REPORTED CHEMICAL ODOR COMING FROM RT BLEED. FOUND RESIDUAL OIL AT RT ENG INTAKE CLEANED AREA OF OIL. PREVIOUSLY SUBMITTED CORRECTED DATE.

Part: SOCKET — LOOSE (MLG INDICATOR) · airframe 29,501 hrs · 36,272 cycles

PILOT REPORTED UPPER LANDING GEAR WARNING LIGHT INTERMITTENT. SECURED LOOSE BULB AND SOCKET ON THE LANDING GEAR HANDLE.

Part: HORN — CORRODED (TRIM TAB) · airframe 29,241 hrs · 35,995 cycles

DURING SCHEDULED ROUTINE INSPECTION DISCOVERED LT ELEVATOR TRIM TAB HORN EXFOLIATED. REPLACED LT ELEVATOR TRIM TAB.

Part: UNKNOWN — ODOR (CABIN) · airframe 29,178 hrs · 35,919 cycles

UPON ARRIVAL, BURNING ODOR NOTICED IN COCKPIT AND CABIN. INSPECTED BLOWERS AND AVIONICS, RAN BOTH ENGINES WITH BLEEDS ON COULD NOT ODOR BURNING.

Part: COVER — UNSECURE (PAX DOOR) · airframe 29,116 hrs · 35,846 cycles

PILOT REPORTED UNABLE TO LOCK MAIN CABIN DOOR PROPERLY. INSPECTED AND SECURED PLASTIC COVER ON DOOR. OPS CHECK GOOD.

Part: SKIN — CORRODED (RT WING) · airframe 29,062 hrs · 35,789 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED RT UPPER WING SKIN T/E CORROSION AND DEBOND BETWEEN WING STA 136.036 THROUGH 196.06. REMOVED DAMAGED SKIN AND INSTALLED EXTERNAL REPAIR DOUBLER.

Part: SPAR — CORRODED (LT WING) · airframe 29,062 hrs · 35,789 cycles

DURING SCHEDULED INSP DISCOVERED LT WING FWD SPAR AFT FLANGE AREA 3 HAS CORROSION. REMOVED CORROSION AND INSTALLED REPAIR STRAP.

Part: SPAR — CORRODED (LT WING) · airframe 29,062 hrs · 35,789 cycles

DURING SCHEDULE INSP DISCOVERED LT WING FWD FRONT SPAR AREA 2 HAS CORROSION. REMOVED CORROSION AND INSTALLED REPAIR STRAP.

Part: SPAR — CORRODED (LT WING) · airframe 29,062 hrs · 35,789 cycles

DURING SCHEDULED INSP DISCOVERED LT WING COLLECTOR TANK AREA 1 FWD SPAR AFT FLANGE HAS CORROSION. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR STRAP.

Part: STRINGER — CORRODED (LT WING) · airframe 29,062 hrs · 35,789 cycles

DURING SCHEDULED INSP DISCOVERED LT WING COLLECTOR TANK AREA 1 J STRINGER HAS CORROSION.

Part: SKIN — CORRODED (BS 303) · airframe 29,062 hrs · 35,789 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED RT FUSELAGE BELLY EXFOLIATED AT FS 303.25. REMOVED EXFOLIATED SKIN AND INSTALLED FILLER AND DOUBLER REPAIR.

Part: SKIN — CRACKED (BS 310) · airframe 29,062 hrs · 35,789 cycles

DURING SCHEDULED ROUTINE MX 2.25 INCH CRACK ON RT FUSELAGE BELLY AT FS 310.00. INSTALLED FILLER AND DOUBLER REPAIR.

Part: LINE — CRACKED (HYDRAULIC SYS) · airframe 28,892 hrs · 35,619 cycles

PILOT REPORTED LT BRAKE PEDAL GOES TO THE FLOOR. REMOVED AND REPLACED CRACKED HYD BRAKE LINE.

Part: CABLE — BROKEN (DOOR) · airframe 28,891 hrs · 35,618 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED FWD AIRSTAIR DOOR CAMS NOT MOVING. REPLACED FWD LOWER DOOR CABLE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,822 hrs · 35,548 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED LT FUSELAGE BELLY SKIN HAS .75 INCH CRACK AT FS 260.750. STOP DRILLED CRACK AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER.

Part: UNKNOWN — ODOR (CABIN) · airframe 28,708 hrs · 35,424 cycles

FLIGHT: 9180, DURING FLIGHT, STRONG BURNING RUBBER ODOR WITH RT BLEED AIR VALVE OPEN, GOES AWAY WHEN VALVE IS CLOSED, HAPPENS ONLY IN FLIGHT. INSPECTED FUEL LINES ,OIL LINES BYPASS AND THRU VALVE PERFORMED RUN UPS AT 90 PERCENT WITH BLEEDS ON NO DISCREPANCY FOUND. TEST FLIGHT SATISFACTORY. SUSPECT RESIDUAL ODOR FROM PREVIOUS BURNING ODOR ITEM.

Part: DISPLAY — INTERMITTENT (EADI) · airframe 28,706 hrs · 35,421 cycles

DURING FLIGHT, CAPTAIN`S EADI FLICKERED A FEW TIMES, DISPLAY THEN SHRUNK FOLLOWED BY STRONG BURNING ODOR. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. REPAIRED BROKEN WIRE AT EFIS SCREEN COOLING FAN. OPS CHECK NORMAL.

Part: HINGE BRACKET — CORRODED (RT ELEVATOR) · airframe 28,186 hrs · 34,891 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED RT ELEVATOR OTBD HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR OTBD HINGE BRACKET.

Part: ACTUATOR — BYPASSING (LT MLG) · airframe 27,842 hrs · 34,550 cycles

FLIGHT NR 9191 PNS/TPA DURING FLIGHT LANDING GEAR RELAY CIRCUIT BREAKER POPPED. REPLACED LT MLG ACTUATOR. OPS CHECK NORMAL.

Part: DOOR — MALFUNCTIONED (CABIN DOOR) · airframe 27,459 hrs · 34,173 cycles

FLIGHT 9154 - MCO/MIA - PILOT REPORTED CHECK FORWARD CABIN DOOR FOR PROPER OPERATION APPEARS TO JAM. INSPECTED FORWARD CABIN DOOR. NO DEFECTS NOTED. OPERATIONAL CHECK NORMAL.

Part: HINGE BRACKET — CORRODED (RT ELEVATOR) · airframe 26,008 hrs · 32,615 cycles

DURING SCHEDULED ROUTINE MAINT, DISCOVERED RT ELEVATOR CTR HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR CTR HINGE BRACKET.

Part: HINGE BRACKET — CORRODED (LT ELEVATOR) · airframe 26,008 hrs · 32,615 cycles

DURING SCHEDULED ROUTINE MAINT DISCOVERED LT CTR ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED LT ELEVATOR CENTER HINGE BRACKET.

Part: HINGE BRACKET — CORRODED (LT ELEVATOR) · airframe 26,008 hrs · 32,615 cycles

DURING SCHEDULED ROUTINE MAINT, DISCOVERED LT ELEVATOR OB HINGE BRACKET EXFOLIATED. REPLACED LT ELEVATOR OB HINGE BRACKET.

Part: LATCH — BROKEN (EMERGENCY EXIT) · airframe 25,929 hrs · 32,515 cycles

DURING SCHEDULED ROUTINE MAINT, DISCOVERED RT AFT EMERGENCY EXIT DOOR TOP CAM BROKEN. REPLACED EMERGENCY EXIT ARM LATCH ASSY.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 25,641 hrs · 32,190 cycles

DURING SCHEDULED ROUTINE MX, DISCOVERED EXFOLIATION AT LOWER FUSELAGE SKIN BETWEEN FS 288.00 AND FS 305.00. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED AN EXTERNAL DOUBLER REPAIR.

Part: BRACKET — CORRODED (RUDDER) · airframe 25,044 hrs · 31,486 cycles

AT SCHEDULED INSPECTION DISCOVERED LOWER RUDDER ATTACH BRACKET EXFOLIATED. REPLACED LOWER RUDDER BRACKET.

Part: BRACKET — CORRODED (RUDDER) · airframe 25,044 hrs · 31,486 cycles

AT SCHEDULED INSPECTION DISCOVERED UPPER RUDDER ATTACH BRACKET EXFOLIATED. REPLACED UPPER RUDDER BRACKET.

Part: WARNING HORN — MALFUNCTIONED (MLG) · airframe 24,682 hrs · 31,062 cycles

FLIGHT: 9259 DURING APPROACH LANDING GEAR WARNING HORN SOUNDS WHEN POWER IS PULLED BACK, WHILE SILENCING THE HORN SILENCE BUTTON NOT WORKING. PERFORMED LANDING GEAR OPERATIONAL CHECK NO DEFECTS NOTED.

Part: LANDING GEAR — MALFUNCTIONED · airframe 23,387 hrs · 29,576 cycles

FLIGHT: 9220 PBI/TPA AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. DIVERTED AND LANDED WITHOUT INCIDENT. LANDING GEAR OPERATIONAL CHECK NORMAL COULD NOT DUPLICATE.

Part: HANDLE — MALFUNCTIONED (MLG) · airframe 23,391 hrs · 29,584 cycles

FLIGHT: 5402 FLL/FLL AFTER TAKEOFF LANDING GEAR DID NOT RETRACT ON FIRST ATTEMPT RECYCLED HANDLE THEN THE GEAR RETRACTED. RETURNED TO FLL LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR HANDLE SWITCH ASSEMBLY. LANDING GEAR OPERATIONAL, CHECK NORMAL. TEST FLIGHT SATISFACTORY.

Part: SKIN — DAMAGED (BS 523-531)

FLIGHT 9196 GGT/FLL DURING PREFLIGHT, FOUND AIRCRAFT DAMAGE AT LEFT FUSELAGE AFT OF CARGO DOOR FUSELAGE STATION 523.5 TO 531.0 AT STRINGER 10L. REPAIRED DAMAGE BY INSTALLING EXTERNAL REINFORCEMENT DOUBLER PER BEECH STRUCTURAL REPAIR MANUAL 51-70-06.

Part: BRACKET — CORRODED (LT ELEVATOR)

AT SCHEDULED ROUTINE MAINTENANCE, LEFT OUTBOARD ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LEFT OUTBOARD ELEVATOR HINGE BRACKET. (M)

Part: BRACKET — CORRODED (RT ELEVATOR)

AT SCHEDULED ROUTINE MAINTNANCE, RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT OB ELEVATOR HINGE BRACKET.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING)

DURING TAKE OFF STALL WARNING WENT OFF. REMOVED AND REPLACED STALL WARNING COMPUTER, OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY.

Part: NOZZLE — CLOGGED (LT WING)

FLT 9177 - EYW - DURING TAXI PASSENGER IN SEAT 2A REPORTED HE SAW SMOKE AT HIS FEET AND SMELLED BURNING ODOR. INSPECTED AIRCRAFT AND NO TRACE OF BURNING SMELL WAS DETECTED WITH AIRCRAFT AT HIGH POWER. RAN WITH ALL ENVIRONMENTAL SYSTEMS ON. ONLY CONDENSATION OBSERVED. REMOVED AND REPLACED FOG NOZZLE. OPS CHECK NORMAL. (M)

Part: SWITCH — FAILED (RT MLG)

AZO - FLT 3010 - AFTER TAKEOFF FROM AZO, LANDING GEAR WOULD NOT RETRACT. RETURNED TO AZO AND LANDED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED SEVERAL UP AND DOWN CYCLES WITHOUT FAILURE. APPLIED REFRIGERANT TO RIGHT LANDING GEAR SQUAT SWITCH AND THE GEAR DID NOT RETRACT. REMOVED AND REPLACED THE RIGHT SQUAT SWITCH IAW BEECH 1900D MM CHAP 32-60-05. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: MLG — MALFUNCTIONED (FUSELAGE)

AZO - FLT 3010 - AFTER TAKEOFF FROM AZO, LANDING GEAR WOULD NOT RETRACT. RETURNED TO AZO AND LANDED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED SEVERAL UP AND DOWN CYCLES WITHOUT FAILURE, SIMULATING AIRLOAD AND VIBRATION ON WIRING. SYSTEM OPS CHECKED GOOD IAW BEECH 1900D MM CHAP 32-30-00. AIRCRAFT RETURNED TO SERVICE. (X)

Part: MLG — MALFUNCTIONED (FUSELAGE)

CLE - FLT 3027 - AFTER TAKEOFF FROM PIT, LANDING GEAR FAILED TO RETRACT INITIALLY. AFTER 30-60 SECONDS, GEAR CAME UP. CONTINUED ON TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE CYCLED GEAR SEVERAL TIMES IAW BEECH 1900D MM CHAP 32-30-00. SYSTEM OPS CHECKED GOOD. NO DEFECTS FOUND. AIRCRAFT RETURNED TO SERVICE. (X)

Part: SWITCH — DIRTY (LANDING GEAR)

MBS-CLE - FLT 3240 - THE CREW REPORTED THE RIGHT GEAR LIGHT 'R AND H' ARE INTERMITTENT. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED THE PRESS/RESET PUSHBUTTON, CLEANED ALL THE SWITCHES AND INSPECTED THE WIRING HARNESSES, AND PERFORMED OPS CHECK IAW B1900D MM32-30-00, NO DEFECTS WERE NOTED. THE AIRCRAFT WS RELEASED TO SERVICE. (M)

Part: DUCT — LOOSE (NR 1 ENGINE)

CLE - FLT 3129 - THE CREW REPORTED THE LEFT FIRE T-HANDLE ILLUMINATED DURING TAXI TO THE RUNWAY, THE LIGHE EXTINGUISHED AFTER PULLING T-HANDLE. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE RESECURED THE NR 1 ENGINE RIGHT INLET DE-ICE DUCT TO THE EXHAUST STACK IAW B1900 MM 78-00-00 AND PERFORMED OPERATIONAL CHECK OF THE FIRE DETECTION SYSTEM IAW B1900 MM 26-00-00, NO DEFECTS NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: SWITCH — OUT OF ADJUST (COCKPIT)

CLE - FLT 4399 - CREW REPORTED THAT THE AUTO-FEATHER DISABLED AT 700 FEET WITH ENGINES AT FULL POWER AND IT FAILED TO RE-ARM. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE AUTOFEATHER POWER SWITCHES IAW B1900 MM 61-21-02, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: TRANSDUCER — FAILED (LT WING)

CLE - FLT 3151 - CREW REPORTED THAT THE STALL WARNING CAME ON AT TAKEOFF AND REMAINED ON. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLAFED THE STALL WARNING COMPUTER AND LIFT TRANSDUCER. THE OPERTIONAL CHECKS WERE UNSUCCESSFUL. MAINTENANCE REWIRED THE LIFT TRANSDUCER IAW B1900D MM 27-32-01. OPERATIONAL CHECK WAS GOOD, CALIBRATION OF SYSTEM WAS ACCOMPLISHED IAW B1900D MM 27-31-00. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: START/GEN — FAILED (RT ENG)

FLT 3190 - CREW REPORTED THAT ON ATTEMPTED ENG START, THE RT STARTER/GEN CONTINUED TO RUN WITH THE ENG SHUT DOWN AND THE STARTER SW OFF. THE CREW RECEIVED A FIRE IND AND ACTIVATED THE FIRE EXTINGUISHER. MX INSPECTED THE A/C AND REMOVED AND REPLACED THE RIGHT STARTER/GEN IAW B1900D MM 24-30-01, THE RIGHT ENG POWER SUPPLY AND THE BUS TIE CONTROL PC BOARD WERE ALSO REPLACED IAW B1900D MM 24-30-00. THE RIGHT FIRE BOTTLE WAS REPLACED IAW B1900 MM 24-30-00. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: ELEVATOR TRIM — FROZE UP (EMPENNAGE)

IAH - FLT NR 2805 - DURING CRUISE, THE ELEVATOR TRIM FROZE AT ALTITUDE. MAINTENACNE CLEANED AND LUBED TRIM TAB HINGES AND LUBED BOTH ELEVATOR TRIM TAB ACTUATORS, AND THE AIRCRFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: LIMITER — BLOWN (LANDING GEAR)

CLE - PLANE DEPARTED. UPON TRYING TO RETRACT GEAR, RECEIVED NO INTRANSIT LIGHTS INDICATION OF MOTOR OPERATION. PILOTS THEN TURNED BACK AND LANDED AT CLE. FLT 2403 DEPARTING CLE, REMOVED AND REPLACED BLOWN CURRENT LIMITER.