N81546

Part: PRINTED CKT BOARD — FAULTY (LANDING GEAR) · airframe 33,380 hrs · 41,902 cycles

FLIGHT: 4067 DUJ/DUJ AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT, AFTER SELECTED UP CIRCUIT BREAKER POPPED. REPLACED PCB A316, OPERATIONAL CHECKS GOOD.

Part: WARNING SWITCH — OUT OF ADJUST (COCKPIT) · airframe 32,479 hrs · 40,050 cycles

FLIGHT: 4069 CLE/DUJ DURING APPROACH LANDING GEAR WARNING HORN ACTIVATES AT 1600 FTLB WHEN RETARDING PROP LEVERS TURBINE SPEED WAS 88.8%. ADJUSTED LEFT AND RIGHT PEDESTAL HORN SWITCHES, TEST FLIGHT SATISFACTORY.

Part: BRACKET — LOOSE (NLG) · airframe 32,465 hrs · 40,026 cycles

FLIGHT: 4037 BIM/FLL PILOT REPORTED AFTER EXTENDING GEAR ON FINAL HEARD REPETITIVE VIBRATING/BANGING NOISE COMING FROM NOSE WHEEL AREA. RE-SECURED BRACKET FOR ANTISKID COVER IN NOSE WHEEL WELL. LANDING GEAR OPERATIONAL CHECK NORMAL.

Part: UNKNOWN — ODOR (CABIN) · airframe 32,392 hrs · 39,922 cycles

PILOT REPORTED STRONG BURNING RUBBER ODOR IN FLIGHT, WENT AWAY WITH RIGHT BLEED AIR INSTRUMENT AND ENVIRONMENTAL OFF. PERFORMED VISUAL INSPECTION OF LEFT AND RIGHT BLEED AIR SYSTEMS AND PERFORMED OPERATIONAL CHECK OF BLEED AIR SYSTEMS. OPS CHECKED GOOD, NO DEFECTS FOUND.

Part: LINKAGE — DEFECTIVE (NLG DOOR) · airframe 32,161 hrs · 39,586 cycles

FLIGHT: 3982 PNS/TPA PILOT REPORTED LOUD RATTLING NOISE COMING FROM WHEEL WELL WITH WITH GEAR EXTENDED. REPLACED NOSE GEAR DOOR RIGHT UPPER BRACKET BUSHING AND RIGHT DOOR LINKAGE AND ROD ENDS.

Part: CAM — OBSTRUCTED (CABIN DOOR) · airframe 32,161 hrs · 39,586 cycles

FLIGHT: 3982 PNS/TPA PILOT REPORTED CABIN DOOR DIFFICULT TO OPEN FROM INSIDE AIRCRAFT WHEN HANDLE IS LIFTED LOUD CLICKING NOISE IS HEARD. CLEANED EXCESSIVE GREASE FROM TWO UPPER DOOR CAMS OPERATIONAL CHECK NORMAL.

Part: SKIN — CORRODED (FUSELAGE) · airframe 31,836 hrs · 39,073 cycles

DURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED MINOR CORROSION APPROXIMATELY FS 250 AT STRINGER 15L. REMOVED DAMAGED FUSELAGE SKIN AND INSTALLED INSERTION AND EXTERNAL DOUBLER REPAIRS.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 31,836 hrs · 39,073 cycles

DURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED CORROSION APPROXIMATELY FS 250 AT STRINGER 15R. REMOVED DAMAGED STRINGER AND INSTALLED STRINGER SPLICE REPAIR INSERTION AND EXTERNAL DOUBLER REPAIRS.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 31,836 hrs · 39,073 cycles

DURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED BULKHEAD CRACKED FS 163 STRINGER 9R STARTING AT STRINGER CLEARANCE RADIUS 1.5 INCHES. STOPPPED DRILLED CRACKED AND INSTALLED DOUBLER REPAIR.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,836 hrs · 39,073 cycles

DURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED LEFT CLOSING ANGLE CRACKED APPROXIMATELY 2.0 INCHES AT FS 288. STOPPPED DRILLED CRACKED AND INSTALLED REPAIR ANGLE.

Part: DOOR FRAME — CRACKED (CARGO BAY) · airframe 31,836 hrs · 39,073 cycles

DURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED AFT CARGO DOOR FRAME AT FS 510 APPROXIMATELY LEFT STRINGER 4 CRACKED APPROXIMATELY 2.0 INCHES. REMOVED DAMAGED SECTION OF FRAME AND INSTALLED 45 INCH SECTION OF FRAME SPLICE REPAIR.

Part: DOOR — BINDING (EMERGENCY EXIT) · airframe 31,621 hrs · 38,752 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED LT EMERGENCY EXIT WILL NOT OPEN FROM THE INSIDE. CLEANED AND LUBRICATED LT EMERGENCY EXIT, OPS CHECK GOOD.

Part: TRUSS — CRACKED (ENGINE MOUNT) · airframe 31,456 hrs · 38,542 cycles

DURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS COWLING ATTACH BRACKETS WELD AREA CRACKS AND FORWARD LOWER ENGINE MOUNT ATTACH POINTS WELD AREA CRACKS. PERFORMED WELD REPAIR TO ENGINE TRUSS ATTACH BRACKETS WELD AREAS AND FORWARD LOWER ENGINE MOUNT ATTACH POINTS WELD AREAS.

Part: TRUSS — CRACKED (ENGINE MOUNT) · airframe 31,456 hrs · 38,542 cycles

DURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS COWLING ATTACH BRACKETS WELD AREA CRACKS AND RIGHT FORWARD LOWER ENGINE MOUNT ATTACH POINT WELD AREA CRACK. PERFORMED WELD REPAIR TO ENGINE TRUSS ATTACH BRACKETS WELD AREAS AND RIGHT FORWARD LOWER ENGINE MOUNT ATTACH POINTS WELD AREA.

Part: HANDLE — BINDING (EMERGENCY EXIT) · airframe 30,832 hrs · 37,803 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED LT EMERGENCY EXIT HANDLE HARD TO OPEN. LUBRICATED LT EMERGENCY EXIT HANDLE.

Part: DOOR — LACK OF LUBE (EMERGENCY EXIT) · airframe 30,140 hrs · 37,020 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED LT EMERGENCY EXIT HARD TO OPEN. LUBRICATED LT EMERGENCY EXIT DOOR OPS CHECKS NORMAL.

Part: HINGE — CORRODED (RT ELEVATOR) · airframe 29,176 hrs · 35,879 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED SURFACE CORROSION AT RT ELEVATOR OTBD HINGE. REPLACED RT ELEVATOR OTBD HINGE.

Part: TORQUE TUBE — CORRODED (RT ELEVATOR) · airframe 29,176 hrs · 35,879 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED RT ELEVATOR TORQUE TUBE EXFOLIATED. REPLACED RT ELEVATOR TORQUE TUBE.

Part: DOOR FRAME — CRACKED (BS 150) · airframe 29,025 hrs · 35,701 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED AIRSTAIR DOOR FUSELAGE FRAME CRACKS AT FS 150.60 WL 103.50 AND WL 106.00. REMOVED DAMAGED SECTION OF DOOR FRAME AND INSTALLED FRAME INSERT ANGLE REPAIR.

Part: CABLE ASSY — FRAYED (AIRSTAIR) · airframe 29,025 hrs · 35,701 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED AIRSTAIR DOOR UPPER AFT AND LOWER FWD DOOR CABLES NEED REPLACED. REPLACED UPPER AFT AND LOWER FWD DOOR CABLES. ACFT DOWN FOR STRUCTURAL INSP.

Part: HANDLE — BINDING (EMERGENCY EXIT) · airframe 29,025 hrs · 35,701 cycles

DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT AFT EMERGENCY EXIT INSIDE HANDLE BINDS AND HARD TO REACH FULL TRAVEL TO OPEN. LUBRICATED EMERGENCY EXIT INNER HANDLE, CORE OPS CHECK NORMAL. ACFT DOWN FOR STRUCTURAL INSP.

Part: DOOR — BINDING (EMERGENCY EXIT) · airframe 29,025 hrs · 35,701 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED RT AFT EMERGENCY EXIT INSIDE HANDLE BINDS AND HARD TO REACH FULL TRAVEL TO OPEN. LUBRICATED EMERGENCY EXIT INNER HANDLE CORE OPS CHECK NORMAL. ACFT DOWN FOR STRUCTURAL INSP.

Part: DOOR — INOPERATIVE (AIRSTAIR) · airframe 28,883 hrs · 35,541 cycles

PILOT REPORTED AIRSTAIR DOOR WILL NOT OPEN FROM INSIDE. PERFORMED OPS CHECK ON AIRSTAIR DOOR NO DEFECTS NOTED.

Part: WIRE — CHAFED (ZONE 400) · airframe 28,845 hrs · 35,491 cycles

AFTER EXECUTING BEFORE LANDING CHECKLIST, LANDING GEAR FAILED TO EXTEND. MANUALLY EXTENDED LANDING GEAR AND LANDED WITHOUT FURTHER INCIDENT. REPAIRED CHAFED WIRE G16C22 AT RT TOP NACELLE.

Part: DOOR — STIFF (EMERGECNY EXIT) · airframe 28,807 hrs · 35,440 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED RT AFT EMERGENCY EXIT HARD TO OPEN. INSPECTED CLEANED AND LUBED RT AFT EMERGENCY EXIT. OPS CHECK GOOD.

Part: DOOR — OBSTRUCTED (EMERGENCY EXIT) · airframe 28,657 hrs · 35,253 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED RT AFT EMERGENCY EXIT DOOR HARD TO OPEN. ADJUSTED RT AFT EMERGENCY EXIT DOOR UPHOLSTRY, DOOR OPERATES SMOOTHLY.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 28,616 hrs · 35,202 cycles

PILOT REPORTED STRONG FUEL ODOR IN COCKPIT. SEALED AUK FUEL TANK NO LEAKS NOTED.

Part: SKIN — DAMAGED (RT WING) · airframe 28,555 hrs · 35,131 cycles

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED FASTENERS PULLING THROUGH THE RIGHT UPPER WING SKIN BETWEEN W.S 124.25 AND 143.00. REMOVED LEAKING RIVETS, FABRICATED AND INSTALLED AN EXTERNAL DOUBLER REPAIR.

Part: SKIN — CORRODED (RT WING) · airframe 28,148 hrs · 34,699 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED RT WING TOP T/E SKIN HAS SURFACE CORROSION. DURING CLEANING DISCOVERED CORROSION, RWS 159.51 THRU 171.29 AND RWS 183.07 THRU 196.06 REMOVED CORROSION AND INSTALLED EXTERNAL DOUBLER REPAIRS.

Part: CABLE — BROKEN (PAX DOOR) · airframe 27,615 hrs · 34,083 cycles

PILOT REPORTED CABIN DOOR WILL NOT OPEN. REPLACED FWD LOWER DOOR CABLE, OPS CHECK OK.

Part: PRINTED CKT BOARD — DEFECTIVE (LANDING GEAR) · airframe 26,583 hrs · 32,974 cycles

FLIGHT 5202 FLL/FLL - AFTER TAKEOFF LANDING GEAR SELECTED UP DISCOVERED LANDING GEAR CIRCIUT BREAKER POPPED. REPLACED TIME DELAY RELAY PCB. OPERATIONAL CHECK NORMAL.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 26,582 hrs · 32,973 cycles

AT SCHEDULED INSPECTION DISCOVERED A .5 INCH CRACK RIGHT AIRCRAFT FUSELAGE BELLY RBL 29.06. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER BEECH STRUCTURAL REPAIR MANUAL 53-90-18.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 26,582 hrs · 32,973 cycles

AT SCHEDULED INSPECTION DISCOVERED A .5 INCH CRACK LEFT AIRCRAFT FUSELAGE BELLY LBL 29.06. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER BEECH STRUCTURAL REPAIR MANUAL 53-90-18.

Part: KEELBEAM — CRACKED (LT NACELLE) · airframe 26,582 hrs · 32,973 cycles

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT NACELLE INBOARD KEEL HAS .75 INCH CRACK FORWARD AND ABOVE LANDING GEAR BOLT. REMOVED AND REPLACED INBOARD KEEL.

Part: SKIN — CORRODED (LT WING) · airframe 26,582 hrs · 32,973 cycles

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT OUTBOARD WING UPPER SKIN TRAILING EDGE HAD CORROSION AND DEBOND BETWEEN WS 121 THROUGH 194.85. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED AN EXTERNAL REPAIR DOUBLER.

Part: HINGE BRACKET — CORRODED (RUDDER) · airframe 26,091 hrs · 32,405 cycles

DURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED UPPER RUDDER HINGE BRACKET SHOW SIGNS OF EXFOLIATION. REPLACED UPPER RUDDER HINGE BRACKET.

Part: HINGE BRACKET — CORRODED (RUDDER) · airframe 26,091 hrs · 32,405 cycles

DURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED LWR RUDDER HINGE BRACKET SHOW SIGNS OF EXFOLIATION. REPLACED LOWER RUDDER HINGE BRACKET.

Part: REGULATOR — MALFUNCTIONED (BLEED AIR SYS) · airframe 26,047 hrs · 32,349 cycles

FLIGHT 9205, AFTER TAKEOFF, STRONG SCENT OF BURNED RUBBER IN COCKPIT. (NO SMOKE) THE PNEUMATIC PRESSURE GAUGE PEGGED OVER THE RED LINE AND VACUUM PRESSURE GAUGE PEGGED AT ZERO, WHEN TRYING TO ADD HEAT, USE DEICE BOOTS ON ANY OTHER ENVIRONMENTAL PRESSURE FUNCTION, SMELL GETS SIGNIFICANTLY WORSE. REPLACED PRESSURE REGULATOR AND TEST RAN ENGINES. PERFORMED BLEED AIR SYSTEM OPERATIONAL CHECK SYS, NO SMELL DETECTED.

Part: ARM — BROKEN (EMERGENCY EXIT) · airframe 25,596 hrs · 31,846 cycles

DURING SCHEDULED ROUTINE MAINT, DISCOVERED THE LT EMERGENCY EXIT ARM ASSY BROKEN. REPLACED LT EMERGENCY EXIT ARM ASSY.

Part: UPLOCK SWITCH — DAMAGED (LT MLG) · airframe 25,260 hrs · 31,464 cycles

AFTER TAKEOFF LANDING GEAR RETRACTION GEAR HANDLE LIGHT REMAIN ILLUMINATED. REPLACED LT MAIN LANDING GEAR UPLOCK SWITCH.

Part: ACTUATOR — MALFUNCTIONED (LT MLG) · airframe 24,754 hrs · 30,862 cycles

DURING FLIGHT LANDING GEAR INTRANSIT LIGHT ILLUMINATED. REPLACED LT MLG ACTUATOR. OPERATIONAL CHECK NORMAL.

Part: UPLOCK SWITCH — OUT OF ADJUST (MLG) · airframe 24,616 hrs · 30,704 cycles

FLIGHT:9197 TPA/FLL - DURING FLIGHT, LANDING GEAR HANDLE LIGHT FLICKERS ON AND OFF. ADJUSTED LEFT MAIN LANDING GEAR UPLOCK SWITCH OPERATIONAL CHECK NORMAL.

Part: UPLOCK SWITCH — OUT OF ADJUST (MLG) · airframe 24,496 hrs · 30,570 cycles

FLIGHT: 5404, DURING FLIGHT LANDING GEAR HANDLE LIGHT ILLUMINATED. INSPECTED LANDING GEAR SYSTEM RIGGED LT LANDING GEAR UPLOCK SWITCH. LANDING GEAR OPERATIONAL CHECK GOOD.

Part: SWITCH — OUT OF ADJUST (MLG HANDLE) · airframe 24,474 hrs · 30,545 cycles

FLIGHT: 9234, AFTER TAKEOFF, LANDING GEAR HANDLE LIGHT REMAINS ILLUMINATED IN THE UP POSITION. ADJUSTED RT MAIN LANDING GEAR UP POSITION SWITCH OPERATIONAL CHECK NORMAL.

Part: MOTOR — FAILED (MLG) · airframe 23,525 hrs · 29,450 cycles

AFTER TAKEOFF LANDING GEAR CIRCUIT BREAKER POPPED GEAR UNSAFE LIGHT ILLUMINATED NOSE GEAR RETRACTED BUT BOTH MAIN GEARS STAYED DOWN. CONTINUED, MANUALLY EXTENDED NOSE GEAR LANDED WITHOUT INCIDENT. REPLACED THE LANDING GEAR DC MOTOR OPERATIONAL CHECK NORMAL.

Part: STRUT — LOW (NLG)

FLIGHT: 9214 MIA/TPA AFTER LANDING DISCOVERED NOSE WHEEL WELL DAMAGED DURING GEAR EXTENSION. SERVICED NOSE LANDING GEAR STRUT LANDING GEAR EXTENSION AND RETRACTION, OPERATIONAL CHECK NORMAL.

Part: HINGE BRACKET — CORRODED (LEFT ELEVATOR)

AT SCHEDULED ROUTINE MAINTENANCE LEFT OUTBOARD ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION.-------REPLACED LEFT OUTBOARD ELEVATOR HINGE BRACKET.

Part: HINGE BRACKET — CORRODED (RIGHT ELEVATOR)

AT SCHEDULED ROUTINE MAINTENANCE RIGHT OUTBOARD ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION.--------REPLACED RIGHT OUTBOARD ELEVATOR HINGE BRACKET.

Part: SKIN — DENTED (FUSELAGE)

DURING ROUTINE SCHEDULED MAINTENANCE FOUND LEFT FUSELAGE FORWARD OF CARGO DOOR HAS DENTED AREAS. REPAIRED DENTED AREAS BY INSTALLING INSERTION PATCH AND INTERIOR REINFORCEMENT DOUBLER IN ACCORDANCE WITH 1900 STRUCTURAL REPAIR MANUAL.

Part: HINGE BRACKET — CORRODED (LT ELEVATOR)

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

Part: HINGE BRACKET — CORRODED (RT ELEVATOR)

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

Part: BRACKET — CORRODED (RT ELEVATOR)

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

Part: BRAKE — MALFUNCTIONED (RT MLG)

RT BRAKES INEFFECTIVE. REMOVED AND REPLACED NR THREE AND NR 4 BRAKE ASSEMBLIES OPERATIONAL CHECK NORMAL.

Part: COMPUTER — SHORTED (FLT DIRECTOR)

FLT 9215 - TPA/MIA - DURING APPROACH, YAW DAMP/RUDDER BOOST FAIL ANNUNCIATOR ILLUMINATED, FOLLOWED BY LEFT AC BUS ANNUNCIATOR. ELECTRICAL SMELL OF SMOKE OBSERVED IN COCKPIT. REMOVED AND REPLACED FDR COMPUTER. OPERATIONAL CHECK NORMAL. (M)

Part: BOLT — LOOSE (VERTICAL STAB)

(BOLT) AT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM.

Part: FIRE LOOP — DEFECTIVE (NR 2 ENGINE)

RIC - FLT 3056 - THE CREW REPORTED THAT THE NR 2 ENGINE FIRE LOOP LIGHT ILLUMINATED IN FLIGHT. THE AIRCRAFT RETURNED TO RIC WHERE IT LANDED WITHOUT INCIDENT, AND MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FIRE BOTTLE. FLT 4378, WHEN TAKEOFF POWER WAS APPLIED THE RED FIRE T HANDLE LIGHT ILLUMINTED, THE CREW DISCHARGED THE NR 2 FIRE BOTTLE. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FIRE BOTTLE AND THE NR 2 ENGINE FIRE LOOP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: VALVE — FAILED (RT BLEED AIR)

CLE - FLT 3161 - CREW REPORTED THAT THE RIGHT HAND BLEED AIR FAIL LIGHT ILLUMINATED IN-FLIGHT. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND BLEED AIR SHUT OFF VALVE IAW B1900 MM 36-00-02, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (X)

Part: ACTUATOR — INOPERATIVE (NLG STEERING)

CLE - FLT 3099 - CREW REPORTED THAT AFTER LANDING, WHILE TAXIING TO THE GATE THE NOSE WHEEL STEERING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NOSE WHEEL STEERING DISCONNECT ACTUATOR IAW B1900 MM 32-50-01, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: BRUSH BLOCK — CHAFED WIRE (RT PROP)

CLE - FLT 3057 - CREW REPORTED THE RIGHT PROP DE-ICE WOULD NOT TEST FOR FIRST FLIGHT CHECKS IN AUTO OR MANUAL MODES. AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED THE PROP AND REMOVED AND REPLACED A CHAFFED WIRE ON THE BRUSH BLOCK IAW B1900D MM 30-60-00. OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: ACTUATOR — FAILED (LT MLG)

TLH - FLT 2801 - DURING APPROACH TO TLH, LT MLG DOWNLOCK LIGHT DID NOT ILLUMINATE UNTIL APPROXIMATELY 1 MINUTE AFTER NOSE AND RT MLG LIGHTS ILLUMINATED. AIRCRAFT LANDED AT TLH WITHOUT INCIDENT. INSPECTED AND APPROVED FOR FERRY FLIGHT FROM TLH TO IAH IN A GEAR DOWN CONDITION. IAH MAINTENANCE REMOVED AND REPLACED LT MLG ACTUATOR. PERFORMED OPERATION CHECK OF LANDING GEAR SYSTEM, NO DEFECTS NOTED, AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)