N17541

Part: HANDLE — LACK OF LUBE (EMERGENCY EXIT) · airframe 32,257 hrs · 37,483 cycles

REPORT: DURING SCHEDULED ROUTINE C-2 INSPECTION DISCOVERED RIGHT FORWARD EMERGENCY EXIT DOOR OUTSIDE HANDLE STIFF (HARD TO OPEN. LUBRICATED RIGHT FORWARD EMERGENCY EXIT DOOR OUTSIDE HANDLE.

Part: HANDLE — LACK OF LUBE (EMERGENCY EXIT) · airframe 32,057 hrs · 37,264 cycles

DURING SCHEDULED ROUTINE C-1 INSPECTION DISCOVERED LEFT EMERGECNY EXIT OUTER HANDLE WILL NOT SPRING OPEN. LUBRICATED LEFT EMERGENCY EXIT OUTER HANDLE. OUTER HANDLE OPEN AND CLOSED NORMALLY.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,568 hrs · 36,709 cycles

REPORT: DURING SCHEDULED ROUTINE INSPECTION DISCOVERED AIRSTAIR DOOR LOWER COUNTER BALANCE BRACKET ATTACH POINT SKIN CRACK. REMOVED DAMAGED AREA AND INSTALLED REPAIR FILLER AND DOUBLER REPAIR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,568 hrs · 36,709 cycles

REPORT: DURING SCHEDULED ROUTINE INSPECTION DISCOVERED AIRSTAIR DOOR LOWER COUNTER BALANCE BRACKET ATTACH POINT SKIN CRACK. REMOVED DAMAGED AREA AND INSTALLED REPAIR FILLER AND DOUBLER REPAIR.

Part: RELAY — SHORTED (LANDING GEAR) · airframe 31,461 hrs · 36,583 cycles

FLIGHT 9257 EYW/FLL PILOT REPORTED LANDING GEAR RELAY POPPED WHEN EXTENDING GEAR. REPLACED LANDING GEAR RELAY OPERATIONAL CHECK OK.

Part: SWITCH — DEFECTIVE (WARNING HORN) · airframe 31,195 hrs · 36,280 cycles

PILOT REPORTED ON GEAR RETRACTION LANDING GEAR HORN SOUNDED AND STAYED RED UNTIL LANDING GEAR WAS EXTENDED AGAIN. REPLACED LANDING GEAR WARNING HORN SWITCH.

Part: ANNUNCIATOR — NO INDICATION · airframe 30,825 hrs · 35,826 cycles

PILOT REPORTED WITH N1 AT 95 PERCENT "AFX DISABLE" ANNUNCIATOR WAS ILLUMINATED AND LT AFX WAS NOT ILLUMINATED. RERACKED ANNUNCIATOR FAULT DETECTION PCB AUTOFEATHER TEST OPS CHECK GOOD.

Part: INDICATION SYS — INOPERATIVE (MLG) · airframe 30,818 hrs · 35,820 cycles

FLIGHT: 9131 TPA/TLH PILOT REPORTED DURING APPROACH NO GEAR SAFE INDICATION AND LANDING GEAR INDICATOR CIRCUIT BREAKER POPPED. RETURNED TO TPA LANDED WITHOUT INCIDENT. INSPECTED PC BOARD AND CONNECTORS PERFORMED LANDING GEAR SWING FIVE TIMES. VISUALLY INSPECTED ALL DOWNLOCK SWITCHES NO DISCREPANCIES NOTED. CLEANED WATER IN BELLY OF AIRCRAFT UNDER PC BOARDS OPERATIONAL CHECKED GOOD.

Part: BRACKET — CRACKED (COWLING) · airframe 30,493 hrs · 35,426 cycles

DURING MAGNETIC PARTICLE INSP, DISCOVERED ENGINE TRUSS COWL BRACKET WELD AREA CRACKED. PERFORMED WELD REPAIR TO ENGINE TRUSS COWL BRACKET WELD AREA.

Part: HANDLE — STIFF (EMERGENCY EXIT) · airframe 30,115 hrs · 35,013 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED LT EMERGENCY EXIT HANDLE STIFF TO OPERATE. LUBRICATED LT EMERGENCY EXIT HANDLE.

Part: HINGE BRACKET — CORRODED (ELEVATOR) · airframe 29,940 hrs · 34,799 cycles

DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT ELEVATOR CENTER HINGE BRACKET EXFOLIATED. REPLACED RIGHT ELEVATOR CENTER HINGE BRACKET.

Part: HINGE BRACKET — CORRODED (ELEVATOR) · airframe 29,940 hrs · 34,799 cycles

DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT ELEVATOR INBOARD HINGE BRACKET HAS CORROSION. REPLACED RIGHT ELEVATOR INBOARD HINGE BRACKET.

Part: HINGE BRACKET — CORRODED (ELEVATOR) · airframe 29,940 hrs · 34,799 cycles

DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT ELEVATOR CENTER HINGE BRACKET EXFOLIATED. REPLACED RIGHT ELEVATOR CENTER HINGE BRACKET.

Part: BULB — INOPERATIVE (MLG INDICATOR) · airframe 29,665 hrs · 34,497 cycles

DURING APPROACH SELECTED LANDING GEAR DOWN HAD GREEN LIGHT INDICATION ON THE MAIN GEAR BUT NOT ON THE NOSEWHEEL. R & R LANDING GEAR INDICATOR BULBS.

Part: HANDLE — BINDING (EMERGENCY EXIT) · airframe 29,587 hrs · 34,412 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED SEAT 6A EMERGENCY EXIT INTERIOR HANDLE IS HARD TO OPERATE. LUBRICATED SEAT 6A EMERGENCY EXIT INTERIOR AND EXTERIOR DOOR HANDLES. OPS CHECKS GOOD.

Part: STRINGER — CORRODED (BS 258 S14L) · airframe 29,587 hrs · 34,412 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED INTERIOR CORROSION APPROX FS 258, STRINGER 14L, FWD OF ANGLE AT SPLICE AREA OF STR 14L. REMOVED DAMAGED SECTION OF STRINGER AND SPLICED IN NEW STRINGER AND INSTALLED EXTERNAL DOUBLER REPAIRS.

Part: SHIM — CORRODED (BS 363 S15-16L) · airframe 29,587 hrs · 34,412 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED CORROSION FS 363 FWD AND AFT OF ANGLE BETWEEN STRINGERS 15L AND STRINGER 16. REMOVED AREA OF CORROSION AND REPLACED SECTION OF DAMAGED SHIM.

Part: ANGLE — CRACKED (BS 150 S9L) · airframe 29,587 hrs · 34,414 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED INTERIOR FUSELAGE ANGLE CRACKED AT FS 150 STRINGER 9AL AT AIRSTAIR DOOR TOP AFT ATTACH POINT OF LOWER BRACKET. (OPEN)

Part: ANGLE — CRACKED (BS 150 S9L) · airframe 29,587 hrs · 34,414 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED INTERIOR FUSELAGE ANGLE CRACKED AT FS 150 STR, 9AL AT AIRSTAIR DOOR TOP AFT ATTACH POINT OF LOWER BRACKET. REMOVED 2.25 INCHES OF DAMAGED ANGLE AND INSTALLED REPAIR ANGLE.

Part: PANEL — OUT OF LIMITS (MAIN PAX) · airframe 29,247 hrs · 34,036 cycles

PILOT REPORTED CABIN DOOR HARD TO OPEN AFTER LANDING. TRIMMED CABIN DOOR INTERIOR PANEL AROUND PUSH BUTTON OPS CHECK GOOD.

Part: LINE — LEAKING (HYDRAULIC SYSTEM) · airframe 29,099 hrs · 33,885 cycles

DURING FLIGHT HYD LOW LIGHT ILLUMINATED UPON LANDING GEAR EXTENSION, FOUND LARGE HYD FLUID PUDDLE UNDER WING. REPLACED HAND PUMP HYD RETURN LINE. LANDING GEAR OPS CHECK GOOD.

Part: ACTUATOR — BYPASSING (MLG) · airframe 29,057 hrs · 33,840 cycles

DURING FLIGHT LANDING GEAR MOTOR RECYCLING IN AIR ABOUT EVERY THREE TO FOUR MINUTES. REPLACED LT MLG ACTUATOR, OPS CHECK GOOD.

Part: HINGE — CORRODED (RUDDER) · airframe 28,904 hrs · 33,671 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED RUDDER CTR HINGE HAS CORROSION. REPLACED RUDDER CTR HINGE.

Part: HINGE — CORRODED (RUDDER) · airframe 28,904 hrs · 33,671 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED VERTICAL STABILIZER UPPER RUDDER HINGE HAS CORROSION. REPLACED VERTICAL STABILIZER UPPER RUDDER HINGE.

Part: PRESSURE SWITCH — OUT OF ADJUST (NLG) · airframe 28,817 hrs · 33,571 cycles

PILOT REPORTED DELAY IN NOSE WHEEL EXTENSION 4 SECONDS AFTER MAINS. REPLACED HYD PRESSURE SWITCH AND ADJUSTED NLG DOWN POSITION SWITCH. LANDING GEAR OPS CHECK NORMAL.

Part: ACCESS PANEL — DELAMINATED (RT WING) · airframe 28,752 hrs · 33,511 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED RT WING FUEL ACCESS PANEL 631DB LEAKING FUEL. INSTALLED EXTERNAL RING DOUBLER ON WING SKIN AT FUEL ACCESS PANEL 631DB, NO LEAKS NOTED.

Part: STRINGER — CORRODED (LT WING) · airframe 28,716 hrs · 33,477 cycles

DURING SCHEDULED X-RAY INSP DISCOVERED LT WING COLLECTOR TANK LWR SKIN AFT OF MAIN SPAR BONDED STR HAS MINOR SURFACE CORROSION. REMOVED CORROSION AND INSTALLED AN EXTERNAL REPAIR DOUBLER.

Part: SPAR — CORRODED (LT WING) · airframe 28,716 hrs · 33,477 cycles

DURING SCHEDULED X-RAY INSP OF LT WING COLLECTOR TANK FOUND SEVERAL SPOTS OF CORROSION ON LWR MAIN SPAR. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR STRAP.

Part: DOOR — STUCK (RIGHT AFT) · airframe 28,269 hrs · 33,015 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED RT AFT EMERGENCY EXIT WILL NOT COME OUT OF FRAME. (JAMMED) LUBRICATED RT AFT EMERGENCY EXIT. OPS CHECK GOOD.

Part: HINGE BRACKET — CORRODED (RT ELEVATOR) · airframe 27,877 hrs · 32,631 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED RT ELEVATOR OTBD HINGE BRACKET EXFOLIATED. C/A: REPLACED RT ELEVATOR OTBD HINGE BRACKET.

Part: HINGE BRACKET — CORRODED (RT ELEVATOR) · airframe 27,877 hrs · 32,631 cycles

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

Part: SQUAT SWITCH — FAILED (MLG) · airframe 27,463 hrs · 32,186 cycles

DURING TEST FLIGHT LT MAIN LANDING GEAR DID NOT EXTEND. MANUALLY EXTENDED LANDING GEAR. LT MAIN GEAR ILLUMINATED DOWN AND LOCKED. OBTAINED 3 GREEN DOWN AND LOCKED INDICATION. REPLACED LT MLG SQUAT SWITCH ASSY. TEST FLIGHT SATISFACTORY.

Part: WIRE — CHAFED (LT NACELLE) · airframe 27,408 hrs · 32,122 cycles

DURING FLIGHT, DISCOVERED LANDING GEAR CIRCUIT BREAKER POPPED. REPAIRED CHAFED WIRE D6D22 ON TOP LT NACELLE.

Part: PCB — FAILED (MLG) · airframe 27,360 hrs · 32,065 cycles

PILOT REPORTED NO 3 GREEN GEAR INDICATION LIGHTS. REPLACED PCB A319. LANDING GEAR OPERATIONAL CHECK NORMAL.

Part: PCB — DAMAGED (MLG) · airframe 27,360 hrs · 32,065 cycles

PILOT REPORTED NO 3 GREEN GEAR INDICATION LIGHTS. REPLACED PCB A319. LANDING GEAR OPS CHECK, NORMAL.

Part: CIRCUIT BREAKER — TRIPPED (LANDING GEAR) · airframe 27,357 hrs · 32,062 cycles

DURING APPROACH LANDING GEAR INDICATION CIRCUIT BREAKER POPPED AFTER SELECTING GEAR DOWN. RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. OPS CHECK FOUND TO BE WORKING OK. INSPECTED LANDING GEAR SYSTEMS UNABLE TO FIND ANY PROBLEM OPERATIONAL CHECK OK.

Part: WIRE — BROKEN (MLG) · airframe 27,125 hrs · 31,844 cycles

FLIGHT: 9270 DURING APPROACH LANDING GEAR INDICATOR CIRCUIT BREAKER POPPED AFTER GEAR EXTENSION. FOUND BROKEN BROKEN WIRE ON LEFT LANDING GEAR DOWN LOCK CONNECTOR. SPLICED BROKEN WIRE.LANDING GEAR OPERATIONAL CHECK NORMAL.

Part: CIRCUIT BREAKER — UNKNOWN (MLG INDICATOR) · airframe 27,125 hrs · 31,844 cycles

FLIGHT: 9233 DURING FLIGHT LANDING GEAR INDICATOR CIRCUIT BREAKER POPPED UNABLE TO RESET. RETURNED TO FLL. REPLACED LANDING GEAR INDICATOR CIRCUIT BREAKER. LANDING GEAR OPERATIONAL CHECK NORMAL.TEST FLIGHT SATISFACTORY.

Part: CIRCUIT BREAKER — TRIPPED (MLG) · airframe 27,122 hrs · 31,841 cycles

AFTER TAKEOFF, LANDING GEAR CIRCUIT BREAKER POPPED AFTER GEAR RETRACTED, RESET CIRCUIT BREAKER, STAYED IN THE REST OF THE FLIGHT. PERFORMED OPS CHECK OF LANDING GEAR. OPS CHECK GOOD. COULD NOT DUPLICATE.

Part: DOOR — OUT OF RIG (EMERGENCY EXIT) · airframe 26,674 hrs · 31,384 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED RT AFT EMERGENCY EXIT HARD TO OPEN. RERIGGED RT AFT EMERGENCY EXIT. OPS CHECK GOOD.

Part: SKIN — CORRODED (RT WING) · airframe 26,674 hrs · 31,384 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED RT OTBD WING UPPER SKIN TRAILING EDGE HAD CORROSION AND DEBOND BETWEEN WS 139 THROUGH 158. REMOVED DAMAGED SKIN AND FABRICATED AND INSTALLED AN EXTERNAL REPAIR DOUBLER.

Part: WIRE — BROKEN (LT MLG) · airframe 26,492 hrs · 31,207 cycles

FLIGHT 5201 MIA/FLL - DURING APPROACH LEFT LANDING GEAR INDICATION LIGHTS DOES NOT SHOW LOCKED. CONTINUED TO FLL. LANDED WITHOUT INCIDENT. REPAIRED BROKEN WIRE AT LEFT MAIN LANDING GEAR CONNECTOR P273. OPERATIONAL CHECK NORMAL.

Part: HANDLE — LACK OF LUBE (EMERGENCY EXIT) · airframe 26,432 hrs · 31,145 cycles

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT EMERGENCY EXIT DIFFICULT TO OPEN. LUBRICATED LEFT EMERGENCY EXIT HANDLE.

Part: SQUAT SWITCH — LOOSE (RT MLG) · airframe 25,448 hrs · 30,062 cycles

FLIGHT: 9140 AFTER TAKEOFF, LANDING GEAR WILL NOT RETRACT. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT RESECURED RT LANDING GEAR SQUAT SWITCH. LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHECK GOOD.

Part: ANNUNCIATOR — LOOSE (COCKPIT) · airframe 25,236 hrs · 29,832 cycles

FLIGHT: 9208, DURING APPROACH, LT LANDING GEAR INDICATOR DID NOT ILLUMINATE WITH GEAR DOWN, ATTEMPTED TO PUMP GEAR DOWN. THE ANNUNCIATOR CAME ON BY ITSELF. INSPECTED LANDING GEAR SYS, SECURED ANNUNCIATOR LEGEND. OPERATIONAL CHECK GOOD.

Part: DOWNLOCK SWITCH — FAILED (MLG) · airframe 25,119 hrs · 29,699 cycles

FLIGHT: 9164, DURING APPROACH, LANDING GEAR INDICATED DOWN AND LOCKED (3) GREEN. HOWEVER, FLAPS WOULD NOT EXTEND BEYOND 17 DEGREES WITHOUT GEAR WARNING HORN SOUNDING. UPON LANDING THE GEAR HANDLE LIGHT ILLUMINATED. GEAR HANDLE LIGHTS AND GEAR HORN WILL NOT EXTINGUISH OR SILENCE. REPLACED RT MLG DOWNLOCK SWITCH.

Part: DOWNLOCK SWITCH — OUT OF ADJUST (LT MLG) · airframe 25,122 hrs · 29,688 cycles

FLIGHT:9265, DURING APPROACH WHEN PLACING LANDING GEAR DOWN LT GREEN LIGHTS WILL NOT ILLUMINATE. ADJUSTED LT DOWNLOCK SWITCH.

Part: MASTER CYLINDER — BYPASSING (BRAKES) · airframe 25,106 hrs · 29,681 cycles

FLIGHT: 9182, DURING TAXI RT BRAKES FAILS OCCASIONALLY. REPLACED CAPTAINS RT MASTER CYLINDER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 22,699 hrs · 26,876 cycles

AT SCHEDULED INSPECTION DISCOVERED 2 CRACKS AT NR 2 COMM ANTENNA (FS400) 1 CRACK 5.5 INCHES RUNNING LONGITUDINALLY FORWARD FROM FS 403 THE OTHER CRACK 1.5 INCHES LONG RUNNING LONGITUDINALLY FORWARD FROM FS 397. STOP DRILLED CRACKS AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER IAW STRUCTURAL REPAIR MANUAL 51-70-06.

Part: HINGE BRACKET — CORRODED (LT STABILIZER) · airframe 22,692 hrs · 26,866 cycles

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

Part: LANDING GEAR — MALADJUSTMENT · airframe 22,264 hrs · 26,367 cycles

FLIGHT:9199 EYW/MCO/DURING APPROACH, LANDING GEARS DID NOT EXTEND, MANUAL GEAR EXTENSION EXECUTED. MAINTENANCE FERRY TO FLL. INSPECTED LANDING GEAR SYSTEM REPLACED HYDRAULIC PUMP MOTOR AND CIRCUIT BREAKER. LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHECK NORMAL.

Part: LINE — LOOSE (MLG BRAKES) · airframe 21,990 hrs · 26,044 cycles

FLIGHT: 9247 FLL/BIM DURING TAXI COMPLETE LOSS OF BRAKE PRESSURE ON THE RIGHT BRAKES. TIGHTENED RIGHT BRAKE LINE OPERATIONAL CHECK GOOD.

Part: BRAKE ASSY — MALFUNCTIONED (MLG)

DURNG TAXI, LT AND RT BRAKES FEEL SPONGY. REQUIRES ADDITIONAL PRESSURE TO APPLY BRAKES. BELD ALL FOUR BRAKES. OPERATIONAL CHECK NORMAL. (K)

Part: BRACKET — CORRODED (LT STAB ELEVATOR)

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

Part: BRACKET — CORRODED (RT STAB ELEVATOR)

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

Part: BRACKET — CORRODED (LT STAB 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 STAB ELEVATOR)

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

Part: CIRCUIT BOARD — SHORTED (BLEED AIR)

DURING FLIGHT, SMELLED ELECTRICAL ODOR IN COCKPIT. SELECTED LT BLEED AIR ENVIRONMENTAL OFF. CONTINUED TO NAS. LANDED WITHOUT INCIDENT. MAINTENANCE FERRY. REPAIRED CHAFFED WIRE FROM PRESSURE REGULATOR PIN F. REMOVED AND REPLACED BLEED AIR PC BOARD A317. OPERATIONAL CHECK NORMAL.

Part: CIRCUIT BOARD — SHORTED (ENVIRO CONTROL)

DURING FLIGHT, ELECTRICAL SMOKE IN FLIGHT DECK. LEFT ENVIRONMENTAL WHITE OFF LIGHT ILLUMINATED. PULLED CIRCUIT BREAKER. CONTINUED TO FLL. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ENVIRONMENTAL CONTROL PC BOARD. (M)

Part: CONTACTOR — DIRTY (LT FIRE BOTTLE)

DURING FLIGHT, LEFT FIRE EXTINGUISHER DISCHARGE LIGHT FLICKERS. CONTINUED TO DESTINATION. CLEANED CONTACTS AT LEFT FIRE BOTTLE. OPERATIONAL CHECK, OK.

Part: BOLT — LOOSE (VERTICAL STAB)

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 BEECH MM.

Part: CONTROL HANDLE — WEAK (COCKPIT)

FLT 9172 - FPO/FLL - DURING APPROACH, LANDING GEAR INTRANSIT LIGHTS INOPERATIVE. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE. PERFORMED LANDING GEAR EXTENSION AND RETRACTION. OPS CHECK NORMAL. (M)

Part: ACTUATOR — FAILED (LT MAIN GEAR)

PIT - FLT 3030 - ON APPROACH TO PIT, THE LEFT MLG FAILED TO EXTEND. THE CREW RECYCLED THE GEAR AND THE GEAR CAME DOWN WITH NORMAL INDICATION. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT MLG ACTUATOR IAW BEECHCRAFT MM 32-30-10. ALL OPERATIONAL CHECKS WERE GOOD IAW 32-30-10. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: BRAKE — FAILED (LEFT)

CLE - FLT 3372 - AFTER LANDING IN CRW, THE CREW REPORTED HIS LEFT BRAKE FAILED DURING TAXI TO THE GATE. THE AIRCRAFT CONTINUED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED THE BRAKE SYSTEM IAW BEECHCRAFT MM 12-10-00. PERFORMED AIRCRAFT TAXI AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: WARNING LIGHT — ILLUMINATED (AUTOFEATHER SYS)

FLT 3213 - PILOT REPORTED, THE AUTOFEATHER OFF AMBER CAUTION ANNUNCIATOR ILLUMINATED ON TAKEOFF ROLL. THE AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 61-3/3 PLACARD NUMBER 116062. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (BATTERY COMP)

FLT 3075 - PILOT REPORTED THAT THE BATTERY CHARGE LIGHT WOULD NOT GO OUT. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE MAIN BATTERY IAW BEECHCRACT 1900D MM 24-32-00. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: BOLT — LOOSE (RT ENG TRUSS)

AXO - DURING A SCHEDULED INSPECTION, THE LOWER OUTBOARD TRUSS BOLT WAS FOUND LOOSE ON THE RIGHT HAND ENGINE. MAINTENANCE REMOVED AND REPLACED THE LOWER OUTBOARD TRUSS BOLT NUT AND RETAINER ON THE RIGHT HAND ENGINE IAW B1900 MM 71-20-00, AND EA NR 7120-01018. AIRCRAFT RELEASED FOR SERVICE. AIRCRAFT TT: 6,847.0 HOURS. TOTAL CYCLES: 8,145.