N49543

Part: SKIN — CORRODED (LT WING) · airframe 34,191 hrs · 40,021 cycles

DURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT WING ON TOP TRAILING EDGE SURFACE CORROSION. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR.

Part: WIRE — SHORTED (MLG) · airframe 33,945 hrs · 39,717 cycles

FLIGHT4026, LANDING GEAR HAS TO BE MANUALLY PUMPED, THREE GREEN AFTER MANUAL EXTENSION. RECONNECTED HYDRAULIC POWER PACK SELECT VALVE WIRING AT LEFT STUB WING INBOARD OF FUSELAGE, LANDING GEAR EXTENSION AND RETRACTION, OPS CHECKED GOOD.

Part: WIRE — SHORTED (MLG) · airframe 33,945 hrs · 39,717 cycles

FLIGHT 4026, LANDING GEAR HAS TO BE MANUALLY PUMPED, THREE GREEN AFTER MANUAL EXTENSION. RECONNECTED HYDRAULIC POWER PACK SELECT VALVE WIRING AT LEFT STUB WING INBOARD OF FUSELAGE, LANDING GEAR EXTENSION AND RETRACTION. OPS CHECKED GOOD.

Part: HANDLE — LACK OF LUBE (EMERGENCY EXIT) · airframe 33,585 hrs · 39,267 cycles

DURING SCHEDULED ROUTINE C-3 INSPECTION DISCOVERED RIGHT AFT EMERGENCY EXIT INNER HANDLE STIFF. LUBRICATED RIGHT AFT EMERGENCY EXIT HANDLE.

Part: HANDLE — LACK OF LUBE (EMERGENCY EXIT) · airframe 33,585 hrs · 39,267 cycles

DURING SCHEDULED ROUTINE C-3 INSPECTION DISCOVERED RIGHT FORWARD EMERGENCY EXIT OUTER HANDLE WILL NOT SPRING OPEN. LUBRICATED RIGHT FORWARD EMERGENCY EXIT DOOR OUTER HANDLE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 33,100 hrs · 38,634 cycles

REPORT: DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED BELLY SKIN CORROSION AFT OF LOWER BEACON AT FS 378.25. REMOVED CORROSION AND INSTALLED FILLER AND DOUBLER REPAIR.

Part: TORQUE TUBE — CORRODED (LT ELEVATOR) · airframe 33,058 hrs · 38,591 cycles

DURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT ELEVATOR TORQUE TUBE CORROSION. REPLACED LEFT ELEVATOR TORQUE TUBE.

Part: TORQUE TUBE — CORRODED (RT ELEVATOR) · airframe 33,058 hrs · 38,591 cycles

DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT ELEVATOR TORQUE TUBE CORROSION. REPLACED RIGHT ELEVATOR TORQUE TUBE.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 32,977 hrs · 38,485 cycles

DURING SCHEDULED ROUTINE INSPECTION DISCOVERED AVIONICS DOOR FUSELAGE FRAME RIGHT CHANNEL HAS .6 INCH CRACK AT AFT LOWER CORNER RADIUS. CUT OUT CRACK AND INSTALLED REPAIR STRAP.

Part: SWITCH — OUT OF ADJUST (AUTOFEATHER SYS) · airframe 32,700 hrs · 38,155 cycles

FLIGHT 9205 TCB/FLL DURING DESCENT AND APPROACH TO LANDING WITH AUTOFEATHER ARMED THE AFX DISABLE ANNUNCIATOR ILLUMINATES WITH VERY MOVEMENT OF THE POWER LEVER. RE-ADJUSTED AUTOFEATHER ARMING SWITCH OPERATIONAL CHECK SATISFACTORY.

Part: STRINGER — DEBONDED (FUSELAGE) · airframe 31,940 hrs · 37,279 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED BONDED STRINGER DEBONDED FROM FUSELAGE SKIN FROM FS 363 TO FS 423. OPEN

Part: BULKHEAD — CRACKED (BS 456-468.25) · airframe 31,940 hrs · 37,279 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED CRACK BETWEEN FS 456 TO 468.25 BETWEEN STRINGERS 11R AND 12R ON CARGO FLOOR BULKHEAD. 288. REPAIRED CRACK, INSTALLED DOUBLER 2.1 INCHES X 8.3 INCHES BETWEEN FS 456.00 TO 468.25.

Part: ANGLE — CRACKED (BS 288) · airframe 31,940 hrs · 37,279 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED LT WING FUSELAGE CLOSING ANGLE CRACKED APPROX 1.75 INCHES AT FS 288. REPAIRED LT WING FUSELAGE CLOSING ANGLE.

Part: HANDLE — STIFF (EMERGENCY EXIT) · airframe 31,898 hrs · 37,230 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED RT AFT EMERGENCY EXIT DOOR INNER HANDLE STIFF TO OPERATE. LUBRICATED RT EMERGENCY EXIT DOOR INNER HANDLE. OPS CHECK NORMAL.

Part: ISOLATOR — CRACKED (ENGINE MOUNT) · airframe 31,884 hrs · 37,208 cycles

DURING MAGNETIC PARTICLE INSP DISCOVERED ISOLATOR MOUNT WELD AREA CRACKS. PERFORMED WELD REPAIR TO ENGINE TRUSS TUBE WELD AREAS.

Part: HANDLE — BINDING (EMERGENCY EXIT) · airframe 31,269 hrs · 36,504 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED RT AFT EMERGENCY EXIT DOOR HARD TO OPEN. LUBRICATED RT AFT EMERGENCY EXIT DOOR HANDLE. OPS CHECK OK.

Part: SKIN — CORRODED (BS 423.25 S16) · airframe 30,785 hrs · 35,973 cycles

DURING SCHEDULED ROUTINE MX, DISCOVERED FUSEALGE BELLY SKIN EXFOLIATION AT FS 423.25 STRINGER 16. REMOVED DAMAGED SKIN AND INSTALLED EXTERNAL DOUBLER REPAIR.

Part: CABLE — FRAYED (AIRSTAIR DOOR) · airframe 30,759 hrs · 35,945 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED AIRSTAIR DOOR LOWER AFT CABLE FRAYED AND LOWER BELLCRANK LOOSE. REPLACED AIRSTAIR DOOR LOWER AFT CABLE AND ADJUSTED LOWER BELLCRANK SCREWS.

Part: TRIMMER — BINDING (ELEVATOR) · airframe 30,422 hrs · 35,571 cycles

DURING FLIGHT, ELEVATOR TRIM WHEEL BINDS UP UNABLE TO SEE TRIM TABS ON WHEEL FOR ALL STAGES OF FLIGHT. REPLACED ELEVATOR TRIM TAB INDICATOR OPS CHECK OK. TEST FLIGHT SATISFACTORY.

Part: TRIMMER — BINDING (ELEVATOR) · airframe 30,422 hrs · 35,571 cycles

DURING FLIGHT ELEVATOR TRIM WHEEL BINDS UP UNABLE TO SEE TRIM TABS ON WHEEL FOR ALL STAGES OF FLIGHT. REPLACED ELEVATOR TRIM TAB INDICATOR OPS CHECK OK. TEST FLIGHT SATISFACTORY.

Part: UPLOCK SWITCH — OUT OF ADJUST (MLG) · airframe 30,391 hrs · 35,538 cycles

DURING FLIGHT LANDING GEAR CONTROL HANDLE RED LIGHTS FLICKER ON AND OFF WHEN IN TURBULENT FLIGHT CONDITIONS. C/A: ADJUSTED RT MLG UP POSITION INDICATOR SWITCH. LANDING GEAR OPS CHECK GOOD.

Part: FRAME — CRACKED (BS 150) · airframe 29,922 hrs · 35,039 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED AIRSTAIR DOOR FUSELAGE FRAME ANGLE CRACKED AT FS 150.60 AT GAS STRUT LOWER ATTACH POINT. REMOVED DAMAGED SECTION OF ANGLE AND INSTALLED FRAME ANGLE REPAIR.

Part: SPAR — CORRODED (RT WING) · airframe 29,604 hrs · 34,693 cycles

DURING SCHEDULED X-RAY INSP, DISCOVERED RT WING LWR AFT SPAR ON COLLECTOR TANK HAS SMALL SPOT OF SURFACE CORROSION BETWEEN WS 114.25 TO 124.25. BLENDED OUT CORROSION AND INSTALLED REPAIR STRAP. NOTE: PREVIOUSLY SUBMITTED, OPEN.

Part: TORQUE TUBE — CORRODED (RT ELEVATOR) · airframe 28,958 hrs · 34,019 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED RT ELEVATOR TORQUE TUBE SHOW SIGNS OF EXFOLIATION. REPLACED RT ELEVATOR TORQUE TUBE.

Part: TORQUE TUBE — CORRODED (LT ELEVATOR) · airframe 28,958 hrs · 34,019 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED LT ELEVATOR TORQUE TUBE SHOW SIGNS OF EXFOLIATION. REPLACED LT ELEVATOR TORQUE TUBE ASSY.

Part: HINGE BRACKET — CORRODED (RT ELEVATOR) · airframe 28,958 hrs · 34,019 cycles

DURING ROUTINE INSP DISCOVERED RT ELEVATOR CTR HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR CTR HINGE BRACKET.

Part: HINGE BRACKET — CORRODED (LT ELEVATOR) · airframe 28,958 hrs · 34,019 cycles

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

Part: HINGE BRACKET — CORRODED (LT ELEVATOR) · airframe 28,958 hrs · 34,019 cycles

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

Part: HORN — CORRODED (ELEVATOR TRIM TA) · airframe 27,958 hrs · 34,019 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED RT ELEVATOR INBD TRIM TAB HORN EXFOLIATED. REPLACED RT ELEVATOR TRIM TAB.

Part: HINGE BRACKET — CORRODED (ELEVATOR) · airframe 27,899 hrs · 32,950 cycles

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

Part: HINGE BRACKET — CORRODED (RUDDER) · airframe 27,899 hrs · 32,950 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED LOWER RUDDER HINGE BRACKET HAS EXFOLIATION. REPLACED LOWER RUDDER HINGE BRACKET.

Part: HINGE BRACKET — CORRODED (RUDDER) · airframe 27,899 hrs · 32,950 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED RUDDER UPPER HINGE BRACKET HAS EXFOLIATION. REPLACED RUDDER UPPER HINGE BRACKET

Part: DOOR — STUCK (EMERGENCY EXIT) · airframe 27,710 hrs · 32,766 cycles

DURING SCHEDULED ROUTINE MAINT, DISCOVERED LT EMERGENCY EXIT DOOR DIFFICULT TO OPEN. LUBRICATED LT EMERGENCY EXIT DOOR. OPS CHECK GOOD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 27,356 hrs · 32,385 cycles

AT SCHEDULED INSPECTION DISCOVERED EXFOLIATION AT LOWER FUSELAGE SKIN AT FS 250.750 STRINGER 15L. REMOVED DAMAGED SKIN AND INSTALLED REPAIR DOUBLER PER BEECH STRUCTURAL REPAIR MANUAL 51-70-06.

Part: CABLE ASSY — BROKEN (AIRSTAIR DOOR) · airframe 27,121 hrs · 32,144 cycles

FLIGHT 9146 - TPA/MIA - PILOT REPORTED FORWARD DOOR CAMLOCKS STUCK. DOOR WOULD NOT OPEN FROM INSIDE OR OUTSIDE. REPLACED FORWARD AIRSTAIR DOOR UPPER FORWARD CABLE ASSEMBLY.

Part: SKIN — CORRODED (RT WING) · airframe 26,503 hrs · 31,431 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED RT OTBD WING, UPPER SKIN, T/E HAD CORROSION AND DEBOND BETWEEN WS 121 THROUGH 194.85. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED AND EXTERNAL REPAIR DOUBLER

Part: WIRE — LOOSE (FIRE BOTTLE) · airframe 26,154 hrs · 31,046 cycles

FLIGHT:9263, DURING FLIGHT, RT DISCHARGE LIGHT ILLUMINATED INTERMITTENTLY. RESECURED WIRE AT RT FIRE BOTTLE.

Part: SKIN — CRACKED (BS 288) · airframe 24,054 hrs · 29,815 cycles

AT SCHEDULED INSPECTION DISCOVERED AIRCRAFT BELLY RT SIDE HAS A FUSELAGE CRACK AT FS 288.0. STOP DRILLED CRACK AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER IAW STRUCTURAL REPAIR MANUAL 53-90-18.

Part: HANDLE — OUT OF ALIGNMENT (EMERGENCY EXIT) · airframe 24,240 hrs · 28,870 cycles

AT SCHEDULED FLEET CAMPAIGN INSPECTION: SEAT 6F HATCH COVER NEEDS ADJUSTMENT CATCHING ON SIDEWALL. ADJUSTED SEAT 6F EMERGENCY HATCH COVER.

Part: SKIN — GROUND DAMAGE (BS 782-500) · airframe 23,417 hrs · 27,927 cycles

FLIGHT: 9214, DURING GROUND HANDLING BAGGAGE CART DAMAGE BELOW CARGO DOOR LOCATED AT F.S 482.75 TO F.S 500. CUT OUT DAMAGE SECTION OF SKIN 17.0 IN X 7.0 IN FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER 20.0 IN X 10.0 IN IAW STRUCTURAL REPAIR MANUAL 51-70-06.

Part: SMOKE — DETECTED (CABIN)

MCO/MIA DURING FLIGHT SMELL OF SMOKE, NO SMOKE WAS VISUALLY OBSERVED AND ODOR WAS DISSIPATING. CONTINUED TO MIA LANDED WITHOUT INCIDENT. INSPECTED BOTH VENT BLOWERS UNDER CABIN FLOOR, NO DEFECTS NOTED. COULD NOT DUPLICATE SMELL OF SMOKE.

Part: WARNING LIGHT — FALSE ACTIVATION (RT FIRE DETECTOR)

DURING FLIGHT RIGHT FIRE DISCHARGE ANNUNCIATOR ILLUMINATED INTERMITTENTLY. INSPECTED THE RIGHT FIRE PROTECTION SYSTEM, NO DEFECTS NOTED.

Part: WARNING LIGHT — FALSE ACTIVATION (RT EXTINGUISHER)

DURING FLIGHT RIGHT FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATES INTERMITTENTLY. CLEANED CONTACTS AT THE RIGHT FIRE EXTINGUISHER.

Part: WIRE HARNESS — LOOSE (FIRE EXTINGUISHE)

DURING FLIGHT RIGHT ENGINE DISCHARGE LIGHT ILLUMINATED ON AND OFF. SECURED WIRE BUNDLE AT THE RIGHT WHEEL WELL FIRE EXTINGUISHER BOTTLE.

Part: WIRE — OUT OF POSITION (EXTINGUISHER)

DURING FLIGHT RIGHT ENGINE FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATED INTERMITTENTLY. REPOSITION WIRES AT THE RIGHT FIRE EXTINGUISHER ANNUNCIATOR.

Part: CONNECTOR — LOOSE (FIRE DETECTOR)

DURING FLIGHT, RT FIRE EXTINGUISHER DISCHARGE ANNUNCIATOR ILLUMINATED INTERMITTENTLY. RESECURED WIRE CONNECTORS AT RT FIRE EXTINGUISHER ANNUNCIATOR SWITCH. (K)

Part: O-RING — WORN (NR 3 BRAKE)

NO BRAKES AFTER PRESSING THE RT BRAKE PEDAL. REPLACED NR 3 AND 4 BRAKE ASSEMBLIES. UPON BRAKE REMOVAL, DETERMINED NR 3 BRAKE SWIVEL FITTING O-RING TO BE LEAKING. (K)

Part: ENGINE — FAILED (RIGHT)

FLT 9187 - MHH/FLL - DUIRNG APPROACH, ON SHORT FINAL TO RUNWAY 9 LEFT AT 500 FEET, THE NR 2 ENGINE FAILED. LANDED WITHOUT FURTHER INCIDENT. PILOT SHUTDOWN ENGINE ON TAXI IN. REMOVED AND REPLACED NR 2 ENGINE ASSY. OPERATIONAL CHECK NORMAL. (M)

Part: ENGINE — FAILED (NR 2)

DURING APPROACH, ON SHORT FINAL TO RUNWAY 9 LT AT 500 FT, THE NR 2 ENGINE FAILED. LANDED WITHOUT FURTHER INCIDENT. PILOT SHUT DOWN ENGINE ON TAXI IN. REMOVED AND REPLACED NR 2 ENGINE ASSEMBLY (GG AND PS). OPERATIONAL CHECK NORMAL. NOTE: SUSPECT NR 2 PT BLADE FAILURE.

Part: BLADE — FAILED (RT ENGINE)

DURING APPROACH, ON SHORT FINAL TO RUNWAY 9 LEFT AT 500 FEET, THE NR2 ENGINE FAILED. LANDED WITHOUT FURTHER INCIDENT. PILOT SHUTDOWN ENGINE ON TAXI IN. REMOVED AND REPLACED NR2 ENGINE ASSY (GG AND PS). OPERATIONAL CHECK NORMAL. NOTE: VERIFIED TO BE 2ND STAGE PT BLADE FAILURE. (CLOSED 5/4/05) (K)

Part: TURBINE BLADES — DAMAGED (LT ENGINE)

FLT 9240 - FLL - DURING LEFT ENGINE START AT APPROXIMATELY 30 PERCENT N1, A GRINDING NOISE WAS HEARD AND STRANGE VIBRATION FELT IN LEFT PROP LEVER. SHUT DOWN ENGINE. DEMATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES FAILED. POWER SECTION HAS INTERNAL DAMAGE. REPLACED LEFT POWER SECTION MODULE AND ROUTED FAILED UNTI FOR FURTHER ANALYSIS AND REPAIR. (M)

Part: TURBINE BLADES — FAILED (LT ENGINE)

DURING LEFT ENGINE START AT APPROXIMATELY 30 PERCENT N1, A GRINDING NOISE WAS HEARD AND STRANGE VIBRATION FELT IN LEFT PROP LEVER. SHUT DOWN ENGINE. DEMATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES FAILED. POWER SECTION HAS INTERNAL DAMAGE. REPLACED LT POWER SECTION MODULE AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. CONFIRMED 2ND STAGE POWER TURBINE BLADE FAILURE. SUBSTANTIAL DAMAGE OCCURRED. FULL OVERHAUL OF POEWR SECTION REQUIRED. (M)

Part: POWER UNIT — CONTAMINATED (RT ENGINE)

AT SCHEDULED ROUTINE INSPECTION (A CHECK) THE RIGHT ENGINE WAS DETERMINED TO HAVE DISCOLORED (BLACK OIL). C/A CHANGED THE ENGINE OIL AND OIL FILTER. PLACED ENGINE ON OIL WATCH. REPLACED THE RIGHT POWER SECTION MODULE AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR.

Part: OIL SYSTEM — CONTAMINATED (ENGINE)

AT SCHEDULED ROUTINE INSPECTION (A CHECK) THE RIGHT ENGINE WAS DETERMINED TO HAVE DISCOLORED "BLACK OIL". CHANGED THE ENGINE OIL AND OIL FILTER. PLACED ENGINE ON OIL WATCH.

Part: BOLT — LOOSE (VERTICAL STAB)

AT SCHEDULED ROUTINE INSPECTION VERTICAL FIN LOWER ATTACH BOLTS REQUIRED RETORQUE. RETORQUED FOUR LOWER VERTICAL BOLTS IAW MM.

Part: PRINTED CKT BOARD — UNSECURE (E/E BAY)

FLT 9511 - MIA-FLL - AFTER TAKEOFF, LANDING GEAR FAILED TO STOW COMPLETELY. SECURED PCBA316. OPERATIONAL CHECK OF LANDING GEAR EXTENSION AND RETRACTION NORMAL. (M)

Part: HUB — SCORED (BRG RETENTION)

PROPELLER WAS RECEIVED FOR O/H WITH EXCESSIVE GREASE LEAKAGE FROM ALL BLADES. PROP WAS DISASSEMBLED TO START O/H PROCESS. WHEN HUB UNIT WAS SPLIT, THERE WAS EXCESSIVE AMOUNTS OF GREASE INSIDE. UPON FURTHER INSPECTION, THE BEARING RACE HAD SHATTERED INTO SEVERAL PIECES, SCORING THE INSIDE RETENTION AREA. REWORK WAS BEYOND ALLOWABLE LIMITS. HUB WAS RETIRED FROM SERVICE.

Part: BEARING — DAMAGED (BLADE BEARING)

PROPELLER WAS RECEIVED FOR O/H WITH EXCESSIVE GREASE LEAKAGE FROM ALL BLADES. WHEN PROP WAS DISASSEMBLED, THE HUB UNIT WAS FILLED WITH EXCESSIVE AMOUNTS OF GREASE. UPON FURTHER INSPECTION, THE GREASE WAS FOUND TO CONTAIN SEVERAL PIECES OF THE BLADE BEARING RACE. THE BEARING RACE WAS SHATTERED INTO SEVERAL SMALL PIECES. THE SHATTERED BEARING CAUSED DAMAGED TO THE HUB RETENTION AREA.

Part: MOTOR — ODOR (TE FLAPS)

CLE - FLT 3231 - DURING TAXI, THE CREW REPORTED A SMOKE SMELL IN THE COCKPIT. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP MOTOR IAW BEECHCRAFT 1900D MM 27-50-03. OPERATIONAL CHECKS WERE GOOD IAW 27-50-00. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: EVA TUBE — FAILED (LT WING)

CLE - FLT 3221 - THE CREW REPORTED A LEFT BLEED AIR FAIL LIGHT ILLUMINATED IN-FLIGHT WHEN PASSING THROUGH 10,500 FEET ALTITUDE. THE LIGHT EXTINGUISHED WHEN THEY DESCENDED BELOW 6,500 FEET ALTITUDE. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPAIRED EVA TUBING IN THE LEFT WING IAW BEECH 1900D MM 26-11-00. THE AIRCRAFT WAS RELEASED TO SERVICE. (X)

Part: RETRACT MECH — REQ'D SERVICE (LT MLG)

CLE-PIT - FLT 3030 - THE CREW REPORTED THE LEFT MAIN GEAR LIGHT DID NOT ILLUMINATED WHEN THE GEAR WAS SELECTED DOWN. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED THE HYDRAULIC RESEVOIR AND PERFORMED OPS CHECK OF THE GEAR IAW B1900D MM 32-30-00, NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: SWITCH — FAILED (ENGINE)

CLE - FLT 3439 - THE CREW REPORTED THAT ON TAKEOFF THE 'AFX DISABLE' LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. THE CREW ABORTED TAKEOFF AND THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE A/F HIGH PRESSURE SWITCH IAW B1900D MM 61-21-00 AND REMOVED AND REPLACED PC BOARD A123 IAW B1900D MM 31-51-05. OPS CHECK OF THE SYSTEM WAS GOOD IAW B1900D MM 61-21-00. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: PC BOARD — FAILED (CABIN)

CLE - FLT 3439 - THE CREW REPORTED THAT ON TAKEOFF THE 'AFX DISABLE' LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. THE CREW ABORTED TAKEOFF AND THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE A/F HIGH PRESSURE SWITCH IAW B1900D MM 61-21-00 AND REMOVED AND REPLACED PC BOARD A123 IAW B1900D MM 31-51-05. OPS CHECK OF THE SYSTEM WAS GOOD IAW B1900D MM 61-21-00. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: PC BOARD — FAILED (AUTOFEATHER SYS)

CLE - FLT 3056 - THE CREW REPORTED THE 'AFX DISABLE' LIGHT REMAINED ILLUMINATED UP TO 15,000 FEET. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PC BOARD, AND PERFORMED OPERATIONAL CHECKS OF THE AUTOFEATHER SYSTEM IAW BEECHCRAFT MM 61-21-00. THE AIRCRAFT WAS RELEASED TO SERVICE. (X)

Part: PC BOARD — FAILED (AUTOFEATHER SYS)

IAD - FLT 3015 - THE CREW REPORTED THAT ON TAKEOFF ROLL, THE 'AFX DISABLE' ANNUNCIATOR ILLUMINATED AT 90 KIAS, THE AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTEANCE REMOVED AND REPLACED PCBA123 AND PERFORMED OPS CHECKS AND ENGINE RUNS IAW BEECHCRAFT MM 61-21-00, NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (X)

Part: SWITCH — DIRTY (AUTOFEATHER SYS)

CAK - FLT 3008 - THE CREW REPORTED THAT ON TAKEOFF ROLL, THE 'AFX DISABLE' ANNUNCIATOR ILLUMINATED AND THE LEFT AUTOFEATHER SYSTEM UNARMED. THE AIRCRAFT REJECTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED PRESSURE SWITCHES IAW BEECHCRAFT MM 61-21-00, THE AIRCRAFT WAS RELEASED TO SERVICE. (X)

Part: VERTICAL GYRO — FAILED (COCKPIT)

CLE - FLT 3239 - CREW REPORTED THAT THE FIRST OFFICERS ELECTRONIC ATTITUDE DIRECTOR INDICATOR FAILED IN FLIGHT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE NR 2 VERTICAL GYRO, ALL OPERATIONAL CHECKS WERE GOOD IAW COLLINS COMPONENT MANUAL. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: SWITCH — DIRTY (NLG)

CLE - FLT 3107 - CREW REPORTED GREEN LIGHT FOR THE NOSE LANDING GEAR CAME ON ABOUT ONE MINUTE AFTER GEAR EXTENSION, NO OTHER WARNING INDICATIONS. MAINTENANCE INSPECTED AIRCRAFT AND CLEANED NOSE GEAR MICROSWITCHES. OPERATIONAL CHECKS WERE GOOD IAW B100D MM 32-30-00. AIRCRAFT WAS RELEASED FOR SERVICE. (X)

Part: ACTUATOR — FAILED (NLG)

CLE - FLT 3097 - CREW REPORTED THE NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. THE GREEN LIGHT DID ILLUMINATE AFTER THE LANDING GEAR WAS CYCLED SEVERAL TIMES. MAINTNANCE INSPECTED ACFT AND REMOVED AND REPLACED NOSE GEAR ACTUATOR IAW B1900D MM 32-30-14. THE NLG WAS RIGGED AND ADJUSTED IAW B1900D, MM 32-30-13, 32-60-01, AND 32-60-01. OPERATIONAL CHECKS WERE GOOD, AIRCRAFT RELEASED FOR SERVICE. (X)

Part: SWITCH — DIRTY (NLG)

CLE - FLT 3242 - CREW REPORTED AFTER LANDING GEAR EXTENSION, NOSE GEAR LIGHT DID NOT ILLUMINATE. THE CREW RECEIVED NO WARNING HORN WITH THE POWER REDUCED OR WITH FLAPS SET AT 35 DEGREES, THE LIGHT TESTED PROPERLY WITH THE PRESS-TO-TEST SWITCH. THE LIGHT DID ILLUMINATE AFTER CYCLING THE LANDING GEAR 3 TIMES. MAINTENANCE INSPECTED AIRCRAFT AND CLEANED NOSE GEAR DOWNLOCK SWITCH, OPERATIONAL CHECKS WERE GOOD IAW B1900D MM 32-30-00. THE ACFT RELEASED FOR SERVICE. (X)

Part: PC BOARD — FAULTED (LANDING GEAR)

CLE - FLT 3102 - CREW REPORTED LANDING GEAR HANDLE WOULD NOT GO INTO RETRACT POSITION WITHOUT USING DOWNLOCK RELEASE BUTTON. MAINTENANCE INSPECTED AND RELEASED ACFT IAW B1900D MEL NR 32-8, CONTROL NR 89516. ON 8-28-96, MAINTENANCE REMOVED AND REPLACED THE PRINTED CIRCUIT BOARD IAW B1900D MM 32-31-01. OPERATIONAL CHECKS WERE GOOD IAW B1900D MM 32-30-00. THE AIRCRAFT WAS REMOVED FROM MEL AND RELEASED FOR SERVICE. (X)

Part: INDICATOR — FAULTED (NLG)

CLE - FLT 3278 - CREW REPORTED WHEN LANDING GEAR WAS EXTENDED, NOSE GEAR LIGHT DID NOT ILLUMINATE. THE CREW CYCLED THE LANDING GEAR TWICE AND THE NOSE GEAR LIGHT ILLUMINATED, ALL OTHER INDICATIONS WERE NORMAL. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LANDING GEAR INDICATOR IAW B1900D MM 32-10-00. OPERATIONAL CHECKS WERE GOOD IAW B1900D MM 32-60-00. AIRCRAFT RELEASED FOR SERVICE. (X)