N69549

Part: TRUSS — DAMAGED (ENGINE) · airframe 31,311 hrs · 37,315 cycles

REPORT: DURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS TUBE DAMAGED. PERFORMED ENGINE TRUSS REPAIR IN ACCORDANCE WITH FAA APPROVED DATA CONTAINED IN DRAWING 1005272-7, 8110-3, DERT-510208-CE.

Part: SKIN — CORRODED (RT WING) · airframe 31,714 hrs · 39,551 cycles

REPORT: DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RIGHT WING UPPER SKIN TRAILING EDGE CORROSION AND DEBOND INBOARD OF WING STATION 209.97 DAMAGE 5/16 X 1/8 HOLE. REMOVED DAMAGED SKIN AND INSTALLED AN EXTERNAL REPAIR DOUBLER.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 31,686 hrs · 37,737 cycles

FLIGHT: 9180 EYW/TPA PILOT REPORTED LANDING GEAR WILL NOT RETRACT RETURNED EYW LANDED WITHOUT INCIDENT. UNABLE TO DUPLICATE OPERATIONAL CHECK NORMAL.

Part: TRUSS — CRACKED (RT ENGINE) · airframe 31,389 hrs · 37,400 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 POINT WELD AREA.

Part: STRINGER — CRACKED (VERTICAL STAB) · airframe 31,149 hrs · 37,115 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED VERTICAL STAB RT SIDE APPEARS TO HAVE CRACKS AT EACH OF THE 3 CHORD STRINGERS AT CSS 54.026. STOP DRILLED CRACKS AND INSTALLED REPAIR STRAPS THREE EACH.

Part: RIB — CRACKED (VERT STABILIZER) · airframe 31,149 hrs · 37,115 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED VERTICAL STABILIZER LT SIDE, 1 CRACK AT CSS 54.026. STOP DRILLED CRACK AND INSTALLED REPAIR STRAP.

Part: RELAY — SHORTED (MLG) · airframe 31,099 hrs · 37,059 cycles

PILOT REPORTED LANDING GEAR WILL NOT RETRACT. CONTINUED, LANDED WITHOUT INCIDENT. REPLACED K3 RELAY LANDING GEAR OPS CHECK GOOD.

Part: CONTROL CABLE — BROKEN (PAX DOOR) · airframe 30,833 hrs · 36,751 cycles

PILOT REPORTED LT CABLE ON AIRSTAIR DOOR BROKEN. REPLACED FWD LOWER CABLE CONTROL ASSY OPS CHECK NORMAL.

Part: CABLE — BROKEN (PAX DOOR) · airframe 30,833 hrs · 36,751 cycles

PILOT REPORTED RT CABLE ON AIRSTAIR DOOR BROKEN. REPLACED RT AIRSTAIR DOOR CABLE ASSY.

Part: HAND RAIL — OUT OF POSITION (PAX DOOR) · airframe 29,750 hrs · 35,510 cycles

FLIGHT 9174 PILOT REPORTED DURING PREFLIGHT FOUND CABIN DOOR HARD TO OPEN. REPOSITIONED CABIN DOOR TOP HANDRAIL CABLE OPERATIONAL CHECKED GOOD.

Part: DOOR — BINDING (MAIN PAX) · airframe 29,690 hrs · 35,445 cycles

PILOT REPORTED CABIN DOOR DIFFICULT TO OPEN. CLEANED EXCESS GREASE FROM LOCKING MECHANISM, OPS CK GOOD.

Part: CABLE ASSY — FRAYED (AIRSTAIR DOOR) · airframe 29,679 hrs · 35,432 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED AIRSTAIR DOOR LWR FWD CABLE FRAYED. REPLACED AIRSTAIR DOOR LOWER FWD CABLE.

Part: ALTIMETER — INTERMITTENT (COCKPIT) · airframe 29,549 hrs · 32,298 cycles

CAPT'S ALTIMETER WORKING INTERMITTENTLY THROUGHOUT CLIMB. R & R CAPTAIN'S ALTIMETER. OPS CHECKS SATISFACTORY AT THIS TIME.

Part: INDICATOR — INOPERATIVE (MLG) · airframe 29,409 hrs · 35,148 cycles

PILOT REPORTED "HH" LANDING GEAR ANNUNCIATOR INOPERATIVE. REPLACED LANDING GEAR INDICATOR ASSY, OPS CHECK GOOD.

Part: SKIN — CORRODED (LT WING) · airframe 29,327 hrs · 35,057 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED LT WING T/E BY THE NR 1 FLAP, 2 SPOTS OF SURFACE CORROSION. DURING CLEANING OF SURFACE CORROSION DISCOVERED UPPER WING SKIN CORROSION BETWEEN LWS 136 THROUGH 196. REMOVED DAMAGED SKIN AND INSTALLED AN EXTERNAL REPAIR DOUBLER.

Part: STRINGER — CORRODED (LT WING) · airframe 28,695 hrs · 34,388 cycles

DURING REMOVAL OF MINOR CORROSION FROM LT WING COLLECTOR TANK J STRINGER, DISCOVERED CORROSION OUT OF LIMITS BETWEEN WS 114.25 TO WS 124.25. REMOVED CORROSION AND INSTALLED EXTERNAL REPAIR STRAP.

Part: SKIN — CORRODED (BS 243-258.2) · airframe 28,695 hrs · 34,388 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED CORROSION ON ACFT BELLY SKIN AT FS 243.280 TO 258.280. REMOVED DAMAGED SKIN AND INSTALLED AN EXTERNAL DOUBLER REPAIR.

Part: SPAR — CORRODED (LT WING) · airframe 28,695 hrs · 34,388 cycles

DURING SCHEDULED LT WING X-RAY INSP, DISCOVERED SURFACE CORROSION ON MAIN SPAR AFT FLANGE BETWEEN WS 114.25 TO 124.25. REMOVED CORROSION AND INSTALLED AN INTERNAL REPAIR STRAP AND EXTERNAL DOUBLER REPAIR.

Part: STRINGER — CORRODED (RT WING) · airframe 28,695 hrs · 34,388 cycles

DURING SCHEDULED RT WING X-RAY INSP, DISCOVERED SPOTS OF CORROSION ON FWD BONDED STRINGER OTBD OF WS 124.25. REMOVED CORROSION AND INSTALLED AN EXTERNAL REPAIR STRAP.

Part: SKIN — CORRODED (RT WING) · airframe 28,695 hrs · 34,388 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED RT WING UPPER SKIN T/E CORROSION AND DEBOND BETWEEN WS 133.86 TO WS 173.50. REMOVED DAMAGE AND INSTALLED EXTERNAL DOUBLER REPAIR.

Part: LATCH — DAMAGED (AIRSTAIR DOOR) · airframe 28,471 hrs · 34,147 cycles

PILOT REPORTED AIRSTAIR DOOR ONCE CLOSED, LATCH DIFFICULT TO TURN AND LOCK. RIGGED LATCH POST. OPS CHECK GOOD.

Part: HINGE — DAMAGED (AIRSTAIR DOOR) · airframe 28,468 hrs · 34,145 cycles

PILOT REPORTED WHEN CLOSING MAIN CABIN DOOR, UPPER LT CAM LOCK SCRAPES AGAINST LOCK. REPLACED AIRSTAIR DOOR TOP AND BOTTOM HINGES.

Part: DOOR — OUT OF ADJUST (MAIN PAX) · airframe 28,458 hrs · 34,135 cycles

PILOT REPORTED CABIN DOOR VERY HARD TO CLOSE. LUBRICATED CAMS AND REPOSITIONED DOOR CABLES. OPS CHECK GOOD.

Part: ACCESS PANEL — LEAKING (RT WING) · airframe 28,269 hrs · 33,917 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED RT WING COLLECTOR TANK FUEL ACCESS PANEL 632 AT, FUEL LEAK. FABRICATED AND INSTALLED EXTERNAL DOUBLER RING FOR RT UPPER WING FUEL ACCESS PANEL 632 AT.

Part: HORN — CORRODED (LT ELEVATOR) · airframe 28,083 hrs · 33,713 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED LT ELEVATOR TRIM TAB INBD CONTROL HORN EXFOLIATED. REPLACED LT ELEVATOR TRIM TAB ASSY.

Part: TORQUE TUBE — CORRODED (LT ELEVATOR) · airframe 28,083 hrs · 33,713 cycles

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

Part: UNKNOWN — ODOR (CABIN) · airframe 27,963 hrs · 33,582 cycles

AFTER TAKEOFF WHEN BLEED AIR VALVES TURNED TO OPEN BURNING ODOR FROM PANEL VENTS WAS DETECTED. PERFORMED ENGINE RUN AT TAKEOFF AND CRUISE POWER SETTINGS OPENED BOTH BLEEDS NO BURNING ODOR OR SMOKE PRESENT.

Part: CABLE ASSY — FRAYED (AIRSTAIR) · airframe 27,035 hrs · 32,592 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED AIRSTAIR DOOR COUNTER BALANCE CABLE ASSEMBLY FRAYED. REPLACED AIRSTAIR DOOR COUNTER BALANCE CABLE ASSY.

Part: DOOR — STIFF (EMERGENCY EXIT) · airframe 26,838 hrs · 32,411 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED RT AFT EMERGENCY EXIT DOOR DIFFICULT TO OPEN. LUBRICATED RT AFT EMERGENCY EXIT DOOR INTERIOR LOCKING MECHANISM.

Part: DAMPENER — CRACKED (ASD) · airframe 26,085 hrs · 31,648 cycles

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED AIRSTAIR DOOR COUNTER BALANCE SUPPORT ASSEMBLY DAMPENER CRACK. REPLACED AIRSTAIR DOOR COUNTER BALANCE UPPER SUPPORT ASSEMBLY DAMPENER.

Part: LOCK — LACK OF LUBE (EMERGENCY EXIT) · airframe 26,085 hrs · 31,648 cycles

AT SCHEDULED ROUTINE MAINT DISCOVERED LT AFT EMERGENCY EXIT FROZEN AND WILL NOT OPEN. APPLIED LUBRICANT TO LT AFT EMERGENCY EXIT LOCKING ASSY. OPS CHECK NORMAL.

Part: LOCK — LACK OF LUBE (EMERGENCY EXIT) · airframe 26,085 hrs · 31,648 cycles

AT SCHEDULED ROUTINE MAINT, DISCOVERED RT AFT EMERGENCY EXIT FROZEN AND WILL NOT OPEN, APPLIED LUBRICANT TO RT AFT EMERGENCY EXIT LOCKING ASSY. OPERATIONAL CHECK NORMAL.

Part: RELAY — FAILED (LANDING GEAR)

FLIGHT 9132 MIA/TPA PILOT DISCREPANCY. DURING APPROACH WHEN LANDING GEAR CONTROL SELECTED DOWN CIRCUIT BREAKER POPPED. HAD TO RESET SEVERAL TIMES BEFORE ALL GEAR CAME DOWN AND LOCKED 3 GREEN. C/A REPLACED LANDING GEAR RELAY. OPS CHECK NORMAL. TEST FLIGHT SATISFACTORY.

Part: CIRCUIT BREAKER — POPPED (COCKPIT)

FLIGHT 9130 FPO/FLL PILOT DISCREPANCY DURING APPROACH, WHEN LANDING GEAR HANDLE SELECTED DOWN THE LANDING GEAR CIRCUIT BREAKER POPPED. RESET THE CIRCUIT BREAKER AND THE LANDING GEAR EXTENDED NORMALLY. C/A TROUBLE SHOT LANDING GEAR SYSTEM. NO DEFECTS NOTED. SERVICED HYDRAULIC FLUID TO CORRECT LEVEL. LANDING GEAR OPS CHECK NORMAL.

Part: HINGE BRACKET — CORRODED (ELEVATOR)

AT SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT OUTBOARD ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED RT OUTBOARD ELEVATOR HINGE BRACKET. (S)

Part: HINGE BRACKET — CORRODED (LT ELEVATOR)

AT SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT INBOARD ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED LT INBOARD ELEVATOR HINGE BRACKET. (S)

Part: HINGE BRACKET — CORRODED (LT ELEVATOR)

AT SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT CENTER ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED LT CENTER ELEVATOR HINGE BRACKET. (S)

Part: VALVE — INTERMITTENT (MLG) · airframe 24,124 hrs · 29,398 cycles

FLIGHT: 9276 EYW/FLL AFTER TAKEOFF THE LANDING GEAR REQUIRED RECYCLING FOUR TIMES TO RETRACT. REPLACED THE LANDING GEAR SERVICE VALVE. LANDING GEAR OPERATIONAL CHECK NORMAL.

Part: CONTROL HANDLE — INTERMITTENT (MLG) · airframe 24,122 hrs · 29,394 cycles

FLIGHT: 9131, AFTER TAKEOFF LANDING GEAR DID NOT RETRACT WHEN LANDING GEAR SELECTED UP. RETURNED TO TPA. LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR CONTROL HANDLE . LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHECK NORMAL.

Part: VALVE — MISRIGGED (MLG) · airframe 24,088 hrs · 29,355 cycles

FLIGHT: 9279 DURING APPROACH, LANDING GEAR WOULD NOT EXTEND. MANUALLY EXTENDED LANDING GEAR. LANDED WITHOUT INCIDENT. FOUND LANDING GEAR GROUND SERVICE VALVE IN THE UP POSITION PLACED IN THE DOWN POSITION. LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHECK GOOD.

Part: SQUAT SWITCH — OUT OF ADJUST (RT MLG) · airframe 24,082 hrs · 29,347 cycles

FLIGHT: 9128 AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. RETURNED TO DEPARTURE. LANDED WITH OUT INCIDENT. READJUSTED RT MAIN LANDING GEAR SQUAT SWITCH.

Part: HANDLE — FAILED (MLG) · airframe 23,826 hrs · 29,050 cycles

DURING APPROACH LANDING GEAR DID NOT EXTEND ON THE FIRST AND SECOND SELECTION OF THE GEAR SELECTOR KNOB TO THE DOWN POSITION. RETURNED TO FLL LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR HANDLE. OPERATIONAL CHECK NORMAL.

Part: RELAY — FAILED (MLG) · airframe 23,816 hrs · 29,036 cycles

AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. REPLACED MLG RELAY, COULD NOT DUPLICATE OPERATIONAL CHECK NORMAL.

Part: UNKNOWN — UNKNOWN (LANDING GEAR) · airframe 23,680 hrs · 28,873 cycles

DURING APPROACH LANDING, GEAR WOULD NOT EXTEND WHEN GEAR HANDLE SELECTED DOWN, DIVERTED. MANUALLY EXTENDED LANDING GEAR. LANDED WITHOUT INCIDENT. TROUBLESHOT SYSTEM COULD NOT DUPLICATE OPERATIONAL CHECK NORMAL.

Part: UNKNOWN — UNKNOWN (LANDING GEAR) · airframe 23,468 hrs · 28,624 cycles

DURING APPROACH LANDING GEAR WOULD NOT EXTEND WITH THE GEAR HANDLE DOWN, CYCLED LANDING GEAR AND THE RT GEAR EXTENDED PARTIALLY THEN 10 SECONDS LATER ALL GEARS EXTENDED. INSPECTED LANDING GEAR SYSTEM NO DEFECTS NOTED. LANDING GEAR OPERATIONAL TEST NORMAL. TEST FLIGHT SATISFACTORY.

Part: HINGE BRACKET — CORRODED (LT STABILIZER) · airframe 22,873 hrs · 27,919 cycles

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

Part: SPAR CAP — DAMAGED (RT WING) · airframe 21,314 hrs · 26,138 cycles

RT WING REAR SPAR LOWER CAP AFT FLANGE DEFLECTED .046 INCHES UPWARD. LOCATED AT WS 104.50. HAND FORMED SPAR FLANGE BACK TO ORIGINAL PROFILE, PERFORMED NDT EDDY CURRENT INSP BY A QUALIFIED LEVEL III INSPECTOR NO CRACK INDICATIONS NOTED. FABRICATED AND INSTALLED SHIM AND STRAP IAW FAA APPROVED DATA.

Part: SPAR CAP — DAMAGED (RT WING)

FLIGHT: 9137 SAQ/FLL RT LANDING GEAR COLLAPSE BACKWARDS ON LANDING FOUND RT WING REAR SPAR LOWER CAP AFT FLANGE DEFLECTED .046 INCHES UP. HAND FORMED SPAR FLANGE BACK TO ORIGINAL PROFILE PERFORMED NDT EDDY CURRENT INSPECTION BY A QUALIFIED LEVEL III INSPECTOR NO CRACK INDICATIONS NOTED. REPAIRED SPAR IAW FAA APPROVED DATA CONTAINED IN FIELD REPAIR FR-CO-01354 REV 1.

Part: BOLT — BROKEN (RT MLG)

FLIGHT: 9137 SAQ/FLL DURING APPROACH RT MLG UNSAFE INDICATION. RT LANDING GEAR COLLAPSE BACKWARDS ON LANDING. FOUND RT MLG DRAG BRACE ATTACH BOLT BROKEN.

Part: HINGE BRACKET — CORRODED (VERT STABILIZER)

AT SCHEDULED MAINTENANCE, DETERMINED VERTICAL STABILIZER LOWER HINGE BRACKET TO BE EXFOLIATED. REPLACED VERTICAL STABILIZER LOWER HINGE BRACKET. (K)

Part: WIRE — LOOSE (EXTINGUISHER)

DURING FLIGHT, RT ENGINE FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATED. SECURED FIRE EXTINGUISHER SQUIB WIRES IN RT WHEEL WELL. (SO29200508218) (K)

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 (ELEVATOR)

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

Part: BRACKET — CORRODED (ELEVATOR)

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

Part: TRUSS — CRACKED (ENGINE)

AT SCHEDULED MAGNUFLUX INSPECTION, ENGINE TRUSS WAS DETERMINED TO HAVE A RADIAL CRACK IN THE LOWER RIGHT GUIDE PIN RADIUS. RAYTHEON AIRCRAFT COMPANY, THE MANUFACTURER, DETERMINED THAT THE BOSS GUIDE WAS NOT REPAIRABLE AND THAT ITS REPLACEMENT WOULD REQUIRE USE OF THE PRODUCTION JIG. NO REPAIR WAS AUTHORIZED. ENGIEN TRUSS WAS REPLACED WITH SERVICEABLE UNIT. (M)

Part: BLADE — BROKEN (LT ENGINE)

FLT - 9161 - DURNG TAKEOFF, LOUD BANG OCCURRED ON LEFT ENGINE. ABORTED TAKEOFF. SEPARATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT FOUR POWER TURBINE BLADES WERE BROKE OFF AT THE BLADE ROOT. POWER SECTION HAS MAJOR INTERNAL DAMAGE. REPLACED LEFT POWER SECTION MODUEL AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. SUSPECT NR 2 PT BLADE FAILURE. (M)

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 WITH BEECH MAINTENANCE MANUAL.

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 MFG MM.

Part: CIRCUIT BREAKER — FAILED (LANDING GEAR)

FLT 9318 - TCB-FLL - DURING APPROACH, LANDING GEAR WOULD NOT EXTEND. MANUALLY PUMPED LANDING GEAR DOWN. REMOVED AND REPLACED LANDING GEAR SYSTEM HYDRAULIC MOTOR CIRCUIT BREAKER. PERFORMED LANDING GEAR EXTENSION AND RETRACTION. OPERATIONAL CHECK NORMAL. (M)

Part: CONTROL HANDLE — INTERMITTENT (COCKPIT)

FLT 9159 - NAS/FLL - DURING APPROACH, LANDING GEAR WOULD NOT EXTEND ON FIRST TRY. EXTENDED ON SECOND ATTEMPT. REMOVED AND REPLACED LANDING GEAR SELECTOR. PERFORMED LANDING GEAR EXTENSION AND RETRACTION. OPERATIONAL CHECK NORMAL. (M)

Part: ACTUATOR — OUT OF ADJ

CLE FLT.#3032 THE CREW REPORTED LANDING GEAR RED UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION.MAINTENANCE ADJUSTED NOSE LANDING GEAR ACTUATOR. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: TRANSMITTER — ERRATIC (LT ENGINE)

CLE THE CREW REPORTED NR 1 FUEL FLOW GAUGE FLUCTUATES. MAINTENANCE REPLACED THE NR 1 ENGINE FUEL FLOW TRANSMITTER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LAMP — BURNED OUT (COCKPIT)

CLE FLIGHT# 3196 THE CREW REPORTED THE UPPER RED LIGHT ON GEAR HANDLE WAS INOPERATIVE.MAINTENANCE REPLACED THE UPPER LAMP ON THE GEAR HANDLE.OPERATIONAL CHECKS WERE GOOD.

Part: BLOWER — FAULTY (CABIN)

CLE FLIGHT 3236 THE CREW REPORTED A STRONG ODOR THROUGHOUT THE CABIN. MAINTENANCE INSPECTED AND REPLACED THE FORWARD VENT BLOWER. OPERATIONAL CHECKS WERE GOOD.

Part: POWERPACK — FAILED (LT WING)

CLE FLIGHT 3130 THE CREW REPORTED THE GEAR WOULD NOT EXTEND IN FLIGHT. THE GEAR HAD TO BE EXTENED MANUALLY. THE CREW ALSO REPORTED THE HYDRAULIC POWERPACK CIRCUIT BREAKER DID POP. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE HYDRAULIC POWER PACK. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TRANSMITTER — ERRATIC (LT ENGINE)

CLE FLIGHT 3102, THE CREW REPORTED THE NR 1 ENGINE FUEL FLOW INDICATOR WAS ERRATIC DURING FLIGHT. THE FLUX WAS REPORTED BETWEEN 700PPH AND 1000PPH. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE FUEL FLOW TRANSMITTER. OPERATIONAL CHECKS WERE GOOD.

Part: ENGINE — FAILED (NR 1 ENGINE)

LEX - FLT 3108 - THE CREW REPORTED NR 1 ENGINE LOST OIL PRESSURE IN FLIGHT AND THE ENGINE SHUT DOWN. THE AIRCRAFT DIVERTED AND LANDED IN CVG WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE. (M)

Part: PACKING — FAILED (LEFT GEAR)

CREW REPORTED THE CAPTAINS LEFT BRAKE GOES ALL THE WAY TO THE FLOOR WITHOUT STOPPING ACTION. A/C TAXIED TO THE GATE WITHOUT FURTHER INCIDENT.MX INSPECTED AND FOUND THE LEFT INBOARD BRAKE SWIVEL TO BE LEAKING. THE BRAKE SWIVEL WAS REBUILT WITH NEW PACKINGS AND THE SYSTEM WAS BLED IAW BEECHCRAFT MM 32-40-05. A/C WAS RELEASED FOR SERVICE.

Part: MASTER CYLINDER — FAILED (LT BRAKE)

AFTER LANDING THE CREW REPORTED THE CAPTAINS LEFT BRAKE PEDAL HAD NO RESISTANCE. A/C TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MX REMOVED/REPLACED THE CAPTAINS LEFT BRAKE MASTER CYLINDER IAW BEECHCRAFT MM 32-40-06. A/C WAS RELEASED FOR SERVICE.

Part: DUCT — DISCONNECTED (NR 2 ENGINE)

FLT 3130 - AFTER TAKEOFF, THE CREW REPORTED A BURNING SMELL IN COCKPIT (ELECTRICAL). THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. AFTER LANDING THE SMELL DISSIPATED. MAINTENANCE INSPECTED AND FOUND THE NR 2 ENGINE BLEED DUCT ON THE PRECOOLER DISCONNECTED. MAINTENANCE RECONNECTED BLEED DUCT IAW BEECHCRAFT MM 21-11-08. RAN ENGINES AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: ACTUATOR — FAILED (RT MLG)

CLE - FLT 3042 - ON APPROACH, THE CREW SELECTED THE GEAR DOWN AND DID NOT GET THE GREEN INDICATION FOR A DOWN AND LOCKED ON THE RIGHT GEAR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR DOWNLOCK POSITION SWITCH (P/N 404EN1-6)IAW BEECH MM 32-60-02. MAINTENANCE ALSO REMOVED AND REPLACED THE RIGHT MLG ACTUATOR IAW BEECH MM 32-30-10. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE 7/3/00. (M)

Part: SWITCH — FAILED (COCKPIT)

CLE - FLT 3150 - THE CREW REPORTED AFTER TAKEOFF FROM CLEVELAND, THE GEAR HANDLE WOULD NOT MOVE. THE RED DOWN LOCK RELEASE BUTTON WAS DEPRESSED TO MOVE GEAR TO UP POSITION. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE AND PERFORMED OPERATIONAL CHECKS IAW BEECHCRAFT 1900D MM 32-30-00. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: COMPRESSOR — FAILED (RT WING)

CLE - FLT 3377 - THE CREW REPORTED THE SMELL OF SMOKE AND UNUSUAL VIBRATION NOTED AFTER LANDING. THE CREW TURNED OFF THE MODE CONTROLLER AND THE SMELL OF SMOKE AND THE VIBRATION STOPPED. MAINTENANCE INSPECTED AND FOUND THE VCM COMPRESSOR FROZEN. THE AIRCRAFT WAS RELEASED IAW MEL 21-1. MAINTENANCE REPLACED THE VCM COMPRESSOR IAW 1900D MAINTENANCE MANUAL 21-52-02. THE FUNCTIONAL CHECKS WERE GOOD AND THE MEL WAS REMOVED ON 5/26/00. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: ENGINE — MALFUNCTIONED (RIGHT)

FLT 3173 - THE CREW REPORTED THE RIGHT ENGINE LOST POWER. THE AIRCRAFT RETURNED TO ERI WITHOUT FURTHER INCIDENT. MAINTENANCE RAN THE NR 2 ENGINE, CHECKED ALL ENGINE RIGGING AND PERFORMED ENGINE RUNS. NO DEFECTS WERE NOTED IAW BEECHCRAFT MM 76-10-00. THE AIRCRAFT WAS RELEASED. (M)

Part: BLEED AIR SYSTEM — MALFUNCTIONED (RIGHT)

FWA - FLT 120G - THE CREW REPORTED THAT SMOKE ENTERED THE CABIN IN-FLIGHT DURING SINGLE ENGINE SIMULATION, THE AIRCRAFT RETURNED TO FWA WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE RIGHT ENVIRONMENTAL BLEED AIR SYSTEM ON MEL NR 21-14 CONTROL NR 183678 CAT 'C'. THE AIRCRAFT WAS RELEASED TO SERVICE. (X)

Part: ELT — DAMAGED (FUSELAGE)

IAH - FLT 3910 - THE CREW REPORTED THAT THE ELT REMOTE SWITCH LIGHT WAS ILLUMINATED WITH THE SWITCH IN THE OFF POSITION BUT, THE ELT WAS NOT TRANSMITTING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE ELT CASE TO BE DAMAGED. MAINTENANCE REMOVED AND REPLACED THE ELT IAW B1900 MM 25-60-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: TRUSS — CRACKED (RT ENGINE)

CLE - DURING A SCHEDULED INSPECTION, THE RIGHT HAND ENGINE TRUSS MOUNT WAS FOUND CRACKED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND ENGINE TRUSS MOUNT ASSEMBLY IAW B1900 MM 7120-00. AIRCRAFT RELEASED FOR SERVICE. ACFT TT 2,779.4 HOURS. ACFT TC 3,345. (X)

Part: TRUSS — CRACKED (LT ENGINE)

CLE - DURING A SCHEDULED INSPECTION, THE LEFT HAND ENGINE TRUSS MOUNT WAS FOUND CRACKED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND ENGINE TRUSS MOUNT ASSY IAW B1900 MM 71-20-00. ACFT TT 2,779.4 HOURS. ACFT TC 3,345. (X)