N198GA

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 39,982 hrs · 52,287 cycles

AIRCRAFT DEPARTED DEN AND SHORTLY AFTER CLIMBOUT, LEVELING OUT AT 10K', THE PILOT BEGAN PULLING BACK POWER AND EXPERIENCED THE RIGHT ENGINE PROPELLER BECAME "JERKY" AND SPORADIC WITHOUT ANT PROPELLER LEVER INPUTS. SOON AFTER, THE RIGHT ENGINE ITT CLIMBED TO 1100C AND THE ENGINE WAS SHUTDOWN> THE PILOT NOTIFIED DEN AND RETURNED TO BASE WITHOUT ANY FURTHER INCIDENTS.

Part: TRIM SYSTEM — MALFUNCTIONED (ELEVATOR) · airframe 39,051 hrs · 51,067 cycles

ELECTRIC ELEVATOR TRIM ACTUATED UN-COMMANDED. THE PILOT PRESSED THE 'TRIM DISCONNECT' BUTTON WHICH STOPPED THE ELECTRIC TRIM OPERATION.

Part: COMPUTER — FAULTY (STALL WARNING) · airframe 38,153 hrs · 49,964 cycles

STALL WARNING HORN SOUNDED CONTINUOUSLY FROM THE TIME THE ACFT TOOK OFF. PILOT ELECTED TO RETURN TO TAKEOFF AIRFIELD FOR AN UNEVENTFUL LANDING. SUBSEQUENT INSPECTION REVEALED THE LIFT DETECTOR COMPUTER WAS FAULTY.

Part: TERMINAL — CORRODED (CIRCUIT BREAKER) · airframe 38,142 hrs · 49,951 cycles

AFTER TAKEOFF, WHEN GEAR SELECTED UP, THEY FAILED TO RETRACT. PILOT RETURNED TO TAKEOFF AIRFIELD FOR UNEVENTFUL LANDING. SUBSEQUENT INSPECTION FOUND THE LG POWER CB POPPED & CORROSION ON THE CB TERMINALS.

Part: SKIN — DEBONDED (LT WING) · airframe 37,091 hrs · 48,928 cycles

LEFT WING DEBOND. UPPER SKIN OF BONDED PANEL IN AREA AROUND FUEL BAY ACCESS OVAL PANEL DEBONDED FROM FUEL ACCESS DISH & HONEYCOMB CORE.

Part: ANGLE — CRACKED (NACELLE)

ANGLE LOCATED ABOVE THE ICE DOOR HINGE, THIS ANGLE HOLDS THE LOWER FIRE SEAL BULKHEAD. WHEN THIS ANGLE CRACKS, IT ALLOWS THE OUTSIDE COWL RIVETS TO WORK LOOSE, AND THIS CAUSES THE COWL SIDE SKIN TO CRACK. (M)

Part: PANEL — SHORTED (COCKPIT)

FLT 9449 - RSW-TPA - DURING TAXI, HEARD AND SAW ELECTRICAL ARC ON MAIN CIRCUIT BREAKER PANEL, THERE WAS A SMELL OF ELECTRICAL SMOKE. REMOVED AND REPLACED LUMINESCENT PANEL IAW BEECHCRAFT MM CHAP 33. OPERATIONAL CHECK NORMAL. (M)

Part: CABLE — BROKEN (PAX DOOR)

MIA/MCO - FLT 9380 - FORWARD CABIN DOOR WILL NOT OPEN WHEN HANDLE IS ROTATED. REMOVED AND REPLACED BROKEN DOOR CABLE.

Part: BRACKET — CORRODED (LT ELEVATOR)

AT SCHEDULED EMPENNAGE INSPECTION, DETERMINED LEFT ELEVATOR OUTBOARD AND CENTER HINGE ATTACH BRACKETS TO HAVE INTERGRANULAR CORROSION. REMOVE AND REPLACED OUTBOARD AND CENTER HINGE, ATTACH BRACKETS. (M)

Part: SPAR CAP — CORRODED (LT ELEVATOR)

AT SCHEDULED EMPENNAGE INSPECTION DETERMINED LEFT ELEVATOR UPPER AND LOWER SPAR CAPS TO HAVE INTERGRANULAR CORROSION THE LAST FOUR INCHES OUTBOARD. REPLACED LEFT ELEVATOR UPPER AND LOWER SPAR CAPS, P/N'S 101-920014-45, AND 101-620014-47. (M)

Part: SPAR CAP — CORRODED (LT ELEVATOR)

AT SCHEDULED, EMPENNAGE INSPECTION DETERMINED LEFT ELEVATOR UPPER AND LOWER SPAR CAPS TO HAVE INTERGRANULAR CORROSION THE LAST FOUR INCHES OUTBOARD. REPLACED LEFT ELEVATOR UPPER AND LOWER SPAR CAPS PART NR 'S 101-920014-45, AND 101-620014-47. (M)

Part: HINGE — CORRODED (LT ELEVATOR)

AT SCHEDULED EMPENNAGE INSPECTION DETERMINED LEFT ELEVATOR, OUTBOARD AND CENTER HINGE ATTACH BRACKETS TO HAVE INTERGRANULAR CORROSION. REMOVED AND REPLACED OUTBOARD AND CENTER HINGE, ATTACH BRACKETS. (M)

Part: CIRCUIT BOARD — DAMAGED (LANDING GEAR)

FLT 7299 - NAS-MIA - WHILE IN FLIGHT, LANDING GEAR HANDLE WOULD NOT EXTEND GEAR. EXTENDED GEAR MANUALLY. A/C LANDED SAFELY. REMOVED AND REPLACED PRINTED CIRCUIT BOARD. (M)

Part: CIRCUIT BOARD — FAILED (LANDING GEAR)

FLT 7383 - MIA-MCO - CIRCUIT BREAKER POPPED AND WOULD NOT RESET. GEAR WAS MANUALLY EXTENDED. SECURED PRINTED CIRCUIT BOARD, E173, CONNECTOR. SYSTEM CHECED GOOD ON JACKS. (M)

Part: UPLOCK SWITCH — OUT OF ADJUST (LT MLG)

FLT 7251 - MCO-EYW - ON APPROACH INTO EYW, WITH GEAR HANDLE DOWN. CIRCUIT BREAKER POPPED WOULD NOT RESET. DIVERTED TO MIA AND MANUALLY EXTENDED GEAR. AIRCRAFT LANDED SAFELY. ADJUSTED LEFT UPLOCK SWITCH. SYSTEM CHECKED GOOD ON JACKS. (M)

Part: ENGINE — FAILED (RIGHT)

MIA/NAS - FLT 7156 - RIGHT ENGINE QUIT ON CLIMB-OUT. REMOVED AND REPLACED RIGHT ENGINE. (X)

Part: FIRE LOOP — OUT OF POSITION (RT ENGINE)

FLT 7485 - NAS-FLL - RIGHT FIREWALL FUEL VALVE HANDLE ILLUMINATED FOR ABOUT 20 SECONDS AND EXTINGUISHED AT IDLE DURING TAXI. REPOSITIONED RIGHT ENGINE FIRE LOOP TO PROPER POSITION. PERFORMED OPERATIONAL CHECK OF THE SYSTEM WITH TEST SWITCH. (M)

Part: SWITCH WIRE — LOOSE (LT POWER LEVER)

FLT 396 - MCO/MIA - GEAR HORN AND HANDLE LIGHT WILL NOT ILLUMINATE WHEN POWER LEVERS ARE RETARDED OR FLAPS ARE LOWERED PAST APPROACH. SECURED WIRE AT LEFT POWER LEVER MICROSWITCH WITH AIRCRAFT ON JACKS. CYCLED GEAR SEVERAL TIMES. NO DEFECTS NOTED. (M)

Part: O-RING — PINCHED (LT ENGINE)

FLT - 477 - FLL/NAS - LEFT ENGINE LOST OIL PRESSURE THEN THE ENGINE SHUTDOWN ITSELF. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO MIA AND LANDED WITHOUT INCIDENT. INSPECTED AND DETERMINED THAT THE LEFT OIL FILTER COVER O-RING WAS PINCHED ALLOWING LEAKAGE. REMOVED AND REPLACED O-RING. LEAK CHECK AND POWER ASSURANCE RUNS GOOD. AIRCRAFT RELEASED TO SERVICE.

Part: WIRE — CHAFED (GEAR INDICATION)

FLT 169 - TPA-MIA - LANDING GEAR INDICATION CIRCUIT BREAKER POPS DURING RETRACTION CYCLED ONLY. REPAIRED CHAFED WIRE UNDER CENTER FLOOR AT PLUG P313. OPS CHECK GOOD ON GEAR SWINGS, OPS CHECK GOOD ON TEST FLIGHT. (M)

Part: SKIN — CRACKED (RT WING)

AT SCHEDULED INSPECTION, THE RIGHT UPPER WING SKIN WAS DETERMINED TO BE CRACKED, ZONE 632. REMOVED DAMAGED AREA, INSTALLED FILLER DOUBLER IAW BEECH SRM CHAPTER 51-70-00, FIGURE 15. (M)

Part: SKIN — CRACKED (LT WING)

AT SCHEDULED INSPECTION, THE LEFT UPPER WING SKIN CRACKED, ZONE 532. REMOVED DAMAGED AREA, INSTALLED FILLER AND DOUBLER IAW BEECH SRM 51-70-00, FIGURE 15. (M)

Part: OIL SYST — OVER SERVICED (RT ENGINE)

MIA-ELH - FLT 465 - SMOKE IN CABIN, AC RETURNED TO MIA WITHOUT FURTHER INCIDENT. DETERMINED RT ENGINE TO BE OVER SERVICED. DRAINED OIL TO PROPER LEVEL. AC WAS TEST FLOWN WITH SATISFACTORY RESULTS AND RELEASED FOR SERVICE.

Part: BREAKER — TRIPPED (MLG)

FLT 487A - MCO-MIA - LANDING GEAR CIRCUIT BREAKER POPPED ON RETRACT OUT OF MCO. TROUBLE SHOT SYSTEM WIRING. PERFORMED SEVERAL GEAR SWINGS. OPS CHECK GOOD, COULD NOT DUPLICATE.