N344AM

Part: BULKHEAD — CRACKED (ZONE 200) · airframe 4,698 hrs · 17,851 cycles

A CRACK WAS DISCOVERED ON THE AFT BULKHEAD CENTER STRUCTURE. THE CRACK MEASURES APPROXIMATELY 1.0 INCH LONG

Part: SCREW — WRONG PART (ZONE 100) · airframe 4,226 hrs · 16,333 cycles

DURING INSTALLATION OF SEAT TRACK RAIL, IT IS NOTED THAT ONE SCREW (PN: 22256BE060018L) IS TOO LONG AND INTERFERES WITH THE STATIONARY COLLECTIVE TUBE FLANGE (PN: 350A27513120).

Part: SEAL — UNSECURE (ENGINE INLET) · airframe 3,711 hrs · 14,519 cycles

CHECKS SHOWED LOSS OF ENGINE POWER AT A HOVER. INSUFFICIENT POWER AVAILABLE TO EVEN EXECUTE A NORMAL TAKEOFF. BLEED AIR VALVE WASN'T CLOSING UNTIL 98% NG AND BURNING SMELL STILL NOTICEABLE. **SUPPLEMENTAL INFORMATION**10-29-2021, FOUND THAT THE REAR INLET BARRIER FILTER RUBBER SEAL HAD CAME UN GLUED FROM ENGINE COWLING.

Part: BLEED VALVE — MALFUNCTIONED (ENGINE) · airframe 3,711 hrs · 14,519 cycles

DURING CRUISE FLIGHT EXPERIENCED A YAW KICK, BURNING RUBBER SMELL AND FLI FAILURE. NO LOSS OF FLIGHT CONTROLS OR OTHER INDICATIONS. PRECAUTIONARY LANDED AT AIRPORT MINUTES LATER. SUBSEQUENT FLIGHT CHECKS SHOWED LOSS OF ENGINE POWER AT A HOVER. INSUFFICIENT POWER AVAILABLE TO EVEN EXECUTE A NORMAL TAKEOFF. BLEED AIR VALVE WASN'T CLOSING UNTIL 98% NG AND BURNING SMELL STILL NOTICEABLE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

CARGO COMPARTMENT SMOKE DETECTOR LIGHT ILLUMINATED INFLIGHT ON APPROACH. DISCHARGED CARGO COMPARTMENT FIRE EXTINGUISHER. REMOVED AND REPLACED CARGO COMPARTMENT SMOKE DETECTOR. REMOVED AND REPLACED CARGO FIRE EXTINGUISHER BOTTLE AND CARTRIDGE. SYSTEM CHECKS GOOD. RETURNED TO SERVICE. (M)

Part: FIRE EXTINGUISHER — DISCHARGED (CARGO BAY)

CARGO COMPARTMENT SMOKE DETECTOR LIGHT ILLUMINATED INFLIGHT. DISCHARGED CARGO COMPARTMENT FIRE EXTINGUISHER. REMOVED AND REPLACED CARGO FIRE EXTINGUISHER BOTTLE AND CARTRIDGE. (M)

Part: BRACKET — CORRODED (AVIONICS RACK)

LOWER AFT AVIONICS RACK 'L' BRACKET CORRODED. REMOVED CORRODED BRACKET, AND REPLACED WITH A NEW BRACKET. (M)

Part: SWIVEL — LEAKING (RT MLG)

ON CLIMB AFTER TAKEOFF, GEAR HANDLE WAS SELECTED UP. HYDRAULIC QTY WENT TO ZERO WITH HYDRAULIC CWP LIGHT. REMOVED AND REPLACED RT HYDRAULIC SWIVEL AND SERVICED HYD SYSTEM. (M)

Part: OIL SYSTEM — REQUIRED SERVICE (RT ENGINE)

ON TAXI, RIGHT HAND ENGINE OIL PRESSURE LIGHT CAME ON. RIGHT HAND ENGINE OIL LEVEL LOW, ADDED ONE QUART OF OIL. RUN-UP CHECKS GOOD. (X)

Part: CONNECTOR — DIRTY (RT ENGINE)

RIGHT HAND INTAKE HEAT INOPERABLE. CYCLING ON CLIMB-OUT. CLEANED OIL OUT OF RIGHT HAND THERMAL CONTROLLER AND LOAD MONITOR CANNON PLUGS. (X)

Part: THERM CONTROLLER — FAILED (RT ENGINE)

RIGHT ENGINE INTAKEOF LIGHT CYCLES ON AND OFF, ABOUT EVERY 5-10 SECONDS. REMOVED AND REPLACED RIGHT THERMAL CONTROLLER. (M)

Part: ITT GAUGE — MALFUNCTIONED (RIGHT)

RIGHT ENGINE ITT FLUX FROM 760 TO 820 DURING CLIMB-OUT BOTH DIGITAL AD ANALOG. CLEANED ALL CANNON PLUGS. SWAPPED GAUGES FOR TROUBLESHOOTING. GROUND RAN A/C, CHECKS GOOD. (M)

Part: AUTO COARSEN — MALFUNCTIONED (E/E COMPT)

AUTO COARSEN CWP ON DURING TAKEOFF. HAD PILOT PERFORM P3 TEST. AUTO COARSEN PASSED TEST. (M)

Part: WEU — FAILED (LEFT)

LEFT PITOT FAILED, INTERMITTENT. REMOVED AND REPLACED WEU. (M)

Part: RELAYS — FAILED (LANDING GEAR)

OAT AND CONFIG LIGHTS ON AFTER TAKEOFF. GEAR WOULD NOT RETRACT. REMOVED AND REPLACD RELAYS 8GA29GA. (M)

Part: RELAYS — FAILED (E/E COMPT)

AFTER TAKEOFF, GEAR WOULD NOT RETRACT. OAT AND CONFIG LIGHT ON. REMOVED AND REPLACED RELAYS. (M)

Part: LINE — FAILED (RIGHT)

INBOUND TO MEMPHIS IT LOST ALL HYD PRESSURE AND QUANTITY, HAD TO EMERGENCY EXTEND GEAR. LINE CREW REPLACED HYD PUMP PRESSURE LINE. (M)

Part: TRANSDUCER — INOP (LT MLG BRAKE)

ANTI-SKID LIGHT ON SHORTLY AFTER TOUCHDOWN, NO BRAKING ACTION WHEN BRAKES ARE APPLIED. PUT PUMP IN OVERRIDE TO GET BRAKING ACTION. REMOVED LEFT OUTBOARD WHEEL SPEED TRANSDUCER IAW AMM. PERFORMED A HIGH SPEED RUN/TAXI. OPS CHECK GOOD. AIRCRAFT FOR SERVICE. (M)

Part: ENGINE — FLAMED OUT (LEFT)

LEFT ENGINE FLAME-OUT. AUTO RE-START, TEMP RISE LEFT SIDE, PLUS 20 DEGREES CELSIUS. NO FURTHER PROBLEM NOTED, OAT MINUS 7 DEGREES CELSIUS, ENGINE ANTI-ICE AND PROPELLER HEAT ON. SUSPECT LEFT ENGINE INGESTED ICE. BRIGHT LIGHT INSPECTED, LEFT ENGINE, STAGE 1 COMPRESSOR BLADES. NO DAMAGE NOTED. PERFORMED GPA RUNS. ALL PARAMETERS WITHIN LIMITS. AIRCRAFT OK FOR SERVICE. (X)