N430MQ
Registered owner: MW CAN DO LLC, WI (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
9 reports on file, 1995-02-10 – 1996-11-27.
Part: TRUNNION LEG — FAILED INSP (RIGHT)
ORD - RIGHT LANDING GEAR FAILED ULTRASOUND INSPECTION OF TRUNNION LEG AS PER MESSIER DOWTY TECHNIQUE A/VT NR 20317/96 (FCD E9-32-002). REPLACED GEAR ASSEMBLY IAW ATR 42 JIC 32-11-00. OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: TRUNNION LEG — FAILED INSP (LEFT)
ORD - LEFT LANDING GEAR FAILED ULTRASOUND INSPECTION OF TRUNNION LEG AS PER MESSIER DOWTY TECHNIQUE A/VT NR 20317/96 (FCD E9-32-002). REPLACED GEAR ASSEMBLY IAW ATR 42 JIC 32-11-00. OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: POWER SUPPLY — FAILED (CABIN)
LAN - FORWARD AND FLOOR EMERGENCY LIGHTS INOP. RAI'D POWER SUPPLY 3WL (2 UNITS) AND 29WL (2 UNITS). AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
LAN - FORWARD AND FLOOR EMERGENCY LIGHTS INOP. RAI'D POWER SUPPLY 3WL (2 UNITS) AND 29WL (2 UNITS). AIRCRAFT WAS RETURNED TO SERVICE. REFERENCE SIMA962781.
Part: BATTERY PACK — DISCHARGED (CABIN)
LAN - FORWARD AND FLOOR EMERGENCY LIGHTS INOP. RAI'D POWER SUPPLY 3WL (2 UNITS) AND 29WL (2 UNITS). AIRCRAFT WAS RETURNED TO SERVICE. REFERENCE SIMA962781.
Part: PROP BRAKE — FAILED (RT ENG)
GRB - FLT NR 4240 - AFTER ENGINE START AND PROP BRAKE ON, PILOT NOTED PROP BRAKE UNLOCK WARNING ON CAP PANEL. UPON VIEWING THE ENGINE CREW NOTED FIRE FROM THE FORWARD ENGINE COWLING AREA. FIRE BOTTLES WERE DISCHARGED AND CFR WAS CALLED TO ENSURE FIRE WAS EXTINGUISHED. MAINTENANCE REMOVED AND DEFERRED THE PROP BRAKE PER MEL PROCEDURES. ENGINE AND COWLS INSPECTED FOR OVERHEAT DAMAGE AND NONE FOUND. AIRCRAFT RETURNED TO SERVICE. (M)
Part: IDLER LEVER — LOOSE BEARING (RT AILERON)
MQT - DURING BRIDGE INSPECTION AND COMPLIANCE OF EO E9-2700-001, MAINTENANCE FOUND THE FIFTH FROM INBOARD IDLER LEVER ON THE RIGHT WING TO HAVE EXCESSIVE PLAY IN THE BEARING. THE IDLER LEVER WAS REMOVED AND INSPECTED AND A FUNCTIONAL CHECK OF THE AILERON SYSTEM WAS COMPLIED WITH IAW EO E9-2700-001. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (W)
Part: BELLCRANK — LACK OF LUBE (LT AILERON)
MQT - DURING BRIDGE INSPECTION AND COMPLIANCE OF EO E9-2700-001, MAINTENANCE FOUND THE INBOARD BELLCRANK ON THE LEFT AILERON TO HAVE A DRY BEARING. THE BELLCRANK WAS REMOVED AND INSPECTED AND A FUNCTIONAL CHECK OF THE AILERON SYSTEM WAS COMPLIED WITH IAW EO E9-2700-001. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (W)
Part: HYD LINE — CHAFED (HYD BAY)
RSW - FLT 3525 - IN-FLIGHT FROM MIA TO RSW, BLUE SYSTEM HYDRAULIC LOW LEVEL INDICATION CAME ON FOLLOWED BY BLUE PUMP LOW PRESS AND LOSS OF BLUE HYD SYSTEM. AIRCRAFT DECLARED EMERGENCY AND MADE ZERO DEGREE FLAP LANDING AT RSW. EMERGENCY EVACUATION WAS NOT REQUIRED, LANDED WITHOUT INCIDENT. MTX INSPECTED AND FOUND PRESSURE LINE FROM BLUE HYD PUMP CHAFED. REPLACED LINE, PERFORMED NECESSARY LEAK CHECKS AND RETURNED AIRCRAFT TO SERVICE. PART TOTAL CYCLES, 15,980. (X)