N4254R

PIPER PA-32-300 · 1969 · Fixed-wing single-engine · 1 engine · 6 seats · Valid Registration

Registered owner: STAR MARIANAS AIR INC, MP (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
STAR MARIANAS AIR INC (1SMA)Certificate holder—Matched by certificate designator

Accident & incident history

PIPER PA-32 No injuries Part 91 — operator not named in the NTSB record
Source: NTSB case LAX75OL010

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.

2 reports on file, 2017-07-07 – 2017-10-31.

PARTIAL RPM/PWR LOSS · 2017-10-31 Matched by certificate designator
ATA 7414

Part: MAGNETO — MALFUNCTIONED (ENGINE) · airframe 15,136 hrs

AFTER INITIATING TAKEOFF ROLL BY ADVANCING THROTTLE FULL FORWARD, PILOT NOTED LESS THAN NORMAL POWER AND VERIFIED MAXIMUM RPM ACHIEVED WAS 2000 RPM. PILOT REJECTED TAKEOFF AND RETURNED TO GATE. POST FLIGHT RUN-UP REVEALED ROUGH RUNNING ENGINE ABOVE 1,200 RPM, WHEN IGNITION SWITCH PLACED ON RIGHT HAND MAGNETO ONLY, ENGINE WOULD LOSE SUBSTANTIAL RPM. WITH ONLY LEFT MAGNETO SELECTED ENGINE WOULD RUN NORMALLY.

Source: SDR 1SMA201710310001
OTHER · 2017-07-07 Matched by certificate designator
ATA 7603

Part: JOINT — FAILED (THROTTLE) · airframe 14,876 hrs

AFTER TAKING OFF AND SETTING CLIMB POWER, PILOT NOTED THROTTLE MOVEMENT HAD NO IMPACT ON MANIFOLD PRESSURE SETTING AND HE WAS UNABLE TO CONTROL THE ENGINE POWER WITH THE THROTTLE. UPON DISCOVERY, PILOT DECLARED AN EMERGENCY AND ASKED TO LAND ON A RUNWAY TEMPORARILY CLOSED AS IT WAS LONGER AND THE NECESSARY ENGINE SHUTDOWN. ATC WAS UNABLE TO PROVIDE CLEARANCE TO LAND ON THE CLOSED RUNWAY, SO PILOT OPTED TO CONTINUE FLT TO AIRPORT OF INTENDED DESTINATION 10 MILES SOUTH USING CLIMB POWER AND RPM SETTINGS FOR THE FLIGHT. AFTER LANDING WAS ASSURED, PILOT SHUT THE ENGINE DOWN AND EXECUTED A SAFE LANDING. VISUAL INSPECTION REVEALED A CRACK AROUND THE WELD ON THE THROTTLE JOINT ASSEMBLY WHICH HAD RESULTED IN A COMPLETE DISCONNECTION OF THE THROTTLE CABLE TO FUEL INJECTOR SERVO.

Source: SDR 1SMA201707161