N4599X

PIPER PA-32-300 · 1975 · 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
STAR MARIANAS AIR INC (1SMA)Operatoron 2019-04-19Operator named in NTSB report

Accident & incident history

Accident · 2019-04-19 Operator named in NTSB report
Piper PA32 No injuries Part 135 — STAR MARIANAS AIR INC

Operated by Star Marianas Air Inc (per NTSB report)

Source: NTSB case GAA19CA268

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.

3 reports on file, 2012-07-16 – 2026-06-15.

FLUID LOSS; FLAME/FIRE · 2026-06-15 Matched by certificate designator
ATA 3240

Part: BRAKE — BURNED (ZONE 700) · airframe 11,503 hrs

DURING TAXI FOLLOWING CONSECUTIVE REJECTED TAKEOFFS, THE AIRCRAFT EXPERIENCED A LANDING GEAR BRAKE FIRE. INVESTIGATION REVEALED THAT THE HEAT GENERATED BY THE CONSECUTIVE ABORTS CAUSED THE CALIPER HYDRAULIC SEAL (P/N: MS28775-222 O-RING) TO MELT AND FAIL. THIS FAILURE ALLOWED HYDRAULIC FLUID TO LEAK DIRECTLY ONTO THE HOT BRAKE DISK. THE FLUID IGNITED UPON CONTACT, RESULTING IN A LOCALIZED FIRE, A LOSS OF LEFT BRAKE PRESSURE, AND THERMAL DAMAGE TO THE LANDING GEAR, WHEEL FAIRING, AND SURROUNDING WING STRUCTURE.

Source: SDR 1SMA20260615001
PARTIAL RPM/PWR LOSS · 2014-07-30 Matched by certificate designator
ATA 7414

Part: MAGNETO — FAULTED (LEFT) · airframe 5,939 hrs

PILOT REPORTED THAT DURING TAKEOFF ROLL, ENGINE DID NOT SEEM TO BE PRODUCING FULL POWER AND WASN'T REACHING MAX RPM. TAKEOFF ABORTED AND DURING TAXI TO TERMINAL, PILOT PERFORMED MAGNETO CHECK AT LOW RPM. DETERMINED THAT ENGINE WOULD NOT RUN WHEN LT MAGNETO WAS SELECTED ON IGNITION SWITCH. VISUAL INSPECTION DID NOT REVEAL ANY OBVIOUS REASON FOR FAILURE. REPLACEMENT OF LT MAGNETO CORRECTED ISSUE. FAULTY MAGNETO BEING SENT FOR TEAR DOWN INSPECTION AND OVERHAUL.

Source: SDR 2014F00138
PARTIAL RPM/PWR LOSS; WARNING INDICATION · 2012-07-16 Matched by certificate designator
ATA 2810

Part: CAP — FAILED (FUEL SYSTEM) · airframe 3,804 hrs

PILOT MADE AN IMMEDIATE RETURN TO AIRPORT AND UNSCHEDULED LANDING AFTER ENCOUNTERING ROUGH RUNNING ENGINE AND PARTIAL LOSS OF RPM AT APPROX 500 FEET AGL, AFTER TAKEOFF, WHILE SETTING CLIMB POWER AND FUEL FLOW. FUEL FLOW INDICATION ERRATIC, FUEL PRESSURE APPEARED NORMAL. ACFT LANDED SAFELY & TAXIED TO BLOCK UNDER ITS OWN POWER. SHORTLY AFTER LANDING ENGINE APPEARED TO BE RUNNING SMOOTHLY AGAIN. ACFT HAD ACCUMULATED 18 HOURS OF FLIGHT TIME OVER PREVIOUS WEEK AND IS REGULARLY FLOWN. INSPECTION OF FUEL STORAGE SYS REVEALED SMALL AMOUNT OF WATER IN SELECTED FUEL TANK (LT TIP TANK), ESTIMATED AT 2-3 TABLESPOONS. INSPECTION OF FUEL CAP ASSEMBLY REVEALED ONE SCREW ATTACHING LOWER METALIC LOCKING PORTION OF CAP ASSEMBLY TO UPPER ASSEMBLY WAS NO LONGER ABLE TO BE SECURED DUE TO STRIPPED THREADS IN UPPER CAP ASSEMBLY. CAP REPLACED WITH A NEW AND ENGINE RAN NORMAL. SEVERAL HIGH SPEED / HIGH POWER GROUND RUNS WERE MADE, WITH ENGINE OPERATING NORMALLY.

Source: SDR 2012F00139