N241JA

PIPER PA-28-181 · 2020 · Valid Registration

Registered owner: HOT WINGS AVIATION LLC, IN (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

O · 2001-03-21 Matched by certificate designator
ATA 7603

LT THROTTLE BINDING WHEN ADVANCED FOR TAKEOFF POWER. FOUND BINDING OF LEFT AFT ENGINE THROTTLE CONTROL DUE TO POSSIBLE EXCESSIVE ROUTING OF CONTROL TO CONFORM TO NACELLE SIZE. REROUTED CONTROL TO INCREASE RADIUS OF BEND INSIDE NACELLE AND CONTROL OPERATED NORMALLY.

Source: SDR 20010411CW006 · FAA SDRS
O · 2001-02-01 Matched by certificate designator
ATA 2130

CABIN COULD NOT MAINTAIN PRESSURIZATION AT FL350, MAINTENANCE PERFORMED A GROUND PRESSURIZATION FUNCTIONAL CHECK NORMALLY. A PNEUMATIC CHECK VALVE DISCOVERED WITH BROKEN SPRING WAS REPLACED, HOWEVER, INITIAL FLIGHT TEST WAS NOT SUCCESSFUL. MAINTENANCE TROUBLESHOT SUSPECTED LOSS OF PRESSURIZED AIR FROM RIGHT ENGINE AND REPLACED NR2 ENGINE FUEL CONTROL TO CORRECT IMPROPER BLEED VALVE SCHEDULING, WHICH RESULTED IN MAINTAINING A NORMAL BLEED AIR SUPPLY. TEST FLIGHT FOR PRESSURIZATION WAS GOOD.

Source: SDR 20010327CW014 · FAA SDRS
O · 2001-01-10 Matched by certificate designator
ATA 2130

AC COULD NOT MAINTAIN PRESSURIZATION AND INCREASE IN CABIN ALTITUDE RESULTED IN OXYGEN MASK DROP AND AURAL WARNINGS, AS APPROPRIATE. AC DESCENDED TO FL220 AND CREW WAS ABLE TO MANUALLY RESTORE CABIN ALTITUDE TO NORMAL. AC CONTINUED FLT TO HOME BASE, NORMALLY. AT SUBMISSION OF M&D REPORT, MALFUNCTION HAS NOT BEEN DETERMINED. 8010-4 WILL BE SUBMITTED ON DISCOVERY CAUSE OF PROBLEM.

Source: SDR 20010213CW009 · FAA SDRS
O · 2001-01-05 Unresolved
ATA 7931

LEFT ENGINE OIL PRESSURE GAGE NOTED TO HAVE DROPPED AND STUCK AT 12 PSI, OIL PRESSURE ON TAXI FOR TAKEOFF. AC WAS RETURNED TO MAINTENANCE AND A SERVICEABLE OIL PRESSURE INDICATOR WAS INSTALLED. OIL PRESSURE INDICATED NORMAL ON RUNUP/FUNCTIONAL CHECK.

Source: SDR 20010213CW008 · FAA SDRS
O · 2000-03-08 Matched by certificate designator
ATA 3244

AIRCRAFT HAD 2 FLAT TIRES AFTER LANDING. ANTI-SKID SYSTEM WAS NON-OPERATIONAL (DEFERRED STATUS) AND POSSIBLE POOR RUNWAY BRAKING CAUSE OF TIRE FAILURE. TIRE AND WHEEL ASSYS (4 EACH) WERE REPLACED. AIRCRAFT RETURNED TO BASE MAINTENANCE AND MADE NORMAL LANDING. (X)

Source: SDR 20001027SH002 · FAA SDRS
O · 1998-06-22 Unresolved
ATA 5510

DISCOVERED SEVERAL SMALL CRACKS INSIDE HORIZONTAL STABILIZER LOCATED AT LEFT AND RIGHT BL 19.40. CRACKS WERE NOTED DURING SCHEDULED INSPECTION OF THE AREA. A REPAIR WAS PERFORMED BY AN FAA CERTIFIED REPAIR STATION, FOLLOWING N.D.T. CONFIRMATION OF THE CRACKS. CRACKS WERE IN THE BULB STRINGER AT THE RIB LOCATED RT BL 19.40

Source: SDR 99ZZZX5 · FAA SDRS