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N292PA

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2002 Piper PA-44-180 · Lycoming O-360 series

Open in FAA registry

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Registered owner
Skywest Leasing Inc
Location
St George, UT
Owner type
Corporation
Serial number
4496116
Year built
2002
Type
Fixed wing multi engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
February 19, 2002
Certificate issued
July 7, 2025
Expires
July 31, 2032
Mode S code
A2FE2E
Piper PA-44-180Airframe model · 4 seats · 2 engines · 558 registeredTCDS A19SOAirframe · Piper PA-44-180TCDS E-286Engine · Lycoming O-360 series

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming O-360 model are included below.

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Airworthiness directives that may apply · 65

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1963In forceSuperseded2026
See all 73 ADs

Information bulletins that may apply · 21

Advisory, not mandatory.

See all 30 bulletins

NTSB investigations

No NTSB investigations matched to N292PAMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Piper PA-44-180 aircraft

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Incident 20200304001549ITakeoff: Departure Roll · Deer Valley, AZStarted takeoff roll at charlie 3. Began simulated engine failure prior to VMC.takeoff was normal takeoff. Flight instructor simulated engine failure with RH mixture. Approximately 5 knots when initiated. Reduced mixture slowly. Student recognized asymmetric…Mar 4, 2020 · Minor damage

Service difficulty reports · 9

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR FQAR20200430001Strut · crackedDURING THE TAKEOFF ROLL AFTER A SIMULATED ENGINE FAILURE ON TAKEOFF, THE LEFT GEAR FAILED WHERE THE STRUT TUBE IS ATTACHED TO THE LOWER STRUT CASTING,CAUSING THE LOWER GEAR ASSEMBLY TO BREAK AWAY, BREAKING THE TORQUE LINK AT THE MIDDLE BOLT, CAUSING THE PLANE Mar 4, 2020 · N292PA · Piper PA44180 · Main Landing Gear Strut/Axle/TruckSDR FQAR20190821011Stiffener · crackedHAVE SEEN A NUMBER OF AILERONS CRACK WHILE IN SERVICE, CRACKS SEEM TO HAPPEN MOSTLY AT THE 5TH AND 6TH STIFFENING FLUTE. DURING PREVIOUS REPAIRS WE NOTED THAT PIPER CHANGED THE DESIGN OF THE LOWER SKIN IN THAT THE 6TH FLUTE WAS SHORTER THAN IN PREVIOUS VERSIONAug 21, 2019 · N292PA · Piper PA44180 · AileronsSDR FQAR20180206006Bracket · crackedDURING ROUTINE INSPECTION A BRACKET IN THE NOSE COMPARTMENT WAS FOUND CRACKED. BRACKET IS LOCATED AGAINST AFT NOSE FIREWALL AT TOP OF COMPARTMENT AND JOINS UPPER NOSE STRINGER TO FIREWALL.Jan 24, 2018 · N292PA · Piper PA44180 · Fuselage Miscellaneous StructureSDR FQAR20160504021Push-Pull Cable · disconnectedDURING PREFLIGHT ENGINE RUN UP, THE PILOT NOTED THE CARB HEAT FOR THE RT ENGINE WAS INOPERATIVE. TECHS FOUND THAT THE CARB HEAT CABLE HAD SNAPPED AT THE AIR BOX. CABLE SNAPPED AT SWAGE WHERE CABLE MEETS ROD END. CABLE HAD BEEN IN SERVICE 1 YEAR. THE DESIGN OFMay 4, 2016 · N292PA · Piper PA44180 · Air Intake Anti/De-Ice SystemSDR FQAR20160307010Doubler · crackedDURING INSPECTION, A BULKHEAD DOUBLER IN THE EMPENNAGE WAS FOUND CRACKED. THE DEFECT WAS VISIBLE BY REMOVING A FAIRING THAT JOINS THE EMPENNAGE AND VERTICAL FIN AND LOOKING UP AND AFT. THE DOUBLER HAD 2 CRACKS; 1 TO THE SIDE OF THE UPPER, 2ND FROM RIGHT MOSTMar 7, 2016 · N292PA · Piper PA44180 · Fuselage Main, BulkheadSDR FQAR20150512033Downlock Switch · separatedON APPROACH, AS THE GEAR WAS LOWERED THE PILOTS NOTED THERE WAS NO DOWN-AND-LOCKED INDICATION FOR THE RT MAIN GEAR. THE PILOTS ABORTED THE APPROACH AND RAN CHECKLISTS TO GET A POSITIVE GEAR INDICATION WITH NO SUCCESS. THEY WERE ABLE TO PERFORM AN UNEVENTFUL May 11, 2015 · N292PA · Piper PA44180 · Landing Gear Position and WarningSDR FQAR20150402025Throttle Cable · jammedON CLIMB, WHEN THE PILOTS ATTEMPTED TO REDUCE POWER TO CRUISE SETTING, THE LT ENGINE THROTTLE BECAME JAMMED AT FULL POWER. THE PILOTS DECIDED TO RETURN TO THE AIRPORT. THEY WERE FORCED TO SHUTDOWN THE ENGINE TO ALLOW THE ACFT TO LAND. INSPECTION REVEALED THApr 1, 2015 · N292PA · Piper PA44180 · Power LeverSDR 2009FA0000997Wire Harness · brokenLT MLG WIRING HARNESS WIRES ON DOWN LOCK SWITCH BROKE AT SWITCH CAUSING AN INDICATION OF UNSAFE GEAR.Dec 1, 2009 · N292PA · Piper PA44180 · Landing Gear System WiringSDR 2009FA0000996Wire Harness · brokenLT MLG WIRING HARNESS WIRES ON DOWN LOCK SWITCH BROKE AT SWITCH CAUSING AN INDICATION OF UNSAFE GEAR.Dec 1, 2009 · N292PA · Piper PA44180 · Landing Gear System Wiring

STCs that may be installed · 249

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 249 STCs