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N436PA

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2001 Piper PA-44-180 · Lycoming O&VO-360 series

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© OpenStreetMap
Registered owner
Bird Acquisition LLC
Location
Phoenix, AZ
Owner type
LLC
Serial number
4496079
Year built
2001
Type
Fixed wing multi engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
September 11, 2001
Certificate issued
October 1, 2007
Expires
September 30, 2028
Mode S code
A53AAE
Piper PA-44-180Airframe model · 4 seats · 2 engines · 558 registeredTCDS A19SOAirframe · Piper PA-44-180Engine modelLycoming O&VO-360 series

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming O&VO-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 · 1

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

NTSB WPR13CA316Accident · No injuriesData collectionFinal reportCasa Grande, AZThe pilot's failure to extend the landing gear before landing. Contributing to the accident was the pilot's and the flight examiner's distracted attention.Jul 5, 2013 · Substantial damage

FAA incident reports · 3

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

Accident 20130705012089ALanding: Touchdown · Casa Grande, AZWhile performing a simulated engine failure. The pilot was looking for traffic during final approach to runway 5 in Casa Grande, AZ regional airport. The gear warning horn was on during the entire time of the approach. The aircraft landed gear up. VMC…Jul 5, 2013 · Substantial damageIncident 20040807027819IGround Taxi, Other Airplane · Jacksonville, FL(-23) Pilot attempted to reposition from taxiway "b" to taxiway "a". He misjudged the clearance needed to avoid a taxiway light and the prop came in contact with it, damaging the light. The aircraft prop was repaired at Craig air center, in Jacksonville, and…Aug 7, 2004 · Minor damageIncident 20020309008679ILevel Off Touchdown · West Palm Beach, FL(-23) Pilot failed to put gear down during instructional flight. Props struck runway & a/c settled onto runway.Mar 9, 2002 · Minor damage

Service difficulty reports · 6

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

SDR FQAR20160125003Doubler · crackedTHE AFT FUSELAGE BULKHEAD, HAD BEEN FOUND CRACKED AND WAS IN THE PROCESS OF BEING REPLACED. WHEN THE BULKHEAD WAS REMOVED, THE DOUBLER, SUBJECT OF THIS REPORT, WAS FOUND TO HAVE NUMEROUS CRACKS AS WELL. CRACKS WERE CONCENTRATED IN THE 2 OTBD TOP RIVET HOLES,Jan 25, 2016 · N436PA · Piper PA44180 · Fuselage Main, BulkheadSDR FQAR20160125002Bulkhead · crackedDURING A ROUTINE INSPECTION, CRACKS WERE NOTED IN A BULKHEAD IN THE AFT UPPER FUSELAGE ADJACENT TO THE DORSAL FIN FORWARD ATTACH FITTING. THE CRACKS WERE MADE VISIBLE BY REMOVAL OF THE FAIRING THAT COVERS THE FORWARD ATTACH FITTING. FURTHER INSPECTION OF THEJan 25, 2016 · N436PA · Piper PA44180 · Fuselage Main, BulkheadSDR FQAR20150527073Angle · crackedDURING A PROGRESSIVE INSPECTION, AN ANGLE IN THE RT WING WAS FOUND TO BE CRACKED BEHIND THE LANDING GEAR SIDE BRACE FITTING. THE CRACKED ANGLE HAD BEEN INSTALLED IAW SB1161 AND WAS CONTAINED IN KIT PN 767-398.May 27, 2015 · N436PA · Piper PA44180 · Wing Miscellaneous StructureSDR FQAR20150527071Angle · crackedDURING A PROGRESSIVE INSPECTION, AN ANGLE IN THE LT WING WAS FOUND TO BE CRACKED BEHIND THE LANDING GEAR SIDE BRACE FITTING. THE CRACKED ANGLE HAD BEEN INSTALLED IAW SB 1161 AND WAS CONTAINED IN KIT PN 767-397.May 27, 2015 · N436PA · Piper PA44180 · Wing Miscellaneous StructureSDR 2012FA0000059Angle · crackedDURING A SCHEDULED INSPECTION, A CRACK WAS FOUND IN THE NACELLE ANGLE. UPON FURTHER INVESTIGATION, IT WAS FOUND THAT THE CRACK WAS BETWEEN THE 2 RIVETS THAT EXTENDED THRU THE WING SKIN INTO CAP (P/N 67097-002 OR -003 DEPENDENT ON SIDE) WHICH IS ATTACHED TO A Jan 4, 2012 · N436PA · Piper PA44180 · Nacelle/Pylon, Plate/SkinSDR 2012FA0000058Angle · crackedDURING A SCHEDULED INSPECTION, A CRACK WAS FOUND IN THE NACELLE ANGLE. UPON FURTHER INVESTIGATION, IT WAS FOUND THAT THE CRACK WAS BETWEEN THE 2 RIVETS THAT EXTENDED THRU THE WING SKIN INTO CAP (P/N 67097-002 OR -003 DEPENDENT ON SIDE) WHICH IS ATTACHED TO A Jan 4, 2012 · N436PA · Piper PA44180 · Nacelle/Pylon Miscellaneous Structure

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