Registered owner
Bird Acquisition LLC
Location
Phoenix, AZ
Owner type
LLC
Serial number
4496070
Year built
2001
Type
Fixed wing multi engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
July 20, 2001
Certificate issued
October 1, 2007
Expires
September 30, 2028
Mode S code
A536F7

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 55

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
ADs by the year they took effect: 62 ADs
19631
19641
19661
19671
19692
19772
19794
19804
19813
19821
19892
19911
19921
19942
19951
19963
19972
19982
20001
20031
20042
20053
20063
20071
20083
20091
20103
20122
20131
20161
20171
20211
20221
20242
20261
See all 62 ADs

Information bulletins that may apply · 17

Advisory, not mandatory.

See all 19 bulletins

NTSB investigations

No NTSB investigations matched to N435PAMatched 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 · 3

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

Service difficulty reports · 5

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

SDR FQAR20160301008Doubler · crackedDURING A ROUTINE INSPECTION, A DOUBLER INSTALLED ON A BULKHEAD IN THE EMPENNAGE WAS FOUND TO BE CRACKED. THE CRACKED DOUBLER WAS MADE VISIBLE BY REMOVING THE FAIRING BETWEEN THE VERTICAL FIN AND AFT FUSELAGE AND LOOKING AFT AND UP WITH A MIRROR AND FLASHLIGHT.Mar 1, 2016 · N435PA · Piper PA44180 · Fuselage Main, BulkheadSDR FQAR20150608077Angle · 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 SB 1161 AND WAS CONTAINED IN KIT PN 767-398.Jun 8, 2015 · N435PA · Piper PA44180 · Wing Miscellaneous StructureSDR FQAR20150608076Angle · 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 SB1161 AND WAS CONTAINED IN KIT PN 767-397.Jun 8, 2015 · N435PA · Piper PA44180 · Wing Miscellaneous StructureSDR FQAR20150421028Oil Cooler · leakingON PREFLIGHT INSPECTION, THE PILOTS NOTED AN OIL STREAK EMANATING FROM UNDER THE INBD SIDE OF THE RT ENGINE COWL. MAINTENANCE REMOVED THE COWLING AND SAW A GREAT DEAL OF FRESH OIL ALL OVER THE INSIDE OF THE ENGINE COWLINGS. THE TECH RAN THE ENGINE WITH THE TApr 20, 2015 · N435PA · Piper PA44180 · Engine Oil CoolerSDR 2012FA0000056Angle · 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 · N435PA · Piper PA44180 · Nacelle/Pylon Miscellaneous Structure

STCs that may be installed · 235

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

See all 235 STCs

Earlier aircraft with this N-number · 1

This aircraft carried N435PA before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.