Registered owner
Coco Aircraft Inc
Owner type
Corporation
Serial number
2843303
Year built
1999
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, normal, utility
Airworthiness date
December 7, 1999
Certificate issued
August 6, 2021
Expires
August 31, 2028
Mode S code
ACA6CD

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 60

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: 69 ADs
19631
19641
19661
19671
19692
19774
19793
19804
19821
19862
19893
19911
19921
19951
19964
19971
19982
19991
20001
20011
20042
20052
20065
20071
20083
20091
20103
20122
20131
20151
20161
20172
20182
20212
20221
20243
20261
See all 69 ADs

Information bulletins that may apply · 22

Advisory, not mandatory.

See all 24 bulletins

NTSB investigations

No NTSB investigations matched to N914PAMatched 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-28-181 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 · 10

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

SDR FQAR20190213003Rib · crackedDURING A ROUTINE INSPECTION FOUND THE RIBS IN THE RIGHT WING AT WING STATION 64.59 AND 86.03 CRACKED AT THE FLANGE AT THE END RIVET, UPPER SIDE.Feb 8, 2019 · N914PA · Piper PA28181 · Wing, Rib/BulkheadSDR FQAR20190213002Rib · crackedDURING A ROUTINE INSPECTION FOUND THE RIBS IN THE RIGHT WING AT WING STATION 64.59 AND 86.03 CRACKED AT THE FLANGE AT THE END RIVET, UPPER SIDE.Feb 8, 2019 · N914PA · Piper PA28181 · Wing, Rib/BulkheadSDR FQAR201805150029Bracket · crackedDURING ROUTINE INSPECTION, FOUND FORWARD FLAP HANDLE MOUNTING BRACKET CRACKED, BRACKET IS LOCATED IN THE TUNNEL AND IS THE MOUNTING POINT FOR THE 2 FORWARD BOLTS FOR THE FLAP HANDLE ASSEMBLY, BELIEVE CRACKING IS CAUSED BY FLIGHT CREWS INADVERTENTLY STEPPING ONMay 11, 2018 · N914PA · Piper PA28181 · Trailing Edge FlapsSDR FQAR20170620053Blower Motor · failedDURING FLIGHT, THE PILOT NOTICED THE CABIN VENT BLOWER FAN OPERATION BECAME VERY LOUD (SCREECHING) AND A STRONG BURNING ODOR WAS NOTED. THE AC/FA BLOWER CIRCUIT BREAKER BLEW SHORTLY THEREAFTER; AN UNEVENTFUL RETURN TO THE AIRPORT WAS MADE. WHEN A MAINTENANCE PJun 20, 2017 · N914PA · Piper PA28181 · Air Distribution FanSDR FQAR20170615048Angle · crackedDURING A ROUTINE INSPECTION, AN ANGLE IN THE RIGHT WING THAT IS CO-LOCATED WITH THE OUTBOARD FLAP MOUNTING BRACKET WAS FOUND TO BE CRACKED THROUGH THE RIVETS.Jun 15, 2017 · N914PA · Piper PA28181 · Wing Miscellaneous StructureSDR FQAR20161027045Bracket · crackedWHEN THE ELT WAS BEING REMOVED FOR INSPECTION, THE TECH DISCOVERED TWO 2" CRACKS NEXT TO THE NUTPLATES IN THE ELT MOUNTING BRACKET. THESE CRACKS CAN ONLY BE SEEN WHEN THE ELT TRAY IS REMOVED.Oct 27, 2016 · N914PA · Piper PA28181 · Fuselage Main, Attach FittingsSDR FQAR20150523052Cylinder Head · crackedBORESCOPE EXAMINATION REVEALED THE NR 4 CYLINDER HEAD WAS CRACKED. AFTER THE CYLINDER WAS REMOVED, CRACKING WAS SEEN AT THE LOWER SPARK PLUG HOLE. THE CYLINDER HEAD CASTING NR C-02077.May 23, 2015 · N914PA · Piper PA28181 · Reciprocating Engine Cylinder SectionSDR FQAR20150523051Cylinder Head · crackedBORESCOPE EXAMINATION REVEALED THE NR 3 CYLINDER HEAD WAS CRACKED. AFTER THE CYLINDER WAS REMOVED, CRACKING WAS SEEN AT THE LOWER SPARK PLUG HOLE. THE CYLINDER HEAD CASTING NR C-02195.May 23, 2015 · N914PA · Piper PA28181 · Reciprocating Engine Cylinder SectionSDR FQAR20150217016Bracket · crackedDURING A PROGRESSIVE INSPECTION EVENT, A BRACKET WAS FOUND CRACKED BELOW WHERE THE FLAP HANDLE IS MOUNTED. THE BRACKET IN QUESTION IS LOCATED IN THE TUNNEL IN THE CENTER OF THE CABIN FLOOR AND IS USED TO MOUNT THE FLAP HANDLE ASSY. IT CONTAINS NUT PLATES TO AFeb 12, 2015 · N914PA · Piper PA28181 · Fuselage Main, Attach FittingsSDR 2011FA0000049Shaft · mismanufacturedLOOKING UNDER 10X YOU CAN SEE MACHINE MARKS ON THE THREADS OF THE SHAFT PREVENTING THE SHAFT FROM THREADING INTO THE TRIM BARREL. 4 IN STOCK ALL ARE FROM DATE 3/19/10 WITH A BATCH NR OF 6641D28J ALL WITH SAME DEFECT. USED A SHAFT WITH A DIFFERENT BATCH NR ANJan 18, 2011 · N914PA · Piper PA28181 · Stabilizer Control System

STCs that may be installed · 369

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

See all 369 STCs