This N-number isn't registered right now. Below is its last known registration, canceled Feb 4, 2023.
Safety record in brief:1 NTSB accident (substantial damage, Jan 1994)8 ADs may apply6 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
The pilot not maintaining clearance from the snowbank during final approach. A factor in this accident was the proximity of the snowbank to the active runway.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for BFO94LA036)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2018-07-03 | Placard and Markings | Apr 20, 2018 | Airframe (PA-28-161)Serial numbers per Table 1 to paragraph (c) of this AD |
| 2016-07-21 | Wing Ribs/Bulkhead | Apr 26, 2016 | Airframe (PA-28-161)Certain serial numbers: PA-28-161 2842393–2842395; PA-28-181 2843769–2843775; PA-28-181 2843779–2843791; PA-28R-201 2844152; PA-28-161 2842010–2842392; PA-28-181 2843021–2843768; … |
| 2013-02-13 | Stabilizer Control System | Mar 11, 2013 | Airframe (PA-28-161) |
| 2010-26-04 | Piper Aircraft, Inc. Model PA-28-161 Airplanes | Feb 1, 2011 | Airframe (PA-28-161)Only with: Equipped with Thielert TAE-125-01 engine installed per STC No. SA03303AT. |
| 2010-15-10 | Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series Airplanes | Aug 31, 2010 | Airframe (PA-28-161)Certain serial numbers: PA-28-140 28-20001–28-26946; PA-28-140 28-7125001–28-7725290; PA-28-150 28-03; PA-28-150 28-1–28-4377; PA-28-150 28-1760A; PA-28-160 28-03; … |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2004-14-12 | The New Piper Aircraft, Inc., Models PA-28-161, PA-28-181, PA-28R-201, PA-32R-301 (HP)… | Aug 10, 2004 | Airframe (PA-28-161)Certain serial numbers: PA-28-161 2842026–2842180; PA-28-181 2843112–2843565; PA-28R-201 2844014–2844099; PA-32R-301 3246098–3246214; PA-32R-301T 3257028–3257327; PA-34-220T 3449042–3449292; … |
| 99-26-05 | The New Piper Aircraft, Inc. Models PA- 25, PA-25-235, PA-25-260, PA-28S-160… | Jan 13, 2000 | Airframe (PA-28-161)Only with: Equipped with Purolator air filter P/N 638873, Model CA161PL, or Piper P/N 460-632 (PS60007-2); PA-28-151/161 only when STC SA2946SO is incorporated. |
| 95-26-13 | The New Piper Aircraft, Inc. (Formerly Piper Aircraft Corporation) PA28 and PA32 Series… | Feb 5, 1996 | Airframe (PA-28-161)Only with: Equipped with oil cooler hose assemblies that do not meet TSO-C53a, Type D requirements. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
DURING 100 HR INSPECTION, FOUND BOTH EARS CRACKED THAT SCISSORS LINK ATTACHES TO ON UPPER END OF LEFT MAIN GEAR STRUT.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING ROUTINE INSPECTION AXLE STUB WAS FOUND CRACKED 75 PERCENT OF THE WAY AROUND. AREA INVOLVED WAS IN THE EAR AREA WHERE THE SCISSORS ATTACH AT THE LOWER END CASTING. WHERE SCISSORS ATTACH BOTH EARS WERE CRACKED ON THE INSIDE AND EXTENDING ACROSS THE WIDTH OF THE EAR.
From FAA Service Difficulty Reports; matched by N-number and serial number.BOLT SHEARED OFF ALLOWING INNER STRUT TUBE TO PASS THRU BLOCK ON TOP OF FORK, COME OUT THE BOTTOM OF THE FORK AND PASS THRU THE TIRE AND TUBE, STOPPING AT THE WHEEL. TOWER ADVISED PILOT HE HAD SMOKE SHOWING OFF THE TIRE. AFTER LANDING, THE PRESSURE OF THE STRUT PUSHED THE INNER TUBE, 65230-000…
From FAA Service Difficulty Reports; matched by N-number and serial number.CARBURETOR WAS REMOVED FROM SERVICE. ENGINE DIESELED AFTER SHUTDOWN, AND LEAKING FUEL AT THE SEAM BETWEEN THE TOP HALF OF THE CARBURETOR AND THE LOWER BOWL SECTIONS. ALL THE SCREWS AND SAFETIES WERE IN PLACE. THERE WAS A DEFINITE GAP BETWEEN THE 2 MATING SURFACES. ACFT WAS ALSO RUNNING VERY RICH…
From FAA Service Difficulty Reports; matched by N-number and serial number.TIRE WENT FLAT WHEN THE ACFT WAS JACKED. TIRE APPEARS FINE. SMALL PINHOLE IN SIDEWALL OF THE TUBE.
From FAA Service Difficulty Reports; matched by N-number and serial number.CRACKS IN RADIUS OF SCISSORS EARS. POSSIBLE CAUSE FATIGUE ON HIGH TIME AIRCRAFT.
From FAA Service Difficulty Reports; matched by N-number and serial number.