This N-number isn't registered right now. Below is its last known registration, canceled Nov 16, 2015.
Safety record in brief:1 NTSB accident (substantial damage, Aug 2009)7 ADs may apply4 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 student pilot's failure to maintain pitch control during landing and the flight instructor's delayed remedial action, resulting in a hard landing.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA09CA484)
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 |
|---|---|---|---|
| 2013-02-13 | Stabilizer Control System | Mar 11, 2013 | Airframe (PA-34-200T) |
| 2010-15-10 | Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series Airplanes | Aug 31, 2010 | Airframe (PA-34-200T)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; … |
| 2005-15-10 | The New Piper Aircraft, Inc. Models PA-34-200T, PA-34-220T, PA-44-180, and PA-44-180T… | Aug 26, 2005 | Airframe (PA-34-200T)Certain serial numbers: PA-34-200T 34-7570002–34-8170092; PA-34-220T 34-8133002–3449278; PA-44-180 44-7995001–4496168; PA-44-180T 44-8107001–44-8207020; PA-34-220T 3449279–3449309; PA-44-180 4496169–4496190. Only with: Equipped with a model 91E92-1 or 91E93-1 aircraft heater fuel pump. |
| 2005-13-16 | The New Piper Aircraft, Inc. PA-34 Series Airplanes | Aug 8, 2005 | Airframe (PA-34-200T) |
| 99-05-09 | The New Piper Aircraft, Inc. PA-23, PA- 24, PA-28, PA-32, and PA-34 Series Airplanes | Mar 19, 1999 | Airframe (PA-34-200T)Certain serial numbers: PA-23-235 27-505–27-622; PA-23-250 27-01–27-2504; PA-24-180 24-103–24-3687; PA-24-250 24-103–24-3687; PA-24-260 24-3642; PA-24-260 24-4000–24-5028; …. Only with: Equipped with Purolator air filter P/N 638873, Model CA161PL, or Piper P/N 460-632 (PS60007-2). |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 97-01-01 R1 | The New Piper Aircraft, Inc. PA-24, PA- 28R, PA-30, PA-32R, PA-34, and PA-39 Series… | Dec 8, 1998 | Airframe (PA-34-200T)Certain serial numbers: PA-28R-180 28R-30002–28R-31135; PA-28R-180 28R-7130001–28R-7130013; PA-28R-200 28R-35001–28R-35820; PA-28R-200 28R-7135001–28R-7635539; PA-28R-201 28R-7737002–28R-7737096; PA-28R-201T 28R-7703001–28R-7703239; …. Only with: All serials of PA-24, PA-24-250, PA-24-260, PA-24-400, PA-30, PA-39; PA-28R, PA-32R, PA-34 models (all serials of PA-34-200) only if not equipped with Piper P/N 78717-02 (or FAA-approved equivalent) main gear sidebrace stud in both main gear sidebrace bracket assemblies. |
| 98-04-27 | The New Piper Aircraft Corporation Models PA-23, PA-23-160, PA-23-235, PA-23-250… | Mar 13, 1998 | Airframe (PA-34-200T) |
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.
P/N 63901-28 AND P/N 63901-70 HOSES (TT 7,264.3 HRS) CAUSED CONTAMINATION TO BE INJECTED INTO ORFICE FITTING OF NOSE GEAR ACTUATOR CAUSING NOSE TO NOT COME OUT OF WHEELWELL MAKING FOR A NOSE GEAR UP LANDING. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number.P/N 63901-28 AND P/N 63901-70 HOSES (TT 7,264.3 HRS) CAUSED CONTAMINATION TO BE INJECTED INTO ORFICE FITTING OF NOSE GEAR ACTUATOR CAUSING NOSE TO NOT COME OUT OF WHEELWELL MAKING FOR A NOSE GEAR UP LANDING. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number.LANDING GEAR POWER RACK WOULD NOT PUT GEAR IN EXTENDED POSITION - UPON DISASSEMBLY - COMMUTATOR ARMATURE SEEMED TO BE 'OUT OF ROUND DUE TO THE BRUSH MARKS. THE BRUSHES WERE NOT WORN EXCESSIVE.
From FAA Service Difficulty Reports; matched by N-number and serial number.PIPER SB 956, PART II, WAS C/W AT 4,914 HOURS TT ON 5-92. PART II IS PERMANENT COMPLIANCE AND BOLTS USED WERE LOOSE ON ATTACH FITTINGS. THESE ARE A LARGER BOLT THAN ORIGINAL WITH AIRCRAFT. RETORQUED ALL BOLTS PER SB 956, PART II.
From FAA Service Difficulty Reports; matched by N-number and serial number.