N753401976 Piper PA-28R-200
Safety record in brief:No NTSB accidents or incidents since 19825 ADs may apply8 service difficulty reports
Registration
FAA Aircraft Registry · Oct 18, 2026- Registered owner
- High Point Aviation LLC
- Owner type
- LLC
- City, state
- Spencerport, NY
- Certificate issued
- Mar 8, 2016
- Expires
- Mar 31, 2029
- Airworthiness
- Standard · Normal
- Airworthiness date
- May 17, 1976
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Piper
- Model
- PA-28R-200
- Year
- 1976
- Serial number
- 28R-7635292
- Aircraft type
- Fixed wing single engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 4
- Engines
- 1
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- AA282B
Engine
- Make and model
- Lycoming I0360 Ser
- Type
- Reciprocating
- Power
- 180 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2016 – nowHigh Point Aviation LLCSpencerport, NY · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (5)
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-28R-200)Serial numbers per Table 1 to paragraph (c) of this AD |
| 2013-02-13 | Stabilizer Control System | Mar 11, 2013 | Airframe (PA-28R-200) |
| 2010-15-10 | Piper Aircraft, Inc. PA-28, PA-32, PA-34, and PA-44 Series Airplanes | Aug 31, 2010 | Airframe (PA-28R-200)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; … |
| 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-28R-200)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. |
| 95-26-13 | The New Piper Aircraft, Inc. (Formerly Piper Aircraft Corporation) PA28 and PA32 Series… | Feb 5, 1996 | Airframe (PA-28R-200)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.
Service Difficulty Reports (8)
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.
- Fuselage · skin · crackedSep 14, 2005
AT CABIN ENTRANCE, WING WALK, FOUND SUPPORT PANEL UNDER WING WALK CRACKED. FAILURE DUE TO REPEATED WALKING ON. IF FACTORY STAMPED SUPPORT OUT OF HEAVIER, THICKER PANEL, MAY HELP PROLONG FAILURE. (EA21200507814) (K)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Power plant · hinge pin · failedSep 2, 1996
DURING PRE-FLIGHT RUN UP, POWER WAS LIMITED TO 1,900 RPM. THE ALTERNATE AIR DOOR WAS FOUND IN THE FUEL METERING UNIT, THE HINGE PIN HAD WORN COMPLETELY THROUGH IN 600 HOURS OF OPERATION. (ONE YEAR AT FLIGHT SCHOOL). SUBMITTER RECOMMENDATION, A TAB ON THE ALTERNATE AIR DOOR COULD PROVIDE BOTH A…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Stabilizers · trim tab · crackedJul 1, 1996
DURING 100-HOUR INSPECTION, THE TRIM TAB WAS DISCONNECTED TO ACCOMODATE REPLACEMENT OF TRIM BARREL HARDWARE, THE TRIM TAB WAS FOUND TO BE CRACKED: UNDER THE ATTACH BRACKET, AT THE EDGE OF THE ATTACH BRACKET, INTO THE SUPPORTING RIBS., ON BOTH LT AND RT TRIM TAB.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 8 reportsShow fewer reports
- Reciprocating engine · crankcase · crackedJun 19, 1996
DURING 100-HOUR INSPECTION, THE CRANKCASE WAS FOUND CRACKED (2 INCHES). THIS WAS THE SAME CRACK THAT WAS FOUND 2 YEARS AGO WHEN THE ENGINE HAD 1,500 HOURS TSMO. THE CASE HALVES WERE REPLACED AND NOW 1,000 HOURS LATER, THE SIMILAR CRACK HAS RE-APPEARED. SUSPECT VIBRATION PROBLEM.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Stabilizers · trim tab · crackedJun 19, 1996
DURING 100-HOUR INSPECTION, THE TRIM TAB WAS DISCONNECTED TO ACCOMMODATE REPLACEMENT OF TRIM BARREL HARDWARE, THE TRIM TAB WAS FOUND CRACKED; UNDER THE ATTACH BRACKET, AT THE EDGE OF THE ATTACH BRACKET, INTO THE SUPPORTING RIBS, AND ON BOTH LEFT AND RIGHT TRIM TABS.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Stabilizers · trim tab · crackedJun 19, 1996
DURING 100-HOUR INSPECTION, THE TRIM TAB WAS DISCONNECTED TO ACCOMMODATE REPLACEMENT OF TRIM BARREL HARDWARE, THE TRIM TAB WAS FOUND CRACKED; UNDER THE ATTACH BRACKET, AT THE EDGE OF THE ATTACH BRACKET, INTO THE SUPPORTING RIBS, AND ON BOTH LEFT AND RIGHT TRIM TABS.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Hydraulic power · power pack · defectiveApr 3, 1996
AFTER OPERATING FOR 500 HOURS, THE HYDRAULIC POWER PACK BEGAN TO CAVITATE EITHER BECAUSE OF AIR OR CONTAMINATION. THE SM INSTRUCTIONS CLEARLY STATE 'OPERATE PUMP TO PURGE AIR FROM SYSTEM' WHENEVER REPLACING THE PUMP, A CYLINDER, OR A LINE. UNFORTUNATELY, THESE STEPS WILL NOT PURGE AIR NOR…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Power plant · mount · crackedApr 4, 1995
FLIGHT CREW MEMBER IDENTIFIED CRACK ON ENGINE MOUNT RING TUBE ADJACENT TO DIP STICK. INTERESTINGLY, THIS CRACK IS IDENTICAL TO THOSE FOUND ON AIRCRAFT AFFECTED BY PIPER SL 568. SUBMITTER RECOMMENDS A REVIEW/EXPANSION OF THIS SL AND THE ADDITION OF REINFORCEMENT TO PRECLUDE CRACKING AT NEXT ENGINE…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 18, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 18, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026