Piper PA-28

Aircraft model · Fixed wing single engine · Airplane · registry code 7102801

Manufacturer (registry)
PIPER
Model
PA-28
Registry code
7102801
Registered
117 aircraft
Type
Fixed wing single engine
Engines
1 · Reciprocating
Seats
2
Weight class
Up to 12,499 lb
Cruise speed
107 mph
Certification
Type certificated

Model codes come from the FAA registry’s reference file. ADs are matched to them by model name and maker.

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Aircraft by year built · 192

1958Registered nowDeregistered2026
Aircraft by the year they were built: 192 aircraft
19581
196181
196286
19633
19642
19651
19662
19671
19682
19692
19722
19761
19771
19791
19801
19831
19844

Airworthiness directives that may apply · 0

ADs whose products match this airframe model. Each AD’s applicability may narrow it by serial number, part number or configuration.

No ADs matched this model

Information bulletins that may apply · 2

Query with SQL
duckdb -csv -c "SELECT s.saib_number, any_value(s.title) AS title, max(s.issue_date) AS issue_date, any_value(s.status) AS status
  FROM 'https://openairdocs.org/data/latest/faa_saib.parquet' s
  WHERE s.saib_id IN (SELECT saib_id FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_saib.parquet' WHERE aircraft_model_code IN ('7102801'))
  GROUP BY s.saib_number ORDER BY issue_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

Registered aircraft · 117

See all 117 registered aircraft
Query with SQL
duckdb -csv -c "SELECT n_number, serial_number, year_manufactured, status, registrant_name, registrant_city, registrant_state
  FROM 'https://openairdocs.org/data/latest/faa_aircraft_registration.parquet'
  WHERE aircraft_model_code IN ('7102801')
  ORDER BY n_number"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

NTSB investigations · 146

Aircraft matched to this model through the registry, by N-number and event date, checked against the reported serial number, make and model.

See all 146 investigations
Query with SQL
duckdb -csv -c "SELECT c.\"ntsbNumber\", c.\"eventDate\", c.\"eventType\", c.\"eventCity\", c.\"eventStateOrRegion\", a.n_number, a.\"aircraftMake\", a.\"aircraftModel\", c.\"highestInjuryLevel\", c.\"totalFatal\", c.\"completionStatus\", c.report_url
  FROM 'https://openairdocs.org/data/latest/ntsb_aircrafts.parquet' a JOIN 'https://openairdocs.org/data/latest/ntsb_case_detail.parquet' c ON c.\"mKey\" = a.case_mkey
  WHERE a.aircraft_model_code IN ('7102801')
  ORDER BY c.\"eventDate\" DESC, c.\"ntsbNumber\" DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

FAA incident reports · 90

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

See all 90 incident reports
Query with SQL
duckdb -csv -c "SELECT report_number, event_date, event_type, city, state, aircraft_make, aircraft_model, aircraft_damage, fatal_injuries, n_number
  FROM 'https://openairdocs.org/data/latest/faa_incident_report.parquet'
  WHERE aircraft_model_code IN ('7102801')
  ORDER BY event_date DESC, report_number DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

Service difficulty reports · 15

SDR T7KR2021080900001Points · excess playPOINT CONTACT SHAFT ON CAM ARM IS RIVETED ON. THE RIVET IS NOT TIGHT. THE POINT CONTACT SHAFT IS MOVING WITHIN THE POINT CAM ARM, SO, THE POINT CONTACT DOES NOT RISE WITH THE CAM LOBE. HENCH, NO OPENING OF THE POINTS MEANS NO COLLAPSE OF THE ELECTRICAL FIELD OAug 5, 2021 · Piper PA28* · Magneto/DistributorSDR 2019FA0000045Doubler · crackedCOMMON PROBLEM, CRACKS ON THE UNDERSIDE OF THE RIGHT WING WALK SECTION P/N 62061-02. THIS WING PANEL IS COMPOSED OF 2 PARTS: AN OUTER SKIN AND AN ATTACHED REINFORCED PAN, OR DOUBLER CONSISTING OF 8 EXPANDED BLISTERS THAT RUN LATERALLY WITH CURVED ENDS. DURINGFeb 24, 2019 · Piper PA28* · Wing, Plate/SkinSDR 2014FA0000042Crankshaft · failedDURING CRUISE FLIGHT, THE PILOT REPORTED AN ENGINE STOPPAGE, WHICH WAS FOLLOWED BY AN EMERGENCY LANDING. A POST ENGINE TEARDOWN INSPECTION REVEALED THAT THE CRANKSHAFT HAD SEPARATED JUST INBD FROM THE NR 3 CYLINDER ROD MOUNTING JOURNAL.Jan 21, 2014 · N5310W · Piper PA28* · Reciprocating Engine Power SectionSDR 2014FA0000234Bracket · crackedFOUND CRACKED BRACKET.Dec 14, 2013 · Piper PA28* · Fuselage Miscellaneous StructureSDR WS9R031908001Retainer · brokenDISCOVERED THAT ALL (4) OF THE PUSH ROD TUBE RETAINERS WERE BROKE UPON REMOVING THE ROCKER BOX COVERS. THIS ENGINE HAD JUST BEEN OVERHAULED AND HAS TEST CELL TIME ONLY.Mar 19, 2008 · Piper PA28* · Reciprocating Engine Cylinder SectionSDR 2007FA0000225Bracket · crackedTHIS BRACKET IS RIVETED IN THE CENTER TUNNEL AND ACCEPTS (2) BOLTS AT THE FORWARD SIDE OF THE FLAP HANDLE SUPPORT MOUNT. THIS IS A DIFFICULT AREA TO SEE, EVEN WITH A MIRROR. WE HAVE FOUND (6) CRACKED BRACKETS SO FAR TO DATE. SUSPECT FATIGUE AND AIR LOADS CAFeb 15, 2007 · Piper PA28* · Trailing Edge Flap Control SystemSDR 2001FA0000594Gascolator · crackedDURING ENGINE START, AN INDUCTION FIRE STARTED WHEN THE CARBURETOR BACKFIRED. THE FIRE COULD NOT BE EXTINGUISHED AND DESTROYED THE AIRCRAFT. DURING AN INVESTIGATION THE GASCOLATOR COVER WAS FOUND CRACKED. IT APPEARS THE FUEL LEAKING FROM THE COVER APPEARS TJul 24, 2001 · Piper PA28* · Aircraft Fuel Distribution SystemSDR SW15200110851Pump · defectivePART INSTALLED NEW AT OVERHAUL. TEST CESS OPERATION WITHIN REQUIRED PRESSURE AND FLOW. AT INSTALLATION IN AIRCRAFT, PUMP WOULD NOT FUNCTION AND WOULD NOT ALLOW FUEL TO BE PUMPED THRU USING BOOST PUMP.Apr 5, 2001 · Piper PA28* · Engine Fuel PumpSDR 99ZZZX3482Skin · crackedDOUBLER UNDER RIGHT UPPER WING ROOT SKIN CRACKING (BOTH FORWARD AND AFT SECTIONS). DUE TO NORMAL STRESS FROM GETTING IN AND OUT OF AIRCRAFT, THE UPPER SKIN FLEXES ENOUGH TO CONCENTRATE STRESSES AROUND THE STIFFENERS BEND RADIUS TO CAUSE CRACKING. THIS LEADS Aug 25, 1999 · Piper PA28* · Fuselage Main, Plate/SkinSDR 98ZZZX839Sender · failedSUDDENLY, RT FUEL TANK INDICATED TOTALLY EMPTY. FLIGHT WAS TERMINATED AND FUEL QUANTITY VISUALLY VERIFIED AS NEARLY ONE-HALF FULL. TANK WAS TOPPED OFF AND STILL INDICATED BONE DRY. MECHANICS TESTED GAUGE WITH A VARIABLE RESISTOR INSERTED IN GROUND CIRCUIT AFeb 9, 1998 · Piper PA28* · Fuel Quantity SensorSDR EY2R9601338Hub · corrodedCORROSION FOUND ON HUB.Dec 1, 1996 · Piper PA28* · Propeller Hub SectionSDR EY2R9601234Hub · corrodedHUB CORRODED.Nov 1, 1996 · Piper PA28* · Propeller Hub SectionSDR 96ZZZX4930Pin Plug · failedCYLINDER REMOVED FROM ENGINE DUE TO ALUMINUM IN OIL SCREEN. FOUND PIN PLUG SHAVED COMPLETELY OFF ON NR 3 CYLINDER ALLOWING PIN TO RUB AGAINST CYLINDER WALL. THESE TYPES OF PIN PLUGS ARE A LOOSE FIT UNLIKE SUPERIOR AIR PARTS, INC., STYLE AND WERE INSTALLED WISep 9, 1996 · Piper PA28* · Reciprocating Engine Cylinder SectionSDR EY2R9600526Propeller · corrodedPROPELLER ASSY FOUND CORRODEDApr 1, 1996 · Piper PA28* · Propeller AssemblySDR 95ZZZX1250Skin · corrodedFUSELAGE SKIN PANELS ACROSS TOP OF INST. PANEL SEVERELY CORRODED. WATER MOST LIKELY ENTERED THROUGH A WINDSHIELD LEAK. (THIS IS 2ND PA 28 OF THIS VINTAGE FOUND WITH THIS DEFECT IN LAST 3 YEARS). RECOMMEND INSPECTION BELOW VINYL AND REMOVAL OF FOAM BACKED VIFeb 1, 1995 · N5311W · Piper PA28* · Fuselage Main, Plate/Skin
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'PA28'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.