Aircraft model · Fixed wing multi engine · Airplane · registry code 4230102

Manufacturer (registry)
HAWKER SIDDELEY
Model
DH-125
Registry code
4230102
Registered
0 aircraft
Type
Fixed wing multi engine
Engines
2 · Turbo-jet
Seats
10
Weight class
20,000 lb and over
Cruise speed
320 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 · 16

1963Registered nowDeregistered2026
Aircraft by the year they were built: 16 aircraft
19631
19642
19655
19664
19671
19691
19701
19761

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.

1994In forceSuperseded2026
ADs by the year they took effect: 3 ADs
19941
20012
Superseded and historical ADs · 3
Query with SQL
duckdb -csv -c "SELECT d.ad_number, d.status, d.subject, d.effective_date
  FROM 'https://openairdocs.org/data/latest/faa_directive.parquet' d
  WHERE d.ad_id IN (SELECT ad_id FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_directive.parquet' WHERE aircraft_model_code IN ('4230102'))
  ORDER BY coalesce(d.effective_date, d.publication_date, d.issue_date) DESC, d.ad_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.

Registered aircraft · 0

No aircraft currently registered with this model

NTSB investigations · 5

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

First occurrence, 1982 to 2007

Of 1 case with NTSB’s older coding, defined in its coding manual.

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 ('4230102')
  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 · 3

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

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 ('4230102')
  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 · 10

SDR CA140411004Rod · loose(CAN) FLIGHT CREW REPORTED WEAK BRAKES AFTER LANDING ROLLOUT. INVESTIGATION OF THE BRAKE ASSEMBLY IDENTIFIED THAT NR 2 ASSY WAS WORN BEYOND LIMITS. BRAKE ASSEMBLY REPLACED, BLED AND CHECKED SERVICEABLE IAW AMM CH32. THE REASON FOR THIS SDR IS THAT THE BRAKE AApr 8, 2014 · Hwksly DH125* · Landing Gear Brake SystemSDR 2006FA0001231Static Port · misinstalledROSEMOUNT STATIC PORTS DO NOT FIT CONTOUR OF AIRCRAFT SKIN. PORTS ARE NOT UNIFORM IN THICKNESS. CAN NOT INSTALL NEW PORT AND MATCH STEP HEIGHT TO MEET ORIGINAL RVSM CERTIFICATION. OTHER ISSUES: WHEN PORT IS INSTALLED, PORT CAUSE STRESS. AC SKIN DO TO CONTOUNov 30, 2006 · N700VT · Raythn DH125 · Pitot/Static SystemSDR RBR32201028Balance Weight · corrodedBOTH ELEVATOR MASS BALLAST WEIGHTS AND COVERS HAVE RUST. CORROSION REMOVAL REQUIRED FOR INSPECTION.Jul 3, 2006 · N322BC · Raythn DH125 · Elevator StructureSDR RBR32201014Door · crackedLEFT MAIN GEAR DOOR CRACKED AT FWD HINGE ATTACHMENT.Jul 3, 2006 · N322BC · Raythn DH125 · Landing Gear DoorsSDR RBR32201015Skin · corrodedLEFT UPPER SPEEDBRAKE HAS CORROSION X-RAY REVEALED CORROSION AT CENTER SPAR.Jul 3, 2006 · N322BC · Raythn DH125 · SpoilersSDR RBR32201079Doubler · corrodedCORROSION FOUND ON ANTENNA DOUBLER MOUNTED TO CHIN FAIRING.Jul 3, 2006 · N322BC · Raythn DH125 · Fuselage Miscellaneous StructureSDR RBR32201089Cap · corrodedLT ELEVATOR FWD CAP CORRODED BEYOND LIMITS.Jul 3, 2006 · N322BC · Raythn DH125 · Elevator StructureSDR ZLWA0601Servo · failedON TAKEOFF RUDDER OSCILLATES WHEN YAW DAMPNER ENGAGED.Jun 5, 2006 · N85HH · Raythn DH125 · Rudder Control SystemSDR HAG06002Longeron · crackedCRACK IN KEEL LONGERON BETWEEN FRAMES 4 AND 5, APROXIMATE STATION 175.00.CRACK IS ONLY IN LONGERON, NOT IN MAIN BEAM. CRACK LOCATED IN LOWER AFT HOLE FOR NOSE GEAR ATTACH BRACKET. DISCOVERED DURING REQUIRED CHECK OF ATTACH BOLT TORQUE, ALL BOLTS FOUND LOOSE.Apr 6, 2006 · N125CK · Raythn DH125 · Fuselage Main, Longeron/StringerSDR 20010403CW007Tire · failedA LANDING GEAR/WHEEL TYPE SPEED RELATED VIBRATION WAS REPORTED BY THE FLIGHT CREW. INVESTIGATION REVEALED A BUMPED OUT AREA OF TREAD ON THE RIGHT OUTBOARD MAIN TIRE. THE AREA WAS APPROX 9 INCHES LONG PLUS THE TIRE WIDTH OF THE TREAD AREA. THAT AREA WAS .18Feb 26, 2001 · N333DP · Raythn DH125 · Tire
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 = 'DH125'
  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.