Engine model · Turbo-prop · 450 hp · registry code 51658

Manufacturer (registry)
P & W
Model
R-985-39A
Registry code
51658
Type
Turbo-prop
Power
450 hp

Model codes come from the FAA registry’s reference file.

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Airworthiness directives that may apply · 0

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

No ADs matched this model

Registered aircraft · 2

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 engine_model_code IN ('51658')
  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

No NTSB investigations matched to aircraft with this engine modelMatched through the registry by N-number, so foreign aircraft and some older cases aren’t counted.

FAA incident reports

No reports matched to aircraft with this engine modelMatched through the registry by N-number, so foreign aircraft and some older reports aren’t counted.

Service difficulty reports · 5

SDR CA150826006Retainer · damaged(CAN) DURING MAINTENANCE THERE WAS EVIDENCE THE UPPER TANK COVER GASKETS P/N C2PT529-27 WERE LEAKING. THIS AIRCRAFT HAS MOD 2/1376 INSTALLED TO INTRODUCE RUBBER FUEL TANK LINERS. THE GASKETS WERE REPLACED AND THE TANK FILLED WITH FUEL. THE TANK STILL LEAKED BEAug 12, 2015 · Dhav DHC2MKI · Fuel StorageSDR CA130102005Support Fitting · cracked(CAN) THIS RT FLOAT MODEL EDO 679-4930, SN: TB492, FOUND TO HAVE THE AFT SPREADER BAR SUPPORT FITTING, PN: 901-23060-1 DAMAGE, CRACKED. APPEARING TO BE THE RESULT OF INTER-GRANULAR CORROSION. THIS CRACKED FITTING, PN: 901-23060-1, WAS REPLACED WITH A NEW UNIJan 2, 2013 · Dhav DHC2MKI · Wheel/Ski/FloatSDR CA121203019Bar · cracked(CAN) WHILE CARRYING OUT A ANNUAL INSPECTION ON THE ACFT, THE AFT FLOAT SPREADER BAR PN 58-C-067-2 WAS FOUND TO HAVE A CRACK 4" IN LENGTH LOCATED ON THE LT SIDE AT THE L/E SKIN AREA WHICH RAN THROUGH THE PULLEY BRACKET FOR THE WATER RUDDER RETRACT CABLE. THEDec 3, 2012 · Dhav DHC2MKI · Wheel/Ski/FloatSDR CA060529008Vent · wrong partTHIS FRONT TANK FUEL VENT TUBE FOUND TO HAVE DISCONNECTED FROM THE RUBBER BLADDER. THE HOSE CLAMP WAS TIGHT BUT THE TUBE WAS ABLE TO WORK ITSELF FROM THE BLADDER CAUSING FUEL LEAKAGE AND GASES TO ESCAPE FROM THE BLADDER. IN INVESTIGATING THIS OCCURRENCE IT WMay 24, 2006 · Dhav DHC2MKI · Aircraft Fuel Distribution SystemSDR CA060524002Wheel · corrodedTHIS PART WAS INSTALLED MAY 31/04 IN ACCORDANCE WITH VIKING AIR GROSS WEIGHT INSTRUCTION. IT WAS NOTICED THAT EARLY CORROSION HAD BEGUN AT THE WHEEL GEAR ATTACHMENT HOLE. THE CORROSION WAS DEEP AND THE PART WAS REPLACED WITH A NEW UNIT. POSSIBLE CAUSE FOR TMay 12, 2006 · Dhav DHC2MKI · Wheel/Ski/Float
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 engine_model_key = 'R98539A'
  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.