Engine model · Reciprocating · 300 hp · registry code 17240

Manufacturer (registry)
CONT MOTOR
Model
IO-520-E
Registry code
17240
Type
Reciprocating
Power
300 hp
Data sheet
TCDSE5CE
Holder
Continental Aerospace Technologies, Inc.

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

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Airworthiness directives that may apply · 27

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

1974In forceSuperseded2026
ADs by the year they took effect: 27 ADs
19741
19791
19801
19812
19882
19911
19932
19961
19981
19991
20001
20041
20071
20092
20101
20121
20141
20161
20221
20234
See all 33 ADs
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_engine_model_directive.parquet' WHERE engine_model_code IN ('17240'))
  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.

Information bulletins that may apply · 10

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_engine_model_saib.parquet' WHERE engine_model_code IN ('17240'))
  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 · 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 ('17240')
  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 · 2

Matched to this engine model through the registry, by N-number and event date.

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 engine_model_code IN ('17240')
  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 · 11

SDR E5ZR2018061300177Connecting Rod · oil starvationAFTER TEARING DOWN OF THE ENGINE, THE NR 5 CYLINDER FAILED DUE TO OIL STARVATION OF THE CONNECTING ROD CAP FOR UNKNOWN REASONS. THIS CAUSED FAILURE OF THE ROD CAP BOLTS. THE CAP BOLTS STRETCHED, SNAPPED AND THEY SHOW SIGNS OF BURN MARKS.May 21, 2018 · N206S · Beech 95B55 · Reciprocating Engine Cylinder SectionSDR E5ZR2018061300178Connecting Rod · failedAFTER TEARING DOWN OF THE ENGINE IN QUESTION IT IS OUR OPINION THAT THE FAILURE WAS DO TO OIL STARVATION OF THE #5 CYLINDER CONNECTING ROD CAP FOR UNKNOWN REASONS. THIS CAUSED FAILURE OF THE ROD CAP BOLTS. THE CAP BOLTS STRETCHED, SNAPPED AND THEY SHOW SIGNSMay 21, 2018 · N206S · Beech 95B55 · Reciprocating Engine Power SectionSDR E5ZR20180613001Connecting Rod · failedAFTER TEARING DOWN THE ENGINE IN QUESTION IT IS OUR OPINION THAT THE FAILURE WAS DO TO OIL STARVATION OF THE NR 5 CYLINDER CONNECTING ROD CAP FOR UNKNOWN REASONS. THIS CAUSED FAILURE OF THE ROD CAP BOLTS. THE CAP BOLTS STRETCHED, SNAPPED AND THEY SHOW SIGNS May 21, 2018 · N206S · Beech 95B55 · Reciprocating Engine Power SectionSDR CA120117004Mount · broken(CAN) THE RT FORWARD ENGINE MOUNT LEG BROKE INTO 2 PIECES. THE PIECES REMAINED ATTACHED TO THE ENGINE AND THE ENGINE MOUNT.Dec 23, 2011 · Cessna A185E · Engine Mount SectionSDR 2010FA0000409Barrel · wornPILOT STATED THAT WHILE IN FLIGHT AT 5000 FT, HE WAS UNABLE TO CHANGE THE MIXTURE SETTING ON THE LT ENGINE. THIS ENGINE HAD JUST RETURNED FROM A MAJOR O/H DUE TO TBO REQUIREMENTS. ACCORDING TO THE PILOT, THIS ENGINE HAD NOT HAD ANY PREVIOUS PROBLEMS IN THE PApr 3, 2010 · N8911Z · Cessna 310G · Mixture ControlSDR 2007FA0001088Rib · crackedAT ANNUAL INSPECTION FOUND CRACK ON FLAP RIB. (FLAP ROD ATTACH POINT) BOTH LT AND RT FLAPS. (K)Nov 9, 2007 · N127RW · Beech 95B55 · Trailing Edge FlapsSDR MHJ2002F00002Cylinder · separatedNR 4 CYLINDER FOUND SEPERATED FROM CRANKCASE, CAUSE UNKNOWN. ENGINE REMOVED FROM AIRCRAFT AND SENT TO OVERHAUL FACILITY.Feb 18, 2002 · N401PW · Cessna 401 · Reciprocating Engine Cylinder SectionSDR BSY2002F00004Tach Generator · inoperativeLEFT TACH QUIT AFTER TAKE OFF, RETURNED TO AIRPORT. REMOVED AND REPLACED THE GENERATOR OPS CHECKS GOOD.Feb 8, 2002 · N3703Q · Beech 58 · Engine RPM Indicating SystemSDR 20000831SH017Cam · strippedENGINE FAILURE CAUSED BY TEETH BEING STRIPPED OFF OF CAMGEAR. ONE TOOTH APPEARS TO HAVE BEEN FRACTURED AND THE FOLLOWING 6 TEETH WERE STRIPPED. GEAR WAS STILL PROPERLY FASTENED TO CAMSHAFT. THE CRANKSHAFT GEAR WAS NOT DAMAGED. NO FOREIGN MATERIALS WERE FOAug 10, 2000 · N22EW · Beech 95B55 · Reciprocating Engine Power SectionSDR 97ZZZX2805Adapter · bindingWHILE PERFORMING COMPRESSION TEST, DISCOVERED ENGINE WOULD LOCK-UP WHEN ROTATED BACKWARDS. TROUBLESHOOTING REVEALED STARTER ADAPTER WAS CAUSE OF PROBLEM. FURTHER INSPECTION OF ADAPTER SHOWED ACCUMULATION OF RUST AT STARTER MOUNTING PAD. THIS WAS SECOND NEWLYMay 19, 1997 · N488SP · Cessna 310N · Reciprocating Engine Rear SectionSDR 95ZZZX2886Crankshaft · crackedEMERGENCY LANDING MADE DUE TO OIL LOSS AND PRESSURE LOSS. FOUND OIL LOSS AT APPROXIMATELY 1 QUART PER MINUTE AT 1,000 RPM. REMOVED PROPELLER AND FOUND FLANGE CRACKED 50 PERCENT AROUND CIRCUMFERENCE OF FLANGE. FAILURE OF CRANKSHAFT (LOSS OF PROPELLER) WAS VEMay 19, 1995 · N3653A · Beech 95B55 · Reciprocating Engine Power Section
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 = 'IO520E'
  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.