Engine model · Reciprocating · 400 hp · registry code 41951

Manufacturer (registry)
LYCOMING
Model
IO-720-B1B
Registry code
41951
Installed in
0 registered aircraft
Type
Reciprocating
Power
400 hp
Data sheet
TCDS1E15
Holder
Textron Lycoming Subsidiary of Textron Inc.

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

On this page

Airworthiness directives that may apply · 15

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

1975In forceSuperseded2026
ADs by the year they took effect: 20 ADs
19751
19771
19781
19791
19921
19951
19971
19982
20032
20041
20081
20101
20111
20122
20151
20221
20261
See all 20 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 ('41951'))
  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 · 1

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 ('41951'))
  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 · 0

No aircraft currently registered with this engine model

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 · 10

SDR CA110908005Hose · ruptured(CAN) PILOT NOTICED LOW FUEL PRESSURE AND POWER LOSS ON NR2 ENGINE DURING CLIMBOUT. PILOT SELECTED FUEL BOOST PUMP "ON" WITH NO IMPROVEMENT IN PERFORMANCE OR INCREASE IN FUEL PRESSURE. PILOT ELECTED TO RETURN TO BASE. ACFT LANDED AND TAXIED TO HANGAR WITHOUTSep 7, 2011 · Aircraft Fuel Distribution SystemSDR CA091020006Line · ruptured(CAN) PILOT DECLARED EMERGENCY UPON DISCOVERING HYD SYS FAILURE AND LANDED. AFTER LANDING, THE PILOT HAD NO CONTROL OF NOSE WHEEL STEERING OR BRAKES AND ACFT VEERED OFF THE RUNWAY TO RT, ONTO GRASS AND A DITCH. THE RT MLG BROKE OFF CAUSING CONSIDERABLE DAMAGE Sep 2, 2009 · Gulstm 680FLP · Hydraulic System, MainSDR CA090819007Rivet · corrodedACFT IS HANGARED. ACFT WAS NOTED TO HAVE MISSING RIVET (HEAD) AT LT WS 24-54. LWR SPAR CAP AREA. TCAC WAS CONTACTED AND WE WERE ADVISED TO REPLACE RIVETS AND INSPECT THE AREA IAW TCAC SB 208A. ULTRASONIC INSP WAS COMPLETED BETWEEN WS 24 - WS 52. AVERAGE FLAug 4, 2009 · Gulstm 680F · Wing Main, Frame StructureSDR AUS20031061Ignition Lead · faulty(AUS) RT ENGINE NR 7 CYLINDER LOWER IGNITION LEAD DEFECTIVE AT SPARK PLUG END.Oct 20, 2003 · Gulstm 680FLP · Ignition Harness (Distribution)SDR AUS20030973Pin · cracked(AUS) LT AND RT MAIN LANDING GEAR ACTUATOR CLEVIS PINS CRACKED.Sep 15, 2003 · Gulstm 680FL · Landing Gear ActuatorSDR AUS20011373Bearing · delaminated(AUS) ENGINE NO1 MAIN BEARING DELAMINATED. METAL CONTAMINATION OF OIL FILTER.Dec 18, 2001 · Gulstm 680FL · Reciprocating Engine Power SectionSDR AU000424Cooler · cracked(AUS) RIGHT ENGINE OIL COOLER LEAKING FROM PREVIOUS WELD REPAIR.May 30, 2000 · Gulstm 680FL · Engine Oil CoolerSDR AU971386Blade · cracked(AUS) PROPELLER BLADE CRACKED. CRACK ORIGINATED FROM A NICK IN THE BLADE LOCATED APPROXIMATELY 76.2MM (3IN) FROM THE BLADE TIP.CRACK LENGTH 12.7MM (0.5IN). SUSPECT THE CRACK WAS INITIATED BY A PIECE OF METAL WIRE WHICH WAS FOUND IN THE BLADE DURING DRESSING OUOct 7, 1997 · Gulstm 680FLP · Propeller Blade SectionSDR AU960147Gasket · leaking(AUS) ENGINE DRIVEN FUEL PUMP RELIEF VALVE GASKET LEAKINGJan 26, 1996 · Gulstm 680FLP · Engine Fuel DistributionSDR 95ZZZX6763Injector Line · chafedREF TEXTRON SB 342B ISSUED 10-22-93, PAGE 32. CLAMP NR 47, CYL NR 3, RT ENG, FOUND INJECTOR LINE AND IGNITION LEAD BOTH DEEPLY SCORED UNDER CLAMP. SUSPECT CAUSE, INEFFECTIVE CLAMPING ACTION OF CLAMP, PN 71829, WHEN USED WITH SLEEVE TO CLAMP LEAD AND INJECTOROct 30, 1995 · N1414S · Gulstm 680FL · Engine Fuel Distribution
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 = 'IO720B1B'
  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.

STCs that may be installed · 25

Approved for this engine model: the STC’s model list names it on its data sheet, or a series that includes it. The registry doesn’t record which STCs an aircraft has.

See all 25 STCs
Query with SQL
duckdb -csv -c "SELECT s.stc_number, s.description, s.holder, s.status, s.status_date, m.matched_model
  FROM (
    SELECT stc_number, min(matched_model) AS matched_model
    FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet'
    WHERE engine_model_code IN ('41951')
    GROUP BY stc_number
  ) m JOIN 'https://openairdocs.org/data/latest/faa_stc.parquet' s USING (stc_number)
  ORDER BY s.status = 'Current' DESC, s.status_date DESC, s.stc_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.