Beech M35

Aircraft model · Fixed wing single engine · Airplane · registry code 1151526

Manufacturer (registry)
BEECH
Model
M35
Registry code
1151526
Registered
225 aircraft
Type
Fixed wing single engine
Engines
1 · Reciprocating
Seats
5
Weight class
Up to 12,499 lb
Cruise speed
150 mph
Certification
Type certificated
Data sheet
TCDS3A15
Holder
Textron Aviation Inc.

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

On this page

Aircraft by year built · 301

1958Registered nowDeregistered2026
Aircraft by the year they were built: 301 aircraft
19581
195978
1960218
19612
19731
19961

Airworthiness directives that may apply · 24

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

1970In forceSuperseded2026
ADs by the year they took effect: 29 ADs
19701
19723
19752
19811
19841
19891
19941
19951
19961
19972
19981
19991
20002
20012
20021
20031
20051
20071
20191
20221
20232
20241
See all 29 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_aircraft_model_directive.parquet' WHERE aircraft_model_code IN ('1151526'))
  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 · 5

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 ('1151526'))
  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 · 225

See all 225 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 ('1151526')
  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.

STCs approved for this model · 419

See all 419 STCs
Query with SQL
duckdb -csv -c "SELECT s.stc_number, s.description, s.holder, s.status, s.status_date
  FROM 'https://openairdocs.org/data/latest/faa_stc.parquet' s
  WHERE s.stc_number IN (SELECT stc_number FROM 'https://openairdocs.org/data/latest/faa_stc_model.parquet' WHERE model_key = 'M35')
  ORDER BY s.status = 'Current' 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.

NTSB investigations · 147

Aircraft matched to this model through the registry, by N-number and event date.

See all 147 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 ('1151526')
  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 · 219

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

See all 219 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 ('1151526')
  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 · 14

SDR 2011FA0000306Hub · crackedTHE PROPELLER WAS INSPECTED FOR COMPLETE O/H AND THE HUB WAS FOUND TO HAVE A CRACKED BLADE RETENTION THREADS. THIS MODEL OF PROPELLER HAS A HISTORY OF CRACKING AND THE MFG HAS ADDED APROVISION TO RED DYE OIL, FILL THE PROPELLER FOR EARLY CRACK DETECTION, THE May 6, 2011 · N389Z · Beech M35 · Propeller Hub SectionSDR 2011FA0000117Structure · crackedPERFORMED INSP IAW MFG SAFETY COMUNIQUE NR 313 / FAA SAIB CE-11-21. FOUND RT FLAP L/E CRACKED (ABOUT 1.5 IN LONG) IN THE VICINITY OF THE "FLAP ACTUATOR BRACKET". FURTHER FOUND NOSE RIB CRACKED AS WELL. REMOVED FLAP FOR REPAIRS.Feb 18, 2011 · N9893R · Beech M35 · Trailing Edge FlapsSDR 2011FA0000116Structure · crackedPERFORMED INSP IAW SAFETY COMUNIQUE NR 313. FOUND RT FLAP L/E CRACKED (ABOUT 1.5 INCH LONG) IN THE VICINITY OF THE "FLAP ACTUATOR BRACKET". FURTHER FOUND NOSE RIB CRACKED AS WELL. REMOVED FLAP FOR REPAIRS.Feb 18, 2011 · N9893R · Beech M35 · Leading Edge DevicesSDR 2005FA0000983Rod End · defectiveTHE BEARING END PARTED FROM THE THREAD PORTION OF THE ROD END, CAUSING COLAPSE OF THE NOSE LANDING GEAR. THE DEFECT APPEARED ON ROLL OUT AFTER LANDING, WHEN THE NOSE GEAR COLLAPSED. STRUCTURAL FAILURE OF THE ROD END. (SW15200512716) (K)May 5, 2005 · N374Z · Beech M35 · Landing Gear Retraction/Extension SystemSDR 2005FA0000347Brace · corrodedFIND A HIGH PERCENTAGE OF THESE PARTS CORRODED ABOVE THE LOWER BUSHING IN THE GROVE WHERE THE FELT FITS. THIS PART IS MADE OF MAGNESUM SO THE MOISTURE RETAINED BY THE FLET AND GREASE ALLOWS PART TO CORROD. MFG ALLOWS ONLY 10 PERCENT OF WALL THICKNESS TO BE RFeb 18, 2005 · Beech M35 · Main Landing GearSDR 2004FA0000365Cable · brokenSTARTER CABLE PN 52621 BROKEN AT THE LUG CONNECTED TO THE STARTER.Mar 29, 2004 · N136X · Beech M35 · Electrical ConnectorsSDR 2004FA0000226Diaphragm · crackedFUEL DIAPHRAGM ON THE FUEL MANIFOLD VALVE SHOWED DETERIORATION DUE TO AGEING. FUEL LEAKED OUT OF THE AIR BLEED HOLE ON THE FUEL MANIFOLD VALVE, CAUSING ENGINE FUEL FLOW PROBLEMS. ADDITIONAL INSPECTIONS AFTER PROLONGED STORAGE.Feb 10, 2004 · N762AA · Beech M35 · Engine Fuel DistributionSDR CA030430004Cylinder · cracked(CAN) NR 4 CYLINDER, ON INVESTIGATION DURING LEAK, DOWN TEST NOTED LOW COMPRESSION AND LEAKAGE IN EXHAUST PORT. CYLINDER REMOVED AND CRACK FOUND IN EXHAUST PORT. THIS ENGINE TYPE NOTED FOR HIGH CYLINDER FAILURE RATE. CYLINDER SCRAPPED.Apr 30, 2003 · Beech M35 · Reciprocating Engine Cylinder SectionSDR 2002FA0000546Battery · shortedLANDING GEAR FAILED TO EXTEND ALL THE WAY. AIRCRAFT LOST ELECTRICAL POWER. REMOVED BATTERY AND FOUND LOW VOLTS WITH NO CAPACITY, BATTERY WOULD NOT CHARGE ON BENCH INTERNALLY SHORTED INSTALLED NEW BATTERY, AIRCRAFT AND FOUND. FIELD CIRCUIT BREAKER POPPED RESApr 16, 2002 · N711DU · Beech M35 · Battery/Charger SystemSDR 20010228CW003Crankcase · crackedDURING ANNUAL INSP, OIL LEAK NOTED AT TOP OF CRANKCASE, CLEANING AND RERUN, OIL LEAK RETURNED. FOUND 1.25 IN CRACK EXTENDING FROM TOP CENTER CASE BOLT HOLE AT AREA WHERE FUEL FLOW DIVIDER BRACKET ATTACHES. CRACK IN NON-CRITICAL AREA AND WITHIN CRACK LIMITATIFeb 1, 2001 · N9748R · Beech M35 · Reciprocating Engine Power SectionSDR 99ZZZX4181Brace · crackedALTERNATOR FAILED EN ROUTE. INSPECTION REVEALED THE FIELD WIRE BROKE LOOSE FROM ALTERNATOR MOST LIKELY DUE TO A CRACKED ALTERNATOR SUPPORT BRACE BEING CRACKED ALLOWING THE ALTERNATOR TO VIBRATE.Oct 25, 1999 · N681V · Beech M35 · DC Generator-AlternatorSDR 98ZZZX995Bracket · failedDURING NORMAL ANNUAL INSPECTION, FOUND BOTH ENGINE MOUNTS BROKEN THROUGH THE MIDDLE. THIS CAUSED ENGINE TO LAY FARTHER DOWN ON ITS LEFT SIDE CAUSING FURTHER DAMAGE TO VALVE COVERS, COWLING, INTAKE MANIFOLD. MOUNTS HAD BROKEN SINCE LAST OIL CHANGE APPROXIMATEFeb 2, 1998 · N9880R · Beech M35 · Engine Mount SectionSDR 97ZZZX837Bolt · corrodedAIRCRAFT INSPECTION FOUND 1 WING BOLT CORRODED AND OTHERS WITH SOME PITTING. ACFT HAD NEVER HAD BOLTS INSPECTED. BEECH MM GIVES BOLTS AND HARDWARE REPLACEMENT AT 15 YRS AND ANTI-CORROSION TREATMENT. MM ALSO STATES BOLTS TO BE MAGNAFLUXED AND CORROSION TREATFeb 12, 1997 · N9580R · Beech M35 · Wing, Attach FittingsSDR AU960230Support · failed(AUS) PROPELLER SPINNER SUPPORT FAILED - SPINNER BULKHEAD CRACKED - THIS IS THE SECOND SIMILAR OCCURRENCE ON THIS AIRCRAFT (LAST TIMEIN AUGUST 1992) - SUSPECT CAUSED COMBINATION OF OUT OF BALANCE PROPELLER AND LOSS OF PRELOAD DUE TO EXCESSIVE HOURS BETWEEN INFeb 22, 1996 · Beech M35 · Propeller Spinner 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 aircraft_model_key = 'M35'
  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.