# Eagle 150B

- Type: Aircraft model (FAA registry)
- Registry code: 0590403
- Manufacturer (registry): EAGLE AIRCRAFT
- Model: 150B
- Aircraft type: Fixed wing single engine
- Category: Airplane
- Engines: 1 · 4 cycle
- Seats: 2
- Weight class: Up to 12,499 lb
- Certification: Light sport
- Data sheet: [TCDS A00005LA](https://openairdocs.org/tcds/A00005LA) (OpenAirDocs)
- Holder: CTRM Aviation Sdn. Bhd.
- Registered aircraft: 1
- Page: https://openairdocs.org/model/eagle-150b

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

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2007-23-06](https://openairdocs.org/ad/2007-23-06): Severe exfoliation corrosion on Wing/ Canard Flap Hinges · CTRM Aviation Sdn. Bhd. 150B. Effective Dec 11, 2007
- [AD 2007-04-02](https://openairdocs.org/ad/2007-04-02): Canard inboard flap hinge support brackets · CTRM Aviation Sdn. Bhd. 150B. Effective Mar 21, 2007
- [AD 2005-05-14](https://openairdocs.org/ad/2005-05-14): Co-pilot rudder pedal assembly · CTRM Aviation Sdn. Bhd. 150B. Effective Apr 22, 2005
- [AD 2004-26-01](https://openairdocs.org/ad/2004-26-01): Inspect the port and starboard undercarriage attach bracket · CTRM Aviation Sdn. Bhd. 150B. Effective Jan 31, 2005
- [AD 2003-19-07](https://openairdocs.org/ad/2003-19-07): Canard rear spar · CTRM Aviation Sdn. Bhd. 150B. Effective Nov 3, 2003
- [AD 2002-02-01](https://openairdocs.org/ad/2002-02-01): Throttle Control Assembly · CTRM Aviation Sdn. Bhd. 150B. Effective Mar 21, 2002
- [AD 2001-09-16](https://openairdocs.org/ad/2001-09-16): Rudder Cables · CTRM Aviation Sdn. Bhd. 150B. Effective Jun 29, 2001

Historical (superseded or no longer in force):

- [AD 2004-11-04](https://openairdocs.org/ad/2004-11-04) (historical): Canard inboard flap hinge support brackets · CTRM Aviation Sdn. Bhd. 150B. Effective Jun 4, 2004

## Registered aircraft (1)

- [N156EA](https://openairdocs.org/aircraft/N156EA): [Mcdonald David R](https://openairdocs.org/faa-owner/MCDONALD%20DAVID%20R), [Eagle Rock, MO](https://openairdocs.org/faa-place/MO/Eagle%20Rock), built 2000, S/N 031

## STCs approved for it (300, first 50)

- [STC SA00034WI](https://openairdocs.org/stc/SA00034WI): Installation of flap and aileron gap seals.. Flight Enhancements
- [STC SA00061LA](https://openairdocs.org/stc/SA00061LA): Installation of JPI digital tachometer.. J P Instruments
- [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics International Inc.
- [STC SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation
- [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector.. Alcor LLC
- [STC SA00088WI](https://openairdocs.org/stc/SA00088WI): Installation of replacement stabilizer and elevator tips.. Curry Aviation LLC
- [STC SA00103BO](https://openairdocs.org/stc/SA00103BO): Installation of Weemax cabin air vent.. Victor Morrel
- [STC SA00149BO](https://openairdocs.org/stc/SA00149BO): Installation of Aircraft Components, Inc. Volt and Vac Alert System, P/N 2044-1. Aircraft Components Inc
- [STC SA00161BO (1 OF 3)](https://openairdocs.org/stc/SA00161BO%20(1%20OF%203)): Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.. Avidyne Corporation
- [STC SA00162SE](https://openairdocs.org/stc/SA00162SE): Installation of telemetry antennas.. US Dept of Interior
- [STC SA00211AT](https://openairdocs.org/stc/SA00211AT): Installation of carbon steel brake discs that have melonite surface treatment.. Aviation Products, Inc
- [STC SA00212AT](https://openairdocs.org/stc/SA00212AT): Installation of carbon steel brake discs that have melonite surface treatment.. Aviation Products, Inc
- [STC SA00215NY](https://openairdocs.org/stc/SA00215NY): Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system.. CAVU Products Limited
- [STC SA00238SE](https://openairdocs.org/stc/SA00238SE): Installation of Aviation Development Corporation's sump mounted chip detector. Aviation Development Corporation
- [STC SA00243BO (2 OF 5)](https://openairdocs.org/stc/SA00243BO%20(2%20OF%205)): Installation of Centurion Consulting, Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100), or without roll steering (p/n 0025-5200).. Icarus Avionics, LLC
- [STC SA00269BO](https://openairdocs.org/stc/SA00269BO): Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ), Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1, and Avidyne Mounting Tray P/N 700-00034-000.. Avidyne Corporation
- [STC SA00270WI](https://openairdocs.org/stc/SA00270WI): Installation of fiberglass replacement wing tips.. Aircraft Development Co
- [STC SA00281BO](https://openairdocs.org/stc/SA00281BO): Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ), Sensor Systems Inc. Antenna P/N S67-1575-109, or equivalent, and optional Avidyne Mounting Tray P/N 700-00165-000. Avidyne Corporation
- [STC SA00284AT](https://openairdocs.org/stc/SA00284AT): Installation of battery access door and elevator trim pulley access door. (Landplanes and Seaplanes 150 hp only). Brubaker Conversion Co, Inc
- [STC SA00285AT](https://openairdocs.org/stc/SA00285AT): Installation of ground power receptacle. (Landplanes and seaplanes 150 hp only). Brubaker Conversion Co, Inc
- [STC SA00290BO](https://openairdocs.org/stc/SA00290BO): Installation of Avidyne Corporation Part Number  700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXX. Avidyne Corporation
- [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation
- [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies
- [STC SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation
- [STC SA00393SE](https://openairdocs.org/stc/SA00393SE): Installation of the G/S 2500 and G/S2500R Aircraft Security Alarm System.. Protective Technologies Int
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA00402SE](https://openairdocs.org/stc/SA00402SE): Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed). Aviation Development Corporation
- [STC SA00406WI](https://openairdocs.org/stc/SA00406WI): Installation of replacement flap trailing edge bulbs with AOG Drawing. Athena Aircraft, LLC
- [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation
- [STC SA00432SE](https://openairdocs.org/stc/SA00432SE): Installation of EGT 701 series fuel flow instrument.. J P Instruments
- [STC SA00648SE](https://openairdocs.org/stc/SA00648SE): Fabrication of R.M.D. Aircraft Lighting, Inc., wing-tip and landing light Kit No. 00190-C.. Knots 2U Ltd.
- [STC SA00680SE (3 OF 6](https://openairdocs.org/stc/SA00680SE%20(3%20OF%206): Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.. Electronics International
- [STC SA00709CH](https://openairdocs.org/stc/SA00709CH): Installation of replacement wing root vent described by Dwg Nos. 8-30-96-1& 8-30-96-2, no rev, both dtd 8/30/96, or later FAA app rev.. Flight Products, Inc
- [STC SA00709LA](https://openairdocs.org/stc/SA00709LA): Installation of control wheel. Includes provisions only for a push-to-talk (PTT) switch. Separate FAA approval of PTT switch is required.. Trevor Burward-Hoy
- [STC SA00709SE](https://openairdocs.org/stc/SA00709SE): Installation of replacement control surface skin panels.. Athena Aircraft, LLC
- [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance  Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine
- [STC SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance  Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine
- [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance  Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine
- [STC SA00780SE](https://openairdocs.org/stc/SA00780SE): Installation of the True Lock Safety Retention Axle Lock Nut System. True Lock LLC
- [STC SA00812CH](https://openairdocs.org/stc/SA00812CH): Replace Cessna Sun Visor assemblies with Aircraft Replacement Fabricated Components tinted Sun Visor Assemblies.. Vantage Plane Plastic Ltd
- [STC SA00861SE](https://openairdocs.org/stc/SA00861SE): Installation of J.P. Instruments (JPI) fuel flow indicating system. J P Instruments
- [STC SA00871SE](https://openairdocs.org/stc/SA00871SE): Installation of cockpit sunvisors. Rosen Sunvisor Systems LLC
- [STC SA00897WI](https://openairdocs.org/stc/SA00897WI): Installation of Concorde Battery Corporation (VRSLA) Valve regulated sealed lead acid battery.. Aero-Mach Wilco LLC
- [STC SA00954SE (1 OF 2)](https://openairdocs.org/stc/SA00954SE%20(1%20OF%202)): Installation of J.P. Instruments (JPI) Primary Temperature Indicating System in accordance with JPI Installation Manual for the EDM 711, Report 106P, Revision B, dated August 2, 2001, or later FAA approved revision.. J P Instruments
- [STC SA01005DE](https://openairdocs.org/stc/SA01005DE): Installation of a EarthX ETX900-TSO Lithium battery. EarthX Inc.
- [STC SA01015SE](https://openairdocs.org/stc/SA01015SE): Installation of eligible Alaska Bushwheel, Inc. wheels and TSO-C62d tires. ABI LLC
- [STC SA01026SE](https://openairdocs.org/stc/SA01026SE): Improved fuel gascolator assembly.. Steve's Aircraft
- [STC SA01032WI](https://openairdocs.org/stc/SA01032WI): Installation of external aerodynamic Vortelator Kit on airplanes. Aircraft Development Co
- [STC SA01077SE](https://openairdocs.org/stc/SA01077SE): Installation of fluoropolymer film.. Columbia Pacific Airlines
- [STC SA01105WI-D (1 OF 2)](https://openairdocs.org/stc/SA01105WI-D%20(1%20OF%202)): Installation of Bendix/King KMD 550/850 Multi-Function Display System with Optional Traffic, Terrain and Weather Sensors.  This STC also is approved for some single-engine aircraft.  See SA01105WI-D (2 of 2).. Honeywell International Inc.

All 300: https://openairdocs.org/model/eagle-150b/stcs.md

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (9)

As reported by operators and repair stations, by the model named in the report.

- [SDR 2013FA0000253](https://openairdocs.org/sdr/2013FA0000253), Apr 27, 2013: BULKHEAD. CRACKED. FUSELAGE TAILCONE BULKHEAD, FOUND TO BE CRACKED IN BEND RADIUS AT BOTH RUDDER STOP BOLT LOCATIONS. BULKHEAD REINFORCEMENT PLATE, PN 0412181-1, FOUND TO BE CRACK
- [SDR 2012FA0000528](https://openairdocs.org/sdr/2012FA0000528), Aug 2, 2012: BLOCK. CORRODED. CORROSION FOUND ON FORWARD AND AFT WING SPARS UNDER FUEL TANK SPACER BLOCKS, IN FUEL TANK MOUNTING BAY. PROBLEM DISCOVERED WHEN FUEL TANKS WERE REMOVED FOR REPA
- [SDR 2004FA0000191](https://openairdocs.org/sdr/2004FA0000191), Feb 11, 2004: SKIN. CRACKED. REMOVED HORIZONTAL STABILIZER FOR TAILCONE REPAIR. FOUND TWO 1.5 INCH CRACKS RADIATING FROM LOWER FORWARD CORNER OF TAIL CONE SKIN WHERE BOTTOM OF HORIZONTAL LE
- [SDR 2004FA0000190](https://openairdocs.org/sdr/2004FA0000190), Feb 11, 2004: SKIN. CRACKED. REMOVED HORIZONTAL STABILIZER FOR TAILCONE REPAIR. FOUND TWO 1.5 INCH CRACKS RADIATING FROM LOWER FORWARD CORNER OF TAIL CONE SKIN WHERE BOTTOM OF HORIZONTAL LE
- [SDR AQF2002F00000](https://openairdocs.org/sdr/AQF2002F00000), Jul 6, 2002: CYLINDER. CRACKED. LOOKING FOR OIL LEAK. FOUND CRACK INSIDE CYLINDER ABOUT MIDWAY. CIRCULAR COVERING APPROXIMATELY 30 PERCENT OF RADIUS. 1600 HOURS SMOH
- [SDR AU010172](https://openairdocs.org/sdr/AU010172), Mar 5, 2001: COMPASS. OUT OF ADJ. (AUS) COMPASS SWING OUT OF DATE. NO COMPASS CORRECTION CARD FITTED.
- [SDR AU000817](https://openairdocs.org/sdr/AU000817), Sep 7, 2000: FITTING. CORRODED. (AUS) LEFT AND RIGHT WING REAR ATTACHMENT FITTINGS CORRODED. (X)
- [SDR CA000329005](https://openairdocs.org/sdr/CA000329005), Mar 21, 2000: SPAR. CORRODED. (CAN) THE AIRCRAFT WINGS WERE REMOVED FOR A DETAILED INSPECTION AND HEAVY INTERGRANULAR CORROSION WAS FOUND ON THE INBOARD FACE OF THE FUSELAGE REAR SPAR CARRY 
- [SDR AU970565](https://openairdocs.org/sdr/AU970565), May 5, 1997: PISTON PIN. GALLED. (AUS) PISTON PIN PLUG LOOSE AND GALLING ON CYLINDER BORE

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Cessna 150B](https://openairdocs.org/model/cessna-150b): 111 registered aircraft, registry code 2071806
- [Eagle EAGLE 150B](https://openairdocs.org/model/eagle-eagle-150b): 6 registered aircraft, registry code 05607TE

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