# Akrotech Europe CAP 10B

- Type: Aircraft model (FAA registry)
- Registry code: 0950104
- Manufacturer (registry): AKROTECH EUROPE
- Model: CAP 10B
- Aircraft type: Fixed wing single engine
- Category: Airplane
- Engines: 1 · Reciprocating
- Seats: 2
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS A36EU](https://openairdocs.org/tcds/A36EU) (OpenAirDocs)
- Holder: CEAPR
- Registered aircraft: 0
- Page: https://openairdocs.org/model/akrotech-europe-cap-10b

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 2011-06-01](https://openairdocs.org/ad/2011-06-01): Flight Controls · APEX CAP 10 B. Effective Apr 13, 2011
- [AD 2008-17-07](https://openairdocs.org/ad/2008-17-07): Flight controls tie rod · APEX CAP 10 B. Effective Sep 23, 2008
- [AD 2008-13-32](https://openairdocs.org/ad/2008-13-32): Luggage compartment · APEX CAP 10 B. Effective Aug 12, 2008
- [AD 2008-09-02](https://openairdocs.org/ad/2008-09-02): Upper spar flange inspection · APEX CAP 10 B. Effective May 27, 2008
- [AD 2008-07-05](https://openairdocs.org/ad/2008-07-05): Front fuel tank · APEX CAP 10 B. Effective Apr 30, 2008
- [AD 2008-07-04](https://openairdocs.org/ad/2008-07-04): Control stick base cover · APEX CAP 10 B. Effective Apr 30, 2008
- [AD 2007-13-14](https://openairdocs.org/ad/2007-13-14): Lower rudder support · APEX CAP 10 B. Effective Aug 3, 2007
- [AD 2007-10-13](https://openairdocs.org/ad/2007-10-13): Aileron spades · APEX CAP 10 B. Effective Jun 21, 2007
- [AD 2007-09-05](https://openairdocs.org/ad/2007-09-05): Reduced elevator deflection · APEX CAP 10 B. Effective Jun 4, 2007
- [AD 2007-09-06](https://openairdocs.org/ad/2007-09-06): Central wing spar block · APEX CAP 10 B. Effective May 21, 2007
- [AD 91-23-03](https://openairdocs.org/ad/91-23-03): Fuel System · APEX CAP 10 B. Effective Dec 10, 1991

Historical (superseded or no longer in force):

- [AD 2003-04-02](https://openairdocs.org/ad/2003-04-02) (historical): Inspection Opening in Wing · APEX CAP 10 B. Effective Apr 4, 2003
- [AD 99-21-23](https://openairdocs.org/ad/99-21-23) (historical): Flight Manual - Airspeed · APEX CAP 10 B. Effective Dec 3, 1999
- [AD 98-12-10](https://openairdocs.org/ad/98-12-10) (historical): Wing Main Spar · APEX CAP 10 B. Effective Jul 17, 1998
- [AD 93-10-11](https://openairdocs.org/ad/93-10-11) (historical): Wing Spar · APEX CAP 10 B. Effective Jul 23, 1993

## Information bulletins (advisory) (7)

- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-14-01](https://openairdocs.org/saib/CE-14-01): Placards and Markings: Flat Spin Recovery and Aircraft Flight Manual (AFM) Revision of CAP 10B Aeroplanes. Issued Nov 4, 2013
- [SAIB CE-05-54](https://openairdocs.org/saib/CE-05-54): . Issued May 24, 2005
- [SAIB CE-05-52](https://openairdocs.org/saib/CE-05-52): . Issued May 9, 2005
- [SAIB CE-04-82](https://openairdocs.org/saib/CE-04-82): . Issued Aug 27, 2004
- [SAIB CE-04-42](https://openairdocs.org/saib/CE-04-42): . Issued Jan 8, 2004
- [SAIB ACE-98-34](https://openairdocs.org/saib/ACE-98-34): . Issued Jun 4, 1998

## Registered aircraft

None registered with this model now.

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (15)

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

- [SDR AUS20040188](https://openairdocs.org/sdr/AUS20040188), Mar 16, 2004: FCU. CONTAMINATED. (AUS) FUEL CONTROL UNIT FINGER FILTER CONTAMINATED. WORKSHOP INSPECTION FOUND A FINE HAIR LIKE SUBSTANCE.
- [SDR AUS20030029](https://openairdocs.org/sdr/AUS20030029), Jan 14, 2003: WING. FAULTY. (AUS) LH AILERON INBOARD FORWARD EDGE BINDING ON TRAILING EDGE OF LOWER WING SKIN. SUSPECT MANUFACTURING ERROR.
- [SDR AUS20020705](https://openairdocs.org/sdr/AUS20020705), Jul 8, 2002: FITTING. CRACKED. (AUS) LH AND RH MAIN LANDING GEAR ATTACHMENT BLOCKS CRACKED. RH FILLERDELAMINATED FROM SPAR ADJACENT TO UNDERCARRIAGE ATTACHMENT. FOUND DURING INSPECTION IAW AD
- [SDR AUS20020629](https://openairdocs.org/sdr/AUS20020629), Jun 21, 2002: FITTING. CRACKED. (AUS) LANDING GEAR LH FORWARD INBOARD LOWER AND RH FORWARD OUTBOARD LOWER ATTACHMENT BLOCKS CRACKED. FOUND DURING INSPECTION IAWAD/CAP/4A2.
- [SDR AUS20020612](https://openairdocs.org/sdr/AUS20020612), Jun 18, 2002: CAMSHAFT. WORN. (AUS) CAMSHAFT LOBES AND ASSOCIATED LIFTERS (3OFF) BADLY WORN.
- [SDR AUS20020044](https://openairdocs.org/sdr/AUS20020044), Jan 21, 2002: RELAY. FAULTY. (AUS) STARTER RELAY FAULTY.
- [SDR AUS20020023](https://openairdocs.org/sdr/AUS20020023), Jan 7, 2002: FITTING. CRACKED. (AUS) LH AND RH FORWARD LANDING GEAR ATTACHMENT BLOCKS CRACKED. FOUND DURING INSPECTION IAW AD/CAP10/3.
- [SDR AUS20011136](https://openairdocs.org/sdr/AUS20011136), Oct 25, 2001: SKIN. FRACTURED. (AUS) LH WING LOWER SKINFRACTURED BETWEEN SPARS ADJACENT TO NO3 RIB.CRACK LENGTH 600MM (23.6IN).
- [SDR AU990837](https://openairdocs.org/sdr/AU990837), Aug 18, 1999: FITTING. CRACKED. (AUS) RIGHT MAIN LANDING GEAR ATTACHMENT BLOCK CRACKED FROM LOWER FORWARD INBOARD ATTACHMENT HOLE.
- [SDR AU990577](https://openairdocs.org/sdr/AU990577), Jun 7, 1999: PLUG. FAILED. (AUS) NR 2 PISTON PIN PLUG WORN AWAY. PLUG HAD WORN INTO THE PISTON OIL RING LAND. THE ENGINE WAS INSPECTED AND ALL OTHER PISTON PIN PLUGS WERE FOUND WITH VARIO
- [SDR AU990546](https://openairdocs.org/sdr/AU990546), Jun 4, 1999: PLUG. WORN. (AUS) NR 2 CYLINDER PISTON PIN PLUG WORN. PISTON OIL RING LANDS DAMAGED. METAL CONTAMINATION OF THE ENGINE OIL SYSTEM.
- [SDR AU980363](https://openairdocs.org/sdr/AU980363), Mar 26, 1998: WINDSHIELD. CRACKED. (AUS) FORWARD WINDSCREEN CRACKED. CRACK ORIGINATED FROM A CRACK REPAIR CARRIED OUT IN JULY 1997.
- [SDR 98ZZZX1319](https://openairdocs.org/sdr/98ZZZX1319), Mar 1, 1998: FUEL VALVE. MALFUNCTIONED. REFERENCE: P/N 70-20-00 (91752) INVERTED FUEL VALVE WAS FOUND TO BE INTERMITTENT (HANGS UP). DISASSEMBLY AND INSPECTION FOUND A 'WEAR MARK' ON HOUSING - POSSIBL
- [SDR AU980038](https://openairdocs.org/sdr/AU980038), Jan 14, 1998: FUEL SYSTEM. MALFUNCTION. (AUS) DURING TRAINING CIRCUITS ON DOWNWIND TURN, POWER WAS REDUCED FROM FULL SETTING TO 2000RPM AND THE ENGINE SUFFERED A POWER LOSS AND WOUND DOWN TO 800RPM. S
- [SDR AU971482](https://openairdocs.org/sdr/AU971482), Nov 20, 1997: FITTING. CRACKED. (AUS) LH AND RH FORWARD UNDERCARRIAGE ATTACHMENT BLOCKS CRACKED. FOUND DURING INSPECTION IAW SB15 2(B).

## STCs that may be installed (OpenAirDocs) (22)

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

- [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC
- [STC SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC
- [STC SA04568CH](https://openairdocs.org/stc/SA04568CH): Installation of the uAvionix tailBeaconX, a tail mounted position light with integrated Automatic Dependent Surveillance - Broadcast (ADS-B) Out and 1090MHz Mode-S transponder functionality. uAvionix Corporation
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. 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 SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA03819NY](https://openairdocs.org/stc/SA03819NY): Installation and maintenance of Oratex 6000 Covering and Coating System. Lanitz-Prena Folien Factory GmbH
- [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc
- [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [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 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 SA01435SE](https://openairdocs.org/stc/SA01435SE): Installation of J.P. Instruments (JPI) Primary Engine Data Management System. J. P. Instruments
- [STC SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine
- [STC SA00024NY](https://openairdocs.org/stc/SA00024NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less. Airwolf Filter Corporation
- [STC SA00478CH](https://openairdocs.org/stc/SA00478CH): Installation of Cooper Superflite 102 Fabric. Aviation Products Systems Inc
- [STC SA563CH](https://openairdocs.org/stc/SA563CH): Authorizes installation of engines equipped w/Unison Limited Authority Spark Advance Regulator (LASAR) ignition system w/Cylinder Head Temp. (CHT) monitoring capability on airframes. engines. Champion Aerospace LLC
- [STC SA593CH](https://openairdocs.org/stc/SA593CH): Install Champion SlickSTART magneto booster system. Champion Aerospace LLC
- [STC SA5159NM](https://openairdocs.org/stc/SA5159NM): Installation of chip detector system. Northwest Aircraft Inc
- [STC SA001410BO](https://openairdocs.org/stc/SA001410BO) (historical): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation
- [STC SA00765DE PAGE 1](https://openairdocs.org/stc/SA00765DE%20PAGE%201) (historical): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine

## PMA parts (OpenAirDocs) (22)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [S1069](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131295691720260806152306.0001): 100R Fuel Placard. Swift Fuels, LLC · PMA PQ04423CE · Modification part · Jul 20, 2026
- [73-CFG-R](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123057781520260806152400.0001): Fuel Quantity Indication Placard. Swift Fuels, LLC · PMA PQ04423CE · Modification part · Jul 20, 2026
- [UAV-1004236-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147327119520230707211229.0001): AV-30-C. uAvionix Corporation · PMA PQ05445NM · Modification part · Jun 28, 2023
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID547411912220210702175212.0001): Aspen Avionics · PMA PQ03868SW · Jan 20, 2021
- [V674UL94](https://drs.faa.gov/browse/excelExternalWindow/26465837A7672E7A86258583004BE923.0001): UL94 Fuel Placard. Swift Fuels, LLC · PMA PQ04423CE · Modification part · Nov 25, 2019
- [9100-001-C](https://drs.faa.gov/browse/excelExternalWindow/DD343890DCD8BFDB86258569004013FB.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-D](https://drs.faa.gov/browse/excelExternalWindow/C7B6725B325949E98625856900401478.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9200-000-B](https://drs.faa.gov/browse/excelExternalWindow/BD58B0712CA0C6AA86258569004016AD.0001): MaxPulse Landing Light Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-G](https://drs.faa.gov/browse/excelExternalWindow/ADE62C91D97E8B788625856900401557.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-E](https://drs.faa.gov/browse/excelExternalWindow/A37F050253EE808A86258569004014BA.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9200-000-A](https://drs.faa.gov/browse/excelExternalWindow/8E10EF4D973C1D6D8625856900401662.0001): MaxPulse Landing Light Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-A](https://drs.faa.gov/browse/excelExternalWindow/62DC748A2B9B1D9386258569004012FD.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-F](https://drs.faa.gov/browse/excelExternalWindow/3746AAB4CC0D6883862585690040151B.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-B](https://drs.faa.gov/browse/excelExternalWindow/32446D71EB78157686258569004013B2.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [B-00371-1](https://drs.faa.gov/browse/excelExternalWindow/DEA0CACA14E9BB0886257AB60074824B.0001): Alternator Control, 14V. Lamar Technologies LLC · PMA PQ2242NM · Replaces B-00371-16 · Oct 28, 2012
- [B-00371-1](https://drs.faa.gov/browse/excelExternalWindow/FC280121F062576386257AB60073239C.0001): Alternator Control, 14V. Lamar Technologies LLC · PMA PQ2242NM · Replaces B-00371-16 · Dec 14, 2010
- [SF-D](https://drs.faa.gov/browse/excelExternalWindow/F09A70034CB3EF9885257038006C5719.0001): System II Finish Materials Kit. AAR Distribution · Modification part · Mar 6, 2001
- [SF-P](https://drs.faa.gov/browse/excelExternalWindow/9C365425FEB43FE985257038006C5723.0001): Standard System Finish Materials Kit. AAR Distribution · Modification part · Mar 6, 2001
- [SF-102](https://drs.faa.gov/browse/excelExternalWindow/8549C874FBB403AB85257038006C5709.0001): Fabric. AAR Distribution · Modification part · Mar 6, 2001
- [SF-C](https://drs.faa.gov/browse/excelExternalWindow/2D5350BB7885975385257038006C5711.0001): Dope Finish Materials Kit. AAR Distribution · Modification part · Mar 6, 2001
- [SS-1001](https://drs.faa.gov/browse/excelExternalWindow/C7E32203B0D0EC7E8525704C00570B73.0001): Slick START TM Installation. Slick Aircraft Products, Division of Unison Ind · Modification part · Dec 2, 1997
- [K-1001](https://drs.faa.gov/browse/excelExternalWindow/79670B8722A2299A8525704C00516146.0001): Slick START TM Installation. Slick Aircraft Products, Division of Unison Ind · Modification part · Dec 2, 1997

## The same model under other registry codes

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

- [Avions Mudry ET Cie CAP 10B](https://openairdocs.org/model/avions-mudry-et-cie-cap-10b): 22 registered aircraft, registry code 0950102
- [Constructions Aeronautiques D CAP 10B](https://openairdocs.org/model/constructions-aeronautiques-d-cap-10b): 0 registered aircraft, registry code 0950106

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