# Extra Flugzeugproduktions-Und EA300/L (EXTRA)

- Type: Aircraft model (FAA registry)
- Registry code: 70218DS
- Manufacturer (registry): EXTRA FLUGZEUGPRODUKTIONS-UND
- Model: EA300/L (EXTRA)
- 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 A67EU](https://openairdocs.org/tcds/A67EU) (OpenAirDocs)
- Holder: Extra Flugzeugproduktions- und Vertriebs- GmbH
- Registered aircraft: 1
- Page: https://openairdocs.org/model/extra-flugzeugproduktions-und-ea300-l-extra

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 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022
- [AD 2010-04-11](https://openairdocs.org/ad/2010-04-11): Fuselage · Extra Flugzeugproduktions- und Vertriebs- EA-300L and EA-300/200. Effective Mar 30, 2010
- [AD 2007-02-11](https://openairdocs.org/ad/2007-02-11): Upper longeron · Extra Flugzeugproduktions- und Vertriebs- EA-300, EA-300L, EA-300S and 1 more. Effective Feb 28, 2007
- [AD 2005-11-07](https://openairdocs.org/ad/2005-11-07): Bottom fuselage cover (belly fairing) and the firewall · Extra Flugzeugproduktions- und Vertriebs- EA-300, EA-300L, EA-300S and 1 more. Effective Jul 18, 2005
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2003-17-02](https://openairdocs.org/ad/2003-17-02): Fuel selector valve · Extra Flugzeugproduktions- und Vertriebs- EA-300L, EA-300S and EA-300/200. Effective Oct 10, 2003
- [AD 98-24-07](https://openairdocs.org/ad/98-24-07): Rudder Pedal Footrest · Extra Flugzeugproduktions- und Vertriebs- EA-300, EA-300L and EA-300S. Effective Dec 28, 1998

## Information bulletins (advisory) (6)

- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-12-01](https://openairdocs.org/saib/CE-12-01): Flight Controls: Rudder Cable Maintenance. Issued Oct 24, 2011
- [SAIB CE-04-79](https://openairdocs.org/saib/CE-04-79): . Issued Aug 27, 2004
- [SAIB CE-03-14](https://openairdocs.org/saib/CE-03-14): . Issued Dec 31, 2002
- [SAIB CE-98-04R1](https://openairdocs.org/saib/CE-98-04R1): . Issued Jul 24, 1998
- [SAIB ACE-98-04](https://openairdocs.org/saib/ACE-98-04): . Issued Oct 17, 1997

## Registered aircraft (1)

- [N30VP](https://openairdocs.org/aircraft/N30VP): [International Air Services Inc Trustee](https://openairdocs.org/faa-owner/INTERNATIONAL%20AIR%20SERVICES%20INC%20TRUSTEE), [Carson City, NV](https://openairdocs.org/faa-place/NV/Carson%20City), S/N 1266

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (19)

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

- [SDR 2022FA0000050](https://openairdocs.org/sdr/2022FA0000050), Jan 13, 2022: BRAKE PADS. LOOSE. THE EXTRA 300L UTILIZES A CLEVELAND BRAKE ASSY PN# 30-164 AND CLEVELAND WHEEL ASSEMBLY 40-151. WE FOUND THAT WHEN WE REPLACE THE BRAKE PADS WITH PMA RAPCO BRAKE
- [SDR CA151214007](https://openairdocs.org/sdr/CA151214007), May 3, 2015: BLADE. LOOSE. (CAN) BLADES WERE FOUND LOOSE DURING PRE-FLIGHT INSPECTION IN HUB. PROP TOTAL TIME SINCE NEW 75.8. PROPELLER WAS REMOVED AND SENT FOR TEAR DOWN INSPECTION. PROP
- [SDR 2008FA0000495](https://openairdocs.org/sdr/2008FA0000495), May 25, 2008: FUEL SYS. MALFUNCTIONED. APPROX 9 GALLONS OF FUEL IN CENTER TANK BECAME INACCESSIBLE DURING FLT, PRECAUTIONARY LANDING. AFTER DEPARTING USING CENTER TANK FUEL FOR A 120 MILE FERRY FLIGH
- [SDR 2007FA0001042](https://openairdocs.org/sdr/2007FA0001042), Nov 15, 2007: FUEL CONTROL. MALFUNCTIONED. THE AIRCRAFT EXPERIENCED AN INFLIGHT ENGINE SHUTDOWN RESULTING IN A FORCED LANDING ON THE BEACH. THE CAUSE OF THE INFLIGHT ENGINE SHUTDOWN WAS THE INTERNAL FAIL
- [SDR 2005FA0001579](https://openairdocs.org/sdr/2005FA0001579), Dec 14, 2005: LONGERON. CRACKED. DURING ROUTINE 1,000 HR INSPECTION CRACKS WERE FOUND IN THE UPPER LONGERON AT THE HORIZONTAL STABILIZER ATTACHMENT, THESE WERE VERIFIED USING A FLUORESCENT DYE 
- [SDR 2002FA0001224](https://openairdocs.org/sdr/2002FA0001224), Oct 9, 2002: SETSCREW. BACKED OUT. PROPELLER GOVERNOR SET SCREW INSIDE CASE HALVES, BACKED OUT CAUSING A CHAIN REACTION OF ENGINE DAMAGE. ALL MAJOR ENGINE COMPONENTS BROKEN (NON-REPAIRABLE), RESU
- [SDR 2002FA0000575](https://openairdocs.org/sdr/2002FA0000575), May 6, 2002: SKIN. DELAMINATED. WING SKIN DELAMINATION OCCURRED IN FLIGHT. CRACKS IN PAINT AND FUEL SEEPAGE FROM AREA WAS REASON FOR DISCOVERY. DELAMINATION AREA IS 72 INCHES OUTBOARD ON TOP S
- [SDR 2001FA0000353](https://openairdocs.org/sdr/2001FA0000353), Sep 28, 2001: CONTROL CABLE. LOOSE. ROUTINE ANNUAL INSPECTION REVEALED AFT RUDDER CABLE THIMBLE EYES WERE LOOSE IN THE LOOP AT THE ATTACHMENT TO THE RUDDER. THE THIMBLE COULD BE REMOVED FROM THE L
- [SDR 20001012SH027](https://openairdocs.org/sdr/20001012SH027), Sep 25, 2000: GRIP. DISLODGED. ELEVATOR TRIM BALL GRIP CAME OFF IN-FLIGHT. OWNER COMMENTED HE NOTICED RED MARKS ON HIS RIGHT PANTS LEG JUST ABOVE THE KNEE ON SEVERAL OCCASIONS. SUBMITTER SUGG
- [SDR 20001012SH026](https://openairdocs.org/sdr/20001012SH026), Aug 14, 2000: HEAT SHIELD. FAILED. EXHAUST HEAT SHIELD FAILED ITS CLAMP ATTACH TABS. SUBMITTER STATED THIS CONDITION COULD BE CONSIDERED SERIOUS IN THE EVENT A PART FAILS AND BECOMES LOOSE IN THE
- [SDR 20001016SH004](https://openairdocs.org/sdr/20001016SH004), Jul 25, 2000: HEAT SHIELD. LOOSE. EXHAUST HEAT SHIELD FAILED ITS CLAMP ATTACH TABS. THIS CONDITION COULD BE CONSIDERED SERIOUS IN THE EVENT A PART FAILS AND BECOMES LOOSE IN THE ENGINE COMPARTME
- [SDR CA000801023](https://openairdocs.org/sdr/CA000801023), May 31, 2000: COWLING. ELONGATED. (CAN) SAME PROBLEM AS WITH C-GAKN. COWLING IS FALLING OFF DUE TO STRUCTURALLY INADEQUATE FIREWALL.
- [SDR CA000801022](https://openairdocs.org/sdr/CA000801022), May 31, 2000: FIREWALL. LOOSE. (CAN) FIRE WALL NEEDS TO BE STIFFENED.
- [SDR CA000614046](https://openairdocs.org/sdr/CA000614046), May 26, 2000: FUEL TANK. CRACKED. (CAN) FUEL TANK CRACKED ALONG SIDE WHERE WELDED. AUTOMATIC FUEL CATCH SHIELD DID NOT WORK AND GAS DRIPPED INTO CABIN NOT OVERBOARD AS SUPPOSED TO.
- [SDR CA000801021](https://openairdocs.org/sdr/CA000801021), Apr 5, 2000: BLADE. LOOSE. (CAN) LOOSE PROPELLER BLADES.
- [SDR 99ZZZX2475](https://openairdocs.org/sdr/99ZZZX2475), Jun 5, 1999: HOSE. LEAKING. FUEL HOSE CONNECTS FUSELAGE FILLER NECK WITH MAIN FUSELAGE TANK. HOSE SEPARATED FROM TOP OF TANK AT RANGE AND ALLOWED FUEL TO ENTER COCKPIT. HOSE WAS FOUND CUT 
- [SDR CA000801020](https://openairdocs.org/sdr/CA000801020), Oct 1, 1998: PROPELLER. LOOSE. (CAN) LOOSE PROPELLER BLADES.
- [SDR CA000801019](https://openairdocs.org/sdr/CA000801019), Jan 22, 1998: PROPELLER. LOOSE. (CAN) LOOSE PROPELLER BLADES.
- [SDR 97ZZZX4468](https://openairdocs.org/sdr/97ZZZX4468), Sep 25, 1997: SCREEN. BROKEN. THE AIRCRAFT'S COWLING MOUNTED ALUMINUM AIR INTAKE SCREEN FOUND BROKEN ALONG THE UPPER AND LOWER EDGES. THE SCREEN WAS ONLY SECURED ON THE EDGES. FAILURE WOULD 

## STCs that may be installed (OpenAirDocs) (74, first 50)

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 SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc
- [STC SA12428CH](https://openairdocs.org/stc/SA12428CH): Installation of the Lycoming Engines Electronic Ignition System (EIS). Lycoming Engines, An Operating Division of AVCO Corporation
- [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International Inc
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA01005DE](https://openairdocs.org/stc/SA01005DE): Installation of a EarthX ETX900-TSO Lithium battery. EarthX Inc
- [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine
- [STC SA01435LA](https://openairdocs.org/stc/SA01435LA): Installation of engines modified with Firewall Forward Technologies LLC modified camshaft. Centri-Lube Technologies LLC
- [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC
- [STC SA03282CH](https://openairdocs.org/stc/SA03282CH): Installation of MT propeller model MTV-9-B/C/C200-25. McFarlane Aviation LLC
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc
- [STC SA04776NY](https://openairdocs.org/stc/SA04776NY): The HIPEC Covering and Finishing System must be performed and maintained. HIPEC Aircraft Coatings Inc
- [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 SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc
- [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 SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA09920AC](https://openairdocs.org/stc/SA09920AC): Installation of a Hartzell Propeller Inc. model HC-C3YR-4BN/NC8302-7. Hartzell Propeller Inc
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc
- [STC SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation
- [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition 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 SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc
- [STC SA04424AT](https://openairdocs.org/stc/SA04424AT): Installation of Continental Motors, Inc. (CMI) Shower-of-Sparks Starting Vibrator Booster Systems. Continental Motors, Inc
- [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 SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA2586NM](https://openairdocs.org/stc/SA2586NM): Installation of J.P. Instruments temperature monitoring systems. J P Instruments
- [STC SA00382BO](https://openairdocs.org/stc/SA00382BO): Installation of Globalstar Antenna and Cradle provisions to support a Globalstar GPS-1700 in non-composite airplanes. 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 SA03861NY](https://openairdocs.org/stc/SA03861NY): Installation of Main Wheels and Brake System. Beringer Aero
- [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 SA02119SE PAGE 1](https://openairdocs.org/stc/SA02119SE%20PAGE%201): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc
- [STC SA00478CH](https://openairdocs.org/stc/SA00478CH): Installation of Cooper Superflite 102 Fabric. Aviation Products Systems Inc
- [STC SA01229SE PAGE 1](https://openairdocs.org/stc/SA01229SE%20PAGE%201): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc
- [STC SA02442AK PAGE 1](https://openairdocs.org/stc/SA02442AK%20PAGE%201): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC
- [STC SA01933LA-D PAGE 1](https://openairdocs.org/stc/SA01933LA-D%20PAGE%201): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA02283SE PAGE 1](https://openairdocs.org/stc/SA02283SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc
- [STC SA02402SE PAGE 1](https://openairdocs.org/stc/SA02402SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics International Inc
- [STC SA02717NY PAGE 1](https://openairdocs.org/stc/SA02717NY%20PAGE%201): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC
- [STC SA02015SE-D](https://openairdocs.org/stc/SA02015SE-D): Installation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc
- [STC SA00432SE](https://openairdocs.org/stc/SA00432SE): Installation of EGT 701 series fuel flow instrument. J P Instruments
- [STC SA00861SE](https://openairdocs.org/stc/SA00861SE): Installation of J.P. Instruments (JPI) fuel flow indicating system. J P Instruments
- [STC SA01026SE](https://openairdocs.org/stc/SA01026SE): Improved fuel gascolator assembly. Steve's Aircraft

All 74: https://openairdocs.org/model/extra-flugzeugproduktions-und-ea300-l-extra/stcs.md

## PMA parts (OpenAirDocs) (59, first 50)

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.

- [BB-HDB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144402684620260701191841.0001): Hold Down Bracket. EarthX, Inc. · PMA PQ05466NM · Modification part · Jun 4, 2026
- [MDL TD 031851](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179489903420250508133542.0001): VA-1A( )AndAccessories. Electronics International Inc · PMA PQ0088NM · Modification part · Apr 10, 2025
- [EA-22000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID198003800620220525194342.0001): Controller Wire Harness (14 Pin). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [EA-21000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135828388820220525194213.0001): Six-Cylinder Ignition Controller. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [EA-25000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117736135320220525194010.0001): Six-Cylinder Dual Magneto MTH. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [EA-22000T](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID100530013620220525194454.0001): Controller Wire Harness- Twin (14 Pin). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [ST-761](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID228656986320211110110739.0001): Autopilot. S-Tec Corporation · PMA PQ0978SW · Modification part · Aug 27, 2021
- [EA-23000-A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID639822114120210923143702.0001): EA-23000 Ignition/Starter Switch Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jul 28, 2021
- [EA-23000-A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID500138206520210923143803.0001): EA-23000 Ignition/Starter Switch Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jul 28, 2021
- [700-00190-100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID237477164120210921142546.0001): SkyTrax 100B/200 ADS-B Receiver. Avidyne Corporation · PMA PQ4035CE · Replaces ModificationPart · Jul 28, 2021
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID870439609420210702175223.0001): Aspen Avionics · PMA PQ03868SW · Jan 20, 2021
- [ALE-2008AE-AC](https://drs.faa.gov/browse/excelExternalWindow/E2B30B020A91DE91862585DE00509F79.0001): Stator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-2008AE, as used in alternators ALT… · Sep 1, 2020
- [ALE-2008AA-AC](https://drs.faa.gov/browse/excelExternalWindow/C617AAB83C6B799B862585DE0050A01D.0001): Stator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-2008AA, as used in alternators ALY… · Sep 1, 2020
- [XA-943FS-AC](https://drs.faa.gov/browse/excelExternalWindow/B7CC6ECA46AA2F14862585DE00509E71.0001): Pos. Diode. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces XA-943FS, as used in alternators ALE… · Sep 1, 2020
- [ALE-1013AS-AC](https://drs.faa.gov/browse/excelExternalWindow/9F424D3467678943862585DE00509EFC.0001): Alternator Brush. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-1013AS, as used in alternators ALE… · Sep 1, 2020
- [ALU-3045BS-AC](https://drs.faa.gov/browse/excelExternalWindow/68353ACEF594EACF862585DE0050A127.0001): Brush Assembly. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALU-3045BS, as used in alternators ALE… · Sep 1, 2020
- [ALE-2008ABS-AC](https://drs.faa.gov/browse/excelExternalWindow/6583E821C11FC24F862585DE0050A086.0001): Stator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-2008ABS, as used in alternators… · Sep 1, 2020
- [XA-944JS-AC](https://drs.faa.gov/browse/excelExternalWindow/0388185039CFC4DD862585DE00509DDD.0001): Neg. Diode. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces XA-944JS, as used in alternators ALE… · Sep 1, 2020
- [ALE-2008ABS-AC](https://drs.faa.gov/browse/excelExternalWindow/D6FF39FD09272684862585A80035E2C3.0001): Stator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-2008ABS as used in Kelly… · Jul 14, 2020
- [ALU-3045BS-AC](https://drs.faa.gov/browse/excelExternalWindow/BDCE1BF615C7C07F862585A80035E30E.0001): Brush Assembly. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALU-3045BS as used in Kelly Aerospace… · Jul 14, 2020
- [XA-944JS-AC](https://drs.faa.gov/browse/excelExternalWindow/7D10ABF30982F851862585A80035E125.0001): Neg. Diode. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces XA-944JS as used in Kelly Aerospace… · Jul 14, 2020
- [ALE-2008AE-AC](https://drs.faa.gov/browse/excelExternalWindow/653EDB41D36E637B862585A80035E22A.0001): Stator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-2008AE as used in Kelly Aerospace… · Jul 14, 2020
- [ALE-1013AS-AC](https://drs.faa.gov/browse/excelExternalWindow/5023594FC72E2A5F862585A80035E1DF.0001): Alternator Brush. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-1013AS as used in Kelly Aerospace… · Jul 14, 2020
- [ALE-2008AA-AC](https://drs.faa.gov/browse/excelExternalWindow/4077186575E9032A862585A80035E272.0001): Stator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-2008AA as used in Kelly Aerospace… · Jul 14, 2020
- [XA-943FS-AC](https://drs.faa.gov/browse/excelExternalWindow/2B2BE444A62E7876862585A80035E196.0001): Pos. Diode. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces XA-943FS as used in Kelly Aerospace… · Jul 14, 2020
- [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
- [9100-001-H](https://drs.faa.gov/browse/excelExternalWindow/1AEB415100FB45D8862585690040159F.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [700-00190-100](https://drs.faa.gov/browse/excelExternalWindow/CB6B45C441A97D20862585510065ECA1.0001): SkyTrax 100B. Avidyne Corporation · PMA PQ4035CE · Replaces N/A · May 13, 2019
- [EA-15000](https://drs.faa.gov/browse/excelExternalWindow/BA487E6B82EF95E786258258006F0EA8.0001): Ignition/Starter Switch Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Feb 20, 2018
- [94016-02](https://drs.faa.gov/browse/excelExternalWindow/3AF142A8DEF564FE862580D600749E51.0001): Isolator, Engine. Hutchinson Aerospace & Industry Inc · PMA PQ0524NM · Replaces 94016-02 · Jan 31, 2017
- [SA3-00-D](https://drs.faa.gov/browse/excelExternalWindow/D5B3725F33B5FD1F86258026005E1ADE.0001): Gascolator. Steve's Aircraft · PMA PQ2372NM · Modification part · Jun 1, 2016
- [SA3-00-A](https://drs.faa.gov/browse/excelExternalWindow/AF5F202013722EDE86258026005E1A0E.0001): Gascolator. Steve's Aircraft · PMA PQ2372NM · Modification part · Jun 1, 2016
- [EARHB32S](https://drs.faa.gov/browse/excelExternalWindow/FFCA9708C323938D86257FAB0068FA96.0001): Wide Gap Fine Wire Spark Plug (EIS Spark Plug, Fine Wire, 0.036 inch Gap). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · May 1, 2016
- [EIS-61000-5M](https://drs.faa.gov/browse/excelExternalWindow/809D38D646D3781F86257FAB0068F9DB.0001): Electroair Electronic Ignition System (Kit). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · May 1, 2016
- [EIS-61000-5C](https://drs.faa.gov/browse/excelExternalWindow/6040C85A1BE8346886257FAB0068F9D9.0001): Electroair Electronic Ignition System (Kit). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · May 1, 2016
- [EARHB32E](https://drs.faa.gov/browse/excelExternalWindow/4A3142EBF30EB54886257FAB0068FA94.0001): Wide Gap Massive Electrode Spark Plug (EIS Spark Plug, Massive Electrode, 0.036 inch Gap). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · May 1, 2016
- [EARHM38SE](https://drs.faa.gov/browse/excelExternalWindow/3C9C6C4FED5C756986257FAB0068FA93.0001): Wide Gap Fine Wire Spark Plug (EIS Spark Plug, Fine Wire, 0.036 inch Gap). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · May 1, 2016
- [EA-13000](https://drs.faa.gov/browse/excelExternalWindow/B3C7B4E82732240986257EF40059ADFC.0001): Ignition/Starter Switch Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Oct 29, 2015
- [9230-17003-01](https://drs.faa.gov/browse/excelExternalWindow/9DD900830DCF6B3D86257EBD005F60D4.0001): L-3 Detachable Configuration Module. Acron Aviation Inc. · PMA PQ2024CE · Modification part · Aug 16, 2015
- [9060-17250-01](https://drs.faa.gov/browse/excelExternalWindow/8511FE654B6B00B686257EBD005F5E3F.0001): L-3 Kit Installation NGT-1000/ NGT-2000/ NGT-2500. Acron Aviation Inc. · PMA PQ2024CE · Modification part · Aug 16, 2015
- [9060-17500-02 (right angle RF)](https://drs.faa.gov/browse/excelExternalWindow/76DD7CDEA34E5E2786257EBD005F5FFE.0001): L-3 Kit Installation NGT-9000R Panel Mount. Acron Aviation Inc. · PMA PQ2024CE · Modification part · Aug 16, 2015
- [9230-17003-01](https://drs.faa.gov/browse/excelExternalWindow/6F3D47AA7EA319D086257EBD005F606F.0001): L-3 Detachable Configuration Module. Acron Aviation Inc. · PMA PQ2024CE · Modification part · Aug 16, 2015

All of them: https://openairdocs.org/model/extra-flugzeugproduktions-und-ea300-l-extra/pma.md

## The same model under other registry codes

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

- [Extra Flugzeugbau EA 300/L](https://openairdocs.org/model/extra-flugzeugbau-ea-300-l): 125 registered aircraft, registry code 70218DG
- [Extra Flugzeugproduktions EA 300/L](https://openairdocs.org/model/extra-flugzeugproduktions-ea-300-l): 32 registered aircraft, registry code 70218DN

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.