# Siai-Marchetti F.260

- Type: Aircraft model (FAA registry)
- Registry code: 8121206
- Manufacturer (registry): SIAI-MARCHETTI
- Model: F.260
- Aircraft type: Fixed wing single engine
- Category: Airplane
- Engines: 1 · Reciprocating
- Seats: 3
- Weight class: Up to 12,499 lb
- Cruise speed: 66 mph
- Certification: Type certificated
- Data sheet: [TCDS A10EU](https://openairdocs.org/tcds/A10EU) (OpenAirDocs)
- Holder: Aermacchi S.p.A.
- Registered aircraft: 7
- Page: https://openairdocs.org/model/siai-marchetti-f-260

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 2020-09-04](https://openairdocs.org/ad/2020-09-04): Flight Controls · Aermacchi F.260, F.260B, F.260C and 3 more. Effective May 7, 2020
- [AD 2013-22-23 R1](https://openairdocs.org/ad/2013-22-23-R1): Powerplant · Aermacchi F.260, F.260B, F.260C and 5 more. Effective Jul 11, 2014
- [AD 2013-22-23](https://openairdocs.org/ad/2013-22-23): Powerplant · Aermacchi F.260, F.260B, F.260C and 5 more. Effective Dec 16, 2013
- [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 98-13-09](https://openairdocs.org/ad/98-13-09): Airspeed Indicator · Aermacchi F.260, F.260B, F.260C and 1 more. Effective Aug 1, 1998
- [AD 83-06-05 R1](https://openairdocs.org/ad/83-06-05-R1): Nose-Gear Barrel · Aermacchi F.260, F.260B and F.260C. Effective Mar 26, 1984
- [AD 83-08-07](https://openairdocs.org/ad/83-08-07): Propeller Control · Aermacchi F.260, F.260B, S.205 - 18/F and 5 more. Effective May 9, 1983
- [AD 83-06-10](https://openairdocs.org/ad/83-06-10): Propeller Governor Relief Valve · Aermacchi F.260, F.260B and F.260C. Effective Apr 7, 1983
- [AD 77-14-18](https://openairdocs.org/ad/77-14-18): Airplane Control · Aermacchi F.260 and F.260B. Effective Jul 28, 1977
- [AD 76-23-01](https://openairdocs.org/ad/76-23-01): Landing Gear Control Switch · Aermacchi F.260, F.260B, S.205 - 18/R and 4 more. Effective Nov 18, 1976
- [AD 75-22-19](https://openairdocs.org/ad/75-22-19): Main Landing Gear · Aermacchi F.260 and F.260B. Effective Oct 27, 1975
- [AD 75-21-01](https://openairdocs.org/ad/75-21-01): Landing Gear · Aermacchi F.260 and F.260B. Effective Oct 13, 1975
- [AD 75-17-19](https://openairdocs.org/ad/75-17-19): Landing Gear · Aermacchi F.260. Effective Aug 19, 1975
- [AD 75-17-06](https://openairdocs.org/ad/75-17-06): Emergency Landing Gear Control · Aermacchi F.260 and F.260B. Effective Aug 15, 1975

## Information bulletins (advisory) (2)

- [SAIB CE-11-59](https://openairdocs.org/saib/CE-11-59): Engine Fuel and Control: Fuel Selector Valve and Fuel Shut Off Cock. Issued Sep 28, 2011
- [SAIB ACE-98-27](https://openairdocs.org/saib/ACE-98-27): . Issued Apr 23, 1998

## Registered aircraft (7)

- [N260MT](https://openairdocs.org/aircraft/N260MT): [Carlomagno Kent Gene](https://openairdocs.org/faa-owner/CARLOMAGNO%20KENT%20GENE), [San Rafael, CA](https://openairdocs.org/faa-place/CA/San%20Rafael), built 1972, S/N 3-80
- [N266SF](https://openairdocs.org/aircraft/N266SF): [Eastern Stearman Inc Trustee](https://openairdocs.org/faa-owner/EASTERN%20STEARMAN%20INC%20TRUSTEE), [Leesburg, VA](https://openairdocs.org/faa-place/VA/Leesburg), built 1969, S/N 2-29
- [N517P](https://openairdocs.org/aircraft/N517P): [Semonian Gary A](https://openairdocs.org/faa-owner/SEMONIAN%20GARY%20A), [Jasper, GA](https://openairdocs.org/faa-place/GA/Jasper), S/N 106
- [N730W](https://openairdocs.org/aircraft/N730W): [Hoelzen Robert D Trustee](https://openairdocs.org/faa-owner/HOELZEN%20ROBERT%20D%20TRUSTEE), [Kent, WA](https://openairdocs.org/faa-place/WA/Kent), built 1968, S/N 109
- [N7895](https://openairdocs.org/aircraft/N7895): [Matukaitis William K](https://openairdocs.org/faa-owner/MATUKAITIS%20WILLIAM%20K), [Millbury, MA](https://openairdocs.org/faa-place/MA/Millbury), built 1968, S/N 123
- [N797MS](https://openairdocs.org/aircraft/N797MS): [Williamson Marc R](https://openairdocs.org/faa-owner/WILLIAMSON%20MARC%20R), [Parkville, MO](https://openairdocs.org/faa-place/MO/Parkville), built 1969, S/N 2-28
- [N93225](https://openairdocs.org/aircraft/N93225): [Dr Carlton N Walker Dds LLC](https://openairdocs.org/faa-owner/DR%20CARLTON%20N%20WALKER%20DDS%20LLC), [Roswell, NM](https://openairdocs.org/faa-place/NM/Roswell), S/N 104

## NTSB investigations (5)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB WPR11LA374](https://openairdocs.org/ntsb/WPR11LA374), Aug 7, 2011: SIAI Marchetti F.260 (N408FD), Coalinga, CA, substantial damage. Probable cause: A partial loss of engine power immediately after takeoff for undetermined reasons.
- [NTSB ERA09LA516](https://openairdocs.org/ntsb/ERA09LA516), Sep 4, 2009: Siai-Marchetti F.260 (N517P), Atlanta, GA, substantial damage. Probable cause: A total loss of engine power due to a fuel system air leak as a result of a deteriorated O-ring seal in the fuel shut-off cock. Contributing to the accident was the exceedance of the suggested…
- [NTSB FTW97LA371](https://openairdocs.org/ntsb/FTW97LA371), Sep 30, 1997: Siai-Marchetti F.260 (N260MT), Santa Rosa, NM, substantial damage. Probable cause: improper planning/decision by the pilot, which led to fuel exhaustion, loss of engine power, and a forced landing. A related factor was the lack of suitable terrain for the forced landing.
- [NTSB FTW94FA220](https://openairdocs.org/ntsb/FTW94FA220), Jul 5, 1994: SIAI-Marchetti F.260 (N260MS), Dover, OK, destroyed, 2 fatal. Probable cause: FAILURE OF THE PILOT TO MAINTAIN ADEQUATE ALTITUDE WHILE PERFORMING AN AEROBATIC DEMONSTRATION. FACTORS RELATED TO THE ACCIDENT WERE: THE PILOT'S INADEQUATE TRAINING, HIS LACK OF EXPERIENCE IN THE…
- [NTSB IAD78FA044](https://openairdocs.org/ntsb/IAD78FA044), Feb 20, 1978: Siai-Marche SF260 (N7896), Charlotte, NC, destroyed, 2 fatal

## FAA accident and incident reports (7)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20210519009159I](https://openairdocs.org/incident/20210519009159I), May 19, 2021: Siai-Marchetti F.260 (N260MT), Carson City, NV, Minor damage. Subsequent to landing, the right main landing gear collapsed during rollout. Investigation indicates that main landing gear push pull tube p/n 260-14-22-3 bent…
- [Incident 20140601008069I](https://openairdocs.org/incident/20140601008069I), Jun 1, 2014: Siai-Marchetti F.260 (N7895), Fitchburg, MA, Minor damage. On June 3 2014 pilot departed sterling airport (3B3) AT10AM local with two passengers, on board. PIC proceeded to fly to a unidentified grass strip in Vermont.…
- [Accident 20110806017339A](https://openairdocs.org/incident/20110806017339A), Aug 6, 2011: Siai-Marchetti F.260 (N408FD), Coalinga, CA, Substantial damage. During takeoff, at 100 feet above runway 14, the aircraft lost partial power. The pilot was unable to climb and made an emergancy landing in the field about…
- [Accident 20090904049209A](https://openairdocs.org/incident/20090904049209A), Sep 4, 2009: Siai-Marche F.260 (N517P), Kennesaw, GA, Substantial damage. The interview with the pilot in command Mr. Gary semonian revealed the following: Mr. Semonian holds an FAA private pilot certificate and has 400 hours in this…
- [Accident 19970930029239A](https://openairdocs.org/incident/19970930029239A), Sep 30, 1997: Mrchti F260 (N260MT), Santa Rosa, NM, Substantial damage. Lost power enroute near fueling stop Q58. Damaged F260 landing on dirt road. Fuel tanks were empty. (-23) see narrative #FTW97LA371.
- [Accident 19940705017329A](https://openairdocs.org/incident/19940705017329A), Jul 5, 1994: Mrchti F260 (N260MS), Dover, OK, Destroyed, 2 fatal. During demo of warplane attack on a bridge for tv show. Made thrid pass with wing over at 50 ft AGL. Failed pullout.
- [Accident 19780220016449A](https://openairdocs.org/incident/19780220016449A), Feb 20, 1978: Mrchti SF260 (N7896), Charlotte, NC, Destroyed. 8HRS total actual instruments. Flaps up.

## STCs that may be installed (OpenAirDocs) (94, 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 SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc
- [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC
- [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 SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation 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 SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC
- [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 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 SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC
- [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 SA09902AC](https://openairdocs.org/stc/SA09902AC): Installation of BendixKing KFD 900 Flight Display System. Honeywell International Inc. (Bendix King)
- [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 SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International 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 SA04280CH](https://openairdocs.org/stc/SA04280CH): Install rocker switch assemblies on dual magneto configuration in accordance with Electroair Acquisition Corporation Installation Instructions as listed on AML No. SA04280CH, or later FAA approved revision. Electroair Acquisition 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 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 SA01435SE](https://openairdocs.org/stc/SA01435SE): Installation of J.P. Instruments (JPI) Primary Engine Data Management System. J. P. Instruments
- [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 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 SA02212AK](https://openairdocs.org/stc/SA02212AK): Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Seaplanes North LLC
- [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 SA02428SE](https://openairdocs.org/stc/SA02428SE): Installation of an Air Stream Switch for an electric time recording device on non-pressurized aircraft. Henry F Rogers/David E Polley
- [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 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 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 SA02930NY](https://openairdocs.org/stc/SA02930NY): Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3, G2, and G1 and 1200C model G4 as primary Cylinder Head Temperature (CHT), Exhaust Gas Temperature (EGT), and Turbine Inlet Temperature (TIT) Instruments. Insight Instrument Corporation

All 94: https://openairdocs.org/model/siai-marchetti-f-260/stcs.md

## PMA parts (OpenAirDocs) (136, 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.

- [S1069](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154714783420260806152255.0001): 100R Fuel Placard. Swift Fuels, LLC · PMA PQ04423CE · Modification part · Jul 20, 2026
- [73-CFG-R](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID150409311320260806152350.0001): Fuel Quantity Indication Placard. Swift Fuels, LLC · PMA PQ04423CE · Modification part · Jul 20, 2026
- [LSM-200-700-11](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116104597720250417183919.0001): Hub Cap Assy. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · Dec 10, 2024
- [MDL103216-000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108417396320240221143417.0001): SkyView HDX Instrumentation. Dynon Avionics, Inc. · PMA PQ05359NM · Modification part · Jan 26, 2024
- [UAV-1004236-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123345788220230707211216.0001): AV-30-C. uAvionix Corporation · PMA PQ05445NM · Modification part · Jun 28, 2023
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183074175320220706160035.0001): Whelen Aerospace Technologies · PMA PQ1372CE · Jun 21, 2022
- [EA-22000T](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193896523720220525194441.0001): Controller Wire Harness- Twin (14 Pin). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [EA-21000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID175245646520220525194154.0001): Six-Cylinder Ignition Controller. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [EA-22000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169180202920220525194329.0001): Controller Wire Harness (14 Pin). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [89000026-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167313053520240229155306.0001): Final Assembly KCP 100 Control Panel. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [89000020-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149133796820240229155255.0001): Final Assembly KSD 100 Primary Flight Display (PFD). Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [89000026-003](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140343051020240229155312.0001): Final Assembly KCP 100 Control Panel(Landscape). Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [89000023-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106322412320240229155301.0001): Final Assembly KG 71 Air Data Attitude and Heading Reference System (ADHRS). Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [700-00190-100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID784105903420210921142529.0001): SkyTrax 100B/200 ADS-B Receiver. Avidyne Corporation · PMA PQ4035CE · Replaces ModificationPart · Jul 28, 2021
- [EA-23000-A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID767383620202109231436430.0001): 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/DRSDOCID430625338120210923143746.0001): EA-23000 Ignition/Starter Switch Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jul 28, 2021
- [409-00003-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID261645249820210702175206.0001): Internal Battery Pack, Refresh. Aspen Avionics · PMA PQ03868SW · Modification part · Jan 20, 2021
- [1049-4000-03-001C](https://drs.faa.gov/browse/excelExternalWindow/FB6A4D62429A217F86258633006145AB.0001): Roll Steering Converter. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4201-20](https://drs.faa.gov/browse/excelExternalWindow/ED78E4F8D3C63347862586330061461D.0001): Annunciator Kit GDC31. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4200-20](https://drs.faa.gov/browse/excelExternalWindow/CBC6239248334CCE86258633006145E5.0001): Connector Kit GDC31. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4200-50](https://drs.faa.gov/browse/excelExternalWindow/86CBD103649292948625863300614693.0001): Isolation Coupler Installation Kit. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4000-03-001B](https://drs.faa.gov/browse/excelExternalWindow/6583D9B2B4E75DBE862586330061451A.0001): E50Roll Steering Converter. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4801-01](https://drs.faa.gov/browse/excelExternalWindow/39A0DF401545910A8625863300614652.0001): Isolation Coupler. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [9230-17003-01](https://drs.faa.gov/browse/excelExternalWindow/74A1EA49501842C886258616005ECD09.0001): Detachable Configuration Module. Aviation Communication and Surveillance Systems · PMA PQ1571NM · Replaces 9230-17003-01 · Nov 2, 2020
- [TACH2](https://drs.faa.gov/browse/excelExternalWindow/29C3872705863D03862585E500683D52.0001): Tach2 Signal Converter. SureFly Partners Ltd · PMA PQ03861SW · Modification part · Sep 7, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID966130781420220125131351.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID746150319920220125131433.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID641147647920220125131333.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID464286905920220125131314.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID371378329120220125131408.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID319645970120220125131455.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [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
- [MDL 103216-000](https://drs.faa.gov/browse/excelExternalWindow/A5FAC4121A00318086258569004A2249.0001): SkyView HDX Instrumentation. Dynon Avionics, Inc. · PMA PQ05359NM · Modification part · Jul 14, 2019
- [01-0771833-20](https://drs.faa.gov/browse/excelExternalWindow/FFF505DF238D9E3E86258557004EB967.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 30, 2019
- [01-0771833-25](https://drs.faa.gov/browse/excelExternalWindow/D17366A21258BFC186258557004EB9A2.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 30, 2019
- [01-0771833-10](https://drs.faa.gov/browse/excelExternalWindow/D0F0E113B870DF1C86258557004EB8E0.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 30, 2019
- [01-0771833-15](https://drs.faa.gov/browse/excelExternalWindow/CB6A5B42DF6A574686258557004EB925.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 30, 2019
- [01-0790750-10](https://drs.faa.gov/browse/excelExternalWindow/8FBCEA35A3837D6386258557004EB9D7.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 30, 2019
- [01-0790750-20](https://drs.faa.gov/browse/excelExternalWindow/5919E033D600DA3386258557004EBA0C.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 30, 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

All of them: https://openairdocs.org/model/siai-marchetti-f-260/pma.md

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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.
