# N312FL: 2011 Embraer S A EMB-505

- Status: Valid registration
- Airframe: [Embraer S A EMB-505](https://openairdocs.org/model/embraer-s-a-emb-505) (registry code 326040C, 9 seats)
- Engine: [Pratt & Whitney Canada PW535E](https://openairdocs.org/engine/pratt-whitney-canada-pw535e) (registry code 52297)
- Data sheets: [TCDS A60CE](https://openairdocs.org/tcds/A60CE) (Embraer S.A.), [TCDS E00053EN](https://openairdocs.org/tcds/E00053EN) (Pratt & Whitney Canada Inc.) (OpenAirDocs)
- Serial number: 50500037
- Year built: 2011
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: September 23, 2011
- Certificate issued: March 7, 2023
- Expires: March 31, 2030
- Mode S code: A34EC7
- Registered owner: [Bam Acquisitions LLC](https://openairdocs.org/faa-owner/BAM%20ACQUISITIONS%20LLC)
- Location: [Carmel, IN](https://openairdocs.org/faa-place/IN/Carmel)
- Owner type: LLC
- Owner's area on the map: 39.9666° N, 86.1751° W: Placed by OpenAirDocs at the center of ZIP code 46032, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=312FL
- Page: https://openairdocs.org/aircraft/N312FL

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 13 in force

### Matched by airframe (Embraer S A EMB-505)

- [AD 2026-10-18](https://openairdocs.org/ad/2026-10-18): Flight Control System · Embraer EMB-505. Effective Jul 6, 2026
- [AD 2026-03-05](https://openairdocs.org/ad/2026-03-05): Autopilot Main Servo · Embraer EMB-505. Effective Mar 31, 2026
- [AD 2024-22-06](https://openairdocs.org/ad/2024-22-06): Cabin Equipment/Furnishings · Embraer EMB-505. Effective Jan 2, 2025
- [AD 2024-17-09](https://openairdocs.org/ad/2024-17-09): Cabin Equipment/Furnishings · Embraer EMB-505. Effective Nov 12, 2024
- [AD 2023-21-04](https://openairdocs.org/ad/2023-21-04): Indicating/recording system · Embraer EMB-505. Effective Dec 11, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2022-05-12](https://openairdocs.org/ad/2022-05-12): Elevator Structure, Rudder Structure, Ailerons · Embraer EMB-505. Effective Apr 13, 2022
- [AD 2021-24-21](https://openairdocs.org/ad/2021-24-21): Operations · Embraer EMB-500 and EMB-505. Effective Jan 25, 2022
- [AD 2018-07-10](https://openairdocs.org/ad/2018-07-10): Flight Controls · Embraer EMB-500 and EMB-505. Effective May 15, 2018
- [AD 2016-22-02](https://openairdocs.org/ad/2016-22-02): Equipment/Furnishing · Embraer EMB-500 and EMB-505. Effective Dec 1, 2016
- [AD 2014-19-01](https://openairdocs.org/ad/2014-19-01): Landing Gear · Embraer EMB-505. Effective Oct 22, 2014
- [AD 2012-13-04](https://openairdocs.org/ad/2012-13-04): Flight Controls · Embraer - Empresa Brasileira de Aeronautica EMB-505. Effective Aug 6, 2012

### Matched by engine (Pratt & Whitney Canada PW535E)

- [AD 2025-05-13](https://openairdocs.org/ad/2025-05-13): Turbine Section · Pratt & Whitney Canada PW535E and PW535E1. Effective Apr 23, 2025

### Historical (superseded or no longer in force)

- [AD 2023-22-11](https://openairdocs.org/ad/2023-22-11) (historical): Autopilot Main Servo · Embraer EMB-505. Effective Dec 26, 2023
- [AD 2023-21-06](https://openairdocs.org/ad/2023-21-06) (historical): Cabin Equipment/Furnishings · Embraer EMB-505. Effective Dec 11, 2023
- [AD 2020-12-08](https://openairdocs.org/ad/2020-12-08) (historical): Elevator Structure; Rudder Structure; Ailerons · Embraer EMB-505. Effective Jul 1, 2020
- [AD 2013-22-20](https://openairdocs.org/ad/2013-22-20) (historical): Landing Gear · Embraer EMB-505. Effective Nov 8, 2013
- [AD 2011-20-01](https://openairdocs.org/ad/2011-20-01) (historical): Flight Controls · Embraer - Empresa Brasileira de Aeronautica EMB-505. Effective Oct 31, 2011

## Information bulletins (advisory) (2 in force)

- [SAIB CE-16-23](https://openairdocs.org/saib/CE-16-23): Navigation; Degraded Attitude and Heading Reference System (AHRS) Performance When Operating in Areas of Unreliable or Unavailable Global Positioning System (GPS) Signal. Issued Sep 7, 2016
- [SAIB CE-10-46](https://openairdocs.org/saib/CE-10-46): Navigation; Embraer EMB-505 Terrain Awareness Warning System (TAWS) Instructions in Airplane Flight Manual. Issued Aug 16, 2010

## NTSB investigations

None matched to N312FL.

## FAA accident and incident reports

None matched to N312FL.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N312FL not matched to an aircraft (35)

They name N312FL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DU4R108](https://openairdocs.org/sdr/DU4R108), May 31, 2005: PAN. CORRODED. RT FLOOR PAN AT BS 1016 WL208.1 CORRODED. S/O 109001, N/R 22825
- [SDR DU4R107](https://openairdocs.org/sdr/DU4R107), May 27, 2005: ANGLE. CORRODED. FWD ENTRY DOOR THRESHOLD HAS CORRODED ANGLE (OB OF INNER CHORD). S/O 109001, N/R 23118.
- [SDR DU4R106](https://openairdocs.org/sdr/DU4R106), May 27, 2005: BUSHING. CORRODED. LT HORIZONTAL STAB AFT SPAR, UPPER ATTACH LUG, CENTER SECTION, AFT FACE HAS CORROSION AROUND BUSHING. S/O 109001, N/R 22994
- [SDR DU4R05105](https://openairdocs.org/sdr/DU4R05105), May 27, 2005: BUSHING. CORRODED. LT HORIZONTAL STAB FRONT SPAR, UPPER ATTACH BOLT BORE, BUSHINGS HAVE PITTING CORROSION. S/O 109001, N/R 22971.
- [SDR DU4R104](https://openairdocs.org/sdr/DU4R104), May 27, 2005: FLOOR SUPPORT. CORRODED. CORROSION AT FLOORBOARD SUPPORT ANGLE FROM BS 949 TO 1000 RBL 68.0. S/O 109001, N/R 22787
- [SDR 103](https://openairdocs.org/sdr/103), May 27, 2005: SEAT TRACK. GOUGED. CABIN RT OB SEAT TRACK HAS NUMEROUS GOUGES STA. 540 TO 727E. S/O 109001, N/R 22858
- [SDR 102](https://openairdocs.org/sdr/102), May 27, 2005: SEAT TRACK. GOUGED. CABIN LT IB SEAT TRACK HAS NUMEROUS GOUGES STA. 540 TO 727E. S/O 109001, N/R 22850
- [SDR 85](https://openairdocs.org/sdr/85), May 2, 2005: FLOORBEAM. CORRODED. CORRODED AFT CABIN FLOORBEAM UPPER SKIN FROM BS 987 LBL 48.0.
- [SDR 84](https://openairdocs.org/sdr/84), May 2, 2005: FRAME. CRACKED. CRACKED FRAME AT BS 294.5, WL 208.1 FWD GALLEY DOOR.
- [SDR 83](https://openairdocs.org/sdr/83), May 2, 2005: CREASE BEAM. CORRODED. R-1 SERVICE DOOR INNER CHORD CREASE BEAM HAS CORROSION THRU OUT THE BEAM.
- [SDR 82](https://openairdocs.org/sdr/82), May 2, 2005: SHEAR TIE. CRACKED. CABIN UPPER LOBE SHEAR TIE CRACKED AT BS 639 S-4L.
- [SDR 81](https://openairdocs.org/sdr/81), May 2, 2005: FRAME. CRACKED. LOWER FWD SIDE OF FRAME AT STA 616 S-16R CRACKED AT LOWER FASTENER.
- [SDR 80](https://openairdocs.org/sdr/80), May 2, 2005: SKIN. GOUGED. AIRCRAFT DAMAGE BELOW AFT PIT FROM BELT LOADER BS 755-790, S-25R. LOG PAGE ITEM NR1 PG. 158526,S/O 109001, N/R 22583.
- [SDR DU4R20050428](https://openairdocs.org/sdr/DU4R20050428), Apr 28, 2005: FLOOR SUPPORT. CORRODED. CORROSION AT FLOORBOARD ANGLE SUPPORT FROM BS 947 - 1000 LBL 68.
- [SDR 78](https://openairdocs.org/sdr/78), Apr 26, 2005: SKIN. DENTED. DENTS AND GOUGES STA 770 - 827 STR 26 - 27 RT BELOW AFT PIT DOOR.
- [SDR F3LA200400117](https://openairdocs.org/sdr/F3LA200400117), Dec 12, 2004: PROXIMITY SENSOR. FAULTY. FLIGHT CREW REPORTED LANDING GEAR WARNING HORN STUCK ON WHEN FULLY CONFIGURED ON FINAL AND WOULD NOT SILENCE UNTIL FLAPS RETURNED TO UP POSITION AFTER LANDING. 
- [SDR F3LA200400066](https://openairdocs.org/sdr/F3LA200400066), Jun 6, 2004: FIRE LOOP. FAULTY. AIR RETURN, NR 2 ENG OVERHEAT CAUTION LIGHT ILLUM TWICE. DECLARED EMERGENCY, LANDED W/O INCIDENT. ON DESCENT, MASTER CAUTION SYS ILLUM 4 TIMES, NO SIX PACK INDI
- [SDR F3LA200400064](https://openairdocs.org/sdr/F3LA200400064), May 23, 2004: PANEL. DAMAGED. DURING C-6 CHECK, INSPECTION REPORTED SCREW BROKEN ON NR 1 PYLON TOP AFT FAIRING PANEL ATTACHED TO THE WING AND A CRACK FROM THE HOLE. REPLACED PANEL PER SRM 51
- [SDR F3LA200400063](https://openairdocs.org/sdr/F3LA200400063), May 23, 2004: PANEL. CRACKED. DURING C-6 CHECK, INSPECTION REPORTED RT WING UPPER SURFACE AFT PYLON PANEL CRACKED AT AFT I/B CORNER AT FASTENER COMMON TO FUEL CELL. REPLACED PANEL PER SRM 51
- [SDR F3LA200300156](https://openairdocs.org/sdr/F3LA200300156), Dec 2, 2003: SUPPORT. BROKEN. DURING WALK-AROUND, FLIGHT CREW REPORTED NR 7 FLAP TRANSMISSION FLAP TRACK FAIRING A-FRAME ATTACH POINTS BROKEN. REPLACED NR 7 FLAP TRACK FAIRING A-FRAME AND SU
- [SDR F3LA200200198](https://openairdocs.org/sdr/F3LA200200198), Jul 24, 2002: FMC. FAULTY. AIR TURNBACK. ON CLIMBOUT, THE FLIGHT CREW REPORTED THE ONLY MODE CONTROL WAS N1. NO AUTO-PILOT, NO AUTO THROTTLE OR MODE CONTROL. MAINTENANCE REMOVED AND REPLA
- [SDR F3LA200200139](https://openairdocs.org/sdr/F3LA200200139), May 4, 2002: CHANNEL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON Z-CHANNEL AFT GALLEY SUPPORTS, STA 1028, BBL 10L AND BBL 10R. REPLACED CORRODED Z-CHANNEL PER EA 53-737-165, 
- [SDR F3LA200200138](https://openairdocs.org/sdr/F3LA200200138), May 4, 2002: PAN. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED AFT LAV PAN BETWEEN STA 1016 AND THE AFT PRESSURE BULKHEAD HAD THREE CORRODED FASTENERS ON RT SIDE, 16 INCHES FROM CENTER 
- [SDR F3LA200200137](https://openairdocs.org/sdr/F3LA200200137), Apr 25, 2002: FRAME. CRACKED. DURING C-4 CHECK, INSPECTION REPORTED FRAME CRACKED AT BS 663.75, STR 1R AND 2R. REMOVED DAMAGE IN FRAME PER SRM 53-00-07 FIG 209. FABRICATED FILLERS AND REPAIR
- [SDR F3LA200200134](https://openairdocs.org/sdr/F3LA200200134), Apr 25, 2002: SILL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED FLOOR ANGLE CORRODED AT L1 ENTRY THRESHOLD, STA 312 TO 344. REMOVED L1 MOP SILL PER SRM 53-10-15. INSTALLED NEW MOP SILL P
- [SDR F3LA200200130](https://openairdocs.org/sdr/F3LA200200130), Apr 15, 2002: PANEL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT RT TRANSITION PANEL CORRODED FROM STA 767 TO STA 787. REPLACED TRANSITION PANEL PER SRM 51-40-02 AND
- [SDR F3LA200200126](https://openairdocs.org/sdr/F3LA200200126), Apr 15, 2002: STRAP. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO COMPARTMENT DOOR FRAME UNDER UPPER FLANGE AT NUT PLATES AT STA 794, STR 25-R. REPLACED CORRODED RAD
- [SDR F3LA200200125](https://openairdocs.org/sdr/F3LA200200125), Apr 15, 2002: DOOR FRAME. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO COMPARTMENT DOOR FRAME WEB FROM STR 23-R TO 25-R. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 
- [SDR F3LA200200128](https://openairdocs.org/sdr/F3LA200200128), Apr 11, 2002: NUT PLATE. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON NUT PLATES OF FLOORBEAM AT STA 344, LBL 10. REPAIRED DAMAGE PER SRM 53-00-51.
- [SDR F3LA200200129](https://openairdocs.org/sdr/F3LA200200129), Apr 11, 2002: STRAP. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOORBOARD TIE DOWN STRAP CORRODED AROUND SCREW HOLES. REPAIRED DAMAGE PER SRM 51-10-2, 51-40-02 AND
- [SDR F3LA200200127](https://openairdocs.org/sdr/F3LA200200127), Apr 11, 2002: PANEL. CORRODED. DURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO COMPARTMENT RT TRANSITION PANEL FROM STA 767 TO 727. FABRICATED AND INSTALLED REPLACEMENT PANEL PER
- [SDR F3LA200200123](https://openairdocs.org/sdr/F3LA200200123), Apr 6, 2002: INTERCOSTAL. CRACKED. DURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL AT STA 344-360, BL 0, CRACKED ON TOP FLANGE FWD END AND HAS DAMAGE ON BOTTOM FLANGE. FABRICATED REPAIR PARTS P
- [SDR F3LA200200124](https://openairdocs.org/sdr/F3LA200200124), Apr 5, 2002: CROSSBEAM. CRACKED. DURING C-4 CHECK, INSPECTION REPORTED C-1 DOOR LOWER CROSSBEAM WEB CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 51-70-13.
- [SDR F3LA200200121](https://openairdocs.org/sdr/F3LA200200121), Apr 2, 2002: SKIN. CRACKED. MAINTENANCE REPORTED SKIN CRACKED AT OUTBOARD END OF NR 6 SLAT. REMOVED DAMAGED AREA AND INSTALLED REPAIR PER SRM 57-43-01 FIG 206 AND SRM 51-40-02.
- [SDR F3LA99122](https://openairdocs.org/sdr/F3LA99122), Sep 23, 1999: TIRE. FAILED. DEN - UPON ARRIVAL IN BOS, FLIGHT CREW REPORTED NR 4 MAIN TIRE RECAP MISSING. TIRE REMAINED INFLATED. MAINTENANCE IN BOS REPLACED NR 4 MAIN TIRE AND WHEEL ASSY 

## STCs that may be installed (OpenAirDocs) (47)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Embraer S A EMB-505)

- [STC SA12141IB](https://openairdocs.org/stc/SA12141IB): GOGO HDX antenna systems integration. FTI ENGINEERING NETWORK GmbH
- [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies
- [STC SA04761NY](https://openairdocs.org/stc/SA04761NY): True Blue TS56 Emergency Battery Power Supply Replacement. Mid-Continent Instrument Co. Inc
- [STC SA12286AT](https://openairdocs.org/stc/SA12286AT): Installation of a LEO Connectivity System. Embraer Engineering & Technology Center, USA, Inc
- [STC SA12143CH](https://openairdocs.org/stc/SA12143CH): Installation of SpaceX Starlink Aviation System. Nextant Aerospace
- [STC SA11158SC](https://openairdocs.org/stc/SA11158SC): Demonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS). Liberty Partners Inc
- [STC SA02779SE](https://openairdocs.org/stc/SA02779SE): Installation of Gogo AVANCE L3 Inflight Connectivity System. AeroMech Incorporated
- [STC SA12140IB](https://openairdocs.org/stc/SA12140IB): Mechanical provisions for the installation of a GOGO HDX antenna. FTI ENGINEERING NETWORK GmbH
- [STC SA09887AC](https://openairdocs.org/stc/SA09887AC): Installation of an Avionica MK-III mini Quick Access Recorder (QAR) and optional 4G or LTE Avionica Cellular Module (avCM. Aircraft Systems and Manufacturing Inc
- [STC SA03316CH](https://openairdocs.org/stc/SA03316CH): Activation of an 802.11 a/b/g/n WiFi System. Elliott Aviation Technical Products Development Inc
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA09942AC](https://openairdocs.org/stc/SA09942AC): Installation of Schatz Bearing Corporation, Radial Bearing P/N’s : KP60BHT-H-OPG and KP64BHT-H-OPG. AV8 PMA LLC
- [STC SA00087IB](https://openairdocs.org/stc/SA00087IB): Medical reconfiguration of the EMB-505. UMLAUT ENGINEERING GMBH
- [STC SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH
- [STC SA04552AT](https://openairdocs.org/stc/SA04552AT): Installation of cargo compartment floor covering. Embraer Engineering and Technology Center, USA, Inc
- [STC SA04548AT](https://openairdocs.org/stc/SA04548AT): Installation of an Avionica, LLC Quick Access Recorder/Data Concentrator model avRDC MAX (QAR) P/N 804-1250-32 and optional Avionica, LLC Cellular Module LTE (avCM LTE) P/N 650-0100-05. Aircraft Systems and Manufacturing Inc
- [STC SA00038IB](https://openairdocs.org/stc/SA00038IB): Replacement of the Passenger Seat Cushion Covers and Foams on the Embraer S.A. EMB-505. Waypoint Aerotec Limited
- [STC SA09856AC](https://openairdocs.org/stc/SA09856AC): Installation of BendixKing Aerowave 100 In-flight Data Link System for non-essential, non-required aircraft Cabin Systems & Equipments. Honeywell International Inc (Bendix King)
- [STC SA01727WI](https://openairdocs.org/stc/SA01727WI): Interior Alteration for Installation of a Coffee Maker and Modification of No Smoking Signs. Netjets Aviation Inc
- [STC SA04514NY](https://openairdocs.org/stc/SA04514NY): Single/Dual Transponder System ADS-B Upgrade. Scandinavian Avionics Design ApS
- [STC SA04463AT](https://openairdocs.org/stc/SA04463AT): Installation of a Gogo Business Aviation Avance L5 Air To Ground (ATG) In-Flight Entertainment and Connectivity (IFEC) System. Embraer Engineering & Technology Center - USA Inc
- [STC SA03010CE](https://openairdocs.org/stc/SA03010CE): Installation of a Lacobucci HF Electronics Nespresso Machine PIN HFE96-28T-10 and/or Monogram System -TIA Division Wavejet Microwave Oven PIN 400-1860-01. Embraer Engineering & Technology Center - USA Inc
- [STC SA04397NY](https://openairdocs.org/stc/SA04397NY): Installation of Satcom system. 328 Support Services GmbH
- [STC SA03003CE](https://openairdocs.org/stc/SA03003CE): Installation of an Aviator 200 Satcom System. Embraer Engineering & Technology Center - USA Inc
- [STC SA03005CE](https://openairdocs.org/stc/SA03005CE): Installation of an Aviator 200 Satcom System. Embraer Engineering & Technology Center - USA Inc
- [STC SA03001CE](https://openairdocs.org/stc/SA03001CE): Installation of Honeywell High Frequency (HF) Communication System, model KHF1050HF, and AvTec Selective Calling (SELCAL), model CSD-714. Embraer Engineering & Technology Center - USA Inc
- [STC SA03006CE](https://openairdocs.org/stc/SA03006CE): Installation of a Medical Evacuation Configuration (Medevac). Embraer Engineering & Technology Center - USA Inc
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC SA00959DE](https://openairdocs.org/stc/SA00959DE): Installation of Concorde valve regulated Lead-Acid batteries in replacement of aircraft main batteries. Concorde Battery Corporation
- [STC SA00901DE](https://openairdocs.org/stc/SA00901DE): Installation of up to Two Exxternally Mounted Gimbal Systems. Straight Flight Inc
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA03004CE](https://openairdocs.org/stc/SA03004CE): In accordance with Part 23 regulations specified in the current certification basis of Type Certificate Number A60CE, installation of pilot's new, extended seat tracks. Embraer S.A
- [STC SA03956AT](https://openairdocs.org/stc/SA03956AT): Installation of Aircell ATG-4000 High Speed Internet System (AHSI) and Aircell Axxess II Iridium Satcom or Aircell Aviator 200 SBB Satcom, Aircell ATG 5000 High Speed Internet System (AHSI) all with Wireless Local Area Network (WLAN). Nextant Aerospace
- [STC SA03973NY](https://openairdocs.org/stc/SA03973NY): Replacement of existing TCAS 7.0 by TCAS 7.1. Scandinavian Avionics Design ApS
- [STC SA03764NY](https://openairdocs.org/stc/SA03764NY): Installation of the Low Gain Satcom Antenna. Roeder Praezision GMBH
- [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS
- [STC SA04278AT](https://openairdocs.org/stc/SA04278AT): Installation of a cabin In-Flight Entertainment & Passenger Audio System. Embraer Engineering & Technology Center - USA Inc
- [STC SA04145CH](https://openairdocs.org/stc/SA04145CH): Installation of a cosmetic threshold in the aft baggage compartment to protect interior coverings/materials from loading and removal of baggage. Elliott Aviation Technical Products Development, Inc
- [STC SA04260AT](https://openairdocs.org/stc/SA04260AT): Installation of an 802.11 Wireless Internet System. Embraer Engineering & Technology Center - USA Inc
- [STC SA04243AT](https://openairdocs.org/stc/SA04243AT): Installation of AFT Lavatory Coat Hanger Support. Embraer Engineering & Technology Center - USA Inc
- [STC SA01969SE](https://openairdocs.org/stc/SA01969SE): Installation of a Mid-Continent MD302 Standby Attitude Module. Mid-Continent Instruments and Avionics
- [STC SA03352CH](https://openairdocs.org/stc/SA03352CH): Activation of an 802.11 a/b/g and n Wi-Fi System. Elliott Aviation Technical Products Development, Inc
- [STC SA01789WI](https://openairdocs.org/stc/SA01789WI): Quasar II Cabin Lighting with eConnect and Noise Mitigation. Duncan Aviation Inc
- [STC SA01760WI](https://openairdocs.org/stc/SA01760WI): Installation of an Aircell Universal Cabin System (UCS) 5000 with Wireless Local Area Network (WLAN). Duncan Aviation Inc
- [STC SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System. Garmin International Inc
- [STC SA01703WI](https://openairdocs.org/stc/SA01703WI): Installation of Concorde RG-380E/44 and RG-390E VRSLA Batteries. Concorde Battery Corporation
- [STC SA01692WI](https://openairdocs.org/stc/SA01692WI): Installation of Aircell High Speed Internet (AHSI) System with Wireless Local Area Network (WLAN) capability. Duncan Aviation Inc

## Related

- Other Embraer S A EMB-505 aircraft: https://openairdocs.org/model/embraer-s-a-emb-505/aircraft.md
- The Pratt & Whitney Canada PW535E engine: https://openairdocs.org/engine/pratt-whitney-canada-pw535e.md

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