# N332QS: 2013 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: 50500184
- Year built: 2013
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: December 18, 2013
- Certificate issued: March 23, 2026
- Expires: March 31, 2033
- Mode S code: A39EAC
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=332QS
- Page: https://openairdocs.org/aircraft/N332QS

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 N332QS.

## FAA accident and incident reports

None matched to N332QS.

## Service difficulty reports (16)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR DXTA2026072408944](https://openairdocs.org/sdr/DXTA2026072408944), Jul 21, 2026: WARNING MESSAGE. FALSE ACTIVATION. CARGO DOOR LT OPEN CAS ON CLIMBOUT. THE BAGGAGE DOOR CAS WAS NOT PRESENT WHEN THERE WAS POWER TO THE AIRCRAFT. DID A GENERAL VISUAL INSPECTION OF THE AREA AND N
- [SDR DXTA2026071608842](https://openairdocs.org/sdr/DXTA2026071608842), Jul 15, 2026: WARNING MESSAGE. FALSE ACTIVATION. AT FL400, A FLAPS FAIL CAS AND SPOILER FAULT CAS MESSAGE WERE DISPLAYED. THE ASSOCIATED CHECKLIST WAS ACCOMPLISHED, AND THE FCE WAS RESET; HOWEVER, THE CAS MESS
- [SDR DXTA2025090804843](https://openairdocs.org/sdr/DXTA2025090804843), Sep 5, 2025: SEAL. LEAKING. MAIN CABIN DOOR SEAL MAKING A STEADY HISSING NOISE FROM BOTTOM OF DOOR WHILE CLIMBING TO FL410. NO CAS OR PRESSURIZATION INDICATIONS ASSOCIATED. OPENED AND CLEA
- [SDR DXTA2025081204556](https://openairdocs.org/sdr/DXTA2025081204556), Aug 10, 2025: SPOILER SYS. FAULTED. CRUISE FLIGHT AT FL410. FLAPS FAIL AND SPOILER FAULT CAS. PER QRH, MANUAL FCE 1 RESET WAS UNSUCCESSFUL AND MESSAGES REMAINED. DURING LANDING ROLLOUT SWPS FAULT 
- [SDR DXTA2025052103550](https://openairdocs.org/sdr/DXTA2025052103550), May 18, 2025: SERVO. DEFECTIVE. VENTRAL RUD FAIL CAS APPEARED THREE TIMES IN FLIGHT. FIRST, CLIMBING BELOW 10,000, APPROX 200 KNOTS, THIS MESSAGE APPEARED ALONG WITH AP FAIL AND YD FAIL. ALL M
- [SDR DXTA2024092200612](https://openairdocs.org/sdr/DXTA2024092200612), Sep 20, 2024: BATTERY PACK. INOPERATIVE. EMER LIGHTS REMAINED ON IN ARMED POSITION, PRIOR AND AFTER ENGINE START. CORRECTIVE ACTION: REMOVED #1 EMERGENCY LIGHT BATTERY P/N: 7450LS-00 S/N: 006489 AND #2
- [SDR DXTA2023081492760](https://openairdocs.org/sdr/DXTA2023081492760), Aug 10, 2023: UNKNOWN. UNKNOWN. TRANSPONDER: BOTH TRANSPONDERS SWITCHING BACK AND FORTH, BOTH FAILING, ACCOMPANIED BY STEADY TCAS FAIL YELLOW CAS. PER THE CONTACT CENTER RECOMMEDATIONS PERFORM
- [SDR DXTA2023072691730](https://openairdocs.org/sdr/DXTA2023072691730), Jul 25, 2023: BATTERY. FAILED. CABIN EMER LIGHT FLASHING IN FLIGHT. REMOVED FWD EMERGENCY UGHT BATTERY P/N 74501.S-OO 5/N 006643 AND INSTALLED A TESTED BATTERY P/ N 74501.S-00 5/N 006489(TEST
- [SDR DXTA2023061288280](https://openairdocs.org/sdr/DXTA2023061288280), Jun 12, 2023: UNKNOWN. UNKNOWN. PASSENGER COMPARTMENT LIGHTING: WHEN SELECTING CABIN EMERGENCY LIGHTS TO ARM, ALL EMER LIGHTS COME ON AS NORMAL. HOWEVER, THE EMER LIGHTS STAY ON IN THE ARMED P
- [SDR DXTA2022121976550](https://openairdocs.org/sdr/DXTA2022121976550), Dec 18, 2022: SEAL. LEAKING. MAIN DOOR: MAIN DOOR SEAL IS LEAKING. VERY HIGH PITCH NOISE COMING OUT OF THE DOOR. REMOVED MAIN CABIN DOOR RUBBER SEAL PN 505-38948-901 NSN AND INSTALLED NEW M
- [SDR DXTA2022121476130](https://openairdocs.org/sdr/DXTA2022121476130), Dec 13, 2022: SEAL. NOT BONDED. MAIN DOOR SEAL HOWLING LOUDLY, CLIMBIMG THRU 10,000 FT, ABOUT 4 PSI. DURING DESCENT, STOPPED HOWLING AT 2.3 PSI. DOOR HANDLE STIFF & DIFFICULT TO CLOSE, BOTH IN
- [SDR DXTA2022010354560](https://openairdocs.org/sdr/DXTA2022010354560), Dec 31, 2021: BATTERY. NONE. CABIN EMERG LIGHT: EMERGENCY CABIN LIGHTING STARTED FLASHING ON THE DECENT INTO BOSTON. *** CORRECTIVE ACTION *** COMPLIED WITH TROUBLESHOOTING PRECEDURE AS OUT
- [SDR DXTA2021010804572](https://openairdocs.org/sdr/DXTA2021010804572), Jan 8, 2021: POWER SUPPLY. MALFUNCTIONED. DURING ENGINE START EMER LT NOT ARM CAS ILLUMINATED. PERFORMED THE GROUND RESET PROCEDURE AS DESCRIBED AND CAS MESSAGE EXTINGUISHED. AFTER TAKEOFF THE EMERGENCY
- [SDR 2020FA0000407](https://openairdocs.org/sdr/2020FA0000407), Sep 13, 2020: BALANCE WEIGHT. CORRODED. DURING ACCOMPLISHMENT OF SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING LEFT ELEVATOR ADJUSTABLE MASS BALANCE WEIGHTS BELOW TOLER
- [SDR DXTA2014111005923](https://openairdocs.org/sdr/DXTA2014111005923), Nov 7, 2014: DISPLAY. INOPERATIVE. GSD 1 FAIL GOLDEN CASS MESSAGE AT FL 320. PERFORMED FIM TASK 31-41-00-810-815-A WITH NO DEFECTS NOTED. REMOVED & INSTALLED A OVERHAULED GSD 41-1 IAW AMM 31-41-0
- [SDR DXTA2014031005680](https://openairdocs.org/sdr/DXTA2014031005680), Mar 8, 2014: UNKNOWN. ODOR. DURING CLIMB OUT A SLIGHT ACRID ODOR WAS NOTICED. CLIMBING THROUGH FL230 RECEIVED NR 1 BLEED FAIL CAS. UPON LEVELING AT FL270 THE ODOR INCREASED TO AN EXTREMELY

## Service difficulty reports on N332QS not matched to an aircraft (11)

They name N332QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA200702680](https://openairdocs.org/sdr/DXTA200702680), Dec 14, 2007: GROMMET. WORN. FL410 AT CRUISE, SOUND OF SIGNIFICATE AMOUNT OF AIR PASSING THRU MAIN CABIN DOOR.CABIN PRESSURE MAINTAINED. ADJUSTED DOOR FRAME SOCKETS AS REQUIRED DUE TO DOOR 
- [SDR DXTA200702142](https://openairdocs.org/sdr/DXTA200702142), Apr 25, 2007: UNKNOWN. ODOR. SMELL OF FUMES FROM OVERHEAD WEMAC VENTS ESPECIALLY WHEN TEMPERATURE CONTROL IS ADJUSTED TO A WARMER SETTING. [SUP 05-02-07] INSPECTED ENGINES FOR INTERNAL OIL 
- [SDR DXTA200601812](https://openairdocs.org/sdr/DXTA200601812), Dec 22, 2006: UPLOCK SWITCH. LOOSE. AFTER DEPARTURE THE GEAR HANDLE WAS RAISED, HOWEVER THE RED "GEAR UNSAFE AND "HYD PRESS' REMAINED ILLUMINATED. GEAR APPEARED TO EXTEND WITH NORMAL INDICATIONS. 
- [SDR DXTA200601188](https://openairdocs.org/sdr/DXTA200601188), Jan 9, 2006: BRAKE ASSY. WEAK. BRAKE PEDALS FEEL SOFT, SPONGY AND MOVE FURTHER THAN NORMAL. ITEM IS UNDER INVESTIGATION.
- [SDR DXTA200601176](https://openairdocs.org/sdr/DXTA200601176), Jan 1, 2006: BRAKE. WEAK. DURING BRAKE CHECK CO-PILOTS BRAKES GRAB AND TURN AIRPLANE TO LEFT. CO-PILOT REPORTED THAT BRAKES FELT MUSHY. BLED BRAKE SYSTEM IAW CHAP 32-42-00 OF THE 560 MM.
- [SDR DXTA200501170](https://openairdocs.org/sdr/DXTA200501170), Dec 28, 2005: ACCUMULATOR. OVERSERVICED. BRAKES NOT FUNCTIONING PROPERLY, WHILE TAXIING STRAIGHT AHEAD BRAKE PEDALS WERE STIFF AND NON-REACTIVE, THEN WOULD CATCH ONE SIDE AT A TIME CAUSING DIRECTIONAL 
- [SDR DXTA200501163](https://openairdocs.org/sdr/DXTA200501163), Dec 28, 2005: BRAKE ASSY. MALFUNCTIONED. BRAKES FUNCTIONED PROPERLY AT LAX & SMO. TOUCHDOWN BRAKING AT CRQ NORMAL. DURING TAXI, BRAKE PEDALS STIFF AND DO NOT REACT IMMEDIATELY. AFTER A FEW MOMENTS LEFT
- [SDR DXTA200501117](https://openairdocs.org/sdr/DXTA200501117), Nov 27, 2005: LINE. LEAKING. DURING TAXI-OUT, CO-PILOTS RIGHT BRAKE PEDAL GOES TO THE FLOOR WITH MINIMAL BRAKE EFFECTIVENESS. AFTER PUMPING BRAKE PEDAL , FULL PRESSURE RETURNS TO BRAKE PEDA
- [SDR DXTA200501109](https://openairdocs.org/sdr/DXTA200501109), Nov 25, 2005: LINE. LEAKING. DURING TAXI-OUT, CO-PILOTS RIGHT BRAKE PEDAL GOES TO THE FLOOR WITH MINIMAL BRAKE EFFECTIVENESS. AFTER PUMPING BRAKE PEDAL, FULL PRESSURE RETURNS TO BRAKE PEDAL
- [SDR DXTA200501082](https://openairdocs.org/sdr/DXTA200501082), Nov 13, 2005: LINE. LEAKING. RIGHT SIDE, RIGHT BRAKE PEDAL FEELS LIKE IT LOSES PRESSURE BUT REGAINS IT WITH MINOR PUMPING. APPLIED BRAKE PRESSURE TO RIGHT BRAKE AND DUPLICATED SQUAWK. INSPE
- [SDR DXTA200500916](https://openairdocs.org/sdr/DXTA200500916), Aug 23, 2005: BRAKE ASSY. WEAK. CO-PILOT TAXING TO RUNWAY, RT BRAKE PEDAL GOES APPROXIATELY FIVE INCHES MORE THAN LT PEDAL TO APPLY FULL PRESSURE. ITEM IS UNDER INVESTIGATION.

## 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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