# N374QS: 2015 Embraer Executive EMB-505

- Status: Valid registration
- Airframe: [Embraer Executive EMB-505](https://openairdocs.org/model/embraer-executive-emb-505) (registry code 3260390, 8 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: 50500289
- Year built: 2015
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, commuter
- Airworthiness date: August 19, 2015
- Certificate issued: November 14, 2025
- Expires: November 30, 2032
- Mode S code: A44416
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=374QS
- Page: https://openairdocs.org/aircraft/N374QS

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 Executive 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 N374QS.

## FAA accident and incident reports

None matched to N374QS.

## Service difficulty reports (14)

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 DXTA2026100509949](https://openairdocs.org/sdr/DXTA2026100509949), Sep 30, 2026: CONTROL MODULE. FAULTED. GOT A BRK FAIL CAS MESSAGE WHILE TAXIING OUT. HAD TO APPLY MAX PEDAL PRESSURE TO GET ANY BRAKES AT ALL AND IT SEEMED AS IF THE LEFT BRAKE WOULD GRAB WHEN I FINA
- [SDR DXTA2026012006593](https://openairdocs.org/sdr/DXTA2026012006593), Jan 19, 2026: BATTERY PACK. FAULTED. EMER LIGHT NOT ARM CAS ON WITH SWITCH IN ARM, ENGINES RUNNING AND NO GPU. GROUND RESET PROCEDURE UNSUCCESFUL. REVIEWED SL505-33-0005 REV 5 "EMER LIGHT T/S" AND 
- [SDR DXTA2025120505944](https://openairdocs.org/sdr/DXTA2025120505944), Dec 2, 2025: PRESSURE SWITCH. FAULTED. PASSING FL215 "FUEL 1 FEED FAULT" WHITE CAS DISPLAYED. ON FUEL SYNOPTIC PAGE, DISPLAYED AMBER X OVER EJECTOR PUMP 1. REMOVED AND REPLACED LEFT FAULTY PRESSURE S
- [SDR 2025FA0000772](https://openairdocs.org/sdr/2025FA0000772), Nov 19, 2025: SKIN. CORRODED. CORROSION FOUND ON TOP OF BOTH WINGS FWD OF SPEED BRAKES
- [SDR DXTA2025092905113](https://openairdocs.org/sdr/DXTA2025092905113), Sep 27, 2025: LIGHT. BROKEN. THE WHITE EMER LIGHT LOCATED IN THE LAV AREA BELOW THE TOILET IS INOP WHEN TESTING THE EMERGENCY LIGHTS CORRECTIVE ACTION: TECHS FOUND THE EMERGENCY LIGHTING AS
- [SDR DXTA2025021802406](https://openairdocs.org/sdr/DXTA2025021802406), Feb 17, 2025: DOOR. OUT OF ALIGNMENT. MAIN DOOR: DOOR MISALIGNED AND WILL NOT CLOSE. TOP RIGHT PIN IS NOT SEATING FOUND MED TOP TRIM PEICE GETING HUNG UP ON THE DOOR CAUSING IT TO NOT CLOSE ALL THE 
- [SDR DXTA2025021202290](https://openairdocs.org/sdr/DXTA2025021202290), Feb 7, 2025: DOOR. OUT OF ADJUST. MAIN DOOR: MAIN CABIN DOOR WILL NOT CLOSE. THE DOOR IS MISALIGNED WITH AN INCH GAP. FROM THE OUTSIDE THE DOOR SEAL IS PINCHED. SEE PIC
- [SDR DXTA2024051011733](https://openairdocs.org/sdr/DXTA2024051011733), May 10, 2024: CONTROL PANEL. FAULTED. AFTER POWERING DOWN THE AIRCRAFT WITH THE EMER LIGHT SWITCH IN THE OFF POSITION THE EMERGENCY LIGHTS REMAINED ON. AFTER CYCLING THE SWITCH WE WERE ABLE TO GET T
- [SDR DXTA2024042911640](https://openairdocs.org/sdr/DXTA2024042911640), Apr 28, 2024: BATTERY. FAILED. ALL CABIN EMERGENCY LIGHTS ILLUMINATE AND REMAIN ON WITH THE EMER LT SWITCH IN THE ARM POSITION. REMOVED FAULTY EMERGENCY BATTERY. REF. AMM 33-52-01. REPLACED F
- [SDR DXTA2024040511409](https://openairdocs.org/sdr/DXTA2024040511409), Apr 4, 2024: VALVE. FAILED. STARTED ENGS TO DEPART & ACFT BEGAN ROLLING WITH PARKING BRAKE SET & GOOD PRESSURE IN EM BRK ACCUMULATOR. REGULAR BRAKES WORKED, BUT EM BRAKE DID NOT. RESET EM 
- [SDR DXTA2023032883310](https://openairdocs.org/sdr/DXTA2023032883310), Mar 28, 2023: UNKNOWN. UNKNOWN. EMERGENCY LIGHTS FLICKER INFLIGHT AND REMAIN ON WITH THE SWITCH SET TO ARM. R/R FWD AND AFT EMERGENCY LIGHT BATTERY PACKS IAW PHENOM 300 AMM 33-52-01. OPS CHECK
- [SDR 2020FA0000389](https://openairdocs.org/sdr/2020FA0000389), Aug 29, 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 DXTA2018093001482](https://openairdocs.org/sdr/DXTA2018093001482), Sep 30, 2018: NOT REPORTED. MALFUNCTIONED. WITH THE AIRCRAFT POWERED WITH A GPU, WE RECEIVED AN OVERVOLTAGE OF 30V AND THE GPU AUTOMATICALLY DISCONNECTED. AT THE SAME TIME A STRONG ACRID, BURNING, ELECTR
- [SDR DXTA2016030806195](https://openairdocs.org/sdr/DXTA2016030806195), Mar 8, 2016: CONTROL MODULE. FAILED. ON LANDING ROLL OUT, WHEN BRAKING APPLIED TO DECELERATE, BRAKE FAIL MSG ILLUMINATED ON CAS. ZERO BRAKING ACHIEVED USING NORMAL BRAKES. EMERGENCY BRAKE SYS USED.

## Service difficulty reports on N374QS not matched to an aircraft (9)

They name N374QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA200802960](https://openairdocs.org/sdr/DXTA200802960), Mar 23, 2008: TRIM TAB. OBSTRUCTED. JAMMED ELEVATOR TRIM TAB ON DEPARTURE. FOUND FOD WEDGED IN CHAIN SPROCKET AREA OF PEDESTAL. REMOVED FOD, NO DAMAGE NOTED, CLEANED AND LUBED TRIM COMPONENTS, OPS
- [SDR DXTA20082960](https://openairdocs.org/sdr/DXTA20082960), Mar 23, 2008: SPROCKET. OBSTRUCTED. JAMMED ELEVATOR TRIM TAB ON DEPARTURE. FOUND FOD WEDGED IN CHAIN SPROCKET AREA OF PEDESTAL. REMOVED FOD, NO DAMAGE NOTED, CLEANED AND LUBED TRIM COMPONENTS, OPS
- [SDR DXTA200802753](https://openairdocs.org/sdr/DXTA200802753), Jan 8, 2008: WIRE. DAMAGED. ON INITIAL CLIMB OUT LANDING GEAR HANDLE WOULD NOT MOVE. REPLACED 5 EA WIRE SPLICES AT LT MAIN GEAR SQUAT SWITCH, REPACKED LT MAIN GEAR STRUT, SERVICED STRUT, I
- [SDR DXTA200702670](https://openairdocs.org/sdr/DXTA200702670), Dec 10, 2007: SQUAT SWITCH. ERRATIC. PRESSURIZATION INOP ON CLIMBOUT CABIN RATE HAD NO CONTROL OF RATE OF CLIMB. AT ALTITUDE CONTROLLER HAD NO EFFECT ON CABIN ALT. ON DESCENT PRESSURIZATION FAILED 
- [SDR DXTA200702551](https://openairdocs.org/sdr/DXTA200702551), Oct 18, 2007: SHUTTLE VALVE. DEFECTIVE. CAPT AND FO'S BRAKES ARE SPONGY. PEDALS REQUIRES MORE THAN USUAL PRESSURE TO ACHIEVE BRAKING ACTION. REMOVED DEFECTIVE RT BRAKE SHUTTLE VALVE , INSTALLED SHUTTL
- [SDR DXTA200702534](https://openairdocs.org/sdr/DXTA200702534), Oct 11, 2007: BRAKE ASSY. WEAK. CAPT AND FO BRAKES ARE SPONGY. COMPLIED WITH TAXI AND BRAKE CHECK OF AIRCRAFT NO DEFECTS NOTED. WORK DONE IAW CE560 MM 32-42-00
- [SDR DXTA200702531](https://openairdocs.org/sdr/DXTA200702531), Oct 8, 2007: BRAKE. MALFUNCTIONED. F/O'S BRAKES GO TO THE FLOOR WHEN PRESSED. 11-01-07 FOUND BRAKES TO BE SPONGY. BLEED BRAKES THREE TIMES IAW CE-560MM CH 32-42-00. OPS CHECKS GOOD.
- [SDR DXTA200500674](https://openairdocs.org/sdr/DXTA200500674), Apr 11, 2005: B-NUT. LOOSE. F/O'S BRAKES (LEFT AND RIGHT) FEELS SPONGY. CAPT'S BRAKES ARE OK. ALSO, IF YOU PUMP THE F/O'S BRAKES, BRAKES COME UP TO HAVING PRESSURE. REMOVED COCKPIT AND DRO
- [SDR 2003FA0000806](https://openairdocs.org/sdr/2003FA0000806), Jul 31, 2003: CONTROL CABLE. OUT OF RIG. DURING INSP FLAP PRESELECT CABLE P/N: 5565175-4CR, LOCATED IN COCKPIT CTR PEDESTAL, WAS FOUND BROKEN IN HALF AT SWEDGED BALL END. DURING INSTALLATION OF NEW CAB

## 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 Executive 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 Executive EMB-505 aircraft: https://openairdocs.org/model/embraer-executive-emb-505/aircraft.md
- The Pratt & Whitney Canada PW535E engine: https://openairdocs.org/engine/pratt-whitney-canada-pw535e.md

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