# N609DP: 1998 Embraer EMB-145LR

- Status: Valid registration
- Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212, 55 seats)
- Engine: [Allison AE-3007A](https://openairdocs.org/engine/allison-ae-3007a) (registry code 03030)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT) (Embraer S.A.), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (Rolls-Royce Corporation) (OpenAirDocs)
- Serial number: 145069
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 30, 1998
- Certificate issued: September 29, 2011
- Expires: September 30, 2027
- Mode S code: A7E907
- Registered owner: [American Airlines Inc](https://openairdocs.org/faa-owner/AMERICAN%20AIRLINES%20INC)
- Location: [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth)
- Owner type: Corporation
- Owner's area on the map: 32.8240° N, 97.0491° W: Placed by OpenAirDocs at the center of ZIP code 76155, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=609DP
- Page: https://openairdocs.org/aircraft/N609DP

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): 104 in force

### Matched by airframe (Embraer EMB-145LR)

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2025-08-07](https://openairdocs.org/ad/2025-08-07): Flight Controls · Embraer EMB-145, EMB-145ER, EMB-145MR and 4 more. Effective Jun 26, 2025
- [AD 2024-26-07](https://openairdocs.org/ad/2024-26-07): Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Mar 11, 2025
- [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 2021-07-14](https://openairdocs.org/ad/2021-07-14): Main landing gear · Yaborã Indústria Aeronáutica EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 10 more. Effective Apr 20, 2021
- [AD 2021-04-09](https://openairdocs.org/ad/2021-04-09): Engine fuel and control · Yaborã Indústria Aeronáutica EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 10 more. Effective Mar 30, 2021
- [AD 2019-03-30](https://openairdocs.org/ad/2019-03-30): Engine Exhaust · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Mar 26, 2019
- [AD 2017-15-16](https://openairdocs.org/ad/2017-15-16): Flight controls · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Sep 5, 2017
- [AD 2017-12-09](https://openairdocs.org/ad/2017-12-09): Fuel · Embraer EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 10 more. Effective Jul 20, 2017
- [AD 2017-04-12](https://openairdocs.org/ad/2017-04-12): Ice and rain protection · Embraer EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 10 more. Effective Mar 29, 2017
- [AD 2015-02-13](https://openairdocs.org/ad/2015-02-13): Nacelles/pylons; Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Mar 6, 2015
- [AD 2013-22-18](https://openairdocs.org/ad/2013-22-18): Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Nov 20, 2013
- [AD 2012-19-06](https://openairdocs.org/ad/2012-19-06): Stabilizers · Embraer EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 9 more. Effective Oct 29, 2012
- [AD 2011-21-15](https://openairdocs.org/ad/2011-21-15): Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 7 more. Effective Nov 23, 2011
- [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011
- [AD 2010-16-02](https://openairdocs.org/ad/2010-16-02): Airborne Auxiliary Power · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Sep 9, 2010
- [AD 2010-16-01](https://openairdocs.org/ad/2010-16-01): Fuel · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Sep 9, 2010
- [AD 2010-12-07](https://openairdocs.org/ad/2010-12-07): Wings · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Jul 22, 2010
- [AD 2010-11-01](https://openairdocs.org/ad/2010-11-01): Fuselage · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jul 6, 2010
- [AD 2010-10-11](https://openairdocs.org/ad/2010-10-11): Landing gear · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jun 21, 2010
- [AD 2010-07-02](https://openairdocs.org/ad/2010-07-02): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 26 more. Effective May 3, 2010
- [AD 2010-03-07](https://openairdocs.org/ad/2010-03-07): Landing gear · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 11, 2010
- [AD 2009-26-02](https://openairdocs.org/ad/2009-26-02): Ice and rain protection · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 19, 2010
- [AD 2009-01-05](https://openairdocs.org/ad/2009-01-05): Maximum takeoff weight (MTOW) · Embraer EMB-145, EMB-145EP, EMB-145ER and 4 more. Effective Mar 27, 2009
- [AD 2008-22-19](https://openairdocs.org/ad/2008-22-19): Flight deck · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 19, 2008
- [AD 2008-17-05](https://openairdocs.org/ad/2008-17-05): Fuel tanks · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Sep 23, 2008
- [AD 2008-10-08](https://openairdocs.org/ad/2008-10-08): Reduces the compliance time for doing the modification · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective May 23, 2008
- [AD 2008-05-02](https://openairdocs.org/ad/2008-05-02): Tail section or rudder pedals · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Apr 8, 2008
- [AD 2008-03-03](https://openairdocs.org/ad/2008-03-03): Elevator control system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Feb 14, 2008
- [AD 2007-24-03](https://openairdocs.org/ad/2007-24-03): Forward fuselage right hand (RH) side skin · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Jan 2, 2008
- [AD 2007-10-11](https://openairdocs.org/ad/2007-10-11): Electrical bonding clamps · Embraer EMB-135BJ (Legacy 600), EMB-135LR, EMB-145LR and 2 more. Effective Jun 21, 2007
- [AD 2007-04-09](https://openairdocs.org/ad/2007-04-09): Left- and right-hand windshield temperature controllers · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 23, 2007
- [AD 2007-04-03](https://openairdocs.org/ad/2007-04-03): Pitot static heating relay K0057 · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 21, 2007
- [AD 2006-19-04](https://openairdocs.org/ad/2006-19-04): Honeywell COM unit and Mode S transponder · Bombardier BD-700-1A10, BD-700-1A11, 550 and 26 more. Effective Oct 17, 2006
- [AD 2006-16-17](https://openairdocs.org/ad/2006-16-17): Torque values of the screws that attach the seat tracks · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Sep 25, 2006
- [AD 2006-07-01](https://openairdocs.org/ad/2006-07-01): Horizontal stabilizer control unit (HSCU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective May 1, 2006
- [AD 2006-03-06](https://openairdocs.org/ad/2006-03-06): Pilot's and co-pilot's seat tracks · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 13, 2006
- [AD 2005-25-17](https://openairdocs.org/ad/2005-25-17): Auxiliary power unit (APU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 18, 2006
- [AD 2005-24-11](https://openairdocs.org/ad/2005-24-11): Elevator gust lock system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 9, 2006
- [AD 2005-24-02](https://openairdocs.org/ad/2005-24-02): Airplane flight manual (AFM) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 28, 2005
- [AD 2005-23-20](https://openairdocs.org/ad/2005-23-20): Auxiliary power unit (APU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 27, 2005
- [AD 2005-23-13](https://openairdocs.org/ad/2005-23-13): Nose landing gear (NLG) wheel · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 19, 2005
- [AD 2005-22-08](https://openairdocs.org/ad/2005-22-08): Total air temperature (TAT) sensor heating system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Nov 30, 2005
- [AD 2005-20-37](https://openairdocs.org/ad/2005-20-37): Main landing gear (MLG) trailing arms and integrity of the MLG pivot axle sealant. · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Nov 16, 2005
- [AD 2005-14-02](https://openairdocs.org/ad/2005-14-02): Left and right engine fire handles · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Aug 15, 2005
- [AD 2005-14-03](https://openairdocs.org/ad/2005-14-03): Engine-driven hydraulic pump · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Aug 10, 2005
- [AD 2005-13-22](https://openairdocs.org/ad/2005-13-22): Electric fuel pumps · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jul 7, 2005
- [AD 2005-05-09](https://openairdocs.org/ad/2005-05-09): Forward upper liners · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Apr 14, 2005
- [AD 2005-04-05](https://openairdocs.org/ad/2005-04-05): Air turbine starter (ATS) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 24, 2005
- [AD 2005-01-05](https://openairdocs.org/ad/2005-01-05): Nose Landing Gear Wheel Nuts and Associated Inner and Outer Seals, and Reidentifying the Landing Gear Strut · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Feb 9, 2005

### Matched by engine (Allison AE-3007A)

- [AD 2020-16-13](https://openairdocs.org/ad/2020-16-13): Turbine Engine Compressor Section · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 5 more. Effective Aug 14, 2020
- [AD 2017-26-06](https://openairdocs.org/ad/2017-26-06): Turbine/turboprop Engine, Turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 7 more. Effective Jan 31, 2018
- [AD 2013-26-06](https://openairdocs.org/ad/2013-26-06): High-pressure turbine (HPT) stage 2 wheels · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 5 more. Effective Feb 7, 2014
- [AD 2011-22-03](https://openairdocs.org/ad/2011-22-03): Low-cycle fatigue cracks · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 4 more. Effective Nov 17, 2011
- [AD 2007-24-05](https://openairdocs.org/ad/2007-24-05): Engine oil temperature · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 8 more. Effective Jan 2, 2008
- [AD 2004-04-05](https://openairdocs.org/ad/2004-04-05): Engine oil system · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Mar 9, 2004
- [AD 2001-25-05](https://openairdocs.org/ad/2001-25-05): Compressor Cone Shafts · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Jan 23, 2002
- [AD 2001-19-03](https://openairdocs.org/ad/2001-19-03): High Pressure Turbine 1st to 2nd Stage Turbine Spacer · Rolls-Royce AE 3007A and AE 3007C. Effective Oct 29, 2001
- [AD 2001-17-31](https://openairdocs.org/ad/2001-17-31): Second Stage High Pressure Turbine Wheel · Rolls-Royce AE 2100A, AE 2100C, AE 2100D3 and 2 more. Effective Oct 5, 2001
- [AD 2000-18-06](https://openairdocs.org/ad/2000-18-06): Digital Electronic Controls · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Sep 22, 2000
- [AD 2000-13-01](https://openairdocs.org/ad/2000-13-01): Turbine Wheels · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Sep 1, 2000
- [AD 2000-11-22](https://openairdocs.org/ad/2000-11-22): Critical Life-Limited Parts · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Aug 7, 2000
- [AD 99-03-03](https://openairdocs.org/ad/99-03-03): Full Authority Digital Engine Control (FADEC) · Rolls-Royce AE 3007A and AE 3007A1/1. Effective Feb 16, 1999
- [AD 98-11-32](https://openairdocs.org/ad/98-11-32): Sump Magnetic Chip Collector Plug · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Jun 18, 1998

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

- [AD 2008-13-14](https://openairdocs.org/ad/2008-13-14) (historical): Fuel system limitations (FSL) · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Jul 30, 2008
- [AD 2007-12-17](https://openairdocs.org/ad/2007-12-17) (historical): Metallic tubes enclosing the vent and pilot valve wires · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 9 more. Effective Jul 19, 2007
- [AD 2006-22-05](https://openairdocs.org/ad/2006-22-05) (historical): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 27 more. Effective Dec 1, 2006
- [AD 2006-20-08](https://openairdocs.org/ad/2006-20-08) (historical): Rod ends of aileron power control actuator, superseding AD 99-05-04 · Embraer EMB-145, EMB-145EP, EMB-145ER and 4 more. Effective Nov 8, 2006
- [AD 2006-04-02](https://openairdocs.org/ad/2006-04-02) (historical): Pitot static heating relay K0057 · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 9 more. Effective Mar 31, 2006
- [AD 2005-26-15](https://openairdocs.org/ad/2005-26-15) (historical): Certain components of the elevator control system · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 8 more. Effective Feb 3, 2006
- [AD 2005-25-04](https://openairdocs.org/ad/2005-25-04) (historical): Tail section or rudder pedals · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 9 more. Effective Dec 23, 2005
- [AD 2001-17-04](https://openairdocs.org/ad/2001-17-04) (historical): Horizontal Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR, EMB-145 and 3 more. Effective Sep 5, 2001
- [AD 2000-04-09](https://openairdocs.org/ad/2000-04-09) (historical): Elevator Servo Tab and Spring Tab Hinge Fittings of the Horizontal Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR, EMB-145 and 3 more. Effective Mar 10, 2000
- [AD 2010-19-01](https://openairdocs.org/ad/2010-19-01) (historical): High pressure turbine · Rolls-Royce AE 3007A. Effective Oct 27, 2010
- [AD 2009-08-51](https://openairdocs.org/ad/2009-08-51) (historical): High-pressure turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 6 more. Effective May 27, 2009
- [AD 2008-26-06](https://openairdocs.org/ad/2008-26-06) (historical): High-pressure turbine (HPT) · AE 3007A. Effective Jan 8, 2009
- [AD 2008-19-51](https://openairdocs.org/ad/2008-19-51) (historical): AE 3007A, AE 3007A1, AE 3007A1E and 5 more
- [AD 2001-08-15](https://openairdocs.org/ad/2001-08-15) (historical): Oil System · AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective May 14, 2001
- [AD 2000-09-05](https://openairdocs.org/ad/2000-09-05) (historical): Cone Shafts · AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Jul 5, 2000
- [AD 99-02-51](https://openairdocs.org/ad/99-02-51) (historical): Starter Shaft Seal · AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Apr 20, 1999

All 120: https://openairdocs.org/aircraft/N609DP/ads.md

## Information bulletins (advisory) (8 in force)

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021
- [SAIB AIR-20-17](https://openairdocs.org/saib/AIR-20-17): Air Conditioning - Cabin Pressure Control System. Issued Nov 3, 2020
- [SAIB NM-19-17](https://openairdocs.org/saib/NM-19-17): Ice and Rain Protection: Electrical Wiring Terminations at Pitot and TAT Relays. Issued Dec 5, 2019
- [SAIB NM-10-13](https://openairdocs.org/saib/NM-10-13): Navigation: Flight Management System. Issued Jan 7, 2010
- [SAIB NM-09-03](https://openairdocs.org/saib/NM-09-03): Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations. Issued Dec 11, 2008
- [SAIB NM-08-15](https://openairdocs.org/saib/NM-08-15): Instruments: Contamination of the Attitude Heading Reference System (AHRS) Computers. Issued Mar 26, 2008
- [SAIB NM-07-40](https://openairdocs.org/saib/NM-07-40): Embraer EMB-135/145 Landing Gear Incident. Issued Jul 9, 2007
- [SAIB NM-07-20](https://openairdocs.org/saib/NM-07-20): Flight Data Recorders. Issued Mar 21, 2007
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations

None matched to N609DP.

## FAA accident and incident reports (2)

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 20190413002719I](https://openairdocs.org/incident/20190413002719I), Apr 13, 2019: Embraer EMB-145LR (N609DP), Philadelphia, PA, Minor damage. On Saturday, April 13, 2019, piedmont airlines flight 5009 stuck a bird just prior to touchdown while landing at Philadelphia international airport (phl). The…
- [Incident 20131006018229I](https://openairdocs.org/incident/20131006018229I), Oct 6, 2013: Embraer EMB-145LR (N609DP), Peoria, IL, Minor damage. American eagle flight 3176, an emb 145LR, N609DP, serial number 145069, departed pia for dfw. Climbing through about 11,000 the crew heard a loud pop and…

## Service difficulty reports (111, newest 50)

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 HNAA2021120600595](https://openairdocs.org/sdr/HNAA2021120600595), Dec 5, 2021: NONE. NONE. PDIS 609 26-14 2598841 05DEC21 CLT CLOSE DURING APPROACH LAV SMOKE EICAS MESSAGE AND WARNING APPEARED WITH NO SMOKE OBSERVED IN LAV. MSG EXTINGUISHED ON ITS OWN
- [SDR HNAA2021081800386](https://openairdocs.org/sdr/HNAA2021081800386), Aug 17, 2021: UNKNOWN. ODOR. PDIS 609 05-50 2585201 17AUG21 PHL CLOSE LAV SMOKE IND AFTER TAKEOFF. WITH METAL/PLASTIC BURNING SMELL HISTORY: NO HISTORY FACT 17AUG21 23:51 PHL RAN #1 AND #2 
- [SDR HNAA2021010400002](https://openairdocs.org/sdr/HNAA2021010400002), Jan 2, 2021: UNKNOWN. ODOR. STRONG GAS ODOR IN COCKPIT AND CABIN. PERFORMED ENGINE RUNS ON BOTH APU + ENGINE BLEED WITH PACKS ON AND OFF NO EVIDENCE OF GAS SMELL. A/C OK FOR SERVICE.
- [SDR HNAA2020111300326](https://openairdocs.org/sdr/HNAA2020111300326), Nov 12, 2020: RELAY. BURNED. PITOT 3 INOPERABLE DISPLAYED ON EICAS DURING FLIGHT. MAINTENANCE PERFORMED: FIM TASK 30-31-00-810-803-A STEPS 1-4 UPON FURTHER INVESTIGATION FOUND BURNT PIN ON 
- [SDR HNAA2020071300192](https://openairdocs.org/sdr/HNAA2020071300192), Jul 10, 2020: WARNING MESSAGE. FALSE ACTIVATION. ON CLIMBOUT GOT BLD 1 LEAK MSG. FOLLOWED QRH AND MSG EXTINGUISHED AFTER A COUPLE MINUTES. MAINTENANCE: PERFORMED EMB FIM TASK 36-20-00-810-801A, BLOCKS 1,9,10 A
- [SDR HNAA2020030300084](https://openairdocs.org/sdr/HNAA2020030300084), Mar 2, 2020: CONNECTOR. DEFECTIVE. PDIS 609 30-31 2215751 02MAR20 PHL ASSGN PITOT 3 INOP MSG AFTER STARTING #1 ENGINE 30123 00 AD AIRCRAFT IS CURRENTLY IN WORK AT PHL. FIX:(PHL RON,04MAR20)R&RD P
- [SDR HNAA2018092100227](https://openairdocs.org/sdr/HNAA2018092100227), Sep 20, 2018: WARNING SYSTEM. ACTIVATED. SPOILER FAIL EICAS MESSAGE.
- [SDR HNAA2018091100219](https://openairdocs.org/sdr/HNAA2018091100219), Sep 10, 2018: CONNECTOR. DIRTY. SPOILER FAIL EICAS MSG AFTER T/O WITH SPOILERS INDICATING INTERMITTENTLY OPEN-CLOSE. INSPECTED AND CLEANED ALL INBOARD SPOILER CONNECTORS. PERFORMED OPS CHECK O
- [SDR HNAA2018081000187](https://openairdocs.org/sdr/HNAA2018081000187), Aug 8, 2018: TRANSCEIVER. MALFUNCTIONED. WEATHER RADAR WILL NOT PAINT ANY KNOWN WEATHER. R & R THE WEATHER RADAR R/T, OPS CHECKED GOOD IAW AMM 34-42-00.
- [SDR HNAA2018080300180](https://openairdocs.org/sdr/HNAA2018080300180), Aug 2, 2018: INDICATION SYS. FALSE INDICATION. ON TAKEOFF ROLL NR 2 ENGINE OIL PRESSURE WENT INTO THE YELLOW. CHECKED CMC MESSAGES. NO RELATED MESSAGES. CREW CONFIRMED MESSAGE EXTINGUISHED WITH NORMAL ENGINE
- [SDR HNAA2018062600127](https://openairdocs.org/sdr/HNAA2018062600127), Jun 22, 2018: WIRE. BURNED. STRONG ELECTRICAL ODOR IN THE FLIGHT DECK, DURING DESCENT FOR AT LEAST 2 MINUTES. NO SMOKE NOTED. R & R LANDING CONTACTOR K0233 DUE TO A BURNED WIRE OPS CHECKED
- [SDR HNAA2018052100004](https://openairdocs.org/sdr/HNAA2018052100004), May 19, 2018: CONNECTOR. DAMAGED. FLOOR EMERGENCY LIGHT INOPERATIVE BY SEATS 8A & 9A. REMOVED LIGHT STRIP, AND FOUND THE CONNECTOR PIN WAS NOT CONNECTED. CONNECTED THE PIN AND SECURED LIGHT.
- [SDR HNAA2017090700302](https://openairdocs.org/sdr/HNAA2017090700302), Sep 2, 2017: INVERTER. INOPERATIVE. EMERGENCY EXIT LIGHT ABOVE FA SEAT INOPERATIVE. REMOVED & REPLACED THE EMERGENCY LIGHT DC/AC INVERTER IAW 33-50-11-000/400-801-A. OK FOR SERVICE.
- [SDR HNAA2017071200239](https://openairdocs.org/sdr/HNAA2017071200239), Jul 10, 2017: LINE. LEAKING. NR 1 HYD SYS FAIL MESSAGE AFTER LANDING. EDP WAS NOT OPERATED FOR MORE THAN 15 MIN WITH NO FLUID. INSPECTED AND FOUND A HYD LINE UNDER PANEL 192AL LEAKING. R & 
- [SDR HNAA2017041200117](https://openairdocs.org/sdr/HNAA2017041200117), Apr 8, 2017: APU. FIRE. DURING APU START, GROUND CREW REPORTED FIRE COMING FROM APU. DOWN POWERED THE ACFT AND ON EXITING SAW ONLY SMOKE COMING FROM THE TAIL. INSPECTED THE APU BAY FOR
- [SDR HNAA2017032700096](https://openairdocs.org/sdr/HNAA2017032700096), Mar 26, 2017: CIRCUIT BREAKER. TRIPPED. PITCH TRIM MAIN INOPERATIVE EICAS MESSAGE DURING CLIMB, FOUND THE CIRCUIT BREAKER TRIPPED. RESET THE CIRCUIT BREAKER C9 AND OPS CHECKED IAW AMM 27-40-00-700-802
- [SDR HNAA201701040003](https://openairdocs.org/sdr/HNAA201701040003), Jan 4, 2017: WARNING MESSAGE. FALSE ACTIVATION. NR 2 BLEED LEAK WARNING MESSAGE DISPLAYED AFTER TAKEOFF. PERFORMED QRH PROCEDURES, WARNING WENT AWAY AND REPEATEDLY CAME ON AND WENT AWAY. GROUND RAN AIRCRAFT A
- [SDR HNAA2016122800350](https://openairdocs.org/sdr/HNAA2016122800350), Dec 28, 2016: WARNING LIGHT. FALSE ACTIVATION. DURING FLIGHT, LANDING GEAR WAS EXTENDED AND WHEN RETRACTED, RECEIVED A LANDING GEAR DISAGREE MESSAGE ON EICAS. MESSAGE EXTINGUISHED DROPPING BELOW 200KTS. AIRC
- [SDR HNAA2016120500373](https://openairdocs.org/sdr/HNAA2016120500373), Dec 5, 2016: CLAMP. DAMAGED. DURING CLIMBOUT AT 8000 FT, CREW HEARD LOUD THUNK, FOLLOWED BY BLEED 1 LEAK MESSAGE. RAN QH, THE BLEED 2 LEAK MESSAGE DISPLAYED. RAN QRH, THEN BLEED, THEN BLEED
- [SDR SIMA20161020003](https://openairdocs.org/sdr/SIMA20161020003), Oct 20, 2016: SPAR. CRACKED. RIGHT WING SPAR I LOWER FLANGE CRACKED. REPAIRED THE SPAR IAW ERS-EM-57MR-710.
- [SDR SIMA20161014003](https://openairdocs.org/sdr/SIMA20161014003), Oct 14, 2016: BATTERY PACK. INOPERATIVE. LEFT FUSELAGE FRONT FAIRING EXTERNAL EMERGENCY LIGHT AND CEILING AISLE NR 1 EMERGENCY LIGHT DO NOT COME ON DURING TEST. REMOVED AND REPLACED THE NR 1 EMERGENCY 
- [SDR SIMA20161013001](https://openairdocs.org/sdr/SIMA20161013001), Oct 13, 2016: SHEAR ANGLE. CORRODED. FRAME 65 SHEAR ANGLE AT CARGO DOOR LOWER SILL IS CORRODED. REMOVED AND REPLACED THE SHEAR ANGLE IAW SRM 53-31-04.
- [SDR SIMA20160919004](https://openairdocs.org/sdr/SIMA20160919004), Sep 19, 2016: CHARGER. INOPERATIVE. LEFT FUSELAGE FRONT FAIRING EXTERNAL EMERGENCY LIGHT AND CEILING AISLE NR 1 EMERGENCY LIGHT DO NOT COME ON DURING TEST. REMOVED AND REPLACED THE NR 1 EMERGENCY 
- [SDR SIMA20160919001](https://openairdocs.org/sdr/SIMA20160919001), Sep 19, 2016: EXCITER. INOPERATIVE. NR 2 ENGINE START HUNG AT 32 PERCENT N2. ABORTED AND MOTORED THEN HAD STRONG ODOR OF FUEL IN COCKPIT & CABIN DECLARED EMERGENCY RETURNED TO GATE. REMOVED AND RE
- [SDR SIMA20160829001](https://openairdocs.org/sdr/SIMA20160829001), Aug 29, 2016: O-RING. LEAKING. AT 37000 FT, RED BLEED 1 LEAK INDICATION AND EICAS MESSAGE. EXTINGUISHED DESCENDING THROUGH 24000 FT. REPLACED O-RING AT JOINT 21 IAW AMM 36-11-10, LEAK CHECKED
- [SDR SIMA20160413005](https://openairdocs.org/sdr/SIMA20160413005), Apr 13, 2016: UPLOCK. FAILED. UPON GEAR RETRACTION, LT MAIN & NOSE GEAR RETRACTED NORMALLY. RT MAIN SHOWED IN TRANSIT & UNSAFE INDICATION WITH A LOUD THUMPING SOUND COMING FROM FUSELAGE BEHI
- [SDR SIMA20160411003](https://openairdocs.org/sdr/SIMA20160411003), Apr 11, 2016: PROXIMITY SWITCH. FAILED. DEPARTED & UPON GEAR RETRACTION A LOUD CONTINUOUS THUMPING NOISE COULD BE HEARD A LOUD WITH RT MAIN GEAR INDICATION ON EICAS CYCLING, BETWEEN UP & IN TRANSIT EX
- [SDR SIMA20160201001](https://openairdocs.org/sdr/SIMA20160201001), Feb 1, 2016: FLASHLIGHT. INTERMITTENT. CAPTAINS FLASHLIGHT INTERMITTENT. R & R CAPTAINS FLASHLIGHT IAW AMM 25-60-00. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150930001](https://openairdocs.org/sdr/SIMA20150930001), Sep 30, 2015: WIRE. BROKEN. EMERGENCY LIGHT STRIP FLOOR NR 7 WIRE BROKEN. R & R FLOOR NR 7 EMER LIGHT STRIP IAW AMM IAW 33-50-00. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150706003](https://openairdocs.org/sdr/SIMA20150706003), Jul 6, 2015: FADEC. MALFUNCTIONED. LARGE FLUCTUATIONS ON ENG NR 1 THRUST AT CRUISE ALTITUDE. TRANSFERRED TO NRWC 609-XNA-02379. REFERENCE NRWC 609-XNA-02379. REPLACED ENG 1 FADEC 1B IAW AMM 73-22
- [SDR SIMA20150613003](https://openairdocs.org/sdr/SIMA20150613003), Jun 13, 2015: QUICK DISCONNECT. UNSECURE. AIRCRAFT WAS SLOW TO STOP ON LANDING. AT GATE NOTICED RT INBD BRAKE WAS LOW GREEN WHILE OTHER 3 INDICATORS HIGH GREEN. SUSPECT RT INBD BRAKE INOPERATIVE. NO MSG
- [SDR SIMA20150609003](https://openairdocs.org/sdr/SIMA20150609003), Jun 9, 2015: ROLLER. LACK OF LUBE. MAIN CABIN DOOR DIFFICULT TO OPEN OR CLOSE. LUBED PAX DOOR ROLLERS, AND R & R INNER DOOR HANDLE IAW MM 52-18-05. OPS CHECKED GOOD AT THIS TIME.
- [SDR SIMA20150516001](https://openairdocs.org/sdr/SIMA20150516001), May 16, 2015: LIGHT. INOPERATIVE. EXIT SIGN LIGHT AT TOP OF THE RT OVERWING DOOR INOPERATIVE. R & R EMER LIGHT DC & AC INVERTER NR 5 IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150414004](https://openairdocs.org/sdr/SIMA20150414004), Apr 14, 2015: SIGN. INOPERATIVE. RIGHT EMER EXIT DOOR SIGN IS INOPERATIVE. R & R RT EMER EXIT DOOR SIGN IAW AMM 33-50-14. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150321001](https://openairdocs.org/sdr/SIMA20150321001), Mar 21, 2015: UPLOCK. DEFECTIVE. UPON RAISING GEAR AFTER TAKEOFF UNUSUAL NOISE, THUNK, THUNK, THUNK ETC & LT GEAR INDICATOR CYCLED BETWEEN UP & IN TRANSIT. TRANSFERRED TO NRWC 609-DFW-02208. R 
- [SDR SIMA20150321002](https://openairdocs.org/sdr/SIMA20150321002), Mar 21, 2015: CONNECTOR. DEFECTIVE. UPON RAISING GEAR AFTER TAKEOFF UNUSUAL NOISE, THUNK, THUNK, THUNK ETC, & LT GEAR INDICATOR CYCLED BETWEEN UP & TRANSIT. R & R LT MLG FWD DOWNLOCK PROXIMITY SWI
- [SDR SIMA20150317002](https://openairdocs.org/sdr/SIMA20150317002), Mar 17, 2015: SIGN. INOPERATIVE. CABIN FWD EMER EXIT SIGN INOPERATIVE. R & R CABIN FWD EMER EXIT SIGN IAW AMM 33-50-14. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150309002](https://openairdocs.org/sdr/SIMA20150309002), Mar 9, 2015: O-RING. DAMAGED. BLEED 1 LEAK CLIMBING THRU 13000. IAW AOM VOL 1, IT EXTINGUISHED. FOLLOWING DUCT LINES INSPECTION IAW AMM 36-11-09 FOUND O RING 21 LEAKING. R & R O RING, LEAK C
- [SDR SIMA20150205007](https://openairdocs.org/sdr/SIMA20150205007), Feb 5, 2015: LIGHT. INOPERATIVE. ROW 3 EMER LIGHT INOPERATIVE. R & R ROW 3 EMER LIGHT BULB IAW AMM 33-50-08-000-801-A & 33-50-08-400-801-A. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150112003](https://openairdocs.org/sdr/SIMA20150112003), Jan 12, 2015: LIGHT. INOPERATIVE. RIGHT OVERWING EXIT SIDEWALL MARKER LIGHT INOPERATIVE. R & R RT OVERWING EXIT SIDEWALL MARKER IAW AMM 33-50-14. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150104004](https://openairdocs.org/sdr/SIMA20150104004), Jan 4, 2015: PIN. NOT SEATED. RIGHT OVERWING EXIT DOOR AFT EMER LIGHT INOPERATIVE. RESEATED ELEC PIN CONNECTIONS FOR RT OVERWING EXIT DOOR AFT EMER LIGHT IAW SWPM 20-50-00. OPERATIONS CHECKE
- [SDR SIMA20141101010](https://openairdocs.org/sdr/SIMA20141101010), Nov 1, 2014: LIGHT. BROKEN. LEFT NR 3 EMER LIGHT STRIP BROKE. R & R LT NR 3 EMER LIGHT STRIP IAW AMM 33-50-12. SEE NRTC BOW 169909 FOR OPERATIONS CHECK.
- [SDR SIMA20141101009](https://openairdocs.org/sdr/SIMA20141101009), Nov 1, 2014: LIGHT. BROKEN. LEFT NR 4 EMER LIGHT STRIP BROKE. R & R LT NR 4 EMER LIGHT STRIP IAW AMM 33-50-12. SEE NRTC BOW 169909 FOR OPERATIONS CHECK.
- [SDR SIMA20141101008](https://openairdocs.org/sdr/SIMA20141101008), Nov 1, 2014: SKIN. CRACKED. FRAME 75 SKIN CRACKED AT FASTENER HOLE, BELOW STRINGER 2R. REPAIRED FRAME 75 SKIN CRACK IAW ERS-EM-53MR-901.
- [SDR SIMA20141101007](https://openairdocs.org/sdr/SIMA20141101007), Nov 1, 2014: CONNECTOR. BROKEN. EMERGENCY LIGHT STRIP CONNECTOR BROKEN AT FLOOR PANEL 261BF. R & R EMER LIGHT STRIP CONNECTOR IAW WM 31-10-02 & SWPM 20-00-03. SEE BOW 169909 FOR OPERATIONS CHE
- [SDR SIMA20141101006](https://openairdocs.org/sdr/SIMA20141101006), Nov 1, 2014: CONNECTOR. BROKEN. EMERGENCY LIGHT STRIP CONNECTOR BROKEN AT FLOOR PANEL 241BF. R & R EMER LIGHT STRIP CONNECTOR IAW WM 31-10-02 & SWPM 20-00-03. SEE BOW 169909 FOR OPERATIONS CHE
- [SDR SIMA20141101005](https://openairdocs.org/sdr/SIMA20141101005), Nov 1, 2014: SKIN. CRACKED. FRAME 75 SKIN CRACKED AT FASTENER HOLE, BELOW STRINGER 2L. REPAIRED FRAME 75 SKIN CRACK AT FASTENER HOLE, BELOW STRINGER 2L IAW ERS-EM-53MR-901.
- [SDR SIMA20141003003](https://openairdocs.org/sdr/SIMA20141003003), Oct 3, 2014: COMPUTER. MALFUNCTIONED. DURING CRUISE AT 360 IN STRAIGHT & LEVEL FLIGHT. AP DISCONNECTED & BEGAN A RIGHT TURN & A 400 FT DECENT FLIGHT CREW CORRECTED & RETURNED TO CRUISE COURSE & ALT,
- [SDR SIMA20140920002](https://openairdocs.org/sdr/SIMA20140920002), Sep 20, 2014: CONNECTOR. LOOSE. RIGHT OVERWING EMER LIGHT IS INOPERATIVE. REMOVED PANEL 194 AR FOUND CONNECTOR LOOSE. CLEANED & RECONNECTED CONNECTION IAW AMM 33-50-10. OPERATIONS CHECKED GOOD
- [SDR SIMA20140824002](https://openairdocs.org/sdr/SIMA20140824002), Aug 24, 2014: LIGHT. INOPERATIVE. PARKING BRAKE LIGHT INOPERATIVE. REPLACED BULBS IN PARKING BRAKE LIGHT INDICATOR IAW AMM 20-13-04. OPERATIONS CHECKED GOOD. BULBS OBTAINED FROM KIT.

All 111: https://openairdocs.org/aircraft/N609DP/reports.md

## STCs that may be installed (OpenAirDocs) (75, first 50)

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 EMB-145LR)

- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST02176AT-D](https://openairdocs.org/stc/ST02176AT-D): Installation of a Teledyne Mini Flight Data Acquistion Unit. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST02216AT-D](https://openairdocs.org/stc/ST02216AT-D): Installation of Teledyne Mini Flight Data Acquisition Unit in a Provisioned EMB-135/145. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST02310AT](https://openairdocs.org/stc/ST02310AT): Installation of SAF-T-GLO photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST01409LA](https://openairdocs.org/stc/ST01409LA): Installation of a reinforced cockpit door. Safran Cabin Inc
- [STC ST01984LA-D](https://openairdocs.org/stc/ST01984LA-D): Modification and installation of passenger seats, passenger service units and filler panels, seat track covers, and seat row placards. Safran Cabin Inc
- [STC ST04219NY](https://openairdocs.org/stc/ST04219NY): Installation of SpaceX Starlink Aviation System. Aerospace Design & Compliance LLC
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST00640DE](https://openairdocs.org/stc/ST00640DE): Installation of Tropospheric Airborne Meteorolocigal Data Reporting System (TAMDAR). FLYHT Inc
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST04159CH](https://openairdocs.org/stc/ST04159CH): Upgrade of Honeywell Primus II Communications Units RCZ-8XX Transponders to support Certification of Automatic Dependent Surveillance -Broadcast (ADS-B) Out. CMD Flight Solutions LLC
- [STC ST04527CH](https://openairdocs.org/stc/ST04527CH): Installation of a 16 passenger configuration. C&L STC Holdings LLC
- [STC ST04177NY](https://openairdocs.org/stc/ST04177NY): Installation of ALI LED Cabin Lighting, Cabin and Crew AC Power Outlets, LH Fwd Closet and Misc Cabin Mods. C & L STC Holdings LLC
- [STC ST01983WI](https://openairdocs.org/stc/ST01983WI): Installation of a folding stair in the main entrance for models equipped with a side-hinged main door. Worldwide Aviation Engineering LLC
- [STC ST04212NY](https://openairdocs.org/stc/ST04212NY): Installation of Universal UNS-1Lw Flight Management System. C&L Engineering Services, LLC
- [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC ST04213NY](https://openairdocs.org/stc/ST04213NY): PAX Social Distance Floorplan Reconfiguration. C&L Engineering Services LLC
- [STC ST04281AT](https://openairdocs.org/stc/ST04281AT): Installation for the Upgrade of the NZ-2000 FMS computer for software version NZ6. Chippewa Aerospace Inc
- [STC ST03158CH-D](https://openairdocs.org/stc/ST03158CH-D): Installation of a Reconfiguration of a Cabin Floorplan. Standard Aero Business Aviation Services LLC
- [STC SA9087SC-D](https://openairdocs.org/stc/SA9087SC-D): RECORE® Hamilton Sundstrand heat exchanger, P/N 816630-1 / -2 in accordance with Honeywell LORI Sealed Drawing List SDL3869-1 Rev. A, dated June 7, 2005 or later FAA approved revision. Honeywell International Inc
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST01039DE](https://openairdocs.org/stc/ST01039DE): Passenger seating arrangement for 30 or less passengers. Deluxe Public Charter LLC
- [STC ST04537NY](https://openairdocs.org/stc/ST04537NY): Installation of Air Filtration. Kilroy Aviation LLC
- [STC ST09858SC](https://openairdocs.org/stc/ST09858SC): Installation of cabin automatic coffee brewing system. Safran Cabin Germany Gmbh
- [STC ST04255CH](https://openairdocs.org/stc/ST04255CH): Installation of an Automatic Dependent Surveillance-Broadcast (ADS-B Out) System. ENVOY AIR
- [STC ST03420NY](https://openairdocs.org/stc/ST03420NY): Installation of a Cabin Interior. Delta Engineering Corporation
- [STC ST02327LA](https://openairdocs.org/stc/ST02327LA): Installation of replacement proximity sensor harness assembly part numbers used on the nose and main landing gears. Safran Electrical Components USA Inc
- [STC ST04423NY](https://openairdocs.org/stc/ST04423NY): Installation of ADS-B Out. FTI Engineering Nework GmbH
- [STC ST00015IB](https://openairdocs.org/stc/ST00015IB): Installation of a Honeywell HF Communication System, model KHF 1050, with provisions for a dual installation. Embraer Engineering & Technology Center - USA Inc
- [STC ST00014IB](https://openairdocs.org/stc/ST00014IB): Installation of a second Honeywell HF Communication System, model KHF 1050. 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 ST04333NY](https://openairdocs.org/stc/ST04333NY): Installation of sat: Tglo® Photolumincsccnt Aisle Path Marking System. STG Aerospace Ltd
- [STC ST10550SC](https://openairdocs.org/stc/ST10550SC): Installation of a WeatherMASTER X-Band Fuselage Nose Radome Assembly. The NORDAM Group LLC
- [STC ST04316CH](https://openairdocs.org/stc/ST04316CH): Installation of a Smartsky System in accordance with StandardAero Master Data List 1034570, Revision (C), dated March 23, 2019 or later FAA approved revision. StandardAero Business Aviation Services LLC
- [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST000081B](https://openairdocs.org/stc/ST000081B): Installation of a second SELCAL channel. EMBRAER - Empresa Brasileira de Aeronautica
- [STC ST00008IB](https://openairdocs.org/stc/ST00008IB): Installation of a second SELCAL channel. EMBRAER - Empresa Brasileira de Aeronautica
- [STC ST03177NY](https://openairdocs.org/stc/ST03177NY): Installation of a Honeywell ADS-B (Out), EHS and FreeFlight GPS. Delta Engineering Corporation
- [STC ST01520WI](https://openairdocs.org/stc/ST01520WI): Installation of the Concorde RG-442 VRSLA Battery and Temperature Sensor in place of the original Nickel-Cadmium Battery. Concorde Battery Corporation
- [STC ST00361BO](https://openairdocs.org/stc/ST00361BO): Installation of a Honeywell Primus II (XS-852) ADS-B Out System. Pro Star Aviation, LLC
- [STC ST04282CH](https://openairdocs.org/stc/ST04282CH): Installation of Honeywell CD-830 Control Display Unit (CDU). Nextant Aerospace
- [STC ST01702WI](https://openairdocs.org/stc/ST01702WI): Change seating configuration to 30 passengers by removal of seats. Worldwide Aircraft Engineering LLC
- [STC ST04108CH](https://openairdocs.org/stc/ST04108CH): Installation of Gogo Business Aviation ATG-8000 High Speed Internet with Wireless Local Area Network (WLAN). Nextant Aerospace
- [STC ST04367AT](https://openairdocs.org/stc/ST04367AT): Removal of the Existing Honeywell DL-900 or DL-950 Data Loader and Installation of the Honeywell DL-1000 Data Loader. Chippewa Aerospace Inc
- [STC ST04190AT](https://openairdocs.org/stc/ST04190AT): Installation of an ADS-B Out. Chippewa Aerospace Inc
- [STC ST02406LA](https://openairdocs.org/stc/ST02406LA): Installation of TCAS version 7.1. Aviation Communication and Surveillance Systems (ACSS) LLC

All 75: https://openairdocs.org/aircraft/N609DP/stcs.md

## Related

- Other Embraer EMB-145LR aircraft: https://openairdocs.org/model/embraer-emb-145lr/aircraft.md
- The Allison AE-3007A engine: https://openairdocs.org/engine/allison-ae-3007a.md

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