# N600BP: 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 AE3007C series](https://openairdocs.org/engine/allison-ae3007c-series) (registry code 03028)
- 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: 145044
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 6, 1999
- Certificate issued: September 28, 2011
- Expires: September 30, 2027
- Mode S code: A7C766
- 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=600BP
- Page: https://openairdocs.org/aircraft/N600BP

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. The registry lists only the engine series, so ADs for every Allison AE3007C model are included.

## ADs that may apply (OpenAirDocs): 102 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 AE3007C series)

- [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 2017-11-05](https://openairdocs.org/ad/2017-11-05): Turbine/ turboprop Engine, Turbine Section · Rolls-Royce AE 3007C and AE 3007C1. Effective Jul 18, 2017
- [AD 2015-02-08](https://openairdocs.org/ad/2015-02-08): Turbine wheels · Rolls-Royce AE 2100D2, AE 2100D2A, AE 2100D3 and 11 more. Effective Mar 11, 2015
- [AD 2009-24-04](https://openairdocs.org/ad/2009-24-04): Fan spinner · Rolls-Royce AE 3007A1, AE 3007A1E, AE 3007A1P and 5 more. Effective Dec 28, 2009
- [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 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 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 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 113: https://openairdocs.org/aircraft/N600BP/ads.md

## Information bulletins (advisory) (9 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 NE-11-22](https://openairdocs.org/saib/NE-11-22): Engine Controls. Issued Feb 23, 2011
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations

None matched to N600BP.

## NTSB investigations on N600BP not matched to an aircraft (1)

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

- [NTSB CHI78FEE30](https://openairdocs.org/ntsb/CHI78FEE30), Apr 24, 1978: N American NA265 (N600BP), West Chicago, IL, substantial damage

## FAA accident and incident reports

None matched to N600BP.

## Reports on N600BP not matched to an aircraft (1)

They name N600BP, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Accident 19780424030059A](https://openairdocs.org/incident/19780424030059A), Apr 24, 1978: Rkwell NA26530 (N600BP), West Chicago, IL, Substantial damage

## Service difficulty reports (126, 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 HNAA2021050300164](https://openairdocs.org/sdr/HNAA2021050300164), Apr 30, 2021: TAT PROBE. MALFUNCTIONED. IN CRUISE TAT 2 INOPERATIVE IN EICAS. NO NOTED INDICATION ISSUES. R & R TAT 2 SENSOR IAW AMM 34 15 03. OPS CHECKED GOOD. R & R RELAY K0494 PER AMM 20 13 02. OPS
- [SDR HNAA2020090900254](https://openairdocs.org/sdr/HNAA2020090900254), Sep 9, 2020: WHEEL. FAILED. ABNORMAL NOISE AND ODOR FROM NOSE WHEEL AREA DURING TAKEOFF ROLL. MAINTENANCE R& R LT AND RT NOSE WHEEL ASSY, I/A/W 32-49-05. OK FOR SERVICE, PCS.
- [SDR HNAA2020080300241](https://openairdocs.org/sdr/HNAA2020080300241), Jul 31, 2020: DUCT. BLOWN. ON TAKE OFF 2 LOUD POPS WERE HEARD IN CABIN BETWEEN RIGHT E-EXIT AND AFT BULKHEAD, FOLLOWED BY A BLEED 1 LEAK ON EICAS. AT 10,000 FT CABIN WAS LOSING PRESSURIZA
- [SDR HNAA2020022600079](https://openairdocs.org/sdr/HNAA2020022600079), Feb 22, 2020: TRIM SYSTEM. INOPERATIVE. PITCH TRIM MAIN INOP. BACK-UP OPS NORMAL.....FIX: TRANSCRIBED TO WORK PACKAGE SEQ 1 DATED 22FEB20. R&RD HSA(HORIZ STAB ACTUATOR) IAW AMM 27-40-02. PERFORMED HSA
- [SDR HNAA2020021700066](https://openairdocs.org/sdr/HNAA2020021700066), Feb 15, 2020: TRIM SYSTEM. MALFUNCTIONED. PDIS 600 27-41 2110041 15FEB20 PHL CLOSE PITCH TRIM MAIN INOP ON EICAS DURING CLIMB WITH AUTO PILOT ENGAGED FACT 15FEB20 14:27 PHL RESET PITCH TRIM 1/ PITCH TRI
- [SDR HNAA2020011700019](https://openairdocs.org/sdr/HNAA2020011700019), Jan 15, 2020: PUMP. LEAKING. HYD SYS 1 FLUID LOSS IN FLIGHT....FIX:FOUND #1ENG DRIVEN HYD PUMP LEAKING OUT DRAIN TUBE. R&RD #1ENG DRIVEN HYD PUMP IAW 29-10-03-000-801-A AND 29-10-03-400-801
- [SDR HNAA2018081300190](https://openairdocs.org/sdr/HNAA2018081300190), Aug 10, 2018: DISPLAY. MALFUNCTIONED. FIRST OFFICER`S ALTITUDE INDICATOR ON THE PFD SHOWED A RED X AND SPEED BUGS ON SPEED TAPE. DISAPPEARED AT VR SELECTED ADC 1 ON THE FIRST OFFICER`S REV PNL, ALL 
- [SDR HNAA2018072000161](https://openairdocs.org/sdr/HNAA2018072000161), Jul 19, 2018: WINDOW. OPEN. CAPT DV WINDOW OPENED IN FLIGHT SHORTLY AFTER TAKEOFF. WINDOW WOULD NOT REMAIN CLOSED WITHOUT ASSISTANCE. INSPECTED CAPTAINS STORM WINDOW TRACK AND SEALS. NO DE
- [SDR HNAA2018052500113](https://openairdocs.org/sdr/HNAA2018052500113), May 10, 2018: UNKNOWN. ODOR. ACRID SMOKE ODOR IN THE FLIGHT DECK AND FORWARD CABIN. NO VISUAL SIGNS OF SMOKE. VISUALLY INSPECTED AVIONICS NOSE BAY AND AROUND WINDSHIELDS, FOUND NO EVIDENCE 
- [SDR HNAA2018041100080](https://openairdocs.org/sdr/HNAA2018041100080), Apr 10, 2018: UNKNOWN. ODOR. PASSENGER REPORTED POSSIBLE ELECTRICAL ODOR IN CABIN. MX UNABLE TO DUPLICATE DISCREPANCY. NO ELECTRICAL ODOR PRESENT IN ACFT AT THIS TIME. NO OBVIOUS DEFECTS NO
- [SDR HNAA2017101600350](https://openairdocs.org/sdr/HNAA2017101600350), Oct 15, 2017: ENGINE. FIRE. GROUND CREW REPORTED A NR 1 ENGINE FIRE AT EXHAUST NOZZLE DURING TAXI. CREW REPORTED THE ENGINE WAS JUST PREVIOUSLY SHUTDOWN AND NO ABNORMAL INDICATIONS OR MESS
- [SDR HNAA2017100200343](https://openairdocs.org/sdr/HNAA2017100200343), Sep 29, 2017: UNKNOWN. UNKNOWN. AT 100 KNOTS DURING TAKE OFF, AIRCRAFT ABRUPTLY YAWED TO THE LEFT. COMPLIED WITH GVI ON NLG AND MLG. NO DEFECTS FOUND. ALL TIRE PRESSURES WERE GOOD. OK FOR SERV
- [SDR HNAA2017090700301](https://openairdocs.org/sdr/HNAA2017090700301), Sep 1, 2017: LIGHT. INOPERATIVE. EMERGENCY LIGHT AT ROW 17 INOPERATIVE. R & R EMERGENCY LIGHT ASSY IAW AMM 33-50-08-000/400-802-A, OPS CHECKED GOOD.
- [SDR HNAA2017082100279](https://openairdocs.org/sdr/HNAA2017082100279), Aug 18, 2017: ENGINE. FIRE. GATE AGENT NOTICED FLAMES AND SMOKE EMINATING FROM THE NR 1 ENGINE WHILE ENGINE WAS SHUTDOWN. INSPECTED AND NO DAMAGE NOTED. GVI ENGINE INLET AND EXIT AND NACEL
- [SDR HNAA2016120900381](https://openairdocs.org/sdr/HNAA2016120900381), Dec 9, 2016: WARNING SYSTEM. FALSE ACTIVATION. HS VLV CAUTION ILLUMINATED AFTER ENGINE START. GROUND RAN BOTH ENGINE. PERFORMED 1 AND 2 ENGINE HSV FUNCTION TEST IN ACCORDANCE WITH MM 36-11-02. OPS CHECKED GO
- [SDR HNAA2016121200387](https://openairdocs.org/sdr/HNAA2016121200387), Dec 8, 2016: VALVE. FAILED. AFTER ENGINE START, HS VALVE 1 FAILED. R & R THE NR 1 HSV AND PRESSURE SWITCH IAW AMM 36-11-02. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR HNAA2016112100354](https://openairdocs.org/sdr/HNAA2016112100354), Nov 21, 2016: WARNING LIGHT. FALSE ACTIVATION. DURING TAKEOFF, EICAS CAUTION MESSAGE HS VALVE ILLUMINATED, NR 1 ENGINE N2 WAS ABOVE 80%. MESSAGE EXTINGUISHED AFTER REJECTED TAKEOFF AND THRUST LEVERS AT IDLE.
- [SDR HNAA2016101400318](https://openairdocs.org/sdr/HNAA2016101400318), Oct 14, 2016: WARNING LIGHT. FALSE ACTIVATION. DURING ICE PROTECTION TEST IN FLIGHT, STAB ANTI-ICE FAILED APPEARS ON EICAS. TROUBLESHOT IAW FIM 30-12-00-810-805-A. PERFORMED OPS CHECKED ON ANTI-ICE SYSTEM IA
- [SDR SIMA20160725005](https://openairdocs.org/sdr/SIMA20160725005), Jul 25, 2016: VALVE. CORRODED. TOILET WASTE VALVE SUPPORT BUCKET IS CORRODED. REMOVED AND REPLACED TOILET WASTE VALVE SUPPORT BUCKET IAW SRM 51-40-02
- [SDR SIMA20160720006](https://openairdocs.org/sdr/SIMA20160720006), Jul 20, 2016: WIRE. BROKEN. NR 1 EMERGENCY LIGHT HAS A BROKEN WIRE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP IAW AMM 33-50-12.
- [SDR SIMA20160720004](https://openairdocs.org/sdr/SIMA20160720004), Jul 20, 2016: FLOOR SUPPORT. CRACKED. LEFT OMEGA BEAM IS CRACKED AT NUTPLATE HOLE ABOVE FRAME 69. REPAIRED THE OMEGA BEAM IAW ERS-EM-53MR-2199
- [SDR SIMA20160720007](https://openairdocs.org/sdr/SIMA20160720007), Jul 20, 2016: WIRE. BROKEN. LEFT NR 1 EMERGENCY LIGHT CONNECTION BROKEN. REPAIRED THE WIRE IAW SWPM 20-50-00
- [SDR SIMA20160720005](https://openairdocs.org/sdr/SIMA20160720005), Jul 20, 2016: SKIN. DAMAGED. RUDDER LOWER RT SIDE TRAILING EDGE SKIN HAS A BLEND-OUT AREA. ACCOMPLISHED PERMANENT REPAIR OF THE RUDDER IAW ERS-EM-55MR-441
- [SDR SIMA20160712002](https://openairdocs.org/sdr/SIMA20160712002), Jul 12, 2016: FRAME. CORRODED. FRAME 65 IS CORRODED BELOW CARGO DOOR GUIDE PLATE. REMOVED AND REPLACED THE FRAME IAW SRM 51-40-02.
- [SDR SIMA20160417002](https://openairdocs.org/sdr/SIMA20160417002), Apr 17, 2016: INVERTER. INOPERATIVE. THREE AFT EMER FLOOR LIGHT STRIPS INOPERATIVE. R & R NR 6 EMER LIGHT DC & AC INVERTER. OPERATIONS CHECKED GOOD FOR ALL EMER FLOOR LIGHT STRIPS IAW AMM 33-50-11.
- [SDR SIMA20160414005](https://openairdocs.org/sdr/SIMA20160414005), Apr 14, 2016: LIGHT. INOPERATIVE. EMERGENCY FLOOR PROXIMITY LIGHT STRIP, FOURTH FROM FRONT INOPERATIVE. DEFERRED IAW MEL 33-30. R & R EMER FLOOR PROXIMITY LIGHT STRIP, 4TH FROM FRONT IAW AMM 33-
- [SDR SIMA20160401003](https://openairdocs.org/sdr/SIMA20160401003), Apr 1, 2016: TRANSDUCER. FAILED. ABORTED TAKEOFF AT 80KTS. BRAKE DEGRADED MSG & AT THE SAME TIME ACFT SWERVED TO THE LEFT. R & R NR 4 WHEEL SPEED TRANSDUCER IAW AMM 32-41-03. PERFORMED FUNCTION
- [SDR SIMA20160215002](https://openairdocs.org/sdr/SIMA20160215002), Feb 15, 2016: DOOR. LACK OF LUBE. FLIGHT ATTENDANTS REPORTS THE MAIN CABIN DOOR NOT OPEN OR CLOSE EASILY. CLEANED & LUBRICATED MAIN DOOR IAW AMM 52-18-00. OPERATIONS CHECKED GOOD AT THIS TIME.
- [SDR SIMA20160120007](https://openairdocs.org/sdr/SIMA20160120007), Jan 20, 2016: STRUCTURE. CRACKED. CRACK AT RIVET BELOW ACCESS PANEL 113AZ. MARKED WITH MX INFO TAG. PERFORMED PERMANENT REPAIR TO CRACK AT RIVET BELOW ACCESS PANEL 114AZ IAW ERS-EM-53MR-1880.
- [SDR SIMA20160120006](https://openairdocs.org/sdr/SIMA20160120006), Jan 20, 2016: STRUCTURE. CRACKED. CRACK AT RIVET BELOW ACCESS PANEL 114AZ. MARKED WITH MX INFO TAG. PERFORMED PERMANENT REPAIR TO CRACK AT RIVET BELOW ACCESS PANEL 114AZ IAW ERS-EM-53MR-1880.
- [SDR SIMA20160120005](https://openairdocs.org/sdr/SIMA20160120005), Jan 20, 2016: UPLOCK. FAILED. UNUSUAL THUMPING NOISE COMING FROM UNDERNEATH COCKPIT AREA. HAPPENED ON TWO SEPARATE TIMES WITH VIBRATION FELT BY BOTH PILOTS. REMOVED AND REPLACED NLG UPLOCK B
- [SDR SIMA20160107002](https://openairdocs.org/sdr/SIMA20160107002), Jan 7, 2016: INVERTER. INOPERATIVE. FOUND FLOOR STRIPS NR 2 AT NR 3 NOT WORKING. R & R NR 3 INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.
- [SDR SIMA20151225003](https://openairdocs.org/sdr/SIMA20151225003), Dec 25, 2015: REGULATOR VALVE. FAILED. ANTI-ICE FAIL FOLLOWED BY ANTI-ICE COND. ANTI-ICE INOPERATIVE, BUT ALL VLVS INDICATED OPEN. MSG CLEARED & SYS WORKED MANUALLY WITHOUT FURTHER ISSUES. TRANSFERRE
- [SDR SIMA20151103002](https://openairdocs.org/sdr/SIMA20151103002), Nov 3, 2015: UNKNOWN. ODOR. STRONG ELEC BURNING ODOR THROUGHOUT ACFT, WHILE TAXING UP TO GATE. PERFORMED GVI OF ALL AVIONICS COMPARTMENTS, GVI OF MAIN CABIN AREA, GVI OF MAIN CABIN LIGHTS,
- [SDR SIMA20151001002](https://openairdocs.org/sdr/SIMA20151001002), Oct 1, 2015: FLASHLIGHT. INOPERATIVE. CAPTAINS FLASH LIGHT QUIT WORKING. R & R CAPTAINS FLASH LIGHT ASSEMBLY IAW AMM 25-60-00. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150915001](https://openairdocs.org/sdr/SIMA20150915001), Sep 15, 2015: LIGHT. INOPERATIVE. RIGHT FWD OVERWING EMER LIGHT INOPERATIVE. R & R RT FWD OVERWING EMER LIGHT LAMP. OPERATIONS CHECKED GOOD IAW AMM 33-50-10.
- [SDR SIMA20150822001](https://openairdocs.org/sdr/SIMA20150822001), Aug 23, 2015: RADIO ALTIMETER. FAILED. ON CLIMB OUT RA SHOWED 25 FT GREEN WITH MIN BOX SHOWING & GND INDICATION UNDER ALTITUDE. NUMEROUS AURAL WARNINGS & MASTER CAUTIONS INCLUDING BANK ANGLE, PULL UP
- [SDR SIMA20150819004](https://openairdocs.org/sdr/SIMA20150819004), Aug 19, 2015: LIGHT. INOPERATIVE. RIGHT FWD EMER WING LIGHT INOPERATIVE. R & R FWD WING EMER LIGHT IAW AMM 33-50-07.
- [SDR SIMA20150330002](https://openairdocs.org/sdr/SIMA20150330002), Mar 30, 2015: MECHANISM. LACK OF LUBE. MAIN CABIN DOOR EXCEPTIONALLY DIFFICULT TO OPEN & CLOSE. LUBRICATED ACTUATING & LOCKING MECHANISM ON MAIN CABIN DOOR IAW AMM 52-18-00. OPENING & CLOSING GOOD IA
- [SDR SIMA20150319004](https://openairdocs.org/sdr/SIMA20150319004), Mar 19, 2015: DOOR. SCRATCHED. PASSENGER DOOR SCRATCHED & GOUGED ON LOWER TE. TRANSFERRED TO AML PAGE 3740390 ITEM 1. SATISFACTORILY ACCOMPLISHED ERS-EM-52MR-308.
- [SDR SIMA20141221003](https://openairdocs.org/sdr/SIMA20141221003), Dec 21, 2014: ENGINE. POWER LOSS. NUMBER 2 ENG UNABLE TO PRODUCE COMMANDED THRUST IN DETENT DURING CRUISE & NR 2 N1 ABOUT 1% BELOW COMMANDED THRUST. NR 2 ITT WAS ON BORDER OF AMBER A FEW TIMES. 
- [SDR SIMA20141117004](https://openairdocs.org/sdr/SIMA20141117004), Nov 17, 2014: LIGHT. INOPERATIVE. SERVICE DOOR EMER LIGHT INOPERATIVE. R & R SERVICE DOOR EXTERNAL EMER LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A. OPERATIONS CHECKED GOOD. CHARG
- [SDR SIMA20141013002](https://openairdocs.org/sdr/SIMA20141013002), Oct 13, 2014: RIB. CHAFED. LEFT WING AILERON PCA HYDRAULIC LINES CHAFING INTERNAL RIBS OF WING. COMPLIED WITH REPAIR OF LT WING RIB 21 IAW ERS-EM-57MR-260.
- [SDR SIMA20141009002](https://openairdocs.org/sdr/SIMA20141009002), Oct 9, 2014: RIB. GOUGED. LEFT WING RIB 21 GOUGED. COMPLIED WITH LT WING RIB 21 REPAIR IAW ERS-EM-57MR-260.
- [SDR SIMA20141008012](https://openairdocs.org/sdr/SIMA20141008012), Oct 8, 2014: RIB. CRACKED. RIGHT AFT MLG RIB THAT ATTACHES THE BELLY FAIRING IS CRACKED LOWER OTBD CORNER. R & R RT AFT MLG RIB THAT ATTACHES THE BELLY FAIRING IAW SRM 51-40-02.
- [SDR SIMA20141008010](https://openairdocs.org/sdr/SIMA20141008010), Oct 8, 2014: GUSSET. CRACKED. GALLEY FLOOR GUSSET HAS A CRACK AT FRAME 18. INSTALLED NEW GALLEY FLOOR GUSSET IAW SRM 51-40-02.
- [SDR SIMA20141005008](https://openairdocs.org/sdr/SIMA20141005008), Oct 5, 2014: SUPPORT BRACKET. CRACKED. FOUND SUPPORT BRACKET FOR THE BLEED AIR DUCT, JUST AFT OF APU CHECK VLV IN THE AFT AVIONICS TO BE CRACKED. R & R RT AFT MLG RIB THAT ATTACHES THE BELLY FAIRING 
- [SDR SIMA20141001008](https://openairdocs.org/sdr/SIMA20141001008), Oct 1, 2014: SUPPORT. CRACKED. LEFT OVERWING PANEL SUPPORT FLANGE IS CRACKED AT FRAME 48. REPAIRED LT OVERWING PANEL SUPPORT FLANGE AT FRAME 48 IAW SRM 53-23-12.
- [SDR SIMA20141001007](https://openairdocs.org/sdr/SIMA20141001007), Oct 1, 2014: BRACKET. CRACKED. RIGHT OVERWING PANEL SUPPORT FLANGE HAS A CRACKED BRACKET AT FRAME 48. R & R RT OVERWING SUPPORT FLANGE BRACKET IAW SRM CH 51-40-02.
- [SDR SIMA20141001006](https://openairdocs.org/sdr/SIMA20141001006), Oct 1, 2014: SUPPORT ANGLE. CRACKED. SUPPORT ANGLE CRACKED, AFT OF THE RT MLG WELL FOR THE AFT BELLY FAIRING. R & R BRACKET IAW SRM CH 51-40-02.

All 126: https://openairdocs.org/aircraft/N600BP/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/N600BP/stcs.md

## Related

- Other Embraer EMB-145LR aircraft: https://openairdocs.org/model/embraer-emb-145lr/aircraft.md
- The Allison AE3007C series engine: https://openairdocs.org/engine/allison-ae3007c-series.md

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