# N856AE: 2003 Embraer EMB-135KL

- Status: Valid registration
- Airframe: [Embraer EMB-135KL](https://openairdocs.org/model/embraer-emb-135kl) (registry code 3260302, 37 seats)
- Engine: [Allison AE-3007A1/3](https://openairdocs.org/engine/allison-ae-3007a1-3) (registry code 03036)
- 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: 145748
- Year built: 2003
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 28, 2003
- Certificate issued: July 10, 2025
- Expires: July 31, 2032
- Mode S code: ABBDA7
- Registered owner: [Avi Sales & Leasing Services LLC](https://openairdocs.org/faa-owner/AVI%20SALES%20%26%20LEASING%20SERVICES%20LLC)
- Location: [Muskegon, MI](https://openairdocs.org/faa-place/MI/Muskegon)
- Owner type: LLC
- Owner's area on the map: 43.1800° N, 86.2868° W: Placed by OpenAirDocs at the center of ZIP code 49441, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=856AE
- Page: https://openairdocs.org/aircraft/N856AE

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): 81 in force

### Matched by airframe (Embraer EMB-135KL)

- [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 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 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 2007-04-09](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
- [AD 2004-25-21](https://openairdocs.org/ad/2004-25-21): Pitch trim system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 26, 2005
- [AD 2004-25-12](https://openairdocs.org/ad/2004-25-12): Passenger service unit (PSU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 13, 2005
- [AD 2004-24-03](https://openairdocs.org/ad/2004-24-03): Internal o-ring seal · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 23 more. Effective Jan 3, 2005

### Matched by engine (Allison AE-3007A1/3)

- [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 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 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 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 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 2003-25-08](https://openairdocs.org/ad/2003-25-08): 1st and 2nd stage turbine spacers · Rolls-Royce AE 3007A1, AE 3007A1E, AE 3007A1P and 3 more. Effective Jan 21, 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 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 2006-04-02](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 2003-09-03](https://openairdocs.org/ad/2003-09-03) (historical): Cartridge flange · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 3 more. Effective May 14, 2003
- [AD 2002-16-06](https://openairdocs.org/ad/2002-16-06) (historical): Auxiliary power unit (APU) · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135KE, EMB-135KL and 2 more. Effective Aug 27, 2002
- [AD 2002-08-21](https://openairdocs.org/ad/2002-08-21) (historical): Bonding Jumpers that Connect the Horizontal Stabilizer to the Vertical Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135KE, EMB-135KL and 2 more. Effective May 16, 2002
- [AD 2002-08-18](https://openairdocs.org/ad/2002-08-18) (historical): Actuator Clutches of the Primary and Backup Pitch Trim Systems of the Horizontal Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135KE, EMB-135KL and 2 more. Effective May 16, 2002
- [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 2008-19-51](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 96: https://openairdocs.org/aircraft/N856AE/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 N856AE.

## FAA accident and incident reports (1)

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 20140728011679I](https://openairdocs.org/incident/20140728011679I), Jul 28, 2014: Embraer EMB-135KL (N856AE), Champaign, IL, No damage. Smoke in cabin and lav. Lav smoke indicator on eicas. Declared emergency and returned cmi.

## Service difficulty reports (96, 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 SIMA20190919002](https://openairdocs.org/sdr/SIMA20190919002), Sep 19, 2019: COVER. BROKEN. LT #1 EMERGENCY LIGHT FLOOR STRIP PANEL COVER BROKEN. C/A-REPLACED THE NR 1 EMERGENCY LIGHT FLOOR STRIP PANEL AFTER INSTALLING FLOOR PANEL 231GF IAW AMM 33-50-1
- [SDR SIMA201904011007](https://openairdocs.org/sdr/SIMA201904011007), Mar 29, 2019: UNKNOWN. ODOR. APU FAIL MESSAGE, STRONG ODOR OF FUEL. REMOVED AND REPLACED APU IGNITOR PLUGS IAW AMM 49-44-03. OPC FAILED IAW AMM 49-13-00-02. FURTHER T/S REQUIRED. MEL REMAIN
- [SDR SIMA2019021109001](https://openairdocs.org/sdr/SIMA2019021109001), Feb 9, 2019: CONNECTOR. LOOSE. IN FLIGHT AT 10000 FEET 290 KIAS. CA & FO HEARD BANGING SOUND 5 TIMES. SOUNDED LIKE NOSE GEAR UNCOMMANDED EXTENSION, TRIED TO BANG THROUGH NOSE DOORS UNCOMMANDE
- [SDR SIMA20190112003](https://openairdocs.org/sdr/SIMA20190112003), Jan 12, 2019: LIGHT. INOPERATIVE. FLOOR PROXIMITY STRIP LIGHT INOP. C/A-REMOVED AND REPLACED THE FLOOR PROXIMITY STRIP LIGHT IAW AMM 33-50-12.
- [SDR SIMA201812031001](https://openairdocs.org/sdr/SIMA201812031001), Dec 1, 2018: UPLOCK. FAULTED. LOUD THUMPING NOISE COMING FROM NOSE SECTION OF AIRCRAFT UNDERNIETH MAYBE IN THE NOSE CONE RADOM. GEAR WAS UP IN THE GEAR WELL."TRANSFERRED TO NRWC 856-LGA-0325
- [SDR SIMA20181008002](https://openairdocs.org/sdr/SIMA20181008002), Oct 8, 2018: ROLLER. LACK OF LUBE. MAIN CABIN DOOR HARD TO OPEN AND CLOSE. -C/A-CLEANED & LUBRICATED MAIN DOOR ROLLER & CHECK OK IAW MM 52-18-00.
- [SDR SIMA2018100130004](https://openairdocs.org/sdr/SIMA2018100130004), Sep 30, 2018: LIGHT. INOPERATIVE. FOUND MAIN-DOOR EMERGENCY LIGHT TO BE INOP DURING PS-1 CHECK-C/A-REMOVED AND REPLACED MAIN-DOOR EMERGENCY LIGHT LAMP IAW AMM TASK 33-50-06. OPS CHECK GOOD
- [SDR SIMA2018082017001](https://openairdocs.org/sdr/SIMA2018082017001), Aug 17, 2018: LIGHT. INOPERATIVE. GREEN LIGHT FLOOR EMERGENCY PROXIMITY STRIP FAILS TO ILLUMINATE NEXT TO SEAT 2A AND 3A.-C/A-EMERGENCY FLOOR PROX STRIP AT 2A AND 3A DEFERRED PER MEL 33-30.
- [SDR SIMA2018072320003](https://openairdocs.org/sdr/SIMA2018072320003), Jul 20, 2018: CRADLE. CRACKED. FA FORWARD HANDSET CRACKED. R&R AFT F/A CRADLE IAW AMM 23-31-03, OPS CHECK GOOD.
- [SDR SIMA2018072320005](https://openairdocs.org/sdr/SIMA2018072320005), Jul 20, 2018: HANDSET. CRACKED. FA FORWARD HANDSET CRACKED. SWAPPED FORWARD WITH AFT, AFT FA HANDSET ON MEL. M PROCEDURES C/W.
- [SDR SIMA20180314007](https://openairdocs.org/sdr/SIMA20180314007), Mar 14, 2018: STRUT. LOW. RTF LDG GEAR DISAGREE. AFTER ROTATION DURING GEAR RETRACTION, LG/LVR DISAGREE MESSAGE ON EICAS FOLLOWED SHORTLY BY ENG 1-2 REV DISAGREE. GEAR SHOWED 3 WHITE UP 
- [SDR SIMA20171113001](https://openairdocs.org/sdr/SIMA20171113001), Nov 13, 2017: ENGINE. ODOR. MUSTY ODOR AFTER TL TO THRUST SET POSITION ON TAKEOFF ROLL. AT 500 FT HAD A LAVATORY SMOKE WARNING MESSAGE. FA REPORTED SMOKE IN CABIN, RETURNED FOR LANDING. FA
- [SDR SIMA20171112003](https://openairdocs.org/sdr/SIMA20171112003), Nov 12, 2017: ACM. FAILED. RECEIVED "LAV SMOKE" INDICATION AT APPROXIMATELY 800 AFL IN CLIMB THERE WAS A SMOKE SMELL IN CABIN NORMAL LANDING NOT OVERWEIGHT. "TRANSFERRED TO NRWC 856-DFW-0
- [SDR SIMA20171018001](https://openairdocs.org/sdr/SIMA20171018001), Oct 18, 2017: BALLAST. FAILED. CLIMBING THROUGHT 8000 FT, AFTER TAKE OFF, RECEIVED A LAVATORY SMOKE EICAS WARNING. F/A DID NOT SEE SMOKE BUT SMELLED UNUSUAL FUMES. RETURNED TO DEPARTURE. SMEL
- [SDR SIMA20170906002](https://openairdocs.org/sdr/SIMA20170906002), Sep 6, 2017: BEAM. DAMAGED. PREVIOUS REPAIR FWD OF FR 61 ON LAVATORY CENTER BEAM ELONGATED HOLE DAMAGED. PERFORMED A REPAIR IAW ERS-EM-53MR-2868.
- [SDR SIMA20170831002](https://openairdocs.org/sdr/SIMA20170831002), Aug 31, 2017: FRAME. CRACKED. FRAME 23 CRACKED AT RIVET HOLE BETWEEN STRINGERS 15 - 16R. REPAIRED THE FRAME IAW SRM 53-00-04, ITEM 3, FIG 201.
- [SDR SIMA20170508007](https://openairdocs.org/sdr/SIMA20170508007), May 8, 2017: LIGHT. DAMAGED. NR 6 EMERGENCY LIGHT STRIP DAMAGED ON THE END. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.
- [SDR SIMA20170508003](https://openairdocs.org/sdr/SIMA20170508003), May 8, 2017: LIGHT. DAMAGED. NR 5 LT EMERGENCY LIGHT STRIP DAMAGED AT THE WIRE HOLE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.
- [SDR SIMA20170508004](https://openairdocs.org/sdr/SIMA20170508004), May 8, 2017: LIGHT. DAMAGED. NR 2 LT EMERGENCY LIGHT STRIP DAMAGED AT THE WIRE HOLE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-12.
- [SDR SIMA20170508006](https://openairdocs.org/sdr/SIMA20170508006), May 8, 2017: STRUCTURE. GOUGED. AFT EDGE OF PAX DOOR LOWER AREA IS GOUGED. REPAIRED IAW ERS-EM-52MR-797.
- [SDR SIMA20170410001](https://openairdocs.org/sdr/SIMA20170410001), Apr 10, 2017: DOOR. LACK OF LUBE. FA REPORTED THE MAIN DOOR DIFFICULT TO OPEN, FEELS LIKE THE HANDLE IS CATCHING OR HAS MORE RESISTANCE TO OPEN THAN USUAL. CLEANED AND LUBED MAIN CABIN DOOR IAW 
- [SDR SIMA20170324001](https://openairdocs.org/sdr/SIMA20170324001), Mar 24, 2017: AUTOPILOT SYS. MALFUNCTIONED. AUTOPILOT FAILED DURING GO AROUND, WITH UP & DOWN DRAFT OVERSPEED INDICATION FOR ABOUT 3 MINUTES. PERFORMED A PHASE I INSPECTION IAW AMM 05-50-04, SUB TASK 212-
- [SDR SIMA20161231001](https://openairdocs.org/sdr/SIMA20161231001), Dec 31, 2016: CRADLE. BROKEN. AFT CABIN FLASHLIGHT CRADLE IS BROKEN. REMOVED AND REPLACED THE CRADLE IAW AMM 33-50-16.
- [SDR SIMA20161120002](https://openairdocs.org/sdr/SIMA20161120002), Nov 20, 2016: PANEL. INOPERATIVE. PASSENGER DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LIGHT PANEL ASSY, IAW AMM 25-23-04. OPS CHECKED GOOD.
- [SDR SIMA20160530002](https://openairdocs.org/sdr/SIMA20160530002), May 30, 2016: LIGHT. INOPERATIVE. MAIN CABIN DOOR EMER LIGHT INOPERATIVE. R & R LAMP IN MAIN DOOR EMER LIGHT IAW AMM 33-50-06. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.
- [SDR SIMA20151221001](https://openairdocs.org/sdr/SIMA20151221001), Dec 21, 2015: FLASHLIGHT ASSY. BROKEN. WHILE TROUBLESHOOTING FLASHLIGHT PIREP, FOUND CAPTAIN'S FLASHLIGHT CRADLE BROKEN. R & R HOLDER IAW AMM 33-50-16.
- [SDR SIMA20151221002](https://openairdocs.org/sdr/SIMA20151221002), Dec 21, 2015: LAMP. INOPERATIVE. CAPTAINS FLASHLIGHT WILL NOT CHARGE. TRIED 2 DIFFERENT HOLDERS. FOUND FLASHLIGHT BULB ASSEMBLY DAMAGED. R & R LAMP ASSEMBLY IAW CMM 25-60-02. OPERATIONS CHECKED
- [SDR SIMA20151122001](https://openairdocs.org/sdr/SIMA20151122001), Nov 22, 2015: UNKNOWN. SMOKE. AFTER TAKEOFF SMOKE IN THE CABIN, FOLLOWED BY LAVATORY SMOKE EICAS WARNING. COMPLIED WITH ETN EM 72-034 & FIRST STEPS OF ENG GROUP WORK SCOPE. ALTHOUGH INITIAL 
- [SDR SIMA20150609004](https://openairdocs.org/sdr/SIMA20150609004), Jun 9, 2015: LAMP. INOPERATIVE. DURING PS 2 CHECK, FOUND MAIN PAX DOOR EMERGENCY LIGHT INOPERATIVE. R & R THE LAMP IAW MM 33-50-10. OPS CHECKED GOOD.
- [SDR SIMA20150531002](https://openairdocs.org/sdr/SIMA20150531002), May 31, 2015: HOLDER. BROKEN. FLIGHT ATTENDANT FLASHLIGHT HOLDER BROKEN. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16.
- [SDR SIMA20150307001](https://openairdocs.org/sdr/SIMA20150307001), Mar 7, 2015: PROXIMITY SENSOR. FAILED. IMMEDIATELY AFTER ROTATION RECEIVED A LG AIR & GND FAIL CAUTION MSG & COULD NOT RAISE THE LG, MSG EXTINGUISHED UPON TOUCHDOWN. R & R NOSE GEAR WEIGHT ON WHEELS 
- [SDR SIMA20150210006](https://openairdocs.org/sdr/SIMA20150210006), Feb 10, 2015: LIGHT. INOPERATIVE. COCKPIT OVERHEAD EMER LIGHT INOPERATIVE. R & R COCKPIT OVERHEAD EMER LIGHT LAMP IAW AMM 33-50-05-000-801-A & 33-50-05-400-801-A. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150128013](https://openairdocs.org/sdr/SIMA20150128013), Jan 28, 2015: FIREWALL. CRACKED. APU FIRE WALL IS CRACKED AT THE LOWER LT MOUNT AREA, THE UPPER LT MOUNT & THE LOWER RT MOUNT AREA. 3 CRACKS TOTAL APPROX 4.5 INCHES IN LENGTH. COMPLIED WITH PAR
- [SDR SIMA20150128012](https://openairdocs.org/sdr/SIMA20150128012), Jan 28, 2015: SUPPORT BRACKET. CRACKED. FUEL PIPE SUPPORT BRACKET AT RT WING RIB 3 BENEATH 631AB IS CRACKED. REMOVED & INSTALLED NEW FUEL PIPE SUPPORT BRACKET IAW AMM 20-10-01.
- [SDR SIMA20150128011](https://openairdocs.org/sdr/SIMA20150128011), Jan 28, 2015: SUPPORT BRACKET. CRACKED. FUEL PIPE SUPPORT BRACKET AT LT WING RIB 3 BENEATH 531AB IS CRACKED. R & R FUEL PIPE SUPPORT BRACKET AT LT WING RIB 3 BENEATH PANEL 531AB IAW AMM 20-10-01.
- [SDR SIMA20150128010](https://openairdocs.org/sdr/SIMA20150128010), Jan 28, 2015: WEB. CRACKED. LEFT MLG AFT GEAR WELL WEB HAS A 1 INCH LONG CRACK. R & R LT MLG AFT GEAR WELL WEB IAW SRM 51-40-02.
- [SDR SIMA20150128006](https://openairdocs.org/sdr/SIMA20150128006), Jan 28, 2015: SUPPORT BRACKET. CRACKED. FUEL PIPE SUPPORT BRACKET AT RT WING BENEATH 631AB IS CRACKED. REMOVED & INSTALLED NEW FUEL PIPE SUPPORT BRACKET IAW AMM 20-10-01.
- [SDR SIMA20150128002](https://openairdocs.org/sdr/SIMA20150128002), Jan 28, 2015: FITTING. CRACKED. CLIP ON THE AFT EDGE OF THE SERVICE DOOR SILL OTBD FLOOR SUPPORT HAS 1/8 INCH CRACK. INSTALLED NEW CLIP ON THE AFT EDGE OF THE SERVICE DOOR SILL IAW SRM 51-40-0
- [SDR SIMA20150128003](https://openairdocs.org/sdr/SIMA20150128003), Jan 28, 2015: ATTACH BRACKET. CRACKED. LEFT ENG PYLON FWD PRE-COOLER ATTACHMENT BRACKET IS CRACKED. R & R LT ENG FWD PRE-COOLER ATTACH BRACKET ETN EM-54-056.
- [SDR SIMA20150128004](https://openairdocs.org/sdr/SIMA20150128004), Jan 28, 2015: SKIN. CRACKED. RIGHT ENG TR LOWER DOOR SKIN HAS A CRACK AROUND A RIVET AT THE OTBD CORNER. REPAIRED IAW SRM 54-30-01 FIGURE 207.
- [SDR SIMA20150128001](https://openairdocs.org/sdr/SIMA20150128001), Jan 28, 2015: ATTACH BRACKET. CRACKED. RIGHT ENG PYLON FWD PRE-COOLER ATTACHMENT BRACKET IS CRACKED. REPLACED PRE-COOLER ATTACH BRACKET IAW SRM 51-40-02.
- [SDR SIMA20150128007](https://openairdocs.org/sdr/SIMA20150128007), Jan 28, 2015: SUPPORT BRACKET. CRACKED. FUEL PIPE SUPPORT BRACKET AT LT WING RIB 3 BENEATH 531AB IS CRACKED. R & R FUEL PIPE SUPPORT BRACKET AT LT WING RIB 3 BENEATH 531AB IAW AMM 20-10-01.
- [SDR SIMA20150125002](https://openairdocs.org/sdr/SIMA20150125002), Jan 25, 2015: BUSHING. LOOSE. LEFT AILERON OTBD ACTUATOR ATTACHMENT LUG HAS BOTH HAT BUSHINGS LOOSE OR MIGRATING. LT AILERON OTBD HAT BUSHING ON THE DAMPER FITTING IS LOOSE IN THE FITTING BO
- [SDR SIMA20150121005](https://openairdocs.org/sdr/SIMA20150121005), Jan 21, 2015: SUPPORT ANGLE. CRACKED. RIGHT VERTICAL STAB TO FUSELAGE SUPPORT ANGLE IS CRACKED IN 2 AREAS NEAR FRAME 76 RT. REPLACED RT VERTICAL STAB TO FUSELAGE FWD SUPPORT ANGLE IAW EO EM-53MR-128
- [SDR SIMA20150121009](https://openairdocs.org/sdr/SIMA20150121009), Jan 21, 2015: ATTACH ANGLE. CRACKED. RIGHT LOWER ATTACHMENT ANGLE NR 2 IS CRACKED ON THE LE APPROX 3/8 INCHES LONG. FOR THE LATERAL WING TO FUSELAGE FAIRING. R & R RT LOWER ATTACHMENT ANGLE NR 2 IA
- [SDR SIMA20150121008](https://openairdocs.org/sdr/SIMA20150121008), Jan 21, 2015: ATTACH ANGLE. CRACKED. RIGHT LOWER ATTACHMENT ANGLE NR 3 IS CRACKED ON THE LE APPROX 1/2 INCH LONG. FOR THE LATERAL WING TO FUSELAGE FAIRING. R & R RT LOWER ATTACHMENT ANGLE NR 3 IAW 
- [SDR SIMA20150121007](https://openairdocs.org/sdr/SIMA20150121007), Jan 21, 2015: ATTACH ANGLE. CRACKED. LEFT LOWER ATTACHMENT ANGLE NR 1 IS CRACKED ON THE LE APPROX 2 INCHES LONG. FOR THE LATERAL WING TO FUSELAGE FAIRING. REPLACED DAMAGED LT LOWER ATTACHMENT ANGLE
- [SDR SIMA20150121010](https://openairdocs.org/sdr/SIMA20150121010), Jan 21, 2015: ATTACH ANGLE. CRACKED. LEFT LOWER ATTACHMENT ANGLE NR 2 IS CRACKED ON THE LE APPROX 1 INCH LONG. FOR THE LATERAL WING TO FUSELAGE FAIRING. R & R LT LOWER ATTACHMENT ANGLE NR 2 FOR THE
- [SDR SIMA20150121006](https://openairdocs.org/sdr/SIMA20150121006), Jan 21, 2015: ATTACH ANGLE. CRACKED. LEFT UPPER ATTACHMENT ANGLE IS CRACKED 1/2 INCH BY A RIVET BETWEEN FRAMES 48 - 49. FOR THE LATERAL WING TO FUSELAGE FAIRING. R & R LT UPPER ATTACHMENT ANGLE BET
- [SDR SIMA20150121004](https://openairdocs.org/sdr/SIMA20150121004), Jan 21, 2015: FRAME. CRACKED. FRAME 23 IS CRACKED AT STRINGER 15R. COMPLETED REPAIR IAW E0-EM-53MR-1808.

All 96: https://openairdocs.org/aircraft/N856AE/reports.md

## STCs that may be installed (OpenAirDocs) (55, 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-135KL)

- [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 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 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 ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [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 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 ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [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 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 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 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
- [STC ST04282AT](https://openairdocs.org/stc/ST04282AT): Installation of the Honeywell DU-875 LCD Flight Display. Chippewa Aerospace Inc
- [STC ST04015AT](https://openairdocs.org/stc/ST04015AT): Installation of the Honeywell NZ-2000 FMS/GPS System with or without WAAS/LPV. Chippewa Aerospace Inc
- [STC ST04191AT](https://openairdocs.org/stc/ST04191AT): Installation of the Honeywell Sky Connect Tracker Iridium Satcom System. Chippewa Aerospace Inc
- [STC ST02524LA](https://openairdocs.org/stc/ST02524LA): Installation of TCAS version 7.0. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST03483AT](https://openairdocs.org/stc/ST03483AT): Installation of a Portable Beverage Dispensing System, P/N B43-FA-001. Dynamo Beverage Company, USA, L.L.C
- [STC ST03999AT](https://openairdocs.org/stc/ST03999AT): Installation of a Single Honeywell HF-1050 HF Communication System. Chippewa Aerospace Inc
- [STC ST01619CH](https://openairdocs.org/stc/ST01619CH): Installation of a Lavatory Service Shutoff Valve. AeroControlex Group TransDigm Inc
- [STC ST03994AT](https://openairdocs.org/stc/ST03994AT): Installation of Bleed Air Coupling Sleeve Kit. Seal Dynamics
- [STC ST02638AT](https://openairdocs.org/stc/ST02638AT): Installation of an improved aircraft toilet rinse/fill shutoff valve and asociated hardware. Parker Hannifin Corporation, Parker Aerospace
- [STC ST03890AT](https://openairdocs.org/stc/ST03890AT): Installation of an L-3 Communications Micro Quick Access Recorder (MQAR). Chippewa Aerospace, Inc
- [STC ST02882CH-D](https://openairdocs.org/stc/ST02882CH-D): Installation of a Honeywell Flight Management System (FMS #2). Standard Aero
- [STC ST02803CH-D](https://openairdocs.org/stc/ST02803CH-D): Installation of a Honeywell KHF-1050 system. Standard Aero
- [STC ST01008LA-D](https://openairdocs.org/stc/ST01008LA-D): Installation of Hollingsead International Sentry One Cabin Mounted Video Camera System. Audio International

All 55: https://openairdocs.org/aircraft/N856AE/stcs.md

## Related

- Other Embraer EMB-135KL aircraft: https://openairdocs.org/model/embraer-emb-135kl/aircraft.md
- The Allison AE-3007A1/3 engine: https://openairdocs.org/engine/allison-ae-3007a1-3.md

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