# N822AE: 2002 Embraer EMB-135KL

- Status: Valid registration
- Airframe: [Embraer EMB-135KL](https://openairdocs.org/model/embraer-emb-135kl) (registry code 3260302, 37 seats)
- Engine: [Rolls-Royce AE3007 series](https://openairdocs.org/engine/rolls-royce-ae3007-series) (registry code 54582)
- 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: 145581
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 17, 2002
- Certificate issued: February 23, 2024
- Expires: February 28, 2031
- Mode S code: AB384E
- Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, 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=822AE
- Page: https://openairdocs.org/aircraft/N822AE

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 Rolls-Royce AE3007 model are included.

## ADs that may apply (OpenAirDocs): 87 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 (Rolls-Royce AE3007 series)

- [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 2018-17-04](https://openairdocs.org/ad/2018-17-04): Turbine section · Rolls-Royce AE 2100D2A, AE 2100D3 and AE 3007A2. Effective Sep 21, 2018
- [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 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 2009-04-03](https://openairdocs.org/ad/2009-04-03): 2nd stage, 3rd stage, and 4th stage compressor wheels · Rolls-Royce AE 1107C and AE 3007A1E. Effective Mar 24, 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 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 2006-04-02](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 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 104: https://openairdocs.org/aircraft/N822AE/ads.md

## Information bulletins (advisory) (10 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 CE-00-18](https://openairdocs.org/saib/CE-00-18): . Issued Mar 30, 2000
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations

None matched to N822AE.

## 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 20080810843549I](https://openairdocs.org/incident/20080810843549I), Aug 10, 2008: Emb EMB135KL (N822AE), San Diego, CA, Minor damage. (-23) Acft departed lax for san on 8/10/08, crew reported a/c generator blew prior to landing at san without further incident. Visual inspection by contract…

## Service difficulty reports (123, 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 SIMA20210225001](https://openairdocs.org/sdr/SIMA20210225001), Feb 25, 2021: LAMP. INOPERATIVE. LEFT EXTERNAL EMERGENCY LIGHT INOP-CA-RAR LH EXTERNAL EMERGENCY LIGHT LAMP IAW AMM 33-50-10 OPERATIONAL CHECK GOOD.
- [SDR SIMA20201105001](https://openairdocs.org/sdr/SIMA20201105001), Nov 5, 2020: FLASHLIGHT. MISSING. AFT F/A FLASHLIGHT MISSING. C/A: FLIGHT CREW PLACARDED AFT F/A FLASHLIGHT, REF MEL 25-53AUTH 110065-C MOC 680820.
- [SDR SIMA20200715001](https://openairdocs.org/sdr/SIMA20200715001), Jul 15, 2020: SIGN. INOPERATIVE. FWD EMERG EXIT SIGN AT 11 ABC INOP. REPLACED EMERG EXIT SIGN FWD AT SEAT 11 ABC OPERATION CHECK GOOD PER AMM 33-50-10.
- [SDR SIMA202006198001](https://openairdocs.org/sdr/SIMA202006198001), Jun 18, 2020: LAMP. INOPERATIVE. MAIN DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MAIN DOOR EXTERNAL EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-06-000-801-A AND 33-50-06-400-801
- [SDR SIMA202001087001](https://openairdocs.org/sdr/SIMA202001087001), Jan 7, 2020: SLEEVE. LEAKING. DURING CLIMB PACK 1/2 VLV CLOSED. LEVEL AT 13,000 CAB ALT CONTINUED TO CLIMB AFTER RESETING PACK 1. RETURN TO DFW-C/A-FOUND LEAK AT THE AIR CONDITIONING EXHAUST
- [SDR SIMA20200102001](https://openairdocs.org/sdr/SIMA20200102001), Jan 2, 2020: O-RING. LEAKING. BLEED 2 LEAK ENROUTE. COMPLIED WITH QRH PROCEDURES. DID NOT LAND OVERWEIGHT-C/A-FOUND LEAK ON JOINT 20 AND 22 REMOVED AND REPLACED O-RING IAW EMB 140 AMM 36-11-
- [SDR SIMA2020010227004](https://openairdocs.org/sdr/SIMA2020010227004), Dec 27, 2019: DRIVE ASSY. INOPERATIVE. FLAP FAIL AFTER LANDING STUCK AT 1-C/A-REMOVED AND REPLACED FLAP SHROUD DRIVER IN LH, INBOARD FLAP 1 IAW EMB 140 AMM 27-50-00 AND S.B. NO:145-57-0012. OPERATION
- [SDR SIMA201911297001](https://openairdocs.org/sdr/SIMA201911297001), Nov 27, 2019: WARNING MESSAGE. FALSE ACTIVATION. PACK 1 FAIL MSG IN FLIGHT. EMERGENCY DECLARED FLT -C/A-PERFORMED OPERATIONAL CHECK OF PACK 1 IAW ERJ 140 AMM 21-20-00-700-801-A. OPS CHECK NORMAL. NO DEFECTS NO
- [SDR SIMA20190926002](https://openairdocs.org/sdr/SIMA20190926002), Sep 26, 2019: MECHANISM. LACK OF LUBE. FA REPORTS MAIN CABIN DOOR IS DIFFICULT TO CLOSE DUE TO LOOSE HANDLE-C/A-AT THIS TIME LUBRICATED MAIN DOOR LOCKING MECHANISM IAW AMM 52-10-00.OPS. CK FOUND OK.D
- [SDR SIMA20190701005](https://openairdocs.org/sdr/SIMA20190701005), Jul 1, 2019: NOT REPORTED. DENTED. DENT FOUND BELOW CARGO DOOR BETWEEN FRAMES 66 AND FRAMES 67 AND STRG21R AND STRG 20L. MAJOR REPAIR. C/A-REPAIRED DENT BELOW CARGO DOOR IAW ERS-EM-53MR-3826. SEE
- [SDR SIMA201906241001](https://openairdocs.org/sdr/SIMA201906241001), Jun 21, 2019: SMOKE DETECTOR. NO TEST. CAPT REPORTS CARGO SMOKE DETECTOR PUSH BUTTON LIGHT STAYS ON WHEN TESTED. REMOVED AND REPLACED #2 CARGO SMOKE DETECTOR IAW E140 AMM 26-15-01 AND SMOKE DETECTOR 
- [SDR SIMA20190508003](https://openairdocs.org/sdr/SIMA20190508003), May 8, 2019: TRIM SWITCH. DIRTY. "PIRIM MAIN INOP" MSG DURING FLIGHT. C/A-ACCOMPLISHED INSPECTION, CLEANING AND LUBRICATION OF PILOT AND CO-PILOT PITCH TRIM SWITCHES IAW AMM 27-40-03. ALSO PERF
- [SDR SIMA20190313002](https://openairdocs.org/sdr/SIMA20190313002), Mar 13, 2019: ROLLER. OBSTRUCTED. MAIN CABIN DOOR HARD TO OPEN + CLOSE. C/A-REMOVED FOD FROM MAIN DOOR ROLLER. OPENED AND CLOSED DOOR SEVERAL TIMES. HANDLE LOAD IS 40 LBS. OPC GOOD REF IAW AMM 5
- [SDR SIMA20190118001](https://openairdocs.org/sdr/SIMA20190118001), Jan 18, 2019: INVERTER. INOPERATIVE. FOUND EMERGENCY EXIT LIGHT IN FWD CABIN BY GALLEY INOP. C/A-REMOVED AND REPLACED EMERGENCY LIGHT DC/AC INVERTER 1 IAW AMM 33-50-11. OPC GOOD.
- [SDR SIMA20190105005](https://openairdocs.org/sdr/SIMA20190105005), Jan 5, 2019: WHEEL. DEFECTIVE. HIGH SPEED VIBRATION APPEARS TO COME FROM NOSE WHEEL 40-70 KNOTS. C/A-FOUND NLG TIRES TO BE OUT OF ROUND. REMOVED AND REPLACED LT NLG WHEEL AND TIRE ASSY IAW W/
- [SDR SIMA201810086001](https://openairdocs.org/sdr/SIMA201810086001), Oct 6, 2018: LIGHT. INOPERATIVE. AFT FLOOR PROXIMITY STRIP AT ROW 16 INOP-C/A-REMOVED AND REPLACED AFT FLOOR PROXIMITY STRIP AT ROW 16A C/W IAW AMM 33-50-01. OPS IS GOOD.
- [SDR SIMA2018092523005](https://openairdocs.org/sdr/SIMA2018092523005), Sep 23, 2018: PROXIMITY SWITCH. CORRODED. "SPOILER FAIL" EICAS CAUTION PRESENTED IN FLIGHT MULTIPLE TIMES WITH SPEED BRAKE LEVER CLOSED. FOUND CORROSION ON SPOILER PROX SWITCHES. R&R ALL FOUR SPOILER PR
- [SDR SIMA2018092019003](https://openairdocs.org/sdr/SIMA2018092019003), Sep 19, 2018: HANDLE. FAILED. FIRE EXTINGUISHER T HANDLE DOES NOT ILLUMINATE DURINGFIRE DET TEST. REMOVED AND REPLACED RT ENG FIRE EXTINGUISHING HANDLE IAW AMM 26-21-01. OPS CHECK GOOD.
- [SDR SIMA201809065003](https://openairdocs.org/sdr/SIMA201809065003), Sep 5, 2018: BATTERY. DISCHARGED. EMERGENCY LIGHTS AT EXIT SIGNS AT EMERGENCY EXIT WING DOORS ARE INOP. REMOVED AND REPLACED NR 3 BATTERY POWER SUPPLY IAW AMM 33-50-04. OPERATIONAL CHECK GOOD. B
- [SDR SIMA20180830002](https://openairdocs.org/sdr/SIMA20180830002), Aug 30, 2018: ROLLER. DIRTY. FLIGHT ATTENDANT REPORTED MAIN DOOR DIFFICULT TO CLOSE AND LATCH. C/A-CLEANED & LUBRICATED MAIN DOOR FRAME ROLLERS IAW AMM 53-21-02. OPC GOOD AT THIS TIME.
- [SDR SIMA20180826001](https://openairdocs.org/sdr/SIMA20180826001), Aug 26, 2018: DUCT. LEAKING. NR 2 BLEED LEAK, IN FLIGHT, MESSAGE STAYED PRESENT FOR AT LEAST 5 - 6 MINUTES BEFORE GOING AWAY. DIVERTED BACK TO DEPARTURE. FOUND THE DUCT IN THE NR 2 PYLON LE
- [SDR SIMA201808275001](https://openairdocs.org/sdr/SIMA201808275001), Aug 25, 2018: CLAMP. LEAKING. NR 2 ENGINE BLEED LEAK, NR 2 BLEED LEAK.. ADJUSTED THE CROSSBLEED CLAMPS IAW AMM 36-10-01, PERFORMED AN OPS CHECK OF THE NR 2 BLEED SYSTEM, NO MESSAGE NOTED WIT
- [SDR SIMA20180819009](https://openairdocs.org/sdr/SIMA20180819009), Aug 19, 2018: DRAG ANGLE. CRACKED. RIGHT FWD VERTICAL STAB TO FUSELAGE DRAG ANGLE WAS CRACKED AT THE AFT END FASTENER. REMOVED AND REPLACED THE DRAG ANGLE IAW SRM 51-40-02.
- [SDR SIMA2018082718003](https://openairdocs.org/sdr/SIMA2018082718003), Aug 18, 2018: FITTING. CRACKED. PAX DOOR CUTOUT REINFORCEMENT FITTING WAS CRACKED AT FRAME 20, STRINGER 3L. REMOVED AND REPLACED THE REINFORCEMENT FITTING IAW SRM 51-40-02.
- [SDR SIMA2018082718004](https://openairdocs.org/sdr/SIMA2018082718004), Aug 18, 2018: FRAME. CRACKED. FRAME 23 WAS CRACKED BETWEEN STRINGERS 15R - 16R. REPAIRED THE FRAME IAW SRM 53-00-04.
- [SDR SIMA2018082717002](https://openairdocs.org/sdr/SIMA2018082717002), Aug 17, 2018: WIRE. BROKEN. EMERGENCY LIGHT STRIP AT 241BF HAD BROKEN WIRES ON THE ACFT SIDE. REPAIRED THE WIRES IAW SWPM 20-21-00.
- [SDR SIMA2018082716002](https://openairdocs.org/sdr/SIMA2018082716002), Aug 16, 2018: SUPPORT. CRACKED. RIGHT OVERWING EMERGENCY EXIT HATCH LOWER SUPPORT WAS CRACKED AT THE FWD END, INSIDE LOWER BAY. REMOVED AND REPLACED THE SUPPORT IAW SRM 51-40-02.
- [SDR SIMA2018082715005](https://openairdocs.org/sdr/SIMA2018082715005), Aug 15, 2018: YOKE. CRACKED. LEFT ENGINE FWD LOWER PYLON YOKE WAS CRACKED. REMOVED AND REPLACED THE LT FORWARD LOWER PYLON YOKE FITTING IAW EO EM-54MR-386.
- [SDR SIMA2018092727003](https://openairdocs.org/sdr/SIMA2018092727003), Jul 27, 2018: LENS. CRACKED. EMERGENCY EXIT LIGHT LENS CRACKED ON CEILING PANEL 253CLC-C/A-COMPLETE:REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS ON CEILING PANEL 253 CLC IAW CD CMM 25-28-
- [SDR SIMA2018073026001](https://openairdocs.org/sdr/SIMA2018073026001), Jul 26, 2018: BATTERY. DISCHARGED. EMERGENCY LIGHT INOP AT ROW 7A FLOOR PROXI STRIP, AND OVERWING HATCH. REMOVED AND REPLACED NUMBER 3 BATTERY AND BATTERY POWER SUPPLY IAW AMM 33-50-04. OPS CK GO
- [SDR SIMA201807132004](https://openairdocs.org/sdr/SIMA201807132004), Jul 12, 2018: POWER SUPPLY. INOPERATIVE. FOUND BATTERY POWER SUPPLY NR 3 TO BE INOP DURING PS-1 CHECK. REMOVED AND REPLACED NR 3 BATTERY POWER SUPPLY IAW AMM 33-50-04 OPC GOOD A/C OK FOR SERVICE.
- [SDR SIMA20180628001](https://openairdocs.org/sdr/SIMA20180628001), Jun 28, 2018: O-RING. DAMAGED. BLEED 1 LEAK IN FLIGHT. INSPECTED FOR BLEED 1 LEAK FOUND JOINT 11 AND 13 LEAKING. REMOVED AND REPLACE ORINGS AT JOINT 11 AND 13 AND OPS CHECKS AND LEAK CHECK GO
- [SDR SIMA20180401001](https://openairdocs.org/sdr/SIMA20180401001), Apr 1, 2018: ACM. FAILED. BOTH PACKS INOPERATIVE DURING CLIMB OUT. REMOVED AND REPLACED THE LT ACM IAW AMM 21-51-03. OPS CHECKED GOOD. NO LEAKS NOTED. R & R THE CONDENSER MIXER IAW AMM 2
- [SDR SIMA20180225001](https://openairdocs.org/sdr/SIMA20180225001), Feb 25, 2018: SIGNAL COND UNIT. FAILED. AFTER TAKEOFF, FUEL QUANTITY INDICATIONS WENT TO AMBER DASHES AND EICAS MESSAGE E1/2 LOW FUEL MESSAGE PRESENTED. RMOVED AND REPLACED THE WING FUEL CONDITIONING 
- [SDR SIMA20180223004](https://openairdocs.org/sdr/SIMA20180223004), Feb 23, 2018: SMOKE DETECTOR. CONTAMINATED. LAVATORY SMOKE DETECTION TEST FAILED IAW PS-2 MTX W. C. CLEANED LINT FROM THE LAVATORY SMOKE DETECTOR, PERFORMED AN OPS CHECK IAW AMM 26-14-00. OPS CHECKED GOOD
- [SDR SIMA20180213003](https://openairdocs.org/sdr/SIMA20180213003), Feb 13, 2018: FLASHLIGHT. FAILED. VISIBLE SMOKE IN THE COCKPIT, CLIMBING THROUGH FL180. SMELLED LIKE ELECTRICAL SMOKE, FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. FOUND THE FWD FA AND AFT FA F
- [SDR SIMA20180107002](https://openairdocs.org/sdr/SIMA20180107002), Jan 7, 2018: DOOR. OUT OF ADJUST. F/A REPORTED THE MAIN CABIN DOOR DIFFICULT TO OPEN. DOOR ADJUSTED AND TESTED IAW AMM 52-10-01. OPS CHECKED GOOD.
- [SDR SIMA20170317002](https://openairdocs.org/sdr/SIMA20170317002), Mar 17, 2017: CRADLE. BROKEN. FWD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT CRADLE IS BROKEN. REMOVED AND REPLACED THE CRADLE IAW AMM 33-50-16. OPS CHECKED GOOD.
- [SDR SIMA20170207003](https://openairdocs.org/sdr/SIMA20170207003), Feb 7, 2017: LIGHT. INOPERATIVE. EMERGENCY FLOOR PROXIMITY LIGHTING STRIP AT ROWS 15 AND 16 INOP. REMOVED AND REPLACED EMERGENCY FLOOR PROXIMITY LIGHTING STRIP AT ROWS 15-16 IAW AMM33-50-12. OP
- [SDR SIMA20161018001](https://openairdocs.org/sdr/SIMA20161018001), Oct 18, 2016: ROLLER. LACK OF LUBE. MAIN CABIN DOOR VERY DIFFICULT TO OPEN. CLEANED AND LUBRICATED LOWER FORWARD AND AFT ROLLERS ON MAIN CABIN DOOR IAW EMB-140 AMM 52-18-00. OOR OPENS AND CLOSES P
- [SDR SIMA20160722004](https://openairdocs.org/sdr/SIMA20160722004), Jul 22, 2016: LIGHT. INOPERATIVE. AFT AISLE EMERGENCY CEILING LIGHT INOPERATIVE. R & R AFT AISLE EMERGENCY CEILING LIGHT BULB IAW AMM 33-50-08, OPS CK GOOD.
- [SDR SIMA20160528001](https://openairdocs.org/sdr/SIMA20160528001), May 28, 2016: DOOR SILL. CORRODED. CARGO DOOR CUT OUT LOWER CTR SILL CORRODED. REPAIRED CARGO DOOR CTR SILL IAW SRM 51-40-02 & 51-20-01.
- [SDR SIMA20160511001](https://openairdocs.org/sdr/SIMA20160511001), May 11, 2016: CASE. CHAFED. RIGHT OVERWING PANEL EMER LIGHT ASSEMBLY INTERIOR CASE IS CHAFED. R & R RT OVERWING PANEL EMER LIGHT ASSEMBLY IAW AMM 33-50-10.
- [SDR SIMA20160425003](https://openairdocs.org/sdr/SIMA20160425003), Apr 25, 2016: FRAME. CORRODED. FRAME 65 IS CORRODED UNDER FWD LOWER CARGO DOOR GUIDE PLATE. REPAIRED FRAME 65 UNDER FWD LOWER CARGO DOOR GUIDE PLATE IAW SRM 53-31-04 ITEM 4E FIG 212.
- [SDR SIMA20160421004](https://openairdocs.org/sdr/SIMA20160421004), Apr 21, 2016: HINGE FITTING. CORRODED. LEFT ELEVATOR SERVO TAB INBD HINGE FITTING CORRODED AT BONDING WIRE ATTACHMENT. R & R LT ELEVATOR SERVO TAB INBD HINGE FITTING IAW AMM 55-22-01, SRM 51-20-03 & 
- [SDR SIMA20160331010](https://openairdocs.org/sdr/SIMA20160331010), Mar 31, 2016: SKIN. CRACKED. LEFT UPPER FUSELAGE SKIN CRACKED IN 2 PLACES. CRACK 1 IS JUST AFT OF FRAME 75 & ABOVE STRINGER 2L. CRACK IS APPROX 3/8" LONG. CRACK 2 IS AT THE FIRST FASTENER A
- [SDR SIMA20160331009](https://openairdocs.org/sdr/SIMA20160331009), Mar 31, 2016: SKIN. CRACKED. RIGHT UPPER FUSELAGE SKIN CRACKED AT FIRST FASTENER, BELOW STRINGER 2R. CRACK IS APPROX 3/8" LONG. PERFORMED REPAIR OF RT UPPER FUSELAGE SKIN CRACKS IAW ERS-EM-
- [SDR SIMA20150901002](https://openairdocs.org/sdr/SIMA20150901002), Sep 1, 2015: WIRE. BROKEN. AFT ROW EMER LIGHT FLOOR STRIP HAS BROKEN WIRE. R & R AFT ROW EMER LIGHT FLOOR STRIP IAW MM 33-50-12. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150805006](https://openairdocs.org/sdr/SIMA20150805006), Aug 5, 2015: LIGHT. INOPERATIVE. MAIN DOOR OVERHEAD EMER LIGHT INOPERATIVE. R & R MAIN DOOR OVERHEAD EMER LIGHT IAW AMM 33-50-06. OPERATIONS CHECKED GOOD.
- [SDR SIMA20150519001](https://openairdocs.org/sdr/SIMA20150519001), May 19, 2015: BRAKE. FIRE. AFTER LANDING, ACFT BEHIND US REPORTED LT INBD TIRE ON FIRE, THEN WENT OUT SHORTLY. R & R NR 2 BRAKE ASSEMBLY IAW WC 32-600-14. R & R NR 2 BRAKE TEMP SENSOR IAW

All 123: https://openairdocs.org/aircraft/N822AE/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/N822AE/stcs.md

## Related

- Other Embraer EMB-135KL aircraft: https://openairdocs.org/model/embraer-emb-135kl/aircraft.md
- The Rolls-Royce AE3007 series engine: https://openairdocs.org/engine/rolls-royce-ae3007-series.md

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.