# N15527: 2001 Embraer EMB-135LR

- Status: Valid registration
- Airframe: [Embraer EMB-135LR](https://openairdocs.org/model/embraer-emb-135lr) (registry code 3260305, 37 seats)
- Engine: [Allison AE-3007A](https://openairdocs.org/engine/allison-ae-3007a) (registry code 03030)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT) (Embraer S.A.), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (Rolls-Royce Corporation) (OpenAirDocs)
- Serial number: 145413
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 6, 2001
- Certificate issued: May 29, 2018
- Expires: May 31, 2028
- Mode S code: A0DF80
- Registered owner: [Corporate Flight Management Inc](https://openairdocs.org/faa-owner/CORPORATE%20FLIGHT%20MANAGEMENT%20INC)
- Location: [Smyrna, TN](https://openairdocs.org/faa-place/TN/Smyrna)
- Owner type: Corporation
- Owner's area on the map: 35.9628° N, 86.5297° W: Placed by OpenAirDocs at the center of ZIP code 37167, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=15527
- Page: https://openairdocs.org/aircraft/N15527

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): 89 in force

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

- [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 2007-10-11](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
- [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

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

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

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

- [AD 2008-13-14](https://openairdocs.org/ad/2008-13-14) (historical): Fuel system limitations (FSL) · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Jul 30, 2008
- [AD 2007-12-17](https://openairdocs.org/ad/2007-12-17) (historical): Metallic tubes enclosing the vent and pilot valve wires · Embraer - Empresa Brasileira de Aeronautica EMB-135BJ, EMB-135ER, EMB-135KE and 9 more. Effective Jul 19, 2007
- [AD 2006-22-05](https://openairdocs.org/ad/2006-22-05) (historical): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 27 more. Effective Dec 1, 2006
- [AD 2006-04-02](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 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 2001-17-03](https://openairdocs.org/ad/2001-17-03) (historical): Engine Thrust Reverser Stow/Transit Switches · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR and EMB-145 Series (all). Effective Sep 5, 2001
- [AD 2001-10-15](https://openairdocs.org/ad/2001-10-15) (historical): Fire Extinguisher Bottles · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR and EMB-145 Series (all). Effective Jun 8, 2001
- [AD 2001-10-01](https://openairdocs.org/ad/2001-10-01) (historical): Airplane Flight Manuals--APU Start/Stop Switch Panel · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR and EMB-145 Series (all). Effective May 29, 2001
- [AD 2000-19-03](https://openairdocs.org/ad/2000-19-03) (historical): Fuel System Tubing · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR, EMB-145 and 1 more. Effective Oct 3, 2000
- [AD 2000-19-02](https://openairdocs.org/ad/2000-19-02) (historical): Electric Fuel Pumps · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR and EMB-145 Series (all). Effective Oct 3, 2000
- [AD 2000-13-02](https://openairdocs.org/ad/2000-13-02) (historical): Precooler Differential Pressure Switches · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR and EMB-145 Series (all). Effective Jul 3, 2000
- [AD 2000-04-09](https://openairdocs.org/ad/2000-04-09) (historical): Elevator Servo Tab and Spring Tab Hinge Fittings of the Horizontal Stabilizer · Embraer - Empresa Brasileira de Aeronautica EMB-135ER, EMB-135LR, EMB-145 and 3 more. Effective Mar 10, 2000
- [AD 2010-19-01](https://openairdocs.org/ad/2010-19-01) (historical): High pressure turbine · Rolls-Royce AE 3007A. Effective Oct 27, 2010
- [AD 2009-08-51](https://openairdocs.org/ad/2009-08-51) (historical): High-pressure turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 6 more. Effective May 27, 2009
- [AD 2008-26-06](https://openairdocs.org/ad/2008-26-06) (historical): High-pressure turbine (HPT) · AE 3007A. Effective Jan 8, 2009
- [AD 2008-19-51](https://openairdocs.org/ad/2008-19-51) (historical): AE 3007A, AE 3007A1, AE 3007A1E and 5 more
- [AD 2001-08-15](https://openairdocs.org/ad/2001-08-15) (historical): Oil System · AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective May 14, 2001
- [AD 2000-09-05](https://openairdocs.org/ad/2000-09-05) (historical): Cone Shafts · AE 3007A, AE 3007A1, AE 3007A1P and 4 more. Effective Jul 5, 2000
- [AD 99-02-51](https://openairdocs.org/ad/99-02-51) (historical): Starter Shaft Seal · AE 3007A, AE 3007A1, AE 3007A1P and 5 more. Effective Apr 20, 1999

All 114: https://openairdocs.org/aircraft/N15527/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 N15527.

## FAA accident and incident reports

None matched to N15527.

## Service difficulty reports (44)

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 ASOA201701234002](https://openairdocs.org/sdr/ASOA201701234002), Jan 23, 2017: ENGINE. FLAMED OUT. IAH - FLIGHT 4231, THE CREW REPORTED ENG NR 2 OUT IN FLIGHT. THE AIRCRAFT LANDED IN IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER 2 ENG
- [SDR ASOA201610164076](https://openairdocs.org/sdr/ASOA201610164076), Oct 11, 2016: METERING UNIT. INOPERATIVE. FLIGHT 4193, THE CREW REPORTED THAT IMMEDIATELY AFTER TAKEOFF, THE NR 2 ENGINE SHUTDOWN, WITH NO N2 OR FUEL FLOW, AND RECEIVED E2 NO DISP, E2 CTL FAIL, SPOILER 
- [SDR ASOA201610164075](https://openairdocs.org/sdr/ASOA201610164075), Oct 11, 2016: FADEC. INOPERATIVE. FLIGHT 4193, THE CREW REPORTED THAT IMMEDIATELY AFTER TAKEOFF, THE NR 2 ENGINE SHUTDOWN, WITH NO N2 OR FUEL FLOW, AND RECEIVED E2 NO DISP, E2 CTL FAIL, SPOILER 
- [SDR ASOA201610164074](https://openairdocs.org/sdr/ASOA201610164074), Oct 11, 2016: FADEC. MALFUNCTIONED. FLIGHT 4193, THE CREW REPORTED THAT IMMEDIATELY AFTER TAKEOFF, THE NR 2 ENGINE SHUTDOWN, WITH NO N2 OR FUEL FLOW, AND RECEIVED E2 NO DISP, E2 CTL FAIL, SPOILER 
- [SDR ASOA20160905070H](https://openairdocs.org/sdr/ASOA20160905070H), Sep 5, 2016: LIGHT. INOPERATIVE. THE CREW REPORTED THAT THE FIRST SEGMENT OF AISLE PATH LIGHTING WAS INOPERATIVE. MAINTENANCE R & R THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECT
- [SDR ASOA20160404015](https://openairdocs.org/sdr/ASOA20160404015), Apr 4, 2016: FRAME. CRACKED. DURING C-CHECK. RT FRAME 10 IS CRACKED. REPLACED RT FRAME 10 IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150424039](https://openairdocs.org/sdr/ASOA20150424039), Apr 24, 2015: UNKNOWN. ODOR. THE CREW REPORTED THAT THE GASPER FAN HAD A BURNING ODOR WITH PACK NR 2 AND NOT RUNNING THE NR 2 RECIRCULATION FAN. ACFT WAS APPROVED FOR RETURN TO SERVICE. MAI
- [SDR ASOA20150424039H](https://openairdocs.org/sdr/ASOA20150424039H), Apr 24, 2015: FAN. FAILED. THE CREW REPORTED THAT THE GASPER FAN HAD A BURNING ODOR WITH PACK NR 2 AND NOT RUNNING THE NR 2 RECIRCULATION FAN. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131211215](https://openairdocs.org/sdr/ASOA20131211215), Dec 11, 2013: DRAG ANGLE. CRACKED. DURING 1A INSPECTION, THE RT FWD DRAG ANGLE, PROFILE, WAS FOUND TO BE CRACKED AT FRAME 76. MAINTENANCE R & R THE AFFECTED DRAG ANGLE, PROFILE, AND THE ACFT WAS 
- [SDR ASOA201311274](https://openairdocs.org/sdr/ASOA201311274), Nov 27, 2013: SILL. CORRODED. DURING C-CHECK, CENTER SERVICE DOOR SILL CORRODED. MAINTENANCE R & R DOOR SILL IAW SRM 51-40-02. RETURNED TO SERVICE.
- [SDR ASOA20131127273](https://openairdocs.org/sdr/ASOA20131127273), Nov 27, 2013: THRESHOLD. CORRODED. DURING C-CHECK CARGO DOOR LOWER THRESHOLD CORRODED. MAINTENANCE REPAIRED THRESHOLD IAW SRM 51-40-02. RETURNED TO SERVICE.
- [SDR ASOA20131127272](https://openairdocs.org/sdr/ASOA20131127272), Nov 27, 2013: SHEAR TIE. CRACKED. DURING C-CHECK SHEAR TIE AT FRAME 75, S2L-2R CORRODED. MX R & R SHEAR TIE IAW EC5310-01317. RETURNED TO SERVICE.
- [SDR ASOA20130313029](https://openairdocs.org/sdr/ASOA20130313029), Mar 13, 2013: INVERTER. INOPERATIVE. DURING ROUTINE MX THE EMERGENCY LIGHT ABOVE THE F/A SEAT FAILED TO ILLUMINATE WHEN TESTED. MX REPLACED THE EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED THE SY
- [SDR CHQA201100223](https://openairdocs.org/sdr/CHQA201100223), Jun 13, 2011: UNKNOWN. ODOR. CREW REPORTED, SHORTLY AFTER TAKEOFF A SMOKE ODOR IN THE CABIN AND THE COCKPIT. A LAVATORY SMOKE INDICATION THEN APPEARED ON THE EICAS. REPORTED THAT AFTER APPR
- [SDR CHQA201100197](https://openairdocs.org/sdr/CHQA201100197), May 28, 2011: LIGHT. INOPERATIVE. DURING INSPECTION, THE RIGHT AFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTS WITH NO DE
- [SDR CHQA201100072](https://openairdocs.org/sdr/CHQA201100072), Mar 22, 2011: CARBON SEAL. WORN. CREW REPORTED THAT UPON TAKEOFF, AT APPROXIMATELY 400 FEET, CREW BECAME AWARE OF SMOKE IN THE COCKPIT AND CABIN. AFTER LEVELING OFF AT 4000 FEET, THE SMOKE RAPI
- [SDR CHQA201000202](https://openairdocs.org/sdr/CHQA201000202), Oct 22, 2010: PRESSURE SWITCH. FAULTY. CREW REPORTED THAT ON CLIMB-OUT FROM MKE, RECEIVED A RUDDER SYS 1-2 INOP MESSAGE ALONG WITH A YAW DAMP FAIL MESSAGE ON EICAS. THE QRH WAS FOLLOWED AND THE MESSA
- [SDR CHQA201000095](https://openairdocs.org/sdr/CHQA201000095), May 10, 2010: TRANSDUCER. FAILED. AFTER LANDING THE CREW REPORTED THAT HIGH SPEED BRAKING WAS INEFFECTIVE. BOTH BRAKE PEDALS WENT TO THE FLOOR WITH LITTLE EFFECT. CREW ALSO REPORTED THAT BRAKING
- [SDR CHQA200900216](https://openairdocs.org/sdr/CHQA200900216), Oct 8, 2009: SOLENOID VALVE. DETERIORATED. AFTER TAKEOFF WHEN A POSITIVE RATE OF CLIMB WAS ESTABLISHED, THE GEAR HANDLE WAS SELECTED TO THE UP POSITION, AND AFTER A FEW SECONDS THE CREW RECEIVED A RED GE
- [SDR CHQA200900214](https://openairdocs.org/sdr/CHQA200900214), Oct 2, 2009: ELECTRONIC UNIT. FAULTY. FLIGHT 1206, IND TO MKE. AFTER TAKEOFF, THE CREW SELECTED THE GEAR UP AND RECEIVED A 3 RED INDICATION SHOWING DOWN IN ADDITION TO LG LEVER DISAGREE ON EICAS. TH
- [SDR CHQA200900206](https://openairdocs.org/sdr/CHQA200900206), Sep 20, 2009: UNKNOWN. MALFUNCTIONED. FLIGHT 1119, MKE TO SDF. CREW REPORTED THAT AFTER DEPARTURE THE LANDING GEAR FAILED TO RETRACT ALONG WITH A LANDING GEAR LEVER DISAGREE MESSAGE. THE CREW RAN TH
- [SDR C2XA07IA206](https://openairdocs.org/sdr/C2XA07IA206), Sep 14, 2007: CONTROL HANDLE. DEFECTIVE. IAH - FLIGHT 2206, THE CREW REPORTED LANDING GEAR DOES NOT RETRACT PROPERLY, LANDING GEAR HANDLE SELECTED UP GEAR INDICATION 3 DOWN FOR 5 - 10 SEC THEN IN TRANS
- [SDR C2XA07IA086](https://openairdocs.org/sdr/C2XA07IA086), Apr 12, 2007: UNKNOWN. UNKNOWN. IAH - FLIGHT 2922 AFTER TAKEOFF, THE CREW SELECTED GEAR LEVER TO UP POSTION BUT GEAR DID NOT RETRACT, CYCLED LEVER BACK DOWN THEN UP RETRACTED NORMAL. THE AIRCR
- [SDR C2XA07IA012](https://openairdocs.org/sdr/C2XA07IA012), Jan 11, 2007: INDICATION SYS. MALFUNCTIONED. IAH - FLIGHT 3109, THE CREW REPORTED AFTER T/O THE GEAR STARTED TO RETRACT, GOT AMBER THEN RED INDICATIONS WITH LANDING GEAR LEVER DISAGREE MESSAGE. THE GEAR ST
- [SDR C2XA05IA104](https://openairdocs.org/sdr/C2XA05IA104), Sep 10, 2005: LIGHT. INOPERATIVE. LRD - FLIGHT 2359, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT BOTH SIDE PANEL EXIT LIGHTS AT THE OVERWING EXITS WERE INOPERATIVE. THE CREW RESET THE EM
- [SDR C2XA05SH096](https://openairdocs.org/sdr/C2XA05SH096), Aug 9, 2005: FIREWALL. CRACKED. SHV - DURING C-CHECK APU FIRE WALL CRACK AROUND NUT PLATE FASTENERS AT 3 O`CLOCK POSITION. MAINTENANCE REPAIRED APU FIREWALL AT 3 O`CLOCK POSITION IAW EC 5330-0
- [SDR C2XA05SH101](https://openairdocs.org/sdr/C2XA05SH101), May 11, 2005: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK CORROSION ON RT OMEGA BEAM AT FR 18. MAINTENANCE REPAIRED RT OMEGA BEAM AT FR 18 IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RE
- [SDR C2XA04TY099](https://openairdocs.org/sdr/C2XA04TY099), Jun 23, 2004: THRESHOLD. CORRODED. DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE PASSENGER ENTRY DOOR THRESHOLD PLATE. MAINTENANCE REMOVED AND REPLACED THE THRESHOLD PLATE IAW EMB SRM 
- [SDR C2XA04IA022](https://openairdocs.org/sdr/C2XA04IA022), Mar 1, 2004: PROXIMITY SWITCH. FAULTY. DURING CLIMB THE NOSE GEAR DOORS DID NOT RETRACT AFTER THE NOSE LANDING GEAR WAS UP AND LOCKED. THE AIRCRAFT RETURNED TO XNA AND LANDED WITHOUT INCIDENT. THE AI
- [SDR C2XA03BT115](https://openairdocs.org/sdr/C2XA03BT115), Dec 7, 2003: CONTROLLER. FAULTY. CREW REPORTED, AUTO PRESSURIZATION FAILED DURING DESCENT. AIRCRAFT WAS RELEASED IAW MEL 21-31-03/1 CONTROL NUMBER 037305. AIRCRAFT RETURNED TO SERVICE. MAINTENA
- [SDR C2XA03CL189](https://openairdocs.org/sdr/C2XA03CL189), Nov 18, 2003: LIGHT. INOPERATIVE. CLE FLIGHT 2051 THE CREW REPORTED THE RIGHT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE RIGHT WING AFT EMERGENCY LIGHT. OPE
- [SDR C2XA03CL117](https://openairdocs.org/sdr/C2XA03CL117), Jul 2, 2003: CHARGER. FAULTY. DURING ROUTINE MAINTENANCE THE EMERGENCY AISLE PATH LIGHTS WERE DIM. MAINTENANCE REPLACED THE NR 2 EMERGENCY BATTERY CHARGER. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA03TY050](https://openairdocs.org/sdr/C2XA03TY050), Apr 16, 2003: HANDLE. SHORTED. TYS- DURING A SCHEDULED 1-C INSPECTION THE FIRE HANDLE NR 2 WOULD NOT LIGHT UP DURING THE FIRE DETECTION TEST. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE FIRE
- [SDR C2XA03TY049](https://openairdocs.org/sdr/C2XA03TY049), Apr 15, 2003: SHEAR TIE. BENT. TYS, DURING A SCHEDULED INSPECTION A DENT WAS FOUND ON THE LEFT FORWARD FUSELAGE BETWEEN FRAMES 10 AND 11 AND BETWEEN STRINGERS 13L AND 15L. MAINTENANCE REMOVED
- [SDR C2XA03TY048](https://openairdocs.org/sdr/C2XA03TY048), Apr 15, 2003: FLOORBEAM. CORRODED. TYS, DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL PLATE WAS FOUND CORRODED AFT OF THE COCKPIT STEP IN THE GALLEY. MAINTENANCE REMOVED AND REPLACED THE CENT
- [SDR C2XA03TY047](https://openairdocs.org/sdr/C2XA03TY047), Apr 15, 2003: STRINGER. BENT. TYS, DURING A SCHEDULED INSPECTION A TEMPORARY REPAIR BETWEEN FRAMES 24 AND 25 AT STRINGER 12R, WAS MADE PERMANENT. REMOVED THE OLD REPAIR STRINGER 12R, CUT OUT
- [SDR C2XA02CL235](https://openairdocs.org/sdr/C2XA02CL235), Nov 30, 2002: WIRE HARNESS. FAULTY. CLE FLIGHT#3141 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE DURING FLIGHT ASSOCIATED WITH "THUMP" NOISE UNDER NOSE.THE AIRCRAFT LANDED WITHOUT FURT
- [SDR C2XA02CL162](https://openairdocs.org/sdr/C2XA02CL162), Aug 4, 2002: RECEPTACLE. BURNED. SLP - FLIGHT 4153, THE CREW REPORTED A STRONG SMELL OF BURNING RUBBER FROM THE NR 2 COFFEE JUG. THE AIRCRAFT WAS RELEASED IAW 25-60-02/3D. MAINTENANCE REPLACED 
- [SDR C2XA02CL136](https://openairdocs.org/sdr/C2XA02CL136), Jun 27, 2002: FIRE LOOP. CHAFED. DTW FLIGHT 3318 THE CREW REPORTED A NR 2 FIRE DETECT FAIL MESSAGE ON TAKEOFF. THE TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED A
- [SDR C2XA02CL081](https://openairdocs.org/sdr/C2XA02CL081), Mar 24, 2002: MODULE. FAULTY. CLE FLIGHT 3029 THE CREW REPORTED THE EMERGENCY LIGHTS WOULD NOT GO OUT. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EMERGENCY LIGHT CONTROL MOD
- [SDR C2XA01CL247](https://openairdocs.org/sdr/C2XA01CL247), Dec 17, 2001: CONTROL HANDLE. INTERMITTENT. CLE FLIGHT 3064 THE CREW REPORTED THE LANDING GEAR DID NOT RETRACT. RECYCLED AND IT WAS SLOW TO RETRACT. MAINTENANCE REPLACED THE LANDING GEAR HANDLE ASSEMBLY. 
- [SDR C2XA01CL185](https://openairdocs.org/sdr/C2XA01CL185), Jul 28, 2001: FIREWALL. CRACKED. CLE MAINTENANCE DURING ACCOMPLISHMENT OF SB 145-49-0009 AND 145-49-0018 MAINTENANCE FOUND THE APU FIREWALL CRACKED IN SEVERAL PLACES. THE AIRCRAFT WAS RELEASED 
- [SDR C2XA01CL118](https://openairdocs.org/sdr/C2XA01CL118), May 24, 2001: CONTROL HANDLE. DEFECTIVE. CLE FLIGHT 3678 THE CREW REPORTED THE NOSE GEAR WAS SLOW TO RETRACT. RECEIVED A L/G GEAR LEVER DISAGREEMENT. THE MESSAGE CLEARED ON ITS OWN. THE AIRCRAFT LANDED
- [SDR C2XA01IA234](https://openairdocs.org/sdr/C2XA01IA234), Apr 29, 2001: LANDING GEAR. MALFUNCTIONED. BPT - DURING TRAINING FLIGHT 838, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PERFO

## STCs that may be installed (OpenAirDocs) (72, 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-135LR)

- [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 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 ST02815LA](https://openairdocs.org/stc/ST02815LA): Installation of Airworthy R/H and L/H Stowage Units. Airworthy Incorporated
- [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 ST04327CH](https://openairdocs.org/stc/ST04327CH): Installation of High Speed Internet System and Wireless Activation. Nextant Aerospace 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 ST04525AT](https://openairdocs.org/stc/ST04525AT): Installation of the Universal Avionics Flight Management System (FMS) Model No. UNS-1LW. SKH Aerospace 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 ST00818DE](https://openairdocs.org/stc/ST00818DE): Installation of Honeywell Control Display Unit (CDU) model CD-830. Premier Air Center LLC d/b/a West Star Aviation
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST09858SC](https://openairdocs.org/stc/ST09858SC): Installation of cabin automatic coffee brewing system. Safran Cabin Germany Gmbh
- [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 ST00010IB](https://openairdocs.org/stc/ST00010IB): Installation of convection oven model 1546-1 series, P/N 400-2095-01-R, on left-hand galley, P/N 135-85121-401. Embraer Engineering & Technology Center - USA Inc
- [STC ST04049NY](https://openairdocs.org/stc/ST04049NY): Installation of a Hoffman Engineering LLC LED Landing Light to replace the OEM Q4559 Series Incandescent Lamp, used as a Landing/Takeoff Light. Hoffman Engineering LLC
- [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 ST03889AT](https://openairdocs.org/stc/ST03889AT): Installation of Aircell Axxess Cabin Telecommunication Router (CTR) 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

All 72: https://openairdocs.org/aircraft/N15527/stcs.md

## Earlier aircraft with N15527

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N15527 before.

- [Cancelled 1994-11-15](https://openairdocs.org/deregistered/N15527-1994-11-15): Beech 1900D, S/N UE117. Exported to Australia. Owner: [Rangeflyers Inc](https://openairdocs.org/faa-owner/RANGEFLYERS%20INC), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)
- [Cancelled 1970-06-12](https://openairdocs.org/deregistered/N15527-1970-06-12): Stearman-Hammond Y-1S, S/N 313, built 1937. Owner: [O E Lee & Co](https://openairdocs.org/faa-owner/O%20E%20LEE%20%26%20CO), [Billings, MT](https://openairdocs.org/faa-place/MT/Billings)

## Related

- Other Embraer EMB-135LR aircraft: https://openairdocs.org/model/embraer-emb-135lr/aircraft.md
- The Allison AE-3007A engine: https://openairdocs.org/engine/allison-ae-3007a.md

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