# N16981: 1999 Embraer EMB-145LR

- Status: Valid registration
- Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212, 55 seats)
- Engine: [Allison AE-3007A](https://openairdocs.org/engine/allison-ae-3007a) (registry code 03030)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT) (Embraer S.A.), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (Rolls-Royce Corporation) (OpenAirDocs)
- Serial number: 145208
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 19, 1999
- Certificate issued: September 13, 2022
- Expires: September 30, 2029
- Mode S code: A116A7
- Registered owner: [Delux Public Charter LLC](https://openairdocs.org/faa-owner/DELUX%20PUBLIC%20CHARTER%20LLC)
- Location: [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas)
- Owner type: LLC
- Owner's area on the map: 32.8483° N, 96.8255° W: Placed by OpenAirDocs at the center of ZIP code 75209, 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=16981
- Page: https://openairdocs.org/aircraft/N16981

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 104 in force

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

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2025-08-07](https://openairdocs.org/ad/2025-08-07): Flight Controls · Embraer EMB-145, EMB-145ER, EMB-145MR and 4 more. Effective Jun 26, 2025
- [AD 2024-26-07](https://openairdocs.org/ad/2024-26-07): Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Mar 11, 2025
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2021-07-14](https://openairdocs.org/ad/2021-07-14): Main landing gear · Yaborã Indústria Aeronáutica EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 10 more. Effective Apr 20, 2021
- [AD 2021-04-09](https://openairdocs.org/ad/2021-04-09): Engine fuel and control · Yaborã Indústria Aeronáutica EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 10 more. Effective Mar 30, 2021
- [AD 2019-03-30](https://openairdocs.org/ad/2019-03-30): Engine Exhaust · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Mar 26, 2019
- [AD 2017-15-16](https://openairdocs.org/ad/2017-15-16): Flight controls · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Sep 5, 2017
- [AD 2017-12-09](https://openairdocs.org/ad/2017-12-09): Fuel · Embraer EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 10 more. Effective Jul 20, 2017
- [AD 2017-04-12](https://openairdocs.org/ad/2017-04-12): Ice and rain protection · Embraer EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 10 more. Effective Mar 29, 2017
- [AD 2015-02-13](https://openairdocs.org/ad/2015-02-13): Nacelles/pylons; Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Mar 6, 2015
- [AD 2013-22-18](https://openairdocs.org/ad/2013-22-18): Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Nov 20, 2013
- [AD 2012-19-06](https://openairdocs.org/ad/2012-19-06): Stabilizers · Embraer EMB-135BJ (Legacy 600), EMB-135BJ (Legacy 650), EMB-135ER and 9 more. Effective Oct 29, 2012
- [AD 2011-21-15](https://openairdocs.org/ad/2011-21-15): Fuselage · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 7 more. Effective Nov 23, 2011
- [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011
- [AD 2010-16-02](https://openairdocs.org/ad/2010-16-02): Airborne Auxiliary Power · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Sep 9, 2010
- [AD 2010-16-01](https://openairdocs.org/ad/2010-16-01): Fuel · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Sep 9, 2010
- [AD 2010-12-07](https://openairdocs.org/ad/2010-12-07): Wings · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Jul 22, 2010
- [AD 2010-11-01](https://openairdocs.org/ad/2010-11-01): Fuselage · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jul 6, 2010
- [AD 2010-10-11](https://openairdocs.org/ad/2010-10-11): Landing gear · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jun 21, 2010
- [AD 2010-07-02](https://openairdocs.org/ad/2010-07-02): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 26 more. Effective May 3, 2010
- [AD 2010-03-07](https://openairdocs.org/ad/2010-03-07): Landing gear · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 11, 2010
- [AD 2009-26-02](https://openairdocs.org/ad/2009-26-02): Ice and rain protection · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 19, 2010
- [AD 2009-01-05](https://openairdocs.org/ad/2009-01-05): Maximum takeoff weight (MTOW) · Embraer EMB-145, EMB-145EP, EMB-145ER and 4 more. Effective Mar 27, 2009
- [AD 2008-22-19](https://openairdocs.org/ad/2008-22-19): Flight deck · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 19, 2008
- [AD 2008-17-05](https://openairdocs.org/ad/2008-17-05): Fuel tanks · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Sep 23, 2008
- [AD 2008-10-08](https://openairdocs.org/ad/2008-10-08): Reduces the compliance time for doing the modification · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective May 23, 2008
- [AD 2008-05-02](https://openairdocs.org/ad/2008-05-02): Tail section or rudder pedals · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Apr 8, 2008
- [AD 2008-03-03](https://openairdocs.org/ad/2008-03-03): Elevator control system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Feb 14, 2008
- [AD 2007-24-03](https://openairdocs.org/ad/2007-24-03): Forward fuselage right hand (RH) side skin · Embraer EMB-135ER, EMB-135KE, EMB-135KL and 8 more. Effective Jan 2, 2008
- [AD 2007-10-11](https://openairdocs.org/ad/2007-10-11): Electrical bonding clamps · Embraer EMB-135BJ (Legacy 600), EMB-135LR, EMB-145LR and 2 more. Effective Jun 21, 2007
- [AD 2007-04-09](https://openairdocs.org/ad/2007-04-09): Left- and right-hand windshield temperature controllers · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 23, 2007
- [AD 2007-04-03](https://openairdocs.org/ad/2007-04-03): Pitot static heating relay K0057 · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 21, 2007
- [AD 2006-19-04](https://openairdocs.org/ad/2006-19-04): Honeywell COM unit and Mode S transponder · Bombardier BD-700-1A10, BD-700-1A11, 550 and 26 more. Effective Oct 17, 2006
- [AD 2006-16-17](https://openairdocs.org/ad/2006-16-17): Torque values of the screws that attach the seat tracks · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Sep 25, 2006
- [AD 2006-07-01](https://openairdocs.org/ad/2006-07-01): Horizontal stabilizer control unit (HSCU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective May 1, 2006
- [AD 2006-03-06](https://openairdocs.org/ad/2006-03-06): Pilot's and co-pilot's seat tracks · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 13, 2006
- [AD 2005-25-17](https://openairdocs.org/ad/2005-25-17): Auxiliary power unit (APU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 18, 2006
- [AD 2005-24-11](https://openairdocs.org/ad/2005-24-11): Elevator gust lock system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jan 9, 2006
- [AD 2005-24-02](https://openairdocs.org/ad/2005-24-02): Airplane flight manual (AFM) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 28, 2005
- [AD 2005-23-20](https://openairdocs.org/ad/2005-23-20): Auxiliary power unit (APU) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 27, 2005
- [AD 2005-23-13](https://openairdocs.org/ad/2005-23-13): Nose landing gear (NLG) wheel · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Dec 19, 2005
- [AD 2005-22-08](https://openairdocs.org/ad/2005-22-08): Total air temperature (TAT) sensor heating system · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Nov 30, 2005
- [AD 2005-20-37](https://openairdocs.org/ad/2005-20-37): Main landing gear (MLG) trailing arms and integrity of the MLG pivot axle sealant. · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Nov 16, 2005
- [AD 2005-14-02](https://openairdocs.org/ad/2005-14-02): Left and right engine fire handles · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Aug 15, 2005
- [AD 2005-14-03](https://openairdocs.org/ad/2005-14-03): Engine-driven hydraulic pump · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Aug 10, 2005
- [AD 2005-13-22](https://openairdocs.org/ad/2005-13-22): Electric fuel pumps · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Jul 7, 2005
- [AD 2005-05-09](https://openairdocs.org/ad/2005-05-09): Forward upper liners · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Apr 14, 2005
- [AD 2005-04-05](https://openairdocs.org/ad/2005-04-05): Air turbine starter (ATS) · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Mar 24, 2005
- [AD 2005-01-05](https://openairdocs.org/ad/2005-01-05): Nose Landing Gear Wheel Nuts and Associated Inner and Outer Seals, and Reidentifying the Landing Gear Strut · Embraer EMB-135BJ (Legacy 600), EMB-135ER, EMB-135KE and 9 more. Effective Feb 9, 2005

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

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

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

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

All 120: https://openairdocs.org/aircraft/N16981/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 N16981.

## FAA accident and incident reports

None matched to N16981.

## Service difficulty reports (113, 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 ASOA2019042635062](https://openairdocs.org/sdr/ASOA2019042635062), Apr 23, 2019: INVERTER. INOPERATIVE. DURING MX INSPECTION THE EMERGENCY SIGN IN FRONT OF 3C WAS INOP.MX REMOVED BAD #3 INVERTER AND INSTALLED NEW INVERTER IAW EMB145 AMMII 33-50-11, OPS CHECK GOOD 
- [SDR ASOA201902274010](https://openairdocs.org/sdr/ASOA201902274010), Feb 27, 2019: COFFEEMAKER. ODOR. PVD - FLIGHT 4870 THE CREW REPORTED A BURNED WIRE INSULATION SMELL COMING FROM COFFEE MAKER AREA, AND THAT THE SMELL WENT AWAY AFTER BOTH COFFEE MAKERS WERE TUR
- [SDR ASOA201901157009](https://openairdocs.org/sdr/ASOA201901157009), Jan 15, 2019: RIB. CRACKED. TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND THE RIGHT MLG RIB NR 5 CRACKED. MAINTENANCE R/R THE NR 5 RIB IAW ECTC ETD 2018-145-13565,REEF. TASKCARD-145-306 RH R
- [SDR ASOA201901157008](https://openairdocs.org/sdr/ASOA201901157008), Jan 15, 2019: BUSHING. WORN. TYS A/CIS IN C-CHECK WHEN THE INSPECTORS FOUND THE RT AND LT VERTICAL STAB BUSHINGS WORN. MAINTENANCE REAMED BOTH BUSHINGS AND INSTALLED THE OVERSIZED BUSHING A
- [SDR ASOA201901097006](https://openairdocs.org/sdr/ASOA201901097006), Jan 9, 2019: BUSHING. DAMAGED. RUDDER 1 2ND FROM BOTTOM ATTACH BRACKET UPPER HAT BUSHING DAMAGED. REMOVED BUSHINGS, REAMED HOLE, INSTALLED NEW OVERSIZE BUSHINGS. AIRCRAFT IN C CHECK.
- [SDR ASOA201901037002](https://openairdocs.org/sdr/ASOA201901037002), Jan 3, 2019: FRAME. CRACKED. A/C IS IN FOR A C-CHECK INSPECTION THE INSPECTORS FOUND A CRACKED FRAME ON THE LT SIDE OF THE DV WINDOW CUTOUT AT FR 12A-13. MAINTENANCE HAD TO REMOVE THE PAX D
- [SDR ASOA201901027001](https://openairdocs.org/sdr/ASOA201901027001), Jan 2, 2019: FRAME. CORRODED. TYS A/C IS IN FOR A C-CHECK INSPECTION WHEN INSPECTION FOUND CORROSION AT STRINGER 21R BETWEEN FRAMES 17 THRU 19. MAINTENANCE REPAIRED THE SECTION BETWEEN FRAME
- [SDR ASOA201802284014](https://openairdocs.org/sdr/ASOA201802284014), Feb 28, 2018: STOP. BROKEN. DURING A MAINTENANCE INSPECTION, THE PAX DOOR FWD LOWER DOOR STOP SEAT WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE STOP SEAT, RIGGED THE PAX DO
- [SDR ASOA201712224068](https://openairdocs.org/sdr/ASOA201712224068), Dec 22, 2017: CHARGER. INOPERATIVE. DURING CREW INSPECTION, THE EMERGENCY LIGHTS WOULD NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY CHARGER, OPS TESTED WITH NO D
- [SDR ASOA20170718008V](https://openairdocs.org/sdr/ASOA20170718008V), Jul 20, 2017: BATTERY. INOPERATIVE. DURING A ROUTINE CHECK, FOUND THAT SEVERAL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERIES NUMBER 3 AND 4 IAW AMM 33-50-04. THE AI
- [SDR ASOA201707135094](https://openairdocs.org/sdr/ASOA201707135094), Jul 13, 2017: BATTERY PACK. INOPERATIVE. DURING INSPECTION, THE EMERGENCY LIGHTS WERE DISCOVERED INOPERATIVE. MX REMOVED AND REPLACED THE NR 3 AND 4 EMERGENCY LIGHT BATTERY PACKS. OPS CHECKED GOOD. ACF
- [SDR ASOA201704043066](https://openairdocs.org/sdr/ASOA201704043066), Apr 4, 2017: SKIN. CRACKED. RIGHT REAR FUSELAGE SKIN CRACKED AROUND RIVETS AT FRAME 75, STRINGER 2R. DAMAGED AREA REPAIRED WITH DOUBLER IAW SRM 53-31-00.
- [SDR ASOA201703303064](https://openairdocs.org/sdr/ASOA201703303064), Mar 30, 2017: CHANNEL. CORRODED. SERVICE DOOR LOWER CHANNEL CORRODED. THE CHANNEL WAS REPLACED IAW SRM 51-40-02.
- [SDR ASOA201703293063](https://openairdocs.org/sdr/ASOA201703293063), Mar 29, 2017: FLOOR SUPPORT. CORRODED. REAR FUSELAGE FLOOR SUPPORT CORRODED. REPLACED IAW SRM 51-40-02.
- [SDR ASOA201703293062](https://openairdocs.org/sdr/ASOA201703293062), Mar 29, 2017: FLOOR SUPPORT. CORRODED. CABIN NR 1 FLOOR SUPPORT CORRODED. REPLACED IAW SRM 51-40-02.
- [SDR ASOA201703293061](https://openairdocs.org/sdr/ASOA201703293061), Mar 29, 2017: GUSSET. CORRODED. LEFT GUSSET CORRODED AROUND ANCHOR NUT BETWEEN FRAMES 16 AND 17. THE GUSSET WAS REPAIRED IAW SRM 53-21-10, ITEM 2, FIG 201.
- [SDR ASOA201703293060](https://openairdocs.org/sdr/ASOA201703293060), Mar 29, 2017: SEAT TRACK. CORRODED. CABIN LT INBOARD SEAT TRACK NR 1 CORRODED. LT INBOARD SEAT TRACK NR 1 REPLACED AS PER 53-01-06.
- [SDR ASOA20160718036](https://openairdocs.org/sdr/ASOA20160718036), Jul 18, 2016: WARNING MESSAGE. FALSE ACTIVATION. PILOT REPORTED EICAS MESSAGE FOR CARGO BAY SMOKE FOR 5 SECONDS, CLIMBING THROUGH 14000 FEET. MX PERFORMED OPS CHECK OF CARGO SMOKE DETECTION SYSTEM WITH NO DEFE
- [SDR ASOA20141208097](https://openairdocs.org/sdr/ASOA20141208097), Dec 8, 2014: FIRE DETECTOR. FAILED. THE CREW REPORTED A NR 2 ENGINE FIRE DETECT FAIL MESSAGE AFTER TAKEOFF. THE ACFT RETURNED TO ORD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND 
- [SDR ASOA20140601060](https://openairdocs.org/sdr/ASOA20140601060), Jun 1, 2014: INVERTER. INOPERATIVE. DURING MX INSPECTION THE AFT GALLEY EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MX R & R THE EMERGENCY LIGHT SYS INVERTER WITH OPS CHECK GOOD. ACFT WAS APPROVED 
- [SDR ASOA20130528053](https://openairdocs.org/sdr/ASOA20130528053), May 28, 2013: CONTROL VALVE. INOPERATIVE. CREW REPORTED ZERO BRAKE EFFECTIVENESS IN LT BRAKE DURING TAXI. MX R & R THE OTBD BRAKE CONTROL VALVE WITH OPS AND TAXI CHECK SUCCESSFUL. ACFT WAS APPROVED FOR 
- [SDR ASOA20130113225](https://openairdocs.org/sdr/ASOA20130113225), Jan 13, 2013: SEAT TRACK. CORRODED. NR 2 RT WALL SEAT TRACK SUPPORT IS CORRODED BEYOND LIMITS AFTER BLEND-OUT. CUT-OUT CORRODED SECTION, FABRICATED AND INSTALLED NEW SEAT TRACK SUPPORT.
- [SDR ASOA20130110223](https://openairdocs.org/sdr/ASOA20130110223), Jan 10, 2013: FRAME. CORRODED. ACFT IS IN FOR A C-CHECK INSPECTION, WHEN A LT SPLICE AT FRAME LBL 15 WAS FOUND CORRODED. MX R & R THE REINFORCEMENT SPLICE AT FRAME IAW SRM 51-20-03 AND 51-40-
- [SDR ASOA20130110222](https://openairdocs.org/sdr/ASOA20130110222), Jan 10, 2013: BRACE. CORRODED. ACFT IS IN FOR A C-CHECK INSPECTION, WHEN THE RT CROSSBRACE WAS FOUND BENT AND CORRODED AT FRAME 17. MX R & R THE CROSSBRACE IAW SRM 51-20-03 AND 51-40-02. ALL 
- [SDR ASOA20130110221](https://openairdocs.org/sdr/ASOA20130110221), Jan 10, 2013: SEAT TRACK. CORRODED. ACFT IN FOR A C-CHECK WHEN CORROSION WAS FOUND ON THE RT LONGITUDAL SEAT TRACK FROM FRAME 48 THRU 52. MX R & R THE SEAT TRACK SUPPORT IAW SRM 51-40-02. ALL WORK
- [SDR ASOA20130109218](https://openairdocs.org/sdr/ASOA20130109218), Jan 9, 2013: ANGLE. CORRODED. DURING A C-CHECK, CORROSION FOUND AROUND NUTPLATED AT THE BAGGAGE DOOR. MX R & R THE BAGGAGE DOOR INBD ANGLE IAW SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE
- [SDR ASOA20130109217](https://openairdocs.org/sdr/ASOA20130109217), Jan 9, 2013: SEAT TRACK. CORRODED. DURING C-CHECK INSPECTION, RT OTBD SEAT TRACK SUPPORT FOUND CORRODED AT FR 55. MX REMOVED THE RIVETS AND FABRICATED A NEW SUPPORT AND INSTALL IAW SRM 51-40-02 A
- [SDR ASOA20130109216](https://openairdocs.org/sdr/ASOA20130109216), Jan 9, 2013: CHANNEL. CORRODED. DURING C-CHECK, LEFT CHANNEL CROSSBEAM AT FRAME 18 WAS FOUND CORRODED. MX BLENDED CORROSION IAW SRM 51-10-03, PERFORMED HFEC, NO CRACKS FOUND AND WAS WITHIN LIM
- [SDR ASOA20130109213](https://openairdocs.org/sdr/ASOA20130109213), Jan 8, 2013: GUSSET. CORRODED. C-CHECK, GUSSET AT FR 17 WAS FOUND WITH MINOR CORROSION AROUND NUTPLATE. MX BLENDED CORROSION LEAVING REMAINING MATERIAL TO BE WITHIN LIMITS IAW SRM 53-21-10. A
- [SDR ASOA20130109212T](https://openairdocs.org/sdr/ASOA20130109212T), Jan 8, 2013: FRAME. CORRODED. C-CHECK, CORROSION FOUND AT FRAME 65 AT THE THRESHOLD. MX R & R THE LOWER SECTION OF FRAME 65IAW ETD 2012-145-018140. ALL WORK ACCOMPLISHED AND WILL BE RELEASED
- [SDR ASOA20130108211](https://openairdocs.org/sdr/ASOA20130108211), Jan 8, 2013: SUPPORT. CORRODED. ACFT IN FOR A C-CHECK, CHECK WHEN THE LT WALL SUPPORT HAD CORROSION ON THE LOWER SIDE OF SUPPORT AT FRAME 60. MX R & R THE LT WALL SUPPORT IAW SRM 51-40-02. ALL
- [SDR ASOA20130108210](https://openairdocs.org/sdr/ASOA20130108210), Jan 8, 2013: BEAM. CORRODED. ACFT IN FOR A C-CHECK, CHECK WHEN THE CARGO DOOR CUTOUT WAS FOUND. CORRODED ON THE THRESHOLD BETWEEN FRAMES 65 AND 68. MX BLENDED THE CORROSION IAW SRM 51-10-03
- [SDR ASOA20130108209](https://openairdocs.org/sdr/ASOA20130108209), Jan 8, 2013: SEAT TRACK. CORRODED. ACFT IN FOR A C-CHECK, WHEN THE NR 4 LT SEAT TRACK WAS FOUND CORRODED IN SEVERAL PLACES. BLENDED AREAS IAW SRM 51-10-03, THE OUT OF LIMIT AREAS IAW SRM 53-00-11
- [SDR ASOA20130105207](https://openairdocs.org/sdr/ASOA20130105207), Jan 4, 2013: SUPPORT. CORRODED. RT OTBD SEAT TRACK SUPPORT CORRODED ON LOWER FOOT. CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R SUPPORT.
- [SDR ASOA20130105206](https://openairdocs.org/sdr/ASOA20130105206), Jan 4, 2013: SUPPORT. CORRODED. NR 1 LEFT WALL SEAT TRACK SUPPORT CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R SUPPORT.
- [SDR ASOA20130105205](https://openairdocs.org/sdr/ASOA20130105205), Jan 4, 2013: GUSSET. CORRODED. GUSSET AT FRAME 65 TO 68 AT Y=-479 IS CORRODED BEYOND LIMITS. R & R GUSSET.
- [SDR ASOA20130105204](https://openairdocs.org/sdr/ASOA20130105204), Jan 4, 2013: STRUCTURE. CORRODED. FRAME 15 DIGITAL IS CORRODED BEYOND LIMITS. R & R DIGITAL.
- [SDR ASOA20130105203](https://openairdocs.org/sdr/ASOA20130105203), Jan 4, 2013: CHANNEL. CORRODED. PAX DOOR U CHANNEL CORRODED BEYOND LIMITS AFTER BLENDING. R & R U CHANNEL.
- [SDR ASOA20130105202](https://openairdocs.org/sdr/ASOA20130105202), Jan 4, 2013: SEAT TRACK. CORRODED. NR 3 LEFT ISLE SEAT TRACK GUSSET IS CORRODED OUT OF LIMITS AFTER BLENDING. R & R GUSSET.
- [SDR ASOA20130103201](https://openairdocs.org/sdr/ASOA20130103201), Jan 3, 2013: SILL. CORRODED. RIGHT SILL IS CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R SILL.
- [SDR ASOA20130103200](https://openairdocs.org/sdr/ASOA20130103200), Jan 3, 2013: ANGLE. CORRODED. LEFT ANGLE HAS CORROSION THAT IS OUT OF LIMITS AFTER BLEND OUT. R & R LEFT ANGLE.
- [SDR ASOA20130103199](https://openairdocs.org/sdr/ASOA20130103199), Jan 3, 2013: GUSSET. CORRODED. CORROSION AFT LAVATORY LT FLOOR GUSSET CORRODED OUT OF LIMITS AFTER BLENDING. R & R FLOOR GUSSET.
- [SDR ASOA20130103198](https://openairdocs.org/sdr/ASOA20130103198), Jan 3, 2013: SUPPORT. CORRODED. SUPPORT IN THE LAVATORY AREA HAS CORROSION OUT OF LIMITS AFTER BLENDING. REMOVED AND REPLACED DOUBLER.
- [SDR ASOA20130103197](https://openairdocs.org/sdr/ASOA20130103197), Jan 3, 2013: BRACE. CORRODED. RT CROSS BRACE IS CORRODED BEYOND LIMITS AFTER BLEND OUT. R & R BRACE.
- [SDR ASOA20130103196](https://openairdocs.org/sdr/ASOA20130103196), Jan 3, 2013: CHANNEL. CORRODED. PAX DOOR U-CHANNELS ARE CORRODED BEYOND LIMITS AFTER BLENDING. R & R CHANNELS.
- [SDR ASOA20121224194](https://openairdocs.org/sdr/ASOA20121224194), Dec 21, 2012: FLOOR SUPPORT. CORRODED. LT FLOOR SUPPORET CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R FLOOR SUPPORT.
- [SDR ASOA20121224193](https://openairdocs.org/sdr/ASOA20121224193), Dec 21, 2012: SILL. CORRODED. LAVATORY RT SILL IS CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R SILL.
- [SDR ASOA20121224192](https://openairdocs.org/sdr/ASOA20121224192), Dec 21, 2012: FLOOR SUPPORT. CORRODED. AFT LAV LT OMEGA BEAM IS CORRODED BEYOND LIMITS AFTER BLEND-OUT. REMOVED DAMAGED SECTION, FABRICATED A FILLER AND DOUBLER AND INSTALLED.
- [SDR ASOA20121224191](https://openairdocs.org/sdr/ASOA20121224191), Dec 21, 2012: SILL. CORRODED. LT SILL IS COORODED BEYOND LIMITS AFTER BLEND-OUT. R & R SILL.
- [SDR ASOA20121224190](https://openairdocs.org/sdr/ASOA20121224190), Dec 21, 2012: ANGLE. CORRODED. CORROSION OUT OF LIMITS AFTER BLEND-OUT AT FRM 68 RT SIDE AT Z=715.7. R & R TEE ANGLE.

All 113: https://openairdocs.org/aircraft/N16981/reports.md

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

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Embraer EMB-145LR)

- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST02176AT-D](https://openairdocs.org/stc/ST02176AT-D): Installation of a Teledyne Mini Flight Data Acquistion Unit. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST02216AT-D](https://openairdocs.org/stc/ST02216AT-D): Installation of Teledyne Mini Flight Data Acquisition Unit in a Provisioned EMB-135/145. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST02310AT](https://openairdocs.org/stc/ST02310AT): Installation of SAF-T-GLO photoluminescent floor proximity emergency escape path marking system (FPEEPMS). STG Aerospace Inc
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST01409LA](https://openairdocs.org/stc/ST01409LA): Installation of a reinforced cockpit door. Safran Cabin Inc
- [STC ST01984LA-D](https://openairdocs.org/stc/ST01984LA-D): Modification and installation of passenger seats, passenger service units and filler panels, seat track covers, and seat row placards. Safran Cabin Inc
- [STC ST04219NY](https://openairdocs.org/stc/ST04219NY): Installation of SpaceX Starlink Aviation System. Aerospace Design & Compliance LLC
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST00640DE](https://openairdocs.org/stc/ST00640DE): Installation of Tropospheric Airborne Meteorolocigal Data Reporting System (TAMDAR). FLYHT Inc
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST04159CH](https://openairdocs.org/stc/ST04159CH): Upgrade of Honeywell Primus II Communications Units RCZ-8XX Transponders to support Certification of Automatic Dependent Surveillance -Broadcast (ADS-B) Out. CMD Flight Solutions LLC
- [STC ST04527CH](https://openairdocs.org/stc/ST04527CH): Installation of a 16 passenger configuration. C&L STC Holdings LLC
- [STC ST04177NY](https://openairdocs.org/stc/ST04177NY): Installation of ALI LED Cabin Lighting, Cabin and Crew AC Power Outlets, LH Fwd Closet and Misc Cabin Mods. C & L STC Holdings LLC
- [STC ST01983WI](https://openairdocs.org/stc/ST01983WI): Installation of a folding stair in the main entrance for models equipped with a side-hinged main door. Worldwide Aviation Engineering LLC
- [STC ST04212NY](https://openairdocs.org/stc/ST04212NY): Installation of Universal UNS-1Lw Flight Management System. C&L Engineering Services, LLC
- [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC ST04213NY](https://openairdocs.org/stc/ST04213NY): PAX Social Distance Floorplan Reconfiguration. C&L Engineering Services LLC
- [STC ST04281AT](https://openairdocs.org/stc/ST04281AT): Installation for the Upgrade of the NZ-2000 FMS computer for software version NZ6. Chippewa Aerospace Inc
- [STC ST03158CH-D](https://openairdocs.org/stc/ST03158CH-D): Installation of a Reconfiguration of a Cabin Floorplan. Standard Aero Business Aviation Services LLC
- [STC SA9087SC-D](https://openairdocs.org/stc/SA9087SC-D): RECORE® Hamilton Sundstrand heat exchanger, P/N 816630-1 / -2 in accordance with Honeywell LORI Sealed Drawing List SDL3869-1 Rev. A, dated June 7, 2005 or later FAA approved revision. Honeywell International Inc
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST01039DE](https://openairdocs.org/stc/ST01039DE): Passenger seating arrangement for 30 or less passengers. Deluxe Public Charter LLC
- [STC ST04537NY](https://openairdocs.org/stc/ST04537NY): Installation of Air Filtration. Kilroy Aviation LLC
- [STC ST09858SC](https://openairdocs.org/stc/ST09858SC): Installation of cabin automatic coffee brewing system. Safran Cabin Germany Gmbh
- [STC ST04255CH](https://openairdocs.org/stc/ST04255CH): Installation of an Automatic Dependent Surveillance-Broadcast (ADS-B Out) System. ENVOY AIR
- [STC ST03420NY](https://openairdocs.org/stc/ST03420NY): Installation of a Cabin Interior. Delta Engineering Corporation
- [STC ST02327LA](https://openairdocs.org/stc/ST02327LA): Installation of replacement proximity sensor harness assembly part numbers used on the nose and main landing gears. Safran Electrical Components USA Inc
- [STC ST04423NY](https://openairdocs.org/stc/ST04423NY): Installation of ADS-B Out. FTI Engineering Nework GmbH
- [STC ST00015IB](https://openairdocs.org/stc/ST00015IB): Installation of a Honeywell HF Communication System, model KHF 1050, with provisions for a dual installation. Embraer Engineering & Technology Center - USA Inc
- [STC ST00014IB](https://openairdocs.org/stc/ST00014IB): Installation of a second Honeywell HF Communication System, model KHF 1050. Embraer Engineering & Technology Center - USA Inc
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST04333NY](https://openairdocs.org/stc/ST04333NY): Installation of sat: Tglo® Photolumincsccnt Aisle Path Marking System. STG Aerospace Ltd
- [STC ST10550SC](https://openairdocs.org/stc/ST10550SC): Installation of a WeatherMASTER X-Band Fuselage Nose Radome Assembly. The NORDAM Group LLC
- [STC ST04316CH](https://openairdocs.org/stc/ST04316CH): Installation of a Smartsky System in accordance with StandardAero Master Data List 1034570, Revision (C), dated March 23, 2019 or later FAA approved revision. StandardAero Business Aviation Services LLC
- [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST000081B](https://openairdocs.org/stc/ST000081B): Installation of a second SELCAL channel. EMBRAER - Empresa Brasileira de Aeronautica
- [STC ST00008IB](https://openairdocs.org/stc/ST00008IB): Installation of a second SELCAL channel. EMBRAER - Empresa Brasileira de Aeronautica
- [STC ST03177NY](https://openairdocs.org/stc/ST03177NY): Installation of a Honeywell ADS-B (Out), EHS and FreeFlight GPS. Delta Engineering Corporation
- [STC ST01520WI](https://openairdocs.org/stc/ST01520WI): Installation of the Concorde RG-442 VRSLA Battery and Temperature Sensor in place of the original Nickel-Cadmium Battery. Concorde Battery Corporation
- [STC ST00361BO](https://openairdocs.org/stc/ST00361BO): Installation of a Honeywell Primus II (XS-852) ADS-B Out System. Pro Star Aviation, LLC
- [STC ST04282CH](https://openairdocs.org/stc/ST04282CH): Installation of Honeywell CD-830 Control Display Unit (CDU). Nextant Aerospace
- [STC ST01702WI](https://openairdocs.org/stc/ST01702WI): Change seating configuration to 30 passengers by removal of seats. Worldwide Aircraft Engineering LLC
- [STC ST04108CH](https://openairdocs.org/stc/ST04108CH): Installation of Gogo Business Aviation ATG-8000 High Speed Internet with Wireless Local Area Network (WLAN). Nextant Aerospace
- [STC ST04367AT](https://openairdocs.org/stc/ST04367AT): Removal of the Existing Honeywell DL-900 or DL-950 Data Loader and Installation of the Honeywell DL-1000 Data Loader. Chippewa Aerospace Inc
- [STC ST04190AT](https://openairdocs.org/stc/ST04190AT): Installation of an ADS-B Out. Chippewa Aerospace Inc
- [STC ST02406LA](https://openairdocs.org/stc/ST02406LA): Installation of TCAS version 7.1. Aviation Communication and Surveillance Systems (ACSS) LLC

All 75: https://openairdocs.org/aircraft/N16981/stcs.md

## Earlier aircraft with N16981

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N16981 before.

- [Cancelled 1988-09-22](https://openairdocs.org/deregistered/N16981-1988-09-22): Bell 206B, S/N 2347. Triennial form not returned

## Related

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

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