# N29917: 2001 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: 145414
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 21, 2001
- Certificate issued: January 27, 2023
- Expires: January 31, 2030
- Mode S code: A31984
- 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=29917
- Page: https://openairdocs.org/aircraft/N29917

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/N29917/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 (1)

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

- [NTSB NYC01IA107](https://openairdocs.org/ntsb/NYC01IA107), Apr 25, 2001: Embraer EMB-145 (N29917), Norfolk, VA, incident, no damage. Probable cause: The manufacturer's inadequate quality control, which resulted in a jammed elevator trim actuator.

## NTSB investigations on N29917 not matched to an aircraft (1)

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

- [NTSB SEA83AA176](https://openairdocs.org/ntsb/SEA83AA176), Aug 13, 1983: Fairchild Hiller FH-1100 (N29917), Toutle, WA, destroyed, 5 fatal

## FAA accident and incident reports (2)

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 20110324003819I](https://openairdocs.org/incident/20110324003819I), Mar 24, 2011: Embraer EMB-145LR (N29917), Cleveland, OH, No damage. Flight number bta 2043 (N29917), reported a possible engine fire after landing runway 6L. The aircraft pulled off onto taxiway k, where the passengers deplaned…
- [Incident 20010425013839I](https://openairdocs.org/incident/20010425013839I), Apr 25, 2001: Emb EMB145 (N29917), Norfolk, VA. (-23) The captain reported that en route from ewr to orf, the "auto trim fail" and the "pit trim #1 fail" icas captions illuminated, and approx. 15 minutes…

## Reports on N29917 not matched to an aircraft (2)

They name N29917, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Accident 19830813040689A](https://openairdocs.org/incident/19830813040689A), Aug 13, 1983: Hiller FH1100 (N29917), Castle Rock, WA, Destroyed, 4 fatal. Sightseeing helicopter crashed into a densely forested area and burned. No witnesses. No engine defects found.
- [Incident 19820923054069I](https://openairdocs.org/incident/19820923054069I), Sep 23, 1982: Frchld FH1100 (N29917), Kelso, WA, Minor damage. Allowed tail rotor to hit ground on autorotation flare, over controlled, landed sideways, collapsing a skid.

## Service difficulty reports (73, 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 ASOA201907125085](https://openairdocs.org/sdr/ASOA201907125085), Jul 12, 2019: INVERTER. INOPERATIVE. DURING MX INSPECTION THE AFT EMERGENCY LIGHT STRIPS 6,7, AND 8 INOP. MX R&R #6 INVERTER WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201903157032](https://openairdocs.org/sdr/ASOA201903157032), Mar 15, 2019: SKIN. DENTED. TYS A/C IS IN C-CHECK WHEN A FUR 5700-01510,DEFECT BO27891 RT L/E 1 WAS DENTED AND REQUIRED A PERMANENT REPAIR. MAINTENANCE CUT OUT THE DAMAGE AREA ,FABRICATED 
- [SDR ASOA201706064042](https://openairdocs.org/sdr/ASOA201706064042), Jun 6, 2017: DISPLAY. SHORTED. THE CREW REPORTED THAT EICAS FAIL IN FLIGHT WITH ODOR OF BURNING ELECTRICAL. THE AIRCRAFT DIVERTED WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE A
- [SDR ASOA201701305009](https://openairdocs.org/sdr/ASOA201701305009), Jan 30, 2017: UNKNOWN. ODOR. PILOT REPORTED BURNING ODOR COMING FROM GALLEY ABOVE THE COFFEE POTS. MX PERFORMED OPERATIONAL CHECK OF COFFEEMAKERS WITH NO BURNING ODOR NOTED AT THIS TIME. AC
- [SDR ASOA20160423021](https://openairdocs.org/sdr/ASOA20160423021), Apr 23, 2016: FITTING. CRACKED. DURING C-CHECK, THE RT ENGINE LOWER FWD MOUNT YOKE FITTING WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE FITTING IAW EC5450-01199. THE ACFT WAS APPROVED FOR RE
- [SDR ASOA20160408017V](https://openairdocs.org/sdr/ASOA20160408017V), Apr 8, 2016: SKIN. CRACKED. DURING C-CHECK THE LT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS AT FRAME 75 STR 1L-2L. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5330-03099. THE ACFT
- [SDR ASOA20160408016](https://openairdocs.org/sdr/ASOA20160408016), Apr 8, 2016: SKIN. CRACKED. DURING C-CHECK THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS AT FRAME 75 AND STRINGERS 2R-3R. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5330-03099
- [SDR ASOA20150730041](https://openairdocs.org/sdr/ASOA20150730041), Jul 30, 2015: OIL SYSTEM. LEAKING. CREW REPORTED AN OIL ODOR COMING FROM NR 1 ENGINE BLEED. MAINTENANCE R & R NR 1 ENGINE. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150726041](https://openairdocs.org/sdr/ASOA20150726041), Jul 26, 2015: DUCT. DIRTY. THE CREW REPORTED A VERY STRONG ODOR OF OIL IN FLIGHT. STRONGER IN DESCENT. MAINTENANCE INSPECTED AND CLEANED AIR DUCTS IAW 21-20-00. NO ODOR WAS NOTED AND ACFT
- [SDR ASOA20140807086](https://openairdocs.org/sdr/ASOA20140807086), Aug 6, 2014: FLASHLIGHT. INOPERATIVE. CREW REPORTED THE AFT CABIN FLASHLIGHT WAS INOPERATIVE. INTIALLY WAS PLACED ON MEL 25-60-05. MAINTENANCE R & R THE FLASHLIGHT WITH OPS CHECK GOOD. ACFT WAS APPR
- [SDR ASOA20140624143](https://openairdocs.org/sdr/ASOA20140624143), Jun 24, 2014: GUSSET. CORRODED. DURING C-CHECK, CORROSION WAS FOUND AROUND TWO NUTPLATES ON CENTER OMEGA BEAM GUSSET, Y-0.0, BETWEEN FRAMES 14 & 18. R & R GUSSET IAW SRM 51-40-02. THE ACFT WAS
- [SDR ASOA20140624142](https://openairdocs.org/sdr/ASOA20140624142), Jun 24, 2014: THRESHOLD. CORRODED. DURING C-CHECK, CARGO DOOR THRESHOLD FOUND CORRODED AT NUTPLATE HOLES. MAINTENANCE R & R THRESHOLD IAW SRM 51-40-02 AND CPM 51-21-04. THE ACFT WAS APPROVED FOR 
- [SDR ASOA20140520088V](https://openairdocs.org/sdr/ASOA20140520088V), May 20, 2014: NUT PLATE. CORRODED. DURING C-CHECK, CORROSION AROUND TWO NUTPLATES ON CENTER OMEGA BEAM GUSSET , Y-0.0, BETWEEN FRAMES 14 AND 18 AS MARKED IN CENTER FUSELAGE I. MAINTENANCE R & R G
- [SDR ASOA20140520087](https://openairdocs.org/sdr/ASOA20140520087), May 20, 2014: THRESHOLD. CORRODED. DURING C-CHECK, CARGO DOOR THRESHOLD HAS CORROSION, AT NUTPLATES HOLES. R & R CARGO DOOR THRESHOLD IAW SRM 51-40-02 AND CPM 51-21-04. THE ACFT WAS APPROVED FOR 
- [SDR ASOA20140517086V](https://openairdocs.org/sdr/ASOA20140517086V), May 17, 2014: FLOOR SUPPORT. CORRODED. DURING C-CHECK, RT FLOOR SUPPORT AT FRAME 53 HAS CORROSION. MAINTENANCE R & R RT FLOOR SUPPORT IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140517085V](https://openairdocs.org/sdr/ASOA20140517085V), May 17, 2014: FLOOR SUPPORT. CORRODED. DURING C-CHECK, CORROSION AROUND NUTPLATE ON CENTER OMEGA BEAM, Y=0.0, GUSSET AT FRAME 20. MAINTENANCE BLENDED CORROSION AROUND NUTPLATE ON CENTER OMEGA BEAM GU
- [SDR ASOA20140517084](https://openairdocs.org/sdr/ASOA20140517084), May 17, 2014: FLOOR SUPPORT. CORRODED. DURING C-CHECK RT FLOOR SILL IN CARGO AREA FRAMES 61-63 IS CORRODED. MAINTENANCE R & R FLOOR SILL AND SPLICE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN 
- [SDR ASOA20140517083](https://openairdocs.org/sdr/ASOA20140517083), May 17, 2014: FLOOR SUPPORT. CORRODED. DURING C-CHECK, CORROSION AROUND NUTPLATE BOTH NUTPLATES ON GUSSETT AT RT OMEGA BEAM, Y+479.0, FRAME 22. MAINTENANCE DETERMINED CORROSION AROUND NUTPLATE HAS 10
- [SDR ASOA20140517082](https://openairdocs.org/sdr/ASOA20140517082), May 17, 2014: FLOOR SUPPORT. CORRODED. DURING C-CHECK, FOUND CORROSION AROUND NUTPLATE ON GUSSETT RT OMEGA BEAM, Y=479.0, FRAME 20. MAINTENANCE DETERMINED CORROSION AROUND NUTPLATE IN GUSSETT IS 100 
- [SDR ASOA20140517081](https://openairdocs.org/sdr/ASOA20140517081), May 17, 2014: FLOOR SUPPORT. CORRODED. DURING C-CHECK LAVATORY UNDER FLOOR OMEGA BEAM CAP IS CORRODED, LOCAL LEVEL 2, AS MARKED ON RT SIDE AROUND NUTPLATE. MAINTENANCE BLENDED CORROSION AROUND NUTPLA
- [SDR ASOA20140517080V](https://openairdocs.org/sdr/ASOA20140517080V), May 16, 2014: FIREWALL. CRACKED. DURING C-CHECK, THE APU FIREWALL WAS FOUND TO BE CRACKED INBD OF STRINGER 12L WHERE THE APU CONTROL HARNESS CONNECTS. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW
- [SDR ASOA20140517079V](https://openairdocs.org/sdr/ASOA20140517079V), May 16, 2014: FLOORBEAM. CORRODED. DURING C-CHECK THE CENTER AISLE CROSSBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO
- [SDR ASOA20140517078](https://openairdocs.org/sdr/ASOA20140517078), May 16, 2014: SHEAR TIE. CORRODED. DURING C-CHECK THE FRAME 65 SHEAR CLIP WAS FOUND TO BE CORRODED BETWEEN STRINGERS 15-16L. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A SPLICE REPAIR IAW SR
- [SDR ASOA20140517077](https://openairdocs.org/sdr/ASOA20140517077), May 16, 2014: FRAME. CORRODED. DURING C-CHECK, FRAME 65 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 16-17L. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-31-04. T
- [SDR ASOA20140516074](https://openairdocs.org/sdr/ASOA20140516074), May 16, 2014: BEARING CAP. CORRODED. DURING C-CHECK CORROSION FOUND ON LT AND RT NLG BEARING CAPS. MAINTENANCE REPLACED LT AND RT NLG BEARING CAPS AND SHIMMED IAW AMM 32-20-01, FOR INSTALLATION SEE
- [SDR ASOA20140516073](https://openairdocs.org/sdr/ASOA20140516073), May 16, 2014: PARTITION. CORRODED. DURING C-CHECK CORROSION ON RT WALL DOUBLER AT FRAME 61 AT FLOOR LEVEL. MAINTENANCE DETERMINED CORROSION 100 PERCENT MATERIAL LOSS, REMOVED WALL DOUBLER, LOCATE
- [SDR ASOA20140516072](https://openairdocs.org/sdr/ASOA20140516072), May 16, 2014: FLOOR SUPPORT. CORRODED. DURING C-CHECK LAVATORY UNDER FLOOR OMEGA BEAM CAP IS CORRODED AS MARKED ON LT SIDE AROUND NUT PLATE. MAINTENANCE DETERMINED CORROSION ON OMEGA BEAM CAP LT SIDE
- [SDR ASOA20140516071](https://openairdocs.org/sdr/ASOA20140516071), May 16, 2014: FLOOR SUPPORT. CORRODED. DURING C-CHECK, CARGO UNDERFLOOR SUPPORT 65-68 LT SIDE UNDER FLOORBOARD 271FF HAS CORROSION. MAINTENANCE R & R FLOOR SUPPORT IAW SRM 51-40-02 AND 53-31-10. ACFT
- [SDR ASOA20140516070V](https://openairdocs.org/sdr/ASOA20140516070V), May 16, 2014: PARTITION. DAMAGED. DURING C-CHECK, BOTH SHOT BOLT HOLES FOR LT COCKPIT PARTION ARE ELONGATED. MAINTENANCE REMOVED CHAFED UPPER PIN GUIDE FABRICATED, LOCATED AND DRILLED UPPER PIN 
- [SDR ASOA20140516069](https://openairdocs.org/sdr/ASOA20140516069), May 16, 2014: STRINGER. CRACKED. DURING C-CHECK, STRINGER 3L AT FRAME 20 IS CRACKED. MAINTENANCE R & R STRINGER IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140516068](https://openairdocs.org/sdr/ASOA20140516068), May 16, 2014: ACCESS PANEL. CORRODED. DURING C-CHECK RT WING ACCESS PANEL 532AB FOUND CORRODED ON BACKSIDE AROUND FASTENER HOLES. MAINTENANCE BLENDED CORROSION AND REMAINED WITHIN ALLOWABLE LIMITS I
- [SDR ASOA20140516067](https://openairdocs.org/sdr/ASOA20140516067), May 16, 2014: ACCESS PANEL. CORRODED. DURING C-CHECK, RT WING ACCESS PANEL 632AB FOUND CORRODED ON BACKSIDE AROUND FASTENER HOLES. MAINTENANCE BLENDED CORROSION. REMAINED WITHIN ALLOWABLE LIMITS IAW
- [SDR ASOA20140516066V](https://openairdocs.org/sdr/ASOA20140516066V), May 16, 2014: FRAME. BROKEN. DURING C-CHECK, FRAME 10 BENEATH CO-PILOT'S DV WINDOW BROKEN. MAINTENANCE REMOVED BROKEN FRAME 10, LOCATED, DRILLED, ALODINED, AND INSTALLED NEW FRAME 10 IAW SR
- [SDR ASOA20140516065](https://openairdocs.org/sdr/ASOA20140516065), May 16, 2014: FRAME. BROKEN. FRAME 10 BENEATH PILOT'S DV WINDOW BROKEN. MAINTENANCE REMOVED BROKEN FRAME 10, LOCATED, DRILLED, ALODINED AND INSTALLED NEW FRAME 10 IAW SRM 53-00-04, 51-40-02
- [SDR ASOA20131104079](https://openairdocs.org/sdr/ASOA20131104079), Nov 4, 2013: CHECK VALVE. LEAKING. THE CREW REPORTED FUEL LEAK ON TAKOFF FOR FIRST FIVE MINUTES THEN WHEN AT 10,000 FT AND REDUCED PITCH NO LEAK WAS NOTICED. MAINTENANCE INSPECTED AND REPLACED TH
- [SDR ASOA06012013316](https://openairdocs.org/sdr/ASOA06012013316), Jun 1, 2013: YOKE. CRACKED. ACFT WAS IN FOR A 5A CHECK, WHEN INSPECTION FOUND NTHE LT FWD LWR ENGINE YOKE CRACKED. MX R & R THE ENGINE YOKE IAW EC 5450-01013. ALL WORK WAS ACCOMPLISHED AND
- [SDR ASOA20130221015](https://openairdocs.org/sdr/ASOA20130221015), Feb 21, 2013: CONTROL MODULE. ODOR. ELECTRICAL BURNING ODOR REPORTED COMING FROM FRONT OF CABIN. R & R THE PASSENGER CABIN LIGHTS CONTROL MODULE ASSY WITH OPS CHECK SUCCESSFUL. ACFT WAS APRROVED F
- [SDR ASOA201302150101](https://openairdocs.org/sdr/ASOA201302150101), Feb 15, 2013: WIRE HARNESS. FAULTY. THE CREW REPORTED A ELECTRICAL BURN ODOR COMING FROM SEAT 1A AREA. MX INSPECTED AND FOUND LIGHT SOCKET SHORTED OUT AT LOCATION SIDEWALL PANEL ABOVE SEAT 1A. THE
- [SDR C2XA11IA109](https://openairdocs.org/sdr/C2XA11IA109), Jun 10, 2011: OUTFLOW VALVE. MALFUNCTIONED. DURING CRUISE THE CREW REPORTED THAT THE AUTO-PRESSURIZATION FAILED AND DECLARED AN EMERGENCY. DIVERTING TO AEX WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAIN
- [SDR C2XA11IA108](https://openairdocs.org/sdr/C2XA11IA108), Jun 10, 2011: OUTFLOW VALVE. INTERMITTENT. DURING CRUISE THE CREW REPORTED THAT THE AUTO-PRESSURIZATION FAILED AND DECLARED AN EMERGENCY DIVERTING TO AEX WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINT
- [SDR C2XA11CL079](https://openairdocs.org/sdr/C2XA11CL079), Mar 24, 2011: KEY. SHORTED. CLE FLT 2043 - THE CREW REPORTED A NR 1 ENGINE FIRE INDICATION ON LANDING. THE CREW FOLLOWED MEMORY ITEMS THEN QRH. MESSAGE REMAINED AND EVSC PROCEDURE WAS FOLL
- [SDR C2XA11SH063](https://openairdocs.org/sdr/C2XA11SH063), Mar 11, 2011: SKIN PANEL. DAMAGED. AC N29917 FERRIED INTO SHV BECAUSE OF GROUND DAMAGE BY LAVATORY TRUCK. SKIN PANEL AT FRAME 61-66 STRINGER 16R TO 19L HAS DAMAGE. FERRY FLIGHT CONDITIONS WERE TO
- [SDR C2XA1`0IA283](https://openairdocs.org/sdr/C2XA1%600IA283), Nov 8, 2010: AHRS. INOPERATIVE. IAH - FLIGHT 2945, THE CREW REPORTED A AHRS NR 1 FAIL MESSAGE IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND 
- [SDR C2XA10IA187](https://openairdocs.org/sdr/C2XA10IA187), Jul 4, 2010: SELECTOR. OUT OF POSITION. MTY - FLIGHT 2151DURING CLIMB THE CREW RECEIVED A LANDING GEAR DISAGREE MESSAGE AND THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT DIVERTED TO NTY WHERE THE A
- [SDR C2XA10SH223](https://openairdocs.org/sdr/C2XA10SH223), Jun 29, 2010: SKIN. CRACKED. SHV - DURING C CHECK THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS (4 EACH) BETWEEN FRAMES 78-79 AND STRINGERS 3L-5L. MAINTENANCE REMOVED THE CRACKS 
- [SDR C2XA10SH222](https://openairdocs.org/sdr/C2XA10SH222), Jun 29, 2010: BEAM. CORRODED. SHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE
- [SDR C2XA10SH200](https://openairdocs.org/sdr/C2XA10SH200), Jun 10, 2010: RELAY. FAILED. AIRCRAFT 29917 - FLT 2056 IAH-MCI DIVERT TO SHV - WING ANTI-ICE FAIL MSG DURING TEST. FLIGHT DIVERTED DURING CRUISE. SHV MAINTENANCE REMOVED AND REPLACED RELAY 
- [SDR C2XA10RI069](https://openairdocs.org/sdr/C2XA10RI069), May 24, 2010: HOSE. LEAKING. FLIGHT 2038 - EWR - FLIGHT CREW REPORTED PACK NR 2 FAIL IN CLIMB. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED PACK HOSE 
- [SDR C2XA10IA056](https://openairdocs.org/sdr/C2XA10IA056), Feb 7, 2010: BATTERY. OVERTEMP. IAH - FLIGHT 2705, DURING TAKEOFF THE CREW REPORTED A BATTERY ONE OVERTEMP INDICATION. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANC
- [SDR C2XA09IA327](https://openairdocs.org/sdr/C2XA09IA327), Dec 26, 2009: STRUT. LOW. IAH - FLIGHT 2573, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AND A ENG 1-2 REV DISAGREE MESSAGE ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT L

All 73: https://openairdocs.org/aircraft/N29917/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/N29917/stcs.md

## Earlier aircraft with N29917

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N29917 before.

- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N29917-undated): Fairchild Hiller FH-1100, S/N 57. 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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