# N13988: 2000 Embraer EMB-145LR

- Status: Valid registration
- Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212, 55 seats)
- Engine: [Allison AE3007C series](https://openairdocs.org/engine/allison-ae3007c-series) (registry code 03028)
- 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: 145265
- Year built: 2000
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 27, 2000
- Certificate issued: August 18, 2022
- Expires: August 31, 2029
- Mode S code: A0A031
- 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=13988
- Page: https://openairdocs.org/aircraft/N13988

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Allison AE3007C model are included.

## ADs that may apply (OpenAirDocs): 102 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 AE3007C series)

- [AD 2017-26-06](https://openairdocs.org/ad/2017-26-06): Turbine/turboprop Engine, Turbine · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 7 more. Effective Jan 31, 2018
- [AD 2017-11-05](https://openairdocs.org/ad/2017-11-05): Turbine/ turboprop Engine, Turbine Section · Rolls-Royce AE 3007C and AE 3007C1. Effective Jul 18, 2017
- [AD 2015-02-08](https://openairdocs.org/ad/2015-02-08): Turbine wheels · Rolls-Royce AE 2100D2, AE 2100D2A, AE 2100D3 and 11 more. Effective Mar 11, 2015
- [AD 2009-24-04](https://openairdocs.org/ad/2009-24-04): Fan spinner · Rolls-Royce AE 3007A1, AE 3007A1E, AE 3007A1P and 5 more. Effective Dec 28, 2009
- [AD 2007-24-05](https://openairdocs.org/ad/2007-24-05): Engine oil temperature · Rolls-Royce AE 3007A, AE 3007A1, AE 3007A1/1 and 8 more. Effective Jan 2, 2008
- [AD 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 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 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 113: https://openairdocs.org/aircraft/N13988/ads.md

## Information bulletins (advisory) (9 in force)

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021
- [SAIB AIR-20-17](https://openairdocs.org/saib/AIR-20-17): Air Conditioning - Cabin Pressure Control System. Issued Nov 3, 2020
- [SAIB NM-19-17](https://openairdocs.org/saib/NM-19-17): Ice and Rain Protection: Electrical Wiring Terminations at Pitot and TAT Relays. Issued Dec 5, 2019
- [SAIB NM-10-13](https://openairdocs.org/saib/NM-10-13): Navigation: Flight Management System. Issued Jan 7, 2010
- [SAIB NM-09-03](https://openairdocs.org/saib/NM-09-03): Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations. Issued Dec 11, 2008
- [SAIB NM-08-15](https://openairdocs.org/saib/NM-08-15): Instruments: Contamination of the Attitude Heading Reference System (AHRS) Computers. Issued Mar 26, 2008
- [SAIB NM-07-40](https://openairdocs.org/saib/NM-07-40): Embraer EMB-135/145 Landing Gear Incident. Issued Jul 9, 2007
- [SAIB NM-07-20](https://openairdocs.org/saib/NM-07-20): Flight Data Recorders. Issued Mar 21, 2007
- [SAIB NE-11-22](https://openairdocs.org/saib/NE-11-22): Engine Controls. Issued Feb 23, 2011
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations

None matched to N13988.

## FAA accident and incident reports

None matched to N13988.

## Service difficulty reports (127, 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 ASOA201906117059](https://openairdocs.org/sdr/ASOA201906117059), Jun 11, 2019: HANDLE. CRACKED. A/C WAS IN C-CHECK WHEN INSPECTION FOUND THE R/H COCKPIT GRAB HANDLE CRACKED FWD. OF FUSELAGE II. MAINTENANCE REPAIRED AREA IAW ETD 2019-145-074630 BY REMOVING 
- [SDR ASOA201906117058](https://openairdocs.org/sdr/ASOA201906117058), Jun 11, 2019: FITTING. CRACKED. A/C WAS IN C-CHECK WHEN INSPECTION FOUND THE RT OUTBOARD FLAP INBD SIDE FITTING CRACKED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALL A DOUBLER REIN-ENFORCE
- [SDR ASOA201906087055](https://openairdocs.org/sdr/ASOA201906087055), Jun 7, 2019: WINDOW POST. CRACKED. L/H WINDSHIELD LATERAL POST CRACKED AT UPPER O/B CORNER AROUND RIVET. REMOVED RIVETS, BOLTS AND SUPPORTS TO FACILITATE INSTALLATION OF REINFORCEMENT FOR L/H WIN
- [SDR ASOA201906087056](https://openairdocs.org/sdr/ASOA201906087056), Jun 6, 2019: WINDOW POST. CRACKED. L/H FUSELAGE WINDSHIELD REINFORCEMENT PILLAR 2 SKIN HOLES FOUND CRACKED. REMOVED AND REPLACED L/H FUSELAGE WINDSHIELD REINFORCEMENT PILLAR. AIRCRAFT STILL IN C 
- [SDR ASOA201905317054](https://openairdocs.org/sdr/ASOA201905317054), May 31, 2019: FLOOR SUPPORT. CORRODED. TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND CORROSION ON THE RT OMEGA BEAM FORWARD OF NUT PLATE. MAINTENANCE CUTOUT THE CORROSION AND FABRICATED AN EXTERNAL DOU
- [SDR ASOA201905317053](https://openairdocs.org/sdr/ASOA201905317053), May 31, 2019: FLOOR SUPPORT. CORRODED. TYS A/CIS IN C-CHECK WHEN INSPECTION FOUND CORROSION AT AFT NUTPLATE OF RT OMEGA BEAM IN THE LAV. MAINTENANCE CUTOUT THE CORROSION, FAB. A DOUBLER IAW SRM 53-24
- [SDR ASOA201905317052](https://openairdocs.org/sdr/ASOA201905317052), May 31, 2019: TRUNNION. CRACKED. TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND THE LT MLG AFT TRUNION CRACKED. MAINTENANCE REMOVED AND REPLACED THE LT TRUNION IAW ECTC ETD2019-145-072657.ALL WORK
- [SDR ASOA2018120314068](https://openairdocs.org/sdr/ASOA2018120314068), Dec 1, 2018: ACM. FROZEN. DFW - FLIGHT 3999 THE CREW REPORTED SMOKE IN THE COCKPIT. THE AIRCRAFT DIVERTED TO DFW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE PLANE AND PLA
- [SDR ASOA201806035150](https://openairdocs.org/sdr/ASOA201806035150), Jun 3, 2018: CONTROL MODULE. FAILED. PILOT REPORTED AN ODOR, CABIN LIGHT WAS GETTING TOO HOT. MX PERFORMED AN INSPECTION OF THE CABIN LIGHTING AND FOUND CABIN LIGHTING CONTROL MODULE AND 1A LIGHT B
- [SDR ASOA2018051605126](https://openairdocs.org/sdr/ASOA2018051605126), May 12, 2018: TRANSDUCER. FAULTY. CREW REPORTED BRAKES WERE SLOW TO REPOND ON LANDING ROLLOUT FOR LANDING. BRAKING WAS NORMAL ON BOTH SIDES ON TAXI TO GATE. REMOVED AND REPLACED THE NR 3 WHEEL S
- [SDR ASOA201704305071](https://openairdocs.org/sdr/ASOA201704305071), Apr 30, 2017: CONTROL UNIT. FAULTY. PILOT REPORTED BRAKES ARE NOT EFFECTIVE AT HIGH SPEEDS, FINE AT IDLE SPEED. LITTLE OR NO BRAKING ACTION ON LANDING. MX REMOVED AND REPLACED THE BRAKE CONTROL UN
- [SDR ASOA201704273120](https://openairdocs.org/sdr/ASOA201704273120), Apr 27, 2017: STRINGER. CRACKED. CRACK ON LT REAR STRINGER 2L AT FRAME 75. THE STRINGER WAS REPAIRED IAW SRM 53-00-03, ITEM 3, FIG 202.
- [SDR ASOA201704273119](https://openairdocs.org/sdr/ASOA201704273119), Apr 27, 2017: SKIN. CRACKED. LEFT REAR FUSELAGE SKIN CRACKED AT TWO PLACES AT FRAME 75, STRINGER 21L. REPAIRED THE SKIN IAW SRM 53-31-01, PARA 11, FIG 219, SHEET 2.
- [SDR ASOA201704273118](https://openairdocs.org/sdr/ASOA201704273118), Apr 27, 2017: DOOR SILL. CORRODED. SERVICE DOOR FRAME FORWARD SILL CUT OUT CORRODED. SILL REPLACED AS PER SRM 51-40-02.
- [SDR ASOA201704263117](https://openairdocs.org/sdr/ASOA201704263117), Apr 26, 2017: TRUNNION. CORRODED. RIGHT MLG FORWARD LOWER TRUNNION CAP CORRODED. THE TRUNNION CAP WAS REPLACED IAW CARD 57-26-00-220-C02-A00.
- [SDR ASOA201704263116](https://openairdocs.org/sdr/ASOA201704263116), Apr 26, 2017: BEARING RACE. CORRODED. CORROSION FOUND ON THE RT MLG FWD UPPER TRUNNION BEARING RACE. THE CORROSION WAS BLENDED OUT IAW 51-10-03 AND ETD2017-145-032710. NDT INSPECTION PERFORMED WITH 
- [SDR ASOA201704253115](https://openairdocs.org/sdr/ASOA201704253115), Apr 25, 2017: SKIN. CRACKED. AFT FUSELAGE SKIN CRACKED AT FRAME 65, AFT RADIO ALTIMETER ANTENNA MOUNT HOLES. REPAIRED IAW ETD2017-145-032887.
- [SDR ASOA201704253114](https://openairdocs.org/sdr/ASOA201704253114), Apr 25, 2017: SKIN. CORRODED. AFT FUSELAGE FRAMES 65 AND 68 CORRODED UNDER RADIO ALTIMETER ANTENNA. CORROOSION REMOVED IAW ETD2017-145-032887.
- [SDR ASOA201704253113](https://openairdocs.org/sdr/ASOA201704253113), Apr 25, 2017: BEAM. CORRODED. CARGO DOOR LOWER BEAM CORRODED. CARGO DOOR ENTRY LOWER BEAM REPLACED IAW SRM 51-40-02.
- [SDR ASOA201704253112](https://openairdocs.org/sdr/ASOA201704253112), Apr 25, 2017: SUPPORT. CORRODED. RIGHT OTBD LAVATORY SUPPORT CORRODED. THE SUPPORT REPLACED IAW SRM 51-40-02
- [SDR ASOA201704243111](https://openairdocs.org/sdr/ASOA201704243111), Apr 24, 2017: DOUBLER. CORRODED. RIGHT CENTER FUSELAGE CORROSION AROUND POTABLE WATER HEATED NIPPLE. DOUBLER BLENDED IAW SRM 51-10-05
- [SDR ASOA201704243110](https://openairdocs.org/sdr/ASOA201704243110), Apr 24, 2017: SEAT TRACK. CORRODED. CABIN LT OTBD SEAT TRACK NR 6 CORRODED. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06-400-801-A.
- [SDR ASOA201704243109](https://openairdocs.org/sdr/ASOA201704243109), Apr 24, 2017: SEAT TRACK. CORRODED. CABIN RT OUTBOARD SEAT TRACK NR 4 CORRODED. REPLACED THE SEAT TRACK IAW AMM 53-01-06-400-801-A.
- [SDR ASOA201704243108](https://openairdocs.org/sdr/ASOA201704243108), Apr 24, 2017: SEAT TRACK. CORRODED. CABIN RT OUTBOARD SEAT TRACK 3 CORRODED. SEAT TRACKED 3 REPLACED IAW AMM 53-01-06-400-801-A
- [SDR ASOA201704243107](https://openairdocs.org/sdr/ASOA201704243107), Apr 24, 2017: SEAT TRACK. CORRODED. RT CABIN SEAT TRACK NR 1 CORRODED. REPLACED THE SEAT TRACK IAW AMM 53-01-06-400-801A
- [SDR ASOA201704243106](https://openairdocs.org/sdr/ASOA201704243106), Apr 24, 2017: SHEAR TIE. CRACKED. FRAME 80 RT SHEAR TIE CRACKED. THE SHEAR TIE WAS REPLACED IAW 51-40-02
- [SDR ASOA201704243105](https://openairdocs.org/sdr/ASOA201704243105), Apr 24, 2017: SHEAR TIE. CRACKED. FRAME 80 LT SHEAR TIE CRACKED. THE SHEAR TIE WAS REPLACED IAW 51-40-02.
- [SDR ASOA201704243103](https://openairdocs.org/sdr/ASOA201704243103), Apr 24, 2017: BUSHING. CORRODED. HORIZONTAL STAB RT PIN BUSHING CORRODED. PIN BUSHING REPLACED.
- [SDR ASOA201704243104](https://openairdocs.org/sdr/ASOA201704243104), Apr 24, 2017: PIN. CORRODED. HORIZONTAL STAB RT PIN CORRODED. PIN REPLACED IAW MM 55-10-01
- [SDR ASOA201704243102](https://openairdocs.org/sdr/ASOA201704243102), Apr 24, 2017: BUSHING. CORRODED. HORIZONTAL STAB LT PIN BUSHING CORRODED. BUSHING REPLACED IAW MM 55-10-01.
- [SDR ASOA201704243101](https://openairdocs.org/sdr/ASOA201704243101), Apr 24, 2017: CHANNEL. CORRODED. SERVICE DOOR LOWER CHANNEL CORRODED. THE CHANNEL WAS REPLACED IAW SRM 51-40-02.
- [SDR ASOA201704243100](https://openairdocs.org/sdr/ASOA201704243100), Apr 24, 2017: ANGLE. CRACKED. COCKPIT LT FRAME 10, UPPER ANGLE CRACKED. THE FRAME ANGLE WAS REPLACED IAW SRM 51-40-02.
- [SDR ASOA201704243099](https://openairdocs.org/sdr/ASOA201704243099), Apr 24, 2017: FRAME. CRACKED. COCKPIT RT FRAME 10 CRACKED. THE FRAME WAS REPLACED IAW SRM 51-40-02.
- [SDR ASOA201704203098](https://openairdocs.org/sdr/ASOA201704203098), Apr 20, 2017: CROSSBEAM. CRACKED. NLG UPLOCK AFT CROSSBEAM CRACKED. THE CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50.
- [SDR ASOA201704203097](https://openairdocs.org/sdr/ASOA201704203097), Apr 20, 2017: CROSSBEAM. CRACKED. NLG UPLOCK FORWARD CROSSBEAM CRACKED. THE CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50.
- [SDR ASOA20161001056](https://openairdocs.org/sdr/ASOA20161001056), Oct 1, 2016: FLAPPER VALVE. LEAKING. THE CREW REPORTED FUEL STREAMING FROM THE LEFT WING INFLIGHT. MAINTENANCE INSPECTED AND FOUND RIGHT WING FLAPPER VALVE DAMAGED. REPLACED THE FLAPPER VALVE AND O
- [SDR ASOA20140515064](https://openairdocs.org/sdr/ASOA20140515064), May 13, 2014: CONTROL PANEL. INOPERATIVE. DURING CRUISE, THE AIRCREW RECEIVED AN EICAS MESSAGE THAT THE EMERGENCY LIGHTS WERE NOT ARMED. MAINTENANCE R & R THE F/A LIGHTING CONTROL PANEL. THE EMERGENCY L
- [SDR ASOA20140513070H](https://openairdocs.org/sdr/ASOA20140513070H), May 13, 2014: MODULE. INOPERATIVE. THE CREW REPORTED AN EMERGENCY LIGHTS NOT ARMED EICAS MESSAGE IN FLIGHT. ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT AND R & R THE OVERHEAD LIG
- [SDR ASOA20131126447](https://openairdocs.org/sdr/ASOA20131126447), Nov 25, 2013: BLEED VALVE. STUCK. AIRCRAFT MADE AN AIR RETURN WHEN THE ENGINE NR 1 SHOWED THAT THE ENGINE 1 BLEED VALVE WAS CLOSED. MAINTENANCE R & R THE NR 1 ENGINE BLEED VALVE REF AMM 36-11-05
- [SDR ASOA20130903066](https://openairdocs.org/sdr/ASOA20130903066), Sep 3, 2013: WINDSHIELD. FAILED. THE CREW REPORTED A NR 1 WINDSHIELD FAILED IN FLIGHT ALONG WITH A ELECTRICAL BURNING SMELL. MX INSPECTED AND REPLACED THE NR 1 WINDSHIELD. OPS CHECKS WERE GOOD.
- [SDR ASOA20130901068](https://openairdocs.org/sdr/ASOA20130901068), Sep 1, 2013: UNKNOWN. ODOR. THE CREW REPORTED A ELECTRICAL BURNING ODOR AFTER WINDSHIELD NR 1 FAIL INFLIGHT. MX INSPECTED AND FOUND NO ELECTRICAL BURNING ODOR. PERFORMED OPS CHECK OF WINDS
- [SDR ASOA20130830065](https://openairdocs.org/sdr/ASOA20130830065), Aug 30, 2013: CONTROLLER. FAULTY. THE CREW REPORTED A BURNING SMELL WHEN WINDSHIELD HEAT NR 2 IS ON. MX INSPECTED AND REPLACED THE NR 2 WINDSHIELD HEAT CONTROLLER. OPS CHECKS WERE GOOD.
- [SDR ASOA20130830064C](https://openairdocs.org/sdr/ASOA20130830064C), Aug 30, 2013: CONTROLLER. FAULTY. THE CREW REPORTED BURNING ODOR WITH WINDSHIELD HEAT NR 1 ON. MX INSPECTED AND REPLACED THE NR 1 WINDSHIELD HEAT CONTROLLER. OPS CHECKED GOOD.
- [SDR ASOA20130712072R](https://openairdocs.org/sdr/ASOA20130712072R), Jul 12, 2013: DUCT. LOOSE. CREW REPORTED PACK NR 2 VALVE CLOSED ON EICAS MESSAGE IN FLIGHT WHICH RESULTED IN LOSS OF BOTH AIR CONDITIONING PACKS AND PRESSURIZATION DUE TO NR 1 PACK BEING 
- [SDR ASOA20130513075](https://openairdocs.org/sdr/ASOA20130513075), May 13, 2013: SKIN. CRACKED. DURING A-CK INSPECTION THE AFT FUSELAGE II SKIN WAS FOUND TO BE CRACKED AT A RIVET BELOW STR 6L ON FR78. MX REMOVED THE DAMAGE, AND PERFORMED A FILLER/DOUBLER R
- [SDR ASOA20130513074](https://openairdocs.org/sdr/ASOA20130513074), May 13, 2013: SKIN. CRACKED. DURING "A" CHECK INSPECTION, THE AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET EBLOW STR 8L AT FR77. MX REMOVED THE DAMAGE, AND PERFORMED A FILLER/DOUBLE
- [SDR ASOA20130513073](https://openairdocs.org/sdr/ASOA20130513073), May 13, 2013: SKIN. CRACKED. DURING "A" CHECK INSPECTION, THE AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET BELOW STR 2R AT FR75. MX REMOVED THE DAMAGE, AND PERFORMED A FILLER/DOUBLE
- [SDR ASOA20130513072](https://openairdocs.org/sdr/ASOA20130513072), May 13, 2013: SKIN. CRACKED. DURING "A" CHECK INSPECTION, THE AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET BELOW STR 8R AT FR77. MX REMOVED THE DAMAGE, AND PERFORMED A FILLER/DOUBLE
- [SDR ASOA20130513071](https://openairdocs.org/sdr/ASOA20130513071), May 13, 2013: SKIN. CRACKED. DURING "A" CHECK INSPECTION, THE AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET BELOW STRINGER 4R AT FR78. MX REMOVED THE DAMAGE, AND PERFORMED A FILLER/D
- [SDR ASOA20130505034](https://openairdocs.org/sdr/ASOA20130505034), May 5, 2013: RELAY. FAULTY. MX REPORTED THE EMERGENCY LIGHTS WOULD NOT ARM. REPLACED RELAY K0275. OPS CHECKED GOOD.

All 127: https://openairdocs.org/aircraft/N13988/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/N13988/stcs.md

## Earlier aircraft with N13988

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N13988 before.

- [Cancelled 1972-10-10](https://openairdocs.org/deregistered/N13988-1972-10-10): Piper PA-23-250, S/N 27-4606. Exported to Mexico. Owner: [Export-Import Inc](https://openairdocs.org/faa-owner/EXPORT-IMPORT%20INC), [Brownsville, TX](https://openairdocs.org/faa-place/TX/Brownsville)

## Related

- Other Embraer EMB-145LR aircraft: https://openairdocs.org/model/embraer-emb-145lr/aircraft.md
- The Allison AE3007C series engine: https://openairdocs.org/engine/allison-ae3007c-series.md

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