# N638AE: 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 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: 145172
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 24, 1999
- Certificate issued: September 2, 2011
- Expires: September 30, 2027
- Mode S code: A85B79
- Registered owner: [American Airlines Inc](https://openairdocs.org/faa-owner/AMERICAN%20AIRLINES%20INC)
- Location: [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth)
- Owner type: Corporation
- Owner's area on the map: 32.8240° N, 97.0491° W: Placed by OpenAirDocs at the center of ZIP code 76155, 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=638AE
- Page: https://openairdocs.org/aircraft/N638AE

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/N638AE/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 N638AE.

## FAA accident and incident reports

None matched to N638AE.

## Service difficulty reports (156, 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 HNAA2022091200258](https://openairdocs.org/sdr/HNAA2022091200258), Sep 9, 2022: NONE. NONE. PDIS 638 27-22 2677131 09SEP22 CLT CLOSE RUD SYS 2 INOP INFLIGHT FACT 09SEP22 10:53 CLT C/W FIM 27-22-00-810-802A STEPS 1,2,3 R/R W RUDDER SYSTEMS PRESSURE SWIT
- [SDR HNAA2022050700177](https://openairdocs.org/sdr/HNAA2022050700177), May 18, 2022: NONE. NONE. PDIS 638 21-01 2514801 19MAY22 AVL CLOSE BURNING FUMES COMING FROM PACKS. FACT 20MAY22 17:18 ROA #2 PACK VLV R&R'D, SEE LP 251481-2 FOR SIGNOFF. R&R'D #1 ACM IA
- [SDR HNAA2021120200593](https://openairdocs.org/sdr/HNAA2021120200593), Nov 30, 2021: NONE. NONE. PDIS 638 36-21 2745471 30NOV21 ROA CLOSE BLEED 2 LEAK MSG IN FLIGHT FACT 30NOV21 12:33 ROA C/W FIM TASK 36-20-00-810-802 INSPECTED AND FOUND V BAND CLAMP ON IB 
- [SDR HNAA2021071500324](https://openairdocs.org/sdr/HNAA2021071500324), Jul 15, 2021: CONTROL CABLE. FRAYED. FLIGHT CREW: WHEN DOING THE FLIGHT CONTROL CHECK (FWD AND AFT) CREW FELT A STICKING POINT. MAINTENANCE: DISCOVERED THAT THE ELEVATOR SERVO BRACKET CABLE WAS COR
- [SDR HNAA2021070600312](https://openairdocs.org/sdr/HNAA2021070600312), Jul 4, 2021: UNKNOWN. ODOR. COMING THROUGH 31K FEET. STRONG ODER NOTICED IN COCK PIT/CABIN. DISSIPATED GOING BACK THROUGH 31K FEET. OCCURRING INTERMITTENTLY ON DESCENT. COULD DUPLICATE ON 
- [SDR HNAA2021063000296](https://openairdocs.org/sdr/HNAA2021063000296), Jun 28, 2021: PUMP. FAULTED. IN CRUISE FLIGHT AT 10K, $2 HYD PSI SPIKED TO 3,800 PSI FOLLOWED BY LOSS OF #2 HYD QUNTY AND SYSTEM PSI DROPPED TO ZERRO. ELECTRIC DRIVEN PUMP TURNED OFF AFTER 
- [SDR HNAA2021041200135](https://openairdocs.org/sdr/HNAA2021041200135), Apr 10, 2021: ECS. ODOR. PDIS 638 21-01 2554732 10APR21 CMI CLOSE BURNING SMELL AT 100 KNOTS IN COCKPIT QUICKLY DISSIPATED AFTER REJECTED TAKE OFF, FACT 11APR21 04:10 CMI PERFORMED FIM 
- [SDR HNAA2021010400001](https://openairdocs.org/sdr/HNAA2021010400001), Jan 1, 2021: A/C PACK. OVERHEATED. POOR AIR FLOW COCKPIT AND PACK 1 OVERHEAT WITH BURNING SMELL. OPERATED PACKS CORRECTLY, IAW AMM 21-00-00-810-001A AND FOLLOWED FIM TASK 21-51-00-810-803A AND CO
- [SDR HNAA2020121400361](https://openairdocs.org/sdr/HNAA2020121400361), Dec 13, 2020: CONTACTOR. BURNED. PDIS 638 49-10 2346991 13DEC20 MDT CLOSE. WHEN PILOT TURNED ON HIS APU HE HAD SHED BUS 1 AND 2 OFF LINE FOLLOWED BY APU GEN OFF BUSS AND ELECTRICAL BURNING SMEL
- [SDR HNAA2020121200360](https://openairdocs.org/sdr/HNAA2020121200360), Dec 10, 2020: STARTER GEN. MALFUNCTIONED. APU GEN OFF BUS MESSAGE APPEARED ON EICAS WITH CLICKING NOISE AND ELECTRICAL BURNING SMELL IN COCKPIT. RESTARTED APU WITH GEN OFF NO SMELL NOTED OR CB S POPPED.
- [SDR HNAA2020110500296](https://openairdocs.org/sdr/HNAA2020110500296), Nov 7, 2020: SLEEVE. DAMAGED. PDIS 638 21-01 2346581 07NOV20 PHL CLOSE. FOLLOWING A/I TEST IN FLT, F/A REPORTED RUSHING AIR NOISE FROM MIDDLE OF CABIN, BURNING SMELL NOTED SHORTLY AFTER. SHU
- [SDR HNAA2020090800253](https://openairdocs.org/sdr/HNAA2020090800253), Sep 7, 2020: UNKNOWN. ODOR. PDIS 638 21-21 2416061 07SEP20 RIC CLOSE. STRONG CHEMICAL ODOR PRESENT IN COCKPIT. OBSERVED WITH PACKS RUNNING. FACT 07SEP20 06:21 RIC. R/R APU CONTACTOR K0291 
- [SDR HNAA2020072100231](https://openairdocs.org/sdr/HNAA2020072100231), Jul 20, 2020: CONTACTOR. BURNED. ON ARRIVAL TO FLIGHT DECK, NOTICED PLASTIC, ELECTRICAL ODOR. MX FOUND CONTACTOR K0119 FOR 1A FUEL PUMP BURNED. ACFT HAS PRIOR HISTORY. R & R THE CONTACTOR IAW A
- [SDR HNAA2020071700194](https://openairdocs.org/sdr/HNAA2020071700194), Jul 16, 2020: CONTACTOR. BURNED. BURNING PLASTIC SMELL IN FLIGT DECK. FOUND BURNT CONTACTOR K0291 BEHIND LIFE VEST STORAGE PANEL. R/R CONTACTOR IAW AMM 24-34-04. OPS CHECK GOOD. OK FOR SERVICE.
- [SDR HNAA2020021400060](https://openairdocs.org/sdr/HNAA2020021400060), Feb 13, 2020: WIRE. DETACHED. EMERGENCY LIGHT ON MAIN DOOR INOP.... RE-ATTACHED WIRES TO THE ELECTRIC CONNECTORS FOR THE EMERGENCY LIGHT. OPS CHECK GOOD.
- [SDR HNAA2020012000023](https://openairdocs.org/sdr/HNAA2020012000023), Jan 18, 2020: UNKNOWN. ODOR. AFTER TAKEOFF CREW NOTED PUNGENT ELECTRICAL/BURNING ODOR IN COCKPIT. SMELL CLEARD SHORTLY AFTER LANDING. MX T/S ISSUE IN REF TO FIM 21-20-00-810-801-A. NO DEFEC
- [SDR HNAA2019102200313](https://openairdocs.org/sdr/HNAA2019102200313), Oct 20, 2019: UNKNOWN. ODOR. PDIS 638 05-50 1995782 20OCT19 GSO CLOSE BURNING ODOR OBSERVED A 26,000 ICING CONDITIONS. SME LL DISSIPATED AT 5000 FT. FACT 20OCT19 13:37 GSO INSP LIGHTS AND P
- [SDR HNAA2019091100267](https://openairdocs.org/sdr/HNAA2019091100267), Sep 10, 2019: GENERATOR. MALFUNCTIONED. GEN #3 SHOWING AMBER DASHES AND 0 AMPS DURING FLIGHT. FIX: R&R GEN 3 IAW AMM 24-31-01 LEAK AND OPS CHECK GOOD. NOTE: AIRCRAFT DIVERTED FROM YQB TO ALB TO BE FIX
- [SDR HNAA2019043000129](https://openairdocs.org/sdr/HNAA2019043000129), Apr 28, 2019: WIRE. BROKEN. NDIS 638 33-51 0011560 28APR19 SBY CLOSE SERVICE DOOR EMERGENCY LIGHT IS INOP 30100 00 BAD FACT 28APR19 08:18 SBY R&R'D LAMP NO FIX. INSPECTED & FOUND BROKEN WI
- [SDR HNAA2019041700103](https://openairdocs.org/sdr/HNAA2019041700103), Apr 16, 2019: A/C PACK. ODOR. 638 21-01 2098402 16APR19 FLO CLOSE ON TAKEOFF FLIGHT DECK FILLED WITH SMELL.ON APPROACH SMELL/HAZE RETURNED AND DISAPATED BEFORE LANDING. 26803 00 SMK MEL 16AP
- [SDR HNAA2019012500028](https://openairdocs.org/sdr/HNAA2019012500028), Jan 23, 2019: FLAP. OUT OF RIG. PDIS 638 27-50 2047071 23JAN19 PHL CLOSE FLAPS FAIL MSG IN FLT AFTER T/O WHEN SETTING FLAPS TO ZERO. FACT 24JAN19 22:25 PHL FOUND FLAPS TO BE OUT OF RIG. PERFOR
- [SDR HNAA2018103100270](https://openairdocs.org/sdr/HNAA2018103100270), Oct 30, 2018: LIGHT. INOPERATIVE. NDIS 638 33-51 0007300 30OCT18 RIC CLOSE AFT CABIN EMERGENCY FLASHLIGHT INOP 28629 00 NGR FACT 30OCT18 07:35 RIC R/R BULB IN AFT CABIN EMERGENCY FLASHLIGHT AS R
- [SDR HNAA2018101900262](https://openairdocs.org/sdr/HNAA2018101900262), Oct 17, 2018: FAN. ODOR. PDIS 638 21-24 1595132 17OCT18 PHL CLOSE ELECTRICAL SMELL OBSERVED AFTER APU ATTEMPTED START. OUTSIDE OF AIRCRAFT NEAR GPU PLUG-IN. 76840 00 VAG HISTORY: FACT 1
- [SDR HNAA2018092600231](https://openairdocs.org/sdr/HNAA2018092600231), Sep 21, 2018: UNKNOWN. FUMES. PDIS 638 21-01 1682341 21SEP18 PHL CLOSE WHILE STARTING EITHER #1 OR #2 ENG OFF APU, FUMES ARE PRESENT THROUGHOUT A/C. APU TEMP SPIKES TO MID 600 DEGREES 21585 
- [SDR HNAA2018052500114](https://openairdocs.org/sdr/HNAA2018052500114), May 12, 2018: UNKNOWN. ODOR. DURING CRUISE, CREW BEGAN TO SMELL AN UNUSUAL ODOR ACCOMPANIED BY RADIO STATIC. ODOR AND STATIC DISAPPEARED AFTER LEAVING PRECIP. FA DID NOT NOTE THE ODOR IN TH
- [SDR HNAA2018052500100](https://openairdocs.org/sdr/HNAA2018052500100), May 2, 2018: INDICATOR. FALSE INDICATION. DURING TAXI OUT, THE NR 1 FUEL TANK LEVEL FLUCTUATED FROM 42 - 4600 LBS. AFTER DEPARTURE THE NR 2 TANK CONTENTS AND TOTAL FOB INDICATIONS ON MFD AND EICAS SHOWE
- [SDR HNAA2018032100062](https://openairdocs.org/sdr/HNAA2018032100062), Mar 20, 2018: INLET. ICED. NR 2 ENGINE REPORTED FOD IN INLET. REMOVED ICE FROM THE NR 2 ENGINE INLET
- [SDR HNAA2018021900036](https://openairdocs.org/sdr/HNAA2018021900036), Feb 15, 2018: CABIN PRESSURE. MALFUNCTIONED. CABIN ALTITUDE REACHED 13,500 FT AT FL190. AUTO PRESSURE MODE HAD NO EFFECT. MANUAL MODE BEGAN TO WORK AT 10,000 FT, MAINTAINING CABIN ALTITUDE OF 5,500 FT. CAB
- [SDR HNAA2018021900035](https://openairdocs.org/sdr/HNAA2018021900035), Feb 14, 2018: OXYGEN MASK. MALFUNCTIONED. SEAT 6A OXYGEN MASK DID NOT DEPLOY. PERFORMED AN OPS CHECK OF THE PAX OXYGEN MASK IAW AMM 35-20-00, NO DEFECTS NOTED. OKAY FOR SERVICE.
- [SDR HNAA2018021900034](https://openairdocs.org/sdr/HNAA2018021900034), Feb 14, 2018: CONTROLLER. FAILED. SLOW LOSS OF PRESSURIZATION AT 34,000 FT. PRESSURIZATION STABILIZED AROUND 15,500 FT. SMALL POP IN CABIN AT THE TIME CABIN ALTITUDE WENT AMBER. R & R THE CABIN 
- [SDR HNAA2018021400030](https://openairdocs.org/sdr/HNAA2018021400030), Feb 11, 2018: INDICATOR. MALFUNCTIONED. FUEL 1 LOW LEVEL MESSAGE AND NR 2 TANK INDICATED ZERO. RANDOM INDICATIONS. ALSO LOST TOTAL FUEL USED. CMC SHOWS FUEL 1 LO LEVEL MESSAGE. PERFORMED A CHECK ON TH
- [SDR SIMA20180124001](https://openairdocs.org/sdr/SIMA20180124001), Jan 24, 2018: FRAME. CHAFED. RIGHT FRAME 65 IN CARGO BAY HAS A CHAFE NEAR STINGER 12R. REPAIRED IAW ERS-EM-53MR-3082.
- [SDR SIMA20180121002](https://openairdocs.org/sdr/SIMA20180121002), Jan 21, 2018: FRAME. CRACKED. FRAME 66 IS CRACKED BETWEEN STRINGERS 17 TO 18L. REPAIRED THE FRAME IAW SRM 53-00-04, AND SRM 51-40-02.
- [SDR SIMA20180121001](https://openairdocs.org/sdr/SIMA20180121001), Jan 21, 2018: SKIN. PUNCTURED. RIGHT SIDE OF RUDDER HAS A HOLE IN THE SKIN NEAR THE LOWER AFT CORNER. REPAIRED THE RUDDER LOWER SKIN IAW ERS EM-55MR-632.
- [SDR SIMA20180118005](https://openairdocs.org/sdr/SIMA20180118005), Jan 18, 2018: FITTING. GOUGED. RIGHT AILERON PCA FITTING IS GOUGED. REMOVED AND REPLACED THE RT AILERON PCA FITTING IAW EO EM-27MR-112.
- [SDR SIMA20180116004](https://openairdocs.org/sdr/SIMA20180116004), Jan 16, 2018: FLOOR SUPPORT. CORRODED. LEFT OMEGA BEAM IS CORRODED BETWEEN FRAMES 58-59. REPAIRED THE LEFT OMEGA BEAM IAW EO EM-53MR-1518.
- [SDR SIMA20180115007](https://openairdocs.org/sdr/SIMA20180115007), Jan 15, 2018: FLOOR SUPPORT. CORRODED. RIGHT CENTER OMEGA BEAM IS CORRODED BETWEEN FRAMES 58 - 59. REPAIRED THE OMEGA BEAM IAW EO EM-53MR-1518.
- [SDR SIMA20180112003](https://openairdocs.org/sdr/SIMA20180112003), Jan 12, 2018: TORQUE BOX. CRACKED. PAX DOOR INNER HANDLE TORQUE BOX HAS A .750 INCH CRACK. REPAIRED THE SUPPORT IAW EO EM-52MR-250.
- [SDR SIMA20180111009](https://openairdocs.org/sdr/SIMA20180111009), Jan 11, 2018: DOOR SILL. CORRODED. CARGO DOOR SILL HAS AN AREA OF CORROSION. INSTALLED A NEW DOOR SILL IAW 51-40-02.
- [SDR SIMA20180111008](https://openairdocs.org/sdr/SIMA20180111008), Jan 11, 2018: SHEAR TIE. CRACKED. SHEAR TIE AT FRAME 80, STRINGER 7L IS CRACKED APPROXIMATELY 1 INCH. R & R THE SHEAR TIE IAW SRM 51-40-02.
- [SDR SIMA20180111012](https://openairdocs.org/sdr/SIMA20180111012), Jan 11, 2018: SHEAR TIE. CRACKED. SHEAR TIE AT FRAME 80, STRINGER 7R IS CRACKED APPROXIMATELY 1 INCH. R & R THE SHEAR TIE IAW SRM 51-40-02.
- [SDR SIMA20180111006](https://openairdocs.org/sdr/SIMA20180111006), Jan 11, 2018: ANGLE. CRACKED. LEFT WING UPPER WING TO FUSELAGE PANEL, LOWER ANGLE, FIRST FROM AFT END IS CRACKED AT FORWARD END. R & R THE ANGLE IAW SRM-51-20-02 AND ETN-EM-53-142.
- [SDR SIMA20180111010](https://openairdocs.org/sdr/SIMA20180111010), Jan 11, 2018: ANGLE. CRACKED. LEFT WING UPPER WING TO FUSELAGE PANEL, LOWER ANGLE, SECOND FROM AFT END IS CRACKED AT THE AFT END. R & R THE LT WING SECOND FROM AFT UPPER WING TO FUSELAGE PAN
- [SDR SIMA20171019002](https://openairdocs.org/sdr/SIMA20171019002), Oct 19, 2017: INVERTER. INOPERATIVE. ROW 3 EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE NR 3 INVERTER IAW AMM 33-50-11 AND WM 33-50-50. EMERGENCY LIGHTING SYSTEM OPS CHECKED GOOD. NO DEFEC
- [SDR SIMA20170926001](https://openairdocs.org/sdr/SIMA20170926001), Sep 26, 2017: LIGHT. INOPERATIVE. LT WING AFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMP AT LT WING AFT OVERWING EMERGENCY EXIT LIGHT IAW AMM 33-50-10. OPS CHECK GOOD.
- [SDR SIMA20170808002](https://openairdocs.org/sdr/SIMA20170808002), Aug 8, 2017: LIGHT. INOPERATIVE. ROW 12 CEILING EMERGENCY LT INOP. REMOVED AND REPLACED ROW 12 CEILING EMERGENCY LIGHT BULB IAW AMM 33-50-08-000-801-A AND 33-50-08-400-801-A OPC GOOD END.
- [SDR SIMA20170502001](https://openairdocs.org/sdr/SIMA20170502001), May 2, 2017: CONNECTOR. UNSECURE. AFT EMERGENCY FLOOR LIGHTING INOPERATIVE. SECURED INVERTER CONNECTOR. OPS CHECKED GOOD IAW AMM 33-50-11.
- [SDR SIMA20170302001](https://openairdocs.org/sdr/SIMA20170302001), Mar 2, 2017: WIRE. BROKEN. MAIN DOOR EXTERIOR EMERENCY LIGHT INOPERATIVE. FOUND A WIRE BROKEN AT SPLICE REMOVED AND REPLACED WIRE TERMINAL AND RECEPTICLE IAW SWPM 20-21-00. OPS CHECKED GO
- [SDR SIMA20170222001](https://openairdocs.org/sdr/SIMA20170222001), Feb 22, 2017: CONNECTOR. UNSECURE. OVERHEAD EMERGENCY LIGHT INOP IN ROW 12 (EXIT SIGN). RESECURED EMERGENCY LIGHT CONNECTOR AND OPS CHECK GOOD IAW EMERGENCY LIGHT TEST AMM 33-50-00.
- [SDR SIMA20170212003](https://openairdocs.org/sdr/SIMA20170212003), Feb 12, 2017: FLASHLIGHT. INOPERATIVE. FA FWD FLASHLIGHT INOPERATIVE. REMOVED & REPLACED THE FLASHLIGHT, OPS OK IAW AMM 33-51-01.

All 156: https://openairdocs.org/aircraft/N638AE/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/N638AE/stcs.md

## 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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