# N19GL: 1992 Brantly B-2B - Status: Valid registration - Airframe: [Brantly B-2B](https://openairdocs.org/model/brantly-b-2b) (registry code 1440506, 2 seats) - Engine: [Lycoming I0360 SER A&C](https://openairdocs.org/engine/lycoming-i0360-ser-a-c) (registry code 41511) - Data sheets: [TCDS 2H2](https://openairdocs.org/tcds/2H2) (Brantly International Inc.) (OpenAirDocs) - Serial number: 2004 - Year built: 1992 - Type: Rotorcraft - Engine type: Reciprocating - Airworthiness: Standard, normal - Airworthiness date: March 29, 2000 - Certificate issued: July 31, 2015 - Expires: July 31, 2028 - Mode S code: A16673 - Registered owner: [Eastern Stearman Inc Trustee](https://openairdocs.org/faa-owner/EASTERN%20STEARMAN%20INC%20TRUSTEE) - Location: [Leesburg, VA](https://openairdocs.org/faa-place/VA/Leesburg) - Owner type: Corporation - Owner's area on the map: 39.1803° N, 77.5335° W: Placed by OpenAirDocs at the center of ZIP code 20176, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=19GL - Page: https://openairdocs.org/aircraft/N19GL 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): 25 in force ### Matched by airframe (Brantly B-2B) - [AD 2023-11-07](https://openairdocs.org/ad/2023-11-07): Ground Proximity System · Airbus Helicopters 47, 206, 210 and 237 more. Effective Jun 22, 2023 - [AD 2021-26-09](https://openairdocs.org/ad/2021-26-09): Tail Rotor Head · Brantly International 305, B-2, B-2A and 1 more. Effective Jan 19, 2022 - [AD 2014-20-16](https://openairdocs.org/ad/2014-20-16): Main Rotor Blade · Brantly International B-2, B-2A and B-2B. Effective Nov 12, 2014 - [AD 2006-12-07](https://openairdocs.org/ad/2006-12-07): ECi cylinder assemblies · Aerostar AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 386 more. Effective Jul 11, 2006 - [AD 2006-08-07](https://openairdocs.org/ad/2006-08-07): Upper tail rotor vertical gearbox (gearbox) · Brantly International B-2, B-2A and B-2B. Effective May 2, 2006 - [AD 68-04-04 R2](https://openairdocs.org/ad/68-04-04-R2): Tail Rotor Blade · Brantly International B-2, B-2A and B-2B. Effective Feb 14, 1983 - [AD 81-17-01](https://openairdocs.org/ad/81-17-01): Starting Vibrator Assemblies · Bendix Starting Vibrator Assemblies, B-2, B-2A and 49 more. Effective Aug 13, 1981 - [AD 72-21-02](https://openairdocs.org/ad/72-21-02): Pylon Bearing Shaft · Brantly International B-2, B-2A and B-2B. Effective Dec 8, 1972 - [AD 71-17-05](https://openairdocs.org/ad/71-17-05): Main Rotor Mast · Brantly International B-2, B-2A and B-2B. Effective Nov 26, 1971 - [AD 68-05-02](https://openairdocs.org/ad/68-05-02): Tail Rotor Drive Shaft · Brantly International 305, B-2, B-2A and 1 more. Effective Mar 30, 1968 - [AD 67-09-02](https://openairdocs.org/ad/67-09-02): Main Rotor Mast · Brantly International B-2, B-2A and B-2B. Effective Apr 20, 1967 - [AD 65-28-01](https://openairdocs.org/ad/65-28-01): Tail Rotor Blades · Brantly International B-2, B-2A and B-2B. Effective Dec 14, 1965 - [AD 62-06-01](https://openairdocs.org/ad/62-06-01): Seat Back Adjustment · Brantly International B-2, B-2A and B-2B. Effective Mar 23, 1962 - [AD 62-05-02](https://openairdocs.org/ad/62-05-02): Fuel Pump Seals · Brantly International B-2, B-2A and B-2B. Effective Feb 28, 1962 - [AD 61-23-01](https://openairdocs.org/ad/61-23-01): Rotor Blade Bond Separation · Brantly International B-2, B-2A and B-2B. Effective Nov 4, 1961 - [AD 61-18-02](https://openairdocs.org/ad/61-18-02): Tail Rotor Modification · Brantly International B-2, B-2A and B-2B. Effective Aug 29, 1961 - [AD 61-16-04](https://openairdocs.org/ad/61-16-04): Transmission Mount Lug · Brantly International B-2, B-2A and B-2B. Effective Aug 14, 1961 - [AD 61-16-03](https://openairdocs.org/ad/61-16-03): Seat Modification · Brantly International B-2, B-2A and B-2B. Effective Aug 4, 1961 - [AD 61-11-02](https://openairdocs.org/ad/61-11-02): Oil System Modification · Brantly International B-2, B-2A and B-2B. Effective Aug 4, 1961 - [AD 61-11-01](https://openairdocs.org/ad/61-11-01): Landing Gear Drag Brace · Brantly International B-2, B-2A and B-2B. Effective May 31, 1961 - [AD 61-04-01](https://openairdocs.org/ad/61-04-01): Clutch Bolts · Brantly International B-2, B-2A and B-2B. Effective Feb 22, 1961 - [AD 60-26-03](https://openairdocs.org/ad/60-26-03): Drive Shaft Coupling · Brantly International B-2, B-2A and B-2B. Effective Dec 20, 1960 - [AD 60-10-02](https://openairdocs.org/ad/60-10-02): Main Rotor Blade · Brantly International B-2, B-2A and B-2B - [AD 60-07-02](https://openairdocs.org/ad/60-07-02): Tail Rotor Drive Shaft · Brantly International B-2, B-2A and B-2B - [AD 60-06-03](https://openairdocs.org/ad/60-06-03): Tail Rotor Guard · Brantly International B-2, B-2A and B-2B ### Matched by engine (Lycoming I0360 SER A&C) None in force. ### Historical (superseded or no longer in force) - [AD 2021-23-13](https://openairdocs.org/ad/2021-23-13) (historical): Ground Proximity System · Airbus Helicopters K-225, K-190A, K-240 and 237 more. Effective Dec 9, 2021 ## Information bulletins (advisory) (2 in force) - [SAIB SW-07-28](https://openairdocs.org/saib/SW-07-28): Rotor blade cracks. Issued Apr 17, 2007 - [SAIB SW-04-90](https://openairdocs.org/saib/SW-04-90): . Issued Sep 23, 2004 ## NTSB investigations None matched to N19GL. ## FAA accident and incident reports None matched to N19GL. ## Service difficulty reports None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. ## STCs that may be installed (OpenAirDocs) (20) 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 (Brantly B-2B) - [STC SH3319NM](https://openairdocs.org/stc/SH3319NM): Installation of Precise Flight Pulselite Control Unit in the Landing /Taxi Recognition Visual Control Light system,. Precise Flight Inc - [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC - [STC SR02704SE](https://openairdocs.org/stc/SR02704SE): Installation and maintenance of the Sunspot 36 and 46 series lights. AeroLED's Holdings LLC - [STC SR00359BO](https://openairdocs.org/stc/SR00359BO): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies - [STC SR01802WI](https://openairdocs.org/stc/SR01802WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel per ASTM D7547. Swift Fuels LLC - [STC SR02394AK](https://openairdocs.org/stc/SR02394AK): Replacement of existing landing and/or hover light bulbs with Light Emitting Diode (LED) lighting system. Seaplanes North LLC - [STC SA01669CH](https://openairdocs.org/stc/SA01669CH): Installation of Challenger Reusable Air Filter. Challenger Aviation Products Inc - [STC SH11CE](https://openairdocs.org/stc/SH11CE): Installation of Hoskins Twilighter Mk II supplementary lights. BF Goodrich Aerospace - [STC SA1315WE](https://openairdocs.org/stc/SA1315WE): Installation of Mixture Monitor (exhaust gas temperature probe, gage and selector) in accordance with Delta Products Part Lists A-192 and A-193, or in accordance with Tri-Star Corporation Mixture Monitor Installation Instructions dated December 9, 1981, or later FAA approved revision and/or Drawing List MM-127 dated November 15, 1981, or later FAA approved revision in aircraft models listed in Master Eligibility List P-80-A-6 revised March 29, 1968, copy attached, or later FAA approved revision. Universal Corporation - [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics International Inc - [STC SA02033AT](https://openairdocs.org/stc/SA02033AT): Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line. M-20 Oil Separators LLC - [STC SA00680SE](https://openairdocs.org/stc/SA00680SE): Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer. Electronics International - [STC SA489EA](https://openairdocs.org/stc/SA489EA): Installation of ARP Inc. carburetor ice detection system. Aircraft & Rotorcraft Products (ARP) Inc - [STC SA02520AT](https://openairdocs.org/stc/SA02520AT): Installation of M-20 Oil Separator, model 600-WP. M-20 Oil Separators LLC - [STC SH12CE](https://openairdocs.org/stc/SH12CE): Replace existing engine induction air filter with AC Spark Plug Filter. Brackett Aero Filters Inc - [STC SA2350NM PAGE 1](https://openairdocs.org/stc/SA2350NM%20PAGE%201): Installation of Electronics International Inc digital carburetor/outside air temperature gauges. Electronics International - [STC SA4302NM](https://openairdocs.org/stc/SA4302NM): Installation of Electronics Int'l digital automatic engine analyzer. Electronics International - [STC SA3862NM PAGE 1](https://openairdocs.org/stc/SA3862NM%20PAGE%201): Installation of Electronics International Primary TIT/EGT/CHT instruments, remote switches and associated accessories. Electronics International - [STC SA2190NM PAGE 1](https://openairdocs.org/stc/SA2190NM%20PAGE%201): Installation of electronics International Digital Volt/Amp Gauges and Accessories. Electronics International - [STC SA2350NM](https://openairdocs.org/stc/SA2350NM) (historical): Installation of Electronics International Inc digital carburetor/outside air temperature gauges listed on the attached continuation sheet and the associated accessories. Electronics International ## Related - Other Brantly B-2B aircraft: https://openairdocs.org/model/brantly-b-2b/aircraft.md - The Lycoming I0360 SER A&C engine: https://openairdocs.org/engine/lycoming-i0360-ser-a-c.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.