# N197GA: 1984 Beech 1900C

- Status: Valid registration
- Airframe: [Beech 1900C](https://openairdocs.org/model/beech-1900c) (registry code 1154161, 19 seats)
- Engine: [Pratt & Whitney Canada PT6A-60A](https://openairdocs.org/engine/pratt-whitney-canada-pt6a-60a) (registry code 52043)
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) (Textron Aviation Inc.), [TCDS E4EA](https://openairdocs.org/tcds/E4EA) (Pratt & Whitney Canada Corp.) (OpenAirDocs)
- Serial number: UB-16
- Year built: 1984
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: August 3, 1984
- Certificate issued: August 4, 2010
- Expires: January 31, 2028
- Mode S code: A182C3
- Registered owner: [Alpine Aviation Inc](https://openairdocs.org/faa-owner/ALPINE%20AVIATION%20INC)
- Location: [Provo, UT](https://openairdocs.org/faa-place/UT/Provo)
- Owner type: Corporation
- Owner's area on the map: 40.2272° N, 111.6958° W: Placed by OpenAirDocs at the center of ZIP code 84601, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=197GA
- Page: https://openairdocs.org/aircraft/N197GA

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): 41 in force

### Matched by airframe (Beech 1900C)

- [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 2014-02-03](https://openairdocs.org/ad/2014-02-03): Flight Controls · Textron 1900, 1900C and 1900D. Effective Mar 7, 2014
- [AD 2013-24-03](https://openairdocs.org/ad/2013-24-03): Stabilizers · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Jan 13, 2014
- [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 2009-23-03](https://openairdocs.org/ad/2009-23-03): Flanges · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Dec 14, 2009
- [AD 2009-23-01](https://openairdocs.org/ad/2009-23-01): Main Landing Gear · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Dec 8, 2009
- [AD 2006-18-51](https://openairdocs.org/ad/2006-18-51): Left and right wing rear spar lower caps · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Sep 8, 2006
- [AD 2005-18-21](https://openairdocs.org/ad/2005-18-21): Elevator hinge support attachments · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Sep 13, 2005
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2004-23-02](https://openairdocs.org/ad/2004-23-02): Nose Landing Gear (NLG) Fork · Textron 100, 1900, 1900C and 50 more. Effective Dec 23, 2004
- [AD 2004-17-02](https://openairdocs.org/ad/2004-17-02): Cross shaft attach bolt · Textron 100, 1900, 1900C and 52 more. Effective Oct 4, 2004
- [AD 2004-09-30](https://openairdocs.org/ad/2004-09-30): Landing Gear Electrical Power Current Limiter · Textron 1900C and 1900C (C-12J). Effective Jun 18, 2004
- [AD 2004-09-07](https://openairdocs.org/ad/2004-09-07): Canted Bulkhead Located at Fuselage Station (FS) 588.10 · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Jun 14, 2004
- [AD 2004-01-13](https://openairdocs.org/ad/2004-01-13): Vent blower assemblies · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Feb 19, 2004
- [AD 2003-20-10](https://openairdocs.org/ad/2003-20-10): Elevator Trim System Maintenance Procedures · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Oct 15, 2003
- [AD 2003-03-18](https://openairdocs.org/ad/2003-03-18): Elevator Control System · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Feb 5, 2003
- [AD 2002-23-11](https://openairdocs.org/ad/2002-23-11): Elevator Balance Weight Attachment Screws · Textron 1900, 1900C, 1900C (C-12J) and 30 more. Effective Jan 10, 2003
- [AD 2001-22-16](https://openairdocs.org/ad/2001-22-16): Engine Truss Assembly · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Dec 17, 2001
- [AD 2001-18-07](https://openairdocs.org/ad/2001-18-07): Flap Flexible Shaft Assemblies · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Oct 12, 2001
- [AD 2000-20-07](https://openairdocs.org/ad/2000-20-07): Cockpit Voice Recorder (CVR) System · Textron 1900, 1900C and 1900D. Effective Nov 22, 2000
- [AD 2000-19-04](https://openairdocs.org/ad/2000-19-04): Wing Fuel Quantity Wiring Harness · Textron 1900C, 1900C (C-12J) and 1900D. Effective Oct 31, 2000
- [AD 97-15-13 R2](https://openairdocs.org/ad/97-15-13-R2): Airstair Door Handle and Latch Housing · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective May 28, 1999
- [AD 99-04-08](https://openairdocs.org/ad/99-04-08): Main Landing Gear Hydraulic Actuators · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Mar 26, 1999
- [AD 99-01-03](https://openairdocs.org/ad/99-01-03): Flaps · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Feb 8, 1999
- [AD 98-26-16](https://openairdocs.org/ad/98-26-16): Emergency Exit Doors · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Feb 5, 1999
- [AD 98-21-20](https://openairdocs.org/ad/98-21-20): Exterior Marking Placards · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Nov 20, 1998
- [AD 97-26-15](https://openairdocs.org/ad/97-26-15): Main Landing Gear Actuator · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Jan 25, 1998
- [AD 97-25-03](https://openairdocs.org/ad/97-25-03): AFM - Limitations - Power Levers · Textron 100, 1900, 1900C and 44 more. Effective Jan 21, 1998
- [AD 97-06-06](https://openairdocs.org/ad/97-06-06): Pilot and Copilot Chairs Locking Pins · Textron 100, 1900, 1900C and 43 more. Effective May 9, 1997
- [AD 95-26-15 R1](https://openairdocs.org/ad/95-26-15-R1): Traffic Alert and Collision Avoidance Systems · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 159 more. Effective Dec 26, 1996
- [AD 96-22-12](https://openairdocs.org/ad/96-22-12): Inspect fuel filter assembly · Textron 1900C, 1900C (C-12J), 1900D and 1 more. Effective Dec 13, 1996
- [AD 96-09-13](https://openairdocs.org/ad/96-09-13): AFM - Icing · Textron 1900, 1900C, 1900D and 7 more. Effective Jun 11, 1996
- [AD 95-14-02](https://openairdocs.org/ad/95-14-02): Instrument Air System · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Aug 31, 1995
- [AD 94-20-05](https://openairdocs.org/ad/94-20-05): Hot Battery Bus · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Oct 14, 1994
- [AD 93-01-16](https://openairdocs.org/ad/93-01-16): Stall Warning Vane Housing · Textron 1900C and 1900C (C-12J). Effective Mar 8, 1993
- [AD 92-06-11](https://openairdocs.org/ad/92-06-11): Autopilot/Flight Director System Wiring · Textron 1900C, 300, B200 and 2 more. Effective Mar 30, 1992
- [AD 85-21-07 R1](https://openairdocs.org/ad/85-21-07-R1): POH/AFM Addendum · Textron 1900, 1900C and 1900C (C-12J). Effective Jul 10, 1987
- [AD 87-04-24](https://openairdocs.org/ad/87-04-24): Elevator Trim Cable System · Textron 1900, 1900C, 200 and 28 more. Effective Apr 14, 1987
- [AD 87-05-02](https://openairdocs.org/ad/87-05-02): POH/AFM Changes · Textron 1900, 1900C and 1900C (C-12J). Effective Mar 23, 1987

### Matched by engine (Pratt & Whitney Canada PT6A-60A)

- [AD 2004-25-18](https://openairdocs.org/ad/2004-25-18): Propeller governor assemblies · Pratt & Whitney Canada PT6A-60A and PT6A-65B. Effective Jan 18, 2005
- [AD 97-04-12](https://openairdocs.org/ad/97-04-12): Compressor Bleed-off Valve · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 52 more. Effective Mar 14, 1997

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

- [AD 2011-27-51](https://openairdocs.org/ad/2011-27-51) (historical): Flight Controls · Hawker Beechcraft 1900, 1900C, 1900C (C-12J) and 1 more. Effective Jan 18, 2012
- [AD 2006-24-11](https://openairdocs.org/ad/2006-24-11) (historical): Forward, vertical, and aft flanges · Hawker Beechcraft 1900C, 1900C (C-12J) and 1900D. Effective Dec 11, 2006
- [AD 97-22-16](https://openairdocs.org/ad/97-22-16) (historical): Vent Blower Assembly Bearing · Raytheon 1900, 1900C, 1900C (C-12J) and 1 more. Effective Dec 5, 1997
- [AD 97-15-13 R1](https://openairdocs.org/ad/97-15-13-R1) (historical): Airstair Door Handle And Latch Housing · Raytheon 1900, 1900C and 1900D. Effective Sep 22, 1997
- [AD 97-15-13](https://openairdocs.org/ad/97-15-13) (historical): Airstair Door Handle And Latch Housing · Raytheon 1900, 1900C and 1900D. Effective Sep 5, 1997
- [AD 97-14-16](https://openairdocs.org/ad/97-14-16) (historical): Outboard Flap Attachment Brackets And Aft Roller Bearings · Raytheon 1900, 1900C and 1900D. Effective Aug 4, 1997
- [AD 97-04-02](https://openairdocs.org/ad/97-04-02) (historical): Exterior Marking Placards For Airstair And Cargo Doors · Raytheon 1900, 1900C and 1900D. Effective Mar 10, 1997
- [AD 95-02-18](https://openairdocs.org/ad/95-02-18) (historical): Engine Truss Assembly · Raytheon 1900, 1900C and 1900D. Effective Mar 25, 1995
- [AD 87-22-01 R1](https://openairdocs.org/ad/87-22-01-R1) (historical): Nose Landing Gear Fork · Raytheon 100 Model or Series (all), 1900, 1900C and 50 more. Effective Sep 30, 1989

## Information bulletins (advisory) (6 in force)

- [SAIB CE-12-36](https://openairdocs.org/saib/CE-12-36): Flight Controls: Aileron. Issued Jun 19, 2012
- [SAIB CE-05-83](https://openairdocs.org/saib/CE-05-83): . Issued Aug 26, 2005
- [SAIB CE-00-24](https://openairdocs.org/saib/CE-00-24): . Issued Jul 11, 2000
- [SAIB CE-00-15](https://openairdocs.org/saib/CE-00-15): . Issued Jan 21, 2000
- [SAIB NE-15-21](https://openairdocs.org/saib/NE-15-21): Fuel Injector Nozzle. Issued Aug 19, 2015
- [SAIB CE-03-24](https://openairdocs.org/saib/CE-03-24): . Issued Feb 19, 2003

## NTSB investigations

None matched to N197GA.

## FAA accident and incident reports (3)

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 20041108030629I](https://openairdocs.org/incident/20041108030629I), Nov 8, 2004: Beech 1900C (N197GA), Honolulu, HI, Minor damage. (-23) On visual approach to runway 8L at hnl, pilot failed to lower landing gear. Pilot claimed he lowered the landing gear and had three green lights, did not…
- [Incident 19990924039949I](https://openairdocs.org/incident/19990924039949I), Sep 24, 1999: Beech 1900C (N197GA), Ft Lauderdale, FL. Aircraft reported instrument out, request to reutrn to fll. A.t.c. in passing info mia center to fll ATCT reported engine out instead attitude indictator, f/o,…
- [Incident 19971031040639I](https://openairdocs.org/incident/19971031040639I), Oct 31, 1997: Beech 1900C (N197GA), Ft Lauderdale, FL. Narrative: on takeoff from fll after passing through 500' captain and first officer observed smoke coming from under the first officers instrument panel. Pilot…

## Service difficulty reports (22)

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 TIMA201912110001](https://openairdocs.org/sdr/TIMA201912110001), Dec 9, 2019: WINDSHIELD. CRACKED. CLIMBED TO 15,000 FT AND HEARD A NOISE THEN NOTICED A CRACK IN WINDSHIELD. CRACK COULD NOT BE FELT ON THE INSIDE. AIRCRAFT RETURNED TO BASE.
- [SDR TIMA2018103100001](https://openairdocs.org/sdr/TIMA2018103100001), Oct 30, 2018: HOSE. CHAFED. ENGINE WAS SHUTDOWN IN FLIGHT AFTER TORQUE AND OIL PRESSURE FLUCTUATIONS. INSPECTION REVEALED THAT THE OIL HOSE CONNECTED BETWEEN THE ENGINE AND OIL COOLER HAD 
- [SDR TIMA20161125017](https://openairdocs.org/sdr/TIMA20161125017), Nov 25, 2016: DOUBLER. CRACKED. DURING A SCHEDULED SIM CHECK, CRACKS WERE DISCOVERED IN THE DOUBLERS OF THE HORIZONTAL STABILIZER FORWARD ATTACHMENT TO THE VERTICAL STABILIZER. TWO, ONE INCH C
- [SDR TIMA20151004005](https://openairdocs.org/sdr/TIMA20151004005), Oct 4, 2015: FASTENER. MISSING. DURING TAKEOFF ROLL, THE RT POWER LEVER DID NOT PROVIDE FULL TRAVEL. TAKEOFF TORQUE COULD NOT BE ACHIEVED ON THE RT ENG & THE TAKEOFF WAS ABORTED. SUBSEQUENT IN
- [SDR TIMA20140811022](https://openairdocs.org/sdr/TIMA20140811022), Aug 11, 2014: SUPPORT. CORRODED. DURING MX INSPECTION THE RT SIDE SEAT SUPPORT RAIL WAS FOUND TO BE CORRODED.
- [SDR TIMA20140811021](https://openairdocs.org/sdr/TIMA20140811021), Aug 11, 2014: SUPPORT. CORRODED. DURING MX INSPECTION THE LT SIDE SEAT SUPPORT RAIL WAS FOUND TO BE CORRODED.
- [SDR TIMA20110004](https://openairdocs.org/sdr/TIMA20110004), Jul 8, 2011: SKIN. CORRODED. DISCOVERED CORROSION DAMAGE ON THE FUSELAGE BELLY SKINS DURING VISUAL INSPECTION. REPAIRED SKINS USING COVER PATCH METHOD IAW BEECH SRM 51-70-6.
- [SDR TIMA20110003](https://openairdocs.org/sdr/TIMA20110003), Jul 8, 2011: SKIN. CORRODED. DISCOVERED CORROSION DAMAGE ON THE FUSELAGE BELLY SKINS DURING VISUAL INSPECTION. REPAIRED SKINS USING COVER PATCH METHOD IAW BEECH SRM 51-70-6.
- [SDR TIMA20080007](https://openairdocs.org/sdr/TIMA20080007), Oct 28, 2008: LIMIT SWITCH. BROKEN. THE LANDING GEAR DID NOT EXTEND WHEN SELECTED. THE PILOT MANUALLY PUMPED THE GEAR DOWN AND LANDED. INVESTIGATION REVEALED THAT THE LT UP-LIMIT ELECTRICAL SWITCH
- [SDR TIM2006F00000](https://openairdocs.org/sdr/TIM2006F00000), Jan 17, 2006: RELAY. FAILED. LANDING GEAR DID NOT EXTEND WHEN SELECTED. PILOT EXTENDED GEAR MANUALLY AND LANDED WITHOUT INCIDENT. MAINTENANCE DETERMINED THAT THE HYDRAULIC POWER PACK MOTOR 
- [SDR 20010216SG005](https://openairdocs.org/sdr/20010216SG005), Jan 20, 2001: BOLT. LOOSE. FLT 9391 - EYW - DURING TAKEOFF, RIGHT FIREWALL FUEL VALVE T-HANDLE ILLUMINATED. ALL ENGINE INSTRUMENTS INDICATED NORMAL. TIGHTENED BOLT ON RIGHT EXHAUST FLEX H
- [SDR 98ZZZX2872](https://openairdocs.org/sdr/98ZZZX2872), Jul 19, 1998: LINE. CRACKED. TCB/MIA - FLT 9138 - GEAR WARNING INOPERABLE. REMOVED AND REPLACED MANUAL BLEED VALVE LINE AT LANDING GEAR POWER PACK. (X)
- [SDR 98ZZZM151](https://openairdocs.org/sdr/98ZZZM151), Dec 29, 1997: SWITCH. INTERMITTENT. FLT 7153 - FPO-FLL - LANDING GEAR WON'T RETRACT. AIRCRAFT FERRIED TO MIA. REMOVED AND REPLACED LANDING GEAR SQUAT SWITCH.
- [SDR 98ZZZM150](https://openairdocs.org/sdr/98ZZZM150), Dec 28, 1997: RETRACT MECH. MALFUNCTIONED. FLT 7201 - FLL-TCS - LANDING GEAR EXTENDED WHILE INFLIGHT WITH GEAR HANDLE IN THE UP POSITION. AIRCRAFT DIVERTED TO FPO AND WAS FERRIED TO MIA. SERVICED AIRCRAF
- [SDR 98ZZZM149](https://openairdocs.org/sdr/98ZZZM149), Dec 24, 1997: RETRACT MECH. MALFUNCTIONED. FLT 7406 - MCO-MIA - LANDING GEAR WOULD NOT RETRACT ON TAKEOFF. AIRCRAFT RETURNED TO MCO AND WAS FERRIED TO MIA. WITH AIRCRAFT ON JACKS, PERFORMED SEVERAL LANDI
- [SDR 99ZZZX736](https://openairdocs.org/sdr/99ZZZX736), Nov 3, 1997: SWITCH. OUT OF ADJUST. MIA/EYW - FLT 7418 - PILOT REPORT: GEAR WOULD NOT RAISE AFTER DEPARTURE. NO HYDRAULIC LIGHT ILLUMINATED. AIRCRAFT RETURNED TO MIA. ADJUSTED SQUAT SWITCH. OPS CH
- [SDR 98ZZZX1946](https://openairdocs.org/sdr/98ZZZX1946), Oct 31, 1997: AIR DISTRIBUTION. VAPOR. FLL/NAS - FLT 7477 - PILOT REPORT: ON CLIMB-OUT, VAPOR SMOKE COMING FROM INSIDE FIRST OFFICER'S PANEL. ACCESSED COPILOT'S PANELS, RAN AIRCRAFT, OPERATED ALL SYS
- [SDR 97ZZZM1096](https://openairdocs.org/sdr/97ZZZM1096), Oct 9, 1997: CONNECTOR. DIRTY. FLT 7219 - FLL/TPA - LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO FLL AND WAS FERRIED TO MIA. INSPECTED AND CLEANED LANDING GEAR SWITCHES AND CANNON PLU
- [SDR 97ZZZM741](https://openairdocs.org/sdr/97ZZZM741), Jun 30, 1997: FIRE WARNING. ILLUMINATED. FLT 7159 - NAS-FLL - LEFT 'T' HANDLE ILLUMINATED AND EXTINGUISHED SEVERAL TIMES IN FLIGHT. AIRCRAFT FERRIED TO MIA, INSPECTED LEFT ENGINE AND NACELLE AREA AND R
- [SDR 97ZZZM524](https://openairdocs.org/sdr/97ZZZM524), Apr 1, 1997: RETRACT MECH. MALFUNCTIONED. FLT 423 - FLL/FPO - GEAR WOULD NOT GO DOWN AFTER 2 ATTEMPTS, UNTIL GO AROUND WAS INITIATED. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS FERRIED TO MIA WITH G
- [SDR 97ZZZM525](https://openairdocs.org/sdr/97ZZZM525), Mar 23, 1997: RETRACT MECH. MALFUNCTIONED. FLT 447 - FLL-MHH - LANDING GEAR MANUALLY EXTENDED. FERRIED AIRCRAFT TO MIA, INSPECTED WIRING BEHIND INSTRUMENT PANEL AND IN WING ROOT WITH AIRCRAFT ON JACKS, C
- [SDR 97ZZZM414](https://openairdocs.org/sdr/97ZZZM414), Mar 14, 1997: MLG. FOD. FLT 485 - TLH-TPA - DOG STRIKE/RIGHT MAIN GEAR INDICATES UNLOCKED. INSPECTED, FERRIED A/C TO MIAMI FROM TLH. ADJUSTED BOTH UPLOCK AND DOWNLOCK SWITCHES, PERFORM

## STCs that may be installed (OpenAirDocs) (176, 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 (Beech 1900C)

- [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC
- [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC
- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA02133SE](https://openairdocs.org/stc/SA02133SE): Installation of a Luma Technologies LT-4500 Series Integrated Light\Emitting Diode (LED) Display Panel and LT-3500 LED light modules. Luma Technologies LLC
- [STC SA12345IB](https://openairdocs.org/stc/SA12345IB): Replacement of the Halon Type 1211 portable fire extinguisher with the Halotron BrX portable fire extinguisher. Cessna Duesseldorf Citation Service Center GmbH
- [STC SA02355AK](https://openairdocs.org/stc/SA02355AK): Installation of cargo barrier net; Tednologies Inc.(TI) P/N 150A-28-000. Tednologies Inc
- [STC SA11158SC](https://openairdocs.org/stc/SA11158SC): Demonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS). Liberty Partners Inc
- [STC SA12202IB](https://openairdocs.org/stc/SA12202IB): Installation of Garmin GWX Weather Radar System. Maxcraft Avionics Ltd
- [STC SA11300DS](https://openairdocs.org/stc/SA11300DS): Upgrade previously installed Collins Aerospace Radar Altimeter. BHE & Associates Ltd
- [STC SA6085NM](https://openairdocs.org/stc/SA6085NM): Installation of interior fluorescent cabin lighting system. Bruce Aerospace Inc
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA106CH](https://openairdocs.org/stc/SA106CH): Installation of TCAS 791 Traffic Alert and Collision Avoidance System I (TCAS I). Acron Aviation Inc
- [STC SA8655SW](https://openairdocs.org/stc/SA8655SW): Installation of interfaced provisions only for TCAS791 Traffic Alert and Collision Avoidance System I (TCAS I). Acron Aviation Inc
- [STC ST00687DE](https://openairdocs.org/stc/ST00687DE): Installation of Tropospheric Airborne Meteorological Data Reporting (TAMDAR) System. FLYHT Inc
- [STC ST02754NY](https://openairdocs.org/stc/ST02754NY): Replacement of JET PS835C or PS835D Battery packs with Securaplane XL244-D Battery Packs. Securaplane Technologies Inc
- [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC
- [STC SA00322BO](https://openairdocs.org/stc/SA00322BO): Installation of a Supplemental Exterior Lighting System. ATI Engineering Services LLC
- [STC SA04051CH](https://openairdocs.org/stc/SA04051CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC
- [STC SA00199IB](https://openairdocs.org/stc/SA00199IB): Manufacture and Installation, Emergency Evacuation Configuration. Bartel Mechanical and Aerospace
- [STC SA01050WI](https://openairdocs.org/stc/SA01050WI): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC. Lists 1900 Series
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA00128IB](https://openairdocs.org/stc/SA00128IB): Antenna Installation and Bulkhead Feedthrough. Avmax Aviation Services Inc
- [STC SA00120IB](https://openairdocs.org/stc/SA00120IB): Installation of the Universal Kapture Cockpit Voice Recorder (CVR) with Recorder Independent Power Supply (RIPS). Avmax Aviation Services Inc
- [STC SA02821AT](https://openairdocs.org/stc/SA02821AT): Installation of a Sandel Model ST3400 Terrain Awareness and Warning System (TAWS), with optional capability as a Traffic Collision Avoidance System (TCAS) Control Display Unit (CDU) or Radio Magnetic Indicator (RMI). Woven Electronics LLC
- [STC SA13BO](https://openairdocs.org/stc/SA13BO): Installation of a Sundstrand Mark VI ground proximity warning system. Woven Electronics LLC
- [STC SA14BO](https://openairdocs.org/stc/SA14BO): Installation of a Collins ALT-55B radio altimeter. Woven Electronics LLC
- [STC SA02010WI](https://openairdocs.org/stc/SA02010WI): Installation of the Mid-Continent Instruments & Avionics MD23 FLEX Custom Function Display (CFD). Mid-Continent Instruments and Avionics
- [STC SA00741WI](https://openairdocs.org/stc/SA00741WI): Installation of the Concorde RG-380E/K series VRSLA batteries in airplanes listed on the attached FAA approved Model List (AML). Aero-Mach Wilco LLC
- [STC SA02204CH](https://openairdocs.org/stc/SA02204CH): Installation of Parker Hannifin Nose Wheel conversion Kit. Kaman Corporation Aircraft Wheel and Brake LLC
- [STC SA1789GL](https://openairdocs.org/stc/SA1789GL): Installation of Cleveland main wheels and brakes. Kaman Corporation Aircraft Wheel and Brake LLC
- [STC SA01094DE](https://openairdocs.org/stc/SA01094DE): Installation of Pratt & Whitney Engine Services FAST (digital engine management) system. Pratt & Whitney Engine Services Inc
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA02562AK](https://openairdocs.org/stc/SA02562AK): Installation of L3 Aviation Products Model FA5000 Flight Data Recorder (FDR) System. ACE Air Cargo
- [STC SA04634NY](https://openairdocs.org/stc/SA04634NY): Modification of the Brake Master Cylinder. Marsh Brothers Aviation Inc
- [STC SA04459NY](https://openairdocs.org/stc/SA04459NY): Installation of MT-Propeller Entwicklung GmbH model MTV-27-1-( )-C-F-R(P)/CFR260-65( ) 5-blade, constant speed, full feathering, reversible propellers and spinners. MT- Propeller Entwicklung GmbH
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA04514NY](https://openairdocs.org/stc/SA04514NY): Single/Dual Transponder System ADS-B Upgrade. Scandinavian Avionics Design ApS
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit. Med-Pac Inc
- [STC SA02677LA](https://openairdocs.org/stc/SA02677LA): Modification to upgrade the existing Mode S Transponder system by installing the ACSS NXT-700 Transponder with ADS-B Out and optionally install the ACSS NXG-900 GPS as the position source for ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC SA02678LA](https://openairdocs.org/stc/SA02678LA): Modification to upgrade the existing Mode S Transponder system by installing the ACSS NXT-600 Transponder with ADS-B Out and optionally install the ACSS NXG-900 GPS as the position source for ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc
- [STC SA01002DE](https://openairdocs.org/stc/SA01002DE): Installation of Garmin G700 TXi display and sensor system. Alaska Central Express Inc
- [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies
- [STC SA01923WI](https://openairdocs.org/stc/SA01923WI): Installation of an Auxiliary Aural Alert System. Hawker Pacific Pty Ltd
- [STC SA01213CH](https://openairdocs.org/stc/SA01213CH): Install air ambulance conversion in accordance with Spectrum Aeromed Inc. Drawings as listed on AML SA01213CH, or later FAA approved revision. Spectrum Aeromed LLC dba Spectrum Aeromed
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA01867WI](https://openairdocs.org/stc/SA01867WI): CoolView Flight Compartment Side and Storm Windows Installation. See attached AML No. SA01867WI for required data. Lee Aerospace, Inc
- [STC SA02194AK](https://openairdocs.org/stc/SA02194AK): Reduction/limitation of passenger seats to nine (9). Hageland Aviation Services, Inc

All 176: https://openairdocs.org/aircraft/N197GA/stcs.md

## Related

- Other Beech 1900C aircraft: https://openairdocs.org/model/beech-1900c/aircraft.md
- The Pratt & Whitney Canada PT6A-60A engine: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-60a.md

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