# N153GA: 1985 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-34
- Year built: 1985
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: March 1, 1985
- Certificate issued: September 17, 2013
- Expires: September 30, 2029
- Mode S code: A0D5EB
- 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=153GA
- Page: https://openairdocs.org/aircraft/N153GA

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 N153GA.

## FAA accident and incident reports (4)

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 20140108000109I](https://openairdocs.org/incident/20140108000109I), Jan 8, 2014: Beech 1900C (N153GA), Great Falls, MT, Minor damage. On January 8, 2014, at 1800 hrs MST, a Beech 1900G while taxing on alpha to A1, was turning to runway 21 and turned short. Struck taxiway light and stopped in…
- [Incident 20090820049539I](https://openairdocs.org/incident/20090820049539I), Aug 20, 2009: Beech 1900C (N153GA), Grand Forks, ND, Minor damage. Upon completion of a successful landing on runway 35L, aircraft utilized taxiway a and contacted barricades that were in place and notamed. Aircraft sustained…
- [Incident 20041115032579I](https://openairdocs.org/incident/20041115032579I), Nov 15, 2004: Beech 1900C (N153GA), Hilo, HI, Minor damage. (-23) On ramp at Hilo airport, pilot closed airstair door from outside. When finished unloading cargo, he proceeded through inside of aircraft to cockpit…
- [Incident 20010906023649I](https://openairdocs.org/incident/20010906023649I), Sep 6, 2001: Beech 1900C (N153GA), Childress, TX. (-23) Flight AIP511 from abq to dfw was a cargo flight with no passengers but did have live animals. The pilot and flight observer smelled fumes from…

## Service difficulty reports (30)

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 TIMA202207130008](https://openairdocs.org/sdr/TIMA202207130008), Jul 12, 2022: ENGINE. SHUTDOWN. PS NORMAL THROUGH 10,000 FT. CLIMBING THROUGH ABOUT 10500 FT THE PILOT NOTICED THE RH TORQUE GAUGE BEGIN TO FALL, THEN THE RH OIL PRESSURE LIGHT CAME ON. PILOT 
- [SDR TIMA20211220002](https://openairdocs.org/sdr/TIMA20211220002), Dec 7, 2021: UNKNOWN. UNKNOWN. GOT SMOKE/HAZE IN THE COCKPIT ONCE LEVELED IN CRUISE. TURNED BACK TO BIL AND SHUT OFF THE BLEED VALVES. ONCE BLEED VALVES WERE OFF THE COCKPIT CLEARED. LANDED A
- [SDR TIMA20161213019](https://openairdocs.org/sdr/TIMA20161213019), Dec 13, 2016: WINDSHIELD. CRACKED. THE PILOT’S SIDE WINDSHIELD CRACKED DURING FLIGHT. THERE WAS A 3 INCH WIDE BAND OF SHATTERING OF THE OUTER LAYER THAT RAN FROM THE TOP TO THE BOTTOM OF THE WIND
- [SDR TIMA20130830009](https://openairdocs.org/sdr/TIMA20130830009), Aug 30, 2013: SKIN. CORRODED. CORROSION FOUND ON BELLY OF ACFT UNDER ADF ANTENNA BS 183.25. REPAIRED.
- [SDR KGBR507Y201105250](https://openairdocs.org/sdr/KGBR507Y201105250), May 25, 2011: SKIN PANEL. CRACKED. CRACK IN SKIN PANEL .5 INCH FWD OF THE TRAILING EDGE, 4.5 INCHES TO 10.5 INCHES FROM THE INBOARD EDGE OF THE FLAP. ALSO ARE 2 CRACKS IN THE AREA OF THE INBOARD 
- [SDR TIMA2010000011](https://openairdocs.org/sdr/TIMA2010000011), Mar 10, 2010: SEAT TRACK. CORRODED. LEFT SIDE SEAT RAIL CORRODED.
- [SDR TIM2005F00000](https://openairdocs.org/sdr/TIM2005F00000), Dec 28, 2004: BLADE. BROKEN. AIRCRAFT DEPARTED AT CRUISE. THE LT ENGINE HAD AN EXPLOSIVE NOISE AND THE LT ENGINE SEIZED. PRE-INSPECTION OF ENGINE INDICATES LOSS OF CT BLADE. (K)
- [SDR 2005FA0000006](https://openairdocs.org/sdr/2005FA0000006), Dec 28, 2004: BLADE. BROKEN. AIRCRAFT DEPARTED, AT CRUISE, THE LT ENGINE HAD AN EXPLOSIVE NOISE AND THE LEFT ENGINE SEIZED. PRE INSPECTION OF ENGINE INDICATES LOSS OF CT BLADE. (K)
- [SDR 2005FA0000005](https://openairdocs.org/sdr/2005FA0000005), Nov 16, 2004: CABLE. BROKEN. ON CLIMBOUT THE AIRSTAIR DOOR OPENED. AC RETURNED, WHEN AIRSTAIR DOOR OPENED IN FLIGHT, DOOR DAMPER BROKE AND SUPPORT CHAINS BROKE. CHAIN HIT PROPELLER AND CAUS
- [SDR TIM2001F00010](https://openairdocs.org/sdr/TIM2001F00010), Oct 15, 2001: BULKHEAD. CRACKED. THE RIGHT ENGINE COWLING BULKHEAD AT STATION 238.18 THAT THE LOWER FRONT ENGINE COWLING ATTACHES TO WAS CRACKED ON THE RIGHT LOWER SIDE. THIS LOCATION IS WERE O
- [SDR 2001F00624](https://openairdocs.org/sdr/2001F00624), Oct 4, 2001: SHAFT. DAMAGED. INSPECTION OF THE FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE CABLES DIAGONAL WRAP TO BE UNWINDING. CONTINUED INSPECTION REVEALE
- [SDR 2001F00622](https://openairdocs.org/sdr/2001F00622), Oct 4, 2001: SHAFT. DAMAGED. INSPECTION OF THE FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE CABLES DIAGONAL WRAP TO BE UNWINDING. CONTINUED INSPECTION REVEALE
- [SDR 2001F00621](https://openairdocs.org/sdr/2001F00621), Oct 4, 2001: SHAFT. DAMAGED. INSPECTION OF THE FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE CABLES DIAGONAL WRAP TO BE UNWINDING. CONTINUED INSPECTION REVEALE
- [SDR TIM2001F00008](https://openairdocs.org/sdr/TIM2001F00008), Sep 6, 2001: MOTOR. SHORTED. AIRCRAFT FILLED WITH SMOKE, CREW MADE AN EMERGENCY LANDING. CHECK OF AIRCRAFT SYSTEMS FOUND THE FORWARD EVAPORATOR MOTOR SHORTED. AIRCRAFT WAS FURTHER INSPECTED
- [SDR 20010507CW019](https://openairdocs.org/sdr/20010507CW019), Mar 7, 2001: STRINGER. CORRODED. INSPECTION REVEALED A .6 INCH SECTION OF FUSELAGE STRINGER 14L CORRODED AT APPROX F.S. 250 FUSELAGE SKIN WAS NOT DAMAGED.
- [SDR 20010507CW015](https://openairdocs.org/sdr/20010507CW015), Mar 7, 2001: BRACKET. CORRODED. INSPECTION DISCOVERED SIGNIFICANT CORROSION ON 2 RT ELEVATOR HINGE BRACKETS.
- [SDR 20010507CW014](https://openairdocs.org/sdr/20010507CW014), Mar 7, 2001: BRACKET. CORRODED. INSPECTION DISCOVERED SIGNIFICANT CORROSION ON 2 RT ELEVATOR HINGE BRACKETS.
- [SDR 20010507CW008](https://openairdocs.org/sdr/20010507CW008), Mar 7, 2001: FLOOR SUPPORT. CORRODED. 4 FLOOR SUPPORT BRACKETS WERE FOUND WITH SIGNIFICANT CORROSION ON THE TOP SURFACE WHERE THEY ARE IN CONTACT WITH THE HONEYCOMB FLOOR PANEL.
- [SDR 20010507CW007](https://openairdocs.org/sdr/20010507CW007), Mar 7, 2001: FLOOR SUPPORT. CORRODED. 4 FLOOR SUPPORT BRACKETS WERE FOUND WITH SIGNIFICANT CORROSION ON THE TOP SURFACE WHERE THEY ARE IN CONTACT WITH THE HONEYCOMB FLOOR PANEL.
- [SDR 20010507CW006](https://openairdocs.org/sdr/20010507CW006), Mar 7, 2001: BRACKET. WORN. INSPECTION FOUND ALL FLAP TRACK BRACKETS WORN BEYOND ACCEPTABLE LIMITS.
- [SDR 20010507CW005](https://openairdocs.org/sdr/20010507CW005), Mar 7, 2001: BRACKET. WORN. INSPECTION FOUND ALL FLAP TRACK BRACKETS WORN BEYOND ACCEPTABLE LIMITS.
- [SDR 20001228AP001](https://openairdocs.org/sdr/20001228AP001), Aug 28, 2000: FIRE LOOP. SHORTED. FLT 9141 - TPA-RSW - DURING FLIGHT, LEFT ENGINE FIRE INDICATION OCCURRED. PRECAUTIONARY SHUTDOWN AND DISCHARGE OF ENGINE FIRE BOTTLE CARRIED OUT. REMOVED AND RE
- [SDR 20000725AP005](https://openairdocs.org/sdr/20000725AP005), Apr 19, 2000: HINGE. CORRODED. DURING SCHEDULED MAINTENANCE, LEFT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED LEFT 
- [SDR 20000427AP008](https://openairdocs.org/sdr/20000427AP008), Feb 8, 2000: ENGINE. FAILED. FLT 9330 - TPA-JAX - WHILE IN DESCENT INTO JACKSONVILLE AT 10,000 FT, A LOUD SQUEALING NOISE WAS HEARD. LEFT ENGINE INDICATED ITT AND TORQUE FLUCTUATIONS. PILOT
- [SDR 98ZZZX2870](https://openairdocs.org/sdr/98ZZZX2870), May 24, 1998: SWITCH. FAILED. TPA/MIA - FLT 7485 - LANDING GEAR INDICATOR CIRCUIT BOARD TRIPS WHEN GEAR RETRACTS AND WILL NOT RESET UNTIL GEAR IS DOWN AND LOCKED. REMOVED AND REPLACED GEAR U
- [SDR 99ZZZX733](https://openairdocs.org/sdr/99ZZZX733), Jun 22, 1997: SWITCH. OUT OF AJDUST. FPO/MIA - FLT 7410 - PILOT REPORT: CANNOT SILENCE WARNING HORN FOR GEAR. ADJUSTED BOTH LEFT AND RIGHT POWER LEVER SWITCHES. (X)
- [SDR 97ZZZM729](https://openairdocs.org/sdr/97ZZZM729), May 27, 1997: RELAY. SHORTED. FLT 7168 - MCO-FLL, UNABLE TO LOWER GEAR, BREAKER POPPED, HYDRAULIC FLUID LOW LIGHT ILLUMINATED. MANUAL EXTENSION ACCOMPLISHED. AIRCRAFT LANDED WITHOUT INCIDENT
- [SDR 97ZZZM527](https://openairdocs.org/sdr/97ZZZM527), Mar 3, 1997: SWITCH. INTERMITTENT. FLT 398 - TCB/FLL - LANDING GEAR LIGHT (INTRANSIT) WOULD NOT GO OFF WHEN LANDING GEAR WAS RETRACTED. NO EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. AI
- [SDR 97ZZZM150](https://openairdocs.org/sdr/97ZZZM150), Dec 25, 1996: BRAKES. INOPERATIVE. FLT 437 - TPA-MIA - RIGHT BRAKE INOP, SLIPS. CLEANED AND SERVICED BRAKES. OK FOR SERVICE. (M)
- [SDR 96ZZZX5988](https://openairdocs.org/sdr/96ZZZX5988), Nov 1, 1996: WARNING LIGHT. MALFUNCTIONED. EYW/MIA - FLT 403 - PILOT REPORT: WHEELS WARNING LIGHT WILL NOT COME ON IN-FLIGHT. SYSTEM FUNCTIONS PROPERLY WHEN RETARDING POWER LEVERS BACK TO ACTUATE WARNING

## 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/N153GA/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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