# N113AX: 1988 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: UC-41
- Year built: 1988
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: September 30, 1988
- Certificate issued: August 28, 1997
- Expires: January 31, 2028
- Mode S code: A0376E
- Registered owner: [Alaska Central Express Inc](https://openairdocs.org/faa-owner/ALASKA%20CENTRAL%20EXPRESS%20INC)
- Location: [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage)
- Owner type: Corporation
- Owner's area on the map: 61.1637° N, 149.9966° W: Placed by OpenAirDocs at the center of ZIP code 99502, 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=113AX
- Page: https://openairdocs.org/aircraft/N113AX

From the FAA registry file of October 22, 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 N113AX.

## 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 20250503014099I](https://openairdocs.org/incident/20250503014099I), May 3, 2025: Beech 1900C (N113AX), Anchorage, AK, No damage. On 05/03/2025, at approx.1214 local, a Beechcraft 1900C model aircraft departed runway 25L at anc for the purpose of first officer training. Shortly after…
- [Incident 20200418000959I](https://openairdocs.org/incident/20200418000959I), Apr 18, 2020: Beech 1900C (N113AX), Anchorage, AK, Minor damage. 4/20/2020 - Contacted by flm on 4/18/2020 regarding an aircraft incident which involved a BE-1900-C aircraft operated by Alaska central express (ace)…
- [Incident 20120116000829I](https://openairdocs.org/incident/20120116000829I), Jan 16, 2012: Beech 1900C (N113AX), Anchorage, AK, Minor damage. PIC requested use of taxiway mike from taxiway romeo for takeoff on runway 32. PIC followed centerline of taxiway mike at first then steered left followed by a…

## Service difficulty reports (48)

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 YADA2023110401](https://openairdocs.org/sdr/YADA2023110401), Nov 4, 2023: HOUSING. ERODED. PILOT REPORTED SEEING OIL ON RH WING DURING PREFLIGHT. MAINTENANCE IDENTIFIED A LEAK FROM A HOLE IN THE RH ENGINE OIL SCAVENGE PUMP HOUSING AND REPLACED SAME. T
- [SDR YADA2023092101](https://openairdocs.org/sdr/YADA2023092101), Sep 21, 2023: MASTER CYLINDER. FAILED. PILOT REPORTED AFTER LANDING AND DURING TAXI "PILOT SIDE LEFT BRAKE GOES FLAT". MAINTENANCE PERFORMED TROUBLESHOOTING AND FOUND THAT THE PILOTS LEFT PEDAL BRAKE
- [SDR YADA20230313001](https://openairdocs.org/sdr/YADA20230313001), Mar 11, 2023: BELLCRANK. CRACKED. WHILE PERFORMING A COMPANY FLEET CAMPAIGN DISCOVERED FORWARD ELEVATOR BELLCRANK CRACKED WEB.
- [SDR YADA202212164001](https://openairdocs.org/sdr/YADA202212164001), Dec 14, 2022: LATCH. OUT OF ADJUST. PILOT REPORTED SMOKE FROM RT CIRCUIT BREAKER PANEL, NR 2 AVIONICS BREAKER MELTED, COMM 2 AND ADF 1 BREAKERS ALSO SMOKED. AIRCRAFT RETURNED TO AIRPORT OF ORIGIN.
- [SDR YADA20190103001](https://openairdocs.org/sdr/YADA20190103001), Jan 3, 2019: SCAVENGE PUMP. LEAKING. AFTER LANDING, CREW NOTICED ENGINE OIL ON LT WING. MAINTENANCE LOCATED OIL LEAK AT NR 1 ENGINE OIL SCAVENGE PUMP HOUSING AND REPLACED SAME. REMOVED HOUSING VERI
- [SDR YADA20180118001](https://openairdocs.org/sdr/YADA20180118001), Jan 18, 2018: SCAVENGE PUMP. LEAKING. MAINTENANCE DISCOVERED THAT THE NR 2 ENGINE OIL SCAVENGE PUMP HOUSING WAS LEAKING THROUGH THE CASTING. OIL SCAVENGE PUMP HOUSING WAS REMOVED AND REPLACED.
- [SDR YADA20170926002](https://openairdocs.org/sdr/YADA20170926002), Sep 26, 2017: DOOR FRAME. CRACKED. WHILE PERFORMING MAINTENANCE INSPECTION DURING A,B,C CHECK FOUND CRACK ON CARGO DOOR FRAME P/N:114-430125-5 AT F.S.: 509.50 . CRACK IS 1.6 INCHES LONG AND BEYON
- [SDR YADA20170926001](https://openairdocs.org/sdr/YADA20170926001), Sep 26, 2017: DOOR FRAME. CRACKED. WHILE PERFORMING MAINTENANCE INSPECTION DURING A,B,C CHECK FOUND MULTIPLE CRACKS AT AIRSTAIR DOOR FRAME. ONE LOCATED ON FRAME P/N:114-420041-37 AND ONE LOCATED 
- [SDR YADA20160109001](https://openairdocs.org/sdr/YADA20160109001), Jan 9, 2017: GUSSET. CRACKED. DURING MAINTENANCE A,B,C STRUCTURAL INSPECTION, FOUND LT INTERCOSTAL GUSSET CRACKED AT FUSELAGE STATION 107. PART HAS BEEN REMOVED AND REPLACED IAW STRUCTURAL R
- [SDR YADA20161130001](https://openairdocs.org/sdr/YADA20161130001), Nov 29, 2016: WINDSHIELD. CRACKED. LT WINDSHIELD CRACKED INFLIGHT.
- [SDR YADA20161029001](https://openairdocs.org/sdr/YADA20161029001), Oct 29, 2016: GROUND WIRE. DISCONNECTED. DURING DEPARTURE, RECIEVED A BATTERY CHARGE LIGHT THAT DID NOT EXTINGUISH. RETURNED TO DEPARTURE. RECONNECTED BATTERY GROUND TERMINAL AND PERFORMED OPS CHECKED 
- [SDR YADA20160815001](https://openairdocs.org/sdr/YADA20160815001), Aug 15, 2016: WIRE. CHAFED. SMOKE COMING FROM RIGHT WING TIP IN VICINITY OF FUEL VENT, FUEL FOUND ON UNDERSIDE OF WING NEAR HEATED FUEL VENT. MAINTENANCE REPLACED FUEL VENT ON RT WING DUE 
- [SDR YADA20160611001](https://openairdocs.org/sdr/YADA20160611001), Jun 11, 2016: UNKNOWN. ODOR. WITH LT BLEED AIR OPEN EXHAUST ODOR IN CABIN, MAINTENANCE COULD NOT DUPLICATE ON GROUND RUNS. ACFT GOING INTO CAMP INSPECTION.
- [SDR YADA20160308001](https://openairdocs.org/sdr/YADA20160308001), Mar 8, 2016: FRAME. CORRODED. DURING STRUCTURAL INSPECTION, CORROSION WAS FOUND ON TOP FLANGE OF FUSELAGE FRAME AT FS 468.25. SUSPECT CORROSION WAS CAUSED BY CARGO SPILLAGE. FRAME WAS REPAIR
- [SDR YADA20151130001](https://openairdocs.org/sdr/YADA20151130001), Nov 30, 2015: UPLOCK SWITCH. SHORTED. LANDING GEAR UNSAFE INDICATION, AFTER RETRACTION, RED LIGHT IN HANDLE. ACFT LANDED UNEVENTFULLY AT AIRPORT OF ORIGIN. IDENTIFIED & REPLACED A FAULTY NOSE GEAR U
- [SDR YADA20151009001](https://openairdocs.org/sdr/YADA20151009001), Oct 9, 2015: CLEVIS PIN. MISSING. PILOT REPORTED COPILOT RT RUDDER PEDAL DISCONNECTED FROM MASTER CYLINDER. REPLACED A MISSING CLEVIS PIN & RELATED COTTER PIN.
- [SDR YADA20150930001](https://openairdocs.org/sdr/YADA20150930001), Sep 30, 2015: FAN. FAILED. PIREP SMELL OF ELEC BURNING IN FLIGHT. CREW ELECTED TO RETURN TO DEPARTURE AIRPORT & LANDED WITHOUT INCIDENT. MX VERIFIED THE RECIRCULATION FAN HAD INTERMITTENT
- [SDR YADA20150725001](https://openairdocs.org/sdr/YADA20150725001), Jul 25, 2015: WARNING LIGHT. INOPERATIVE. LANDING UNSAFE LIGHT & LANDING POSITION LIGHT INOPERATIVE DURING LANDING. PERFORMED FLYBY & EMERGENCY GEAR EXTENSION IAW QRH. AN UNEVENTFUL LANDING WAS PERFORME
- [SDR YADA20141218001](https://openairdocs.org/sdr/YADA20141218001), Dec 18, 2014: HYDRAULIC LINE. RUPTURED. ON APPROACH FLIGHT CREW SELECTED LANDING GEAR DOWN. THE NOSE GEAR FAILED TO COMPLETELY EXTEND & LOCK, LANDING GEAR PUMP CONTINUED TO RUN. THE PILOT PULLED THE L
- [SDR YADA20140516002](https://openairdocs.org/sdr/YADA20140516002), May 16, 2014: ANGLE. CRACKED. CRACK IN VERTICAL STABILIZER FWD SPAR LT ANGLE AT ATTACH BRACKET FASTENER. SEE SB 55-4114 & AD 2013-24-03.
- [SDR YADA20140516001](https://openairdocs.org/sdr/YADA20140516001), May 16, 2014: ANGLE. CRACKED. CRACKS IN VERTICAL STABILIZER FWD SPAR RT ANGLE AT BRACKET ATTACH FASTENERS.
- [SDR YADA20140514001](https://openairdocs.org/sdr/YADA20140514001), May 14, 2014: SPAR. CRACKED. FOUND CRACKS IN HORIZONTAL STABILIZER AFT CENTER SPAR WEB.
- [SDR YADA2014051700327](https://openairdocs.org/sdr/YADA2014051700327), May 14, 2014: SPAR. CRACKED. FOUND CRACKS IN VERTICAL STAB AFT CENTER SPAR WEB.
- [SDR YADA2011F00212](https://openairdocs.org/sdr/YADA2011F00212), Oct 13, 2011: LINE. RUPTURED. ON A PREFLIGHT WALK AROUND INSPECTION OF THE ACFT, THE FLIGHT CREW NOTICED A PUDDLE OF HYD FLUID ON THE GROUND AROUND THE RT MLG. HYD FLUID WAS ALSO NOTED ON TH
- [SDR YADA042111](https://openairdocs.org/sdr/YADA042111), Apr 21, 2011: RELAY. STUCK. ENROUTE, THE PILOT NOTICED THE LANDING GEAR RELAY CIRCUT BREAKER WAS POPPED. THE FLIGHT CREW ALSO THOUGHT THEY COULD HEAR THE LANDING GEAR PUMP RUNNING BUT WERE
- [SDR YADA041511](https://openairdocs.org/sdr/YADA041511), Apr 15, 2011: LANDING GEAR. MALFUNCTIONED. PILOT REPORTED THAT IN CRUISE, NOTICED THE LANDING GEAR RELAY CIRCUT BREAKER WAS POPPED. SEVERAL ATTEMPTS TO RESET THE CIRCUT BREAKER WERE UNSUCCESSFUL. ON ARRI
- [SDR 2010F00251](https://openairdocs.org/sdr/2010F00251), Dec 11, 2010: DOWNLOCK SWITCH. INTERMITTENT. ON APPROACH TO THE AIRPORT, THE GEAR WAS SELECTED DOWN BUT THERE WAS NO INDICATION THE NOSE GEAR WAS DOWN AND LOCKED. THE GEAR WAS CYCLED SEVERAL TIMES AND CYCL
- [SDR YADA122908](https://openairdocs.org/sdr/YADA122908), Dec 29, 2008: PUMP. DAMAGED. ON AN OPS CHECK FLIGHT, PILOT REPORTED LOW PRESSURE FUEL LIGHT ON THE NR 1 ENG, LIGHT WENT OUT WITH AUX PUMP ON. REPLACED PUMP. TEARDOWN OF REMOVED PUMP REVEALE
- [SDR YADA112808](https://openairdocs.org/sdr/YADA112808), Nov 28, 2008: BOOT. SHORTED. OBSERVED SPARKS FROM RT PROP INFLIGHT, SPARKS STOPPED WHEN PROP DEICE WAS TURNED OFF. A/C LANDED UNEVENTFULLY. MAINT REPLACED PROP DUE TO SHORTED DEICE BOOT.
- [SDR YAD2008F00000](https://openairdocs.org/sdr/YAD2008F00000), Jul 11, 2008: SWITCH. FAILED. PILOT REPORTED NOSE GEAR UNSAFE WARNING AFTER VARIOUS ATTEMPTS AT GEAR EXTENSION. GREEN LIGHT CAME ON AT TOUCHDOWN. VERIFIED NOSE GEAR DRAG BRACE SWITCH PLUNGER
- [SDR ACE020508](https://openairdocs.org/sdr/ACE020508), Feb 5, 2008: TUBE. SPLIT. NOSE TIRE LOOSING AIR AFTER LANDING (BET) REPLACED NOSE TIRE ASSY (FOUND INNER TUBE SPLIT ON SEAM 1/8). THIS IS THE LATEST IN A STRING OF INNER TUBE FAILURES FO
- [SDR ACE120407](https://openairdocs.org/sdr/ACE120407), Dec 4, 2007: TUBE. FAILED. PILOT STOPPED AIRCRAFT ON TAXIWAY DUE VIBRATION FROM NOSE TIRE. MAINTENANCE REPLACED FLAT TIRE. INSPECTION OF TIRE AND TUBE IDENTIFIED A NAIL IN TIRE (UNDETERMI
- [SDR ACE032707](https://openairdocs.org/sdr/ACE032707), Mar 25, 2007: STRINGER. CORRODED. LOCATED CORRODED STRINGER NR 14LH AT FS. 250.
- [SDR ACE02050702](https://openairdocs.org/sdr/ACE02050702), Feb 5, 2007: MOTOR. FAILED. FLAPS STOPPED AT TAKEOFF. RETRACTED TO UP ON THE GROUND. THE SMELL OF HOT ELECTRICAL WAS STRONG. REPLACED FAILED FLAP MOTOR AND GEAR BOX.
- [SDR ACE0830061](https://openairdocs.org/sdr/ACE0830061), Aug 30, 2006: WINDSHIELD. CRACKED. PIREP - ON CLIMBOUT ONE WINDSHIELD SHATTERED AND THEN, FIVE MINUTES LATER, THE OTHER WINDSHIELD SHATTERED. UNEVENTFUL LANDING MADE, CREW VERIFIED ONLY OUTER PLY
- [SDR ACE0830062](https://openairdocs.org/sdr/ACE0830062), Aug 30, 2006: WINDSHIELD. CRACKED. PIREP - ON CLIMBOUT ONE WINDSHIELD SHATTERED AND THEN, FIVE MINUTES LATER, THE OTHER WINDSHIELD SHATTERED. UNEVENTFUL LANDING MADE, CREW VERIFIED ONLY OUTER PLY
- [SDR ACE04302006](https://openairdocs.org/sdr/ACE04302006), Apr 30, 2006: SPAR CAP. CORRODED. MAINTENANCE FOUND CORROSION ON FORWARD SPAR LOWER CAP FORWARD FLANGE, IN THE CENTER FUSELAGE BAY, UNDER ORIGINAL SEALANT. REPAIR REQUIRED REMOVAL OF CORROSION A
- [SDR ACE120105](https://openairdocs.org/sdr/ACE120105), Dec 1, 2005: WINDSHIELD. CRACKED. PILOT REPORTED RT FORWARD WINDSHIELD CRACKED. REPLACED CRACKED WINDSHIELD.
- [SDR ACE082605](https://openairdocs.org/sdr/ACE082605), Aug 26, 2005: DIAPHRAGM. RUPTURED. PILOT REPORTED LOW FUEL PRESSURE WARNING LIGHT CAME ON IN FLIGHT. MAINTENANCE REPLACED LEAKING LOW PSI BOOST PUMP. VERIFIED DIAPHRAGM HAD FAILED. FUEL WAS OBSER
- [SDR ACE070805](https://openairdocs.org/sdr/ACE070805), Jul 8, 2005: FUEL HEATER. CRACKED. MAINTENANCE NOTICED OIL RESIDUE ON ENGINE COWLING. LOCATED ENGINE OIL LEAK AT OIL / FUEL HEATER. REPLACED CRACKED HEATER.
- [SDR ACE052105](https://openairdocs.org/sdr/ACE052105), May 21, 2005: WINDSHIELD. CRACKED. PILOT REPORTED LT WINDSHIELD CRACKED ON DESCENT. REPLACED FAILED WINDSHIELD (OUTER PLY FAILED).
- [SDR ACE08282004](https://openairdocs.org/sdr/ACE08282004), Aug 28, 2004: STRINGER CLIP. MISSING. DURING SCHEDULED STRUCTURAL INSPECTION OF THE AREA, FOUND STRINGER CLIP PN. 114-430066-5 NEVER INSTALLED AND THE BULKHEAD AT FS 363.25 HAD CRACKS IN THE FLANGE 
- [SDR ACE082304](https://openairdocs.org/sdr/ACE082304), Aug 23, 2004: LIMIT SWITCH. OUT OF ADJUST. PILOT REPORTED LANDING GEAR HANDLE WARNING LIGHTS REMAINED ON AFTER GEAR WAS RETRACTED. CREW RETURNED TO AIRPORT FOR AN UNEVENTFUL LANDING. MAINTENANCE ADJUSTED
- [SDR ACE071204](https://openairdocs.org/sdr/ACE071204), Jul 12, 2004: SKIN. CORRODED. MAINTENANCE OBSERVED DEFORMATION OF FUSELAGE SKIN AT LAP JOINTS AT STATIONS 348.25 & 430.75 UNDER STRINGER 16. REPAIRS MADE INCLUDED REMOVAL OF EXFOLIATED SHIMS
- [SDR ACE062804](https://openairdocs.org/sdr/ACE062804), Jun 28, 2004: WINDSHIELD. CRACKED. PILOT REPORTED LEFT WINDSHIELD CRACKED ONE HALF HOUR INTO FLIGHT. RETURNED TO ORIGINAL AIRPORT.
- [SDR ACE112503](https://openairdocs.org/sdr/ACE112503), Nov 25, 2003: WARNING SYSTEM. MALFUNCTIONED. NOSE GEAR FAILED TO SHOW DOWN AND LOCKED UNTIL GEAR WAS CYCLED TWICE. MAINTENANCE COULD NOT DUPLICATE FAULT.
- [SDR 113AX62603](https://openairdocs.org/sdr/113AX62603), Jun 26, 2003: INTERCOSTAL. CRACKED. WHILE C/W STRUCTURAL INSPECTION 53-10-02, FOUND .5 INCH CRACK IN OUTER FLANGE RADIUS OF INTERCOSTAL PN 114-430116-7 AT STATION NR 498.25 AND ADJACENT TO THE CAR
- [SDR ACE0531021](https://openairdocs.org/sdr/ACE0531021), Jun 3, 2002: CONTROL CABLE. BROKEN. PILOT ATTEMPTED TO ADJUST ELEVATOR TRIM TO REDUCE CONTROL FORCES AND NOTICED THAT TRIM SYS DID NOT FEEL LIKE IT WAS WORKING NORMAL. AFTER UNEVENTFUL LANDING , P

## 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/N113AX/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

---
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.