# Rockwell International 112

- Type: Aircraft model (FAA registry)
- Registry code: 7630301
- Manufacturer (registry): ROCKWELL INTERNATIONAL
- Model: 112
- Aircraft type: Fixed wing single engine
- Category: Airplane
- Engines: 1 · Reciprocating
- Seats: 4
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS A12SO](https://openairdocs.org/tcds/A12SO) (OpenAirDocs)
- Holder: Commander Aircraft Corporation
- Registered aircraft: 9
- Page: https://openairdocs.org/model/rockwell-international-112

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022
- [AD 2012-02-10](https://openairdocs.org/ad/2012-02-10): Stabilizers · Commander 112, 112B, 112TC and 5 more. Effective Mar 15, 2012
- [AD 2006-03-08](https://openairdocs.org/ad/2006-03-08): Vacuum pumps · Aero Advantage 14-19, 14-19-2, 14-19-3 and 299 more. Effective Mar 10, 2006
- [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 90-04-07](https://openairdocs.org/ad/90-04-07): Wing Spars · Commander 112, 112B, 112TC and 3 more. Effective Mar 9, 1990
- [AD 88-05-06](https://openairdocs.org/ad/88-05-06): Inspect for Cracks · Commander 112, 112B, 112TC and 3 more. Effective Apr 8, 1988
- [AD 85-03-04 R2](https://openairdocs.org/ad/85-03-04-R2): Front Seat and Belt Attachment · Commander 112, 112TC and 114. Effective Apr 27, 1987
- [AD 79-07-02](https://openairdocs.org/ad/79-07-02): Batteries · Aircraft Parts & Development A, A-2, A-3 and 149 more. Effective Apr 3, 1979
- [AD 77-01-08](https://openairdocs.org/ad/77-01-08): Engine Failure · Commander 112. Effective Jan 14, 1977
- [AD 75-22-09](https://openairdocs.org/ad/75-22-09): Ailerons · Commander 112. Effective Nov 4, 1975
- [AD 73-24-01](https://openairdocs.org/ad/73-24-01): Control Surface Hinge Failure · Commander 112. Effective Nov 19, 1973
- [AD 73-14-04](https://openairdocs.org/ad/73-14-04): Engine and Prop Controls · Commander 112. Effective Jul 3, 1973
- [AD 73-14-06](https://openairdocs.org/ad/73-14-06): Cracks in Prop Spinner Bulkhead · Commander 112. Effective Jun 26, 1973

Historical (superseded or no longer in force):

- [AD 2011-07-13](https://openairdocs.org/ad/2011-07-13) (historical): Stabilizers · CPAC 112, 112B, 112TC and 5 more. Effective Apr 4, 2011

## Information bulletins (advisory) (4)

- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-09-40R1](https://openairdocs.org/saib/CE-09-40R1): Flight Controls - Trailing Edge Flap Control System. Issued Oct 19, 2009
- [SAIB CE-09-40](https://openairdocs.org/saib/CE-09-40) (historical): Flight Controls - Trailing Edge Flap Control System. Issued Jul 22, 2009
- [SAIB CE-04-33](https://openairdocs.org/saib/CE-04-33): . Issued Dec 11, 2003

## Registered aircraft (9)

- [N112EF](https://openairdocs.org/aircraft/N112EF): [Commander 112a LLC](https://openairdocs.org/faa-owner/COMMANDER%20112A%20LLC), [Shelburne, VT](https://openairdocs.org/faa-place/VT/Shelburne), built 1975, S/N 309
- [N114SL](https://openairdocs.org/aircraft/N114SL): [Simply Living LLC](https://openairdocs.org/faa-owner/SIMPLY%20LIVING%20LLC), [Fort Myers, FL](https://openairdocs.org/faa-place/FL/Fort%20Myers), S/N 122
- [N1174J](https://openairdocs.org/aircraft/N1174J): [Olson Michael J](https://openairdocs.org/faa-owner/OLSON%20MICHAEL%20J), [Viroqua, WI](https://openairdocs.org/faa-place/WI/Viroqua), built 1974, S/N 174
- [N1231J](https://openairdocs.org/aircraft/N1231J): [Mattson Paul](https://openairdocs.org/faa-owner/MATTSON%20PAUL), [Chula Vista, CA](https://openairdocs.org/faa-place/CA/Chula%20Vista), S/N 231
- [N128AD](https://openairdocs.org/aircraft/N128AD): [Wahl Flying LLC](https://openairdocs.org/faa-owner/WAHL%20FLYING%20LLC), [Germantown, WI](https://openairdocs.org/faa-place/WI/Germantown), built 1974, S/N 219
- [N1429J](https://openairdocs.org/aircraft/N1429J): [Wooley Michael W](https://openairdocs.org/faa-owner/WOOLEY%20MICHAEL%20W), [Navarre, FL](https://openairdocs.org/faa-place/FL/Navarre), built 1976, S/N 429
- [N1476J](https://openairdocs.org/aircraft/N1476J): [Dodgen Charles W](https://openairdocs.org/faa-owner/DODGEN%20CHARLES%20W), [Thomaston, GA](https://openairdocs.org/faa-place/GA/Thomaston), built 1976, S/N 476
- [N202RR](https://openairdocs.org/aircraft/N202RR): [Norton Edward A](https://openairdocs.org/faa-owner/NORTON%20EDWARD%20A), [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas), S/N 350
- [N324X](https://openairdocs.org/aircraft/N324X): [Fontenot Ira Dean](https://openairdocs.org/faa-owner/FONTENOT%20IRA%20DEAN), [Collierville, TN](https://openairdocs.org/faa-place/TN/Collierville), built 1975, S/N 300

## NTSB investigations (4)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ERA25LA292](https://openairdocs.org/ntsb/ERA25LA292), Jul 23, 2025: Rockwell International 112 (N112EF), Burlington, VT, substantial damage, investigation ongoing
- [NTSB ERA23LA202](https://openairdocs.org/ntsb/ERA23LA202), Apr 18, 2023: Rockwell International 112 (N12RX), Miami, FL, substantial damage. Probable cause: Failure of the right main landing gear due to inadequate hydraulic pressure as result of a torn O-ring that was installed on the hydraulic pack’s check valve during overhaul.
- [NTSB MIA05LA012](https://openairdocs.org/ntsb/MIA05LA012), Oct 24, 2004: Rockwell 112A (N112ND), Tampa, FL, substantial damage. Probable cause: The pilot's failure to properly set flaps for takeoff which resulted in the aborted takeoff and subsequent impact with water during an overrun of the runway and seawall.
- [NTSB DEN74FTE91](https://openairdocs.org/ntsb/DEN74FTE91), Jun 27, 1974: Aero Comdr 112A (N1174J), Loveland, CO, substantial damage

## FAA accident and incident reports (10)

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.

- [Accident 20250723010099A](https://openairdocs.org/incident/20250723010099A), Jul 23, 2025: Rockwell International 112 (N112EF), Burlington, VT, Substantial damage. On 7/23, during a return flight to kbtv, the engine lost all power and quit while on right downwind for runway 19. The pilot immediately informed the tower and…
- [Accident 20230418008499A](https://openairdocs.org/incident/20230418008499A), Apr 18, 2023: Rockwell International 112 (N12RX), Miami, FL, Substantial damage. During landing touchdown on runway 9L at tmb, aircraft right main gear collapsed and the propeller hit the ground aircraft veered to the right into the grass…
- [Incident 20130816019229I](https://openairdocs.org/incident/20130816019229I), Aug 16, 2013: Rockwell International 112 (N1231J), Jackson, TN, Minor damage. On August 16, 2013, at approxmently 1752 l, [privacy data omitted] was piloting N1231J, a Rockwell commander 112. During the landing at mkl the aircraft…
- [Accident 20041025027869A](https://openairdocs.org/incident/20041025027869A), Oct 25, 2004: Gulstm 112 (N112ND), Tampa, FL, Substantial damage. (-23) On Sunday October 25, 2004, at 0840 EDT, a rockwell commander 112, N112ND registered to pilot-in-command, collided with the water after running off…
- [Incident 20000215001409I](https://openairdocs.org/incident/20000215001409I), Feb 15, 2000: Gulstm 112 (N1429J), San Antonio, TX, Minor damage. (-23) On February 15, 2000, at 1400 hours, a rockwell MD. 112, N1429J owned by Texas skyways inc. and operated by Mr. Jack johnson,[privacy data omitted]landed…
- [Incident 19880302011349I](https://openairdocs.org/incident/19880302011349I), Mar 2, 1988: Gulstm 112 (N1174J), Imperial, CA. Departed airport and found passenger door open. Returned. Forgot to lower gear. Landed gear up.
- [Incident 19851026075349I](https://openairdocs.org/incident/19851026075349I), Oct 26, 1985: Gulstm 112 (N1231J), Lyndhurst, OH. Low level operation unauthorized over populated area.
- [Incident 19830331018429I](https://openairdocs.org/incident/19830331018429I), Mar 31, 1983: Gulstm 112 (N1231J), Ashtabula, OH, Minor damage. Landed gear up.
- [Incident 19801220089489I](https://openairdocs.org/incident/19801220089489I), Dec 20, 1980: Rkwell 112 (N1231J), Kinsman, OH. Engine failed due to loss of oil through front shaft seal. Pertinent service bulletin not complied with.
- [Accident 19740627020809A](https://openairdocs.org/incident/19740627020809A), Jun 27, 1974: Rkwell 112 (N1174J), Loveland, CO, Substantial damage. Ldg gr down electrical circuitry. Mfr issued service bulletin.

## Service difficulty reports (16)

As reported by operators and repair stations, by the model named in the report.

- [SDR 2024FA0000214](https://openairdocs.org/sdr/2024FA0000214), Mar 11, 2024: STOP. CRACKED. CRACKS FOUND, MULTIPLE PLACES, IN LH AILERON BELLCRANK SUPPORT STRUCTURE. LARGEST CRACK IS 2.5"L. THE SUBJECT PART PROVIDES STRUCTURAL SUPPORT TO THE OUTBOARD E
- [SDR 2015FA0000130](https://openairdocs.org/sdr/2015FA0000130), Apr 8, 2015: SPAR. CORRODED. FOUND BACKSIDE OF LT WING SPAR CORRODED TO 20 PERCENT LOSS OF MATERIAL NEAR FS 70. CORROSION ALSO FOUND ON RT WING IN SAME LOCATION. CORROSION WAS BETWEEN LOWER
- [SDR CA120905006](https://openairdocs.org/sdr/CA120905006), Sep 3, 2012: HORN. CORRODED. (CAN) HOLES CORRODED IN BOTTOM OF ELEVATOR HORN WHICH COULD CAUSE FAILURE OF THE HORN AND CAUSE LOSS OF ELEVATOR CONTROL OF THE AIRCRAFT.
- [SDR 2010FA0000598](https://openairdocs.org/sdr/2010FA0000598), May 15, 2010: CAMSHAFT. BROKEN. PILOT STATED THE ENGINE BECAME ROUGH AFTER TAKEOFF. RETURNED TO AIRPORT & LANDED. FOUND NR 1 CYLINDER TO BE COLDER THAN REST. PULLED ROCKER COVER & NOTED THE VA
- [SDR CA080226004](https://openairdocs.org/sdr/CA080226004), Feb 22, 2008: ALTERNATOR. UNSERVICEABLE. (CAN) ALTERNATOR FAILED, CAUSING MAIN BATTERY TO DRAIN RESULTING IN COMMUNICATION DIFFICULTIES WHICH CAUSED PILOT TO CONTACT TOWER BY CELL PHONE FOR CLEARANCE T
- [SDR 2004FA0000130](https://openairdocs.org/sdr/2004FA0000130), Jan 22, 2004: SPAR. CRACKED. CRACKS FOUND ADJACENT TO UPPER HINGE BRACKET ATTACH HOLES ON RUDDER SPAR. FOUR CRACKS FOUND, EACH BETWEEN .7500 INCH AND 1 INCH LONG. ONE WAS VISIBLE, OTHERS FO
- [SDR 2002FA0001285](https://openairdocs.org/sdr/2002FA0001285), Nov 1, 2002: TORQUE TUBE. CRACKED. DURING INSPECTION OF THIS LANDING GEAR TORQUE TUBE THE PART WAS CLEANED OFF WITH A RAG AND VISUALLY INSPECTED AS USUAL. PAINT WAS SMOOTH AND UNBROKEN AROUND ENT
- [SDR CA010314027](https://openairdocs.org/sdr/CA010314027), Feb 23, 2001: STRUT. CONTAMINATED. (CAN) A/C HAD UNCOMMANDED NOSE GEAR RETRACTION UPON LDG. IT NOTICED DURING POWER PACK PRESSURE TEST THAT 700PSI ON UP SIDE WHEN GEAR EXTENDING & THAT PRESSURE W
- [SDR 20001120SH022](https://openairdocs.org/sdr/20001120SH022), Nov 6, 2000: POWERPACK. MALFUNCTIONED. LANDING GEAR HYDRAULIC POWER PACK BUILDS UP 16 PSI. (AFTER GEAR EXTENSION) IN THE ''UP'' SIDE OF HYDRAULIC CIRCUIT CONTRARY TO COMMANDER 112 SM. POWER PACK VEND
- [SDR 20000501SH009](https://openairdocs.org/sdr/20000501SH009), Mar 13, 2000: HOSE. DETERIORATED. STRATOFLEX HOSE NR 111-4, CURE DATE 3Q92, FULLY DETERIORATED WHILE INSTALLED ON BELGIAN REGISTERED AIRCRAFT. NO OTHER CASES FOUND WITH INSTALLED HOSES. THIS PAR
- [SDR 20000417SH005](https://openairdocs.org/sdr/20000417SH005), Feb 4, 2000: SWITCH. FAILED. PILOT REPORTED NLG DOWN LIGHT INTERMITTENT. INVEST SHOWED HYD ACTUATED NLG DOWN SWITCH ROLLER PN 1JE5 HANGING UP AT BOTTOM OF HOLE AT DNLK ASSY. RE-RIGGED SWITC
- [SDR AU981247](https://openairdocs.org/sdr/AU981247), Sep 24, 1998: RIB. CRACKED. (AUS) RUDDER TOP RIB CRACKED IN TWO PLACES EITHER SIDE OF THE BALANCE WEIGHT ATTACHMENT BOLT. PART TC: 2,294.
- [SDR AU981246](https://openairdocs.org/sdr/AU981246), Sep 24, 1998: RIB. CRACKED. (AUS) VERTICAL STABILIZER RIB CRACKED IN FOUR PLACES. ONE OF THE CRACKS WAS IN A PREVIOUS REPAIR. PART TC: 2,294.
- [SDR 97ZZZX4191](https://openairdocs.org/sdr/97ZZZX4191), Aug 15, 1997: SWITCH. MISADJUSTED. FOUND NOSE GEAR MICROSWITCH INSTALLED TO FULL FORWARD LIMIT ON MOUNTING BRACKET. BRACKET MOUNTED ON ENGINE MOUNT WITH HOSE CLAMPS. FOUND BRACKET INSTALLED TOO F
- [SDR CA970128005](https://openairdocs.org/sdr/CA970128005), Jan 22, 1997: SHAFT. WORN KEYWAY. (CAN) DURING COMPLIANCE WITH AD 96-09-10 IT WAS DISCOVERED THE DRIVE GEAR AND DRIVE SHAFT CONTAINED A KEYWAY. THE KEYWAY AND DRIVE GEAR WERE WORN APPROXIMATELY 
- [SDR CA951130015](https://openairdocs.org/sdr/CA951130015), Nov 16, 1995: SOCKET. LOOSE. (CAN)WHILE CARRYING OUT FLIGHT TEST AFTER AN INSPECTION THE RIGHT HAND GEAR LIGHT FAILED TO ILLUMINATE. PILOT TAPPED THE SOCKET AND THE LIGHT CAME ON. ALL THREE

## STCs that may be installed (OpenAirDocs) (201, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc
- [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 SA12428CH](https://openairdocs.org/stc/SA12428CH): Installation of the Lycoming Engines Electronic Ignition System (EIS). Lycoming Engines, An Operating Division of AVCO Corporation
- [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 SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc
- [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC
- [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International Inc
- [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 SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power supplies. Whelen Aerospace Technologies
- [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc
- [STC SA5757SW](https://openairdocs.org/stc/SA5757SW): Installation of Alcor tru-flow/ fuel flow/totalizer system. Alcor LLC
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics
- [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 SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC
- [STC SA04568CH](https://openairdocs.org/stc/SA04568CH): Installation of the uAvionix tailBeaconX, a tail mounted position light with integrated Automatic Dependent Surveillance - Broadcast (ADS-B) Out and 1090MHz Mode-S transponder functionality. uAvionix Corporation
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA02532AT](https://openairdocs.org/stc/SA02532AT): Installation of subject Michelin tires on appropriate aircraft. For Michelin 5, 6, 8, and 10-inch rim diameter tires on General Aviation Aircraft. Michelin North America Inc
- [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine
- [STC SA04400NY](https://openairdocs.org/stc/SA04400NY): Installation of the Integrated Back-up Battery System (IBBS). TCW Technologies LLC
- [STC SA02771LA](https://openairdocs.org/stc/SA02771LA): Installation of openable window. Ellis and Associates CADD/Technical Illustration
- [STC SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine
- [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC
- [STC SA2677CE](https://openairdocs.org/stc/SA2677CE): Installation of aileron and flap gap seals per Horton-STOL Craft Drawing List #15 with an approval date of August 18, 1994 or later FAA approved revision. Curry Aviation LLC
- [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems 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 SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc
- [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC
- [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA03658NY](https://openairdocs.org/stc/SA03658NY): Installation of MT-Propeller Entwicklung GmbH's Model# MTV-12-B/188-59f 3-Blade constant speed propeller. MT- Propeller Entwicklung GmbH
- [STC SA02426AK](https://openairdocs.org/stc/SA02426AK): Approval of the FreeFlight FDL-978-TX ADS-B system installed. FreeFlight Systems
- [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation
- [STC SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA1229CE](https://openairdocs.org/stc/SA1229CE): Installation of King KFC-200, 2 axis(3 optional) flight control system with KCS 55/55A compass and a KI-255 (or -256) flight command indicator or a KG-258 attitude horizon gyro with a KC-292 mode controller; or stand alone electric trim. Honeywell International Inc
- [STC SA01560WI-D](https://openairdocs.org/stc/SA01560WI-D): Installation of the Honeywell KFD 840 Primary Flight Display System. Honeywell International Inc
- [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 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 SA615EA](https://openairdocs.org/stc/SA615EA): Installation of a Whelen Anti-Collision Strobe Light System as replacement for originally installed anti-collision lights. Whelen Aerospace Technologies
- [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine
- [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc

All 201: https://openairdocs.org/model/rockwell-international-112/stcs.md

## PMA parts (OpenAirDocs) (468, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [73-CFG-R](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188247901220260806152402.0001): Fuel Quantity Indication Placard. Swift Fuels, LLC · PMA PQ04423CE · Modification part · Jul 20, 2026
- [S1069](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155451647420260806152307.0001): 100R Fuel Placard. Swift Fuels, LLC · PMA PQ04423CE · Modification part · Jul 20, 2026
- [066-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124095606820260723131532.0001): Rivet. Game Aerospace, LLC · PMA PQ00052CB · Replaces Cleveland Wheels and Brakes P/N… · Jun 9, 2026
- [RAP164-01501](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140485046920260722154715.0001): Brake Disc. Rapco Inc. · PMA PQ2101CE · Replaces 164-01501 · Jun 3, 2026
- [RAP164-04300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130664647420260722154723.0001): Brake Disc. Rapco Inc. · PMA PQ2101CE · Replaces 164-04300 · Jun 3, 2026
- [MDL TD 031851](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110128735420250508133541.0001): VA-1A( )AndAccessories. Electronics International Inc · PMA PQ0088NM · Modification part · Apr 10, 2025
- [LSM-200-700-11](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151673365120250417183922.0001): Hub Cap Assy. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · Dec 10, 2024
- [8850-5CJ](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107186477620240625133919.0001): MOTOR (14 VDC). McFarlane Aviation Inc. · PMA PQ3732CE · Replaces 8850-5 · Mar 14, 2024
- [MDL103216-000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156844967620240221143421.0001): SkyView HDX Instrumentation. Dynon Avionics, Inc. · PMA PQ05359NM · Modification part · Jan 26, 2024
- [UAV-1004236-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141723824820230707211312.0001): AV-30-C. uAvionix Corporation · PMA PQ05445NM · Modification part · Jun 28, 2023
- [APS105-00200](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169929699120221020170416.0001): Rivet. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 105-00200 · Aug 10, 2022
- [APS66-10500](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119380288120221020170253.0001): Brake Lining. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 066-10500 · Aug 10, 2022
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148044443620220706160135.0001): Whelen Aerospace Technologies · PMA PQ1372CE · Jun 21, 2022
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID158545710620220328175210.0001): C J Aviation, Inc. · PMA PQ1607CE · Mar 3, 2022
- [700-00190-100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID670983375520210921142540.0001): SkyTrax 100B/200 ADS-B Receiver. Avidyne Corporation · PMA PQ4035CE · Replaces ModificationPart · Jul 28, 2021
- [A099001-027](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID263203176620210617194232.0001): Muffler, Heater, Exhaust Assembly. Aerospace Welding Minneapolis, Inc. · PMA PQ2712CE · Replaces EL099001-27 · Jun 3, 2021
- [409-00003-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID265718993320210702175219.0001): Internal Battery Pack, Refresh. Aspen Avionics · PMA PQ03868SW · Modification part · Jan 20, 2021
- [ALE-2008AE-AC](https://drs.faa.gov/browse/excelExternalWindow/E2B30B020A91DE91862585DE00509F79.0001): Stator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-2008AE, as used in alternators ALT… · Sep 1, 2020
- [ALE-2008AA-AC](https://drs.faa.gov/browse/excelExternalWindow/C617AAB83C6B799B862585DE0050A01D.0001): Stator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-2008AA, as used in alternators ALY… · Sep 1, 2020
- [XA-943FS-AC](https://drs.faa.gov/browse/excelExternalWindow/B7CC6ECA46AA2F14862585DE00509E71.0001): Pos. Diode. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces XA-943FS, as used in alternators ALE… · Sep 1, 2020
- [ALE-1013AS-AC](https://drs.faa.gov/browse/excelExternalWindow/9F424D3467678943862585DE00509EFC.0001): Alternator Brush. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-1013AS, as used in alternators ALE… · Sep 1, 2020
- [ALU-3045BS-AC](https://drs.faa.gov/browse/excelExternalWindow/68353ACEF594EACF862585DE0050A127.0001): Brush Assembly. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALU-3045BS, as used in alternators ALE… · Sep 1, 2020
- [ALE-2008ABS-AC](https://drs.faa.gov/browse/excelExternalWindow/6583E821C11FC24F862585DE0050A086.0001): Stator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-2008ABS, as used in alternators… · Sep 1, 2020
- [XA-944JS-AC](https://drs.faa.gov/browse/excelExternalWindow/0388185039CFC4DD862585DE00509DDD.0001): Neg. Diode. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces XA-944JS, as used in alternators ALE… · Sep 1, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID863596391320220125131355.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID700885025920220125131338.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID516792063820220125131439.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID442409033320220125131415.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID273744405220220125131320.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID246784811720220125131502.0001): DAC International · PMA PQ0986SW · Jul 31, 2020
- [ALE-2008ABS-AC](https://drs.faa.gov/browse/excelExternalWindow/D6FF39FD09272684862585A80035E2C3.0001): Stator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-2008ABS as used in Kelly… · Jul 14, 2020
- [ALU-3045BS-AC](https://drs.faa.gov/browse/excelExternalWindow/BDCE1BF615C7C07F862585A80035E30E.0001): Brush Assembly. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALU-3045BS as used in Kelly Aerospace… · Jul 14, 2020
- [XA-944JS-AC](https://drs.faa.gov/browse/excelExternalWindow/7D10ABF30982F851862585A80035E125.0001): Neg. Diode. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces XA-944JS as used in Kelly Aerospace… · Jul 14, 2020
- [ALE-2008AE-AC](https://drs.faa.gov/browse/excelExternalWindow/653EDB41D36E637B862585A80035E22A.0001): Stator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-2008AE as used in Kelly Aerospace… · Jul 14, 2020
- [ALE-1013AS-AC](https://drs.faa.gov/browse/excelExternalWindow/5023594FC72E2A5F862585A80035E1DF.0001): Alternator Brush. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-1013AS as used in Kelly Aerospace… · Jul 14, 2020
- [ALE-2008AA-AC](https://drs.faa.gov/browse/excelExternalWindow/4077186575E9032A862585A80035E272.0001): Stator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALE-2008AA as used in Kelly Aerospace… · Jul 14, 2020
- [XA-943FS-AC](https://drs.faa.gov/browse/excelExternalWindow/2B2BE444A62E7876862585A80035E196.0001): Pos. Diode. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces XA-943FS as used in Kelly Aerospace… · Jul 14, 2020
- [SA20000](https://drs.faa.gov/browse/excelExternalWindow/DF98041CAF259EB18625827400763945.0001): Commander Model 112/114 Elevator Spar Modification. Sterling Aviation Technologies Inc · PMA PQ2158NM · Modification part · Mar 11, 2018
- [A8120-C](https://drs.faa.gov/browse/excelExternalWindow/BF839A1616A80335862581C60057423D.0001): Pump-Motor Assembly. Weldon Pump · PMA PQ2411CE · Replaces Weldon Pump A8120-C, Commander… · Oct 11, 2017
- [44285-RE7](https://drs.faa.gov/browse/excelExternalWindow/8D0A9E407E3DD2B68625816B00628639.0001): Elevator Hinge Fitting Shim. Aerodyme Corporation · PMA PQ2095NE · Replaces 44285-RE7 · Jul 23, 2017
- [44285-RE8](https://drs.faa.gov/browse/excelExternalWindow/65006C57498DDDA18625816B0062868E.0001): Elevator Hinge Fitting Radius Block. Aerodyme Corporation · PMA PQ2095NE · Replaces 44285-RE8 · Jul 23, 2017
- [44285-RE2](https://drs.faa.gov/browse/excelExternalWindow/5FD2A4DA2A766A4B8625816B00628541.0001): Elevator Hinge Fitting. Aerodyme Corporation · PMA PQ2095NE · Replaces 44285-1 · Jul 23, 2017
- [44285-RE2-SP](https://drs.faa.gov/browse/excelExternalWindow/5C42F95D3BFA76148625816B006285E5.0001): Elevator Hinge Fitting. Aerodyme Corporation · PMA PQ2095NE · Replaces 44285-1 · Jul 23, 2017
- [44285-RE9](https://drs.faa.gov/browse/excelExternalWindow/126CA108052212F08625816B006286E3.0001): Elevator Hinge Fitting Plate. Aerodyme Corporation · PMA PQ2095NE · Replaces 44285-RE9 · Jul 23, 2017
- [2307055-1](https://drs.faa.gov/browse/excelExternalWindow/AD2D635BC297B66886258175006DB55B.0001): Aviation Landing Light. Teledyne Reynolds · PMA PQ4015NM · Replaces 4509 · Jul 20, 2017
- [RA063-01200](https://drs.faa.gov/browse/excelExternalWindow/11AB135F1EE8766686257EE40073FC0A.0001): Pressure Plate. Rapco Inc · PMA PQ2101CE · Replaces Cleveland 063-01200 · Oct 13, 2015
- [GF44300-3](https://drs.faa.gov/browse/excelExternalWindow/E4B43237C79E922286257EDD004BEF70.0001): Fin Tip. Knots 2U Ltd · PMA PQ2106CE · Replaces 44300-3 · Oct 8, 2015
- [GF44233-11](https://drs.faa.gov/browse/excelExternalWindow/156B6C6DC975690286257EDD004C40C2.0001): Tip, Rudder. Knots 2U Ltd · PMA PQ2106CE · Replaces 44233-11 · Oct 8, 2015
- [W-2691-II-RH](https://drs.faa.gov/browse/excelExternalWindow/C521B9BF7D18560B86257ECE00502F17.0001): Commander Early 112 Wing Tip Lens Covers (RIGHT). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 42242-4 · Sep 24, 2015
- [W-2691-II-LH](https://drs.faa.gov/browse/excelExternalWindow/2CADF07B85B35CBA86257ECE00502EF8.0001): Commander Early 112 Wing Tip Lens Covers (LEFT). Great Lakes Aero Products Inc · PMA PQ2056CE · Replaces 42242-3 · Sep 24, 2015

All of them: https://openairdocs.org/model/rockwell-international-112/pma.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Aero Commander 112](https://openairdocs.org/model/aero-commander-112): 98 registered aircraft, registry code 0144701

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