# Rockwell International 500-S

- Type: Aircraft model (FAA registry)
- Registry code: 7630410
- Manufacturer (registry): ROCKWELL INTERNATIONAL
- Model: 500-S
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Reciprocating
- Seats: 7
- Weight class: Up to 12,499 lb
- Cruise speed: 163 mph
- Certification: Type certificated
- Data sheet: [TCDS 6A1](https://openairdocs.org/tcds/6A1) (OpenAirDocs)
- Holder: Twin Commander Aircraft LLC
- Registered aircraft: 19
- Page: https://openairdocs.org/model/rockwell-international-500-s

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 2023-09-09](https://openairdocs.org/ad/2023-09-09): Exhaust Turbine System (Recip) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 292 more. Effective Jul 17, 2023
- [AD 2005-18-20](https://openairdocs.org/ad/2005-18-20): "FASTprop" propeller de-icers · Hartzell PHC-C3YF-1RF/F8468A(B,K)-8R constant speed propeller (STC SA00718LA or 17 others). Effective Oct 14, 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 98-08-25 R1](https://openairdocs.org/ad/98-08-25-R1): Nose Landing Gear (NLG) Drag Link Bolt · Twin Commander 500-S, 500-U, 680-F and 9 more. Effective Jan 5, 1999
- [AD 98-20-34](https://openairdocs.org/ad/98-20-34): Airplane Flight Manuals--Severe Icing Conditions · Twin Commander 500, 500-A, 500-B and 24 more. Effective Nov 3, 1998
- [AD 98-14-03](https://openairdocs.org/ad/98-14-03): Transponders · Cessna 172, 172A, 172B and 230 more. Effective Aug 16, 1998
- [AD 98-07-17](https://openairdocs.org/ad/98-07-17): Flap System · Twin Commander 500, 500-A, 500-B and 27 more. Effective May 29, 1998
- [AD 98-08-19](https://openairdocs.org/ad/98-08-19): Wing to Fuselage Attachment Brackets and Straps · Twin Commander 500, 500-A, 500-B and 27 more. Effective May 18, 1998
- [AD 94-04-14](https://openairdocs.org/ad/94-04-14): Spar Cap · Twin Commander 500-S, 500-U, 680-FL(P) and 6 more. Effective Apr 12, 1994
- [AD 94-04-13](https://openairdocs.org/ad/94-04-13): Spar Cap · Twin Commander 500, 500-A, 500-B and 17 more. Effective Apr 12, 1994
- [AD 94-04-11](https://openairdocs.org/ad/94-04-11): Spar Cap · Twin Commander 500-S and 690B. Effective Apr 11, 1994
- [AD 87-21-07 R1](https://openairdocs.org/ad/87-21-07-R1): Fuel Filler Openings · Twin Commander 500, 500-A, 500-B and 16 more. Effective May 5, 1989
- [AD 75-12-09 R2](https://openairdocs.org/ad/75-12-09-R2): Inadvertent Structural Failure · Twin Commander 500, 500-A, 500-B and 12 more. Effective Nov 28, 1981
- [AD 81-19-04](https://openairdocs.org/ad/81-19-04): Hose Assembly · Rajay Hose Assemblies, 500A, 500B and 87 more. Effective Sep 17, 1981
- [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 78-05-06](https://openairdocs.org/ad/78-05-06): Flexible Fuel Cells · Cessna 180, 182, 185 and 98 more. Effective Jun 30, 1978
- [AD 75-12-10](https://openairdocs.org/ad/75-12-10): Autopilots · M7 Aerospace 60, 95-C55, 95-C55A and 17 more. Effective Jun 11, 1975

Historical (superseded or no longer in force):

- [AD 98-08-25](https://openairdocs.org/ad/98-08-25) (historical): Nose Landing Gear (NLG) Drag Link Bolt · Twin Commander 500-S, 500-U, 680-F and 9 more. Effective May 18, 1998
- [AD 96-12-08](https://openairdocs.org/ad/96-12-08) (historical): Nose Landing Gear (NLG) Drag Link Bolt · Twin Commander 500-S, 500-U, 680-F and 8 more. Effective Jun 27, 1996
- [AD 94-04-17](https://openairdocs.org/ad/94-04-17) (historical): Flap System Cable · Twin Commander 500, 500-A, 500-B and 27 more. Effective Apr 15, 1994

## Information bulletins (advisory) (1)

- [SAIB 2023-14](https://openairdocs.org/saib/2023-14): Landing Gear Retract/Extend System. Issued Nov 14, 2023

## Registered aircraft (19)

- [N106FW](https://openairdocs.org/aircraft/N106FW): [Florida Fish & Wildlife Conservation Commission](https://openairdocs.org/faa-owner/FLORIDA%20FISH%20%26%20WILDLIFE%20CONSERVATION%20COMMISSION), [Lakeland, FL](https://openairdocs.org/faa-place/FL/Lakeland), built 1978, S/N 3305
- [N123HT](https://openairdocs.org/aircraft/N123HT): [Reyes Carlos E](https://openairdocs.org/faa-owner/REYES%20CARLOS%20E), [San Juan, PR](https://openairdocs.org/faa-place/PR/San%20Juan), S/N 3300
- [N233WM](https://openairdocs.org/aircraft/N233WM): [Bosco 74 LLC](https://openairdocs.org/faa-owner/BOSCO%2074%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 3313
- [N2415S](https://openairdocs.org/aircraft/N2415S): [Dodson International Parts Inc](https://openairdocs.org/faa-owner/DODSON%20INTERNATIONAL%20PARTS%20INC), [Rantoul, KS](https://openairdocs.org/faa-place/KS/Rantoul), S/N 1860-39
- [N280MB](https://openairdocs.org/aircraft/N280MB): [Weber Donald E](https://openairdocs.org/faa-owner/WEBER%20DONALD%20E), [St David, AZ](https://openairdocs.org/faa-place/AZ/St%20David), built 1975, S/N 3255
- [N292S](https://openairdocs.org/aircraft/N292S): [Martin James David](https://openairdocs.org/faa-owner/MARTIN%20JAMES%20DAVID), [Graford, TX](https://openairdocs.org/faa-place/TX/Graford), built 1976, S/N 3274
- [N2BZ](https://openairdocs.org/aircraft/N2BZ): [Bosco74 LLC](https://openairdocs.org/faa-owner/BOSCO74%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1975, S/N 3227
- [N32GL](https://openairdocs.org/aircraft/N32GL): [G E Air Inc](https://openairdocs.org/faa-owner/G%20E%20AIR%20INC), [Broussard, LA](https://openairdocs.org/faa-place/LA/Broussard), built 1978, S/N 3312
- [N42MS](https://openairdocs.org/aircraft/N42MS): [Plukair Texas LLC](https://openairdocs.org/faa-owner/PLUKAIR%20TEXAS%20LLC), [Houston, TX](https://openairdocs.org/faa-place/TX/Houston), built 1976, S/N 3259
- [N42NZ](https://openairdocs.org/aircraft/N42NZ): [Co Fire Aviation Leasing Inc](https://openairdocs.org/faa-owner/CO%20FIRE%20AVIATION%20LEASING%20INC), [Fort Morgan, CO](https://openairdocs.org/faa-place/CO/Fort%20Morgan), built 1979, S/N 3322
- [N507JP](https://openairdocs.org/aircraft/N507JP): [Shrike Comm LLC](https://openairdocs.org/faa-owner/SHRIKE%20COMM%20LLC), [Matthews, NC](https://openairdocs.org/faa-place/NC/Matthews), built 1976, S/N 3262
- [N534SA](https://openairdocs.org/aircraft/N534SA): [Spur Aviation Services Lc](https://openairdocs.org/faa-owner/SPUR%20AVIATION%20SERVICES%20LC), [Twin Falls, ID](https://openairdocs.org/faa-place/ID/Twin%20Falls), built 1968, S/N 1816-22
- [N57262](https://openairdocs.org/aircraft/N57262): [Steelesky Ltd](https://openairdocs.org/faa-owner/STEELESKY%20LTD), [Maineville, OH](https://openairdocs.org/faa-place/OH/Maineville), built 1975, S/N 3239
- [N578WY](https://openairdocs.org/aircraft/N578WY): [Bridger Aviation Services LLC](https://openairdocs.org/faa-owner/BRIDGER%20AVIATION%20SERVICES%20LLC), [Belgrade, MT](https://openairdocs.org/faa-place/MT/Belgrade), built 1975, S/N 3261
- [N8536](https://openairdocs.org/aircraft/N8536): [Bosco74 LLC](https://openairdocs.org/faa-owner/BOSCO74%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1975, S/N 3267
- [N929JM](https://openairdocs.org/aircraft/N929JM): [Calhoun Paul M](https://openairdocs.org/faa-owner/CALHOUN%20PAUL%20M), [Larue, TX](https://openairdocs.org/faa-place/TX/Larue), S/N 3319
- [N961SC](https://openairdocs.org/aircraft/N961SC): [Vadnais Kenneth G](https://openairdocs.org/faa-owner/VADNAIS%20KENNETH%20G), [Santa Barbara, CA](https://openairdocs.org/faa-place/CA/Santa%20Barbara), built 1975, S/N 3235
- [N999DA](https://openairdocs.org/aircraft/N999DA): [Towner Andrew J Trustee](https://openairdocs.org/faa-owner/TOWNER%20ANDREW%20J%20TRUSTEE), [Leawood, KS](https://openairdocs.org/faa-place/KS/Leawood), S/N 3290
- [N9QY](https://openairdocs.org/aircraft/N9QY): [Amelia Air LLC](https://openairdocs.org/faa-owner/AMELIA%20AIR%20LLC), [Naples, FL](https://openairdocs.org/faa-place/FL/Naples), built 1979, S/N 3321

## NTSB investigations (11)

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 WPR14TA278](https://openairdocs.org/ntsb/WPR14TA278), Jul 3, 2014: Rockwell International 500 S (N101AA), Willcox, AZ, substantial damage. Probable cause: The pilot’s failure to compensate for tailwind conditions and maintain directional control during landing, which resulted in a runway excursion.
- [NTSB CEN11TA279](https://openairdocs.org/ntsb/CEN11TA279), Apr 8, 2011: Rockwell International 500-S (N51RF), Eden Prairie, MN, substantial damage. Probable cause: The pilot's inadequate compensation for the crosswind while landing, which resulted in a loss of directional control.
- [NTSB CEN09CA156](https://openairdocs.org/ntsb/CEN09CA156), Dec 5, 2008: Rockwell International 500-S (N51RF), Grand Forks, ND, substantial damage. Probable cause: The pilot's failure to extend the landing gear prior to touchdown.
- [NTSB ANC03LA032](https://openairdocs.org/ntsb/ANC03LA032), Mar 19, 2003: Rockwell 500-S (N903AK), Chickaloon, AK, substantial damage. Probable cause: The improper installation of an engine fuel line fitting by contracted maintenance personnel resulting in an in-flight engine fire. Contributing factors in the accident were an inadequate annual…
- [NTSB ATL02IA079](https://openairdocs.org/ntsb/ATL02IA079), Apr 8, 2002: Rockwell International 500-S (N8536), Jackson, AL, incident, no damage. Probable cause: The pilot's inadequate preflight planning and preparation, which resulted in fuel exhaustion, loss of engine power in both engines, and subsequent forced landing in a field.
- [NTSB NYC02FA060](https://openairdocs.org/ntsb/NYC02FA060), Feb 17, 2002: Rockwell 500S (N999N), Exeter, RI, substantial damage, 1 fatal. Probable cause: The pilot's failure to maintain control after encountering icing conditions while on approach for landing. Factors in this accident were the night light conditions and pilot's failure to select the…
- [NTSB CHI99LA059](https://openairdocs.org/ntsb/CHI99LA059), Jan 6, 1999: Rockwell 500-S (N50BA), Plymouth, IN, substantial damage. Probable cause: the pilot's failure to maintain directional control of the airplane while landing. Factors associated with the accident were the tailwind condition and the pilot landing in the wrong direction.
- [NTSB LAX91LA313](https://openairdocs.org/ntsb/LAX91LA313), Jul 15, 1991: Rockwell 500S (N260AC), Kahului, HI, substantial damage. Probable cause: THE PILOT'S INADEQUATE PREFLIGHT INSPECTION OF THE AIRCRAFT AFTER REFUELING. THE FAILURE OF THE AIRCRAFT MANUFACTURER TO PUBLISH THE REFUELING INSTRUCTIONS IN THE OPERATOR'S MANUAL, THE INADEQUATE…
- [NTSB MIA88LA165](https://openairdocs.org/ntsb/MIA88LA165), May 8, 1988: Rockwell 500-S (N57222), Jacksonville, FL, substantial damage
- [NTSB MKC83FA059](https://openairdocs.org/ntsb/MKC83FA059), Jan 30, 1983: Rockwell 500-S (N57222), Kansas City, KS, substantial damage
- [NTSB NYC78FGM41](https://openairdocs.org/ntsb/NYC78FGM41), Jul 7, 1978: Aero Comdr 500S (N280MB), Beaver Falls, PA, substantial damage

## FAA accident and incident reports (18)

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 20140702013019A](https://openairdocs.org/incident/20140702013019A), Jul 2, 2014: Rockwell International 500-S (N101AA), Wilcox, AZ, Substantial damage. Pilot landed on runway 3 unaware of a quartering right tail wind estimated at 15 kt. The pilot reported that he had called the Wilcox FBO before landing and…
- [Accident 20110408005329A](https://openairdocs.org/incident/20110408005329A), Apr 8, 2011: Rockwell International 500-S (N51RF), Eden Prairie, MN, Substantial damage. Pilot lost directional control of aircraft after touchdown, the aircraft veered left and went off the runway.
- [Incident 20081116852829I](https://openairdocs.org/incident/20081116852829I), Nov 16, 2008: Aerocd 500S (N65375), Goldsboro, NC, Minor damage. The pilot stated that he had his mechanic, [privacy data omitted] service the right main landing gear by replacing the strut "o" rings just prior to the post…
- [Incident 20070308006449I](https://openairdocs.org/incident/20070308006449I), Mar 8, 2007: Gulstm 500S (N280MB), Springfield, IL. (-23) [privacy data omitted] aircraft departed sheboygan, WI, to take aerial photos in the st. louis area. After an estimated 4 hours of flight at a point…
- [Incident 20030621015549I](https://openairdocs.org/incident/20030621015549I), Jun 21, 2003: Gulstm 500S (N507JP), West Palm Beach, FL, Minor damage. (-23) While on a flight from jacksonville FL. (Crg) to fort lauderdale (fxe), N507JP experienced engine problems on the #2 engine. The pilot was Mr. John…
- [Accident 20030319003549A](https://openairdocs.org/incident/20030319003549A), Mar 19, 2003: Gulstm 500S (N903AK), Chickaloon, AK, Substantial damage. (-23) On March 19, 2003 at about 1015 local time a rockwell 500S commander (N903AK) piloted by Mr. Matt tomter was on a FAR part 91.407(b) maintenance check…
- [Incident 20020408006989I](https://openairdocs.org/incident/20020408006989I), Apr 8, 2002: Gulstm 500S (N8536), Jackson, AL. (-23) While on an IFR flight plan from bessemer, Alabama (eky) to mobile, Alabama (bfm), N8536 was at a cruising altitude of 8,000 feet when the aircraft lost…
- [Accident 20020217002339A](https://openairdocs.org/incident/20020217002339A), Feb 17, 2002: Gulstm 500S (N999N), Exeter, RI, No damage, 1 fatal. (-23) Narrative attached in ptrs form. Record id, NE012002B0583. Other address listed in isis under aircraft registry master file: [privacy data omitted] NTSB…
- [Incident 20010220004789I](https://openairdocs.org/incident/20010220004789I), Feb 20, 2001: Gulstm 500S (N2BZ), Palmetto, FL, Minor damage. (-23) On February 20, 2001 about 1230 EST, a rockwell international N2BZ departed tampa inbound to sarasota. Pilot noted a gear unsafe warning light and no…
- [Accident 19990106000189A](https://openairdocs.org/incident/19990106000189A), Jan 6, 1999: Gulstm 500S (N50BA), Plymouth, IN, Substantial damage. Byerly aviation air taxi slid off the rwy after landing and sustained substantial damage. No injuries were reported to the 6 POB. (.19) on January 6, 1999, at…
- [Accident 19910714027129A](https://openairdocs.org/incident/19910714027129A), Jul 14, 1991: Gulstm 500S (N260AC), Kahului, HI, Substantial damage. Both engines quit. Ditched in ocean near shore. Possibly not refueled properly last refueling.
- [Incident 19900303009269I](https://openairdocs.org/incident/19900303009269I), Mar 3, 1990: Gulstm 500S (N2BZ), Fernald, IA. Both engines quit due to fuel exhaustion. Made forced landing in field. Refueled and took off.
- [Accident 19880508053249A](https://openairdocs.org/incident/19880508053249A), May 8, 1988: Gulstm 500S (N57222), Jacksonville, FL, Substantial damage. Left gear collapsed on engine shutdown after parking. Witness reported rough handling by pilot. Gear not maintained
- [Incident 19840210011149I](https://openairdocs.org/incident/19840210011149I), Feb 10, 1984: Gulstm 500S (N95SA), Miami, FL, Minor damage. Left wing tip struck the rudder of a parked aircraft. Was repositioning the aircraft for maintenance.
- [Accident 19830129008409A](https://openairdocs.org/incident/19830129008409A), Jan 29, 1983: Gulstm 500S (N57222), Kansas City, KS, Substantial damage. Aircraft crashed during emergency landing due to fuel exhaustion.
- [Incident 19800126015899I](https://openairdocs.org/incident/19800126015899I), Jan 26, 1980: Rkwell 690B (N42MS), Aspen, CO, Minor damage. Aircraft touched down 3800 feet past threshold. Pilot lost directional control during reversing operation.
- [Incident 19780903017269I](https://openairdocs.org/incident/19780903017269I), Sep 3, 1978: Rkwell 500S (N83SA), Ft Collins, CO, Minor damage. Aircraft touched down with gear up. Extended gear, landed safely.
- [Accident 19780707023369A](https://openairdocs.org/incident/19780707023369A), Jul 7, 1978: Rkwell 500S (N280MB), Beaver Falls, PA, Substantial damage. Ground observers told pilot his nosewheel was locked during low ps over field.

## Service difficulty reports (107, newest 50)

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

- [SDR 2022FA0000287](https://openairdocs.org/sdr/2022FA0000287), Mar 2, 2022: TRUNNION. BROKEN. RIGHT MAIN LANDING GEAR FAILED TO EXTEND. LANDING GEAR CASTING FAILURE AT ACTUATOR ATTACHMENT
- [SDR 2013FA0000406](https://openairdocs.org/sdr/2013FA0000406), Jul 12, 2013: DRIVE ASSY. ACTIVATED. DURING FLIGHT, ACFT HAD STRONG BURNING ODOR IN CABIN. INVESTIGATION AND INSPECTION FOUND AIR CONDITIONING COOLING SYSTEM COMPRESSOR DRIVE MOTOR FAILED. UPON REM
- [SDR 2013F00003](https://openairdocs.org/sdr/2013F00003), Jul 23, 2012: LINE. LEAKING. HYDRAULIC FAILURE OCCURRED DUE TO THE HOSE FOR HYD PRESSURE GAUGE BEING DAMAGED, RESULTING IN LEAKAGE OF HYD FLUID AND SUBSEQUENTLY THE INDICATION OF SYS PRESSU
- [SDR V8Z2011F00000](https://openairdocs.org/sdr/V8Z2011F00000), Jun 22, 2011: O-RING. DAMAGED. O-RING IN THE LT MLG RETRACT CYLINDER FAILED WHICH ALLOWED THE HYD SYS OIL TO DRAIN. O-RING WAS MOST LIKELY DAMAGED DURING INSTALLATION. DURING INSTALLATION OF 
- [SDR CA100127016](https://openairdocs.org/sdr/CA100127016), Jan 5, 2010: SPAR CAP. CORRODED. (CAN) AFTER ACCOMPLISHING AD 94-04-14 IT WAS NOTED THAT THE WING LOWER SPAR CAP WAS CORRODED BEYOND THE SAFE LIMIT ACCORDING TO SB 208A. THE ACFT WAS GROUNDED.
- [SDR 2009FA0000306](https://openairdocs.org/sdr/2009FA0000306), Apr 1, 2009: PIN. WORN. PIN IS WORN AND STOP NOSE WHEEL FROM CANTERING, WHEN GEAR WAS RETRACTED, NOSE WHEEL GOT JAMMED IN THE WHEEL WELL AND WOULD NOT EXTEND OR RETRACT. ACFT LANDED WI
- [SDR CA090226003](https://openairdocs.org/sdr/CA090226003), Feb 24, 2009: BRACKET. LOOSE. (CAN) DURING GEAR SWING INSP, IT WAS NOTED THAT ON THE NOSE GEAR DOWN AND LOCKED CYCLE THERE WAS CONSIDERABLE MOVEMENT ON THE ACFT STRUCTURE THAT ATTACHES TO TH
- [SDR CA090129015](https://openairdocs.org/sdr/CA090129015), Jan 26, 2009: SHAFT. CRACKED. ON VISUAL INSPECTION OF THE NOSE LANDING GEAR DRAG BRACE AND BUNGEE SYSTEM, IT WAS FOUND THAT THE SHAFT LINKING THE DRAG BRACE TO THE BUNGEE WAS CRACKED AT THE 
- [SDR EHS2008F00001](https://openairdocs.org/sdr/EHS2008F00001), Aug 11, 2008: O-RING. LEAKING. WHILE FLYING A FIRE MISSION IN SUPPORT OF USFS, THE PILOT NOTICED THE RT GEAR START TO EXTEND FOLLOWED BY A LOSS OF HYDRAULIC PRESSURE. PILOT RETURNED TO THE AI
- [SDR EHS2008F00000](https://openairdocs.org/sdr/EHS2008F00000), Jul 2, 2008: PISTON. BURNED. WHILE FLYING A FIRE MISSION IN SUPPORT OF USFS, THE PILOT NOTICED THE RT ENG OIL PRESSURE FLOWLY STARTING TO DECREASE. THE DECISION WAS MADE TO RETURN TO THE AI
- [SDR 2008FA0000167](https://openairdocs.org/sdr/2008FA0000167), Feb 26, 2008: MAGNETO. WORN. ENGINE WAS GETTING HARD TO START, CHECKED MAG TIMING AND FOUND LT MAG TIMING OUT OF LIMITS, DISASSEMBLED MAG AND FOUND THE CAM WORN OUT . 81.1 HRS SINCE NEW.
- [SDR 2008FA0000164](https://openairdocs.org/sdr/2008FA0000164), Jan 10, 2008: MAGNETO. WORN. ENGINE WAS GETTING HARD TO START, CHECKED MAG TIMING AND FOUND LT MAG TIMING OUT OF LIMITS, DISASSEMBLED MAG AND FOUND THE CAM WORN OUT . 100.3 HRS SINCE NEW
- [SDR 2008FA0000013](https://openairdocs.org/sdr/2008FA0000013), Jan 2, 2008: MAGNETO. WORN. CAM LOBE INSIDE MAG THAT OPENS AND CLOSES POINTS WORN OUT.
- [SDR CA070517007](https://openairdocs.org/sdr/CA070517007), May 8, 2007: WINGLET. SEPARATED. (CAN) IT WAS FOUND THAT THE SHEET METAL SCREWS HOLDING THE TIP ON THE WING HAD ALL COME LOOSE. THE WING TIP THEN VIBRATED FOR A PERIOD OF TIME ,ELONGATING THE S
- [SDR 2007FA0000268](https://openairdocs.org/sdr/2007FA0000268), Mar 8, 2007: B-NUT. LOOSE. PILOT NOTICED A FLUCTUATION AND LOSS OF HYDRAULIC PRESSURE IN FLIGHT, AFTER INSPECTION THE FORWARD HYDRAULIC HOSE B-NUT ON THE LT GEAR ACTUATOR WAS FOUND TO BE 
- [SDR CA070201009](https://openairdocs.org/sdr/CA070201009), Feb 1, 2007: BRACKET. WORN. (CAN) THE ALTERNATOR ADJUSTING BRACKET BOLT HOLE THAT ATTACHES THE BRACKET TO THE ENGINE WAS FOUND CRACKED ALL THE WAY THROUGH. THE BRACKET WAS ONLY BEING HELD 
- [SDR K512006F00000](https://openairdocs.org/sdr/K512006F00000), Aug 1, 2006: BEARING. FAILED. FWD BEARING FAILED IN CUMBUSTION AIR BLOWER LACK OF COMBUSTION AIR PRESSURIZE SHUT DOWN THE HEATER, BUT SMOKE FROM THE BLOWER MOTOR CAME INTO THE COCKPIT AREA. 
- [SDR 2006FA0000466](https://openairdocs.org/sdr/2006FA0000466), Apr 10, 2006: CONNECTING ROD. BROKEN. CUSTOMER WAS ENROUTE TO MAINTENANCE SHOP TO GET ANNUAL INSPECTION, BOTH ENGINES OVERHAULED. RT ENGINE CYLINDER NR 2 CONNECTING ROD BROKE AT THE CRANKSHAFT ATTAC
- [SDR AU510002170](https://openairdocs.org/sdr/AU510002170), Dec 12, 2005: SEAL. WORN. RT MAIN LANDING GEAR RAM SEALS WORN AND LEAKING. LOSS OF HYDRAULIC FLUID.
- [SDR CA050724001](https://openairdocs.org/sdr/CA050724001), Jul 8, 2005: CRANKSHAFT. SHEARED. CRANKSHAFT SPLIT NEXT TO THE NR 3 MAIN BEARING JOURNAL. FAILURE NEXT TO THE NR 4 CONNECTING ROD. CRANKSHAFT THEN BROKE INTO 3 PIECES AND PUNCTURED THE CRANKCASE
- [SDR AU510001503](https://openairdocs.org/sdr/AU510001503), Jun 6, 2005: LINE. BROKEN. (AUS) RT ENGINE NR 2 CYLINDER FUEL INJECTOR LINE BROKEN AT NIPPLE. (CASA NR 510001503).
- [SDR AUS20031276](https://openairdocs.org/sdr/AUS20031276), Dec 18, 2003: SEAL. DAMAGED. (AUS) RT ENGINE OIL FILTER SEAL DAMAGED AND LEAKING. SUSPECT SEAL DAMAGED DURING INSTALLATION. PERSONNEL/MAINTENANCE ERROR.
- [SDR 2003FA0001271](https://openairdocs.org/sdr/2003FA0001271), Dec 2, 2003: CRANKCASE. FAILED. DURING ROUTINE FLIGHT, LOUD NOISE WAS HEARD. RT ENGINE WAS SHUT DOWN AND SECURED. AFTER AN UNEVENTFUL LANDING, AN INSPECTION REVEALED A CATASTROPHIC CRANKCASE F
- [SDR AUS20031077](https://openairdocs.org/sdr/AUS20031077), Oct 22, 2003: RIB. CRACKED. (AUS) RT ELEVATOR FORWARD RIB CRACKED AT TORQUE TUBE OUTBOARD MOUNTING FLANGE. RIB CONTAINS TWO CRACKS FROM TOP AND BOTTOM ATTACHMENT RIVETS.
- [SDR AUS20031298](https://openairdocs.org/sdr/AUS20031298), Sep 26, 2003: CLEVIS. CRACKED. (AUS) MAIN LANDING GEAR CLEVIS CRACKED. FOUND USING MAGNETIC PARTICLE INSPECTION AND VISUAL TECHNIQUES.
- [SDR AUS20030955](https://openairdocs.org/sdr/AUS20030955), Sep 19, 2003: MAGNETO. OUT OF ADJUST. (AUS) LT ENGINE LOST OIL PRESSURE. INSPECTION FOUND NR 4 PISTON FAILED DUE TO DETONATION. FURTHER INVESTIGATION FOUND THE LT MAGNETO TIMING HAD MOVED FROM 20 DE
- [SDR AUS20030975](https://openairdocs.org/sdr/AUS20030975), Sep 16, 2003: PIN. CRACKED. (AUS) LT AND RT MAIN LANDING GEAR ACTUATOR CLEVIS PINS CRACKED.
- [SDR AUS20031078](https://openairdocs.org/sdr/AUS20031078), Sep 12, 2003: RIB. CRACKED. (AUS) RT ELEVATOR FORWARD RIB CRACKED AT TORQUE TUBE OUTBOARD MOUNTING FLANGE. RIB IS CRACKED IN TWO PLACES FROM TOP AND BOTTOM ATTACHMENT RIVETS.
- [SDR AUS20030976](https://openairdocs.org/sdr/AUS20030976), Sep 3, 2003: PIN. CRACKED. (AUS) LT AND RT MAIN LANDING GEAR ACTUATOR CLEVIS PINS CRACKED.
- [SDR AUS20030974](https://openairdocs.org/sdr/AUS20030974), Aug 15, 2003: PIN. CRACKED. (AUS) LT AND RT MAIN LANDING GEAR ACTUATOR CLEVIS PINS CRACKED.
- [SDR 2003FA0000754](https://openairdocs.org/sdr/2003FA0000754), Jul 14, 2003: PROPELLER. INOPERATIVE. PROPELLER ASSY, AIRCRAFT CREW REPORTED RT PROPELLER GOES TO FEATHER ON TAXI WITH HOT OIL. ENGINE AND PROP GOVERNOR CHANGED. PROPELLER SWAPPED. PROBLEM FOUND TO 
- [SDR 03IN170035](https://openairdocs.org/sdr/03IN170035), Jun 21, 2003: CYLINDER HEAD. DEPARTED. A/C EXPERIENCED ENG PROBLEMS APPROX 2 MINUTES AFTER INITIATING DESCENT FROM 11,500. PILOT NOTICED VIBRATION, OBSERVED RT ENG FUEL FLOW FLUCTUATING. ENRICHED FUE
- [SDR AUS20030792](https://openairdocs.org/sdr/AUS20030792), May 28, 2003: CLEVIS. FRACTURED. (AUS) LT MAIN LANDING GEAR ACTUATOR CLEVIS FRACTURED.
- [SDR AUS20030549](https://openairdocs.org/sdr/AUS20030549), May 16, 2003: SEPARATOR. CONTAMINATED. (AUS) RT ENGINE FUEL VAPOUR SEPARATOR BLOCKED BY PARTICLES OF UNKNOWN TYPE.
- [SDR AUS20030571](https://openairdocs.org/sdr/AUS20030571), Apr 26, 2003: ENGINE. FAILED. (AUS) LT ENGINE FAILED TO RESTART IN FLIGHT AFTER AN INTENTIONAL SHUTDOWN. INVESTIGATION COULD FIND NO PROBLEMS WITH THE ENGINE. SUSPECT CAUSED BY OVERPRIMING O
- [SDR FTU2003F00006](https://openairdocs.org/sdr/FTU2003F00006), Apr 14, 2003: ENGINE. CONTAMINATED. DURING A ROUTINE OIL CHANGE WHEN OIL FILTER WAS CUT OPEN FOR INSPECTION, A LARGE AMOUNT OF SILVER PARTICILES WERE FOUND. OIL SUMP SCREEN WAS REMOVED FOR INSPECT
- [SDR FTU2003F00000](https://openairdocs.org/sdr/FTU2003F00000), Dec 19, 2002: BRACKET. BROKEN. DURING ANNUAL INSPECTION AND REMOVAL OF ENGINE FOR OVERHAUL, ALTERNATOR BELT TENSION BRACKET WAS FOUND BROKEN AT THE END THAT IS BOLTED TO THE ENGINE NOSE CASE.
- [SDR AUS20021333](https://openairdocs.org/sdr/AUS20021333), Nov 15, 2002: CABLE. WORN. (AUS) AILERON CABLE FRAYED IN AREA OF FAIRLEAD LOCATED OUTBOARD OF LH NACELLE.
- [SDR AUS20020874](https://openairdocs.org/sdr/AUS20020874), Aug 9, 2002: RESTRICTOR VALVE. BLOCKED. (AUS) FUEL VAPOR SEPARATOR / FILTER ASSEMBLY RESTRICTOR BLOCKED. THE RESTRICTOR IS LOCATED IN THE RETURN LINE FROM THE FUEL DISTRIBUTOR VALVE.
- [SDR AUS20020686](https://openairdocs.org/sdr/AUS20020686), Jul 14, 2002: ENGINE. MALFUNCTIONED. (AUS) LT ENGINE VIBRATING AND LOSING POWER. LIMITED INFORMATION PROVIDED.
- [SDR CA020507021](https://openairdocs.org/sdr/CA020507021), Apr 26, 2002: STUD. SHEARED. (CAN) WHEN THE PILOT SELECTED GEAR DOWN, DID NOT RECEIVE A GREEN NOSE GEAR LIGHT. PILOT DID FLY BYS AND IT WAS NOTED NOSE GEAR WAS NOT IN LOCKED POSITION. PILOT
- [SDR AUS20020295](https://openairdocs.org/sdr/AUS20020295), Mar 20, 2002: DIAPHRAGM. DAMAGED. (AUS) LH ENGINE MANIFOLD VALVE DIAPHRAGM TORN. LENGTH OF TEAR APPROXIMATELY 12.7MM (0.5IN).
- [SDR DO32002F00000](https://openairdocs.org/sdr/DO32002F00000), Dec 13, 2001: LINE. CHAFED. HYDRAULIC PUMP PRESSURE LINE (PN790246-167) AND HYDRAULIC SUPPLY LINE (PN 790246-167). HYDRAULIC LINES ARE LOCATED FORWARD OF EACH MAIN LANDING GEAR ASSEMBLY ON
- [SDR AUS20011017](https://openairdocs.org/sdr/AUS20011017), Sep 21, 2001: PLATE. CORRODED. (AUS) EXTERNAL SPAR CAP SUPPORT PLATE RH SIDE CORRODED IN AREA OF JOINT BETWEEN TWO PLATES. EVIDENCE OF CORROSION IN SIMILAR AREA ON LH SIDE.
- [SDR AUS20010904](https://openairdocs.org/sdr/AUS20010904), Aug 14, 2001: STUD. SHEARED. (AUS) LH ENGINE NO4 CYLINDER HOLDDOWN STUDS (3OFF) SHEARED. FOLLOWING REMOVAL OF THE CYLINDER THE CRANKCASE WAS FOUND TO BE CRACKED THROUGH THE AREA OF THE HOLD
- [SDR AUS20010875](https://openairdocs.org/sdr/AUS20010875), Aug 13, 2001: BEARING. DELAMINATED. (AUS) ENGINE FRONT MAIN BEARING DEFECTIVE. BEARING MATERIAL APPEARS TOBE DELAMINATED FROM BEARING SHELL. METAL CONTAMINATION OF OIL SYSTEM. SUSPECT MANUFACTURIN
- [SDR CA010628039](https://openairdocs.org/sdr/CA010628039), Jun 28, 2001: CAMSHAFT. WORN. (CAN) ENGINE HAD BEEN HARD TO START, LOW STATIC RPM AND HIGH MANIFOLD PRESSURE. ENGINE INSP. REVEALED THAT THE CAMSHAFT LOBE THAT DRIVES NR 5&6 CYL INTAKE VALVE
- [SDR AUS20010689](https://openairdocs.org/sdr/AUS20010689), Jun 22, 2001: CYLINDER. DAMAGED. (AUS) ENGINE CYLINDER HOLED IN AREA ADJACENT TO TOP SPARK PLUG HOLE.
- [SDR AUS20010556](https://openairdocs.org/sdr/AUS20010556), May 28, 2001: PIN. CRACKED. (AUS) MAIN LANDING GEAR CLEVIS PIN CRACKED FROM BOLT HOLE. FOUND DURING INSPECTION IAW SL 376.
- [SDR AUS20010451](https://openairdocs.org/sdr/AUS20010451), Apr 20, 2001: WASHER. FAILED. (AUS) RH ENGINE COUNTERWEIGHT RETAINING WASHER PNO 71907 HAD FAILED ALLOWING THE COUNTERWEIGHT ROLLER PNO 72797 TO MIGRATE ANDCONTACT NO5 CYLINDER CONNECTING RO

All 107: https://openairdocs.org/model/rockwell-international-500-s/reports.md

## STCs that may be installed (OpenAirDocs) (227, 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 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 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 SA8453SW](https://openairdocs.org/stc/SA8453SW): Replace the o-ring seals in the landing gear lower strut. Metrea Special Aerospace ISR Inc
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): 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 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 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 SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine
- [STC SA01435LA](https://openairdocs.org/stc/SA01435LA): Installation of engines modified with Firewall Forward Technologies LLC modified camshaft. Centri-Lube Technologies LLC
- [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 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 SA706GL](https://openairdocs.org/stc/SA706GL): Install Cleveland conversion kit P/N 199-122 (for aircraft using MIL-H05606 brake fluid), or199-122A (for aircraft using 'Skydrol' brake fluid). Kaman Corporation Aircraft Wheel and Brake LLC
- [STC SA1457GL](https://openairdocs.org/stc/SA1457GL): Installation of a Cleveland nose wheel. Kaman Corporation Aircraft Wheel and Brake LLC
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc
- [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 SA11174SC PAGE 2](https://openairdocs.org/stc/SA11174SC%20PAGE%202): 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 SA02426AK](https://openairdocs.org/stc/SA02426AK): Approval of the FreeFlight FDL-978-TX ADS-B system installed. FreeFlight Systems
- [STC SA09763DS](https://openairdocs.org/stc/SA09763DS): Installation of an S-TEC 01326 Digital Flight Control System (DFCS). S-TEC Corporation
- [STC SA02700SE](https://openairdocs.org/stc/SA02700SE): Installation of a Supplemental Lighting System. Aviation Specialties Unlimited 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 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 SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation
- [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation
- [STC SA00344BO PAGE 2](https://openairdocs.org/stc/SA00344BO%20PAGE%202): 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 2](https://openairdocs.org/stc/SA02153LA-D%20PAGE%202): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc
- [STC SA02503AK](https://openairdocs.org/stc/SA02503AK): Installation of AMSAFE State of the Art Restraint System (SOARS) inflatable restraints. AMSAFE Inc
- [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation
- [STC SA01828SE](https://openairdocs.org/stc/SA01828SE): Installation of J.P. Instruments (JPI) EDM-960 Primary Engine Data Management System. J. P. Instruments
- [STC SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine
- [STC SA00024NY](https://openairdocs.org/stc/SA00024NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less. Airwolf Filter Corporation
- [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA02212AK](https://openairdocs.org/stc/SA02212AK): Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Seaplanes North LLC
- [STC SA2586NM](https://openairdocs.org/stc/SA2586NM): Installation of J.P. Instruments temperature monitoring systems. J P Instruments
- [STC SA00382BO](https://openairdocs.org/stc/SA00382BO): Installation of Globalstar Antenna and Cradle provisions to support a Globalstar GPS-1700 in non-composite airplanes. Avidyne Corporation
- [STC SA02428SE](https://openairdocs.org/stc/SA02428SE): Installation of an Air Stream Switch for an electric time recording device on non-pressurized aircraft. Henry F Rogers/David E Polley

All 227: https://openairdocs.org/model/rockwell-international-500-s/stcs.md

## PMA parts (OpenAirDocs) (739, 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.

- [PM-215](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190279733220260625165813.0001): Radome Mask. PM Research, Inc. · PMA PQ10049NE · Modification part · Nov 20, 2024
- [PM-212](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170389039020260625165813.0001): Slipper Wing Tank Mask. PM Research, Inc. · PMA PQ10049NE · Modification part · Nov 20, 2024
- [PM-210](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144916743520251118174432.0001): Radome Mask. PM Research, Inc. · PMA PQ10049NE · Modification part · Nov 20, 2024
- [PM-62](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136515101120251118173816.0001): Radome Mask. PM Research, Inc. · PMA PQ10049NE · Modification part · Nov 20, 2024
- [3111-022ACD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171700726420240917173614.0001): Shim, Brass. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 3111-022 · Sep 4, 2024
- [APS68-03300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID150398778920231102131432.0001): Shim, Brake. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 068-03300 · Sep 25, 2023
- [8000353](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID109620339120221130202559.0001): Engine Oil Cooler. Aero-Classics Heat Transfer Products Inc · PMA PQ2543NM · Replaces Twin Commander630146-509 · Oct 21, 2022
- [APS66-09000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117304379120221020170349.0001): Brake Lining. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 066-09000 · Aug 10, 2022
- [APS177-01600](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID112494461720221020170359.0001): Pin. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 177-01600 · Aug 10, 2022
- [01-0790906-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179133417420220706160228.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · Jun 21, 2022
- [AG627000-13](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105709356820220809130937.0001): Gasket – Marker Beacon. Aviation Devices & Electronic Components LLC (Av-DEC) · PMA PQ3846SW · Modification part · May 10, 2022
- [EA-22000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179015092520220525194438.0001): Controller Wire Harness (14 Pin). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [EA-22000T](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156290539620220525194557.0001): Controller Wire Harness- Twin (14 Pin). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [EA-21000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121833341520220525194325.0001): Six-Cylinder Ignition Controller. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180258754520220809102608.0001): Aviation Devices & Electronic Components LLC (Av-DEC) · PMA PQ3846SW · Apr 18, 2022
- [AG844000-15](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196870767020220408135825.0001): Gasket – UHF/VHF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Feb 8, 2022
- [AG728000-52](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199850266420220408135739.0001): Gasket – Satcom Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Jan 26, 2022
- [RA068-03300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID857416699720220208125018.0001): Shim - Insulator. Rapco Inc · PMA PQ2101CE · Replaces 068-03300 · Jan 20, 2022
- [AG627000-23](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147271201220220408135724.0001): Gasket – Marker Beacon. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Dec 15, 2021
- [AG358000-08](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169149641220220408135836.0001): Gasket – ELT Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 17, 2021
- [AG627000-12](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID160088362320220408140259.0001): Gasket – Marker Beacon Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 17, 2021
- [AG843000-17](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID754109297720211110110533.0001): Gasket - UHF/VHF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Aug 9, 2021
- [EA-23000-A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID966963424420210923143740.0001): EA-23000 Ignition/Starter Switch Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jul 28, 2021
- [EA-23000-A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID689224648120210923143842.0001): EA-23000 Ignition/Starter Switch Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jul 28, 2021
- [MDL-500004-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID644234834820210622140343.0001): Supplemental Lighting System. Aviation Specialties Unlimited Inc · PMA PQ2538NM · Modification part · Mar 11, 2021
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID641445462021070217524901.0001): Aspen Avionics · PMA PQ03868SW · Jan 20, 2021
- [ST-983ST-983-1ST-983-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID247884446620210727191932.0001): Installation of S-TEC 01326 Digital Flight Control System (DFCS)Installation of S-TEC 01326 Digital Flight Control System (DFCS)Installation of S-TEC 01326 Digital Flight Control System (DFCS). S-TEC Corporation · PMA PQ0445SW · Modification part · Jan 12, 2021
- [AG358000-07](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID738714019620210727195156.0001): Gasket – ELT Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Dec 11, 2020
- [1049-4000-03-001C](https://drs.faa.gov/browse/excelExternalWindow/FB6A4D62429A217F86258633006145AB.0001): Roll Steering Converter. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4201-20](https://drs.faa.gov/browse/excelExternalWindow/ED78E4F8D3C63347862586330061461D.0001): Annunciator Kit GDC31. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4200-20](https://drs.faa.gov/browse/excelExternalWindow/CBC6239248334CCE86258633006145E5.0001): Connector Kit GDC31. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4200-50](https://drs.faa.gov/browse/excelExternalWindow/86CBD103649292948625863300614693.0001): Isolation Coupler Installation Kit. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4000-03-001B](https://drs.faa.gov/browse/excelExternalWindow/80F9B5EC9801FD16862586330061456E.0001): Roll Steering Converter. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4801-01](https://drs.faa.gov/browse/excelExternalWindow/39A0DF401545910A8625863300614652.0001): Isolation Coupler. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [AG843000-79](https://drs.faa.gov/browse/excelExternalWindow/7C47B4B54B5941DF862586240047DC8E.0001): Gasket - UHF / AM / IFF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 17, 2020
- [AG477000-35](https://drs.faa.gov/browse/excelExternalWindow/CAA7A03C831CF5A78625861F004520E1.0001): Gasket - GPS ANTENNA. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 11, 2020
- [APS68-03300](https://drs.faa.gov/browse/excelExternalWindow/59A6A96FB4AE250A862586290049F16B.0001): Shim, Brake. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 068-03300 · Nov 4, 2020
- [AG822000-09](https://drs.faa.gov/browse/excelExternalWindow/B363A74FB05068CA862586020044D52C.0001): Gasket - TCAS Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Oct 13, 2020
- [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
- [RA154-03000](https://drs.faa.gov/browse/excelExternalWindow/DD82997F649BC443862585E40035802A.0001): Molded Grease Seal. Rapco Inc · PMA PQ2101CE · Replaces Cleveland Wheels & Brakes 154-03000 · 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
- [APS068-03300](https://drs.faa.gov/browse/excelExternalWindow/A32F8EBA841374C6862585EC00452418.0001): Shim, Brake. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 068-03300 · Aug 26, 2020
- [AG247000-05](https://drs.faa.gov/browse/excelExternalWindow/A8B3EE75D8E4BBD2862585E5006243CC.0001): Gasket - Security System Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Aug 24, 2020
- [AG843000-19](https://drs.faa.gov/browse/excelExternalWindow/6325AFC5586C8E34862585E500649009.0001): Gasket - VHF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Aug 24, 2020
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID994155796020220125131516.0001): DAC International · PMA PQ0986SW · Jul 31, 2020

All of them: https://openairdocs.org/model/rockwell-international-500-s/pma.md

## The same model under other registry codes

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

- [Aero Commander 500 S](https://openairdocs.org/model/aero-commander-500-s): 45 registered aircraft, registry code 0141107

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