# C A S A C-212-DF - Type: Aircraft model (FAA registry) - Registry code: 2410205 - Manufacturer (registry): C A S A - Model: C-212-DF - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-prop - Seats: 19 - Weight class: 12,500 to 19,999 lb - Certification: Type certificated - Data sheet: [TCDS A43EU](https://openairdocs.org/tcds/A43EU) (OpenAirDocs) - Holder: Airbus Defense and Space S.A. - Registered aircraft: 3 - Page: https://openairdocs.org/model/c-a-s-a-c-212-df 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 2022-17-06](https://openairdocs.org/ad/2022-17-06): Fuselage · Airbus Defense and Space C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Sep 29, 2022 - [AD 2020-03-18](https://openairdocs.org/ad/2020-03-18): Flight Controls · Airbus Defense and Space C-212-CB, C-212-CC, C-212-CD and 2 more. Effective Apr 2, 2020 - [AD 2018-19-02](https://openairdocs.org/ad/2018-19-02): Flight controls · Airbus Defense and Space C-212-CB, C-212-CC, C-212-CD and 2 more. Effective Oct 22, 2018 - [AD 2017-01-10](https://openairdocs.org/ad/2017-01-10): Flight controls · Airbus Defense and Space C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Feb 22, 2017 - [AD 2015-16-04](https://openairdocs.org/ad/2015-16-04): Fire Protection · Airbus Defense and Space C-212-CB, C-212-CC, C-212-CD and 23 more. Effective Sep 15, 2015 - [AD 2013-24-09](https://openairdocs.org/ad/2013-24-09): Engine Controls · EADS CASA C-212-CB, C-212-CC, C-212-CD and 2 more. Effective Jan 21, 2014 - [AD 2009-02-01](https://openairdocs.org/ad/2009-02-01): Center wing attachment fittings · EADS CASA C-212-DF. Effective Mar 9, 2009 - [AD 2008-06-13](https://openairdocs.org/ad/2008-06-13): Centre wing lower skin · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Apr 17, 2008 - [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 2004-07-17](https://openairdocs.org/ad/2004-07-17): Nose landing gear (NLG) · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective May 11, 2004 - [AD 99-19-15](https://openairdocs.org/ad/99-19-15): AFM - Limitations Section - Ice Protection Systems · EADS CASA C-212-CB, C-212-CC, C-212-CD and 8 more. Effective Dec 27, 1999 - [AD 99-04-02](https://openairdocs.org/ad/99-04-02): Inspect Fuel Pump Cover Plates For Spark Marks · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Mar 17, 1999 - [AD 98-22-04](https://openairdocs.org/ad/98-22-04): Power Quadrant Cover · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Nov 27, 1998 - [AD 98-18-21](https://openairdocs.org/ad/98-18-21): Corrosion Inspection · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Oct 20, 1998 - [AD 98-12-28](https://openairdocs.org/ad/98-12-28): Inspect False Spar Of Wing For Cracking · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Jul 15, 1998 - [AD 98-10-08](https://openairdocs.org/ad/98-10-08): Lower Shaft & Support Structure Of Rudder · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Jun 17, 1998 - [AD 98-06-02](https://openairdocs.org/ad/98-06-02): Inspect Spherical Bearings Of Aileron Control Rod · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Apr 15, 1998 - [AD 97-21-14](https://openairdocs.org/ad/97-21-14): Inspect Restrictor Pistons · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Nov 24, 1997 - [AD 97-03-13](https://openairdocs.org/ad/97-03-13): Rudder Pedal Setting Mechanisms · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Mar 14, 1997 - [AD 96-09-22](https://openairdocs.org/ad/96-09-22): AFM - Icing · EADS CASA C-212-CB, C-212-CC, C-212-CD and 7 more. Effective Jun 11, 1996 - [AD 92-13-51](https://openairdocs.org/ad/92-13-51): Backup Blocking Device · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Jul 31, 1992 - [AD 91-03-10](https://openairdocs.org/ad/91-03-10): Propeller Speed & Pitch Control System · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Mar 11, 1991 - [AD 89-23-16](https://openairdocs.org/ad/89-23-16): Power Reserve System · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Dec 12, 1989 - [AD 89-22-09](https://openairdocs.org/ad/89-22-09): Passenger Door Evacuation · Step and handrails (Fischer Brothers Avn STC SA906GL). Effective Nov 20, 1989 - [AD 89-19-05](https://openairdocs.org/ad/89-19-05): Rear Passenger Seats · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Oct 14, 1989 - [AD 89-21-08](https://openairdocs.org/ad/89-21-08): Trim Control System · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Oct 5, 1989 - [AD 89-02-08 R1](https://openairdocs.org/ad/89-02-08-R1): Wing Flap Control System · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Sep 5, 1989 - [AD 89-05-01](https://openairdocs.org/ad/89-05-01): Wing Flap Control System · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Apr 3, 1989 - [AD 88-09-02](https://openairdocs.org/ad/88-09-02): Fuel Shut-Off Valves · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Jun 1, 1988 - [AD 87-16-04](https://openairdocs.org/ad/87-16-04): Stall Warning System · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Aug 31, 1987 - [AD 87-10-08](https://openairdocs.org/ad/87-10-08): Crew Door Handle Cover · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Jun 19, 1987 - [AD 87-05-07](https://openairdocs.org/ad/87-05-07): Attendant's Seat · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Mar 25, 1987 - [AD 87-05-06](https://openairdocs.org/ad/87-05-06): Propeller Feathering Control · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Mar 25, 1987 - [AD 87-04-10](https://openairdocs.org/ad/87-04-10): Smoke Detector System · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Mar 9, 1987 - [AD 87-04-02](https://openairdocs.org/ad/87-04-02): Nose Landing Gear · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Mar 2, 1987 - [AD 87-03-04](https://openairdocs.org/ad/87-03-04): Trim Control Markings & Placards · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Feb 19, 1987 - [AD 86-19-05](https://openairdocs.org/ad/86-19-05): Electrical System · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Oct 2, 1986 - [AD 84-12-03](https://openairdocs.org/ad/84-12-03): Structural Flight Controls and Fuel System · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Jul 23, 1984 - [AD 83-02-06](https://openairdocs.org/ad/83-02-06): Fuel Filter System · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Feb 7, 1983 Historical (superseded or no longer in force): - [AD 2021-16-07](https://openairdocs.org/ad/2021-16-07) (historical): Fuselage · Airbus Defense and Space C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Sep 28, 2021 - [AD 2017-19-08](https://openairdocs.org/ad/2017-19-08) (historical): Flight controls · Airbus Defense and Space C-212-CB, C-212-CC, C-212-CD and 2 more. Effective Oct 25, 2017 - [AD 2007-05-01](https://openairdocs.org/ad/2007-05-01) (historical): Cracks had been found in the centre wing lower skin. · Construcciones Aeronauticas C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Mar 14, 2007 - [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996 ## Registered aircraft (3) - [N33CP](https://openairdocs.org/aircraft/N33CP): [Conocophillips Alaska Inc](https://openairdocs.org/faa-owner/CONOCOPHILLIPS%20ALASKA%20INC), [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage), built 1990, S/N 393 - [N405CP](https://openairdocs.org/aircraft/N405CP): [Conocophillips Alaska Inc](https://openairdocs.org/faa-owner/CONOCOPHILLIPS%20ALASKA%20INC), [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage), built 1990, S/N 405 - [N620AR](https://openairdocs.org/aircraft/N620AR): [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), built 1989, S/N 379 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (44) As reported by operators and repair stations, by the model named in the report. - [SDR 8TNC202601220054](https://openairdocs.org/sdr/8TNC202601220054), Jan 22, 2026: FLOORBEAM. BENT. DURING ROUTINE OPERATIONS IN ANCHORAGE, AK (ANC), MAINTENANCE DISCOVERED DAMAGE TO THE ENDS OF LOWER FRAME 13 & 16 INNER FRAME T-CHORD FLANGES AT LBL19 & RBL19, - [SDR 8TNC202601220001](https://openairdocs.org/sdr/8TNC202601220001), Jan 22, 2026: SKIN. CRACKED. DURING ROUTINE MAINTENANCE IN ANCHORAGE, AK (ANC), MAINTENANCE NOTED THAT (2EA.) FASTENERS COMMON TO THE HORIZONTAL STABILIZER LOWER SKIN & SPAR CHORD HAVE CRAC - [SDR 2024F00264](https://openairdocs.org/sdr/2024F00264), Nov 2, 2024: MOTOR. FAILED. MOTOR INOPERATIVE - RETRACTABLE LANDING/TAXI LAMP ASSY - BURNT ELECTRICAL SMELL IN COCKPIT - [SDR 39LA20151117147](https://openairdocs.org/sdr/39LA20151117147), Nov 17, 2015: LANDING LIGHT. SHORTED. ON DEPARTURE, SMOKE NOTICED IN THE COCKPIT. DECLARED EMER & RETURNED. R & R LT LANDING LIGHT IAW MM 33-40-10. - [SDR 39LA20151015146](https://openairdocs.org/sdr/39LA20151015146), Oct 15, 2015: UNKNOWN. SMOKE. DURING APPROACH, THE FLIGHT CREW SMELLED & OBSERVED A PUFF OF SMOKE THAT CAME FROM THE BOTTOM LT SIDE OF THE INSTRUMENT PANEL. NO ACTION WAS TAKEN AS LANDING WA - [SDR 39LA20150501135](https://openairdocs.org/sdr/39LA20150501135), May 1, 2015: ESCAPE HATCH. DEPARTED. DURING TAKEOFF ROLL, THE TOP ESCAPE HATCH DEPARTED THE ACFT. THE TAKEOFF WAS ABORTED WITHOUT INCIDENT & RETURNED TO PARKING. - [SDR 39LA20150115105](https://openairdocs.org/sdr/39LA20150115105), Jan 15, 2015: UNKNOWN. SMOKE. DURING CLIMB OUT AT APPROX 10,000 FT MSL THE FLIGHT CREW REPORTED A STRONG SMOKE SMELL IN THE FLIGHT DECK FOLLOWED BY A PLUME OF SMOKE RISING FROM THE FLOOR BEN - [SDR 39LA20140917102](https://openairdocs.org/sdr/39LA20140917102), Sep 17, 2014: MOUNT FITTING. CORRODED. DURING NDT OF LT ENG MOUNT FITTING INSPECTION, FOUND AFT UPPER LT ENG MOUNT FITTING TO BE CORRODED. REMOVED UPPER ENG MOUNT FITTING PN 212-13116-01.2 & SENT OUT - [SDR 39LA20140917101](https://openairdocs.org/sdr/39LA20140917101), Sep 17, 2014: FRAME. DAMAGED. DURING INSPECTION FOUND NR 11 LT & NR 11 RT FRAMES DAMAGED. LOCALLY FABRICATED FRAMES. WORK PERFORMED IAW DWG 14019-2018 & 14019-2019 INSTRUCTIONS. - [SDR 39LA20140917100](https://openairdocs.org/sdr/39LA20140917100), Sep 17, 2014: FRAME. DAMAGED. DURING INSPECTION FOUND NR 6 LT & NR 6 RT FRAMES DAMAGED. LOCALLY FABRICATED FRAMES. WORK PERFORMED IAW DWG 14019-2013 & 14019-2014 INSTRUCTIONS. - [SDR 39LA2014090599](https://openairdocs.org/sdr/39LA2014090599), Sep 5, 2014: MOUNT FITTING. CORRODED. FOUND CRACK INDICATION ON NR 1 ENG UPPER MOUNT FITTING ON LT WING FWD SPAR NEAR GROUNDING LUG. FURTHER INSPECTION FOUND TO BE LEVEL 2 CORROSION. PART TO BE REPL - [SDR 39LA2014082798](https://openairdocs.org/sdr/39LA2014082798), Aug 27, 2014: SKIN. CRACKED. CRACK FOUND AT STATION 3950 LT SIDE OF FUSELAGE. LOCALLY MANUFACTURED FILLER USING .032 X 2024-T3 & DOUBLER USING .040 X 2024-T3. ALL WORK DONE FOLLOWING DWG 14 - [SDR 39LA2014082797](https://openairdocs.org/sdr/39LA2014082797), Aug 27, 2014: SKIN. CRACKED. CRACK FOUND AT STATION 3950 RT SIDE OF FUSELAGE. LOCALLY MANUFACTURED FILLER USING .032 X 2024-T3 & DOUBLER USING .040 X 2024-T3. ALL WORK DONE FOLLOWING DWG 14 - [SDR 39LA2014082696](https://openairdocs.org/sdr/39LA2014082696), Aug 26, 2014: RIB. CORRODED. TOP INNER RIB OF LT HORIZONTAL STABILIZER AT INBD ATTACH FITTING FOUND CORRODED BEYOND LIMITS. REPLACED INNER RIB AS REQUIRED. - [SDR 39LA2014082695](https://openairdocs.org/sdr/39LA2014082695), Aug 26, 2014: SKIN. CORRODED. RIGHT WING LOWER SURFACE IN AREA OF ENG EXHAUST TRAIL HAS CORROSION DAMAGE FROM ENG EXHAUST PRODUCT. MILITARY TECHNICAL INSTRUCTION 17 TO BE PERFORMED REPAIR OF - [SDR 39LA2014082694](https://openairdocs.org/sdr/39LA2014082694), Aug 26, 2014: SKIN. CORRODED. LEFT WING LOWER SURFACE IN AREA OF ENG EXHAUST TRAIL HAS CORROSION DAMAGE FROM ENG EXHAUST PRODUCT. MILITARY TECHNICAL INSTRUCTION 17 TO BE PERFORMED, REPAIR OF - [SDR 39LA2014082693](https://openairdocs.org/sdr/39LA2014082693), Aug 26, 2014: CHANNEL. CORRODED. RIGHT SEAT TRACK HAT CHANNEL SUPPORT & SEAT TRACK FROM FS 2400 TO 3950 FOUND CORRODED BEYOND LIMITS & IN NEED OF REPLACEMENT. - [SDR 39LA2014082692](https://openairdocs.org/sdr/39LA2014082692), Aug 26, 2014: CHANNEL. CORRODED. LEFT SEAT TRACK SUPPORT HAT CHANNEL & SEAT TRACK FROM FS 3150 TO 3950 FOUND CORRODED BEYOND LIMITS & IN NEED OF REPLACEMENT. - [SDR 39LA2014082691](https://openairdocs.org/sdr/39LA2014082691), Aug 26, 2014: SKIN. DENTED. DURING INSPECTION FOUND RT HORIZONTAL STABILIZER UPPER OTBD SKIN TO HAVE A DENT BEYOND LIMITS. FABRICATED SECTION OF SKIN USING ORIGINAL SKIN AS SAMPLE. MATERIA - [SDR 39LA2014082690](https://openairdocs.org/sdr/39LA2014082690), Aug 26, 2014: MOUNT BRACKET. CORRODED. DURING REMOVAL OF HORIZONTAL STABILIZER FOUND LT LOWER MOUNT BAR CORRODED. LOCALLY MANUFACTURED IAW EO 14019-2028 REV 1R. NO FURTHER ACTION REQUIRED AT THIS TIM - [SDR 39LA2014082689](https://openairdocs.org/sdr/39LA2014082689), Aug 26, 2014: MOUNT BRACKET. CORRODED. DURING REMOVAL OF HORIZONTAL STABILIZER FOUND LT UPPER MOUNT BAR CORRODED. LOCALLY MANUFACTURED IAW EO 14019-2027 REV 1R. NO FURTHER ACTION REQUIRED AT THIS TIM - [SDR 39LA2014082087](https://openairdocs.org/sdr/39LA2014082087), Aug 20, 2014: WINDOW FRAME. CORRODED. DURING WINDSHIELD REMOVAL AT HEAVY CHECK CORROSION FOUND ON THE COPILOT'S WINDSHIELD FRAME INBD VERTICAL SECTION. REPAIRED IAW EO 12032-2036 SUPPORTED BY FAA FO - [SDR 39LA2014082086](https://openairdocs.org/sdr/39LA2014082086), Aug 20, 2014: WINDOW FRAME. CORRODED. DURING WINDSHIELD REMOVAL AT HEAVY CHECK CORROSION FOUND ON THE COPILOT'S WINDSHIELD FRAME INBD VERTICAL SECTION. REPAIRED IAW EO 12032-2036 SUPPORTED BY FAA FO - [SDR 39LA2014082085](https://openairdocs.org/sdr/39LA2014082085), Aug 20, 2014: WINDOW FRAME. CORRODED. DURING WINDSHIELD REMOVAL AT HEAVY CHECK CORROSION FOUND ON THE COPILOT'S WINDSHIELD FRAME LOWER SECTION. REPAIRED IAW EO 12032-2036 SUPPORTED BY FAA FORM 8110- - [SDR 39LA2014082084](https://openairdocs.org/sdr/39LA2014082084), Aug 20, 2014: WINDOW FRAME. CORRODED. DURING WINDSHIELD REMOVAL AT HEAVY CHECK CORROSION FOUND ON THE COPILOT’S WINDSHIELD FRAME LOWER SECTION. REPAIRED IAW EO 12032-2036 SUPPORTED BY FAA FORM 8110- - [SDR 8EKA20140801](https://openairdocs.org/sdr/8EKA20140801), Feb 13, 2014: PANEL. CORRODED. DURING INSPECTION FOUND CORROSION IN AFT CARGO DOOR. REMOVED CORROSION DAMAGED PANELS. FABRICATED & INSTALLED TWO REPAIR PANELS. ALL REPAIRS PERFORMED IAW SRM. - [SDR 8EKA201402060002](https://openairdocs.org/sdr/8EKA201402060002), Jan 30, 2014: PROFILE. CRACKED. DURING 1200 HR FALSE SPAR RECURRING AD INSPECTION, IAW AD 98-12-28. FOUND CRACKS IN THE PROFILE OF FALSE SPAR LOCATED IN THE LT WING. REMOVED LT WING AUXILIARY - [SDR 8EKA2014020600001](https://openairdocs.org/sdr/8EKA2014020600001), Jan 30, 2014: PROFILE. CRACKED. DURING 1200 HR FALSE SPAR RECURRING INSPECTION, & AD INSPECTION AD 98-12-28. FOUND CRACKS IN THE PROFILE OF FALSE SPAR LOCATED IN THE RT WING. REMOVED RT WING A - [SDR 39LA2013122642](https://openairdocs.org/sdr/39LA2013122642), Dec 26, 2013: SKIN. CORRODED. DURING CPCP INSPECTION, FOUND CORROSION ON LT WING TE AT CTR OF INBD FLAP, BETWEEN WING STATION 1266 & 2620. - [SDR 39LA2013121941](https://openairdocs.org/sdr/39LA2013121941), Dec 19, 2013: RIB. DAMAGED. RIGHT HAND OTBD WING RIB AT WS 9500 FOUND DAMAGED WITH MULTIPLE CRACKS & DENTED FORMERS. R & R RT HAND WING RIB IAW EO2013047-311 PARA 8.42 REV B. - [SDR 39LA2013121940](https://openairdocs.org/sdr/39LA2013121940), Dec 19, 2013: SKIN. CORRODED. RIGHT WING EXHAUST TRAIL SKIN SHOWS SIGNS OF HEAT EROSION & CORROSION. REPLACED RT WING EXHAUST TRAIL SKIN IAW EO 2013047-311 PARA 8.22 REV B. - [SDR 39LA2013121939](https://openairdocs.org/sdr/39LA2013121939), Dec 19, 2013: CHANNEL. CORRODED. LEFT WING INBD FLAP TRACK U CHANNEL SHOWS SIGNS OF HEAT EROSION & CORROSION. REPLACED LT WING INBD FLAP TRACK U CHANNEL IAW EO 20130417-311 PARA 8.25 & PARA 8.3 - [SDR 39LA2013121938](https://openairdocs.org/sdr/39LA2013121938), Dec 19, 2013: SKIN. CORRODED. LEFT WING EXHAUST TRAIL SKIN SHOWS SIGNS OF HEAT EROSION & CORROSION. REPLACED LT WING EXHAUST TRAIL SKIN IAW EO 2013047-311 PARA 8.21 REV B. - [SDR 39LA2013121937](https://openairdocs.org/sdr/39LA2013121937), Dec 19, 2013: CHANNEL. CORRODED. LEFT WING INBD FLAP TRACK U CHANNEL SHOWS SIGNS OF HEAT EROSION & CORROSION. REPLACED LT WING INBD FLAP TRACK U CHANNEL IAW EO 20130417-311 PARA 8.25 & PARA 8.3 - [SDR 39LA2013121936](https://openairdocs.org/sdr/39LA2013121936), Dec 19, 2013: SKIN. DENTED. LEFT WING LOWER SKIN DENTED OTBD OF EXISTING REPAIR. R & R REPAIR IAW EO 2013047-311 PARA 8 40 REV B. - [SDR 39LA2013121935](https://openairdocs.org/sdr/39LA2013121935), Dec 19, 2013: SUPPORT CHANNEL. CORRODED. RIGHT SEAT TRACK SUPPORT CHANNEL BETWEEN FS 2400 & FS 2960 HAS HEAVY CORROSION AROUND ATTACHMENTS. REPLACED SEAT TRACK SUPPORT CHANNEL BETWEEN FS 2400 & 2960 IA - [SDR 39LA2013121934](https://openairdocs.org/sdr/39LA2013121934), Dec 19, 2013: SKIN. DENTED. DENT ON LOWER SKIN OF LT HORIZONTAL STABILIZER STATION HSS3620. REPAIRED DAMAGED AREA ON LOWER SKIN OF LT HORIZONTAL STABILIZER BY INSTALLING A DOUBLER STATION - [SDR 39LA2013121933](https://openairdocs.org/sdr/39LA2013121933), Dec 19, 2013: SKIN. DENTED. LEFT SIDE FUSELAGE SKIN HAS A DENT BETWEEN FS 3950 - 4310, BELOW STRINGER 18L. R & R SKIN AT FS 3550 & FS 3950 BELOW STRINGER 18L IAW EO 2013047-311 PARA 8 19 R - [SDR 39LA2013121932](https://openairdocs.org/sdr/39LA2013121932), Dec 19, 2013: SKIN. DENTED. RIGHT SIDE FUSELAGE SKIN DENTED SEVERAL PLACES BETWEEN FS 3550 - 3950 ABOVE & BELOW STRINGER 7R. R & R RT SIDE FUSELAGE SKIN AT FS 3550 - 3950 ABOVE & BELOW STR - [SDR 39LA2013121931](https://openairdocs.org/sdr/39LA2013121931), Dec 19, 2013: SKIN. DENTED. MULTIPLE DENTS IN FUSELAGE CTR BELLY SKIN AROUND FS 4670. FABRICATED REPAIR DOUBLER & INSTALLED IAW CASA 212-300SRM APPENDIX II, FIG B7 & EO 2013047-311 PARA 8 - [SDR 39LA2013121930](https://openairdocs.org/sdr/39LA2013121930), Dec 19, 2013: FRAME. CRACKED. FRAME 27F, STATION 12615 BETWEEN STRINGER 1L & 1R IS CRACKED IN RADIUS BEYOND LIMITS. REPLACED FRAME 27F AT STATION 12615 IAW AIRLIFT EO 2013047-311 PARA 8 41 R - [SDR 39LA201310100001](https://openairdocs.org/sdr/39LA201310100001), Oct 10, 2013: LIGHT. FAILED. DETECTED FUMES IN COCKPIT DURING FLIGHT. FOUND LT TAXI-LANDING LIGHT CIRCUIT BREAKER TRIPPED. GAINED ACCESS TO LT LANDING LIGHT, FOUND ODOR EMINATING FROM LIGHT - [SDR EHAA20130412004](https://openairdocs.org/sdr/EHAA20130412004), Apr 12, 2013: TERMINAL BLOCK. BURNED. DURING FLIGHT LT WINDOW HEAT SHORTED. - [SDR SROM2011011](https://openairdocs.org/sdr/SROM2011011), Sep 25, 2011: WIRE HARNESS. CHAFED. MULTIPLE CIRCUIT BREAKERS ON OVERHEAD PANEL POPPED IN FLIGHT. FLIGHT CREW CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. BREAKERS THAT TRIPPED INSTRUMENT ## STCs that may be installed (OpenAirDocs) (40) 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 ST01305WI-D](https://openairdocs.org/stc/ST01305WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision. Rockwell Collins Inc - [STC ST04105NY](https://openairdocs.org/stc/ST04105NY): Installation of Flight Data Recorder, Flight Data Acquisition Unit, Traffic Advisory Altering System and Navigation Suite. CASA Flight Tech LLC - [STC ST04109NY](https://openairdocs.org/stc/ST04109NY): Update of COMBI. CASA Flight Tech LLC - [STC ST02257AK](https://openairdocs.org/stc/ST02257AK): Modify the aircraft configuration from 23 passenger seats to a combined cargo and passenger configuration. CASA Flight Tech LLC - [STC ST02046AK](https://openairdocs.org/stc/ST02046AK): nstallation of Allied Signal (Sundstrand) Mark VI Ground Proximity Warning System. Erickson Incorporated - [STC ST02047AK](https://openairdocs.org/stc/ST02047AK): Installation of Trimble TNL 2101 I/O global positioning system. Erickson Incorporated - [STC ST02048AK](https://openairdocs.org/stc/ST02048AK): Installation of Trimble TNL 2100T global positioning system. Erickson Incorporated - [STC ST02414AK](https://openairdocs.org/stc/ST02414AK): Reduction/limitation of passenger seats to 19 or fewer. Erickson Incorporated - [STC ST00065MC](https://openairdocs.org/stc/ST00065MC): Installation of a Ballistic Protection System (BPS). Erickson Incorporated - [STC ST03558AT](https://openairdocs.org/stc/ST03558AT): Installation of a Collins TCAS-4000 (TCAS II) System (Version 7.0) with dual Collins TVI-920D VSI/TA/RA Indicators and associated hardware. Woven Electronics, LLC - [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc - [STC ST02548AK](https://openairdocs.org/stc/ST02548AK): Installation of Main Gear Gravel Deflectors. Aero Twin Inc - [STC ST04200NY](https://openairdocs.org/stc/ST04200NY): Installation of 19 Martin Baker Aircraft Company Inc. Seat. Carson Helicopters Inc - [STC ST02540AK](https://openairdocs.org/stc/ST02540AK): Fabrication and installation of Aero Twin, Inc., Rudder Gust Lock Kit No. 4111-212. Aero Twin Inc - [STC ST02433LA](https://openairdocs.org/stc/ST02433LA): Installation of LifePort Triple Litter Stacking System (TLSS). LifePort LLC - [STC ST02099SE](https://openairdocs.org/stc/ST02099SE): Installation of a Supplemental Lighting System; manufactured and installed. Aviation Specialties Unlimited Inc - [STC ST03993AT](https://openairdocs.org/stc/ST03993AT): Installation of a Universal Avionics EFI-890R Electronic Flight Instruments System (EFIS). Air Data Consulting Group, Inc - [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS - [STC ST04157AT](https://openairdocs.org/stc/ST04157AT): Installation of Concorde lead acid batteries to replace nickel-cadmium (NiCd) batteries along with associated hardware. AAR Airlift Group - [STC ST04178AT](https://openairdocs.org/stc/ST04178AT): Replace original equipment Nickel-Cadmium (NiCd) main and auxiliary batteries with Concorde Lead-Acid, main and auxiliary batteries along with associated hardware. Concorde Battery Corporation - [STC ST02401AK](https://openairdocs.org/stc/ST02401AK): Installation of a Nose Gear Gravel Deflector. Aero Twin Inc - [STC ST00673WI-D](https://openairdocs.org/stc/ST00673WI-D): Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System installation. Rockwell Collins Inc - [STC ST02559AK](https://openairdocs.org/stc/ST02559AK): Installation of Aero Twin, Inc. CASA 212 Exhaust Deflector, part number AT-CASA-EXDF-1001. Aero Twin Inc - [STC SA1315SO](https://openairdocs.org/stc/SA1315SO): Installation of refreshment center. Aeronautical Engineers, Inc. Lists C-212 Series - [STC ST00335NY](https://openairdocs.org/stc/ST00335NY): Remove existing starter-generator and install Aircraft Parts Corporation (APC) starter generator P/N. Shurka Aerospace Inc - [STC ST02346AK](https://openairdocs.org/stc/ST02346AK): Restricted category installation of a Forward Looking Infrared (FLIR) system. ConocoPhillips Company - [STC ST01142WI-D](https://openairdocs.org/stc/ST01142WI-D): Modification of a single or dual Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92 control head to a Flight ID capable Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92E control head. Rockwell Collins Inc - [STC ST03305AT](https://openairdocs.org/stc/ST03305AT): Installation of a SINGLE Class-A Sandel ST3400 Terrain Awareness Warning System (TAWS), pilot and co-pilot annunciator panels, and Air Data Computer (ADC) . Presidential Airways Inc - [STC ST01394WI-D](https://openairdocs.org/stc/ST01394WI-D): Modification of a Collins CTL-23 or CTL-23C VHF COMM/NAV Control Panel System installation. Rockwell Collins Inc - [STC ST01398NY](https://openairdocs.org/stc/ST01398NY): Installation of Universal Avionics Systems Corporation CVR-120 cockpit voice recorder (CVR). Approved for serial number 405 ONLY. Sierra Nevada Corporation/Integrated Mission Systems - [STC ST01307WI-D](https://openairdocs.org/stc/ST01307WI-D): Modification of a Collins TVI-920/TVI-920D Vertical Speed/TCAS Indicator installation. Rockwell Collins Inc - [STC ST10215SC](https://openairdocs.org/stc/ST10215SC): Installation of Honeywell Mark VI Enhanced Ground Proximity Warning System (EGPWS) equipped with a HOneywell KMD 850 Multi-Function Display (MFD). Bighorn Airways Inc - [STC SA5603NM-D](https://openairdocs.org/stc/SA5603NM-D): Installation of a Fairchild A100/A100A cockpit voice recorder. Learjet Inc - [STC SA01900AT](https://openairdocs.org/stc/SA01900AT): Installation of a 9 seat passenger configuration. Gryphon Group International, Inc. Lists C-212 Series - [STC ST00608NY-D](https://openairdocs.org/stc/ST00608NY-D): Installation of cargo smoke detector system. CASA Aircraft USA, Inc - [STC ST00615NY-D](https://openairdocs.org/stc/ST00615NY-D): Installation of Cargo Interior. CASA Aircraft USA, Inc - [STC SA971NE](https://openairdocs.org/stc/SA971NE): Installation of a single trimble TNL-3000 GPS/LORAN navigationsystem. Summit Aviation, Inc. Lists C-212 Series - [STC SA3903NM](https://openairdocs.org/stc/SA3903NM): Installation of pedestal covers. American Casa Distributor Inc - [STC SA2135NM](https://openairdocs.org/stc/SA2135NM): Class B aft baggage compartment -9G bulkhead, coat closet, baggage storage and refreshment service unit. Flight Structures Inc. Lists C-212 Series - [STC SA2570CE](https://openairdocs.org/stc/SA2570CE): Replace the original generator control units with Phoenix Aerospace, Inc., Model GC-1010-24-3B solid state generator control units. Phoenix Aerospace Inc. Lists C-212 Series ## PMA parts (OpenAirDocs) (218, 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. - [LSM-500-122](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195333909020260909145848.0001): Parmetheus Pro Instl. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 22, 2026 - [LSM-500-116](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182431779620260909145847.0001): Boom Beam Instl, Casa. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 22, 2026 - [M23065-1470](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174779225620241113171048.0001): Fan Cover. Miraj Corporation · PMA PQ0870NE · Replaces 23065-1470 · Nov 8, 2024 - [M06-201100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195622496020241022163146.0001): Label. Miraj Corporation · PMA PQ0870NE · Replaces Safran 06-201100 · Oct 10, 2024 - [M06-200001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140100423620240223153731.0001): Label. Miraj Corporation · PMA PQ0870NE · Replaces Safran 06-200001 · Feb 15, 2024 - [394390-1-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194442988120231221185038.0001): Flow Divider Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 394390-1-1 · Apr 13, 2023 - [394230-4-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172944965920231221185038.0001): Fuel Solenoid. Honeywell International Inc. · PMA PQ1222NM · Replaces 394230-4-1 · Apr 13, 2023 - [978944-1-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161625104920231221185038.0001): Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 978944-1-1 · Apr 13, 2023 - [394408-10-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157199329620231221185038.0001): Flow Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 394408-10-1 · Apr 13, 2023 - [319980-6-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139156544320231221185037.0001): Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 319980-6-1 · Apr 13, 2023 - [394396-1-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134852963620231221185038.0001): Flow Divider Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 394396-1-1 · Apr 13, 2023 - [129580-7](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124582931120231221185037.0001): Duct Temperature Limiter. Honeywell International Inc. · PMA PQ1222NM · Replaces 129580-7 · Apr 13, 2023 - [C212-TCAS-900](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168728984620230504173355.0001): TCAS 4000 INSTALLATION TOP KIT. Woven Electronics, LLC · PMA PQ00009EB · Replaces C212-TCAS-900 · Dec 1, 2022 - [MG94A-902-1M](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137070962420220916174319.0001): Brush, Electrical Contact. Miraj Corporation · PMA PQ0870NE · Replaces 23093-1305 · Aug 29, 2022 - [M23088-1348](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152168509320220808113437.0001): Brush, Electrical Contact. Miraj Corporation · PMA PQ0870NE · Replaces 300SGL1009-5 · Jul 18, 2022 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137843162120220809130823.0001): Aviation Devices & Electronic Components LLC (Av-DEC) · PMA PQ3846SW · May 10, 2022 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183136835520220809102459.0001): Aviation Devices & Electronic Components LLC (Av-DEC) · PMA PQ3846SW · Apr 18, 2022 - [AG844000-15](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155429232820220408135717.0001): Gasket – UHF/VHF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Feb 8, 2022 - [AG728000-52](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102545922820220408135653.0001): Gasket – Satcom Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Jan 26, 2022 - [111608-1MIT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID910291084820220208124954.0001): Pin. Mitchell PMA, LLC · PMA PQ04379CE · Replaces 111608-1 · Jan 13, 2022 - [AG627000-23](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141640838920220408135615.0001): Gasket, Marker Beacon. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Dec 15, 2021 - [AG358000-08](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157368644820220408135729.0001): Gasket – ELT Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 17, 2021 - [AG627000-12](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111242205720220408140205.0001): Gasket – Marker Beacon Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 17, 2021 - [255001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187682453520220517141829.0001): CVR-120 Installation. Sierra Nevada Corp (HGR) · PMA PQ2041NE · Modification part · Oct 28, 2021 - [AG843000-17](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID936553775020211110110424.0001): Gasket-UHF/VHF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Aug 9, 2021 - [212-201-05-COV](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID876796333120210608151243.0001): 2.00 CHANNEL ASSEMBLY COVER. Carson Helicopters, Inc. · PMA PQ4181NE · Modification part · May 26, 2021 - [MGDC-212](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166914142420210617193111.0001): Main Gear Gravel Deflector Kit. Aero Twin Inc · PMA PQ2503CE · Modification part · Apr 19, 2021 - [AG358000-07](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID572734396202107271951110.0001): Gasket – ELT Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Dec 11, 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 - [4111-212](https://drs.faa.gov/browse/excelExternalWindow/94038EDF0BB9A08A862586260044AD64.0001): Rudder Gust Lock Kit. Aero Twin Inc · PMA PQ2503CE · Modification part · Nov 8, 2020 - [NOHIPOT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170926927620240320173409.0001): Decal. Augusta Aero Innovations LLC · PMA PQ04441CE · Replaces 150SG1139 · Oct 6, 2020 - [NOHIPOT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID150260847520240320173402.0001): Decal. Augusta Aero Innovations LLC · PMA PQ04441CE · Replaces 06-201020 · Oct 6, 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 - [AG822000-03](https://drs.faa.gov/browse/excelExternalWindow/25D416C8B528F4988625859F003C440E.0001): Gasket - TCAS Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · May 31, 2020 - [AG843000-17](https://drs.faa.gov/browse/excelExternalWindow/44F91AF19B0D8D4586258591003A1785.0001): Gasket - UHF/VHF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Jan 1, 2020 - [M30059-1471](https://drs.faa.gov/browse/excelExternalWindow/033AA67180F15A638625856500537B25.0001): Dampener Plate. Miraj Corporation · PMA PQ0870NE · Replaces 30059-1471 · Sep 15, 2019 - [AF212-42001-06-3](https://drs.faa.gov/browse/excelExternalWindow/CE9EC9CFF64E4C1D86258560005A3561.0001): Nose Gear Bolt. Airforms LLC · PMA PQ2644CE · Replaces 212-42001-06-3 · Sep 2, 2019 - [AF212-42001-06-3](https://drs.faa.gov/browse/excelExternalWindow/69931032BCDF63AD86258560005A34F0.0001): Nose Gear Bolt. Airforms LLC · PMA PQ2644CE · Replaces 212-42001-06-1 · Sep 2, 2019 - [AG843000-15](https://drs.faa.gov/browse/excelExternalWindow/445335953945E98886258560003BF2F7.0001): Gasket - VHF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Aug 18, 2019 - [MDL-874-00](https://drs.faa.gov/browse/excelExternalWindow/7D3BB80911BFD485862585690051D34D.0001): Medical Litter System. LifePort, LLC. · PMA PQ0172NM · Modification part · Jul 31, 2019 - [AG728000-18](https://drs.faa.gov/browse/excelExternalWindow/F4DA194164F2F4E686258553004D529A.0001): Gasket - Satcom Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Jun 25, 2019 - [AG247000-04](https://drs.faa.gov/browse/excelExternalWindow/F4D9B388DAECF53586258553004D4A85.0001): Gasket - L-Band Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Jun 25, 2019 - [AG728000-46](https://drs.faa.gov/browse/excelExternalWindow/9AF760F4D66B4F5E86258553004D52E5.0001): Gasket - Satcom Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Jun 25, 2019 - [AG822000-08](https://drs.faa.gov/browse/excelExternalWindow/CB9177DCB006663B862585520042A887.0001): Gasket - TCAS Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Jun 9, 2019 - [AG723000-27](https://drs.faa.gov/browse/excelExternalWindow/0740FB46C2B93B86862585520042A854.0001): Gasket - Radio Altimeter Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Jun 9, 2019 - [MCG-1900](https://drs.faa.gov/browse/excelExternalWindow/C5FE45C228B3339F86258474006122F8.0001): Dampener Hub. Miraj Corporation · PMA PQ0870NE · Replaces 23032-1900 · Feb 24, 2019 - [87-05546-001](https://drs.faa.gov/browse/excelExternalWindow/466DF7E01FA1E8D486258355004A64EA.0001): Light, Landing, PAR 64. Astronics Luminescent Systems Inc · PMA PQ0786NE · Replaces 4559 Q4559 Q4559X TAE0728-1 · Sep 18, 2018 - [2368-503](https://drs.faa.gov/browse/excelExternalWindow/F5EFE87BCCDD317D862582CF006DAD76.0001): Outlet, Air Valve, Individual, Air Cond.. B/E Aerospace, Inc, Business Jet Group, Aerospace Lighting Corporation · PMA PQ0837NE · Replaces AC 720220 · Jun 17, 2018 - [2394 P](https://drs.faa.gov/browse/excelExternalWindow/A1E04C01CA9A7D50862582CF006DAE61.0001): Valve Assy. B/E Aerospace, Inc, Business Jet Group, Aerospace Lighting Corporation · PMA PQ0837NE · Replaces AC 720198 · Jun 17, 2018 All of them: https://openairdocs.org/model/c-a-s-a-c-212-df/pma.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.