# Fairchild SA227-CC - Type: Aircraft model (FAA registry) - Registry code: 3377522 - Manufacturer (registry): FAIRCHILD - Model: SA227-CC - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-prop - Seats: 21 - Weight class: 12,500 to 19,999 lb - Certification: Type certificated - Data sheet: [TCDS A18SW](https://openairdocs.org/tcds/A18SW) (OpenAirDocs) - Holder: Ontic Engineering and Manufacturing Inc. - Registered aircraft: 0 - Page: https://openairdocs.org/model/fairchild-sa227-cc 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 2017-07-01](https://openairdocs.org/ad/2017-07-01): Propellers/Propulsors · M7 Aerospace SA226-AT, SA226-T, SA226-T(B) and 7 more. Effective May 5, 2017 - [AD 2016-25-12](https://openairdocs.org/ad/2016-25-12): Horizontal Stabilizer Structure · M7 Aerospace SA226-AT, SA226-T, SA226-T(B) and 7 more. Effective Jan 12, 2017 - [AD 2016-15-02](https://openairdocs.org/ad/2016-15-02): Flight Controls · M7 Aerospace SA226-AT, SA226-T, SA226-T(B) and 9 more. Effective Aug 26, 2016 - [AD 2016-10-01](https://openairdocs.org/ad/2016-10-01): Elevator Control System · M7 Aerospace SA226-AT, SA226-T, SA226-T(B) and 7 more. Effective Jun 15, 2016 - [AD 2015-19-10](https://openairdocs.org/ad/2015-19-10): Flight Controls · M7 Aerospace SA226-AT, SA226-T, SA226-T(B) and 9 more. Effective Nov 3, 2015 - [AD 2014-15-01](https://openairdocs.org/ad/2014-15-01): Fuselage Main, Structure · M7 Aerospace SA227-AC (C-26A), SA227-AT, SA227-BC (C-26A) and 2 more. Effective Aug 27, 2014 - [AD 2014-09-02](https://openairdocs.org/ad/2014-09-02): Flight Controls · M7 Aerospace SA226-AT, SA226-T, SA226-T(B) and 9 more. Effective Jun 5, 2014 - [AD 2014-06-01](https://openairdocs.org/ad/2014-06-01): Fuselage Main, Bulkhead · M7 Aerospace SA226-AT, SA226-T, SA226-T(B) and 9 more. Effective Apr 25, 2014 - [AD 2012-18-01](https://openairdocs.org/ad/2012-18-01): Wing, Fuselage Attach Fitting · M7 Aerospace SA226-AT, SA226-T, SA226-T(B) and 7 more. Effective Sep 21, 2012 - [AD 2011-02-04](https://openairdocs.org/ad/2011-02-04): Flight Compartment Windows · M7 Aerospace SA226-AT, SA226-T, SA226-T(B) and 9 more. Effective Jan 24, 2011 - [AD 2009-11-06](https://openairdocs.org/ad/2009-11-06): Hydraulic tube assemblies · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 5 more. Effective Jul 2, 2009 - [AD 2007-16-03](https://openairdocs.org/ad/2007-16-03): Pitch trim actuators · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 8 more. Effective Sep 7, 2007 - [AD 2005-06-13](https://openairdocs.org/ad/2005-06-13): Wing spar center web cutout · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 7 more. Effective May 2, 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 2003-19-10](https://openairdocs.org/ad/2003-19-10): Fuel boost pump · M7 Aerospace SA226-AT, SA226-T, SA226-T(B) and 8 more. Effective Nov 7, 2003 - [AD 2000-06-04](https://openairdocs.org/ad/2000-06-04): Pneumatic Deicing Boots · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 8 more. Effective May 5, 2000 - [AD 98-08-20](https://openairdocs.org/ad/98-08-20): Autopilot Servo Actuators · Alliedsignal Avionics Autopilot Servo Actuators, Mystere-Falcon 20 - C5, Mystere-Falcon 20 - D5 and 17 more. Effective Jun 2, 1998 - [AD 97-01-12](https://openairdocs.org/ad/97-01-12): Ground Proximity Warning System · Airtell International Ground Proximity Warning System, Mystere-Falcon 200, EMB-110P1 and 20 more. Effective Feb 25, 1997 - [AD 96-19-05](https://openairdocs.org/ad/96-19-05): Main Landing Gear or Nose Landing Gear Assemblies or Yokes · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 7 more. Effective Oct 1, 1996 - [AD 96-09-16](https://openairdocs.org/ad/96-09-16): Airplane Flight Manual (AFM) - Icing · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 7 more. Effective Jun 11, 1996 - [AD 95-17-09 R1](https://openairdocs.org/ad/95-17-09-R1): Essential Bus Current Limiters · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 7 more. Effective May 13, 1996 - [AD 94-07-10 R1](https://openairdocs.org/ad/94-07-10-R1): Upper Wing Skin Inspection · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 7 more. Effective Mar 25, 1996 - [AD 96-03-03](https://openairdocs.org/ad/96-03-03): Power Control Cable Safety Wire Nuts · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 7 more. Effective Mar 15, 1996 - [AD 95-24-11](https://openairdocs.org/ad/95-24-11): Foreign Object Damage Barriers In Floorboards · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 7 more. Effective Jan 3, 1996 - [AD 90-24-03](https://openairdocs.org/ad/90-24-03): Rudder Trim Link Assemblies · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 10 more. Effective Jan 25, 1991 Historical (superseded or no longer in force): - [AD 2008-12-16](https://openairdocs.org/ad/2008-12-16) (historical): Left-hand (LH) and right-hand (RH) inboard wing leading edge/battery box areas · M7 Aerospace LP SA226-AT, SA226-T, SA226-TC and 4 more. Effective Jul 23, 2008 - [AD 2000-03-17](https://openairdocs.org/ad/2000-03-17) (historical): Pitch Trim Actuator · M7 Aerospace LP SA226-AT, SA226-T, SA226-TC and 8 more. Effective Apr 10, 2000 - [AD 98-19-15 R1](https://openairdocs.org/ad/98-19-15-R1) (historical): Pitch Trim Actuator · M7 Aerospace LP SA226-AT, SA226-T, SA226-TC and 7 more. Effective Mar 3, 2000 - [AD 99-06-02](https://openairdocs.org/ad/99-06-02) (historical): Wing Spar Center Web · M7 Aerospace LP SA226-AT, SA226-T, SA226-TC and 7 more. Effective Apr 16, 1999 - [AD 98-19-15](https://openairdocs.org/ad/98-19-15) (historical): Pitch Trim Actuator · M7 Aerospace LP SA226-AT, SA226-T, SA226-TC and 7 more. Effective Sep 25, 1998 - [AD 97-23-01](https://openairdocs.org/ad/97-23-01) (historical): Pitch Trim Actuator · M7 Aerospace LP SA226-AT, SA226-T, SA226-TC and 8 more. Effective Dec 1, 1997 - [AD 97-02-02](https://openairdocs.org/ad/97-02-02) (historical): Control Column Pitch Bearing Attaching Nuts · M7 Aerospace SA226-AT, SA226-T, SA226-TC and 9 more. Effective Feb 6, 1997 - [AD 93-15-02 R2](https://openairdocs.org/ad/93-15-02-R2) (historical): Pitch Trim Actuator · M7 Aerospace LP SA226-AT, SA226-T, SA226-TC and 8 more. Effective Jul 25, 1996 - [AD 94-07-10](https://openairdocs.org/ad/94-07-10) (historical): Upper Wing Skin Inspection · M7 Aerospace LP SA226-AT, SA226-T, SA226-TC and 7 more. Effective May 27, 1994 - [AD 86-25-04](https://openairdocs.org/ad/86-25-04) (historical): POH/AFM Appendix - Icing · M7 Aerospace LP SA227-AC (C-26A), SA227-AT, SA227-BC (C-26A) and 4 more. Effective Dec 15, 1986 ## Information bulletins (advisory) (15) - [SAIB 2026-15](https://openairdocs.org/saib/2026-15): Forward Pressure Bulkhead. Issued Sep 9, 2026 - [SAIB 2026-14](https://openairdocs.org/saib/2026-14): Rudder Control System, Brake. Issued Aug 25, 2026 - [SAIB CE-20-09](https://openairdocs.org/saib/CE-20-09): Nacelle/Pylon, Frame/Spar/Rib. Issued May 13, 2020 - [SAIB CE-18-11](https://openairdocs.org/saib/CE-18-11): Flight Controls, Elevator Control System. Issued Feb 9, 2018 - [SAIB CE-17-04](https://openairdocs.org/saib/CE-17-04): Landing Gear, Main Landing Gear. Issued Dec 16, 2016 - [SAIB CE-16-06](https://openairdocs.org/saib/CE-16-06): Flight Controls, Rudder Control System. Issued Nov 20, 2015 - [SAIB CE-16-04](https://openairdocs.org/saib/CE-16-04): Engine Controls, Power Lever. Issued Nov 2, 2015 - [SAIB CE-15-09](https://openairdocs.org/saib/CE-15-09): Windows; Flight Compartment Windows. Issued Feb 24, 2015 - [SAIB CE-15-05R1](https://openairdocs.org/saib/CE-15-05R1): Flight Controls, Aileron Control System. Issued Nov 26, 2014 - [SAIB CE-15-05](https://openairdocs.org/saib/CE-15-05) (historical): Flight Controls, Aileron Control System. Issued Nov 25, 2014 - [SAIB CE-13-42](https://openairdocs.org/saib/CE-13-42): Wings, Ailerons. Issued Aug 1, 2013 - [SAIB CE-13-41](https://openairdocs.org/saib/CE-13-41): Landing Gear, Landing Gear Actuator. Issued Jul 23, 2013 - [SAIB CE-13-10](https://openairdocs.org/saib/CE-13-10): Windshield/Door Rain/Ice Removal. Issued Dec 21, 2012 - [SAIB CE-12-08](https://openairdocs.org/saib/CE-12-08): Flight Controls, Elevator Control System. Issued Nov 8, 2011 - [SAIB CE-11-26](https://openairdocs.org/saib/CE-11-26): Wings: Wing Skin. Issued Mar 30, 2011 ## Registered aircraft None registered with this model now. ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (84, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR KY7A2025093000038](https://openairdocs.org/sdr/KY7A2025093000038), Sep 17, 2025: BRAKE. WEAK. LEFT BRAKE SPONGEY, WILL GO ALL THE WAY TO THE FLOOR. BLED & SERVICED BRAKE SYSTEM IAW SA277 MM CH 32-41-00. RTS CHECKS COMPLETED - [SDR JIKA2022062301](https://openairdocs.org/sdr/JIKA2022062301), Jun 23, 2022: INDICATOR. INOPERATIVE. DURING APPROACH TO KCHS, GEAR SELECTED TO DOWN POSITION, LH MLG DOWN LOCK - GREEN LIGHT - DID NOT ILLUMINATE, GEAR WAS MANUALLY EXTENDED AND EMERGENCY WAS DECLA - [SDR JIKA2022033101](https://openairdocs.org/sdr/JIKA2022033101), Mar 31, 2022: CONTROLLER. BROKEN. AMF 1088 - DURING FLIGHT, JUST BEFORE LANDING, PILOT NOTED SMOKE IN THE COCKPIT. THE CONTROL AIR FAN SOUNDED LIKE IT WAS FULL OF MARBLES THEN IT STOPPED AND THE - [SDR JIKA2022020301](https://openairdocs.org/sdr/JIKA2022020301), Feb 3, 2022: NOT REPORTED. NOT REPORTED. LH MLG DID NOT COME DOWN ON APPROACH, RED INTRANSIT LIGHT REMAINED ON AFTER SEVERAL CYCELS. AFTER SEVERAL TRIES LH MAIN CAME DOWN AFTER LEAVING HANDLE DOWN. SJU - [SDR JIKA2021121701](https://openairdocs.org/sdr/JIKA2021121701), Dec 17, 2021: LIGHT. MALFUNCTIONED. THE PILOT REPORTED THAT WHEN THEY LOWERED THE GEAR HANDLE ONLY THE 2 MAIN GEAR GREEN LIGHTS ILLUMINATED. THE NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE, AS WELL A - [SDR JIKA2021102801](https://openairdocs.org/sdr/JIKA2021102801), Oct 28, 2021: INTERFACE UNIT. DEFECTIVE. AMF FLT# 6905 EXPERIENCED A LH ENGINE FLAMEOUT AT 1500 FT DURING CLIMB, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. SJU MAINTENANCE TROUBLESHOT STARTING - [SDR JIKA2021092101](https://openairdocs.org/sdr/JIKA2021092101), Sep 21, 2021: WARNING MESSAGE. FALSE ACTIVATION. DURING CLIMB THE RIGHT “HYD LOW PRESS” ANNUNCIATOR CAME ON, THE HYDRAULIC PRESSURE GAUGE WAS READING NORMAL. PHOENIX MAINTENANCE INSPECTED AND PERFORMED RIGHT H - [SDR JIKA2021072001](https://openairdocs.org/sdr/JIKA2021072001), Jul 20, 2021: TRIM CYLINDER. INOPERATIVE. PILOT REPORTED HAVING A TRIM FAILURE IN FLIGHT. LANSING MAINTENANCE TROUBLESHOT TO THE TRIM ACTUATOR. PART ON HAND PENDING REPLACEMENT AT THIS TIME. - [SDR JIKA2021042801](https://openairdocs.org/sdr/JIKA2021042801), Apr 28, 2021: CONNECTOR. LOOSE. DURING CLIMB OUT FROM KBUR, THERE WAS A BURNING SMELL AND THEN A LITTLE BIT SMOKE COMING OUT FROM RIGHT ESSENTIAL PANEL. LOOKS LIKE SMOKE COMING OUT FROM ONE OF - [SDR JIKA2021022601](https://openairdocs.org/sdr/JIKA2021022601), Feb 26, 2021: UNKNOWN. SMOKE. DURING CRUISE FLIGHT AT 13000 FT. FROM KELP TO KBUR, THE CREW NOTED THERE WAS SMOKE IN THE AFT CABIN. THE CREW REQUESTED DIVERTING TO KPHX. THE AIRCRAFT DESCEND - [SDR JIKA2020122101](https://openairdocs.org/sdr/JIKA2020122101), Dec 21, 2020: CONTROL HANDLE. STUCK. AMF FLT NR 3928. DURING TAKEOFF FROM KBUR, UPON LEVELING AT 5000. PILOT ATTEMPTED TO MOVE THE GEAR HANDLE TO THE UP POSITION, BUT GEAR WOULD NOT RETRACT. PILOT - [SDR JIKA2020110901](https://openairdocs.org/sdr/JIKA2020110901), Nov 9, 2020: COOLING TURBINE. BROKEN. JUST PRIOR TO LEVEL OFF AT 13000, STEADY WING OVERHEAT ANNUNCIATOR LIGHT CAME ON AND SMALL AMOUNT OF SMOKE CAME INTO THE CABIN. THE PILOT WENT THROUGH THE MEMOR - [SDR JIKA2020050142901](https://openairdocs.org/sdr/JIKA2020050142901), Apr 29, 2020: CURRENT LIMITER. BLOWN. ABOUT 15 MINUTES PRIOR TO ARRIVAL TO KLAN FROM KPLN, THE ELECTRICAL INSTRUMENTS STARTED SURGING AND OCCASIONALLY THE COMMS, GPS, AND NAVS ON THE PILOT SIDE WOUL - [SDR JIKA20200227501](https://openairdocs.org/sdr/JIKA20200227501), Feb 25, 2020: WIRE. DAMAGED. DURING TAKEOFF ROLL FROM DFW PITCH TRIM WAS ADJUSTED UP FOR CLIMB. THE TRIM CONTROLS STOPPED WORKING WHILE THE WHEELS LIFTING OFF FROM THE RUNWAY. IT WAS DIFFIC - [SDR KY7A202002240001](https://openairdocs.org/sdr/KY7A202002240001), Feb 20, 2020: BEARING. WORN. MECHANIC TURNED PROPELLER ON GROUND AND NOTICED GRINDING NOISE COMING FROM THE GEAR CASE. FOUND WORN BEARING ON TACH-GENERATOR GEAR ASSEMBLY. MX REMOVED AND REP - [SDR KY7A202002209001](https://openairdocs.org/sdr/KY7A202002209001), Feb 19, 2020: OIL SYSTEM. OVERSERVICED. FLIGHT CREW REPORTED TEMP CONTROL SELECTED AUTO OR HOT, FULL HOT ON CONTROL KNOB HAS SMOKE/HAZE COMING FROM FLOOR AREA IN COCKPIT. MX DRAINED EXCESS OIL FROM AI - [SDR JIKA20200129301](https://openairdocs.org/sdr/JIKA20200129301), Jan 23, 2020: MIXING VALVE. DEFECTIVE. DURING INITIAL CLIMB FROM DFW, AFTER TURNING ON BLEED AIR VALVES, THE COCKPIT BECAME VERY HOT, EVEN THOUGH THE SYSTEM WAS SET AT THE LOWEST SETTING. TEMP SELECT - [SDR JIKA2020011501](https://openairdocs.org/sdr/JIKA2020011501), Jan 10, 2020: CONTROL CABLE. MALFUNCTIONED. AFTER TAKEOFF FROM KELM, APPROXIMATELY 600 AGL, RIGHT ENGINE FLAMEOUT. PILOT NOTICED THE RIGHT FUEL FLOW WAS AT ZERO AND PILOT CHECKED RIGHT ENGINE CONTROL LEVE - [SDR JIKA2019120200501](https://openairdocs.org/sdr/JIKA2019120200501), Nov 25, 2019: OVERHEAT SENSOR. DEFECTIVE. SHORTLY AFTER TAKEOFF FROM DFW, RIGHT ENGINE OIL TEMP EXCEEDED TOLERANCES OVER HIGH RED LINE. PILOT PERFORMED PRECAUTIONARY ENGINE SHUT DOWN, ATC DECLARED AN EM - [SDR JIKA20191118601](https://openairdocs.org/sdr/JIKA20191118601), Nov 18, 2019: ACCUMULATOR. SEPARATED. ON CLIMB OUT FROM KSMX THE PILOT REPORTED THAT THE LEFT AND RIGHT HYDRAULIC SYSTEM FAIL WARNING LIGHTS ILLUMINATED, FOLLOWED BY A LOSS OF HYDRAULIC PRESSURE. TH - [SDR JIKA20191118201](https://openairdocs.org/sdr/JIKA20191118201), Nov 18, 2019: UNKNOWN. SMOKE. WHILE ENROUTE TO SAT, CREW REPORTED SMOKE IN THE COCKPIT WITH AN OILY SMELL. THEY SHUT OFF THE BLEED AIR AND PUT ON THEIR OXYGEN MASK. FLIGHT LANDED WITHOUT INC - [SDR CA190402015](https://openairdocs.org/sdr/CA190402015), Feb 25, 2019: NOZZLE. FAILED. (CAN) THE MAIN OIL JET CRACKED IN THE GEAR BOX CAUSING A BEARING TO FAIL DUE TO LACK OF OIL ON THE BEARING IN THE MAIN GEAR CASE. THE ENGINE WAS PULLED DUE TO T - [SDR HKGA2015F00035](https://openairdocs.org/sdr/HKGA2015F00035), Feb 12, 2015: ANGLE. CRACKED. LT OTBD LOWER ANGLE IN BATTERY BOX CRACKED AT STA 80.87. - [SDR HKGA2015F00034](https://openairdocs.org/sdr/HKGA2015F00034), Feb 12, 2015: ANGLE. CRACKED. LEFT OTBD LOWER ANGLE IN BATTERY BOX CRACKED AT STA 80.87. - [SDR TN8A2015011500001](https://openairdocs.org/sdr/TN8A2015011500001), Dec 31, 2014: VALVE. FAILED. FLIGHT RETURNING TO BASE AFTER FREIGHT CHARTER FLIGHT. UPON APPROACH PILOT SELECTED GEAR DOWN BUT DID NOT RECEIVE A GREEN LIGHT INDICATION FOR THE NOSE GEAR. PI - [SDR CA140331003](https://openairdocs.org/sdr/CA140331003), Mar 27, 2014: PULLEY. NOISY. (CAN) THE FLIGHT CREW REPORTED ROUGHNESS IN CONTROL COLUMN IN FULL NOSE UP CONFIGURATION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOISE IN TAIL IN T - [SDR CA140321015](https://openairdocs.org/sdr/CA140321015), Feb 10, 2014: UNKNOWN. SMOKE. (CAN) DURING TAKEOFF WITH BLEEDS ON HIGH & TEMP CONTROLLER IN AUTO POSITION, THE CABIN BEGAN TO FILL WITH SMOKE. ACFT RETURNED TO BASE & MX COMPLETED NUMEROUS G - [SDR KY7A20131217001](https://openairdocs.org/sdr/KY7A20131217001), Dec 17, 2013: TURBINE. DAMAGED. PILOT REPORTED THAT ON CLIMB OUT THE ENG LOST OIL PRESS. PILOT SECURED THE ENG & RETURNED TO THE DEPARTURE AIRPORT & LANDED. MX FOUND SIGNIFICANT DAMAGE TO THE - [SDR CA131211002](https://openairdocs.org/sdr/CA131211002), Dec 11, 2013: FCU. UNRESPONSIVE. (CAN) ENGINE WAS STARTED, YET WHEN POWER LEVERS WERE MOVED FORWARD TO TAXI THE LT ENGINE WAS UNRESPONSIVE. ACFT WAS RETURNED TO MAINTENANCE AND AFTER TROUBLESHO - [SDR CA130812006](https://openairdocs.org/sdr/CA130812006), Aug 11, 2013: LINE. CRACKED. (CAN) FLIGHT CREW SNAGGED HYD SIGHT GLASS EMPTY AND NO FLAP MOVEMENT WHILE SPOOLING ENGINE, LOCATED AND REPLACED CRACKED HYD LINE UNDER RT CABIN FLOORBOARD JUST - [SDR CA120125012](https://openairdocs.org/sdr/CA120125012), Jan 24, 2012: BRIDGE. FAILED. (CAN) DURING TAKEOFF ROLL THE LT TORQUE GAUGE WAS READING ZERO. TAKEOFF WAS ABORTED. MAINTENANCE WAS CONTACTED AND THEY FOUND THE NR 1 TORQUE RING BRIDGE HAD FA - [SDR CA111118016](https://openairdocs.org/sdr/CA111118016), Oct 28, 2011: TEE FITTING. CRACKED. (CAN) AIRCRAFT RETURNED TO BASE AS LT ENGINE COULD NOT MAKE FULL POWER. LT ENGINE FUEL BOWL TEE FITTING FOUND CRACKED. FITTING REPLACED AND ACFT RETURNED TO SER - [SDR CA110830013](https://openairdocs.org/sdr/CA110830013), Aug 24, 2011: INDICATOR. INTERMITTENT. (CAN) PILOT ABORTED TAKEOFF, WAS NOT ABLE TO GET MORE THAT 35 PERCENT TORQUE ON THE RT ENGINE. MX REPLACED THE FOLLOWING ITEMS AFTER CONFIRMING TORQUE WAS STICK - [SDR CA110829015](https://openairdocs.org/sdr/CA110829015), Aug 19, 2011: SCREW. LOOSE. (CAN) TAKEOFF ABORTED DUE TO RT ENGINE NOT PRODUCING TAKEOFF POWER ON THE TAKEOFF ROLL. CREW TAXIED TO RUN UP AREA AND COULD NOT REPRODUCE THE FAULT. CREW CONTI - [SDR CA110802007](https://openairdocs.org/sdr/CA110802007), Jul 28, 2011: CASE. CRACKED. UPON DISASSEMBLY, FOUND THE STUD AND DOWEL LOOSE ON THE FWD SIDE OF THE CASE AT THE 900 A-CLOCK POSITION LOOKING AT THE CASE. THE DOWEL AND STUD BASE WAS ALSO F - [SDR CA110628001](https://openairdocs.org/sdr/CA110628001), Jun 22, 2011: SPLINE. WORN. EXTERNAL SPLINES HAVE MAJOR STEP WEAR IN THE ROOT AREA. SEVERAL SPLINES HAVE A SHARP STEP AT THE BASE OF THE TOOTH IN THE ROOT AREA, APPROX .005 INCH DEEP. THES - [SDR CA110617010](https://openairdocs.org/sdr/CA110617010), Jun 17, 2011: FUEL CONTROL. CONTAMINATED. THE CYLINDER BORE AND PISTON AREA WAS FOUND CORRODED AND PLUGGED WITH BLACK PARTICLES WHICH APPEAR TO HAVE GENERATED FROM THE PISTON RING SEALS. IT IS SUSPECT T - [SDR CA110519002](https://openairdocs.org/sdr/CA110519002), May 18, 2011: TEE FITTING. CRACKED. AFTER AN OPERATIONAL RUN, FUEL WAS FOUND AROUND THE LT ENGINE FUEL BOWL TEE FITTING. THE FITTING WAS REMOVED AND PRESSURE TESTED. A SMALL CRACK WAS FOUND DIRECT - [SDR CA110401006](https://openairdocs.org/sdr/CA110401006), Mar 30, 2011: BLADE. DAMAGED. (CAN) PILOT REPORTED VIBRATIONS AND DETERMINED IT WAS THE LT PROP. TECHNICAL HISTORY WAS REVIEWED AND FOUND THAT BALANCE WAS AN ISSUE IN THE LIFE OF THE PROP SI - [SDR CA110307002](https://openairdocs.org/sdr/CA110307002), Mar 6, 2011: WINDSHIELD. CRACKED. (CAN) AT 21000 FT DURING CRUISE, 20 MINUTES INTO FLIGHT DEPARTING BS RT WINDSHIELD OUTER GLASS PANE SHATTERED. ACFT DESCENDED, DEPRESSURIZED, TURNED AROUND AND - [SDR CA101022002](https://openairdocs.org/sdr/CA101022002), Oct 20, 2010: STRUT. FRACTURED. LT MAIN GEAR LOWER STRUT TORQUE KNEE ATTACH BOSS FRACTURED AND SEPARATED FROM MAIN LOWER ASSY DURING TAXI CAUSING SEVERE SHIMMY. - [SDR CA101019008](https://openairdocs.org/sdr/CA101019008), Oct 14, 2010: ACTUATOR. SEIZED. FLIGHT CREW REPORTED RUDDER TRIM WOULD NOT MOVE LT OF NEUTRAL. ACTUATOR REMOVED AND FOUND SEIZED. ACTUATOR REPLACED AND ACFT RETURNED TO SERVICE. - [SDR CA090522004](https://openairdocs.org/sdr/CA090522004), May 21, 2009: LANDING GEAR. MALFUNCTIONED. (CAN) ON DESCENT, GEAR WAS SELECTED DOWN AND THE RT GEAR DID NOT EXTEND AND LOCK DOWN ON FIRST ATTEMPT. AFTER MULTIPLE ATTEMPTS ALL 3 GEAR EXTENDED AND WERE VIS - [SDR CA081205008](https://openairdocs.org/sdr/CA081205008), Dec 4, 2008: WINDSHIELD. FAILED. (CAN) ON APPROACH THE LT WINDSHIELD SHATTERED. MX WAS DISPATCHED TO REPLACE THE WINDSHIELD. THE TEMP CONTROLLER WAS FOUND TO BE DEFECTIVE ALSO. TEMP CONTROLLER - [SDR CA080922005](https://openairdocs.org/sdr/CA080922005), Sep 9, 2008: LINE. CRACKED. (CAN) PILOT REPORTED HYD FLUID LEAKING IN LT WW. SMALL PINHOLE WAS FOUND IN LINE. LINE REPLACED AND ACFT RETURNED TO SERVICE. - [SDR CA080905008](https://openairdocs.org/sdr/CA080905008), Sep 2, 2008: A/C PACK. DAMAGED. (CAN) ON APPROACH, THE PILOT NOTICED SMOKE COMING OUT OF FRESH AIR VENTS AND MOMENTS LATER LT WING OVERHEAT LIGHT CAME ON. ACFT LANDED WITHOUT INCIDENT. MX WENT - [SDR CA080611007](https://openairdocs.org/sdr/CA080611007), Jun 10, 2008: BEARING. SPALLED. (CAN) THE REAR TURBINE WAS FOUND WITH HEAVY SPALLING, GALLING, HEAVY SCORING AND MISSING MATERIAL OFF THE OUTER RACEWAY AND ON THE ROLLING ELEMENTS. THE BEARING - [SDR CA071106008](https://openairdocs.org/sdr/CA071106008), Oct 25, 2007: RETAINER. CRACKED. (CAN) WHILE ENGINE WAS BEING REPLACED MAINTENANCE NOTICED FATIQUE CRACKS EMINATING FROM THE (PROP SHAFT) RETAINING BOLT AREA. (TC NR 20071106008) - [SDR CA070319005](https://openairdocs.org/sdr/CA070319005), Mar 16, 2007: IMPELLER. FRACTURED. (CAN) ENGINE WAS REMOVED DUE TO NOT MAKING TARGET TAKEOFF TORQUE. UPON DISASSEMBLY THE 2ND STAGE COMPRESSOR IMPELLER FAILED AND HAS EXPERIENCED A FATIGUE TYPE F - [SDR CA070307009](https://openairdocs.org/sdr/CA070307009), Mar 5, 2007: REGULATOR. MALFUNCTIONED. (CAN) AC DEPARTED BASE AND UPON GEAR RETRACTION BOTH LT AND RT HYD PRESSURE LIGHTS ILLUMINATED FOR 3-4 SECONDS THEN WENT OUT. AIRCRAFT RETURNED TO BASE AND UPON All 84: https://openairdocs.org/model/fairchild-sa227-cc/reports.md ## STCs that may be installed (OpenAirDocs) (63, 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 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 SA11222DS](https://openairdocs.org/stc/SA11222DS): Installation of automatic dependent surveillance- broadcast( ADS-B) Out. BHE & Associates Ltd - [STC SA7093NM](https://openairdocs.org/stc/SA7093NM): Installation of emergency exit lighting system. Bruce Aerospace Inc - [STC SA09768DS](https://openairdocs.org/stc/SA09768DS): Installation of S-TEC 01236 Digital Flight Control System (DFCS). S-Tec Corporation - [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc - [STC ST00789WI](https://openairdocs.org/stc/ST00789WI): Installation of the Fairchild Digital Data Flight Recorder Model F800 or F1000. Worldwide Aircraft Services LLC - [STC SA09169AC](https://openairdocs.org/stc/SA09169AC): Installation of Concorde RG390ES sealed lead-acid batteries. Ontic Engineering and Manufacturing Inc - [STC SA10352SC](https://openairdocs.org/stc/SA10352SC): Installation of an Aviation Communication & Surveillance Systems (ACSS) TCAS II, dual ACSS Mode-S transponders and dual Sextant VSI/TCAS display. Ontic Engineering and Manufacturing Inc - [STC SA04514NY](https://openairdocs.org/stc/SA04514NY): Single/Dual Transponder System ADS-B Upgrade. Scandinavian Avionics Design ApS - [STC SA02677LA](https://openairdocs.org/stc/SA02677LA): Modification to upgrade the existing Mode S Transponder system by installing the ACSS NXT-700 Transponder with ADS-B Out and optionally install the ACSS NXG-900 GPS as the position source for ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC SA02678LA](https://openairdocs.org/stc/SA02678LA): Modification to upgrade the existing Mode S Transponder system by installing the ACSS NXT-600 Transponder with ADS-B Out and optionally install the ACSS NXG-900 GPS as the position source for ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc - [STC SA04405CH](https://openairdocs.org/stc/SA04405CH): Installation of a dual Garmin G700TXi Display System in accordance with Toledo Jet Center Master Data List, Document No. TJC-G700.001-MDL, Revision IR, dated May 6, 2019, or later FAA approved revision. Toledo Jet Center LLC - [STC SA09190AC](https://openairdocs.org/stc/SA09190AC): Installation of an Electric-Driven Vapor Cycle Air Conditioning System. Air Comm Corporation - [STC SA02890AT](https://openairdocs.org/stc/SA02890AT): Installation of a Honeywell Model CAS 67A Traffic Alert and Collision Avoidance System II (TCAS II) with Single Mode-S Transponder. Toledo Jet Center, LLC - [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne 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 SA03973NY](https://openairdocs.org/stc/SA03973NY): Replacement of existing TCAS 7.0 by TCAS 7.1. Scandinavian Avionics Design ApS - [STC ST00276WI](https://openairdocs.org/stc/ST00276WI): Installation of Kedeg Company 21BC11e Coaleser Assemly. Purolator Facet, Inc - [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation - [STC SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation - [STC SA1542GL](https://openairdocs.org/stc/SA1542GL): Install Aero Medical Products Mfg., Inc. Air Ambulance Stretcher P/N 126 using Installation Kit P/N 805. Paul/ Lanna Egan LLC - [STC SA00780SE](https://openairdocs.org/stc/SA00780SE): Installation of the True Lock Safety Retention Axle Lock Nut System. True Lock LLC - [STC SA03642NY](https://openairdocs.org/stc/SA03642NY): Installation of Sandel ST3400 Terrain Awareness Warning System (Class A). Maxcraft Avionics Ltd - [STC SA01969SE](https://openairdocs.org/stc/SA01969SE): Installation of a Mid-Continent MD302 Standby Attitude Module. Mid-Continent Instruments and Avionics - [STC SA01229SE PAGE 1](https://openairdocs.org/stc/SA01229SE%20PAGE%201): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc - [STC SA01933LA-D PAGE 1](https://openairdocs.org/stc/SA01933LA-D%20PAGE%201): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA04182AT](https://openairdocs.org/stc/SA04182AT): Installation of Pilot and Copilot Main Windshield. PPG Aerospace - [STC SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System. Garmin International Inc - [STC SA00269BO](https://openairdocs.org/stc/SA00269BO): Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ), Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1, and Avidyne Mounting Tray P/N 700-00034-000. Avidyne Corporation - [STC SA03893AT](https://openairdocs.org/stc/SA03893AT): Installation of MT-Propeller Model MTV-27-1-E-C-F-R(G)/CFRL250-103. MT-Propeller USA Inc - [STC SA02149AK](https://openairdocs.org/stc/SA02149AK): Installation of GX50/60 GPS Navigator, Capstone configured MX20 Multi-Function Display and UAT transceiver. Garmin International Inc - [STC SA01692SE](https://openairdocs.org/stc/SA01692SE): Installation of a Garmin GMX 200 Multi-Function Display. Garmin International Inc - [STC SA03148NY](https://openairdocs.org/stc/SA03148NY): The installation of the Latitude Technologies Corporation S100 Tracking System. Latitude Technologies Corporation - [STC SA00674WI-D](https://openairdocs.org/stc/SA00674WI-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 SA01487SE-D](https://openairdocs.org/stc/SA01487SE-D): Installation of a GDL 69 or GDL 69A XM Satellite Receiver. Garmin International Inc - [STC SA00281BO](https://openairdocs.org/stc/SA00281BO): Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ), Sensor Systems Inc. Antenna P/N S67-1575-109, or equivalent, and optional Avidyne Mounting Tray P/N 700-00165-000. Avidyne Corporation - [STC SA00243BO](https://openairdocs.org/stc/SA00243BO): Installation of Centurion Consulting, Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100), or without roll steering (p/n 0025-5200). Icarus Avionics, LLC - [STC SA00290BO](https://openairdocs.org/stc/SA00290BO): Installation of Avidyne Corporation Part Number 700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXX. Avidyne Corporation - [STC SA02110CH](https://openairdocs.org/stc/SA02110CH): Installation of a Time Trac Data Recorder. P2 Incorporated - [STC SA01473SE](https://openairdocs.org/stc/SA01473SE): Installation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote Transponde. Garmin AT Inc - [STC SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc - [STC SA01306WI-D](https://openairdocs.org/stc/SA01306WI-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. Rockwell Collins Inc - [STC SA01695SE](https://openairdocs.org/stc/SA01695SE): Installation of an antenna. Garmin AT Inc - [STC SA01141WI-D](https://openairdocs.org/stc/SA01141WI-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-94 Mode S Transponder System installation with CTL-92E control head. Rockwell Collins Inc - [STC SA01487SE](https://openairdocs.org/stc/SA01487SE): Installation of a GDL 69 or GDL 69A XM Satellite Receiver in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0217-00, Revision A, dated December 20, 2004, or later FAA approved revision. Garmin AT Inc - [STC SA01900NY](https://openairdocs.org/stc/SA01900NY): Installation of a Honeywell MK VI EGPWS. Western Avionics All 63: https://openairdocs.org/model/fairchild-sa227-cc/stcs.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.