# Service difficulty reports: Fairchild SA227-CC

A list on [Fairchild SA227-CC](https://openairdocs.org/model/fairchild-sa227-cc.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 84 reports

- [SDR KY7A2025093000038](https://openairdocs.org/sdr/KY7A2025093000038.md): Brake · weak · Sep 17, 2025 · N31171 · Frchld SA227CC · Landing Gear Brake System
  > 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.md): Indicator · inoperative · Jun 23, 2022 · N244DH · Frchld SA227CC · Main Landing Gear
  > 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 DECLARED. AIRCRAFT LANDED IN KCHS WITHOUT FURTHER ISSUE. AIRCRAFT WAS INSPECTED AND FOUND SAFE TO FERRY
- [SDR JIKA2022033101](https://openairdocs.org/sdr/JIKA2022033101.md): Controller · broken · Mar 31, 2022 · N672AV · Frchld SA227CC · Cabin Temperature Controller
  > 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 THERE WAS NO MORE SMOKE. LAN MAINTENANCE REMOVED AND REPLACED CABIN TEMP CONTROL. OPS CHECK GOOD.
- [SDR JIKA2022020301](https://openairdocs.org/sdr/JIKA2022020301.md): Not Reported · not reported · Feb 3, 2022 · N152AF · Frchld SA227CC · Main Landing Gear
  > 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 MAINTENANCE PEROFRMED LANDING GEAR RETRACTION AND EXTENSION CHECK, OPS CHECK GOOD.
- [SDR JIKA2021121701](https://openairdocs.org/sdr/JIKA2021121701.md): Light · malfunctioned · Dec 17, 2021 · N243DH · Frchld SA227CC · Nose/Tail Landing Gear
  > 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 AS NO RED IN TRANSIT LIGHT ILLUMINATED. MAINTENANCE COULD NOT DUPLICATE THE NOSE GEAR DISCREPANCY ON
- [SDR JIKA2021102801](https://openairdocs.org/sdr/JIKA2021102801.md): Interface Unit · defective · Oct 28, 2021 · N249DH · Frchld SA227CC · Engine Controls
  > AMF FLT# 6905 EXPERIENCED A LH ENGINE FLAMEOUT AT 1500 FT DURING CLIMB, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. SJU MAINTENANCE TROUBLESHOT STARTING L/H ENGINE NORMALLY AND FOUND L/H ENGINE BYPASSING AND SURGING IN IDLE WITH NO OTHER INPUTS. DURING
- [SDR JIKA2021092101](https://openairdocs.org/sdr/JIKA2021092101.md): Warning Message · false activation · Sep 21, 2021 · N426MA · Frchld SA227CC · Hydraulic System, Main
  > DURING CLIMB THE RIGHT “HYD LOW PRESS” ANNUNCIATOR CAME ON, THE HYDRAULIC PRESSURE GAUGE WAS READING NORMAL. PHOENIX MAINTENANCE INSPECTED AND PERFORMED RIGHT HYDRAULIC SYSTEM OPERATIONAL CHECKS, ACTUATING THE FLAPS FULL UP TO FULL DOWN REPEATEDLY RH HYDRAULIC
- [SDR JIKA2021072001](https://openairdocs.org/sdr/JIKA2021072001.md): Trim Cylinder · inoperative · Jul 20, 2021 · N672AV · Frchld SA227CC · Flight Control System
  > 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.md): Connector · loose · Apr 28, 2021 · N801AF · Frchld SA227CC · Air Distribution System
  > 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 CIRCUIT BREAKER, PILOT PULLED OUT THAT CIRCUIT BREAKER. PILOT REQUESTED TO RETURN TO KBUR AND FOL
- [SDR JIKA2021022601](https://openairdocs.org/sdr/JIKA2021022601.md): Unknown · smoke · Feb 26, 2021 · N709TR · Frchld SA227CC · Air Distribution System
  > 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 DESCENDED TO 10, 000 FT. AND TURNED OFF THE BLEEDS, THE SMOKE IN THE AFT CABIN WAS CLEARED. AIRCRAFT LAN
- [SDR JIKA2020122101](https://openairdocs.org/sdr/JIKA2020122101.md): Control Handle · stuck · Dec 21, 2020 · N475AF · Frchld SA227CC · Landing Gear Selector
  > 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 CHECKED CIRCUIT BREAKERS WERE NORMAL AND ATTEMPTED TO MOVE THE GEAR HANDLE TO THE UP POSITION WIT
- [SDR JIKA2020110901](https://openairdocs.org/sdr/JIKA2020110901.md): Cooling Turbine · broken · Nov 9, 2020 · N422MA · Frchld SA227CC · Engine Bleed Air System
  > 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 MEMORY ITEMS AND CHECKLIST AND THE LIGHT WENT OUT AND NO MORE SMOKE. RETURNED TO THE DEPARTURE AIRPORT.
- [SDR JIKA2020050142901](https://openairdocs.org/sdr/JIKA2020050142901.md): Current Limiter · blown · Apr 29, 2020 · N709TR · Frchld SA227CC · DC Regulator
  > 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 WOULD FLASH OFF AND ON. PRIOR TO GETTING THE AIRPORT IN SIGHT, THE ELECTRICAL POWER SHUT OFF AND IT TO
- [SDR JIKA20200227501](https://openairdocs.org/sdr/JIKA20200227501.md): Wire · damaged · Feb 25, 2020 · N240DH · Frchld SA227CC · Auto Flight System Wiring
  > 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 DIFFICULT TO MAINTAIN ALTITUDE ASSIGNED SINCE THE AIRCRAFT KEPT CLIMBING. THE PILOT HAD IMMEDIATELY ADVISE
- [SDR KY7A202002240001](https://openairdocs.org/sdr/KY7A202002240001.md): Bearing · worn · Feb 20, 2020 · N571KL · Frchld SA227CC · Engine RPM Indicating System
  > 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 REPLACED THE INTERMEDIATE HOUSING AND GEAR ASSEMBLY, ALSO REPLACED THE FUEL PUMP WHICH FIXED THE GRIND
- [SDR KY7A202002209001](https://openairdocs.org/sdr/KY7A202002209001.md): Oil System · overserviced · Feb 19, 2020 · N538KL · Frchld SA227CC · Cabin Cooling System
  > 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 AIR CYCLE MACHINE.
- [SDR JIKA20200129301](https://openairdocs.org/sdr/JIKA20200129301.md): Mixing Valve · defective · Jan 23, 2020 · N240DH · Frchld SA227CC · Cabin Cooling System
  > 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 SELECTOR SWITCH WAS RECYCLED THROUGH ALL POSITIONS AND CONTROL KNOB WAS KEPT AT LOWEST SETTING, BUT COCKP
- [SDR JIKA2020011501](https://openairdocs.org/sdr/JIKA2020011501.md): Control Cable · malfunctioned · Jan 10, 2020 · N544UP · Frchld SA227CC · Propeller Feathering/Reversing
  > 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 LEVERS, STOP AND FEATHER, BOOST PUMPS AND IGNITION THEN ENGINE HAD WOUND DOWN. PILOT HAD REQUESTED AN
- [SDR JIKA2019120200501](https://openairdocs.org/sdr/JIKA2019120200501.md): Overheat Sensor · defective · Nov 25, 2019 · N241DH · Frchld SA227CC · Engine Oil Indicating System
  > SHORTLY AFTER TAKEOFF FROM DFW, RIGHT ENGINE OIL TEMP EXCEEDED TOLERANCES OVER HIGH RED LINE. PILOT PERFORMED PRECAUTIONARY ENGINE SHUT DOWN, ATC DECLARED AN EMERGENCY. AIRCRAFT LANDED BACK AT DFW WITH NO INCIDENT. MAINTENANCE REMOVED AND REPLACED OIL TEMPERA
- [SDR JIKA20191118601](https://openairdocs.org/sdr/JIKA20191118601.md): Accumulator · separated · Nov 18, 2019 · N673AV · Frchld SA227CC · Hydraulic Accumulator, Auxiliary
  > 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. THE PILOT PERFORMED A MANUAL GEAR EXTENSION RECEIVED THREE GREEN DOWN AND LOCKED INDICATION, DECLARED
- [SDR JIKA20191118201](https://openairdocs.org/sdr/JIKA20191118201.md): Unknown · smoke · Nov 18, 2019 · N569UP · Frchld SA227CC · Air Distribution System
  > 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 INCIDENT AT KSAT. SAT MAINTENANCE INSPECTED THE BLEED AIR SYSTEM FOR EVIDENCE OF OIL, NO DEFECTS FOUND.
- [SDR CA190402015](https://openairdocs.org/sdr/CA190402015.md): Nozzle · failed · Feb 25, 2019 · Frchld SA227CC · Turbine Engine Oil System
  > (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 THE OIL LAB BECAUSE OF MAJOR M50 MATERIAL THAT WAS NOTED FROM THE BEARING.THE ENGINE PART HAS 4612.9
- [SDR HKGA2015F00035](https://openairdocs.org/sdr/HKGA2015F00035.md): Angle · cracked · Feb 12, 2015 · N26959 · Frchld SA227CC · Fuselage Miscellaneous Structure
  > LT OTBD LOWER ANGLE IN BATTERY BOX CRACKED AT STA 80.87.
- [SDR HKGA2015F00034](https://openairdocs.org/sdr/HKGA2015F00034.md): Angle · cracked · Feb 12, 2015 · N26959 · Frchld SA227CC · Fuselage Miscellaneous Structure
  > LEFT OTBD LOWER ANGLE IN BATTERY BOX CRACKED AT STA 80.87.
- [SDR TN8A2015011500001](https://openairdocs.org/sdr/TN8A2015011500001.md): Valve · failed · Dec 31, 2014 · N3114G · Frchld SA227CC · Hydraulic System, Main
  > 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. PILOT RECYCLED GEAR AND REQUESTED TO TERMINATE LANDING. PILOT MANUAL EXTENDED THE LANDING GEAR IAW
- [SDR CA140331003](https://openairdocs.org/sdr/CA140331003.md): Pulley · noisy · Mar 27, 2014 · Frchld SA227CC · Elevator Control System
  > (CAN) THE FLIGHT CREW REPORTED ROUGHNESS IN CONTROL COLUMN IN FULL NOSE UP CONFIGURATION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOISE IN TAIL IN THE FULL NOISE UP CONFIGURATION. MAINTENANCE FOUND A CABLE OFF THE PULLEY, FWD ELEVATOR DOWN SPRIN
- [SDR CA140321015](https://openairdocs.org/sdr/CA140321015.md): Unknown · smoke · Feb 10, 2014 · Frchld SA227CC · Air Distribution System
  > (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 GND RUNS & NO SMOKE IN CABIN. TEST FLIGHT WAS COMPLETED & NO SMOKE IN CABIN. ACFT RELEASED TO SERV
- [SDR KY7A20131217001](https://openairdocs.org/sdr/KY7A20131217001.md): Turbine · damaged · Dec 17, 2013 · N2728G · Frchld SA227CC · Turbine Section
  > 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 3RD STAGE TURBINE & DISASSEMBLED ENG. AFT TURBINE BEARING WAS FOUND DESTROYED, FAILED. 1ST & 2ND
- [SDR CA131211002](https://openairdocs.org/sdr/CA131211002.md): Fcu · unresponsive · Dec 11, 2013 · Frchld SA227CC · Fuel Control/Turbine Engines
  > (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 TROUBLESHOOTING WAS CARRIED OUT THE DRIVE BETWEEN THE FUEL PUMP AND FCU WAS FOUND TWISTED AND THE VESPAL SPLI
- [SDR CA130812006](https://openairdocs.org/sdr/CA130812006.md): Line · cracked · Aug 11, 2013 · Frchld SA227CC · Hydraulic System, Main
  > (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 FORWARD OF MAIN SPAR. LEAK CHECKED AND ACFT RETURNED TO SERVICE.
- [SDR CA120125012](https://openairdocs.org/sdr/CA120125012.md): Bridge · failed · Jan 24, 2012 · Frchld SA227CC · Engine BMEP/Torque Indicating
  > (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 FAILED. SYS WAS SWITCHED OVER TO THE NR 2 BRIDGE AND CALIBRATED. GROUND RUNS CARRIED OUT AND ACFT R
- [SDR CA111118016](https://openairdocs.org/sdr/CA111118016.md): Tee Fitting · cracked · Oct 28, 2011 · Frchld SA227CC · Engine Fuel Distribution
  > (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 SERVICE. ALSO CONNECTOR PLUG WIRE CONTROLLING THE BYPASS VALVE WAS REPAIRED AT THIS TIME.
- [SDR CA110830013](https://openairdocs.org/sdr/CA110830013.md): Indicator · intermittent · Aug 24, 2011 · Frchld SA227CC · Independent Instruments
  > (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 STICKING INTERMITTENTLY RT TORQUE SIGNAL CONDITIONER - PN 3102476-6 AND RT TORQUE GAUGE - PN 27-19158-0
- [SDR CA110829015](https://openairdocs.org/sdr/CA110829015.md): Screw · loose · Aug 19, 2011 · Frchld SA227CC · Power Lever
  > (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 CONTINUED ON AND TAKEOFF WAS IAW MFG PARAMETERS. MX REVIEWED RUN UP NRS AND TIGHTENED UP SCREW "X" WHI
- [SDR CA110802007](https://openairdocs.org/sdr/CA110802007.md): Case · cracked · Jul 28, 2011 · Frchld SA227CC · Accessory Gearboxes
  > 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 FOUND WITH CRACKS. BASE FOUND CRACKED ON BOTH SIDES OF THE DOWEL.
- [SDR CA110628001](https://openairdocs.org/sdr/CA110628001.md): Spline · worn · Jun 22, 2011 · Frchld SA227CC · Fuel Control/Turbine Engines
  > 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. THESE MARKS WERE VISIBLE BY USING A 10X POWER MAGNIFICATION LOOP. SPLINE OD WAS MEASURED AT 0.404" ACRO
- [SDR CA110617010](https://openairdocs.org/sdr/CA110617010.md): Fuel Control · contaminated · Jun 17, 2011 · Frchld SA227CC · Fuel Control/Turbine Engines
  > 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 THAT THE PISTON AND CYLINDER BORE ARE NOT CONCENTRIC WITH EACH OTHER. FURTHER BLOCKAGE AND RESTRICTI
- [SDR CA110519002](https://openairdocs.org/sdr/CA110519002.md): Tee Fitting · cracked · May 18, 2011 · Frchld SA227CC · Fuel Control/Turbine Engines
  > 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 DIRECTLY ABOVE THE WELD LOCATION ON THE TEE FITTING. FITTING REPLACED AND AIRCRAFT RETURNED TO SERVICE.
- [SDR CA110401006](https://openairdocs.org/sdr/CA110401006.md): Blade · damaged · Mar 30, 2011 · Frchld SA227CC · Propeller Assembly
  > (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 SINCE LAST OH. THE BLADES WERE INSPECTED FOR ROTATIONAL PLAY AND FOUND ALL 4 BLADES WERE LOOSE AND 1 B
- [SDR CA110307002](https://openairdocs.org/sdr/CA110307002.md): Windshield · cracked · Mar 6, 2011 · Frchld SA227CC · Flight Compartment Windows
  > (CAN) AT 21000 FT DURING CRUISE, 20 MINUTES INTO FLIGHT DEPARTING BS RT WINDSHIELD OUTER GLASS PANE SHATTERED. ACFT DESCENDED, DEPRESSURIZED, TURNED AROUND AND CAME BACK TO BS.
- [SDR CA101022002](https://openairdocs.org/sdr/CA101022002.md): Strut · fractured · Oct 20, 2010 · Frchld SA227CC · Main Landing Gear Strut/Axle/Truck
  > 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.md): Actuator · seized · Oct 14, 2010 · Frchld SA227CC · Rudder Tab Control System
  > 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.md): Landing Gear · malfunctioned · May 21, 2009 · Frchld SA227CC · Landing Gear Retraction/Extension System
  > (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 VISUALLY CONFIRMED DOWN AND LOCKED. CREW ELECTED TO FLY TO ANOTHER BASE FOR ADDITIONAL MX INSTEAD OF LA
- [SDR CA081205008](https://openairdocs.org/sdr/CA081205008.md): Windshield · failed · Dec 4, 2008 · Frchld SA227CC · Flight Compartment Windows
  > (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 REPLACED ALONG WITH WINDSHIELD AND ACFT RETURNED TO SERVICE.
- [SDR CA080922005](https://openairdocs.org/sdr/CA080922005.md): Line · cracked · Sep 9, 2008 · Frchld SA227CC · Hydraulic System, Main
  > (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.md): A/C Pack · damaged · Sep 2, 2008 · Frchld SA227CC · Cabin Cooling System
  > (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 TO LOOK AND FOUND THAT THE LT COOLING TURBINE HAD A CATASTROPHIC FAILURE. THE LT BLEED SYSTEM WAS M
- [SDR CA080611007](https://openairdocs.org/sdr/CA080611007.md): Bearing · spalled · Jun 10, 2008 · Frchld SA227CC · Engine (Turbine/Turboprop)
  > (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 HAD ONLY 12.5 HOURS SINCE NEW/CAM. THE ENGINE WAS MAKING A STRANGE GRINDING SOUND THAT WAS NOTICED
- [SDR CA071106008](https://openairdocs.org/sdr/CA071106008.md): Retainer · cracked · Oct 25, 2007 · Frchld SA227CC · Propeller Assembly
  > (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.md): Impeller · fractured · Mar 16, 2007 · Frchld SA227CC · Turbine Engine Compressor Section
  > (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 FAILURE. THE PRESENT TIME ON THE IMPELLER IS 20,650.2 HOURS AND 28,175 CYCLES. A LARGE PIECE OF THE
- [SDR CA070307009](https://openairdocs.org/sdr/CA070307009.md): Regulator · malfunctioned · Mar 5, 2007 · Frchld SA227CC · Hydraulic System, Main
  > (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 INVESTIGATION IT WAS FOUND THAT NO RESIDUAL HYD PRESSURE WAS PRESENT AFTER ENGINE SHUTDOWN. UPON

Next page: https://openairdocs.org/model/fairchild-sa227-cc/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = 'SA227CC'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/fairchild-sa227-cc/reports

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