N702M, cancelled Jan 21, 2005

Service difficulty reports · 37

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 n_number = 'N702M' AND deregistration_id = 'N702M-2005-01-21'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 2002F00419Door Seal · failedCABIN ALTITUDE WARNING LIGHT CAME ON ABOVE 10,000 FEET. CREW GOT AIRCRAFT TO PRESSURIZE IN EITHER AUTOMATIC OR MANUAL MODE. CREW RETURNED TO STATION. PASSENGER DOOR SEAL WAS DAMAGED. INITIALLY DEFERRED PRESSURIZATION, THEN LATER REPLACED CABIN DOOR SEAL. Jan 29, 2002 · N702M · Swrngn SA227AC · Passenger/Crew DoorsSDR 2002F00353Seal · damagedDEN - FLT 1314 - CABIN ALTITUDE WARNING LIGHT CAME ON ABOVE 10,000 FEET. CREW COULD NOT GET AIRCRAFT TO PRESSURIZE IN EITHER AUTOMATIC OR MANUAL MODE. CREW RETURNED TO STATION. PASSENGER DOOR SEAL WAS DAMAGED. INITIALLY DEFERRED PRESSURIZATION, THEN LATER Jan 29, 2002 · N702M · Swrngn SA227AC · Passenger/Crew DoorsSDR 2002F00522Hydraulic Line · leakingWDG - FLT 1322 - ON CLIMB-OUT, BOTH HYD LIGHTS CAME ON AND HYDRAULIC PRESSURE GAUGE WENT TO '0'. CREW LANDED AFTER DECLARING EMERGENCY AND MANUALLY EXTENDING THE GEAR. SUSPECTED BREAK IN HYDRAULIC LINE CAUSING FLUID LOSS LEADING TO HYDRAULIC PRESSURE LOSS. Dec 5, 2001 · N702M · Swrngn SA227AC · Hydraulic System, MainSDR 2002F00421Line · leakingON CLIMB-0UT, BOTH HYDRAULIC LIGHTS CAME ON AND HYDRAULIC PRESSURE GAGE WENT TO ZERO. CREW LANDED AFTER DECLARING EMERGENCY AND MANUALLY EXTENDING THE GEAR. SUSPECTED BREAK IN HYDRAULIC LINE CAUSING FLUID LOSS LEADING TO HYDRAULIC PRESSURE LOSS. REPLACED FLDec 5, 2001 · N702M · Swrngn SA227AC · Hydraulic System, MainSDR 2002F00095Hydraulic Line · leakingFLT 1322 - ON CLIMB-OUT, BOTH HYD LIGHTS CAME ON AND HYDRAULIC PRESSURE GATE WENT TO '0'. CREW LANDED AFTER DECLARING EMERGENCY AND MANUALLY EXTENDING THE GEAR. SUSPECTED BREAK IN HYDRAULIC LINE CAUSING FLUID LOSS LEADING TO HYDRAULIC PRESSURE LOSS. REPLACEDec 5, 2001 · N702M · Swrngn SA227AC · Hydraulic System, MainSDR 20010212SG007Hydraulic Line · leakingBIL - FLT 2573 - CREW WS ON DOWNWIND LEG WHEN THE HYDRAULIC PRESSURE LIGHTS STARTED COMING ON INTERMITTENTLY. AFTR FLAPS WERE SELECTED TO 1/2 AND WENT TO THAT SETTING, THE GEAR WOULD NOT INDICATE DOWN AND LOCKED WHEN GEAR DOWN WAS SELECTED. CREW FOLLOWED GEAJan 19, 2001 · N702M · Swrngn SA227AC · Hydraulic System, MainSDR 20010112SG027Indicator · faultyFLT 1318 - DFW - GEAR WAS EXTENDED FOR LANDING AT ELD. THE NLG GREEN DOWN LIGHT DIDN''T COME ON. BULBS AND LIGHT MODULES WERE SWAPPED AND LIGHT DIDN''T COME ON. CREW ELECTED TO RETURN TO DFW. THE CREW GOT THE NLG INDICATOR LIGHT TO COME ON WHLE EN ROUTE TONov 6, 2000 · N702M · Swrngn SA227AC · Instrument PanelSDR 20010112SG028Engine · deterioratedFLT 2570 - BIL - LEFT ENGINE TORQUE DROPPED 15 PERCENT DURING TAEOFF ROLL. MAINTENANCE VERIFIED LOW TORQUE DURING ENGINE RUNS. HOT SECTION DETERIORATION IS SUSPECTED. HSI HAD 3184.7 HOURS, DUE IN 415.3. ENGINE WAS CHANGED. (M)Oct 1, 2000 · N702M · Swrngn SA227AC · Turbine Engine Compressor SectionSDR 20010112SG030Wire · damagedFLT 2584 - BIL - CREW NOTICED CABIN DOOR WARNING LIGHT CAME ON AT APPROX 5.7 TO 6.0 CABIN PRESSURE PSID. INTERMITTENT WIRING PROBLEM. REPLACED WIRING FROM DOOR TO ANNUNCIATOR PANEL. WIRE 3901-22 FROM UPPER CABIN DOOR SWITCH TO FORWARD OF CONNECTOR P22 AT ANSep 19, 2000 · N702M · Swrngn SA227AC · Passenger/Crew DoorsSDR 20010103AP006Wire · misinstalledOLF - FLT 2571 - CABIN DOOR WARNING LIGHT CAME ON ABOVE 10,000 FT OR WHEN CABIN PRESS AS ABOVE 4.5 PSID. INTERMITTENT WIRING PROBLEM. ANNUNCIATOR PNL WAS CHANGED, OPS CHECK UNSATISFACTORY. REPLACED ALL SIX REMAINING MICROSWITCHES AND ASSOCIATED WIRING FOR ASep 6, 2000 · N702M · Swrngn SA227AC · Door System WiringSDR BSAA200000026Diode · failedCABIN DOOR WARNING LIGHT CAME ON ABOVE 10,000 FEET OR WHEN THE CABIN PRESSURIZATION WAS ABOVE 4.5 PSID. MAINTENANCE TRACKED TROUBLE TO 4 BAD DIODES IN THE RL-5 AND RL-6 CVR RELAYS. PART OF THE CVR CIRCUITRY IS SHARED WITH THE DOOR WARNING CIRCUITRY. THE CVRSep 6, 2000 · N702M · Swrngn SA227AC · Data Recorders (Flight/Maintenance)SDR 20001011AP007Clamp · looseGTF - FLT 2550 - LEFT WING OVERHEAT LIGHT CAME ON FLASHING DURING CLIMB-OUT. FLASHING IS 250 CELSIUS SENSOR. CREW FOLLOWED EMERGENCY PROCEDURES, SHUT OFF LEFT GEN AND LEFT BLEED AND RETURNED TO BASE. THE FLASHING WING OVERHEAT LIGHT STAYED ON. THE AIRCRAFTMay 8, 2000 · N702M · Swrngn SA227AC · Airfoil Anti/De-ice SystemSDR 20000717AP006Clamp · looseFLT 2550 - GTF - LEFT WING OVERHEAT LIGHT CAME ON FLASHING DURING CLIMB-OUT. FLASHING IS 250 C SENSOR. CREW FOLLOWED EMERGENCY PROCEDURES, SHUT OFF LEFT GEN AND LEFT BLEED AND RETURNED TO BASE. THE FLASHING WING OVERHEAT LIGHT STAYED ON. THE AIRCRAFT WAS SMay 8, 2000 · N702M · Swrngn SA227AC · Airfoil Anti/De-ice SystemSDR 20000717AP005Clamp · looseFLT 2550 - GTF - LEFT WING OVERHEAT LIGHT CAME ON FLASHING DURING CLIMB-OUT. FLASHING IS 250 C SENSOR. CREW FOLLOWED EMERGENCY PROCEDURES, SHUT OFF LEFT GEN AND LEFT BLEED AND RETURNED TO BASE. THE FLASHING WING OVERHEAT LIGHT STAYED ON. THE AIRCRAFT WAS SMay 8, 2000 · N702M · Swrngn SA227AC · Airfoil Anti/De-ice SystemSDR 20000614SH004Clamp · looseGTF - FLT 2550 - LT WING OVERHEAT LIGHT CAME ON FLASHING DURING CLIMBOUT. (FLASHING IS 250 C SENSOR). CREW FOLLOWED EMERGENCY PROCEDURES, SHUT OFF LT GEN AND LT BLEED, RETURNED TO BASE. THE FLASHING WING OVERHEAT LIGHT STAYED ON. ACFT WAS SHUT DOWN ONCE CLMay 8, 2000 · N702M · Swrngn SA227AC · Airfoil Anti/De-ice SystemSDR 20000602SH014Clamp · looseGTF - FLT 2550 - LEFT WING OVERHEAT LIGHT CAME ON FLASHING DURING CLIMB-OUT. (FLASHING IS 250 C SENSOR). CREW FOLLOWED EMERGENCY PROCEDURES, SHUT OFF LEFT GENERATOR AND LEFT BLEED AND RETURNED TO BASE. THE FLASHING WING OVERHEAT LIGHT STAYED ON. AIRCRAFT WMay 8, 2000 · N702M · Swrngn SA227AC · Air Intake Anti/De-Ice SystemSDR 98ZZZX3817Tach Generator · failedHOT/HRO - FLT 1215 - AIRRAFT WAS RELEASED FOR TAKEOFF FORM HOT TO HRO. WHILE EN ROUTE TO HRO, THE LT RPM GAUGE SLOWLY DROPPED TO ZERO WITH NO APPARENT DROP IN ACTUAL ENGINE RPM. THE FLIGHT CREW CONTACTED MAINTENANCE CONTROL WHO INSTRUCTED THEM TO RETURN TO HSep 25, 1998 · N702M · Swrngn SA227AC · Main Rotor Indicating SystemSDR 98ZZZX3818Belt · brokenHOT/HRO - FLT 1217 - AIRCRAFT WAS RELEASED FOR TAKEOFF FROM HOT TO HRO. WHILE IN CLIMB TO HRO, THE CREW HEARD A LOUD BANG FROM THE FRONT OF THE AIRCRAFT. THERE WERE NO INDICATIONS OF ANY PROBLEMS AND ALL SYSTEMS CHECKED GOOD. THE FLIGHT CREW CONTACTED MAINTSep 24, 1998 · N702M · Swrngn SA227AC · Cabin Cooling SystemSDR ASE98001Retract Mech · malfunctionedDFW-ELD - FLT 1253 - AFTER TAKEOFF, WHEN GEAR WAS SELECTED UP, GEAR FAILED TO RETRACT. CONTINUED CLIMB TO SAFE LEVEL AND COMPLETED CHECKLIST, CONTACTED ATC FOR CLEARANCE TO RETURN TO DFW AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND FOUND EMERGENCYJan 2, 1998 · N702M · Swrngn SA227AC · Landing Gear Retraction/Extension SystemSDR 98ZZZM108'X' Screw · out of adjustDFW - FLT 1231 - BOTH ENGINES REPORTED LOW TORQUE DURING TAKEOFF ROLL, LEFT TORQUE 40 PERCENT, RIGHT TORQUE 80 PERCENT. TAKEOFF ABORTED. AIRCRAFT RETURNED TO GATE AND MAINTENANCE PROCEEDED TO INVESTIGATE. MAINTENANCE GROUND RUNS CONFIRMED LOW TORQUE ASSOCIANov 24, 1997 · N702M · Swrngn SA227AC · Fuel Controlling SystemSDR 98ZZZM107'X' Screw · out of adjustDFW - FLT 1231 - LEFT ENGINE READS 80 PERCENT TORQUE AND RIGHT ENGINE READS 95 PERCENT TORQUE AT 100 PERCENT RPM IN FLIGHT. EGT 620 DEGREES. AIRCRAFT RETURNED TO DFW. MAINTENANCE PERFORMED GROUND RUNS IAW SA227 MM AND GARRETT MM 71-00-00. COULD NOT DUPLICATNov 23, 1997 · N702M · Swrngn SA227AC · Fuel Controlling SystemSDR COMA9720010Control Rod · creasedDURING COMPLIANCE OF A.D. 97-02-02 PER S/B 227-27-041, THE ELEVATOR CONTROL ROD, BETWEEN CONTROL COLUMN AND WALKING BEAM, ROD END BEARING RETAINER/DUST COVER WAS FOUND CREASED. THE ROD END WAS REPLACED WITH A NEW PART.Feb 7, 1997 · N702M · Swrngn SA227AC · Elevator Control SystemSDR COMA9720009Control Rod · creasedDURING COMPLIANCE OF A.D. 97-02-02 PER S/B 227-27-041, THE ELEVATOR CONTROL ROD, BETWEEN CONTROL COLUMN AND WALKING BEAM, ROD END BEARING RETAINER/DUST COVER WAS FOUND CREASED. THE ROD END WAS REPLACED WITH A NEW PART.Feb 7, 1997 · N702M · Swrngn SA227AC · Elevator Control SystemSDR COMA9720008Bearing · wornDURING COMPLIANCE OF A.D. 97-02-02 PER S/B 227-27-041, THE COPILOT'S CONTROL COLUMN ROLLER BEARING FAILED THE TORQUE CHECK. THE BEARING AND THE DOUBLER IT IS ATTACHED TO WERE REPLACED.Feb 7, 1997 · N702M · Swrngn SA227AC · Control Column SectionSDR COMA9720007Bearing · wornDURING COMPLIANCE OF A.D.97-02-02 PER S/B 227-27-041, THE PILOT'S CONTROL COLUMN ROLLER BEARING FAILED THE TORQUE CHECK. THE BEARING AND THE DOUBLER IT IS ATTACHED TO WERE REPLACED.Feb 7, 1997 · N702M · Swrngn SA227AC · Control Column SectionSDR COMA9720006Torque Tube · corrodedDURING COMPLIANCE OF AD 96-21-05, THE RT ELEVATOR TORQUE TUBE WAS FOUND TO HAVE INTERNAL CORROSION BEYOND ACCEPTABLE LIMITS. THE TORQUE TUBE WAS REPLACED WITH A NEW PART.Jan 28, 1997 · N702M · Swrngn SA227AC · Elevator Control SystemSDR COMA9720005Torque Tube · corrodedDURING COMPLIANCE OF AD 96-21-05, THE LT ELEVATOR TORQUE TUBE WAS FOUND TO HAVE INTERNAL CORROSION BEYOND ACCEPTABLE LIMITS. THE TORQUE TUBE WAS REPLACED WITH A NEW PART.Jan 28, 1997 · N702M · Swrngn SA227AC · Elevator Control SystemSDR COMA9620016Fuel Nozzles · malfunctionedLEFT ENGINE DOES NOT ACHIEVE REQUIRED TORQUE FOR TAKEOFF. REPLACED THE ENGINE FUEL NOZZLES.Sep 17, 1996 · N702M · Swrngn SA227AC · Fuel Injector NozzleSDR COMA9620012Downlock Switch · failedTHE RIGHT MLG WOULD NOT INDICATE DOWN AND LOCKED UNTIL CYCLED 3 TIMES. REPLACED THE RIGHT MLG OUTBOARD DOWNLOCK SWITCH.Jul 12, 1996 · N702M · Swrngn SA227AC · Landing Gear Position and WarningSDR COMA9620009Propeller · leakingOIL IS DRIPPING FROM THE LEFT ENGINE PROPELLER. REPLACED PROPELLER.Jun 27, 1996 · N702M · Swrngn SA227AC · Propeller AssemblySDR COMA9620003Egt Compensator · out of adjustRT ENGINE TORQUE ROLLBACK FROM 87 PERCENT TO 82 PERCENT DURING TAKEOFF. RECALIBRATED THE EGT COMPENSATOR.Feb 29, 1996 · N702M · Swrngn SA227AC · Engine EGT/TIT Indicating SystemSDR COM20381Wheel Half · crackedRAMP AGENT NOTICED A PART 0F THE OTBD WHEEL HALF CAME APART, WHILE THE AIRCRFT WAS TAXIING INTO GATE AREA. REMOVED WHEEL S/N FEB88-192 AND TOOK IT OUT OF SERVICE. SENT TO CVG WHEEL SHOP.Jun 29, 1995 · N702M · Swrngn SA227AC · Wheel/Ski/FloatSDR COM20380Tube Assy · brokenHYDRAULIC LEAK LT MLG AREA. REPLACED BROKEN FLAP HYDRAULIC LINE ASSY.Jun 27, 1995 · N702M · Swrngn SA227AC · Hydraulic System, MainSDR COM20368Sas Control · defectiveSAS ARM INDICATOR REMAINED ON ABOVE 145 KNOTS. REPLACED THE SAS CONTROL BOX.May 15, 1995 · N702M · Swrngn SA227AC · Stall Warning SystemSDR COM20367Attitude Gyro · defectiveCOPILOTS ATTITUDE INDICATOR CIRCUIT BREAKER TRIPPED, WILL NOT RESET. REPLACED COPILOTS ATTITUDE INDICATOR.Apr 30, 1995 · N702M · Swrngn SA227AC · Attitude Gyro and Indicating SystemSDR COM20359Doubler · crackedFOUND PAX DOOR UPPER FORWARD CORNER FRAME DOUBLER TO BE CRACKED. FURTHER INSPECTION REVEALED UPPER FORWARD CORNER FRAME ALSO TO BE CRACKED. REPLACED PARTS WITH SERVICEABLE LIKE PARTS AND RETURNED TO SERVICE. CRACKS ARE AT THE APEX OF THE RADIUS ON THE FRAMEMar 11, 1995 · N702M · Swrngn SA227AC · Passenger/Crew DoorsSDR COM20358Frame · crackedFOUND PASSENGER DOOR UPPER FORWARD CORNER FRAME TO BE CRACKED. FIRST NOTICED CORNER DOUBLER (COVER) TO BE CRACKED. WHEN DOUBLER WAS REMOVED FOUND FRAME TO ALSO BE CRACKED. BOTH PARTS CRACKED AT APEX OF CORNER RADIUS. INSTALLED SERVICEABLE PARTS AND RETURNEMar 11, 1995 · N702M · Swrngn SA227AC · Passenger/Crew Doors
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