N253GL
Service difficulty reports · 60
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 = 'N253GL' AND registry_match = 'registration' 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.
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 = 'N253GL' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR GLBA2015021700499Circuit Board · failedTHE HAND MIC SMELLED HOT & STARTED SENDING STATIC TO THE INTERCOM SYS. PLUGGED INTO INTO FIRST OFFICER`S JACK. REPLACED PC BOARD PN ON & OFF 130-340097-1 IN THE AUDIO CONTROL PANEL, SN OFF UNKNOWN, SN ON 504-8-95. WORK ACCOMPLISHED IAW AIM 10-24-01. REPLACSDR GLBA2014110500477Stringer · corrodedDURING A SCHEDULED INSPECTION MAINTENANCE FOUND STRINGER 14L CORRODED BS 228.25, DAMAGED AREA APPROXIMATELY 2 INCHES BY 2 INCHES, DAMAGE FOUND UNDER FRONT EDGE OF PREVIOUS SKIN REPAIR. REPAIRED IAW EO 14-1900-53-052. MAJOR REPAIR .SDR GLBA2014110500476Stringer · corrodedDURING A SCHEDULED INSPECTION FOUND STRINGER 15L CORRODED BS 228.25, DAMAGED AREA APPROXIMATELY 2 INCHES BY 2 INCHES, DAMAGE FOUND ON FRONT EDGE OF PREVIOUS SKIN REPAIR. REPAIRED IAW EO 14-1900-53-051. MAJOR REPAIR.SDR GLBA2014110500475Stringer · corrodedDURING A SCHEDULED INSPECTION FOUND CORROSION ON STRINGER 16 BS 213.25 AREA APPROX 3 INCHES BY 2 INCHES, DAMAGE FOUND UNDER & BETWEEN TWO PREVIOUS SKIN REPAIRS. REPAIRED IAW EO 14-1900-53-050. MAJOR REPAIR.SDR GLBA2014120100472Skin · corrodedDURING A SCHEDULED INSPECTION, FOUND BELLY SKIN CORROSION & A CRACK AT BS 228.25 BETWEEN STRINGER 15 - 16R, .3 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-048. MAJOR REPAIR.SDR GLBA2014120100471Skin · corrodedMAJOR REPAIR DURING A SCHEDULED INSPECTION FOUND A CORRODED AREA APPROX 4 INCHES BY 3 INCHES AT FS 213.25 & STRINGER 16. DURING A SCHEDULED INSPECTION MX FOUND A CORRODED AREA APPROX 4 INCHES BY 3 INCHES AT FS 213.25 & STRINGER 16. REPAIRED IAW EO 14-1900-53SDR GLBA2013101400339Engine · making metalDURING DESCENT, TORQUE ON NR 2 ENGINE DECREASED TO APPROX 400 LBS AND ITT INCREASED TO ABOVE 800 CELSIUS F/O SAW FLAMES COMING OUT BOTH EXHAUST STACKS ON NR 2 ENGINE. SECURED ENGINE USING APPROPRIATE CHECKLISTS. MAINTENANCE FOUND PROPELLER STIFF. FOUND DAMASDR GLBA2013100800338Propeller · making metalPILOT REPORTED THAT THE RT PROP FEATHERED ON FINAL, BEFORE PROPS PUSHED FWD, PROPS AT 1550 TORQUE, DID NOT SECURE ENGINE, PULLED POWER BACK TO IDLE, AS 180KTS, FLAPS 17, DECLARED AN EMERGENCY, SECURED ENGINE ONCE ON GROUND. MAINTENANCE FOUND PROPELLER STIFF ASDR GLBA2013100800336Bulb · inoperativePILOT REPORTED THAT THE EMERGENCY LIGHT AT ROW 6 IS INOPERAITVE. MAINTENANCE REPLACED BULB, OPS CHECKED GOOD.SDR GLBA201310080336Propeller · malfunctionedPILOT REPORTED THAT ON SHORT FINAL THE RT PROP FEATHERED, BEFORE PROPS PUSHED FWD, PROPS AT 1550 TQ 1500, DID NOT SECURE ENG, PULLED PWR BACK TO IDLE, A/S 180 KTS, FLAPS 17, DECLARED EMERGENCY, SECURED ENG ON GROUND, 10 MINS FROM DEPT HAD TQ/PROP FLUX +-25RPMSDR GLBA2013071800274Skin · leakingDURING A SCHEDULED ROUTINE INSPECTION, FOUND A PREVIOUS REPAIR LEAKING FUEL ON THE LT OTBD WING L/E AT WS 192.51 TO 198. REPAIRED IAW EO 13-1900-57-013.SDR GLBA2012112900123Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND CRACK ON THE LT VERTICAL STAB FWD SPAR CAP ANGLE AT VSS 84.10 AND 20 PERCENT CHORD MOVING DOWNWARD, 2.5" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-062. MAJOR REPAIR.SDR GLBA2012112900122Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK ON THE RT VERTICAL STAB FWD SPAR CAP ANGLE AT THE 2ND RIVET FROM THE TOP AT FSS 84.10 AND 20 PERCENT CHORD, .375" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-063. MAJOR REPAIR.SDR GLBA2012101500078Connector · unsecurePILOT REPORTED THAT WHILE EXTENDING THE GEAR, LANDING GEAR HAD NO GREEN LIGHTS, MANUALLY EXTENDED GEAR, STILL NO GREEN INDICATION, DECLARED AN EMERGENCY AND LANDED WITH NO INCIDENT. MX RESEATED THE DOWNLOAD/SAFETY SWITCH CONNECTOR PLUG, OPS CK GOOD.SDR GLBA201206261Door · unlatchedEMERGENCY EXIT AT SEAT 6A UNLATCHED. MX REMOVED, INSPECTED AND RESECURED EXIT DOOR IAW BMM 52-20-00, OK FOR SERVICE.SDR GLBA2012061803Web · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE HORIZ STAB AFT WEB AT HSS 0.00, 4 CRACKS, 1" IN LENGTH. REPAIRED IAW EO 12-1900-55-015. MAJOR REPAIRSDR GLBA20111025GVentral Fin · debondedDURING A SCHEDULED ROUTINE INSPECTION, FOUND THE LT VENTRAL FIN DEBONDED BETWEEN FS 570 AND FS 605, 9.5" ALONG LWR T/E AND INWARD FROM EDGE 3" ON BOTH INBD & OTBD SKINS. MX REPLACED THE VENTRAL.SDR GLBA20111024HFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP FOUND FUSELAGE FRAME AT FS 509 BETWEEN STRINGER 4L & 5L CRACKED AT CARGO DOOR GAS STRUT MOUNT AREA, (UPPER INBD NUTPLATE), 3 CRACKS ABOUT .5" EACH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSDR GLBA20111024GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP FOUND 3 CRACKS AT FUSELAGE FRAME AT FS 456 BETWEEN STRINGER 3L & 4L AT THE UPPER INBD NUTPLATE ON THE CARGO DOOR GAS STRUT MOUNT AREA, ABOUT .5" LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RISDR GLBA20110928FEfis · inoperativePILOT REPORTED THAT THE EHSI DIMMED ON FINAL AND AN ELECTRICAL ODOR WAS NOTICED. MX REPLACED THE EFIS TUBE IAW BMM 34-52-00, OPS CHECKED GOOD, NO ODOR NOTICED.SDR GLBA20110912FSolenoid · dirtyPILOT REPORTED THAT THE LEFT PROPELLER WENT INTO GROUND IDLE DURING LANDING FLARE, RESULTING IN A STONG YAW TO THE LEFT. MX CLEANED THE NR 1 LOW PITCH SOLENOID, OPS CK GOOD.SDR GLBA20110630NCover · torn"SUP" - SIG EVENT - DURING ROUTINE MX INSP FOUND THE LWR AFT AS DOOR HANDRAIL CABLE COVER TORN. MX R & R LOWER AFT AS DOOR CABLE WITH REF TO D1900MM 52-10-02.SDR GLBA20110322FSkin · corrodedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND CORROSION ON THE BELLY SKIN JUST AFT OF THE ADF ANTENNA MEASURING .75". MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-018. MATERIALS UTILIZED ARESDR GLBA20100525FStringer · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND AT FRAME FS 150 AND STRINGER 9AL AT PASSENGERS DOOR FRAME ANGLE LOWER STRUT MOUNT AFT UPPER SCREWHOLE BRACKET AT NUTPLATE LOCATION. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED SDR GLBA20100519HSkin · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE FOUND BELLY SKIN CRACKED AT FS 303.25 LEFT SIDE, 2.1" IN LENGTH, 2.25" INBOARD FROM SKIN EDGE. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-021. MATERSDR GLBA20100521GStringer · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A CRACK WAS FOUND AT FRAME FS 164 AND STRINGER 9AR AND IS .7" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-024. MATERIALS UTILIZED ARE INCLSDR GLBA20100521FFrame · crackedDURING ROUTINE SCHEDULED MX, A CRACK AT FRAME FS 288 AND STR 4C CUTOUT CRACKED .35" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-020. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDERSDR GLBA20100519JSkin · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE FOUND BELLY SKIN CRACKED AT FS 303.25 RIGHT SIDE, 1.9" IN LENGTH, 2.25" INBOARD FROM SKIN EDGE. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-022. MATESDR GLBA201001111Fcu · out of adjustRT ENGINE AUTOFEATHERED ON APPROACH. MX ADJUSTED THE RT FCU ROD TO SPEED UP THE RT ENGINE TO MATCH THE LT ENG IAW MM 76-10-01. OPS CHECK ON GROUND GOOD. RII INSP FOR FCU RIG COMPLIED WITH IAW TASKCARD 4.3.13. IT WAS SATISFACTORY.SDR GLBA200911301Linkage · out of adjustRT AUTO FEATHER ENGAGED ON APPROACH TO LANDING AT 780 FT AGL AS PWR WAS INCREASED FROM IDLE THROUGH 600LBS OF TORQUE. WHEN THE AUTO FEATHER ENGAGED IT WENT IN AND OUT OF FEATHER SEVERAL TIMES BEFORE MORE PWR WAS APPLIED AND THE AUTO FEATHERING CYCLE STOPPED OSDR GLBA200906231Hose · damagedPILOTS REPORTED THAT AFTER TAKEOFF THE GEAR HANDLE WAS MOVED TO THE UP POSITION AND 3 GREEN LIGHTS EXTINGUISHED AND THE INTRANSIT LIGHTS STAYED ILLUMINATED. PILOTS CONFIRMED GEAR DID NOT COME UP. PILOTS MANUALLY PUMPED THE GEAR DOWN. MX FOUND DAMAGED HOSES SDR GLBA20090414AConnector · looseLT PROP GAUGE READ 2000 RPM AFTER SETTING T/O POWER. MAINTENANCE CLEAND AND RE-SECURED CONNECTOR ON THE INDICATOR. ENGINE RUNS WERE PERFORMED WITH THE PILOTS AND THE OPERATIONAL CHECKS WERE GOOD PER MM 77-10-00.SDR GLBA20090305ALanding Gear · malfunctionedFLIGHT 5158 UPON APPROACH THE PILOTS REPORTED THAT THE RIGHT MAIN LANDING GEAR WOULD NOT EXTEND. PILOTS PERFORMED A MANUAL EXTENSION. MAINTENANCE CLEANED THE RIGHT HAND DOWNLOCK SWITCH AND PERFORMED SIX LANDING GEAR EXTESNIONS AND RETRACTIONS IAW MM 32-30-00. SDR GLBA20090212AARib · wornMAJOR REPAIR - DURING SCHEDULED INSPECTION MAINTENANCE THE LEFT FORWARD INBOARD NACELLE KEEL RIB FLANGE WORN AT THE UPPER CORNER AREA AT APPROXIMATELY BL 91.75. MAINTENANCE REPAIRED THE LT FORWARD INBOARD KEEL RIB FLANGE AT THE UPPER CORNER AREA AT APPROXIMATSDR GLBA200901121Switch · out of adjustSIGNIFICANT EVENT, MAINTENANCE ADJUSTED AUTOFEATHER MICROSWITCH IN PEDESTAL IAW 1900D MM 61-21-02. OPERATIONAL CHECK WAS GOOD. LOTS REPORTED THE RIGHT SIDE AUTOFEATHERED FLIGHT ON FINAL WITH PROPS FULL FORWARD WHEN INCREASING POWER.SDR GLBA20060957Blade · damagedEXTENDED ROLLOUT, UPON LANDING, PILOTS REPORTED THAT DUE TO LANDING ROLLOUT BEYOND THE END OF THE RUNWAY, THE RT PROP NR 2 ENGINE STRUCK A RECTANGULAR BOX. PRELIMINARY DAMAGE INDICATES PROP BLADE DAMAGE AND HOLE IN FUSELAGE. [08-01-07] MX INSTALLED TEMP RESDR GLBA20060734Structure · corrodedCORROSION FOUND DURING STRUCTURAL INSPECTION, STA 220-288 AND STR 13L-16L, PENDING REPAIR.SDR 20030789Spar · crackedDURING ROUTINE STRUCTURAL "I" INSPECTION, FOUR CRACKS WERE IDENTIFIED EMANATING FROM THE DE-ICE HOLE ON THE HORIZONTAL CENTER MAIN SPAR CENTER WEB SKIN APPROX 1" LONG EACH UNDER PANEL 332 ATC. REPAIR WAS MADE AND AIRCRAFT RETURNED TO SERVICE.SDR 20030782Truss · crackedWHILE PERFORMING OTHER NON-RELATED MAINTENANCE, THE LT ENGINE TRUSS WAS DISCOVERED TO BE COMPLETELY CRACKED THRU (360 DEGREES) ON THE LOWER LT TUBE JUST ABOVE THE ATTACH BRACKET FOR THE LOWER ENGINE AIR CAN ASSY, ADJACENT TO THE P3 BLEED LINE. NO OBVIOUS CHAFSDR 20030778Axle · crackedRT MAIN GEAR LOWER STRUT AXLE ASSY LUG HAS (2) CRACKS APPROX .05 AND .06 LONG WHERE LOWER TORQUE KNEE ATTACHES TO LUG.SDR GLBA20030739Blower · bindingAIRCRAFT FLYING LEVEL AT 12,000 FT WHEN FLIGHT CREW NOTICED STRONG ODOR IN COCKPIT. CREW RETURNED TO DEPARTURE AIRPORT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED THE FORWARD VENT BLOWER WAS DEFECTIVE, MAKING GRINDING NOISE AND THE CAUSE OF THE RESDR GLBA20030654Structure · corrodedCABIN DOOR CORROSION, REPAIRED DOOR.SDR GLBA20030645Circuit Breaker · trippedLANDING GEAR RELAY CB POPS IN CRUISE, RESEATED P552 ON PCB A316.SDR GLBA20030637Landing Gear · malfunctionedLEFT MLG WILL NOT STAY RETRACTED, NFF OPS CHECK GOOD.SDR GLBA20030606Transducer · malfunctionedLT ENG OIL PRESSURE INDICATOR FLUCUATING OFF SCALE, R&R LT OIL PRESSURE TRANSDUCERSDR GLBA20030514Wire · chafedWHEN TURNING ON TAXI LIGHT THERE WAS SPARK AND SMOKE, REPAIRED CHAFED WIRE REF 33-40-00. OPS CK GOOD.SDR GLBA2003151Flap · stuckFLAPS STUCK AT 17 DEGREES. ADJUSTED FLAP SAFETY SWITCH B27RW82255518T OPS CK GOODSDR GLBA2003111Receiver · incorrectNAV NEEDLE SHOWED 15 DEG ERROR BETWEEN EACH OTHER. REMOVED AND REPLACED NR 2 NAV RECEIVER.SDR GLBA2003039Connector · looseNR 1 NAV FAILED. TIGHTENED CONNECTION ON SPLITTER, OPS CHECK GOOD.SDR GLBA2003038Receiver · failedNR 1 NAV FAILED. REMOVED AND REPLACED NR 1 NAV VIR32.
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