# Service difficulty reports: N253GL A list on [N253GL](https://openairdocs.org/aircraft/N253GL.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 60 reports - [SDR GLBA2015021700499](https://openairdocs.org/sdr/GLBA2015021700499.md): Circuit Board · failed · Feb 15, 2015 · N253GL · Beech 1900D · Interphone/Passenger Announcement (PA) System > THE 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. REPLAC - [SDR GLBA2014110500477](https://openairdocs.org/sdr/GLBA2014110500477.md): Stringer · corroded · Dec 4, 2014 · N253GL · Beech 1900D · Fuselage Main, Longeron/Stringer > DURING 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 GLBA2014110500476](https://openairdocs.org/sdr/GLBA2014110500476.md): Stringer · corroded · Dec 4, 2014 · N253GL · Beech 1900D · Fuselage Main, Longeron/Stringer > DURING 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 GLBA2014110500475](https://openairdocs.org/sdr/GLBA2014110500475.md): Stringer · corroded · Dec 4, 2014 · N253GL · Beech 1900D · Fuselage Main, Longeron/Stringer > DURING 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 GLBA2014120100472](https://openairdocs.org/sdr/GLBA2014120100472.md): Skin · corroded · Dec 1, 2014 · N253GL · Beech 1900D · Fuselage Main, Plate/Skin > DURING 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 GLBA2014120100471](https://openairdocs.org/sdr/GLBA2014120100471.md): Skin · corroded · Dec 1, 2014 · N253GL · Beech 1900D · Fuselage Main, Plate/Skin > MAJOR 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 14-1900-53 - [SDR GLBA2013101400339](https://openairdocs.org/sdr/GLBA2013101400339.md): Engine · making metal · Oct 13, 2013 · N253GL · Beech 1900D · Engine (Turbine/Turboprop) > DURING 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 DAMA - [SDR GLBA2013100800338](https://openairdocs.org/sdr/GLBA2013100800338.md): Propeller · making metal · Oct 7, 2013 · N253GL · Beech 1900D · Propeller Assembly > PILOT 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 A - [SDR GLBA2013100800336](https://openairdocs.org/sdr/GLBA2013100800336.md): Bulb · inoperative · Oct 7, 2013 · N253GL · Beech 1900D · Emergency Lighting > PILOT REPORTED THAT THE EMERGENCY LIGHT AT ROW 6 IS INOPERAITVE. MAINTENANCE REPLACED BULB, OPS CHECKED GOOD. - [SDR GLBA201310080336](https://openairdocs.org/sdr/GLBA201310080336.md): Propeller · malfunctioned · Oct 7, 2013 · N253GL · Beech 1900D · Propeller Feathering/Reversing > PILOT 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 +-25RPM - [SDR GLBA2013071800274](https://openairdocs.org/sdr/GLBA2013071800274.md): Skin · leaking · Jul 18, 2013 · N253GL · Beech 1900D · Wing, Plate/Skin > DURING 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 GLBA2012112900123](https://openairdocs.org/sdr/GLBA2012112900123.md): Spar Cap · cracked · Nov 29, 2012 · N253GL · Beech 1900D · Vertical Stabilizer, Spar/Rib > DURING 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 GLBA2012112900122](https://openairdocs.org/sdr/GLBA2012112900122.md): Spar Cap · cracked · Nov 29, 2012 · N253GL · Beech 1900D · Vertical Stabilizer, Spar/Rib > DURING 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 GLBA2012101500078](https://openairdocs.org/sdr/GLBA2012101500078.md): Connector · unsecure · Oct 14, 2012 · N253GL · Beech 1900D · Landing Gear System Wiring > PILOT 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 GLBA201206261](https://openairdocs.org/sdr/GLBA201206261.md): Door · unlatched · Jun 25, 2012 · N253GL · Beech 1900D · Emergency Exits > EMERGENCY EXIT AT SEAT 6A UNLATCHED. MX REMOVED, INSPECTED AND RESECURED EXIT DOOR IAW BMM 52-20-00, OK FOR SERVICE. - [SDR GLBA2012061803](https://openairdocs.org/sdr/GLBA2012061803.md): Web · cracked · Jun 9, 2012 · N253GL · Beech 1900D · Horizontal Stabilizer Structure > DURING 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 REPAIR - [SDR GLBA20111025G](https://openairdocs.org/sdr/GLBA20111025G.md): Ventral Fin · debonded · Oct 25, 2011 · N253GL · Beech 1900D · Ventral Structure > DURING 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 GLBA20111024H](https://openairdocs.org/sdr/GLBA20111024H.md): Frame · cracked · Oct 24, 2011 · N253GL · Beech 1900D · Fuselage Main, Frame > MAJOR 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 IN - [SDR GLBA20111024G](https://openairdocs.org/sdr/GLBA20111024G.md): Frame · cracked · Oct 24, 2011 · N253GL · Beech 1900D · Fuselage Main, Frame > MAJOR 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 RI - [SDR GLBA20110928F](https://openairdocs.org/sdr/GLBA20110928F.md): Efis · inoperative · Sep 27, 2011 · N253GL · Beech 1900D · Integrated Flight System > PILOT 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 GLBA20110912F](https://openairdocs.org/sdr/GLBA20110912F.md): Solenoid · dirty · Sep 9, 2011 · N253GL · Beech 1900D · Propeller Feathering/Reversing > PILOT 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 GLBA20110630N](https://openairdocs.org/sdr/GLBA20110630N.md): Cover · torn · Jun 28, 2011 · N253GL · Beech 1900D · Passenger/Crew Doors > "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 GLBA20110322F](https://openairdocs.org/sdr/GLBA20110322F.md): Skin · corroded · Mar 21, 2011 · N253GL · Beech 1900D · Fuselage Main, Plate/Skin > MAJOR 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 ARE - [SDR GLBA20100525F](https://openairdocs.org/sdr/GLBA20100525F.md): Stringer · cracked · May 25, 2010 · N253GL · Beech 1900D · Fuselage Main, Longeron/Stringer > MAJOR 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 GLBA20100519H](https://openairdocs.org/sdr/GLBA20100519H.md): Skin · cracked · May 25, 2010 · N253GL · Beech 1900D · Fuselage Main, Plate/Skin > MAJOR 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. MATER - [SDR GLBA20100521G](https://openairdocs.org/sdr/GLBA20100521G.md): Stringer · cracked · May 20, 2010 · N253GL · Beech 1900D · Fuselage Main, Longeron/Stringer > MAJOR 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 INCL - [SDR GLBA20100521F](https://openairdocs.org/sdr/GLBA20100521F.md): Frame · cracked · May 20, 2010 · N253GL · Beech 1900D · Fuselage Main, Frame > DURING 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 ORDER - [SDR GLBA20100519J](https://openairdocs.org/sdr/GLBA20100519J.md): Skin · cracked · May 19, 2010 · N253GL · Beech 1900D · Fuselage Main, Plate/Skin > MAJOR 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. MATE - [SDR GLBA201001111](https://openairdocs.org/sdr/GLBA201001111.md): Fcu · out of adjust · Jan 11, 2010 · N253GL · Beech 1900D · Fuel Control/Turbine Engines > RT 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 GLBA200911301](https://openairdocs.org/sdr/GLBA200911301.md): Linkage · out of adjust · Nov 28, 2009 · N253GL · Beech 1900D · Propeller Feathering/Reversing > RT 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 O - [SDR GLBA200906231](https://openairdocs.org/sdr/GLBA200906231.md): Hose · damaged · Jun 22, 2009 · N253GL · Beech 1900D · Hydraulic System, Main > PILOTS 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 GLBA20090414A](https://openairdocs.org/sdr/GLBA20090414A.md): Connector · loose · Apr 14, 2009 · N253GL · Beech 1900D · Propeller/Propulsor System Wiring > LT 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 GLBA20090305A](https://openairdocs.org/sdr/GLBA20090305A.md): Landing Gear · malfunctioned · Mar 5, 2009 · N253GL · Beech 1900D · Landing Gear Retraction/Extension System > FLIGHT 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 GLBA20090212AA](https://openairdocs.org/sdr/GLBA20090212AA.md): Rib · worn · Feb 12, 2009 · N253GL · Beech 1900D · Nacelle/Pylon, Frame/Spar/Rib > MAJOR 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 APPROXIMAT - [SDR GLBA200901121](https://openairdocs.org/sdr/GLBA200901121.md): Switch · out of adjust · Jan 9, 2009 · N253GL · Beech 1900D · Propeller Feathering/Reversing > SIGNIFICANT 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 GLBA20060957](https://openairdocs.org/sdr/GLBA20060957.md): Blade · damaged · Jun 20, 2007 · N253GL · Beech 1900D · Fuselage Main, Plate/Skin > EXTENDED 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 RE - [SDR GLBA20060734](https://openairdocs.org/sdr/GLBA20060734.md): Structure · corroded · Apr 18, 2006 · N253GL · Beech 1900D · Fuselage Structure (General) > CORROSION FOUND DURING STRUCTURAL INSPECTION, STA 220-288 AND STR 13L-16L, PENDING REPAIR. - [SDR 20030789](https://openairdocs.org/sdr/20030789.md): Spar · cracked · Feb 5, 2005 · N253GL · Beech 1900D · Horizontal Stabilizer, Spar/Rib > DURING 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 20030782](https://openairdocs.org/sdr/20030782.md): Truss · cracked · Jan 15, 2005 · N253GL · Beech 1900D · Engine Mount Section > WHILE 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 CHAF - [SDR 20030778](https://openairdocs.org/sdr/20030778.md): Axle · cracked · Dec 30, 2004 · N253GL · Beech 1900D · Main Landing Gear Strut/Axle/Truck > RT MAIN GEAR LOWER STRUT AXLE ASSY LUG HAS (2) CRACKS APPROX.05 AND.06 LONG WHERE LOWER TORQUE KNEE ATTACHES TO LUG. - [SDR GLBA20030739](https://openairdocs.org/sdr/GLBA20030739.md): Blower · binding · Oct 21, 2004 · N253GL · Beech 1900D · Air Distribution Fan > AIRCRAFT 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 RE - [SDR GLBA20030654](https://openairdocs.org/sdr/GLBA20030654.md): Structure · corroded · Jun 24, 2004 · N253GL · Beech 1900D · Passenger/Crew Doors > CABIN DOOR CORROSION, REPAIRED DOOR. - [SDR GLBA20030645](https://openairdocs.org/sdr/GLBA20030645.md): Circuit Breaker · tripped · Jun 20, 2004 · N253GL · Beech 1900D · Landing Gear System Wiring > LANDING GEAR RELAY CB POPS IN CRUISE, RESEATED P552 ON PCB A316. - [SDR GLBA20030637](https://openairdocs.org/sdr/GLBA20030637.md): Landing Gear · malfunctioned · Jun 10, 2004 · N253GL · Beech 1900D · Main Landing Gear > LEFT MLG WILL NOT STAY RETRACTED, NFF OPS CHECK GOOD. - [SDR GLBA20030606](https://openairdocs.org/sdr/GLBA20030606.md): Transducer · malfunctioned · Apr 8, 2004 · N253GL · Beech 1900D · Engine Oil Pressure > LT ENG OIL PRESSURE INDICATOR FLUCUATING OFF SCALE, R&R LT OIL PRESSURE TRANSDUCER - [SDR GLBA20030514](https://openairdocs.org/sdr/GLBA20030514.md): Wire · chafed · Dec 5, 2003 · N253GL · Beech 1900D · Light System Wiring > WHEN TURNING ON TAXI LIGHT THERE WAS SPARK AND SMOKE, REPAIRED CHAFED WIRE REF 33-40-00. OPS CK GOOD. - [SDR GLBA2003151](https://openairdocs.org/sdr/GLBA2003151.md): Flap · stuck · Nov 19, 2003 · N253GL · Beech 1900D · Trailing Edge Flap Control System > FLAPS STUCK AT 17 DEGREES. ADJUSTED FLAP SAFETY SWITCH B27RW82255518T OPS CK GOOD - [SDR GLBA2003111](https://openairdocs.org/sdr/GLBA2003111.md): Receiver · incorrect · Aug 2, 2003 · N253GL · Beech 1900D · Navigation System > NAV NEEDLE SHOWED 15 DEG ERROR BETWEEN EACH OTHER. REMOVED AND REPLACED NR 2 NAV RECEIVER. - [SDR GLBA2003039](https://openairdocs.org/sdr/GLBA2003039.md): Connector · loose · Mar 25, 2003 · N253GL · Beech 1900D · Attitude and Direction Data System > NR 1 NAV FAILED. TIGHTENED CONNECTION ON SPLITTER, OPS CHECK GOOD. - [SDR GLBA2003038](https://openairdocs.org/sdr/GLBA2003038.md): Receiver · failed · Mar 24, 2003 · N253GL · Beech 1900D · Visual Omnirange (VOR) System > NR 1 NAV FAILED. REMOVED AND REPLACED NR 1 NAV VIR32. Next page: https://openairdocs.org/aircraft/N253GL/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 n_number = 'N253GL' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N253GL/reports --- 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.