# Service difficulty reports: N240GL

A list on [N240GL](https://openairdocs.org/aircraft/N240GL.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 · 71 reports

- [SDR GLBA2015012800494](https://openairdocs.org/sdr/GLBA2015012800494.md): Strut · malfunctioned · Jan 26, 2015 · N240GL · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE CABIN DOOR SNUBBER WAS INOPERATIVE. SERVICED THE PAX DOOR STRUT IAW MM 12-10-00. OPERATIONS CHECKED GOOD.
- [SDR GLBA2014090200436](https://openairdocs.org/sdr/GLBA2014090200436.md): Skin · cracked · Sep 2, 2014 · N240GL · Beech 1900D · Wing, Plate/Skin
  > DURING A SCHEDULED INSPECTION MAINTENANCE FOUND CORROSION IN AN AREA OF 4.5 INCHES BY 3.5 INCHES CAUSING A CRACK & BUILDING SKIN & A SHEARED RIVET BEHIND THE LT VORTEX GENERATOR & IN FRONT OF THE FORMER RING CENTERED AT FS 243.25 & WL 85.40. REPAIRED IAW EO 1
- [SDR GLBA2014081200427](https://openairdocs.org/sdr/GLBA2014081200427.md): Turnbuckle · out of adjust · Aug 11, 2014 · N240GL · Beech 1900D · Emergency Exits
  > RIGHT FWD EMER EXIT HANDLE STICKING OUT. ADJUSTED THE DOOR LATCH TURNBUCKLE IAW MM 52-20-00. OPERATIONS CHECKED GOOD.
- [SDR GLBA2014031700403](https://openairdocs.org/sdr/GLBA2014031700403.md): Door Frame · cracked · Mar 15, 2014 · N240GL · Beech 1900D · Fuselage Main, Structure
  > DURING A SCHEDULED INSPECTION MX FOUND LOWER AIRSTAIR DOOR FRAME AFT CRACKED APPROXIMATELY 1/2 INCH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-022.
- [SDR GLBA2014031700402](https://openairdocs.org/sdr/GLBA2014031700402.md): Door Frame · cracked · Mar 15, 2014 · N240GL · Beech 1900D · Fuselage Main, Structure
  > DURING A SCHEDULED INSPECTION MX FOUND FWD FRAME AIRSTAIR DOOR CUTOUT AT FS 150.6 BETWEEN STRINGER 10L & 11L CRACKED, CRACK IS APPROXIMATELY 1/2 INCHES. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-023.
- [SDR GLBA2013101400340](https://openairdocs.org/sdr/GLBA2013101400340.md): Circuit Breaker · failed · Oct 12, 2013 · N240GL · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT THE LT AUTOFEATHER SYS WILL NOT ENGAGE, THE AUTOFEATHER LIGHT IS NOT ILLUMINATED, BUT DOES PRESS TO TEST. MAINTENANCE REPLACED PCB A129, PERFORMED RUN, OPS CK GOOD.
- [SDR GLBA2013081300293](https://openairdocs.org/sdr/GLBA2013081300293.md): Spar Cap · chafed · Aug 13, 2013 · N240GL · Beech 1900D · Wing Spar
  > DURING A SCHEDULED INSP, FOUND CHAFING ON THE AFT SPAR LOWER CAP AT WS 85.50, APPROX.002 DEEP WITH A SMALL NICK IN THE CENTER OF THE CHAFE, NO OTHER DAMAGE IS NOTED, WIDTH OF THE DAMAGE IS 1.125". REPAIRED IAW EO 13-1900-57-015.
- [SDR GLBA2013031300202](https://openairdocs.org/sdr/GLBA2013031300202.md): Longeron · cracked · Mar 12, 2013 · N240GL · Beech 1900D · Fuselage Main, Longeron/Stringer
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK AT FS 107, LT SIDEWALL LONGERON AT FINGER DOUBLER AREA "M" JUNCTION WITH SIDEWALL FRAME, RADIATES UPWARD FROM A FASTENER HOLE AND TERMINATES BELOW LONGERON BEND RADIUS,.4" IN LENGTH. REPAIRED IAW EO 13-1
- [SDR GLBA2013031300206](https://openairdocs.org/sdr/GLBA2013031300206.md): Doubler · cracked · Mar 11, 2013 · N240GL · Beech 1900D · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE LT SIDEWALL FINGER DOUBLER AT FS 107,.25" IN LENGTH. REPAIRED IAW EO 13-1900-53-026. MAJOR REPAIR.
- [SDR GLBA2013031300205](https://openairdocs.org/sdr/GLBA2013031300205.md): Frame · cracked · Mar 11, 2013 · N240GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE FRAME AT FS 177.35 BETWEEN STR 13 - 14L AFT SIDE, 1 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-023. MAJOR REPAIR.
- [SDR GLBA2013031300204](https://openairdocs.org/sdr/GLBA2013031300204.md): Frame · cracked · Mar 11, 2013 · N240GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE LT SIDEWALL AT FS 107 AT THE UPPER END OF THE FRAME AT THE LAST ATTACHING FASTENER AREA,.75" IN LENGTH. REPAIRED IAW EO 13-1900-53-024. MAJOR REPAIR.
- [SDR GLBA2013031300203](https://openairdocs.org/sdr/GLBA2013031300203.md): Frame · cracked · Mar 11, 2013 · N240GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND 2 CRACKS IN THE RT SIDEWALL FRAME AT FS 107 IN THE BEND RADIUS (UPPER END OF FRAME) AND AT UPPER FASTENER AREA, 1.25" IN LENGTH. REPAIRED IAW EO 13-1900-53-025. MAJOR REPAIR.
- [SDR GLBA2013010400170](https://openairdocs.org/sdr/GLBA2013010400170.md): Spar Cap · cracked · Feb 2, 2013 · N240GL · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSP, FOUND A CRACK IN RT FORWARD SPAR CAP ANGLE AT CSS 69.184 AND 20 PERCENT CHORD, 2.5" IN LENGTH. REPAIRED IAW EO 13-1900-55-005. MAJOR REPAIR.
- [SDR GLBA2013010400169](https://openairdocs.org/sdr/GLBA2013010400169.md): Spar Cap · cracked · Feb 2, 2013 · N240GL · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE LT FWD SPAR CAP ANGLE AT CSS 69.184 AND 20 PERCENT CHORD, 1.75" IN LENGTH. REPAIRED IAW EO 13-1900-55-004. MAJOR REPAIR.
- [SDR GLBA2013010400168](https://openairdocs.org/sdr/GLBA2013010400168.md): Skin · damaged · Feb 2, 2013 · N240GL · Beech 1900D · Elevator, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A HOLE IN THE RT ELEVATOR ON THE T/E RIGHT ABOVE THE OTBD STATIC WICK, APPROX 0.3125 INCHES DEEP BY.25 INCHES WIDE. REPAIRED IAW EO 13-1900-27-002. MAJOR REPAIR.
- [SDR GLBA2012122400139](https://openairdocs.org/sdr/GLBA2012122400139.md): Bulb · inoperative · Dec 23, 2012 · N240GL · Beech 1900D · Emergency Lighting
  > PILOT REPORTED THAT THE CAPT'S INSTRUMENT EMERGENCY LIGHTS WILL NOT TURN ON. MX REPLACED THE BULB, OPS CHECKED GOOD.
- [SDR GLBA2012102200085](https://openairdocs.org/sdr/GLBA2012102200085.md): Skin · corroded · Oct 22, 2012 · N240GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND CORROSION ON THE BELLY SKIN AT FS 243 BETWEEN STRINGERS 16 & 15R, VISIBLE CORROSION IS APPROX 1 BY 1 INCH. REPAIRED IAW EO 11-1900-53-055. MAJOR REPAIR.
- [SDR GLBA2012102200084](https://openairdocs.org/sdr/GLBA2012102200084.md): Skin · corroded · Oct 22, 2012 · N240GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND CORROSION ON THE BELLY SKIN AT FS 213, LOWER FUSELAGE. REPAIRED IAW EO 11-1900-53-056. MAJOR REPAIR.
- [SDR GLBA2012082800040](https://openairdocs.org/sdr/GLBA2012082800040.md): Bulb · inoperative · Aug 26, 2012 · N240GL · Beech 1900D · Landing Gear Position and Warning
  > PILOT REPORTED THAT THEY HAD A GEAR INDICATION PROBLEM, SWAPPED ANNC'S AND IT WORKED, ATC DECLARED EMERGENCY, MX REPLACED THE BULB, OPS CK GOOD.
- [SDR GLBA2012072300017](https://openairdocs.org/sdr/GLBA2012072300017.md): Spar · cracked · Jul 21, 2012 · N240GL · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND 4 CRACKS AROUND THE HORZ STAB AFT SPAR WEB AT HSS 0.00, 1.625" IN LENGTH. REPAIRED IAW EO 12-1900-55-019. MAJOR REPAIR
- [SDR GLBA2012052901](https://openairdocs.org/sdr/GLBA2012052901.md): Spar · chafed · May 26, 2012 · N240GL · Beech 1900D · Wing Spar
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND THE LT WING MAIN SPAR CHAFED AT INBD EDGE OF LOWER ACM PANEL. REPAIRED THE AFFECTED AREA IAW EO 12-1900-57-003.
- [SDR GLBA20111116F](https://openairdocs.org/sdr/GLBA20111116F.md): Placard · missing · Nov 14, 2011 · N240GL · Beech 1900D · Placards and Markings
  > THE SEAT BACK UPRIGHT FOR TAKEOFF AND LANDING, & THE EMERGENCY EVACUATION PLACARD IS MISSING FROM SEAT 5A. MX REPLACED THE PLACARD IAW AIM 5-16-0.
- [SDR GLBA20111104G](https://openairdocs.org/sdr/GLBA20111104G.md): Frame · cracked · Nov 4, 2011 · N240GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK AT THE CARGO DOOR AFT FUSELAGE FRAME OF FS 509 AT THE GAS STRUT MOUNT BETWEEN STRINGERS 4L & 5L,.5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-
- [SDR GLBA20111104F](https://openairdocs.org/sdr/GLBA20111104F.md): Frame · cracked · Nov 4, 2011 · N240GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND 2 CRACKS IN CARGO BAY FRAME FS 456 AT GAS STRUT MOUNT, 1" AND 2" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-062. MATERIALS UTILIZED ARE INCLUDED IN THE
- [SDR GLBA20110920F](https://openairdocs.org/sdr/GLBA20110920F.md): B-Nut · loose · Sep 19, 2011 · N240GL · Beech 1900D · Aircraft Fuel Distribution System
  > "SUP" - SIG EVENT - PILOT REPORTED THAT THERE IS A FUEL LEAK FROM THE BOTTOM OF THE LT ENGINE COWLING. MX TIGHTENED A B-NUT ON THE FUEL PUMP IAW BMM 73-12-00, OPS CK GOOD.
- [SDR GLBA201109071](https://openairdocs.org/sdr/GLBA201109071.md): Bulb · inoperative · Sep 7, 2011 · N240GL · Beech 1900D · Emergency Lighting
  > INSTRUMENT EMERGENCY LIGHT INOPERATIVE. MX REPLACED THE BULB BURNED OUT, IAW BMM 33-10-04, OPS CHECKED GOOD.
- [SDR GLBA20110818J](https://openairdocs.org/sdr/GLBA20110818J.md): Handle · unsecure · Aug 17, 2011 · N240GL · Beech 1900D · Emergency Exits
  > PILOT REPORTED THAT THE RT FWD EMERGENCY DOOR HANDLE APPEARS TO BE HALF WAY OPEN. MX RESECURED THE EXIT DOOR IAW BMM 52-20-00, SEC 1 A-B, OK FOR SERVICE.
- [SDR GLBA20110818H](https://openairdocs.org/sdr/GLBA20110818H.md): Handle · unsecure · Aug 17, 2011 · N240GL · Beech 1900D · Emergency Exits
  > PILOT REPORTED THAT THE RT FWD EMERGENCY DOOR HANDLE APPEARS TO BE HALF WAY OPEN. MX RESECURED THE EXIT DOOR IAW BMM 52-20-00, SEC 1 A-B, OK FOR SERVICE.
- [SDR GLBA20110721G](https://openairdocs.org/sdr/GLBA20110721G.md): Cable · broken · Jul 20, 2011 · N240GL · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE CABIN DOOR SNUBBER CABLE BROKE. MX REPLACED THE SNUBBER CABLE IAW BMM 52-10-01, OPS CHECKED GOOD.
- [SDR GLBA20110711L](https://openairdocs.org/sdr/GLBA20110711L.md): Connector · loose · Jul 10, 2011 · N240GL · Beech 1900D · Fire Protection System Wiring
  > PILOT REPORTED THAT THE FIRE EXTINGUISHER TEST A WAS INOP, DISC ANNUNCIATOR ON BOTH SIDES DID NOT ILLUMINATE WHEN TESTED. MX FOUND A LOOSE CONNECTION ON THE A 257A, SECURED CONNECTOR REF AIM 10-74-1, PERFORMED TEST A, ALL LIGHTS ILLUMINATE, OPS CK GOOD.
- [SDR GLBA201106291](https://openairdocs.org/sdr/GLBA201106291.md): Latch · unsecure · Jun 29, 2011 · N240GL · Beech 1900D · Emergency Exits
  > DURING AN INSP THE PILOT FOUND EMERGENCY EXIT 4C LATCH NOT SECURE. MX INSPECTED EMERGENCY DOOR 4C FOUND LATCH ON OUTSIDE DOOR. NOT SECURE REINSTALLED SECURE EMERGENCY DOOR 4C DOOR. SECURED REF MM 52-20-00 1(B).
- [SDR GLBA20110630M](https://openairdocs.org/sdr/GLBA20110630M.md): Cover · torn · Jun 28, 2011 · N240GL · Beech 1900D · Passenger/Crew Doors
  > "SUP" - SIG EVENT - DURING ROUTINE MX INSP, FOUND THE UPPER AFT AS DOOR CABLE COVER CUT. MX R & R UPPER AFT AS DOOR CABLE IN REF WITH MM 52-10-02.
- [SDR GLBA201103171](https://openairdocs.org/sdr/GLBA201103171.md): Wire · chafed · Mar 16, 2011 · N240GL · Beech 1900D · Fire Protection System Wiring
  > PILOT REPORTED THAT THE #1 FIRE BOTTLE "DISCH" ANNUNCIATOR ILLUMINATED IN FLIGHT. MAINTENANCE INSPECTED AND FOUND A CHAFFED WIRE GOING TO THE LH FIRE BOTTLE, REPAIRED WIRE AND SPLICED IAW AIM 12.8.0, OPS CK GOOD.
- [SDR GLBA20100927G](https://openairdocs.org/sdr/GLBA20100927G.md): Skin · burned · Sep 26, 2010 · N240GL · Beech 1900D · Elevator, Plate/Skin
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A LIGHTENING EXIT HOLE.7" BY 1" DEEP IN THE T/E OF THE LT ELEVATOR, JUST INBD OF CAP AT OUTER STATIC WICK, AT OUTER STATIC WICK, AND A DAMAGED RIVET ON TOP OF THE CAP. MAINTENANCE REPLACED THE RT ELEVA
- [SDR GLBA20100926F](https://openairdocs.org/sdr/GLBA20100926F.md): Skin · burned · Sep 26, 2010 · N240GL · Beech 1900D · Elevator, Plate/Skin
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A LIGHTENING EXIT HOLE.5" BY.5" DEEP IN THE T/E OF THE RT ELEVATOR, JUST INBD OF THE CAP AT THE OUTER STATIC WICK. OPEN
- [SDR GLBA20100716A](https://openairdocs.org/sdr/GLBA20100716A.md): Downlock Switch · failed · Jul 16, 2010 · N240GL · Beech 1900D · Landing Gear Position and Warning
  > PILOT REPORTED THAT NOSE GEAR ANNUNCIATOR FAILED TO ILLUMINATE ON GEAR EXTENSION, PILOTS CONFIRMED THERE WAS A POSITIVE PRESSURE USING THE MANUAL EXTENSION PUMP IN CASE IT WOULD BE REQUIRED, GEAR WAS DOWN AND LOCKED, MANUAL EXTENSION WAS NOT PERFORMED. MAINTEN
- [SDR GLBA20100622F](https://openairdocs.org/sdr/GLBA20100622F.md): Frame · cracked · Jun 21, 2010 · N240GL · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, A CRACK WAS FOUND IN THE FRAME ANGLE AT FS 150 AT THE ATTACH POINT FOR THE LOWER PAX DOOR STRUT MOUNTS UPPER AFT NUTPLATE AREA. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS
- [SDR GLBA20100622H](https://openairdocs.org/sdr/GLBA20100622H.md): Skin · cracked · Jun 21, 2010 · N240GL · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION CRACKS WERE FOUND IN THE UPPER SKIN AT FS 273.25 BETWEEN STRINGER 1 AND STRINGER 3R, CRACKS RANGE FROM.5" TO.7", APPROXIMATELY 7" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIR
- [SDR GLBA20100622G](https://openairdocs.org/sdr/GLBA20100622G.md): Frame · cracked · Jun 21, 2010 · N240GL · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A CRACK WAS FOUND IN THE FRAME AT F.S. 456 AT STRINGER 10R CUTOUT,.35" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-035. MATERIALS UTILI
- [SDR GLBA20100622J](https://openairdocs.org/sdr/GLBA20100622J.md): Frame · cracked · Jun 21, 2010 · N240GL · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A.75" CRACK WAS FOUND ON THE FRAME FLANGE AT F.S. 273.25 AND STRINGER 2R CUTOUT OUTBOARD OF STRINGER 2R, AND CRACKED.7" ON THE FRAME FLANGE INBOARD OF STRINGER 2R, AND A CRACK.7" I/B OF STRINGER 10R. MAI
- [SDR GLBA201005311](https://openairdocs.org/sdr/GLBA201005311.md): Bearing · deteriorated · May 31, 2010 · N240GL · Beech 1900D · Wheel/Ski/Float
  > UPON PRE-FLIGHT INSPECTIONS THE PILOTS REPORTED THAT THE NR 4 MAIN LANDING GEAR WHEEL ASSEMBLY WAS MISSING. (NOTE: THE LANDING GEAR WAS ALSO REMOVED AND REPLACED DUE TO DAMAGE TO THE AXLE ASSEMBLY AND THE BRAKES PRECAUTIONARY). MAINTENANCE REPLACED THE NR 3 ML
- [SDR GLBA20090508B](https://openairdocs.org/sdr/GLBA20090508B.md): Window · cracked · May 8, 2009 · N240GL · Beech 1900D · Flight Compartment Windows
  > (SUP) - DIVERSION - AIRCRAFT N240GL - FLIGHT 10 - THE PILOTS REPORTED THAT ENROUTE FROM "LWT" - "DEN" THE CAPTAINS WINDSHIELD SHATTERED/BROKEN. THE AIRCRAFT DIVERTED TO "CYS" FOR REPAIRS. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW BMM 52-10
- [SDR GLBA20090418A](https://openairdocs.org/sdr/GLBA20090418A.md): Circuit Board · malfunctioned · Apr 18, 2009 · N240GL · Beech 1900D · Central Warning
  > HAD MASTER WARNING AND MASTER CAUTION ANNC FLASHERS ON TAKEOFF, ABORTED. MASTER WARNING FLASHERS SEEMS TO COME ON ANYTIME MASTER CAUTION FLASHERS COMES ON. MAINTENANCE R & R PRINTED CIRCUIT BOARD. OPERATIONAL CHECKS WERE GOOD IAW MM 31-61-10.
- [SDR GLB2008F00016](https://openairdocs.org/sdr/GLB2008F00016.md): Regulator · malfunctioned · Aug 17, 2008 · N240GL · Beech 1900D · Pneumatic Distribution System
  > ACFT 240GL AIR RETURN FLT 5087 "DEN" 08/17/08 PILOTS REPORTED THE PNEUMATIC PRESSURE WAS EXCEEDING REDLINE DURING CLIMBOUT AT FULL POWER SETTINGS. MAINTENANCE ADJUSTED PNEUMATIC REGULATOR AS REQUIRED IAW 1900D MM 36-00-01. OPERATIONAL CHECK WAS GOOD.
- [SDR GLBA20060906](https://openairdocs.org/sdr/GLBA20060906.md): Skin · cracked · Feb 19, 2007 · N240GL · Beech 1900D · Fuselage Main, Plate/Skin
  > UPON ROUTINE INSPECTION, MAINTENANCE DISCOVERED A 3.25 INCH LONG CRACK 27.5 INCHES LT OF BELLY CENTERLINE AT APPROXIMATELY STA. F.S. 352. MAINTENANCE REPAIRED THE CRACK IN THE FUSELAGE IAW SRM 51-70 FROM F.S. 351 TO F.S. 354.25. REPAIR DIMENSIONS 7.25 INCHES B
- [SDR GLBA20060809](https://openairdocs.org/sdr/GLBA20060809.md): Pressure Switch · intermittent · Jul 28, 2006 · N240GL · Beech 1900D · Propeller Feathering/Reversing
  > PROPELLER SYSTEM FLUCTUATED IN AND OUT OF FEATHER ON APPROACH WITH INTERMITTENT AFX DISABLE LIGHT. REPLACED LOW PRESSURE SWITCH (PN 50-389121-47, SN 0245). (TOTAL TIME UNKNOWN)
- [SDR GLBA20060796](https://openairdocs.org/sdr/GLBA20060796.md): Motor · shorted · Jul 3, 2006 · N240GL · Beech 1900D · Trailing Edge Flap Control System
  > IRRITATING SMELL / SMOKE IN COCKPIT/CABIN AFTER FLAP EXTENSION. SHUT ENGINES DOWN ON TAXIWAY, INSPECTED AIRCRAFT AND FOUND FLAP MOTOR SHORTED. REPLACED FLAP MOTOR, OPS CHECK SATISFACTORY.
- [SDR GLBA20060700](https://openairdocs.org/sdr/GLBA20060700.md): Stringer · corroded · Mar 25, 2006 · N240GL · Beech 1900D · Fuselage Main, Longeron/Stringer
  > INSPECTION OF FS258.25 TO 273.25, STRINGER 14R HAD LEVEL (2) CORROSION. REPAIRED IAW MANUFACTURES INSTRUCTIONS (FR-CO-01321) DATED 3-20-06
- [SDR GLBA20050507](https://openairdocs.org/sdr/GLBA20050507.md): Autofeather Sys · malfunctioned · Aug 21, 2005 · N240GL · Beech 1900D · Propeller Feathering/Reversing
  > LEFT ENGINE SOUNDED LIKE IT CYCLED THROUGH AN AUTOFEATHER, INCREASED POWER AND CONDITION CEASED, LANDED WITHOUT INCIDENT. PERFORMED GROUND RUN-UP, COULD NOT DUPLICATE, RETURNED TO SERVICE.
- [SDR 20030830](https://openairdocs.org/sdr/20030830.md): Wire · chafed · Apr 18, 2005 · N240GL · Beech 1900D · Landing Gear System Wiring
  > DURING CLIMB, FLT CREW REPORTED AFX DISABLE AND LEFT AND RIGHT AUTOFEATHER ANNUNCIATORS ILLUMINATED. FLT CREW RETURNED TO AIRPORT WITHOUT INCIDENT. MAINTENANCE REPAIRED CHAFED WIRES AT LT MLG UPLOCK SWITCH. OP CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Next page: https://openairdocs.org/aircraft/N240GL/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 = 'N240GL' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N240GL/reports

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