# Service difficulty reports: N247GL

A list on [N247GL](https://openairdocs.org/aircraft/N247GL.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 · 66 reports

- [SDR TIMA20250603003](https://openairdocs.org/sdr/TIMA20250603003.md): Engine · power loss · Jun 3, 2025 · N247GL · Beech 1900D · Engine (Turbine/Turboprop)
  > AFTER LEVELING OFF AT 14000' LEFT FUEL PRESSURE ANNUNCIATION CAME ON, STNADBY PUMP TURNED ON, FUEL PRESSURE ANNUMC REMAINED ON, FLOW DROPPED, ENGINE ROLLED BACK. PUSHED PROPS/POWER UP, LEFT ENGINE REMINED ROLLED BACK (11%) N1. SHUTDOWN ENGINE CUTOFF, FEATHERED
- [SDR GLBA2017080700677](https://openairdocs.org/sdr/GLBA2017080700677.md): Cable · frayed · Aug 5, 2017 · N247GL · Beech 1900D · Passenger/Crew Doors
  > MAINTENANCE REPORTED THAT THE AIRSTAIR DOOR LOWER FORWARD HANDRAIL CABLE WAS FRAYED. REMOVED AND REPLACED THE HANDRAIL CABLE IAW BMM 52-10-02.
- [SDR GLBA2017072100675](https://openairdocs.org/sdr/GLBA2017072100675.md): Unknown · odor · Jul 19, 2017 · N247GL · Beech 1900D · Fuselage Structure (General)
  > PILOTS REPORTED THAT THERE WAS A LINGERING, FOUL, MOLDY STENCH IN THE COCKPIT AND CABIN. THOUGHT TO BE COMING FROM THE BLOWER VENTS. THE ODOR WAS NOTED AS VERY NAUSEATING AND FATIGUING FOR THE CREW TO FLY IN. MAINTENANCE CLEANED AREAS FORWARD AND AFT OF THE
- [SDR GLBA2017030100636](https://openairdocs.org/sdr/GLBA2017030100636.md): Cable · loose · Feb 27, 2017 · N247GL · Beech 1900D · Passenger/Crew Doors
  > MAINTENANCE DISCOVERED THAT THE PASSENGER DOOR AFT CABLES WERE LOOSE AND REQUIRE ADJUSTMENT. TIGHTENED PASSENGER DOOR AFT CABLE IAW AMM 52-10-02.
- [SDR GLBA2015082600532](https://openairdocs.org/sdr/GLBA2015082600532.md): Skin · cracked · Aug 25, 2015 · N247GL · Beech 1900D · Leading Edge Devices
  > FOUND THE LT INBD LE INSIDE SKIN HAS SEVERAL AREAS OF CHAFING FROM THE CONTROL CABLES RUBBING & HOLES, A.5" SHALLOW HOLE & CHAFE MARKS, A.375",.125" HOLES IN SKIN ONLY, SHALLOW HOLE, SMALL.25" WEAR HOLE,.75" TEAR IN THE EDGE OF THE SKIN & A CRACK,.25" IN
- [SDR GLBA2015071400526](https://openairdocs.org/sdr/GLBA2015071400526.md): Angle · cracked · Jul 12, 2015 · N247GL · Beech 1900D · Fuselage Miscellaneous Structure
  > MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND A 2.8" CRACK IN AN ANGLE AT FS 456.0, AT FWD CARGO FLOOR LEVEL. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 15-1900-53-008.
- [SDR GLBA2015070100525](https://openairdocs.org/sdr/GLBA2015070100525.md): Frame · cracked · Jul 1, 2015 · N247GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE FRAME AT FS 107 BY STRINGER 8L, PROTRUDING OUT OF RIVET ON EITHER SIDE,.25" IN LENGTH. REPAIRED IAW EO 15-1900-53-007. MAJOR REPAIR.
- [SDR GLBA2015062300524](https://openairdocs.org/sdr/GLBA2015062300524.md): Door Frame · cracked · Jun 23, 2015 · N247GL · Beech 1900D · Fuselage Main, Structure
  > MAJOR REPAIR, DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE FRAME AT FS 509.5, AFT SIDE OF CARGO DOOR FRAME AT MID-CARGO FLOOR LEVEL,.7" IN LENGTH. REPAIRED THE AFFECTED AREA. PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 15-1900-53-006.
- [SDR GLBA2014112400469](https://openairdocs.org/sdr/GLBA2014112400469.md): Printed Ckt Board · faulty · Nov 23, 2014 · N247GL · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT ON CLIMB OUT AFX DISABLE LIGHT ILLUMINATED, N1 ABOVE 91% ON THE RT SIDE. REPLACED PCB A123, PN 129-364091-9, SN ON 993-F-94, SN OFF 799-C-93 IAW MI 34-01, SYS OPERATIONS CHECK GOOD.
- [SDR GLBA2014071800422](https://openairdocs.org/sdr/GLBA2014071800422.md): Spar Cap · mechanic error · Jul 16, 2014 · N247GL · Beech 1900D · Wing Spar
  > MAJOR REPAIR DURING A SCHEDULED INSPECTION FOUND THE LT WING SPAR AFT CAP AT WS 12325 FASTENER HOLE MISSED DRILLED THROUGH THE WING SKIN & WING SPAR CAP. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-57-003. MATERIALS UTI
- [SDR GLBA2013032700217](https://openairdocs.org/sdr/GLBA2013032700217.md): Frame · cracked · Mar 27, 2013 · N247GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE FRAME AT FS 164 AND STRINGER 10R, 0.375" IN LENGTH. REPAIRED IAW EO 13-1900-53-028. MAJOR REPAIR.
- [SDR GLBA2013032700216](https://openairdocs.org/sdr/GLBA2013032700216.md): Frame · cracked · Mar 27, 2013 · N247GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK AT FS 451 AND STRINGER 10R FRAME,.5" IN LENGTH. REPAIRED IAW EO 13-1900-53-027. MAJOR REPAIR.
- [SDR GLBA2013032500215](https://openairdocs.org/sdr/GLBA2013032500215.md): Spar Cap · cracked · Mar 25, 2013 · N247GL · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE RT SPAR CAP AT THE SECOND FASTENER, FWD VERT STAB, 0.375" IN LENGTH. REPAIRED IAW EO 13-1900-55-008. MAJOR REPAIR.
- [SDR GLBA2013010400167](https://openairdocs.org/sdr/GLBA2013010400167.md): Uplock Switch · inoperative · Feb 2, 2013 · N247GL · Beech 1900D · Landing Gear Position and Warning
  > PILOT REPORTED THAT ON LANDING, LOWERED THE GEAR, INTRANSIT LIGHT CAME ON AND WENT OUT, GOT GREEN ON MAINS, NOT ON NOSE, MANUALLY EXTENDED GEAR AND STILL NO GREEN ON NOSE. MX REPLACED THE NOSE UPLOCK SWITCH, OPS CK GOOD.
- [SDR GLBA2013012200160](https://openairdocs.org/sdr/GLBA2013012200160.md): Skin · cracked · Jan 22, 2013 · N247GL · Beech 1900D · Elevator, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND 2 CRACKS ON A LT ELEVATOR ASSY IN THE T/E, APPROX 23.1875" OTBD OF TRIM TAB OTBD CUTOUT, ON BOTH SIDES OF THE ELEVATOR SKIN, (TOP AND BOTTOM SIDES), 1" IN LENGTH. REPAIRED IAW EO 13-1900-27-001. MAJOR REPAIR.
- [SDR GLBA2012092000065](https://openairdocs.org/sdr/GLBA2012092000065.md): Spar Cap · cracked · Sep 19, 2012 · N247GL · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE LT FWD SPAR CAP ANGLE AT THE VERT STAB AT VSS 84.10 AND THE 20 PERCENT AT THE SECOND FASTENER, CRACK RADIATES DOWNWARD FROM FASTENER,.375" IN LENGTH. REPAIRED IAW FR-CO-02530, REV 1, STEP 1. MAJO
- [SDR GLBA2012033002](https://openairdocs.org/sdr/GLBA2012033002.md): Spar · cracked · Mar 30, 2012 · N247GL · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND 5 TO 7 CRACKS RADIATING FROM THE CENTER LIGHTNING HOLE ON THE STAB REAR SPAR CENTER WEB, 2.5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-55-009. MATERIAL
- [SDR GLBA2012033001](https://openairdocs.org/sdr/GLBA2012033001.md): Spar · cracked · Mar 30, 2012 · N247GL · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND 2 CRACKS ON MAIN SPAR WEB AT HSS 3.0L AND 3.0R, 1 INCH IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-55-010. MATERIALS UTILIZED ARE INCLUDED IN THE EO. MAJOR REPAI
- [SDR GLBA20111214F](https://openairdocs.org/sdr/GLBA20111214F.md): Frame · cracked · Dec 14, 2011 · N247GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND THE AFT FUSELAGE FRAME AT FS 456 CRACKED AT THE FWD GAS STRUT MOUNT UPPER INBD NUT PLATE, BETWEEN STRINGER 4L AND 5L, 2 CRACKS 1" AND.2" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPE
- [SDR GLBA201112012](https://openairdocs.org/sdr/GLBA201112012.md): Terminal · broken · Nov 29, 2011 · N247GL · Beech 1900D · Door System Wiring
  > ALL THE INSPECTION LIGHTS IN THE AIRSTAIR DOOR SYS ARE INOPERATIVE. MX FOUND A BROKEN TERMINAL WIRE ON THE DOOR, MX REPLACED THE TERMINAL AND OPS CHECKED GOOD.
- [SDR GLBA20111010G](https://openairdocs.org/sdr/GLBA20111010G.md): Stall Warning · false activation · Oct 8, 2011 · N247GL · Beech 1900D · Stall Warning System
  > PILOT REPORTED THAT AT 80 KNOTS IAS THE STALL WARNING HORN SOUNDED AND THE TAKEOFF WAS ABORTED. MX TROUBLESHOT THE SYS, COULD NOT DUPLICATE, CHECKED CONNECTORS ON THE SWITCH HARNESSES, ATTACHED A BREAKOUT BOX, NO DEFECTS FOUND, RESECURED SQUAT SWITCH HARNESS,
- [SDR GLBA20110819G](https://openairdocs.org/sdr/GLBA20110819G.md): Housing · torn · Aug 18, 2011 · N247GL · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE AIRSTAIR CABLE HOUSING IS RIPPED, UPPER AFT. MX REPLACED THE UPPER AFT CABLE IAW BMM 52-10-02, PN: 1440-10GLA.
- [SDR GLBA201102261](https://openairdocs.org/sdr/GLBA201102261.md): Oxygen Mask · unwanted deploy · Feb 25, 2011 · N247GL · Beech 1900D · Passenger Oxygen System
  > PILOT REPORTED THAT ON DECENT PASSENGER OXYGEN MASKS DEPLAYED INADVERTENTLY. MAINTENANCE REPACKED ALL PAX O2 MASKS IN CONTAINERS IAW BMM 35-20-01.
- [SDR GLBA201011241](https://openairdocs.org/sdr/GLBA201011241.md): Bulb · inoperative · Nov 24, 2010 · N247GL · Beech 1900D · Emergency Lighting
  > EMERGENCY LIGHT BULB DID NOT TEST. MAINTENANCE REPLACED THE BULB PN 1864, REF MM 31-10-00, OPS CHECK GOOD.
- [SDR GLBA20100810F](https://openairdocs.org/sdr/GLBA20100810F.md): Skin · dented · Aug 10, 2010 · N247GL · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, A DENT ON RT SIDE OF FUSELAGE AT FS 531 BETWEEN STRINGER 11R AND 10R WAS FOUND. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-049. MATERIALS UTILIZED ARE IN
- [SDR GLBA200909141](https://openairdocs.org/sdr/GLBA200909141.md): Tube · deteriorated · Sep 14, 2009 · N247GL · Beech 1900D · Engine Bleed Air System
  > ABORTED TAKEOFF- AIRCRAFT 247GL DID AN ABORTED TAKEOFF IN HVR FLT 5186 FOR RT BLEED AIR FAIL ANNUNCIATOR ILLUMINATING. CREW RETURNED TO GATE AND CALLED MX. THE CREW AND MX AGREED THAT IT COULD BE MEL'D UNDER 21-3-2 CAT B. THE CREW BEFORE DOING THE MEL RAN T
- [SDR GLBA20090902A](https://openairdocs.org/sdr/GLBA20090902A.md): Outflow Valve · malfunctioned · Sep 2, 2009 · N247GL · Beech 1900D · Pressure Regulator/Outflow Valve
  > ACFT WOULD NOT PRESSURIZE DURING CLIMB OUT. MX SECURED THE RT OUTFLOW VALVE THAT WAS FOUND LOOSE IAW MM 21-30-01-201. AN OPS TEST FLIGHT WAS CONDUCTED AND FOUND TO BE SATISFACTORY.
- [SDR GLBA200906031](https://openairdocs.org/sdr/GLBA200906031.md): Shutoff Valve · deteriorated · Jun 3, 2009 · N247GL · Beech 1900D · Air Distribution System
  > AT 400 FT, TURNED BLEEDS ON AN LT ENVIRO FAIL ANNUN ILLUMINATED, TRIED TO RESET SEVERAL TIMES IAW THE CHECKLIST, DID NOT RESET, RETURNED TO DEPARTURE AND TRANSFERED THE ISSUE TO DML NR 35433 PER MEL 21-14 CAT C ALL O PROCEDURES COMPLIED WITH. MX REMOVED AND R
- [SDR GLBA20090410F](https://openairdocs.org/sdr/GLBA20090410F.md): Door Frame · cracked · Apr 6, 2009 · N247GL · Beech 1900D · Fuselage Main, Structure
  > DURING SCHEDULED STRUCTURAL INSP MX DISCOVERED CRACKS AROUND THE CARGO DOOR UPPER FRAME AT FWD CORNER AREA AT FS 456 AND UPPER FRAME AFT CORNER AT FS 509. APPROXIMATE CRACK LENGTHS 5 INCHES AND 2.75 INCHES RESPECTIVELY. MX REPAIRED THE AFFECTED AREAS IAW EO-0
- [SDR GLBA20090406G](https://openairdocs.org/sdr/GLBA20090406G.md): Skin · cracked · Apr 4, 2009 · N247GL · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR - SKIN CRACKS ON TOP OF FUSELAGE AT F.S. 150.6 AT STRINGER 1 WERE FOUND DURING SCHEDULED STRUCTURAL CHECK. RIVET HEAD WAS SHEARED WITH CRACKS STARTING AT SAID RIVET AND ANOTHER CRACK AT A RIVET SAME LOCATION OTHER SIDE OF STRINGER 1. MAINTENANCE R
- [SDR GLBA200901052](https://openairdocs.org/sdr/GLBA200901052.md): Relay · faulty · Jan 4, 2009 · N247GL · Beech 1900D · Landing Gear Retraction/Extension System
  > SIGNIFICANT EVENT - ENROUTE FROM PGA TO FMN THE PILOTS REPORTED THAT THE GEAR RELAY CIRCUIT BREAKER POPPED TWICE AND THEY HAD TO MANUALLY EXTEND THE GEAR. MX REMOVED AND REPLACED THE LANDING GEAR RELAY IAW MFG MX 32-30. OPS CHECKS WERE GOOD.
- [SDR GLBA20061024](https://openairdocs.org/sdr/GLBA20061024.md): Latch · failed · Nov 7, 2007 · N247GL · Beech 1900D · Passenger/Crew Doors
  > EES - FLIGHT 5041 (DEN) PILOTS REPORTED THE MAIN CABIN DOOR COULD NOT BE OPENED FROM THE INSIDE. MAINTENANCE CLEANED THE PUSH BUTTON SWITCH AND OPERATIONALLY CHECKED THE DOOR. OPS GOOD IAW MM 52-10-00.
- [SDR GLBA20061016](https://openairdocs.org/sdr/GLBA20061016.md): Stringer · cracked · Oct 15, 2007 · N247GL · Beech 1900D · Fuselage Main, Longeron/Stringer
  > STRINGER 10R CRACKED AT FS 451 IAW CRACK IS ABOUT.5 IN LONG AT STRINGER RELIEF CUTOUT. CRACKED AT STRINGER FLANGE. REPAIRED STRINGER FLANGE AT FS 451 IAW. 1900D SRM 51-70. REPAIR DIMENSIONS APPROXIMATELY 9.375 IN BY 1 IN. 2024 T-3.050. RII COMPLIED WITH I
- [SDR GLBA20061015](https://openairdocs.org/sdr/GLBA20061015.md): Frame · cracked · Oct 15, 2007 · N247GL · Beech 1900D · Fuselage Main, Frame
  > FRAME AT FS 451.0 CRACKED AT STRINGER 10R RELIEF CUTOUT CRACK IS.6250 IN LONG. MAINTENANCE REPAIRED FRAME FLANGE AT FS 451.0 IAW 1900D SRM 51-70. REPAIR APPROXIMATELY 6 INCH BY 2 INCH 2024 T3.063. RII COMPLIED WITH IAW TASKCARD 8.2.1.
- [SDR GLBA20061014](https://openairdocs.org/sdr/GLBA20061014.md): Angle · cracked · Oct 15, 2007 · N247GL · Beech 1900D · Fuselage Miscellaneous Structure
  > LT HEAVY ANGLE CRACKED AT FS 288. CRACK LENGTH APPROXIMATELY 1.75 INCH. MAINTENANCE REPAIRED LT HEAVY ANGLE AT FS 288 IAW 1900D SRM 53-90. REPAIR DIMENSIONS APPROXIMATELY 13.5 INCHES. RII COMPLIED WITH IAW TASKCARD 8.2.1.
- [SDR GLBA20060960](https://openairdocs.org/sdr/GLBA20060960.md): Skin · damaged · Jul 1, 2007 · N247GL · Beech 1900D · Fuselage Main, Plate/Skin
  > HOLE IN FUSELAGE ON THE RT SIDE FORWARD OF FS 423.25 AND 2 INCHES ABOVE STRINGER 12R. APPROXIMATELY 1 INCH V SHAPE HOLE/CUT. MAINTENANCE REPAIRED AFFECTED AREA WITH A FLUSH REPAIR IAW MFG SRM 51-70. RII COMPLIED WITH IAW TASKCARD 8.2.1. HOLE CUTOUT SIZE 1.3 IN
- [SDR GLBA20060940](https://openairdocs.org/sdr/GLBA20060940.md): Hydraulic Line · defective · Apr 20, 2007 · N247GL · Beech 1900D · Hydraulic System, Main
  > FLIGHT 5128, ENROUTE, PILOTS REPORTED THAT WHILE INFLIGHT MAIN GEAR EXTENDED AND THE LANDING GEAR RELAY CIRCUIT BREAKER POPPED. CREW MANUALLY EXTENDED GEAR TO ACHIEVE A (3) GREEN CONFIGURATION. MAINTENANCE REMOVED AND REPLACED A FLEXIBLE HYDRAULIC LINE IN THE
- [SDR GLBA20050516](https://openairdocs.org/sdr/GLBA20050516.md): Windshield · failed · Sep 2, 2005 · N247GL · Beech 1900D · Flight Compartment Windows
  > LEFT WINDSHEILD OUTER PLY SHATTERED. REPLACED WINDSHEILD.
- [SDR 20030784](https://openairdocs.org/sdr/20030784.md): Window Frame · cracked · Jan 10, 2005 · N247GL · Beech 1900D · Fuselage Main, Structure
  > DURING ROUTINE STRUCTURAL INSPECTION, ALL THREE EMERGENCY EXIT WINDOW PANS WERE FOUND TO HAVE CRACKS AROUND THE RADIUS. WINDOW PANS WERE REPLACED, AIRCRAFT RETURNED TO SERVICE.
- [SDR GLBA20030721](https://openairdocs.org/sdr/GLBA20030721.md): Handle · corroded · Sep 15, 2004 · N247GL · Beech 1900D · Entrance Stairs
  > AIRSTAIR DOOR HANDLE SHOWS SIGN OF CORROSION, REMOVED CORROSION AND REPAIRED.
- [SDR GLBA20030611](https://openairdocs.org/sdr/GLBA20030611.md): Engine · overtemp · Apr 14, 2004 · N247GL · Beech 1900D · Engine (Turbine/Turboprop)
  > LT ENGINE TEMP LIMITED AT TAKE OFF, PREFORMED GROUND RUN ALL PARAMETERS WITHIN LIMITS
- [SDR GLBA20030597](https://openairdocs.org/sdr/GLBA20030597.md): Indicator · stuck · Mar 25, 2004 · N247GL · Beech 1900D · Airspeed/Mach Indicator
  > NR 2 ASI STUCK AT ZERO, R&R NR 2 ASI PN 130-380005-7
- [SDR GLBA20030578](https://openairdocs.org/sdr/GLBA20030578.md): Static Wick · damaged · Feb 29, 2004 · N247GL · Beech 1900D · Communications System
  > STATIC IN BOTH COMM'S BOTH NAV'S FAILED IN PRECIP, R&R STATIC WICKS PN 101-380053-9
- [SDR GLBA20030577](https://openairdocs.org/sdr/GLBA20030577.md): Radio · malfunctioned · Feb 29, 2004 · N247GL · Beech 1900D · Communications System
  > STATIC IN BOTH COMM'S BOTH NAVS FAILED PRECIP, R & R STATIC WICKS
- [SDR GLBA20030568](https://openairdocs.org/sdr/GLBA20030568.md): Indicator · stuck · Feb 19, 2004 · N247GL · Beech 1900D · Airspeed/Mach Indicator
  > FO'S ASI STUCK AT ZERO, PREFORMED PITOT CK OPS CK GOOD
- [SDR GLBA20030566](https://openairdocs.org/sdr/GLBA20030566.md): Indicator · smoke · Feb 18, 2004 · N247GL · Beech 1900D · Airspeed/Mach Indicator
  > NR 2 ASI STAYED AT ZERO & TOWER REPORTED OF SMOKE ON TAKE OFF ROLL, R&R NR 2 ASI GROUND RAN ACFT INSP ENG NO PROBLEMS NOTED
- [SDR GLBA20030564](https://openairdocs.org/sdr/GLBA20030564.md): Idler Gear · sticking · Feb 13, 2004 · N247GL · Beech 1900D · Aileron Control System
  > AILERON TRIM CATCHES AND STICKS, R&R IDLER GEAR ASSY. OPS CK GOOD
- [SDR GLBA20030553](https://openairdocs.org/sdr/GLBA20030553.md): Indicator · failed · Feb 3, 2004 · N247GL · Beech 1900D · Airspeed/Mach Indicator
  > FAILURE OF FIRST OFFICER'S A/S INDICATOR. PERFORMED GROUND CHECK, FOUND NO DEFECTS.
- [SDR GLBA2003160](https://openairdocs.org/sdr/GLBA2003160.md): Indicator · slow · Nov 28, 2003 · N247GL · Beech 1900D · Airspeed/Mach Indicator
  > FO'S AIRSPEED IND SLOW, TURNED PITOT HEAT ON FOR LONGER PERIOD OPS CK GOOD PN 130-380005-7
- [SDR GLBA2003156](https://openairdocs.org/sdr/GLBA2003156.md): Indicator · failed · Nov 22, 2003 · N247GL · Beech 1900D · Airspeed/Mach Indicator
  > FO'S AIRSPEED FAILED TO WORK ON TAKE OFF, REMOVED AND WARMED FO'S AIRSPEED IND PN1303800057 INSTALLED ASI RUN UP ON PITOT STATIC TEST OPS CK GOOD.

Next page: https://openairdocs.org/aircraft/N247GL/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 = 'N247GL' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N247GL/reports

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