# Service difficulty reports: N220GL

A list on [N220GL](https://openairdocs.org/aircraft/N220GL.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 · 70 reports

- [SDR GLBA2014081400428](https://openairdocs.org/sdr/GLBA2014081400428.md): Skin · damaged · Aug 13, 2014 · N220GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION FOUND A.05 INCH HOLE IN THE BELLY SKIN NEAR THE ADF ANTENNA AT APPROX FS 219. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-028. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.
- [SDR GLBA2014062300417](https://openairdocs.org/sdr/GLBA2014062300417.md): Connector · unsecure · Jun 21, 2014 · N220GL · Beech 1900D · Propeller/Propulsor System Wiring
  > SIG EVENT PILOT REPORTED THAT AN UNSCHEDULED AUTO FEATHER ACTIVATION ON THE RT ENG, ON APPROACH SEVERAL TIMES UNTIL THE SYS WAS TURNED OFF. SECURED THE RT LP AFX SWITCH CONNECTOR, OPERATIONS CHECKED GOOD.
- [SDR GLBA2014010800364](https://openairdocs.org/sdr/GLBA2014010800364.md): Door Frame · cracked · Jan 8, 2014 · N220GL · Beech 1900D · Passenger/Crew Doors
  > DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE LOWER AIRSTAIR DOOR FRAME AT BS 172.0, 1.4 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-001.
- [SDR GLBA2013042600243](https://openairdocs.org/sdr/GLBA2013042600243.md): Connector · damaged · Apr 25, 2013 · N220GL · Beech 1900D · Electrical Power System Wiring
  > PILOT REPORTED THAT THERE WAS A STRANGE ODOR IN THE COCKPIT. MX REPAIRED SEVERAL WIRES AT A CONNECTOR & CHANGED SEVERAL PCBS.
- [SDR GLBA2013040800227](https://openairdocs.org/sdr/GLBA2013040800227.md): Frame · cracked · Apr 8, 2013 · N220GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK ON THE FRAME FLANGE AT FS 177.35 AND STRINGER 13L, 1.5" IN LENGTH. REPAIRED IAW EO 13-1900-53-031. MAJOR REPAIR.
- [SDR GLBA2013040800226](https://openairdocs.org/sdr/GLBA2013040800226.md): Longeron · cracked · Apr 8, 2013 · N220GL · Beech 1900D · Fuselage Main, Longeron/Stringer
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE COCKPIT RT SIDEWALL LONGERON AT FS 107, AT JUNCTION WITH SIDEWALL FRAME,.75" IN LENGTH. REPAIRED IAW EO 13-1900-53-030. MAJOR REPAIR.
- [SDR GLBA2013040800225](https://openairdocs.org/sdr/GLBA2013040800225.md): Frame · cracked · Apr 8, 2013 · N220GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE COCKPIT RT SIDE WALL FRAME AT FS 107 AT THE UPPER 2 FASTENER HOLES, RADIATES FROM EACH HOLE UPWARD, 1" IN LENGTH. REPAIRED IAW EO 13-1900-53-030. MAJOR REPAIR.
- [SDR GLBA2013040800224](https://openairdocs.org/sdr/GLBA2013040800224.md): Skin · cracked · Apr 8, 2013 · N220GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE LT FUSELAGE SKIN AT THE UPPER FWD AREA OF A/S DOOR CUTOUT, RADIATES FROM FASTENER UPWARD & DOWNWARD AT FS 150 AND BELOW STRINGER 4L,.55" IN LENGTH. REPAIRED IAW EO 13-1900-53-031. MAJOR REPAIR.
- [SDR GLBA2013040800223](https://openairdocs.org/sdr/GLBA2013040800223.md): Skin · cracked · Apr 8, 2013 · N220GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSP FOUND 2 CRACKS IN THE UPPER FUSELAGE SKIN AT FS 150 AND STRINGER 1 ON THE LT & RT SIDE OF STRINGER 1,.7" IN LENGTH. REPAIRED IAW EO 13-1900-53-029. MAJOR REPAIR.
- [SDR GLBA2013040100220](https://openairdocs.org/sdr/GLBA2013040100220.md): Circuit Breaker · tripped · Mar 28, 2013 · N220GL · Beech 1900D · Landing Gear Retraction/Extension System
  > PILOT REPORTED THAT UPON EXTENDING THE GEAR THE LANDING GEAR CIRCUIT BREAKER TRIPPED, RAN MANUAL GEAR EXTENTION CHECKLIST, GEAR EXTENDED NORMALLY, A HIGH PITCH NOISE WAS HEARD FROM THE WHEEL WELL AFTER PARKING AT THE GATE. MX FOUND THE POWER PACK RUNNING, REPL
- [SDR GLBA2013022800188](https://openairdocs.org/sdr/GLBA2013022800188.md): Plenum · debonded · Feb 19, 2013 · N220GL · Beech 1900D · Nacelle/Pylon, Main Frame
  > LT OTBD PLENUM PANEL DEBONDED APPROX 5" FROM THE TOP OF PANEL TO APPROX 15" DOWN, THE FULL WIDTH OF THE HONEYCOMB. REPAIRED IAW WITH A FIELD REPAIR.
- [SDR GLBA2012111400107](https://openairdocs.org/sdr/GLBA2012111400107.md): Screw · loose · Nov 14, 2012 · N220GL · Beech 1900D · Propeller Governor
  > PILOT REPORTED THAT ON SHORTLY AFTER LEVELING OFF FROM DECENT NR 1 ENG BEGAN TO TQ SURGE PAST AT 4500 FT LBS REDUCED PWR PROP BEGAN TO SURGE RAN MEM ITEMS BROUGHT POWER TO IDLE, RAN CKLIST, FEATHER PROP, COMPLETED ENG SHUTDOWN. RPM NEVER EXCEEDED 1700. PROP
- [SDR GLBA2012090500046](https://openairdocs.org/sdr/GLBA2012090500046.md): Web · cracked · Sep 5, 2012 · N220GL · Beech 1900D · Horizontal Stabilizer Miscellaneous Structure
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND FOUR CRACKS IN THE HORIZONTAL STAB FWD WEB AT HSS 00.00 PROTRUDING FROM GROMMET HOLE, ONE INCH IN LENGTH. REPAIRED IAW EO 12-1900-55-027. MAJOR REPAIR.
- [SDR GLBA2012090400044](https://openairdocs.org/sdr/GLBA2012090400044.md): Spar · cracked · Sep 2, 2012 · N220GL · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB RT FWD SPAR CAP ANGLE AT 20 PERCENT CHORD AND APPROX VSS 84.10 PROTRUDING FROM THE 2ND FROM TOP FASTNER APPROX.125" TO EITHER SIDE, 2 CRACKS,.25" IN LENGTH. REPAIRED IAW EO 12-1900-5
- [SDR GLBA2012090400045](https://openairdocs.org/sdr/GLBA2012090400045.md): Spar · cracked · Aug 31, 2012 · N220GL · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND CRACK IN THE VERTICAL STAB LT FWD SPAR CAP ANGLE AT 20 PERCENT CHORD AND APPROX VSS 84.10, EXTENDING FROM TOP OF ANGLE TO JUST PAST 2ND FROM TOP FASTENER, 1.5" IN LENGTH. REPAIRED IAW EO 12-1900-55-025.
- [SDR GLBA2012070500011](https://openairdocs.org/sdr/GLBA2012070500011.md): Rib · cracked · Jul 5, 2012 · N220GL · Beech 1900D · Wing, Rib/Bulkhead
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE RIB ON LT INBD WING, INBD RT AT BL 29.06 AND FS 288.00, 2" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-57-005.
- [SDR GLBA2012070500009](https://openairdocs.org/sdr/GLBA2012070500009.md): Spar · chafed · Jul 5, 2012 · N220GL · Beech 1900D · Wing Spar
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND THE SPAR CHAFED AT LT INBD WING LWR FWD AREA,.02380 DEEP. REPAIRED THE AFFECTED AREA IAW EO 12-1900-57-007.
- [SDR GLBA2012030500011](https://openairdocs.org/sdr/GLBA2012030500011.md): Spar · cracked · Mar 5, 2012 · N220GL · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > "SUP" - MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP FOUND A CRACK AT IN THE CENTER WEB OF THE REAR SPAR OF HORZ STAB, CRACK RADIATES FROM THE UPPER RT OF THE LIGHTNING HOLE UPWARD AND OB,.375" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRE
- [SDR GLBA2012030501](https://openairdocs.org/sdr/GLBA2012030501.md): Skin · dented · Mar 5, 2012 · N220GL · Beech 1900D · Wing, Plate/Skin
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION FOUND A DENT IN THE LT WING L/E AT WS 236 MEASURING 4.2" LONG AND 1.5" DEEP.
- [SDR GLBA20120116F](https://openairdocs.org/sdr/GLBA20120116F.md): Placard · missing · Jan 13, 2012 · N220GL · Beech 1900D · Placards and Markings
  > PILOT REPORTED THAT THE EMERGENCY EVACUATION PLACARD AT 7A IS MISSING. MX REPLACED PLACARD AT SEAT 7A IAW AIM 5.2.2.
- [SDR GLBA20111219G](https://openairdocs.org/sdr/GLBA20111219G.md): Pcb · inoperative · Dec 18, 2011 · N220GL · Beech 1900D · Landing Gear Retraction/Extension System
  > PILOT REPORTED THAT THE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF, LANDING GEAR RELAY CB TRIPPED. MX REPLACED THE PCB A316, IAW MI 24-01, OPS CHECKED GOOD IAW MI 32-01.
- [SDR GLBA20111212J](https://openairdocs.org/sdr/GLBA20111212J.md): Circuit Board · malfunctioned · Dec 10, 2011 · N220GL · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT THE RT ENGINE WILL NOT AUTOFEATHER DURING TEST. MX RESEATED THE A123 PCB, OPS CHECKED GOOD.
- [SDR GLBA20111212H](https://openairdocs.org/sdr/GLBA20111212H.md): Connector · dirty · Dec 9, 2011 · N220GL · Beech 1900D · Propeller/Propulsor System Wiring
  > PILOT REPORTED THAT THE AUTOFEATHER OFF ANNUNCIATOR ILLUMINATED. MX CLEANED P277 CONNECTOR AT A123 PCB REF AIM 14.2.0, SYS OPS CHECKED GOOD.
- [SDR GLBA20111130F](https://openairdocs.org/sdr/GLBA20111130F.md): Skin · cracked · Nov 29, 2011 · N220GL · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE LT BELLY SKIN AT FS 300, 2.2" FROM BELLY SKIN LT OTBD EDGE, 1.1" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-066. MATERIALS
- [SDR GLBA20111130G](https://openairdocs.org/sdr/GLBA20111130G.md): Skin · debonded · Nov 29, 2011 · N220GL · Beech 1900D · Passenger/Crew Doors
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND THE AS DOOR INNER SKIN DEBONDED FROM FWD EDGE TO AFT EDGE INWARD FROM LWR EDGE 1.2", DEBONDED 3" AT THE FWD & AFT EDGES. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW
- [SDR GLBA20111109J](https://openairdocs.org/sdr/GLBA20111109J.md): Wire · damaged · Nov 8, 2011 · N220GL · Beech 1900D · Landing Gear System Wiring
  > PILOT REPORTED THAT UPON GEAR RETRACTION THE INTRANSIT LIGHT STAYED ILLUMINATED AND THE LANDING GEAR RELAY CIRCUIT BREAKER TRIPPED, MANUALLY EXTENDED GEAR WITH ALL NORMAL INDICATIONS. MX REPAIRED A WIRE AT THE LANDING GEAR SERVICE VALVE, OPS CHECKED GOOD.
- [SDR GLBA20111109G](https://openairdocs.org/sdr/GLBA20111109G.md): Pcb · inoperative · Nov 8, 2011 · N220GL · Beech 1900D · Propeller Feathering/Reversing
  > "SUP" - PILOT REPORTED THAT THE AFX DISABLE WILL NOT ILLUMINATE DURING AUTOFEATHER TEST. MX REPLACED PCB 129-364091-9 SN: 559895, REF MM 61-21-00, OPS CK GOOD.
- [SDR GLBA20111108F](https://openairdocs.org/sdr/GLBA20111108F.md): Landing Gear · malfunctioned · Nov 7, 2011 · N220GL · Beech 1900D · Landing Gear Retraction/Extension System
  > PILOT REPORTED THAT ON GEAR RETRACTION THE INTRANSIT LIGHT STAYED ILLUMINATED AND LDG GEAR RELAY CB TRIPPED, MANUALLY EXTENDED GEAR WITH ALL NORMAL INDICATIONS. MX MEGGED WIRES 66A22, 66C22, & 66F22 NFF, INSPECTED WIRING IN BEAVER TAIL, NFF, RAN ALL APPLICABL
- [SDR GLBA20111106A](https://openairdocs.org/sdr/GLBA20111106A.md): Pcb · inoperative · Nov 6, 2011 · N220GL · Beech 1900D · Landing Gear Retraction/Extension System
  > UPON SELECTING LANDING GEAR HANDLE DOWN, CB LANDING GEAR RELAY POPPED IMMEDIATELY. GEAR PUMP NOT HEARD. MANUAL GEAR EXTENSION SUCCESSFUL. MX WAS ABLE TO DUPLICATE, REPLACED THE PCB IAW AIM MI 24-01, GEAR SWUNG 3 TIMES IAW AIM MI 32-01, OPS CHECKED GOOD.
- [SDR GLBA20110914F](https://openairdocs.org/sdr/GLBA20110914F.md): Socket · dirty · Sep 13, 2011 · N220GL · Beech 1900D · Door Warning System
  > PILOT REPORTED THAT THE CABIN DOOR INSP LIGHT IS INOPERATIVE. MX CLEANED THE SOCKET AND RESECURED THE BULB, OPS CHECKED GOOD.
- [SDR GLBA20110815G](https://openairdocs.org/sdr/GLBA20110815G.md): Fuse · inoperative · Aug 13, 2011 · N220GL · Beech 1900D · Emergency Lighting
  > PILOT REPORTED THAT THE INSTRUMENT EMERGENCY LIGHTS SWITCH DOES NOT ILLUMINATE ANY INSTRUMENT INDIRECT LIGHTS. MX REPLACED A HOT BUSS FUSE IN THE BATTERY BOX, PN: MDA-5, REF MM 24-00-02, SEC 2, OPS CK GOOD.
- [SDR GLBA20110815F](https://openairdocs.org/sdr/GLBA20110815F.md): Switch · malfunctioned · Aug 12, 2011 · N220GL · Beech 1900D · Emergency Lighting
  > PILOT REPORTED THE THE INSTRUMENT EMERGENCY LIGHTS DO NOT ILLUMINATE WHEN THE BUTTON IS PRESSED. MX INSPECTED AND FOUND THAT THE SYS OPERATED NORMAL, OPS CHECKED GOOD IAW 24-00-02.
- [SDR GLBA20110725H](https://openairdocs.org/sdr/GLBA20110725H.md): Solenoid Valve · inoperative · Jul 22, 2011 · N220GL · Beech 1900D · Hydraulic System, Main
  > PILOT REPORTED THAT THE LANDING GEAR DID NOT COME DOWN WHEN SELECTED, LANDING GEAR RELAY CB POPPED, J-HOOK DID ENGAGE. MX REPLACED THE LANDING GEAR HANDLE AND REPLACED THE HYD PACK SOLENOID VALVE.
- [SDR GLBA20110722G](https://openairdocs.org/sdr/GLBA20110722G.md): Handle · inoperative · Jul 21, 2011 · N220GL · Beech 1900D · Landing Gear Selector
  > PILOT REPORTED THAT THE LANDING GEAR DID NOT COME DOWN WHEN THE HANDLE WAS PLACED IN THE DOWN POSITION, LANDING GEAR RELAY CIRCUIT BREAKER POPPED. MAINTENANCE REPLACED LANDING GEAR CONTROL HANDLE PN: 101-384137-7, SN OFF: B33, 1900-3210-00, PERFORMED 3 SWINGS,
- [SDR GLBA20110718K](https://openairdocs.org/sdr/GLBA20110718K.md): Wire · damaged · Jul 17, 2011 · N220GL · Beech 1900D · Door System Wiring
  > PILOT REPORTED THAT THE CABIN DOOR LOCK OBSERVATION LIGHT WAS INOP. MEL 88657. MAINTENANCE REPAIRED THE WIRE SPLICE D4436 AT THE DOOR ENTRY, IAW 33-20-07, OPS CK GOOD.
- [SDR GLBA20110718F](https://openairdocs.org/sdr/GLBA20110718F.md): Connector · loose · Jul 15, 2011 · N220GL · Beech 1900D · Landing Gear System Wiring
  > PILOT REPORTED THAT WHEN THE GEAR WAS SLECTED DOWN, GEAR UNSAFE LIGHTS ILLUMINATED, & HOOK ENGAGED, LT CIRCUIT BREAKER POPPED, RAN CK, MANUALLY EXTENDED GEAR, UNSAFE LIGHTS WENT OUT. MX CYCL LANDING GEAR, FOUND LOOSE CONNECTOR PLUG ON RT GEAR, CLEANED AND RE
- [SDR GLBA20110711M](https://openairdocs.org/sdr/GLBA20110711M.md): Switch · failed · Jul 9, 2011 · N220GL · Beech 1900D · Door Warning System
  > SIG EVENT - PILOT REPORTED THAT THE AIRSTAIR DOOR INSP LIGHT IS NOT ILLUMINATING. MEL 88288. MAINTENANCE REPLACED THE AIRSTAIR DOOR LOCK OBSERVATION LIGHT SWITCH, PN: 301-1 IAW GMM 12.10.0, OPS CK GOOD.
- [SDR GLBA20100611L](https://openairdocs.org/sdr/GLBA20100611L.md): Frame · cracked · Jun 11, 2010 · N220GL · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION 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 INSPECTI
- [SDR GLBA20100611K](https://openairdocs.org/sdr/GLBA20100611K.md): Frame · cracked · Jun 11, 2010 · N220GL · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION A CRACK WAS FOUND IN THE FRAME AT FS 164 AT CUTOUT FOR STRINGER 9AR,.15" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-033. MATERIALS UTILI
- [SDR GLBA20100611H](https://openairdocs.org/sdr/GLBA20100611H.md): Frame · cracked · Jun 11, 2010 · N220GL · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION A CRACK WAS FOUND IN THE FRAME AT FS 456 AT STRINGER 10R CUTOUT,.4" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-030. MATERIALS UTILIZED AR
- [SDR GLBA20100611J](https://openairdocs.org/sdr/GLBA20100611J.md): Stringer · cracked · Jun 11, 2010 · N220GL · Beech 1900D · Fuselage Main, Longeron/Stringer
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION A CRACK WAS FOUND IN STRINGER 10R AT RIVET 1.2" FORWARD OF FRAME AT FS 451, CRACK PASS THROUGH RIVET HOLE.1" ON EACH SIDE. STRINGER CRACKED AT FS 451, LENGTH.5", CRACKS ARE 1.2" APART. MAINTENANCE REPAIRE
- [SDR GLBA20091026G](https://openairdocs.org/sdr/GLBA20091026G.md): Engine · smoke · Oct 20, 2009 · N220GL · Beech 1900D · Engine (Turbine/Turboprop)
  > PILOTS REPORTED THAT AFTER ENGINE START UP A RAMP AGENT NOTICED SMOKE COMING FROM THE OIL HEATER EXIT ON THE NR 1 ENGINE AND THERE WAS A SMOKE ODOR IN THE CABIN MAINTENANCE INSPECTED THE NR 1 ENGINE FOR LEAKS. NO LEAKS WERE NOTED. CREW RAN THE ENGINES AND NO
- [SDR GLBA20090606B](https://openairdocs.org/sdr/GLBA20090606B.md): Blower · smoke · Jun 6, 2009 · N220GL · Beech 1900D · Air Distribution Fan
  > PILOTS REPORTED THAT ENVIRONMENTAL SMOKE AND FUMES WERE PRESENT IN THE COCKPIT. THE BLOWERS SEEMED TO MAKE THE SITUATION WORSE. PILOTS DECLARED AN EMERGENCY. THE CAPTAINS O2 MASK MIC WAS NOT WORKING WHEN SWITCHING TO THE O2 MASK. MX TROUBLESHOT THE ISSUE AND F
- [SDR GLBA20090326A](https://openairdocs.org/sdr/GLBA20090326A.md): Circuit Board · malfunctioned · Mar 26, 2009 · N220GL · Beech 1900D · Detection System
  > PILOTS REPORTED A LEFT HAND FIRE LOOP ANNUNCIATOR REPEATEDLY TRIPPED IN FLIGHT. ALSO STARTED TRIPPING LEFT HAND T-HANDLE AND MASTER WARNING ANNUNCIATOR (FLASHES). MAINTENANCE RE-RACKED THE FIRE EXTINGUISHING MONITOR PRINTED CIRCUIT BOARD P173. OPERATIONAL CHE
- [SDR GLBA20061109](https://openairdocs.org/sdr/GLBA20061109.md): Skin · damaged · Jun 2, 2008 · N220GL · Beech 1900D · Wing, Plate/Skin
  > MAJOR REPAIR - DURING ROUTINE MX INSPECTION A REPORT OF A FUEL LEAK WAS REPORTED ON THE LEFT LEADING EDGE NEAR THE FUEL BARRIER BOX AT WS 194.8 WING SKIN. ALSO REMOVED TO FACILITATE REPAIR AT WS 177.8 - WS 226.8. **SUPPLEMENTAL INFORMATION WILL BE PROVIDED U
- [SDR GLBA20060988](https://openairdocs.org/sdr/GLBA20060988.md): Spar · cracked · Aug 22, 2007 · N220GL · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > MAJOR REPAIR - UPON ROUTINE INSPECTION THE HORIZONTAL STABILIZER SPAR WEB WAS FOUND TO HAVE TWO CRACKS RADIATING FROM DEICE TUBE HOLE APPROXIMATELY 1/4 INCH & 1/2 INCH. MAINTENANCE REPAIRED MAIN SPAR CENTER WEB ON HORIZONTAL STAB I.A.W. BEECH 1900D SRM 55-91.
- [SDR GLBA20060981](https://openairdocs.org/sdr/GLBA20060981.md): Angle · cracked · Aug 20, 2007 · N220GL · Beech 1900D · Fuselage Miscellaneous Structure
  > MAJOR REPAIR - LT HEAVY ANGLE CRACKED AT F.S. 288. APPROXIMATELY 2 INCHES IN LENGTH. MAINTENANCE REPAIRED THE LT HEAVY ANGLE AT F.S. 288.0 I.A.W. BEECH 1900D SRM 53-90. REPAIR APPROXIMATELY 13 INCHES.
- [SDR GLBA2006980](https://openairdocs.org/sdr/GLBA2006980.md): Angle · cracked · Aug 20, 2007 · N220GL · Beech 1900D · Fuselage Miscellaneous Structure
  > MAJOR REPAIR - RT HEAVY ANGLE CRACKED AT F.S. 288. MAINTENANCE REPAIRED R/H HEAVY ANGLE AT F.S. 288. IAW BEECH 1900 SRM 53-90. REPAIR LENGTH APPROX 13 1/2 INCHES. RII C/W IAW TASKCARD 8.2.1.
- [SDR GLBA20060979](https://openairdocs.org/sdr/GLBA20060979.md): Frame · cracked · Aug 20, 2007 · N220GL · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - FUSELAGE FRAME CRACKED AT F.S. 177.35 RT STRINGER 9 AT RELIEF HOLE. MAINTENANCE STOP DRILLED AND PATCHED AFFECTED AREAS I.A.W. BEECH SRM 51-70. PATCH DIMENSIONS 3 INCH BY 2.4 INCH..080 2024 T3. RII COMPLIED WITH PER TASKCARD 8.2.1.
- [SDR GLBA20060914](https://openairdocs.org/sdr/GLBA20060914.md): Shimmy Dampener · missing · Feb 19, 2007 · N220GL · Beech 1900D · Shimmy Damper
  > UPON PRE-FLIGHT INSPECTION, PILOT REPORT OF SHIMMY DAMPENER DAMAGE/MISSING AND SUSPECTED DAMAGE TO STRUCTURE IN SURROUNDING AREA WAS ALSO REPORTED. MAINTENANCE REMOVED AND REPLACED THE SHIMMY DAMPER IAW B1900D MM 32-20. MAINENANCE REMOVED AND REPLACED STEERIN

Next page: https://openairdocs.org/aircraft/N220GL/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 = 'N220GL' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N220GL/reports

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