# Service difficulty reports: N210GL, cancelled Jun 29, 2026

A list on [N210GL, cancelled Jun 29, 2026](https://openairdocs.org/deregistered/N210GL-2026-06-29.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 · 62 reports

- [SDR TIMA20250215002](https://openairdocs.org/sdr/TIMA20250215002.md): Unknown · odor · Feb 15, 2025 · N210GL · Beech 1900D · Air Distribution System
  > WHILE IN CRUISE FLIGHT AT 10,000FT PILOT BEGAN TO SMELL SOMETHING SUSPICIOUS. MOMENTS LATER THE PILOT EXPERIENCED A LEFT AC BUS FAILURE AND BEGAN TO SEE SMOKE COMING FROM UNDERNEATH THE CO-PILOTS SIDE OF THE AVIONICS PANEL. IMMEDIATELY PROCEEDED WITH THE MEMO
- [SDR GLBA2015042700515](https://openairdocs.org/sdr/GLBA2015042700515.md): Check Valve · leaking · Apr 25, 2015 · N210GL · Beech 1900D · Aircraft Fuel Distribution System
  > SIG EVENT, PILOT REPORTED THAT THERE WAS A STRONG SMELL OF FUEL IN CABIN. REMOVED FLOORBOARDS & INSPECTED FUEL TRANSFER LINES, PRESSURIZED & LEAK CHECKED FUEL LINES, NO DISCREPANCIES NOTED. INOPERATIVE LT & RT ENG ACCESSORIES FOR FUEL LEAKS, NO LEAKS NOTED A
- [SDR GLBA2014022800389](https://openairdocs.org/sdr/GLBA2014022800389.md): Motor · faulty · Feb 26, 2014 · N210GL · Beech 1900D · Trailing Edge Flap Actuator
  > PILOT REPORTED THAT THERE WAS A STRONG BURNING SMELL COMING FROM THE CABIN & IS IRRITATING TO TO EYES. TROUBLESHOT BURNING SMELL COMING FROM FLAP GEAR BOX MOTOR ASSEMBLY. R & R FLAP GEAR BOX MOTOR ASSEMBLY PN 100-524073-1 SN OFF 5693, IAW BMM 27-50-03 OPERAT
- [SDR GLBA2014021300383](https://openairdocs.org/sdr/GLBA2014021300383.md): Motor · faulty · Feb 12, 2014 · N210GL · Beech 1900D · Trailing Edge Flap Actuator
  > PILOT REPORTED THAT WHEN THEY WENT TO EXTEND THE FLAPS HAD A STRONG ELECTRICAL SMELL & THE FLAPS DID NOT EXTEND. MAINTENANCE R&R FLAP GEAR BOX MOTOR P/N 100-524073-1 S/N OFF 6137 S/N ON. 5693 OPS CHECK GOOD AT THIS TIME REF 1900DMM 27-50-03.
- [SDR GLBA2013091300310](https://openairdocs.org/sdr/GLBA2013091300310.md): Skin · cracked · Sep 12, 2013 · N210GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION, FOUND THE LT LOWER BELLY SKIN AT FS 288 CRACKED, 1.75" IN LENGTH. REPAIRED IAW EO 13-1900-53-059. MAJOR REPAIR.
- [SDR GLBA2013090900306](https://openairdocs.org/sdr/GLBA2013090900306.md): Fire Loop · chafed · Sep 6, 2013 · N210GL · Beech 1900D · Fire Detection
  > SIG EVENT - PILOT REPORTED THAT THE RT FIREWALL FUEL VALVE T-HANDLE FLICKERED ON AND OFF IN FLIGHT. MX TESTED FIRE LOOP ON RT SIDE, TESTED NORMAL. INSPECTED FWD AND AFT LOOP FOUND CHAFE ON TOP SIDE OF FWD LOOP. R & R LOOP IAW BMM 26-10-01. OPS CHECK GOOD AT
- [SDR GLBA2013052900255](https://openairdocs.org/sdr/GLBA2013052900255.md): Pressure Blkhd · cracked · May 29, 2013 · N210GL · Beech 1900D · Fuselage Main, Bulkhead
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND 4 CRACKS IN THE FWD PRESSURE BULKHEAD, RT WEB AT FS 84.00, CRACKS AT THE INBD EDGE OF WEB ATTACHING FASTENERS, 2" IN LENGTH. REPAIRED IAW EO 13-1900-53-044. MAJOR REPAIR.
- [SDR GLBA2013052900254](https://openairdocs.org/sdr/GLBA2013052900254.md): Pressure Blkhd · cracked · May 29, 2013 · N210GL · Beech 1900D · Fuselage Main, Bulkhead
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND 7 CRACKS IN THE FWD PRESSURE BULKHEAD, LT WEB AT FS 84.00, CRACKS AT INBD EDGE OF WEB ATTACHING FASTENERS, 3.5" IN LENGTH. REPAIRED IAW EO 13-1900-53-044. MAJOR REPAIR.
- [SDR GLBA2013052800253](https://openairdocs.org/sdr/GLBA2013052800253.md): Frame · cracked · May 28, 2013 · N210GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FUSELAGE FRAME AT FS 177.35 IN THE BEND RADIUS, 1" LENGTH. REPAIRED IAW EO 13-1900-53-043. MAJOR REPAIR.
- [SDR GLBA2013052800252](https://openairdocs.org/sdr/GLBA2013052800252.md): Frame · cracked · May 28, 2013 · N210GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND 2 CRACKS AT THE CARGO DOOR FUSELAGE FRAME AT FS 509 BETWEEN STRINGER 4L & 5L, LOCATED IN THE BEND RADIUS OF THE FRAME, 1" IN LENGTH. REPAIRED IAW EO 13-1900-53-042. MAJOR REPAIR.
- [SDR GLBA2013040100222](https://openairdocs.org/sdr/GLBA2013040100222.md): Structure · cracked · Apr 1, 2013 · N210GL · Beech 1900D · Horizontal Stabilizer Structure
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE TEE SECTION OF THE LT HORIZONTAL STAB LOWER AT HSS 5.000 AND 10.5 PERCENT AT A SCREW HOLE,.5" IN LENGTH. REPAIRED IAW EO 13-1900-55-011. MAJOR REPAIR.
- [SDR GLBA2013032900219](https://openairdocs.org/sdr/GLBA2013032900219.md): Skin · cracked · Mar 28, 2013 · N210GL · Beech 1900D · Horizontal Stabilizer, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK EXTENDING FROM A SCREW HOLE ON THE TOP SIDE OF THE LT HORIZONTAL STAB AT HSS 5.000 AND 10.5 PERCENT CHORD, ON THE FLANGE FOR PANEL 332 BTC ON THE FORWARD LT CORNER,.25" IN LENGTH. REPAIRED IAW EO 13-1900-55
- [SDR GLBA2013032900218](https://openairdocs.org/sdr/GLBA2013032900218.md): Structure · cracked · Mar 28, 2013 · N210GL · Beech 1900D · Horizontal Stabilizer Structure
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE RT HORIZONTAL STAB LOWER TEE SECTION AT HSS 5.000 AND 10.5 PERCENT CHORD, 1.5" IN LENGTH. REPAIRED IAW EO 13-1900-55-010. MAJOR REPAIR.
- [SDR GLBA2012120400126](https://openairdocs.org/sdr/GLBA2012120400126.md): Spar Cap · cracked · Dec 4, 2012 · N210GL · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE LT FWD SPAR CAP ANGLE, RADIATES FROM THE UPPER FWD TASTENER UPWARD TO EDGE OF SPAR CAP,.375" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW FR-CO-02586, STEP 1. MAJOR REPAIR
- [SDR GLBA2012083100043](https://openairdocs.org/sdr/GLBA2012083100043.md): Skin · burned · Aug 31, 2012 · N210GL · Beech 1900D · Elevator, Plate/Skin
  > .5 X.5 INCH BURN HOLE IN TOP AND BOTTOM SKIN, 3.8750" CENTER FROM OTBD TIP OF LT ELEVATOR T/E. REPAIRED THE AFFECTED AREA IAW EO 12-1900-27-002.
- [SDR GLBA2012040203](https://openairdocs.org/sdr/GLBA2012040203.md): Skin · damaged · Apr 2, 2012 · N210GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND THE RT FUSELAGE FS 288 HAS ELONGATED HOLES FROM ATTACHING FAIRING PANEL TO FS 327. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-019. MATERIALS UTILIZED ARE INCLUDED IN T
- [SDR GLBA2012040202](https://openairdocs.org/sdr/GLBA2012040202.md): Fairing · damaged · Apr 2, 2012 · N210GL · Beech 1900D · Aerodynamic Fairings
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A HOLE IN THE FUSELAGE FARING, RT SIDE UNDER AFT WING, AFT OF FS 363.250, 2.25 INCHES JUST ABOVE STRINGER 1R,.687 BY.25. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-01
- [SDR GLBA2012032101](https://openairdocs.org/sdr/GLBA2012032101.md): Spar · cracked · Mar 20, 2012 · N210GL · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND FOUR CRACKS AT A MACHINED HOLE AT 2, 8, 10, & 4 O'CLOCK POSITIONS AT THE HORIZONTAL STAB AFT SPAR WEB AT HSS 0.0,.73" IN LENGTH. ED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-55-008. MATERIALS UTIL
- [SDR GLBA201203191205](https://openairdocs.org/sdr/GLBA201203191205.md): Skin · chafed · Mar 19, 2012 · N210GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND 2 RIVET HEADS CHAFING ON A PREVIOUS REPAIR OF THE LOWER RT WING WHERE THE FUSELAGE MEETS THE WING. REPAIRED IAW EO 12-1900-53-014. MAJOR REPAIR.
- [SDR GLBA2012031904](https://openairdocs.org/sdr/GLBA2012031904.md): Attach Fitting · cracked · Mar 19, 2012 · N210GL · Beech 1900D · Cargo/Baggage Doors
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK AT THE NUTPLATE, FWD CARGO DOOR SNUBBER FUSELAGE ATTACH POINT, UPPER IB NUTPLATE FS 456,.35" IN LENGTH. REPAIRED IAW EO 12-1900-53-014. MAJOR REPAIR
- [SDR GLBA2012031903](https://openairdocs.org/sdr/GLBA2012031903.md): Skin · cracked · Mar 19, 2012 · N210GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FUSELAGE SKIN, LT BELLY AT FS 303.25 WHERE THE FUSELAGE MEETS THE WING, 5" IN LENGTH. REPAIRED IAW EO 12-1900-53-015. MAJOR REPAIR
- [SDR GLBA2012031902](https://openairdocs.org/sdr/GLBA2012031902.md): Frame · cracked · Mar 19, 2012 · N210GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FRAME AT FS 150.6 BETWEEN STRINGERS 2R AND 3R,.9" IN LENGTH. REPAIRED IAW EO 12-1900-53-016. MAJOR REPAIR
- [SDR GLBA2012031901](https://openairdocs.org/sdr/GLBA2012031901.md): Doubler · cracked · Mar 19, 2012 · N210GL · Beech 1900D · Fuselage Main, Structure
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE RT DOUBLER, FWD END, FS 288, 1.2" IN LENGTH. REPAIRED IAW EO 12-1900-53-017.
- [SDR GLBA2012022101](https://openairdocs.org/sdr/GLBA2012022101.md): Warning Light · false activation · Feb 18, 2012 · N210GL · Beech 1900D · Landing Gear Position and Warning
  > PILOT REPORTED THAT THE GEAR INTRANSIT LIGHT ILLUMINATED IN FLIGHT, RAN CHECKLIST, GEAR OPERATED NORMALLY TO THE EXTENDED POSITION, EMERGENCY DECLARED, LANDED SAFELY. MX COULD NOT DUPLICATE, REPLACED THE NLG UPLOCK SWITCH IAW TC 1900-3260.00, OPS CHECKED GOOD
- [SDR GLBA20120209F](https://openairdocs.org/sdr/GLBA20120209F.md): Circuit Board · damaged · Feb 8, 2012 · N210GL · Beech 1900D · Landing Gear System Wiring
  > PILOT REPORTED THAT THE LANDING GEAR DID NOT EXTEND WHEN SELECTED AND RELAY CIRCUIT BREAKER TRIPPED, MANUALLY EXTENDED GEAR, NO IN-TRANSIT LIGHTS, LANDED SAFELY. MX REPLACED THE PCB A116 AND THE LANDING GEAR RELAY, OPS CK GOOD.
- [SDR GLBA20111208F](https://openairdocs.org/sdr/GLBA20111208F.md): Actuator · inoperative · Dec 7, 2011 · N210GL · Beech 1900D · Landing Gear Actuator
  > PILOT REPORTED THAT THE LEFT GEAR INDICATION DID NOT SHOW DOWN AND LOCKED UNTIL APPROX 25 SECONDS AFTER THE HANGLE WAS PLACED IN THE DOWN POSITION. MX REPLACED THE LT MLG ACTUATOR IAW TC 1900-3230.10, PN: 114-300041-15, SN: 0561A, OPS CK GOOD.
- [SDR GLBA20111128F](https://openairdocs.org/sdr/GLBA20111128F.md): Solenoid · dirty · Nov 27, 2011 · N210GL · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT THE ACFT YAWED TO THE LT IN THE LANDING FLARE. MX CLEANED THE LOW PITCH SOLENOID, OPS CHECKED GOOD.
- [SDR GLBA20110809F](https://openairdocs.org/sdr/GLBA20110809F.md): Wire · chafed · Aug 8, 2011 · N210GL · Beech 1900D · Door System Wiring
  > PILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR REMAINS EXTINGUISHED WHEN THE DOOR IS OPENED UP UNTIL ABOUT A FOOT OPEN. MX INSPECTED WIRE AT AIRSTAIR DOOR FOUND 4 CHAFED WIRES, REPAIRED WIRE. PERFORMED CABIN DOOR AM LIGHTING SYS CK, OPS CK GOOD REF CHAP 14,
- [SDR GLBA20110803G](https://openairdocs.org/sdr/GLBA20110803G.md): Switch · inoperative · Aug 2, 2011 · N210GL · Beech 1900D · Door Warning System
  > PILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR GOES OUT WITHOUT LOCKING THE DOOR. MX CLEANED THE MICRO SWITCHES, OPS CK GOOD.
- [SDR GLBA20110802G](https://openairdocs.org/sdr/GLBA20110802G.md): Switch · inoperative · Aug 1, 2011 · N210GL · Beech 1900D · Door Warning System
  > PILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR WENT OUT BEFORE THE DOOR WAS LOCKED. MX CLEANED THE CABIN DOOR MICRO SWITCH REF AIM 14.3.0, OK FOR SERVICE.
- [SDR GLBA20110801H](https://openairdocs.org/sdr/GLBA20110801H.md): Actuator · inoperative · Jul 29, 2011 · N210GL · Beech 1900D · Landing Gear Actuator
  > PILOT REPORTED THAT THE LT MLG BOTH GREEN "L" AND "H" ANNUNCIATORS FLICKERED THEN EXTINGUISHED THEN REILLUMINATED, NO UNSAFE INDICATIONS ON APPROACH & LANDING. MX REPLACED THE LT MLG ACTUATOR, OPS AND RIG CKS IAW TC. 1900-3230.10.
- [SDR GLBA20110706P](https://openairdocs.org/sdr/GLBA20110706P.md): Switch · out of rig · Jul 4, 2011 · N210GL · Beech 1900D · Trailing Flap Position Indicating System
  > PILOT REPORTED THAT UPON RAISING THE LANDING GEAR WHILE FLAPS AT 17 DEGREES. TAKEOFF GEAR WARNING HORN SOUNDED AND COULD NOT BE SILENCED. IN TRANSIT LIGHT REMAINED ILLUMINATED UNTIL FLAPS 0 DEGREES WAS OBTAINED. MX RIGGED LANDING GEAR WARNING HORN FLAP POSIT
- [SDR GLBA20110606G](https://openairdocs.org/sdr/GLBA20110606G.md): Switch · stuck · Jun 4, 2011 · N210GL · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT WITH THE CABIN DOOR OPEN THE CABIN ANNC DID NOT ILLUMINATE. MX CLEANED THE MICRO SWITCH, SYS OPS CK GOOD.
- [SDR GLBA20110603F](https://openairdocs.org/sdr/GLBA20110603F.md): Keelbeam · gouged · Jun 1, 2011 · N210GL · Beech 1900D · Fuselage Main, Keel
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, MX FOUND A GOUGE IN THE RT OTBD KEEL BY A CLAMP ON THE RETRACT/EXTEND LINE FOR THE LT MLG ACTUATOR. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-57-006. MATERIA
- [SDR GLBA20110602F](https://openairdocs.org/sdr/GLBA20110602F.md): Keelbeam · gouged · Jun 1, 2011 · N210GL · Beech 1900D · Fuselage Main, Keel
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, MX FOUND A GOUGE IN THE LT OTBD KEEL BY A CLAMP ON THE RETRACT/EXTEND LINE FOR THE LT MLG ACTUATOR. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-57-005. MATERIAL
- [SDR GLBA20101206A](https://openairdocs.org/sdr/GLBA20101206A.md): Bleed Air Sys · inoperative · Dec 6, 2010 · N210GL · Beech 1900D · Engine Bleed Air System
  > CLIMBING THROUGH 20,000 FT COULDN'T GET CABIN TO QUIT CLIMBING, HAD TO DEPLOY MASKS & RETURN TO DEPARTURE, DIR STUCK AT 3.4 PSI WOULD NOT GO HIGHER. STOWED & RELOCKED MASKS IAW MM 35-20-01. RAN ENG & PRESSURIZED - NO AIR FROM LT BLEED, REMOVED ORIFICE PLATE F
- [SDR GLBA20100819F](https://openairdocs.org/sdr/GLBA20100819F.md): Fastener · loose · Aug 18, 2010 · N210GL · Beech 1900D · Wing Main, Frame Structure
  > SIG EVENT - PILOT REPORTED THAT AN OVERWHELMING ODOR OF FUEL ENTER THE CABIN AND COCKPIT. MAINTENANCE FOUND LOOSE FASTENERS JUST OUTBOARD OF RT NACELLE AT FORWARD SPAR, REPLACED FASTENERS AND SEALED AREA, REFUELED, NO LEAKS OR ODOR PRESENT IAW SRM 51-10-00, C
- [SDR GLBA20100818B](https://openairdocs.org/sdr/GLBA20100818B.md): Fuel Sys · leaking · Aug 18, 2010 · N210GL · Beech 1900D · Fuel Storage
  > OVERWHELMING ODORS OF JET FUEL PRESENT IN CABIN COCKPIT EXTREMELY BAD TO A POINT OF BEING NAUSEATING AND AFFECTING SAFETY SLOW DRIP UNDER RT NACELLE DIFFERENT AREA THAN REPAIR.
- [SDR GLBA20100802J](https://openairdocs.org/sdr/GLBA20100802J.md): Bulkhead · cracked · Aug 2, 2010 · N210GL · Beech 1900D · Fuselage Main, Bulkhead
  > DURING A SCHEDULED ROUTINE INSPECTION A CRACK WAS FOUND AT THE AFT CARGO BAY FLOORBOARD FORWARD SUPPORT BULKHEAD AT F.S. 531.0 LH SIDE WHERE IT ATTACHES TO THE FRAME, 13/16" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPE
- [SDR GLBA20100802K](https://openairdocs.org/sdr/GLBA20100802K.md): Bulkhead · buckled · Aug 2, 2010 · N210GL · Beech 1900D · Fuselage Main, Bulkhead
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A BULKHEAD AT FS 531 AFT CARGO FLOORBOARD FORWARD SUPPORT BUCKLED ABOUT 11/32" AT TOP, TOTAL DAMAGE AREA ABOUT 26" IN LENGTH, AND A.5" CRACK IN THE RADIUS 12" FROM RT SIDE. MAINTENANCE REPAIRED THE AFFECTE
- [SDR GLBA20100730F](https://openairdocs.org/sdr/GLBA20100730F.md): Skin · cracked · Jul 30, 2010 · N210GL · Beech 1900D · Emergency Exits
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A CRACK IN THE SKIN WAS FOUND ON THE EMERGENCY EXIT DOOR 6A, LOWER FORWARD CORNER, 2" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-52-003. M
- [SDR GLBA20100728F](https://openairdocs.org/sdr/GLBA20100728F.md): Frame · cracked · Jul 27, 2010 · N210GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUNTINE INSP A CRACK WAS FOUND IN THE FRAME ANGLE AT FS 303,.5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-045. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDE
- [SDR GLBA20100729G](https://openairdocs.org/sdr/GLBA20100729G.md): Frame · cracked · Jul 27, 2010 · N210GL · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, A2 CRACKS WAS FOUND IN THE FRAME AT FS 456 AND STRINGER 10R CUTOUT,.45" AND.5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-046. MATERIALS UTI
- [SDR GLBA20100409F](https://openairdocs.org/sdr/GLBA20100409F.md): Skin · punctured · Apr 9, 2010 · N210GL · Beech 1900D · Passenger/Crew Doors
  > COMPONENT MAJOR REPAIR - UPON RECEIVING A SERVICEABLE AIRSTAIR DOOR THAT WAS PURCHASED, IT WAS DETERMINED THAT IT REQUIRED A MAJOR REPAIR ON THE EXTERIOR DOOR SKIN DUE TO 3 SCRATCHES AND 1 PUNCTURE THROUGH THE SKIN. MX REPAIRED THE AFFECTED AREA AND PERFORMED
- [SDR GLBA20090807F](https://openairdocs.org/sdr/GLBA20090807F.md): Unknown · odor · Aug 6, 2009 · N210GL · Beech 1900D · Air Distribution System
  > PILOTS REPORTED THAT A STRONG FUEL ODOR FROM THE VENTS IN THE FLIGHT DECK AND CABIN WAS PRESENT. MAINTENANCE INSPECTED THE NR 1 AND 2 ENGINES FOR LEAKS OF WHICH NONE WERE FOUND AND SUBSEQUENTLY PERFORMED INDIVIDUAL ENGINE RUNS WITH NO FUEL ODORS NOTED. REFEREN
- [SDR GLBA20090504F](https://openairdocs.org/sdr/GLBA20090504F.md): Structure · corroded · Apr 28, 2009 · N210GL · Beech 1900D · Passenger/Crew Doors
  > MAJOR REPAIR - AIRSTAIR DOOR WAS FOUND CORRODED ON LOWER END CLOSURE AREA. MAINTENANCE REMOVED A SECTION OF THE LOWER INNER DOOR PAN, CLEANED CORROSIONFROM INNER MATERIAL, INTALLED NEW LOWERE DOOR PAN AND INSTALLED THE HINGE ASSEMBLY IAW EO 09-1900-52-001.
- [SDR GLBA200904225](https://openairdocs.org/sdr/GLBA200904225.md): Pressure Switch · worn · Apr 22, 2009 · N210GL · Beech 1900D · Propeller Feathering/Reversing
  > ON APPROACH AT 500 LBS TORQUE, WHILE LEVELING ALTITUDE AND ADVANCING POWER THE R/H ENGINE ATTEMPTED FEATHER CAUSING CYCLES SIMILAR TO AUTOFEATHER TEST. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND AUTOFEATHER LOW PRESSURE SWITCH AND COMPLIED WITH FCD 1900-0
- [SDR GLBA20090205A](https://openairdocs.org/sdr/GLBA20090205A.md): Circuit Board · shorted · Feb 5, 2009 · N210GL · Beech 1900D · Propeller Feathering/Reversing
  > SUSPECTED AUTO FEATHER - PILOTS REPORTED THAT ON SHORT FINAL THE RT ENGINE CYCLED IN AND OUT OF FEATHER. MX R&R THE A123 PRINTED CIRCUIT BOARD AND OPS CHECKED THE SYSTEM IAW MM 61-21-00.
- [SDR GLBA200901093](https://openairdocs.org/sdr/GLBA200901093.md): Switch · dirty · Jan 7, 2009 · N210GL · Beech 1900D · Propeller Feathering/Reversing
  > SIGNIFICANT EVENT - PILOTS REPORTED THAT THE RT ENG AUTOFEATHERED IN FLIGHT AND CAUSED SURGES AND EXTREME YAWING MOTION. MX CLEANED AFX SWITCHES IAW BMM 61-21-01-201. OPS CHECKS WERE OK.
- [SDR GLBA20061041](https://openairdocs.org/sdr/GLBA20061041.md): Bulb · burned out · Jan 1, 2008 · N210GL · Beech 1900D · Emergency Lighting
  > SMOKE/ODOR - PILOTS REPORTED THE GLARESHIELD INSTRUMENT EMERGENCY LIGHTS WERE SMOKING ON THE GROUND AFTER STARTING ENGINES. REMOVED EMERGENCY FUSE F127. MAINTENANCE REMOVED EMERGENCY FUSE F127 AND REMOVED AND REPLACED BULB IAW MM 33-10. OPERATIONAL CHECK GO

Next page: https://openairdocs.org/deregistered/N210GL-2026-06-29/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 = 'N210GL' AND deregistration_id = 'N210GL-2026-06-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N210GL-2026-06-29/reports

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