# Service difficulty reports: N211GL A list on [N211GL](https://openairdocs.org/aircraft/N211GL.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR GLBA2012090700048](https://openairdocs.org/sdr/GLBA2012090700048.md): Web · cracked · Sep 7, 2012 · N211GL · Beech 1900D · Horizontal Stabilizer Structure > DURING A SCHEDULED ROUTINE INSP FOUND 2 CRACKS IN THE HORIZONTAL STAB FWD WEB AT HSS 00.0 AND FS 630 AT THE DEICE TUBE HOLE, 1" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-028. MAJOR REPAIR - [SDR GLBA2012090600047](https://openairdocs.org/sdr/GLBA2012090600047.md): Rib · cracked · Sep 6, 2012 · N211GL · Beech 1900D · Wing, Rib/Bulkhead > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE LT WING INBD RIB AT BL 29.06 AND WING SPAR JUNCTION, RIBS DOUBLER, 1" IN LENGTH. REPAIRED AFFECTED AREA IAW EO 12-1900-57-010. MAJOR REPAIR - [SDR GLBA2012031601](https://openairdocs.org/sdr/GLBA2012031601.md): Spar · cracked · Mar 15, 2012 · N211GL · Beech 1900D · Horizontal Stabilizer, Spar/Rib > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK EXTENDING FROM THE 2 O'CLOCK POSITION ON THE AFT HORIZONTAL STAB SPAR CENTER WEB,.281" IN LENGTH. REPAIRED IAW FR-EO-02386. MAJOR REPAIR - [SDR GLBA20111219F](https://openairdocs.org/sdr/GLBA20111219F.md): Switch · dirty · Dec 17, 2011 · N211GL · Beech 1900D · Door Warning System > PILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. MX CLEANED THE SWITCH, OPS CHECKED GOOD. - [SDR GLBA20111212F](https://openairdocs.org/sdr/GLBA20111212F.md): Connector · damaged · Dec 11, 2011 · N211GL · Beech 1900D · Propeller/Propulsor System Wiring > PILOT REPORTED THAT THE AUTOFEATHER OFF ANNUNCIATOR ILLUMINATES WITH THE SWITCH ON DURING TAKEOFF, TESTED NORMAL. MX REPAIRED PIN 22 ON THE A123 PCB IAW MI 24-01, OPS CHECKED GOOD. - [SDR GLBA20111007F](https://openairdocs.org/sdr/GLBA20111007F.md): Door Frame · cracked · Oct 7, 2011 · N211GL · Beech 1900D · Fuselage Main, Structure > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, FOUND A CRACK ON THE DOOR LOWER FRAME AT FS 172-174, 2.5" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-058. MATERIALS UTILIZED ARE INCLUDED IN THE EO. - [SDR GLBA20110906G](https://openairdocs.org/sdr/GLBA20110906G.md): Bulb · inoperative · Sep 4, 2011 · N211GL · Beech 1900D · Landing Gear Selector > PILOT REPORTED THAT THE GEAR HANDLE HAS ONE RED LIGHT THAT IS INOPERATIVE. MAINTENANCE REPLACED THE BULB IAW BMM 33-10-05, OPS CHECKED GOOD. - [SDR GLBA201106241](https://openairdocs.org/sdr/GLBA201106241.md): Bulb · inoperative · Jun 24, 2011 · N211GL · Beech 1900D · Emergency Lighting > INSTRUMENT EMERGENCY LIGHT ON F/O SIDE INOPERATIVE. MX REPLACED THE BULBS PN 1864 IAW BMM 33-10-00, OPS CHECKED GOOD. - [SDR GLBA201105241](https://openairdocs.org/sdr/GLBA201105241.md): Line · worn · May 23, 2011 · N211GL · Beech 1900D · Landing Gear Retraction/Extension System > AUTO FEATHER OFF ANNUNCIATION ILLUMINATED WHEN THE AUTO FEATHER WAS TURNED OFF IN THE CLIMB. THE GEAR IN TRANSIT LIGHT THEN ILLUMINATED NO GREEN GEAR LIGHTS ILLUMINATED. DID NOT EXCEED 180 KNOTS. MAINTENANCE REPLACED THE LT MLG RETRACT LINE IAW AIM 10-32-01 - [SDR GLBA20110503F](https://openairdocs.org/sdr/GLBA20110503F.md): Frame · cracked · May 3, 2011 · N211GL · Beech 1900D · Fuselage Main, Frame > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND A CRACK IN CARGO DOOR FUSELAGE FWD FRAME AT F.S. 456, AT THE UPPER IB NUTPLATE AREA AT THE LONG GAS STRUT MOUNT, 1" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUI - [SDR GLBA20110502G](https://openairdocs.org/sdr/GLBA20110502G.md): Keel · cracked · May 2, 2011 · N211GL · Beech 1900D · Fuselage Main, Keel > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE RH NACELLE OB KEEL CRACKED AT GRAVEL FENDER WEB AND THINNED ABOVE CRACK AT UPPER 2 RIVETS. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11 - [SDR GLBA20110502J](https://openairdocs.org/sdr/GLBA20110502J.md): Frame · cracked · May 2, 2011 · N211GL · Beech 1900D · Fuselage Main, Frame > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND TWO CRACKS, FRAME AT F.S. 273.25 AND STRINGER 10L AND IN T-FRAME AT SAME LOCATION,.7" AND.9" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I - [SDR GLBA20110502F](https://openairdocs.org/sdr/GLBA20110502F.md): Skin · cracked · May 2, 2011 · N211GL · Beech 1900D · Fuselage Main, Plate/Skin > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND TWO CRACKS ON LT SIDE OF FUSELAGE UPWARD ALONG F.S. 273.25 AND STRINGER 10L, LENGTHWISE ALONG W.L. 93, 2.2" HIGH AND 4.2 WIDE IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED - [SDR GLBA201120110502H](https://openairdocs.org/sdr/GLBA201120110502H.md): Frame · cracked · May 2, 2011 · N211GL · Beech 1900D · Fuselage Main, Frame > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND FUSELAGE FRAME AT F.S. 456 AND STRINGER 10R CRACKED AT STRINGER CUTOUT,.3" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53 - [SDR GLBA20100910G](https://openairdocs.org/sdr/GLBA20100910G.md): Skin · burned · Sep 10, 2010 · N211GL · Beech 1900D · Ailerons > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A BURN HOLE IN THE RIGHT ELEVATOR 4" INBOARD OF OUTBOARD EDGE,.75" WIDE BY.625" DEEP. MAINTENANCE REPLACED THE RIGHT ELEVATOR, IAW BMM TC 1900-2730-00. REMOVED IN SERVICABLE CONDITION F - [SDR GLBA201007201](https://openairdocs.org/sdr/GLBA201007201.md): Circuit Board · burned · Jul 20, 2010 · N211GL · Beech 1900D · Electrical Power System > PILOT REPORTED THAT ON APPROACH TO PHX FO NOTICED A SYNTHETIC BURNING SMELL BRIEFLY, THEN GOT A BATT TIE ANNUNCIATOR LIGHT. MAINTENANCE INSPECTED THE ELECTRICAL SYSTEM AND FOUND CIRCUIT BOARD A130 HAD A BURNT DIODE, REPLACED BOARD IAW AIM 10-24-01, RAN AIRCRAF - [SDR GLBA201005151](https://openairdocs.org/sdr/GLBA201005151.md): Wire · damaged · May 14, 2010 · N211GL · Beech 1900D · Landing Gear System Wiring > UPON APPROACH TO LAND, SELECTED MLG DOWN IN WHICH THE PUMP SOUNDED, DID NOT RECEIVE INTRANSIT LIGHT & NO GREEN LIGHTS TO INDICATE SAFE MLG. PERFORMED SEVERAL TEST TO ENSURE MLG SAFETY. TASK INCLUDED TAXI LIGHT, AUTOFEATHER, FLAPS AT 35 AND THE GPWS. ALL TEST I - [SDR GLBA20090416A](https://openairdocs.org/sdr/GLBA20090416A.md): Control Handle · deteriorated · Apr 16, 2010 · N211GL · Beech 1900D · Landing Gear Selector > PILOTS REPORTED THAT THE LANDING GEAR CIRCUIT BREAKER TRIPPED, THEY OBSERVED 3 GREEN DOWN LIGHTS. PILOTS THEN RETARDED THE LOWER LEVERS BACK WITH GEAR DOWN AND GOT A GEAR HORN, THE C/B THEN POPPED AGAIN. A MANUAL EXTENSION WAS THEN PERFORMED. MX R & R THE L - [SDR GLBA20090925F](https://openairdocs.org/sdr/GLBA20090925F.md): Structure · damaged · Sep 23, 2009 · N211GL · Beech 1900D · Elevator Structure > LIGHTNING STRIKE ON THE LT ELEVATOR. DISCHARGE ON TRAILING EDGE APPROXIMATELY 9" TO 10.250" FROM TAB CUTOUT ON THE TOP AND BOTTOM SIDES. TRAILING EDGE DAMAGE APPROXIMATELY 1.5" BY.750" EIGHT INCHES OUT FROM TRIM TAB. MAINTENANCE REMOVED AND REPLACED THE ELEV - [SDR GLBA20090425A](https://openairdocs.org/sdr/GLBA20090425A.md): Cabin Pressure · malfunctioned · Apr 25, 2009 · N211GL · Beech 1900D · Cabin Pressure Control System > PILOTS REPORTED THAT UPON CLIMBING THE AIRCRAFT FAILED TO PRESSURIZE AND THEY THEN RETURNED TO FMN. MAINTENANCE OPERATIONALLY CHECKED THE SYSTEM ON THE GROUND WHICH WAS GOOD PER MM 21-30-00. OPERATIONAL CHECK FLIGHT WAS PERFORMED AND WAS SATISFACTORY. - [SDR GLBA200903041](https://openairdocs.org/sdr/GLBA200903041.md): Pedestal · out of adjust · Mar 4, 2009 · N211GL · Beech 1900D · Propeller Feathering/Reversing > UPON SHORT FINAL THE PILOTS REPORTED THAT THE RIGHT HAND PROPELLER BEGAN TO CYCLING IN AND OUT OF AUTOFEATHER. THE PILOT INCREASED POWER HOWEVER IT DID NOT FIX THE PROBLEM. PILOTS TURNED OF THE AFX AND IT STOPPED FEATHERING. MAINTENANCE INSPECTED THE AUTOFEATH - [SDR GLBA20090220J](https://openairdocs.org/sdr/GLBA20090220J.md): Frame · cracked · Feb 20, 2009 · N211GL · Beech 1900D · Fuselage Main, Frame > DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND ON FRAME AT FS 177.35 STRINGER 9R RELIEF CUTOUT. MAJOR REPAIR, MAINTENANCE DETERMINED THIS DID NOT MEET THE CRITERIA OF A MAJOR REPAIR, HOWEVER, MAINTENANCE REPAIRED THE AFFECTED AREA PER BEECH 1900 SRM 51-70-21. - [SDR GLB2008F00026](https://openairdocs.org/sdr/GLB2008F00026.md): Stiffener · cracked · Sep 3, 2008 · N211GL · Beech 1900D · Fuselage Miscellaneous Structure > DURING STRUCTURAL CHECK MAINT DISCOVERED A CRACK ON THE RT WHEEL WELL OB KEEL TAB TO OB FENDER STIFFENER 1" AT THE BOTTOM END OF STIFFENERS TO KEEL AREA. " SUPPLEMENTAL INFORMATION WILL BE PROVIDED UPON COMPLETION OF THE REPAIR". (K) - [SDR GLB2008F00025](https://openairdocs.org/sdr/GLB2008F00025.md): Frame · cracked · Sep 2, 2008 · N211GL · Beech 1900D · Fuselage Main, Frame > DURING STRUCTURAL INSPECTION MAINT FOUND FRAME CRACKED AT STRINGER CUTOUT AT FS 164.4 STRINGER 9AR. LENGTH OF CRACK APPROXIMATELY.5". MAINT REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE IAW SRM 51-70 AT FS 164.4 REPAIR APPROXIMATELY 5 INCH BY 2.5 INCH. 2024-T3 - [SDR GLB2008F00024](https://openairdocs.org/sdr/GLB2008F00024.md): Frame · cracked · Sep 2, 2008 · N211GL · Beech 1900D · Fuselage Main, Frame > DURING STRUCTURAL INSPECTION MAINTENANCE FOUND FRAME CRACKED AT STRINGER CUTOUT FS 177.3 AT STRINGER 9AR. LENGTH OF CRACK APPROXIMATELY.750". MAINTENANCE REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE IAW SRM 51-70 AT FS 177.3 AT STRINGER 9AR. REPAIR APPROXIMA - [SDR GLB2008F00020](https://openairdocs.org/sdr/GLB2008F00020.md): Frame · cracked · Sep 2, 2008 · N211GL · Beech 1900D · Fuselage Main, Frame > DURING STRUCTURAL INSP MAINT FOUND FRAME CRACKED AT STRINGER CUTOUT FS 177.3 AT STRINGER 9AR. LENGTH OF CRACK APPROXIMATELY.750. (K) - [SDR GLB2008F00019](https://openairdocs.org/sdr/GLB2008F00019.md): Frame · cracked · Sep 2, 2008 · N211GL · Beech 1900D · Fuselage Main, Frame > DURING STRUCTURAL INSPECTION MAINT FOUND FRAME CRACKED AT STRINGER CUTOUT AT FS 164.4 STRINGER 9AR. LENGTH OF CRACK APPROXIMATELY.5 INCH. OPEN (K) - [SDR GLB2008F00021](https://openairdocs.org/sdr/GLB2008F00021.md): Connector · loose · Aug 26, 2008 · N211GL · Beech 1900D · Propeller Governor > SUSPECTED AUTOFEATHER EVENT, UPON APPROACH, PILOTS REPORTED THAT RT AUTOFEATHER ACTUATED (AS IT NORMALLY DOES DURING TESTING) ON APPROACH AFTER A MINOR POWER INCREASE. MAINT REMOVED AND REPLACED THE OVERSPEED GOVERNOR IAW MM 61-20. OPS CHECK WAS GOOD, HOWEVER - [SDR GLB2008F00015](https://openairdocs.org/sdr/GLB2008F00015.md): Autofeather Sys · malfunctioned · Aug 15, 2008 · N211GL · Beech 1900D · Propeller Feathering/Reversing > ACFT 211GL SUSPECTED AUTOFEATHER FLT 5127 "PIR" 08/15/08 PILOTS REPORTED DURING FINAL DESCENT INTO LANDING, THAT POWER WAS REDUCED TO APPROX 500 LBS WITH PROPS FULL FORWARD. DURING POWER REDUCTION ONE OR BOTH PROPELLERS APPEARED TO FEATHER, THEN SURGE. POWER - [SDR GLB2008F00000](https://openairdocs.org/sdr/GLB2008F00000.md): Valve · worn · Jun 27, 2008 · N211GL · Beech 1900D · Landing Gear Retraction/Extension System > AC 211GL, AIR RETURN FLT NR 5066 "GBD" 06/27/08. PILOTS REPORTED THAT AFTER GEAR RETRACTION, THE GEAR WOULD NOT RETRACT. APPROXIMATE SPEED AT THE TIME WAS 106 KTS. "3" GREEN LIGHTS, NO RED GEAR UNSAFE LIGHTS. MAINTENANCE REMOVED AND REPLACED SERVICE VALVE IA - [SDR GLB2008F00007](https://openairdocs.org/sdr/GLB2008F00007.md): Landing Gear · malfunctioned · Jun 18, 2008 · N211GL · Beech 1900D · Landing Gear Retraction/Extension System > PILOTS REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT PROPERLY AND AIR RETURNED TO DEPARTURE. MAINT PERFORMED NUMEROUS GEAR RETRACTIONS AND EXTENSIONS IAW MM 32.00. NO DEFECTS WERE NOTED. (K) - [SDR GLBA20061106](https://openairdocs.org/sdr/GLBA20061106.md): Landing Gear · malfunctioned · May 23, 2008 · N211GL · Beech 1900D · Landing Gear Retraction/Extension System > AIR RETURN - FLIGHT 5031 ENROUTE, PILOTS REPORTED THAT THE GEAR WOULD NOT RETRACT PROPERLY. AIRCRAFT WAS FOUND SAFE FOR INTENDED FERRY FLIGHT TO WHERE MAINTENANCE PERFORMED NUMEROUS EXTENSIONS AND RETRACTIONS WITH NO DEFECTS NOTED IAW. MM 32-00. SUBSEQUENT OPE - [SDR GLBA20061079](https://openairdocs.org/sdr/GLBA20061079.md): Wire · detached · Mar 4, 2008 · N211GL · Beech 1900D · Ice/Rain Protection System Wiring > SMOKE/FUMES, FLIGHT 5061 AIR RETURN, PILOTS REPORTED THAT WHILE CLIMBING THROUGH 21.5 FOR 240 THEY NOTICED AN ELECTRICAL FUME ODOR. PILOTS PERFORMED WINDSHILED FAULT EMERGENCY CHECKLIST. TURNING OFF WINSHIELD ANTI-ICE GOT RID OF THE FUMES. MAINT SECURED A LOOS - [SDR GLBA20061011](https://openairdocs.org/sdr/GLBA20061011.md): Angle · cracked · Oct 9, 2007 · N211GL · Beech 1900D · Fuselage Miscellaneous Structure > LT HEAVY ANGLE CRACKED AT FS 288. MX REPAIRED THE LT HEAVY ANGLE AT FS 288 IAW BEECH 1900D SRM 53-90. REPAIR DIMENSIONS 13.5. PN 114-430002-7180. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1. - [SDR GLBA20060902](https://openairdocs.org/sdr/GLBA20060902.md): Unknown · odor · Feb 14, 2007 · N211GL · Beech 1900D · Air Distribution System > UNSCHEDULED LANDING DURING TRAINING, GLA FLIGHT 41. PILOTS REPORTED THAT THE AIRCRAFT HAD JUST BEEN FUELED AND AFTER TAKEOFF A STRONG FUEL ODOR WAS PRESENT. MAINTENANCE INSPECTED THE WINGS AND FUSELAGE FOR LEAKS, AIRED OUT CABIN AND PERFORMED ENVIRONMENTAL CHE - [SDR 20030856](https://openairdocs.org/sdr/20030856.md): Fire Loop · defective · Jun 25, 2005 · N211GL · Beech 1900D · Fire Detection > DURING FLIGHT, FLIGHT CREW NOTICED RT ENGINE T-HANDLE ANNUNCIATOR AND YELLOW (LOOP) ANNUCIATOR FLICKERING ON AND OFF AND WAS DETERMINED BY CREW THAT IT WAS A FALSE INDICATION. MAINTENANCE TROUBLESHOT PROBLEM TO DEFECTIVE RT AFT FIRE LOOP IN ENGINE COMPARTMENT. - [SDR GLBA20030646](https://openairdocs.org/sdr/GLBA20030646.md): Odor · detected · Jun 20, 2004 · N211GL · Beech 1900D · Air Distribution Fan > SMELL OF ELECTRICAL SMOKE IN COCKPIT, INSPECTED A/C SYSTEMS, FOUND NO DEFECTS. - [SDR GLBA20030648](https://openairdocs.org/sdr/GLBA20030648.md): Door · corroded · Jun 19, 2004 · N211GL · Beech 1900D · Passenger/Crew Doors > CABIN DOOR IS CORRODED AROUND BUTTON, REPAIRED CORROSION. - [SDR GLBA2003113](https://openairdocs.org/sdr/GLBA2003113.md): Uplock Switch · malfunctioned · Aug 3, 2003 · N211GL · Beech 1900D · Landing Gear Position and Warning > GEAR INTRANSIT LIGHT DID NOT EXTINGUISH. REMOVED AND REPLACED RT MLG UPLOCK SWITCH. - [SDR GLBA2003089](https://openairdocs.org/sdr/GLBA2003089.md): Skin · cracked · Jun 19, 2003 · N211GL · Beech 1900D · Fuselage Main, Plate/Skin > CRACK IN BELLY SKIN NEAR COMM ANT. REPAIRED SKIN IAW BEECH SRM. - [SDR GLBA2003044](https://openairdocs.org/sdr/GLBA2003044.md): Clutch · stuck · Apr 5, 2003 · N211GL · Beech 1900D · Elevator Tab Control System > ELEVATOR TRIM STUCK. REMOVED AND REPLACED ELEVATOR ELECTRIC TRIM MAGNETIC CLUTCH AND CONNECTING CABLE PULLEYS, OPS CK GOOD. - [SDR GLBA2003036](https://openairdocs.org/sdr/GLBA2003036.md): Wire · broken · Mar 21, 2003 · N211GL · Beech 1900D · Fire Protection System Wiring > LT ENGINE FIRE EXTINGUISHER DISCHARGE LIGHT ILLUM. REPAIRED BROKEN WIRE SPLICE ON LEFT ENG FIRE BOTTLE SQUIB. - [SDR GLBA202182](https://openairdocs.org/sdr/GLBA202182.md): Uplock Switch · malfunctioned · Nov 18, 2002 · N211GL · Beech 1900D · Landing Gear Position and Warning > IN-TRANSIT LIGHT STAYS ON WITH GEAR UP, R&R LT UP-LOCK SWITCH - [SDR GLBA2002135](https://openairdocs.org/sdr/GLBA2002135.md): Plug · missing · Aug 26, 2002 · N211GL · Beech 1900D · Pneumatic Distribution System > RT BLEED FAIL ON TAKE OFF, REPLACED EVA TUBE PLUG OPS CHECK OK. - [SDR GLBA2002109](https://openairdocs.org/sdr/GLBA2002109.md): Switch · stuck · Jul 26, 2002 · N211GL · Beech 1900D · Communications System > #1 COMM FAILED, REPLACED PTT SWITCH OPS CHECKED SATISFACTORY - [SDR GLBA2002076](https://openairdocs.org/sdr/GLBA2002076.md): Cable · broken · Jun 2, 2002 · N211GL · Beech 1900D · Passenger/Crew Doors > CABIN DOOR WILL NOT OPEN. REPLACED INNER DOOR CABLES, OPS CHECKED SYSTEM SATISFACTORY. - [SDR GLBA2002023](https://openairdocs.org/sdr/GLBA2002023.md): Terminal · loose · Feb 21, 2002 · N211GL · Beech 1900D · Trailing Edge Flap Actuator > FLAPS STUCK AT 17 PERCENT, FOUND LOOSE TERMINAL ON MOTOR RELAY. SECURED, OPS CHECKED SYSTEM SATISFACTORY. - [SDR GLBA2001234](https://openairdocs.org/sdr/GLBA2001234.md): Indicator · leaking · Nov 27, 2001 · N211GL · Beech 1900D · Indicating/Recording System > AIR SPEED INDICATOR FAILED ON T/O, REPLACED OPS CHECKED SYSTEM SATISFACTORY - [SDR GLBA2001194](https://openairdocs.org/sdr/GLBA2001194.md): Seal · deteriorated · Sep 1, 2001 · N211GL · Beech 1900D · Air Distribution System > CABIN PRESSURIZATION INOPERATIVE. REPLACED SEAL IN RIGHT WING ROOT, OPS CHECKED SYSTEM SATISFACTORY. - [SDR GLBA2001184](https://openairdocs.org/sdr/GLBA2001184.md): Relay · failed · Aug 20, 2001 · N211GL · Beech 1900D · Landing Gear System > LANDING GEAR CIRCUIT BREAKER POPPED. REPLACED K3 RELAY AND A316 PCB, OPS CHECKED SYSTEM SATISFACTORY. ## 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 = 'N211GL' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N211GL/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.