# Service difficulty reports: N195GL

A list on [N195GL](https://openairdocs.org/aircraft/N195GL.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 · 85 reports

- [SDR GLBA2018030800702](https://openairdocs.org/sdr/GLBA2018030800702.md): Cable · frayed · Mar 6, 2018 · N195GL · Beech 1900D · Passenger/Crew Doors
  > MAINTENANCE REPORTED THAT THE AIRSTAIR DOOR LOWER FORWARD HANDRAIL CABLE IS FRAYED. MAINTENANCE REMOVED AND REPLACED AIRSTAIR DOOR LOWER FORWARD HANDRAIL CABLE IAW MM 52-10-02.
- [SDR GLBA2017121500697](https://openairdocs.org/sdr/GLBA2017121500697.md): Door Frame · cracked · Dec 15, 2017 · N195GL · Beech 1900D · Fuselage Main, Structure
  > MAJOR REPAIR - MAINTENANCE NOTED THAT THE FUSELAGE DOOR FRAME WAS CRACKED AT STRINGER 11L AND FS 171.0. CRACK IS APPROXIMATELY 1.1 INCHES IN LENGTH. ** SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR AND RETENTION OF THE PAPERWORK. **
- [SDR GLBA2017081800678](https://openairdocs.org/sdr/GLBA2017081800678.md): Hinge · loose · Aug 15, 2017 · N195GL · Beech 1900D · Passenger/Crew Doors
  > MAINTENANCE REPORTED THAT THE AIRCRAFT SIDE OF THE AIRSTAIR DOOR HINGE HAD AFT RIVETS WHICH WERE LOOSE. REMOVED AND REPLACED LOOSE RIVETS REF SRM 51-40-03.
- [SDR GLBA2017063000669](https://openairdocs.org/sdr/GLBA2017063000669.md): Cable · worn · Jun 28, 2017 · N195GL · Beech 1900D · Passenger/Crew Doors
  > MAINTENANCE REPORTED THAT THE UPPER AFT AIRSTAIR CABLE IS WORN. REMOVED AND REPLACED THE UPPER AFT AIRSTAIR CABLE IAW AMM 52-10-02.
- [SDR GLBA2017063000668](https://openairdocs.org/sdr/GLBA2017063000668.md): Cable · worn · Jun 28, 2017 · N195GL · Beech 1900D · Passenger/Crew Doors
  > MAINTENANCE REPORTED THAT THE UPPER FWD AIRSTAIR CABLE IS WORN. REMOVED AND REPLACED THE UPPER FWD AIRSTAIR CABLE IAW AMM 52-10-02. PN OFF/ON: 1440-42GLA, NSN.
- [SDR GLBA2017051000654](https://openairdocs.org/sdr/GLBA2017051000654.md): Circuit Breaker · popped · May 8, 2017 · N195GL · Beech 1900D · Landing Gear Retraction/Extension System
  > SIG EVENT, THE CREW DECLARED AN EMERGENCY ON APPROACH FOR LANDING [GEAR] FAILED TO EXTEND NORMALLY. IN TRANSIT LIGHT ILLUMINATED. MAINTENANCE FOUND 60A(CB11) POPPED, INSPECTED WIRES FROM BUS BAR TO C/B TO GEAR MOTOR, NO FAULTS FOUND AIM 14.3. RESET C/B 11 & C/
- [SDR GLBA2017041300648](https://openairdocs.org/sdr/GLBA2017041300648.md): Pressure Switch · dirty · Apr 11, 2017 · N195GL · Beech 1900D · Propeller Feathering/Reversing
  > THE CREW NOTED THAT THEY EXPERIENCED AN UNSCHEDULED AUTOFEATHER CYCLING DURING APPROACH TO LAND. THE ISSUE OCCURRED ON THE RIGHT ENGINE. MAINTENANCE REMOVED AND INSTALLED RIGHT ENGINE COWL IAW TC 1900-7100.10 STEPS 1, 2, 13, AND 14. CLEANED RIGHT LOW PRESSURE
- [SDR GLBA2017020300632](https://openairdocs.org/sdr/GLBA2017020300632.md): Cable · broken · Feb 2, 2017 · N195GL · Beech 1900D · Passenger/Crew Doors
  > MAINTENANCE NOTED THAT THE LOWER FWD AIRSTAIR DOOR CABLE WAS BROKEN.
- [SDR GLBA2017012500630](https://openairdocs.org/sdr/GLBA2017012500630.md): Cable · broken · Jan 23, 2017 · N195GL · Beech 1900D · Passenger/Crew Doors
  > SIG EVENT, PILOT REPORTED THAT THE A/S DOOR CABLE BROKE. ** SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR AND RETENTION OF THE PAPERWORK. **
- [SDR GLBA2016071300596](https://openairdocs.org/sdr/GLBA2016071300596.md): Snubber · disconnected · Jul 12, 2016 · N195GL · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE AIRSTAIR DOOR SNUBBER ARM CENTER PIVOT BOLT WAS DISCONNECTED. OPEN
- [SDR GLBA2015032300506](https://openairdocs.org/sdr/GLBA2015032300506.md): Skin · cracked · Mar 23, 2015 · N195GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION MX FOUND 2 CRACKS IN THE LT FUSELAGE SKIN UNDER THE VORTEX GEN MOUNT AREA. FWD SKIN CRACK IS.9" IN LENGTH AT FS 238.25, STRINGER 12L, & AFT SKIN CRACK IS 1.0" IN LENGTH AT FS 248.25, STRINGER 12L, CRACK 1.9" IN TOTAL LENGTH. RE
- [SDR GLBA2015032000505](https://openairdocs.org/sdr/GLBA2015032000505.md): Frame · cracked · Mar 20, 2015 · N195GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE FUSELAGE FRAME REPAIR & FRAME AT FS 163.975, STRINGER 10R, FRAME CRACK BEYOND STOP DRILL,.65" IN LENGTH. REPAIRED THE FRAME IAW EO 15-1900-53-004. MAJOR REPAIR.
- [SDR GLBA2015031900503](https://openairdocs.org/sdr/GLBA2015031900503.md): Channel · cracked · Mar 19, 2015 · N195GL · Beech 1900D · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE FUSELAGE CHANNEL AT BS 177.35, IN THE BEND RADIUS AT THE OTBD END OF THE CHANNEL, 1.2 INCH IN LENGTH. REPAIRED IAW EO 15-1900-53-002. MAJOR REPAIR.
- [SDR GLBA2015031900504](https://openairdocs.org/sdr/GLBA2015031900504.md): Frame · cracked · Mar 19, 2015 · N195GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION, MX FOUND A CRACK IN THE FUSELAGE FRAME AT FS 177.35 IN THE BEND RADIUS AT THE OTBD END OF THE FRAME, 1.25" IN LENGTH. REPAIRED THE FRAME IAW EO 15-1900-53-003. MAJOR REPAIR.
- [SDR GLBA2015010200488](https://openairdocs.org/sdr/GLBA2015010200488.md): Snubber · low pressure · Dec 30, 2014 · N195GL · Beech 1900D · Passenger/Crew Doors
  > THE AIR STAIR DOOR OPENS REALLY FAST & FOUND THAT THE DOOR SNUBBER PRESS READ 500 PSI. SERVICED THE AIR STAIR DOOR SNUBBER AS NEEDED IAW MI 52-01. OPERATIONS CHECKED GOOD AT THIS TIME.
- [SDR GLBA2014020400375](https://openairdocs.org/sdr/GLBA2014020400375.md): Brake Sys · malfunctioned · Feb 3, 2014 · N195GL · Beech 1900D · Landing Gear Brake System
  > SIG EVENT PILOT REPORTED THAT THE RT BRAKE PEDAL GOES COMPLETELY TO THE FLOOR ON THE CAPTAIN`S & FIRST OFFICER'S SIDE, RIGHT BRAKE COMPLETELY INEFFECTIVE. SUPPLEMENT INFORMATION ION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK
- [SDR GLBA2013110100347](https://openairdocs.org/sdr/GLBA2013110100347.md): Skin · damaged · Nov 1, 2013 · N195GL · Beech 1900D · Wing, Plate/Skin
  > DURING A SCHEDULED INSPECTION, FOUND A DENT FROM A BIRD STRIKE ON THE LT WING L/E BETWEEN WS 236.62 AND 223.48 AND HAS A FUEL LEAK DUE TO THE DAMAGE. REPAIRED IAW EO 13-1900-57-019. MAJOR REPAIR
- [SDR GLBA2012121000132](https://openairdocs.org/sdr/GLBA2012121000132.md): Spar · cracked · Dec 10, 2012 · N195GL · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK AT THE EDGE OF A LIGHTNING HOLE, HORIZONTAL STABILIZER AFT SPAR WEB CENTERLINE AT HSS 0.00,.1" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-068.
- [SDR GLBA2012120700130](https://openairdocs.org/sdr/GLBA2012120700130.md): Skin · corroded · Dec 7, 2012 · N195GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND CORROSION AT FS 228.25, ON SKIN, CORROSION FOUND JUST OTBD OF THIS REPAIR, STRINER 14R 4" OTBD. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-075. MAJOR REPAIR
- [SDR GLBA2012120600129](https://openairdocs.org/sdr/GLBA2012120600129.md): Spar Cap · cracked · Dec 5, 2012 · N195GL · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE LT SPAR CAP ANGLE ON VERTICAL STAB AT SECOND FASTENER FROM THE TOP,.75" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-066. MAJOR REPAIR
- [SDR GLBA2012120600128](https://openairdocs.org/sdr/GLBA2012120600128.md): Spar Cap · cracked · Dec 5, 2012 · N195GL · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND 2 CRACKS IN THE RT SPAR CAP ANGLE ON VERT STAB AT SECOND FASTENER FROM THE TOP, 1.25" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-067. MAJOR REPAIR
- [SDR GLBA2012120600127](https://openairdocs.org/sdr/GLBA2012120600127.md): Skin · corroded · Dec 5, 2012 · N195GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND BELLY CORROSION AT FS 243.25, APPROX 1" LEFT OF STRINGER 16. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-074. MAJOR REPAIR
- [SDR GLBA20111216F](https://openairdocs.org/sdr/GLBA20111216F.md): Filter · leaking · Dec 15, 2011 · N195GL · Beech 1900D · Aircraft Fuel Filter/Strainer
  > PILOT REPORTED THAT THERE IS A FUEL LEAK AROUND THE NR 1 ENG FUEL FILTER. MX REPLACED THE NR1 ENG FUEL FILTER.
- [SDR GLBA20110824G](https://openairdocs.org/sdr/GLBA20110824G.md): Switch · out of adjust · Aug 23, 2011 · N195GL · Beech 1900D · Door Warning System
  > PILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR ILLUMINATED WHEN TAKEOFF POWER WAS APPLIED. MX ADJUSTED THE DOOR LATCH SWITCH IAW MM 52-70-00, OPS CK GOOD.
- [SDR GLBA20110817H](https://openairdocs.org/sdr/GLBA20110817H.md): Lamp · inoperative · Aug 16, 2011 · N195GL · Beech 1900D · Emergency Lighting
  > PILOT REPORTED THAT THE INSTRUMENT EMERGENCY LIGHTS ARE INOP ON THE F/O'S SIDE. MX REPLACED THE LAMP IAW BMM 33-10-04, OPS CK GOOD.
- [SDR GLBA20110725J](https://openairdocs.org/sdr/GLBA20110725J.md): Skin · cracked · Jul 25, 2011 · N195GL · Beech 1900D · Emergency Exits
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND THE EMERGENCY EXIT AT SEAT 6A SKIN CRACKED IN LOWER FWD CORNER, 1.25" INCHES IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-52-009. MATERIALS UTILIZED
- [SDR GLBA20110722H](https://openairdocs.org/sdr/GLBA20110722H.md): Frame · cracked · Jul 22, 2011 · N195GL · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND A CRACK IN THE CARGO DOOR UPPER FRAME AT FS 509.50 BETWEEN STRINGERS 3L & 4L, 3.75" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1
- [SDR GLBA20110714F](https://openairdocs.org/sdr/GLBA20110714F.md): Propeller · malfunctioned · Jul 13, 2011 · N195GL · Beech 1900D · Propeller Feathering/Reversing
  > THE PILOT REPORTED THAT ON APPROACH, AT 500' AGL WITH BOTH TORQUES AROUND 750LBS THE RT ENGINE CYCLED INTO AND OUT OF FEATHER TWICE, ADDED POWER TO 1500LBS AND IT STOPPED. MX FOUND LT ENGINE HIGH & LOW TORQUES OUT OF RIG, RERIGGED POWER LEVERS IAW AIM 7.2.4 &
- [SDR GLBA20101105A](https://openairdocs.org/sdr/GLBA20101105A.md): Pressure Switch · malfunctioned · Nov 5, 2010 · N195GL · Beech 1900D · Propeller Feathering/Reversing
  > LT SIDE PROP AUTOFEATHER W/ 1000LBS TQ SHORT FINAL. STOPPED AUTOFEATHERING ABOVE 1000 LBS TQ. MX INSPECTED THE SYS AND ADJUSTED THE FLIGHT IDLE TORQUE IAW AIM CH 7 SEC 2.5, PARA 2 AND REPLACED THE LOW PRESS SWITCH, RAN ENGINES, OPS CHECK GOOD IAW BMM.
- [SDR GLBA20100823G](https://openairdocs.org/sdr/GLBA20100823G.md): Skin · cracked · Aug 23, 2010 · N195GL · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A 1.1" CRACK IN THE LOWER LEFT FUSELAGE SKIN AT B.L. 26.8 AND F.S. 301.6. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-052. MATERI
- [SDR GLBA20100812F](https://openairdocs.org/sdr/GLBA20100812F.md): Skin · debonded · Aug 12, 2010 · N195GL · Beech 1900D · Entrance Stairs
  > DURING A SCHEDULED ROUNTINE INSP, FOUND THE AIRSTAIR DOOR SKIN DEBONDING ON THE LOWER AFT, APPROX 19" IN LENGTH. MX REPLACED THE AIRSTAIR DOOR BONDED SKIN IAW BMM 52-10-03 AND COMPLIED WITH SB 52-3094, OPS CHECKS GOOD.
- [SDR GLBA20100618G](https://openairdocs.org/sdr/GLBA20100618G.md): Spar · damaged · Jun 12, 2010 · N195GL · Beech 1900D · Wing Spar
  > MAJOR REPAIR UPON SUBSEQUENT INSPECTION MAINTENANCE FOUND LEFT FORWARD SPAR AFT LOWER FLANGE FOUND TO HAVE BEEN DAMAGED BY LEFT DRAG BRACE NEXT TO UPLOCK BRACKET IN LEFT WHEEL WELL. DAMAGE AT BL 107.0 TO 99.0 AND 104.5 TO 101.5 DELAMINATION IS APPROX 8 " LONG
- [SDR GLBA20100615F](https://openairdocs.org/sdr/GLBA20100615F.md): Arm · failed · Jun 12, 2010 · N195GL · Beech 1900D · Landing Gear Retraction/Extension System
  > SIG EVENT - UPON LANDING IN "DEN" THE LEFT HAND MAIN LANDING GEAR COLLAPSED CAUSING SIGNIFICANT DAMAGE TO THE LEFT MAIN LANDING GEAR AND ASSOCIATED SPAR AREA. IT HAS BEEN ISOLATED AT THIS TIME TO A FAILURE OF THE UPPER DRAG BRACE "A" ARM ASSEMBLY LUGS WHICH B
- [SDR GLBA201005122](https://openairdocs.org/sdr/GLBA201005122.md): Switch · deteriorated · May 11, 2010 · N195GL · Beech 1900D · Propeller Feathering/Reversing
  > PILOTS REPORTED THAT THE RIGHT AUTOFEATHER CYCLED DURING LANDING. MAINTENANCE REMOVED AND REPLACED THE LEFT PRESSURE SWITCH. THE OPERATIONAL CHECK WAS GOOD IAW BMM 61-21-01. P/N ON AND OFF 50-389121-47. S/N OFF 0112.
- [SDR GLBA201005121](https://openairdocs.org/sdr/GLBA201005121.md): Switch · malfunctioned · May 10, 2010 · N195GL · Beech 1900D · Propeller Feathering/Reversing
  > PILOTS REPORTED THAT THE AUTOFEATHER SEQUENCE CYCLED MULTIPLE TIMES DURING LANDING FLARE. MAINTENANCE ADJUSTED THE RIGHT AUTOFEATHER ARMING SWITCH IN THE PEDESTAL IAW BMM 61-21-02. OPERATIONAL CHECK WAS GOOD.
- [SDR GLBA20091111F](https://openairdocs.org/sdr/GLBA20091111F.md): Spar · damaged · Nov 10, 2009 · N195GL · Beech 1900D · Wing Spar
  > DURING ROUTINE SCHEDULED MX, DISCOVERED 2 LOCK FASTENER HOLES MISDRILLED (HOLES ARE STEPPED) AT/ON THE LT WING, AFT WING SPAR ON THE FWD SIDE OF THE SPAR AT WS 127.288 AND 129.588. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECT
- [SDR GLBA20091110H](https://openairdocs.org/sdr/GLBA20091110H.md): Spar · damaged · Nov 6, 2009 · N195GL · Beech 1900D · Fuselage Main, Frame
  > DURING ROUTINE SCHEDULED MAINTENANCE AFTER REMOVAL OF A FASTENER, A HOLE WAS FOUND TO BE STEPPED AND OVERSIZED AT THE LEFT HAND WING SPAR W.S. 104.0. APPROXIMATE DIAMETER OF.230". MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIO
- [SDR GLBA20091110G](https://openairdocs.org/sdr/GLBA20091110G.md): Spar · damaged · Nov 6, 2009 · N195GL · Beech 1900D · Wing Spar
  > DURING ROUTINE SCHEDULED MAINTENANCE AFTER REMOVAL OF A FASTENER, PART OF AN EXISTING RIVET WAS IN THE HOLE UPON REMOVING THE RIVET THE DIAMETER OF THE HOLE WAS FOUND TO BE APPROXIMATELY.230" ACROSS AT LEFT HAND WING SPAR W.S. 114.250. MAINTENANCE REPAIRED
- [SDR GLBA20091110F](https://openairdocs.org/sdr/GLBA20091110F.md): Spar · damaged · Nov 6, 2009 · N195GL · Beech 1900D · Wing Spar
  > DURING ROUTINE SCHEDULED MX, A STEPPED LOCK FASTENER WAS FOUND IN THE LT WING SPAR AT WS 124.588. DEPTH OF THE STEP IS APPROX.150" DEEP. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIONS I.A.W. E.O. 09-1900-57-006. MATERIALS
- [SDR GLBA20091104F](https://openairdocs.org/sdr/GLBA20091104F.md): Angle · cracked · Nov 4, 2009 · N195GL · Beech 1900D · Fuselage Miscellaneous Structure
  > DURING ROUTINE SCHEDULED MAINTENANCE A RIGHT HAND HEAVY ANGLE WAS FOUND CRACKED IN THE RADIUS AT F.S. 303.25. CRACK LENGTH APPROXIMATELY 2" LONG EXTENDING 1" FORWARD AND OF AFT OF F.S. 303.25. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED R
- [SDR GLBA200908122](https://openairdocs.org/sdr/GLBA200908122.md): Latch · out of rig · Aug 12, 2009 · N195GL · Beech 1900D · Emergency Exits
  > PILOTS REPORTED THAT THE 6C EMERGENCY EXIT HANDLE APPEARED TO BE UNLOCKED FROM THE OUTSIDE. MX RIGGED THE 6C DOOR LATCH AND OPS CHECKED GOOD.
- [SDR GLBA200908121](https://openairdocs.org/sdr/GLBA200908121.md): Handle · loose · Aug 11, 2009 · N195GL · Beech 1900D · Emergency Exits
  > DURING ROUTINE WALK AROUND PILOTS REPORTED THAT LT OVERWING EXIT HANDLE APPEARED TO BE UNSECURED. MX ENSURED THAT LATCH WAS SECURED MM 52-20-00. SUBSEQUENT INSP BY PILOTS RESULTED IN OBSERVANCE THAT HANDLE BECAME UNSECURED SPONTANEOUSLY. MX REMOVED AND INSP
- [SDR GLBA20090703A](https://openairdocs.org/sdr/GLBA20090703A.md): Tach Generator · deteriorated · Jul 3, 2009 · N195GL · Beech 1900D · Propeller Indication System
  > ABORTED TAKEOFF, PILOTS REPORTED THAT AT TAKEOFF POWER THE PROPELLER RPM ON THE LT SIDE EXCEEDED 2000 RPM AND THE TAKEOFF WAS ABORTED. MX REMOVED AND REPLACED NR 1 PROPELLER TACH GENERATOR IAW 67D MM 70-00-00. OPS AND LEAK CHECKS WERE GOOD IAW MM 77-10-00.
- [SDR GLBA200906011](https://openairdocs.org/sdr/GLBA200906011.md): Indicator · malfunctioned · Jun 1, 2009 · N195GL · Beech 1900D · Engine BMEP/Torque Indicating
  > NR 2 TORQUE GAUGE DROPPED TO 0 ON TAKEOFF ROLL. THE NR 2 TORQUE GAUGE DROPPED TO ZERO. MX REMOVED AND REPLACED THE NR 2 TORQUE GAUGE IAW MM 31-10-00. OPS CHECK WAS GOOD.
- [SDR GLBA2009022809G](https://openairdocs.org/sdr/GLBA2009022809G.md): Keel · cracked · Feb 23, 2009 · N195GL · Beech 1900D · Fuselage Main, Keel
  > MAJOR REPAIR - DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND ON THE LEFT INBOARD KEEL. MAINTENANCE REPAIRED THE LEFT HAND INBOARD KEEL AT FS 321 IAW ENGINEERING ORDER 09-195-01.
- [SDR GLB2008F00005](https://openairdocs.org/sdr/GLB2008F00005.md): Angle · cracked · Jun 18, 2008 · N195GL · Beech 1900D · Fuselage Miscellaneous Structure
  > LT HEAVY ANGLE CRACKED APPROX 1.125 INCH IN LENGTH AT FORWARD BEND RADIUS AT FS 288.0. REPAIRED LT HEAVY ANGLE AT FS 288 IAW SRM 53.90. REPAIR AREA APPROX 13.125 INCH LONG. RII INSPECTION CP,[;OED WOTJ OAW TASKCARD NR 8.2.1. (K)
- [SDR GLBA20060919](https://openairdocs.org/sdr/GLBA20060919.md): Skin · misrepaired · Feb 26, 2007 · N195GL · Beech 1900D · Fuselage Main, Plate/Skin
  > UPON ROUTINE INSPECTIONS MAINTENANCE FOUND THAT A REPAIR MUST CONFORM WITH SRM TECHNICAL DATA SPECIFICATIONS AT FS 126 TO FS 131.3 STRINGER 3R TO APPROXIMATELY 3 INCHES IB OF STRINGER 2R ABOVE PILOTS WINDSHIELD. MAINTENANCE REPAIRED THE AFFECTED AREA AT FS 17
- [SDR GLBA20060918](https://openairdocs.org/sdr/GLBA20060918.md): Stringer · cracked · Feb 26, 2007 · N195GL · Beech 1900D · Fuselage Main, Longeron/Stringer
  > UPON ROUTINE INSPECTIONS, MAINTENANCE FOUND A STRINGER RELIEF HOLE CRACKED AT FS 177.3 RT STRINGER 9AL. MAINTENANCE REPAIRED THE AFFECTED AREA AT FS 177.3 RT STRINGER 9AL RELIEF HOLE IAW SRM 51-70 AND TC 8.2.1.
- [SDR GLBA20060917](https://openairdocs.org/sdr/GLBA20060917.md): Stringer · cracked · Feb 26, 2007 · N195GL · Beech 1900D · Fuselage Main, Longeron/Stringer
  > UPON ROUTINE INSPECTIONS MAINTENANCE FOUND A STRINGER RELIEF HOLE CRACKED AT FS 163.9 RT STRINGER 9AL. MAINTENANCE REPAIRED THE AFFECTED AREA AT FS 163.9 RT STRINGER 9AL RELIEF HOLE IAW SRM 51-70 AND TC 8.2.1.
- [SDR GLBA20060911](https://openairdocs.org/sdr/GLBA20060911.md): Skin · cracked · Feb 20, 2007 · N195GL · Beech 1900D · Fuselage Main, Plate/Skin
  > UPON ROUTINE INSPECTION MAINTENANCE FOUND THE BELLY SKIN CRACKED AT APPROXIMATELY F.S. 298.0, B.L. 27.0. MAINTENANCE REPAIRED BELLY SKIN AT APPROXIMATELY F.S.298.0 B.L. 27.0 PER BEECH SRM 51-70. RII INSPECTION COMPLIED WITH PER TC 8.2.1.

Next page: https://openairdocs.org/aircraft/N195GL/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 = 'N195GL' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N195GL/reports

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