# Service difficulty reports: N169GL

A list on [N169GL](https://openairdocs.org/aircraft/N169GL.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 · 68 reports

- [SDR TIMA20260425001](https://openairdocs.org/sdr/TIMA20260425001.md): Blower Motor · inoperative · Apr 25, 2026 · N169GL · Beech 1900D · Air Distribution Fan
  > WAS IN CRUISE FROM MKG TO IND FOR ABOUT 5 MINUTES. BEGAN TO SMELL ODOR. GOT SLIGHTLY STRONGER WITHIN ABOUT 2 MINUTES. CHOSE TO DIVERT TO SBN. ON APPROACH/FINAL RADIOS CUT IN AND OUT.
- [SDR TIMA20240724009](https://openairdocs.org/sdr/TIMA20240724009.md): Landing Gear · faulted · Jul 24, 2024 · N169GL · Beech 1900D · Landing Gear System
  > DURING FLINAL APPROACH, ALL THREE BUSS TIE ANNUCIATOR LIGHTS ILLUMINATED INDICATING A FAILURE OF THE CENTER BUS. I VERIFIED THE STATUS OF THE ELECTRICAL SYSTEM AND CONFIRMED NO VOLTAGE ON THE CENTER BUS. I REFERRED TO THE QRH DUE TO THE LOSS OF THE CENTER BUSS
- [SDR TIMA20240705007](https://openairdocs.org/sdr/TIMA20240705007.md): Engine · low torque · Jul 5, 2024 · N169GL · Beech 1900D · Engine (Turbine/Turboprop)
  > AFTER DESCENDING AND LEVELING OFF LEFT ENGINE TORQUE NOT RISING PROPERLY AND INCORRECT ENGINE CONTROL / FEEL, PILOT NOTICED IMPROPER POWER OUT OF LEFT ENGINE AND DECLARED EMERGENCY DUE TO PARITIAL POWER ON LEFT ENGINE. PILOT WAS CLEARD TO LAND. LANDED SAFELY A
- [SDR GLBA2018011100699](https://openairdocs.org/sdr/GLBA2018011100699.md): Rudder Pedal · sheared · Jan 9, 2018 · N169GL · Beech 1900D · Rudder Control System
  > PILOTS REPORTED THAT WHILE TAXING OFF THE RUNWAY, WHEN RIGHT RUDDER PRESSURE WAS APPLIED, THE CAPTAIN'S RIGHT RUDDER PEDAL ASSEMBLY SHEARED OFF, FLOPS LOOSE ON THE ASSEMBLY. R & R THE CAPTAIN'S RT RUDDER PEDAL AND ARM ASSEMBLY IAW MM 27-20-03-201. OPS CHECK
- [SDR GLBA2014112100467](https://openairdocs.org/sdr/GLBA2014112100467.md): Unknown · malfunctioned · Nov 20, 2014 · N169GL · Beech 1900D · Landing Gear Retraction/Extension System
  > PILOT REPORTED THAT DURING GEAR RETRACTION, LG HANDLE LIGHT REMAINED ON & LG HANDLE CB POPPED. WENT THROUGH CHECKLIST & MANUALLY EXTENDED GEAR, GOT THREE GREENS, LANDED UNEVENTFULLY. MAINTENANCE PERFORMED OPS CKS ON THE LANDING GEAR SYSTEM IAW MI 32.01, COUL
- [SDR GLBA2013092600325](https://openairdocs.org/sdr/GLBA2013092600325.md): Structure · damaged · Sep 26, 2013 · N169GL · Beech 1900D · Wing Main, Frame Structure
  > DURING A SCHEDULED INSPECTION, FOUND DAMAGE ON THE BOTTOM SIDE OF THE WING TIP, APPROXIMENTLY 3 INCHES FROM WING TIP, DAMAGE DOES NOT APPEAR TO PENATRATE HONEYCOMB. REPLACED THE LT WING TIP ASSY IAW 57-30-00. MAJOR REPAIR.
- [SDR GLBA2013092000322](https://openairdocs.org/sdr/GLBA2013092000322.md): Frame · cracked · Sep 20, 2013 · N169GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED INSP FOUND A CRACK IN THE FUSELAGE FRAME DOUBLER AT BS 177.35 AND STRINGER 13L 1.2 INCHES FROM OTBD EDGE RADIATING INBD, CRACK IS IN THE FLANGE BEND RADIUS OF THE DOUBLER. REPAIRED IAW EO 13-1900-53-064. MAJOR REPAIR.
- [SDR GLBA2013092000321](https://openairdocs.org/sdr/GLBA2013092000321.md): Frame · cracked · Sep 20, 2013 · N169GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE FUSELAGE FRAME AT BS 177.35 AND STRINGER 13L AT THE FRAME FLANGE BEND RADIUS 1.2 INCHES FROM THE OTBD EDGE RADIATING INBD. REPAIRED IAW EO 13-1900-53-065. MAJOR REPAIR.
- [SDR GLBA2013092000320](https://openairdocs.org/sdr/GLBA2013092000320.md): Bulkhead · chafed · Sep 20, 2013 · N169GL · Beech 1900D · Fuselage Main, Bulkhead
  > DURING A SCHEDULED INSPECTION, FOUND A CHAFE IN THE LT WING TO FUSELAGE BULKHEAD AT STRINGER 12L BETWEEN BS 258.25 - 273.25, AREA OF BULKHEAD THAT MEETS AT BELLY SKIN EDGE. REPAIRED IAW EO 13-1900-53-066. MAJOR REPAIR.
- [SDR GLBA2013091900318](https://openairdocs.org/sdr/GLBA2013091900318.md): Door Frame · cracked · Sep 18, 2013 · N169GL · Beech 1900D · Fuselage Main, Structure
  > DURING A SCHEDULED INSPECTION, MX FOUND THE CARGO DOOR FWD FRAME AT FS 456 CRACKED AT THE UPPER INBD GAS STRUT MOUNT ATTACHING NUT PLATE. THE CRACKS RADIATE UPWARD AND INBD FROM THE NUT PLATE. REPAIRED IAW EO 13-1900-53-074. MAJOR REPAIR.
- [SDR GLBA2013091900319](https://openairdocs.org/sdr/GLBA2013091900319.md): Frame · cracked · Sep 18, 2013 · N169GL · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION, MX FOUND THE RT SIDEWALL AT FS 164.415 & STRINGER 9AR, FRAME CUTOUT FOR STRINGER CRACKED.25". REPAIRED IAW EO 13-1900-53-063. MAJOR REPAIR.
- [SDR GLBA2013091900316](https://openairdocs.org/sdr/GLBA2013091900316.md): Spar Cap · cracked · Sep 18, 2013 · N169GL · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING A SCHEDULED INSPECTION, MX FOUND THE LT FWD SPAR CAP ON THE VERTICAL STABILIZER CRACKED AT THE SECOND HOLE. THE CRACK IS APPROXIMATELY.1250 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-55-020. MAJOR REPAIR.
- [SDR GLBA2013091900315](https://openairdocs.org/sdr/GLBA2013091900315.md): Spar Cap · cracked · Sep 18, 2013 · N169GL · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING A SCHEDULED INSPECTION, MX FOUND THE RT FWD SPAR CAP ON THE VERTICAL STABILIZER CRACKED AT THE THIRD HOLE. THE CRACK IS APPROXIMATELY.1250" IN LENGTH. REPAIRED IAW EO 13-1900-55-021. MAJOR REPAIR.
- [SDR GLBA2013091900314](https://openairdocs.org/sdr/GLBA2013091900314.md): Spar · cracked · Sep 18, 2013 · N169GL · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > DURING A SCHEDULED INSPECTION, MX FOUND THE AFT MIDDLE SPAR WEB ON THE HORIZONTAL STABILIZER CRACKED. REPAIRED IAW EO 13-1900-55-022. MAJOR REPAIR.
- [SDR GLBA2013091900313](https://openairdocs.org/sdr/GLBA2013091900313.md): Rib · cracked · Sep 18, 2013 · N169GL · Beech 1900D · Wing, Rib/Bulkhead
  > DURING A SCHEDULED INSPECTION, MX NOTED THAT THE RT WING INBD RIB FLANGE AND DOUBLER WERE CRACKED. REPAIRED IAW EO 13-1900-57-016. MAJOR REPAIR.
- [SDR GLBA2013091900317](https://openairdocs.org/sdr/GLBA2013091900317.md): Door Frame · cracked · Sep 18, 2013 · N169GL · Beech 1900D · Fuselage Main, Structure
  > DURING A SCHEDULED INSPECTION, MX FOUND THAT THE AIRSTAIR DOOR LOWER AFT FRAME CORNER AREA AT APPROXIMATELY FS 172.35 WAS CRACKED, 1.2" IN THE OTBD UPPER BEND RADIUS. REPAIRED IAW EO 13-1900-53-061. MAJOR REPAIR.
- [SDR GLBA2013091600311](https://openairdocs.org/sdr/GLBA2013091600311.md): Keelbeam · bent · Sep 14, 2013 · N169GL · Beech 1900D · Nacelle/Pylon, Main Frame
  > LT INBD KEEL WEB ASSY APPEARS BENT, FWD UPPER EDGE OF WEB ASSY APPEARS TO BE DEFLECTED OTBD APPROXIMATELY.125". LOCATION BL 91.75. REPAIRED IAW EO 13-1900-54-002.
- [SDR GLBA2013091100308](https://openairdocs.org/sdr/GLBA2013091100308.md): Skin · damaged · Sep 10, 2013 · N169GL · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION, FOUND BELLY SKIN AND FASTENER DAMAGED AT FS 468.25 BETWEEN STRINGERS 13 - 14L. REPAIRED IAW EO 13-1900-53-058.
- [SDR GLBA2013090300303](https://openairdocs.org/sdr/GLBA2013090300303.md): Actuator · failed · Sep 2, 2013 · N169GL · Beech 1900D · Landing Gear Retraction/Extension System
  > PILOT REPORTED THAT WHEN SELECTING THE GEAR DOWN, HAD NO LT MAIN INDICATION AND GEAR IN TRANSIT LIGHT REMAINED ILLUMINATED, LANDING GEAR RELAY CIRCUIT BREAKER WAS TRIPPED, RAN CHECKLIST, MANUALLY PUMPED GEAR DOWN UNTILL HANDLE WAS FIRM, PROCEDED TO LAND, LT G
- [SDR GLBA201300145](https://openairdocs.org/sdr/GLBA201300145.md): Wire · broken · Jan 5, 2013 · N169GL · Beech 1900D · Landing Gear System Wiring
  > PILOT REPORTED THAT WHEN THE LANDING GEAR HANDLE WAS SELECTED TO THE UP POSITION, THE RT MAIN DID NOT FULLY RETRACT, LANDING CIRCUIT BREAKER TRIPPED AND HAD TO PUMP GEAR DOWN BEFORE LANDING. MX REPAIRED WIRE G10A22, OPS CK GOOD.
- [SDR GLBA201209071](https://openairdocs.org/sdr/GLBA201209071.md): Landing Gear · malfunctioned · Sep 6, 2012 · N169GL · Beech 1900D · Landing Gear Retraction/Extension System
  > LANDING GEAR FAILED TO EXTEND NORMALY. LANDING GEAR LIGHTS DID NOT ILLUMINATE. MX INSPECTED ALL SYS WIRING AND REPLACED THE LANDING CONTROL HANDLE, PERFORMED SEVERAL GEAR SWINGS, OPS CHECKED GOOD.
- [SDR GLBA201209031](https://openairdocs.org/sdr/GLBA201209031.md): Bulb · inoperative · Sep 3, 2012 · N169GL · Beech 1900D · Emergency Lighting
  > EMERGENCY INSTRUMENT LIGHT ON F/O'S SIDE INOPERATIVE. MX REPLACED THE BULB, OPS CK GOOD.
- [SDR GLBA2012071900016](https://openairdocs.org/sdr/GLBA2012071900016.md): Pressure Blkhd · cracked · Jul 19, 2012 · N169GL · Beech 1900D · Fuselage Main, Bulkhead
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND 4 CRACKS IN THE LT LWR FWD PRESSURE BULKHEAD AT THE INBD EDGE DOUBLER ROW OF FASTENERS, 1.1" IN LENGTH. REPAIRED IAW EO 12-1900-53-038. MAJOR REPAIR.
- [SDR GLBA201112053](https://openairdocs.org/sdr/GLBA201112053.md): Downlock Switch · failed · Dec 3, 2011 · N169GL · Beech 1900D · Landing Gear Position and Warning
  > PILOT REPORTED THAT THE LANDING GEAR INTRANSIT LIGHT ILLUMINATED IN FLIGHT WITH TORQUE AT 3000LB AND AIRSPEED 210KNOTS SLOWED TO 170 AND PUT GEAR DOWN NORMAL APPROPRIATED CHECKK LIST RAN FOR UNSAFE GEAR EVEN WITH ALL INDICATIONS OF GEAR DOWN EXCEPT FOR HANDLE
- [SDR GLBA20111024F](https://openairdocs.org/sdr/GLBA20111024F.md): Annunciator · inoperative · Oct 21, 2011 · N169GL · Beech 1900D · Landing Gear Position and Warning
  > PILOT REPORTED THAT THE LT AND RT LANDING GEAR INDICATION IS INTERMITTENT. MX REPLACED THE ANNUNCIATOR ASSY PN: 90-42291-2, GEAR SWING OPS CKS GOOD, NO DEFECTS NOTED.
- [SDR GLBA20110726G](https://openairdocs.org/sdr/GLBA20110726G.md): Fuse · open · Jul 25, 2011 · N169GL · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE AIR STAIR DOOR WAS INOP. MX REPLACED THE FUSE IN THE BATTERY BOX PNMDL5, IAW BMM 33-20-00, OPS CHECKED GOOD.
- [SDR GLBA20110726F](https://openairdocs.org/sdr/GLBA20110726F.md): Connector · corroded · Jul 25, 2011 · N169GL · Beech 1900D · Door System Wiring
  > PILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR WAS INOPERATIVE. MX FOUND CORROSION ON THE WIRE PINS, REPLACED A401 P1, P2, P3, & P4, SP11 12,13,114,15, & 16 IAW BMM 20-13-00, OPS CK GOOD.
- [SDR GLBA201104153](https://openairdocs.org/sdr/GLBA201104153.md): Bulb · inoperative · Apr 14, 2011 · N169GL · Beech 1900D · Emergency Lighting
  > PILOT REPORTED THAT DURING THERE POST FLIGHT INSP THEY FOUND BOTH INSTRUMENT EMERGENCY LIGHTS ON THE CAPTAIN'S SIDE ARE OUT. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE EMERGENCY LIGHTS BULBS, IAW BMM 33-10-04 PARAGRAPH 1, OPS CHECKED GOOD.
- [SDR GLBA20110223A](https://openairdocs.org/sdr/GLBA20110223A.md): Indicator · reads low · Feb 23, 2011 · N169GL · Beech 1900D · Engine BMEP/Torque Indicating
  > RIGHT ENGINE TORQUE GAUGE WENT DOWN ON CLIMB OUT. ALL OTHER ENGINE INDICATIONS WERE NORMAL,NOTICED ON TAXI IN TORQUE GAUGE WAS BELOW ZERO. MAINTENANCE PERFORMED PARAMETER RUNUP OF LT & RT ENGINES. ALL CHECKS GOOD COULD NOT DUPLICATE DISCREPANCY.
- [SDR GLBA20110203F](https://openairdocs.org/sdr/GLBA20110203F.md): Frame · cracked · Feb 3, 2011 · N169GL · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND A CRACK IN THE FRAME AT FS 280.73 AT STRINGER 5R CUTOUT,.2" IN LENGTH. MAINTENANC PERFORMED ANOTHER INSPECTION ON THE AREA AND FOUND THE THE CRACK WAS A PEN MARK FROM ORIGINAL MANUFACTURE.
- [SDR GLBA20110204H](https://openairdocs.org/sdr/GLBA20110204H.md): Skin · debonded · Feb 3, 2011 · N169GL · Beech 1900D · Passenger/Crew Doors
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND THE AIRSTAIR DOOR LOWER INNER SKIN DEBONDED, AREA 16" X 6" FROM LOWER EDGE INWARD TO STOP HINGE. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-52-0
- [SDR GLBA20110204F](https://openairdocs.org/sdr/GLBA20110204F.md): Frame · cracked · Feb 3, 2011 · N169GL · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND 2 CRACKS AT THE FRAME FS 456.0 RADIATING FROM STRINGER 9AR CUTOUT, UPPER CRACK.6" IN LENGTH, LOWER CRACK.35" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIO
- [SDR GLBA20110204G](https://openairdocs.org/sdr/GLBA20110204G.md): Stringer · cracked · Feb 3, 2011 · N169GL · Beech 1900D · Fuselage Main, Longeron/Stringer
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND A CRACK IN THE STRINGER 9AR AT FS 451.0,.4" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-007. MATERIALS UTILIZED ARE INCLUDED IN TH
- [SDR GLBA201006051](https://openairdocs.org/sdr/GLBA201006051.md): Actuator · malfunctioned · Jun 4, 2010 · N169GL · Beech 1900D · Landing Gear Actuator
  > WHEN LANDING GEAR HANDLE WAS PLACED IN DOWN POSITION WE SAW 3 GREEN, HANDLE INTRANSIT LIGHTS, LG RELAY CB POPPED AND J HOOK CAME DOWN INT LOCKED POSITION OR LESS SIMULTANEOUSLY. MAINTENANCE TROUBLESHOT AND FOUND RIGHT LANDING GEAR ACTUATOR LAGGING UP AND DOWN
- [SDR GLBA20091223A](https://openairdocs.org/sdr/GLBA20091223A.md): Handle · deteriorated · Dec 23, 2009 · N169GL · Beech 1900D · Landing Gear Selector
  > LANDING GEAR WOULD NOT COME DOWN PERFORMED CHECKLIST AND HAND PUMPED THE GEAR ALL 3 GREEN ANNUNCIATORS ILLUMINATED. MX REMOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE IAW MM 31-10-00-201, SECTION 5 AND THE OPERATIONAL CHECK WAS GOOD IAW MM 32-30-00.
- [SDR GLBA200912111](https://openairdocs.org/sdr/GLBA200912111.md): Landing Gear · inoperative · Dec 11, 2009 · N169GL · Beech 1900D · Landing Gear Retraction/Extension System
  > LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. MX JACKED THE ACFT AND PERFORMED A GEAR RETRACTION AND EXTENSION TEST IAW MM 32-30-00. THE OPS CHECK WAS GOOD ON THE GROUND. SUBSEQUENT OPS CHECK FLIGHT WAS UNSATISFACTORY. MX REMOVED AND REPLACED THE MLG SQUAT SW
- [SDR GLBA20091130G](https://openairdocs.org/sdr/GLBA20091130G.md): Autofeather Sys · malfunctioned · Nov 29, 2009 · N169GL · Beech 1900D · Propeller Feathering/Reversing
  > SUSPECTED AUTOFEATHER - PILOTS REPORTED THE RT PROP AUTOFEATHERED IN FLIGHT WHILE REDUCING TORQUE FROM 2500 LBS TO 500 LBS. TOR4QUE LEVELS WERE EVEN THROUGHOUT PWR REDUCTION. MX ADJUSTED THE FLIGHT IDLE TORQUES ON THE RT AND LT ENG IAW MM 76-10-00. OPS CHEC
- [SDR GLBA20090805G](https://openairdocs.org/sdr/GLBA20090805G.md): Uplock Switch · out of adjust · Aug 2, 2009 · N169GL · Beech 1900D · Landing Gear Position and Warning
  > PILOTS REPORTED THAT THE MLG DID NOT RETRACT AFTER TAKEOFF AND IN TRANSIT LIGHTS DID NOT COME ON AND 3 GREEN STILL ANNUNCIATED. PILOTS CYCLED MLG HANDLE WITH THE SAME RESULT. PERFORMED A MANUAL MLG EXTENSION CHECK LIST AT THE DIRECTION OF MX CONTROL. MLG MOT
- [SDR GLBA200908041](https://openairdocs.org/sdr/GLBA200908041.md): Landing Gear · malfunctioned · Aug 2, 2009 · N169GL · Beech 1900D · Landing Gear Retraction/Extension System
  > AFTER TAKE OFF LANDING GEAR WOULD NOT RETRACT
- [SDR GLBA2009072302](https://openairdocs.org/sdr/GLBA2009072302.md): Landing Gear · malfunctioned · Jul 21, 2009 · N169GL · Beech 1900D · Landing Gear Retraction/Extension System
  > LANDING GEAR WOULD NOT RETRACT AFTER T/O.
- [SDR GLBA200907231](https://openairdocs.org/sdr/GLBA200907231.md): Landing Gear · malfunctioned · Jul 21, 2009 · N169GL · Beech 1900D · Landing Gear Retraction/Extension System
  > AIR RETURN PILOTS REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. MAINTENANCE JACKED AIRCRAFT ON RAMP AND PERFORMED 6 GEAR RETRACTION AND EXTENSION CYCLES WITH NO FAILURE. CHECKED SQUAT SWITCH CONNECTORS FOR SECURITY, FOUND OK. PERFORMED 1 M
- [SDR GLBA20061102](https://openairdocs.org/sdr/GLBA20061102.md): Frame · cracked · May 12, 2008 · N169GL · Beech 1900D · Fuselage Main, Frame
  > FRAME AT FS 177.35 CRACKED AT STRINER 9R RELIEF CUTOUT.** MAINT REPAIRED CRACK AT STRINGER RELIEFHOLE AT STRINGER 9R AND FS 177.35 IAW SRM 51-70. REPAIR APPROXIMATELY 3 INCHES BY 4 INCHES. 2024-T3.071. RII INSPECTION COMPLIED IAW TASKCARD 8.2.1.
- [SDR GLBA20061101](https://openairdocs.org/sdr/GLBA20061101.md): Door Frame · cracked · May 12, 2008 · N169GL · Beech 1900D · Fuselage Main, Structure
  > AIRSTAIR DOOR FRAME ANGLE CRACKED AT LOWER SNUBBER MOUNT NUTPLATES. MAINT INSTALLED INSERT AND REPAIR PIECE CUT FROM NEW ANGLE IAW. SRM 53-90-28 AND MFG NEW COVER PLATE. REPAIR AREA APPROXIMATELY 7.7500 INCH BY 8.7500 INCH. RII INSPECTION COMPLIED IAW TASKCAR
- [SDR GLBA20061000](https://openairdocs.org/sdr/GLBA20061000.md): Skin · cracked · Sep 17, 2007 · N169GL · Beech 1900D · Fuselage Main, Plate/Skin
  > BELLY SKIN CRACKED AT WING SPAR FS 290.5 AT BL 29.06 CRACK LENGTH APPROXIMATELY 1.250 INCHES. MAINTENANCE REPAIRED SKIN CRACK AT LT WING SPAR AREA FS 290 AND BL 29.06 IAW SRM 53-90. REPAIR DIMENSION 7 INCH BY 5.8 INCHES. 2024 T3,.040 INCH. RII INSPECTION
- [SDR GLBA20060837](https://openairdocs.org/sdr/GLBA20060837.md): Spar · cracked · Oct 11, 2006 · N169GL · Beech 1900D · Wing Spar
  > RIGHT WING AT BL 114.25 AND F.S. 330 FOUND A.094 CRACK ON AFT SPAR, REPAIR PENDING.
- [SDR 20030850](https://openairdocs.org/sdr/20030850.md): Powerpack · malfunctioned · May 23, 2005 · N169GL · Beech 1900D · Landing Gear Retraction/Extension System
  > UPON APPROACH WHEN LANDING GEAR SELECTED DOWN, GEAR WOULD NOT EXTEND. FLIGHT CREW USED THE MANUAL GEAR DOWN HAND PUMP TO EXTEND GEAR SUCCESSFULLY AND LANDED. MAINTENANCE DISCOVERED HYDRAULIC POWER PACK CIRCUIT BREAKER WAS TRIPPED. RESET CIRCUIT BREAKER AND
- [SDR GLBA20030723](https://openairdocs.org/sdr/GLBA20030723.md): Line · leaking · Sep 20, 2004 · N169GL · Beech 1900D · Hydraulic System, Main
  > LANDING GEAR WILL NOT EXTEND, MANUALLY EXTENDED, FOUND BAD HYD LINE. REMOVED AND REPLACED, OPS CK GOOD.
- [SDR GLBA20030724](https://openairdocs.org/sdr/GLBA20030724.md): Line · inoperative · Sep 20, 2004 · N169GL · Beech 1900D · Hydraulic System, Main
  > LANDING GEAR WILL NOT EXTEND. MANUALLY EXTENDED, REMOVED AND REPLACED HYDRAULIC LINE, PN 101-388016-7.
- [SDR GLBA20030547](https://openairdocs.org/sdr/GLBA20030547.md): Control Cable · inoperative · Jan 31, 2004 · N169GL · Beech 1900D · Elevator Tab Control System
  > EMERGENCY LANDING FOR LOSS OF ELEV TRIM CONTROL, R & R FWD ELEV TRIM TAB CABLE PN 114-524037-25.
- [SDR GLBA2003102](https://openairdocs.org/sdr/GLBA2003102.md): Relay · failed · Jul 7, 2003 · N169GL · Beech 1900D · Landing Gear Retraction/Extension System
  > LANDING GEAR HAD TO BE MANUALLY EXTENDED. REPLACED K3 RELAY, OPS CHECK GOOD.

Next page: https://openairdocs.org/aircraft/N169GL/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 = 'N169GL' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N169GL/reports

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