N169GL

Service difficulty reports · 68

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR TIMA20260425001Blower Motor · inoperativeWAS 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.Apr 25, 2026 · N169GL · Beech 1900D · Air Distribution FanSDR TIMA20240724009Landing Gear · faultedDURING 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 BUSSJul 24, 2024 · N169GL · Beech 1900D · Landing Gear SystemSDR TIMA20240705007Engine · low torqueAFTER 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 AJul 5, 2024 · N169GL · Beech 1900D · Engine (Turbine/Turboprop)SDR GLBA2018011100699Rudder Pedal · shearedPILOTS 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 CHECKJan 9, 2018 · N169GL · Beech 1900D · Rudder Control SystemSDR GLBA2014112100467Unknown · malfunctionedPILOT 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, COULNov 20, 2014 · N169GL · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA2013092600325Structure · damagedDURING 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.Sep 26, 2013 · N169GL · Beech 1900D · Wing Main, Frame StructureSDR GLBA2013092000322Frame · crackedDURING 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.Sep 20, 2013 · N169GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2013092000321Frame · crackedDURING 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.Sep 20, 2013 · N169GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2013092000320Bulkhead · chafedDURING 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.Sep 20, 2013 · N169GL · Beech 1900D · Fuselage Main, BulkheadSDR GLBA2013091900318Door Frame · crackedDURING 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.Sep 18, 2013 · N169GL · Beech 1900D · Fuselage Main, StructureSDR GLBA2013091900319Frame · crackedDURING 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.Sep 18, 2013 · N169GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2013091900316Spar Cap · crackedDURING 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.Sep 18, 2013 · N169GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2013091900315Spar Cap · crackedDURING 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.Sep 18, 2013 · N169GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2013091900314Spar · crackedDURING A SCHEDULED INSPECTION, MX FOUND THE AFT MIDDLE SPAR WEB ON THE HORIZONTAL STABILIZER CRACKED. REPAIRED IAW EO 13-1900-55-022. MAJOR REPAIR.Sep 18, 2013 · N169GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA2013091900313Rib · crackedDURING 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.Sep 18, 2013 · N169GL · Beech 1900D · Wing, Rib/BulkheadSDR GLBA2013091900317Door Frame · crackedDURING 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.Sep 18, 2013 · N169GL · Beech 1900D · Fuselage Main, StructureSDR GLBA2013091600311Keelbeam · bentLT 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.Sep 14, 2013 · N169GL · Beech 1900D · Nacelle/Pylon, Main FrameSDR GLBA2013091100308Skin · damagedDURING A SCHEDULED INSPECTION, FOUND BELLY SKIN AND FASTENER DAMAGED AT FS 468.25 BETWEEN STRINGERS 13 - 14L. REPAIRED IAW EO 13-1900-53-058.Sep 10, 2013 · N169GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2013090300303Actuator · failedPILOT 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 GSep 2, 2013 · N169GL · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA201300145Wire · brokenPILOT 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.Jan 5, 2013 · N169GL · Beech 1900D · Landing Gear System WiringSDR GLBA201209071Landing Gear · malfunctionedLANDING 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.Sep 6, 2012 · N169GL · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA201209031Bulb · inoperativeEMERGENCY INSTRUMENT LIGHT ON F/O'S SIDE INOPERATIVE. MX REPLACED THE BULB, OPS CK GOOD.Sep 3, 2012 · N169GL · Beech 1900D · Emergency LightingSDR GLBA2012071900016Pressure Blkhd · crackedDURING 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.Jul 19, 2012 · N169GL · Beech 1900D · Fuselage Main, BulkheadSDR GLBA201112053Downlock Switch · failedPILOT 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 Dec 3, 2011 · N169GL · Beech 1900D · Landing Gear Position and WarningSDR GLBA20111024FAnnunciator · inoperativePILOT 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.Oct 21, 2011 · N169GL · Beech 1900D · Landing Gear Position and WarningSDR GLBA20110726GFuse · openPILOT 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.Jul 25, 2011 · N169GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA20110726FConnector · corrodedPILOT 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.Jul 25, 2011 · N169GL · Beech 1900D · Door System WiringSDR GLBA201104153Bulb · inoperativePILOT 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.Apr 14, 2011 · N169GL · Beech 1900D · Emergency LightingSDR GLBA20110223AIndicator · reads lowRIGHT 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.Feb 23, 2011 · N169GL · Beech 1900D · Engine BMEP/Torque IndicatingSDR GLBA20110203FFrame · crackedMAJOR 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.Feb 3, 2011 · N169GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20110204HSkin · debondedMAJOR 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 11-1900-52-0Feb 3, 2011 · N169GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA20110204FFrame · crackedMAJOR 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 INSPECTIOFeb 3, 2011 · N169GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20110204GStringer · crackedMAJOR 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 THFeb 3, 2011 · N169GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA201006051Actuator · malfunctionedWHEN 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 DOWNJun 4, 2010 · N169GL · Beech 1900D · Landing Gear ActuatorSDR GLBA20091223AHandle · deterioratedLANDING 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.Dec 23, 2009 · N169GL · Beech 1900D · Landing Gear SelectorSDR GLBA200912111Landing Gear · inoperativeLANDING 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 SWDec 11, 2009 · N169GL · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA20091130GAutofeather Sys · malfunctionedSUSPECTED 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 CHECNov 29, 2009 · N169GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20090805GUplock Switch · out of adjustPILOTS 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 MOTAug 2, 2009 · N169GL · Beech 1900D · Landing Gear Position and WarningSDR GLBA200908041Landing Gear · malfunctionedAFTER TAKE OFF LANDING GEAR WOULD NOT RETRACTAug 2, 2009 · N169GL · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA2009072302Landing Gear · malfunctionedLANDING GEAR WOULD NOT RETRACT AFTER T/O.Jul 21, 2009 · N169GL · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA200907231Landing Gear · malfunctionedAIR 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 MJul 21, 2009 · N169GL · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA20061102Frame · crackedFRAME 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.May 12, 2008 · N169GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20061101Door Frame · crackedAIRSTAIR 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 TASKCARMay 12, 2008 · N169GL · Beech 1900D · Fuselage Main, StructureSDR GLBA20061000Skin · crackedBELLY 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 Sep 17, 2007 · N169GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20060837Spar · crackedRIGHT WING AT BL 114.25 AND F.S. 330 FOUND A .094 CRACK ON AFT SPAR, REPAIR PENDING.Oct 11, 2006 · N169GL · Beech 1900D · Wing SparSDR 20030850Powerpack · malfunctionedUPON 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 May 23, 2005 · N169GL · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA20030723Line · leakingLANDING GEAR WILL NOT EXTEND, MANUALLY EXTENDED, FOUND BAD HYD LINE. REMOVED AND REPLACED, OPS CK GOOD.Sep 20, 2004 · N169GL · Beech 1900D · Hydraulic System, MainSDR GLBA20030724Line · inoperativeLANDING GEAR WILL NOT EXTEND. MANUALLY EXTENDED, REMOVED AND REPLACED HYDRAULIC LINE, PN 101-388016-7.Sep 20, 2004 · N169GL · Beech 1900D · Hydraulic System, MainSDR GLBA20030547Control Cable · inoperativeEMERGENCY LANDING FOR LOSS OF ELEV TRIM CONTROL, R & R FWD ELEV TRIM TAB CABLE PN 114-524037-25.Jan 31, 2004 · N169GL · Beech 1900D · Elevator Tab Control SystemSDR GLBA2003102Relay · failedLANDING GEAR HAD TO BE MANUALLY EXTENDED. REPLACED K3 RELAY, OPS CHECK GOOD.Jul 7, 2003 · N169GL · Beech 1900D · Landing Gear Retraction/Extension System
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