# Service difficulty reports: N122UX A list on [N122UX](https://openairdocs.org/aircraft/N122UX.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 · 64 reports - [SDR GLBA2013102100341](https://openairdocs.org/sdr/GLBA2013102100341.md): Seal · unsecure · Oct 18, 2013 · N122UX · Beech 1900D · Passenger/Crew Doors > PILOT REPORTED THAT THE CABIN ALT HI ILLUM AT FLT LEVEL 240, CABIN ALT STARTED CLIMBING TO AC ALT, O2 MASKS DEPLOYED. MAINTENANCE RESECURED AIRSTAIR DOOR SEAL, OPS CK GOOD. - [SDR GLBA2013040100221](https://openairdocs.org/sdr/GLBA2013040100221.md): Handle · dislodged · Mar 29, 2013 · N122UX · Beech 1900D · Passenger/Crew Doors > PILOT REPORT THAT THE MAIN DOOR HANDLE FELL OFF. MX REPLACED THE DOOR HANDLE, OPS CHECKED GOOD. - [SDR GLBA2013030500197](https://openairdocs.org/sdr/GLBA2013030500197.md): Spar Web · damaged · Mar 4, 2013 · N122UX · Beech 1900D · Horizontal Stabilizer, Spar/Rib > DURING A SCHEDULED ROUTINE INSPECTION, CHANGED AFT SPAR WEB. REPAIRED IAW EO 13-1900-55-006. - [SDR GLBA2013011000149](https://openairdocs.org/sdr/GLBA2013011000149.md): Pcb · failed · Jan 10, 2013 · N122UX · Beech 1900D · Landing Gear System Wiring > PILOT REPORTED THAT ON FINAL, EXTENDED GEAR, INTRANSIT LIGHT ILLUMINATED AND NOTHING ELSE HAPPENED, MANUALLY EXTENDED GEAR, LANDED SAFELY, ATC DECLARED EMERGENCY. MX REPLACED PCB AND LG RELAY, OPS CHECKED GOOD. - [SDR GLBA201300146](https://openairdocs.org/sdr/GLBA201300146.md): Line · inoperative · Jan 6, 2013 · N122UX · Beech 1900D · Hydraulic System, Main > PILOT REPORTED THAT AFTER TAKEOFF, BROUGHT THE GEAR TO THE UP POSITION AND RETRACED NORMALLY, GEAR IN TRANSIT LIGHT ILLUMINATED SHORTLY AFTER, LANDING GEAR FAILS TO REMAIN RETRACTED, LANDING GEAR FAILS TO EXTEND NORMALLY, LANDING GEAR MANUAL EXT, ABNORMAL CHEC - [SDR GLBA2012122400140](https://openairdocs.org/sdr/GLBA2012122400140.md): Eadi · odor · Dec 23, 2012 · N122UX · Beech 1900D · Navigation System > PILOT REPORTED AN ODOR OF SMOKE AND BURNING WIRES IN COCKPIT, DECLARED AN EMERGENCY AND LANDED. REPLACED CAPTAIN`S EADI IAW BMM 34-52-00, OPS CHECKED GOOD. - [SDR GLBA2012100800077](https://openairdocs.org/sdr/GLBA2012100800077.md): Frame · cracked · Oct 8, 2012 · N122UX · Beech 1900D · Fuselage Main, Frame > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK ON FRAME AT FS 163.97 AT STRINGER 9R CUTOUT,.5" IN LENGTH. REPAIRED IAW EO 12-1900-53-053. MAJOR REPAIR. - [SDR GLBA2012100400075](https://openairdocs.org/sdr/GLBA2012100400075.md): Spar · damaged · Oct 4, 2012 · N122UX · Beech 1900D · Horizontal Stabilizer, Spar/Rib > DURING A SCHEDULED ROUTINE INSPECTION MX REQURESTED TO PRECAUTIONARY REPLACEMENT OF THE HSS 0.00 HORIZONTAL STABILIZER AFT SPAR WEB. REPAIRED IAW EO 12-1900-55-047. MAJOR REPAIR - [SDR GLBA2012100200074](https://openairdocs.org/sdr/GLBA2012100200074.md): Frame · cracked · Oct 2, 2012 · N122UX · 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, 1" IN LENGTH. REPAIRED IAW EO 12-1900-53-051. MAJOR REPAIR. - [SDR GLBA2012100200073](https://openairdocs.org/sdr/GLBA2012100200073.md): Pressure Blkhd · cracked · Oct 2, 2012 · N122UX · Beech 1900D · Fuselage Main, Bulkhead > DURING A SCHEDULED ROUTINE INSPECTION, FOUND FOUR CRACKS IN THE LT FWD PRESSURE BULKHEAD INBD EDGE ABOVE INBD RIVET ROW AT STATION 84.00, 1.3" IN LENGTH. REPAIRED IAW EO 12-1900-53-082. MAJOR REPAIR. - [SDR GLBA2012091200054](https://openairdocs.org/sdr/GLBA2012091200054.md): Spar Cap · cracked · Sep 11, 2012 · N122UX · Beech 1900D · Vertical Stabilizer, Spar/Rib > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK ON THE VERTICAL STAB LT SPAR CAP ANGLE AT THE 20 PERCENT CHORD TOP FASTENER AT VSS 84.18,.125" IN LENGTH. REPAIRED IAW FR-CO-02520R1 STEP 1. MAJOR REPAIR - [SDR GLBA2012091200053](https://openairdocs.org/sdr/GLBA2012091200053.md): Angle · cracked · Sep 11, 2012 · N122UX · Beech 1900D · Vertical Stabilizer Miscellaneous Structure > DURING A SCHEDULED ROUTINE INSPECTION, FOUND THREE CRACKS ON THE VERTICAL STAB RT SPAR CAP ANGLE AT THE 20 PERCENT CHORD TOP FASTENER AT VSS 84.10,.5" IN LENGTH. REPAIRED IAW FR-CO-02520R1, STEP 1. MAJOR REPAIR - [SDR GLBA201208151](https://openairdocs.org/sdr/GLBA201208151.md): Flow Divider · inoperative · Aug 13, 2012 · N122UX · Beech 1900D · Cabin Cooling System > AC PRODUCES STRANGE ODOR AFTER TAKEOFF AFTER BLEEDS ARE OPENED. MX REPLACED THE RT ENGINE FLOW DIVIDER, OPS CHECKED GOOD. - [SDR GLBA201206123](https://openairdocs.org/sdr/GLBA201206123.md): Actuator · leaking · Jun 11, 2012 · N122UX · Beech 1900D · Landing Gear Actuator > THE CREW HEARD A LOUD POPPING NOISE COMING FROM THE NOSE AREA UPON GEAR EXTENSION. MX FOUND HYD FLUID LEAKING FROM THE NOSE GEAR ACTUATOR. R & R NLG ACTUATOR PN ON/OFF 112-380022-23, SN OFF 338, SN ON 569, REF MM 32-30-14. OPS, LEAK, AND RIG CHECKS WERE GOOD. - [SDR GLBA2012030502](https://openairdocs.org/sdr/GLBA2012030502.md): Structure · cracked · Mar 5, 2012 · N122UX · Beech 1900D · Vertical Stabilizer > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK AT THE LIGHTNING HOLE EXTENDING BACK AND TO THE LT, AT LT SIDE VERTICAL STAB AT 39.5 PERCENT CHORD AND CSS 69.184, 1.375" IN LENGTH. REPAIRED IAW EO 12-1900-55-006. MAJOR REPAIR - [SDR GLBA20111213F](https://openairdocs.org/sdr/GLBA20111213F.md): Warning Light · false activation · Dec 12, 2011 · N122UX · Beech 1900D · Propeller Feathering/Reversing > PILOT REPORTED THAT ON DPARTURE AUTOFEATHER ANNUNCIATOR ILLUMINATED. MX PERFORMED, OPS CHECKED IAW RUN WORKSHEET AND BMM 61-21-00, NO DEFECTS NOTED. - [SDR GLBA20111204A](https://openairdocs.org/sdr/GLBA20111204A.md): Blower · failed · Dec 4, 2011 · N122UX · Beech 1900D · Air Distribution Fan > PILOT REPORTED THAT SMOKE IN CABIN AND COCKPIT. MX REPLACED THE FORWARD VENT BLOWER, IAW AIM 21-02, ALL CHECKED GOOD. - [SDR GLBA201112011](https://openairdocs.org/sdr/GLBA201112011.md): Wire · damaged · Nov 28, 2011 · N122UX · Beech 1900D · Door System Wiring > CABIN DOOR LIGHT ANNUNCIATOR CAME ON WHILE TAXIING. MX REPAIRED SMASHED WIRE IN DOOR. - [SDR GLBA20110915A](https://openairdocs.org/sdr/GLBA20110915A.md): Display · failed · Sep 15, 2011 · N122UX · Beech 1900D · Attitude and Direction Data System > CAPT'S EADI/EHSI FAILED IN FLIGHT. SMOKED DETECTED IN COCKPIT SMELLED ONLY PULLED FD NR 1 C/B. MX INSPECTED THE SYS AND CHECKED THE WIRING, REPLACED THE EADI SCREEN PN: 622-9681-001, SN 1139, OPS CK GOOD, NO ODOR NOTICED. - [SDR GLBA20110909G](https://openairdocs.org/sdr/GLBA20110909G.md): Snubber · underserviced · Sep 8, 2011 · N122UX · Beech 1900D · Passenger/Crew Doors > PILOT REPORTED THAT THE CABIN DOOR SNUBBER NEEDS SERVICE. MX SERVICED THE DOOR SNUBBER IAW BMM 12-10-00, OK FOR SERVICE. - [SDR GLBA20110909F](https://openairdocs.org/sdr/GLBA20110909F.md): Cable · cracked · Sep 8, 2011 · N122UX · Beech 1900D · Passenger/Crew Doors > PILOT REPORTED THAT THE CABIN DOOR CABLE IS EXPOSED WITH A CRACK IN THE RUBBER COATING, FWD, LOWER. MX REPLACED THE CABLE IAW MM 52-10-02, OPS CHECKED GOOD. - [SDR GLBA200904152](https://openairdocs.org/sdr/GLBA200904152.md): Computer · malfunctioned · Apr 13, 2011 · N122UX · Beech 1900D · Rudder Control System > UNSCHEDULED RUDDER BOOST ACTIVATION IN FLIGHT. RESOLVED WITH EMERGENCY CHECKLIST. YAW DAMPER WORKS CORRECTLY. MX R & R THE NR1 YAW DAMP/ RB COMPUTER, OPS CK GOOD IAW MM 27-26-00. - [SDR GLBA20110218F](https://openairdocs.org/sdr/GLBA20110218F.md): Skin · debonded · Feb 18, 2011 · N122UX · Beech 1900D · Passenger/Crew Doors > DURING A SCHEDULED ROUNTINE INSP MX FOUND THE AIRSTAIR DOOR LOWER INNER SKIN DEBONDED IN AN AREA OF 18" X 6". MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-52-003. MATERIALS UTILIZED ARE INCLUDED IN THE E - [SDR GLBA20101101F](https://openairdocs.org/sdr/GLBA20101101F.md): Skin · torn · Nov 1, 2010 · N122UX · Beech 1900D · Elevator, Plate/Skin > MAJOR REPAIR - THE T/E OF A RT ELEVATOR WAS DAMAGED DURING SHIPPING, THE SKIN WAS TORN 46.5" TO 49.5" FROM INBD EDGE,.75" FROM T/E. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW EO10-1900-27-008, REV 1. MATERIALS UTILIZED ARE INCLUDED - [SDR GLBA20100416J](https://openairdocs.org/sdr/GLBA20100416J.md): Door Frame · cracked · Apr 15, 2010 · N122UX · Beech 1900D · Fuselage Main, Structure > MAJOR REPAIR - THE AIRSTAIR DOOR FRAME AT FUSELAGE FRAME AT FS 150 BETWEEN STRINGERS 10L & 11L WAS FOUND CRACKED. CRACK APPROX.15" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-015 STEPS 5-8. MATERIALS - [SDR GLBA20100416H](https://openairdocs.org/sdr/GLBA20100416H.md): Door Frame · cracked · Apr 15, 2010 · N122UX · Beech 1900D · Fuselage Main, Structure > MAJOR REPAIR - THE FUSELAGE FRAME AT F.S. 177 AT STRINGER 11L WAS FOUND CRACKED IN THE BEND RADIUS. CRACK LENGTH APPROX.2" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-015 STEPS 1-4. MATERIALS UTILIZED - [SDR GLBA20100416G](https://openairdocs.org/sdr/GLBA20100416G.md): Skin · cracked · Apr 15, 2010 · N122UX · Beech 1900D · Fuselage Main, Plate/Skin > MAJOR REPAIR - NEAR THE FWD AIRSTAIR DOOR CUTOUT AT THE LOWER FWD CORNER, FUSELAGE EXTERIOR SKIN AT FS 150 AND STRINGER 11L WAS FOUND CRACKED AT A RIVET HOLE. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW EO 10-1900-53-015, STEPS 9-14. - [SDR GLBA20100416F](https://openairdocs.org/sdr/GLBA20100416F.md): Door Frame · bent · Apr 15, 2010 · N122UX · Beech 1900D · Fuselage Main, Structure > MAJOR REPAIR - THE FUSELAGE FRAME AT F.S. 177 BETWEEN STRINGERS 10L & 11L WERE FOUND BENT AND DENTED ON THE SURFACE INSIDE THE AIRSTAIR DOOR CUTOUT AT THE LOWER AFT CORNER AREA. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW EO 10-1900- - [SDR GLBA20100415F](https://openairdocs.org/sdr/GLBA20100415F.md): Door Frame · cracked · Apr 14, 2010 · N122UX · Beech 1900D · Fuselage Main, Structure > MAJOR REPAIR - UPON A POST FLIGHT CHECK IT WAS DISCOVERED THAT A SMALL DENT AND A CRACK WAS PRESENT AT THE LOWER AFT CORNER OF THE FUSELAGE AIRSTAIR DOOR FRAME. DENT APPROX.125" DEEP AND THE CRACK IS APPROX 1" IN LENGTH WITHIN THE DENT. MX REPAIRED THE AFFEC - [SDR GLBA20090731G](https://openairdocs.org/sdr/GLBA20090731G.md): Spar Cap · cracked · Jul 31, 2009 · N122UX · Beech 1900D · Wing Spar > MAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A CRACK ON THE RT WING AT RBL 114.250, LOWER SPAR CAP, AFT SIDE OF SPAR WHILE PERFORMING SB 57-3816. CRACK IS APPROXIMATELY.040" DEEP AND BASICALLY RADITES OUT FROM A FASTENER HOLE. MX REPAIRED AFFECTED AR - [SDR GLBA20090731F](https://openairdocs.org/sdr/GLBA20090731F.md): Skin · cracked · Jul 28, 2009 · N122UX · Beech 1900D · Fuselage Main, Plate/Skin > DURING ROUTINE SCHEDULED MAINTENANCE 4 CRACKS RADIATING FROM AROUNDTWO RIVETS. ONE ON THE LT OF STRINGER NR 1. LENGTH OF CRACK IS APPROXIMATELY.2 AND.3 INCHES AND ONE ON THE RT OF STRINGER NR 1. LENGTH OF CRACKIS APPROXIMATELY. AND.25 INCHES. MAINTENA - [SDR GLBA20090212A](https://openairdocs.org/sdr/GLBA20090212A.md): Turnbuckle · obstructed · Feb 12, 2009 · N122UX · Beech 1900D · Aileron Control System > IN FLIGHT AILERON WOULD STICK AND POP LOOSE WHEN TURNING FLIGHT CONTROLS BOTH DIRECTIONS. MAINTENANCE INSPECTED AILERON SYSTEM IAW MM 27-10-02. FOUND TURNBUCKLE RUBBING ON LIGHTNING HOLE ANTI-CHAFE PROTECTION. REPAIRED PROTECTION AS REQUIRED. MAINTENANCE C - [SDR GLB2008F00030](https://openairdocs.org/sdr/GLB2008F00030.md): Spar · damaged · Sep 19, 2008 · N122UX · Beech 1900D · Horizontal Stabilizer, Spar/Rib > MAJOR REPAIR FOR CONFORMITY REPLACEMENT REQUESTED OF HORIZONTAL STABILIZER MAIN SPAR CENTER WEB REPAIR. PRIOR REPAIR DOES NOT CONFORM TO SRM DATA. MX REPLACED THE MAIN SPAR CENTER WEB REPAIR IAW BEECH 1900D SRM 55-91. REPAIR APPROXIMATELY 5.75" BY 4.75" OUT - [SDR GLB2008F00029](https://openairdocs.org/sdr/GLB2008F00029.md): Stabilizer · damaged · Sep 19, 2008 · N122UX · Beech 1900D · Horizontal Stabilizer Structure > MAJOR REPAIR ACFT 122UX WHILE TAXIING THE ACFT TO THE GATE THE PILOTS STRUCK A JETWAY WITH THE TAIL OF THE ACFT DAMAGING THE VERTICAL AND HORIZONTAL STABILIZERS. THE STABILIZER WAS DAMAGED AND TWISTED TO THE LT FROM VERTICAL STABILIZER POSITION CSS 39.289 TO - [SDR GLB2008F00027](https://openairdocs.org/sdr/GLB2008F00027.md): Stabilizer · damaged · Sep 19, 2008 · N122UX · Beech 1900D · Vertical Stabilizer > MAJOR REPAIR ACFT N122UX WHILE TAXIING THE ACFT TO THE GATE THE PILOTS STRUCK A JETWAY WITH THE TAIL OF THE ACFT DAMAGING THE VERTICAL AND HORIZONTAL STABILIZERS. THE VERTICAL STABILIZER WAS DAMAGED AND TWISTED TO THE LT FROM VERTICAL STABILIZER POSITION CSS - [SDR GLBA20061088](https://openairdocs.org/sdr/GLBA20061088.md): Actuator · worn · Mar 15, 2008 · N122UX · Beech 1900D · Landing Gear Actuator > ENROUTE, THE LANDING GEAR WOULD NOT EXTEND NORMALLY WHICH REQUIRED THE PILOTS TO MANUALLY PERFORM THE GEAR EXTENSION. MAINT REMOVED AND REPLACED THE LT MLG ACTUATOR IAW MM 32-30. OPERATIONAL CHECKS OF THE GEAR SWINGS ALL CHECKED NORMAL. LANDING GEAR ACTUATOR - [SDR GLBA](https://openairdocs.org/sdr/GLBA.md): Actuator · worn · Mar 15, 2008 · N122UX · Beech 1900D · Landing Gear Actuator > SIGNIFICANT EVENT, ENROUTE, THE LANDING GEAR WOULD NOT EXTEND NORMALLY WHICH REQUIRED THE PILOTS TO MANUALLY PERFORM THE GEAR EXTENSION. MAINT REMOVED AND REPLACED THE LT MLG ACTUATOR IAW MM 32-30. OPERATIONAL CHECKS OF THE GEAR SWINGS ALL CHECKED NORMAL. LAND - [SDR GLBA20061075](https://openairdocs.org/sdr/GLBA20061075.md): Frame · cracked · Feb 25, 2008 · N122UX · Beech 1900D · Fuselage Main, Frame > FUSELAGE FRAME CRACKED.5 NR AT FS 163.9 AND STR 9R MAINT REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE FS 163.9 STRINGER 9R IAW SRM REF. 51-70. REPAIR APPROX 5.5 X 2.5 2024-T3.071. RII INSP COMPLIED IAW TASKCARD 8.2.1. - [SDR GLBA20061076](https://openairdocs.org/sdr/GLBA20061076.md): Frame · cracked · Feb 25, 2008 · N122UX · Beech 1900D · Fuselage Main, Frame > FUSELAGE FRAME CRACKED.5 INCH AT FS 183 AT STRINGER 9R. MAINT REPAIRED FRAME CRACK AT STR RELIEF HOLE FS 183, STRINGER 9R IAW SRM REF 51-70. REPAIR APPROXIMATELY 5.5 INCH X 2.5 2024-T3.071. RII INSPCOMPLIED WITH IAW TASKCARD 8.2.1. - [SDR GLBA20061069](https://openairdocs.org/sdr/GLBA20061069.md): Fire Loop · faulty · Feb 13, 2008 · N122UX · Beech 1900D · Fire Detection > ENG SHUTDOWN- FLIGHT NR 5067 ENROUTE, THE PILOTS SHUTDOWN AND SECURED THE NR 2 ENGINE IN FLIGHT, DUE TO A NR 2 FIREWALL FUEL VALVE HANDLE THAT ILLUMINATED DURING FLIGHT. MAINT REMOVED AND REPLACED THE NR 2 ENG FW FIRELOOP IAW MM 26-10-01. OPS CHECK OF THE SYS - [SDR GLBA20060893](https://openairdocs.org/sdr/GLBA20060893.md): Skin · cracked · Feb 11, 2007 · N122UX · Beech 1900D · Fuselage Main, Plate/Skin > DURING ROUTINE MAINTENANCE, A CRACK WAS FOUND ON THE RT SIDE OF THE FUSELAGE AT FUSELAGE STATION 545.5 AND RIVETS PROTRUDING DOWN THE 3 INCH CRACK AT WATERLINE 112. MX REMOVED DAMAGED AREA APPROXIAMTELY 6.25 INCH LONG BY 5.25 INCHES WIDE AT FUSELAGE STATION 5 - [SDR 20060893](https://openairdocs.org/sdr/20060893.md): Skin · cracked · Feb 11, 2007 · N122UX · Beech 1900D · Fuselage Main, Plate/Skin > DURING ROUTINE MAINTENANCE, A CRACK WAS FOUND ON THE RT SIDE OF THE FUSELAGE AT FUSELAGE STATION 545.5 AND RIVETS PROTRUDING DOWN THE 3 INCH CRACK AT WATERLINE 112. MX REMOVED DAMAGED AREA APPROXIAMTELY 6.25 INCHES LONG BY 5.25 INCHES WIDE AT FUSELAGE STATION - [SDR GLBA20060884](https://openairdocs.org/sdr/GLBA20060884.md): Skin · cracked · Jan 12, 2007 · N122UX · Beech 1900D · Fuselage Main, Plate/Skin > LT FUSELAGE LOWER SKIN, FORWARD SPAR FLANGE HAS (2) PULLED RIVETS WITH 1.2500 INCH CRACK AT F.S. 289.0 AND W.S. 29.06. REPAIRED CRACK AND RIVETS IAW SRM 53-90-18. - [SDR GLBA20060885](https://openairdocs.org/sdr/GLBA20060885.md): Skin · cracked · Jan 12, 2007 · N122UX · Beech 1900D · Fuselage Main, Plate/Skin > RT FUSELAGE LOWER SKIN, FORWARD SPAR FLANGE HAS (2) PULLED RIVETS WITH 1.2500 INCH CRACK AT F.S. 289.0 AND W.S. 29.06. REPAIRED CRACK AND RIVETS IAW SRM 53-90-18. - [SDR GLBA20060812](https://openairdocs.org/sdr/GLBA20060812.md): Doubler · cracked · Aug 8, 2006 · N122UX · Beech 1900D · Fuselage Miscellaneous Structure > LEFT AND RIGHT HEAVY DOUBLERS CRACKED AT FS 288.0 P/N 114-430002-7180 (RIGHT) AND 114-430002-7179 (LEFT). REPAIR PENDING. - [SDR GLBA20060688](https://openairdocs.org/sdr/GLBA20060688.md): Smoke · detected · Mar 1, 2006 · N122UX · Beech 1900D · Air Distribution System > SMOKE IN CABIN. SMOKE APPEARED TO DISSIPATE AFTER TURNING OFF MASTER SWITCH. INSPECTED ELECTRICAL SYSTEM, COULD NOT DUPLICATE. - [SDR GLBA20060679](https://openairdocs.org/sdr/GLBA20060679.md): Smoke · detected · Feb 17, 2006 · N122UX · Beech 1900D · Air Distribution System > REPORT OF SMOKE (ELECTRICAL) SMELL IN COCKPIT, FLIGHT DIRECTOR C/B POPPED, RESET CIRCUIT BREAKER, OPS CHECKED SYSTEM GOOD. - [SDR GLBA20060669](https://openairdocs.org/sdr/GLBA20060669.md): Actuator · intermittent · Feb 11, 2006 · N122UX · Beech 1900D · Landing Gear Actuator > LEFT MAIN LANDING GEAR GREEN INDICATOR ILLUMINATED ON EXTENSION BUT FLICKERED, WHEN RETRACTED WENT BACK ABOUT HALFWAY. MANUALLY EXTENDED GEAR, INSPECTED AND REPLACED LEFT MAIN LANDING GEAR ACTUATOR. - [SDR GLBA20060665](https://openairdocs.org/sdr/GLBA20060665.md): Downlock Switch · out of adjust · Feb 6, 2006 · N122UX · Beech 1900D · Landing Gear Position and Warning > LEFT MAIN LANDING GEAR HAD NO INDICATION OF GEAR DOWN AND LOCKED, INDICATOR INOPERATIVE-WILL NOT TEST. OVERFLEW LAR TO DEN LANDED WITHOUT INCIDENT. INSPECTED AND RIGGED LEFT MAIN LANDING GEAR DOWNLOCK SWITCH. - [SDR 20030828](https://openairdocs.org/sdr/20030828.md): Frame · cracked · Mar 30, 2005 · N122UX · Beech 1900D · Fuselage Main, Frame > DURING ROUTINE INSPECTION, A.55 INCH CRACK WAS FOUND ON THE INTERCOSTAL FRAME FLANGE AT FS 498.25 BELOW STRINGER 2L. CRACK WAS REPAIRED IAW WITH EO. AIRCRAFT RETURNED TO SERVICE. Next page: https://openairdocs.org/aircraft/N122UX/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 = 'N122UX' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N122UX/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.