N122UX

Service difficulty reports · 64

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 = 'N122UX' 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 GLBA2013102100341Seal · unsecurePILOT 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.Oct 18, 2013 · N122UX · Beech 1900D · Passenger/Crew DoorsSDR GLBA2013040100221Handle · dislodgedPILOT REPORT THAT THE MAIN DOOR HANDLE FELL OFF. MX REPLACED THE DOOR HANDLE, OPS CHECKED GOOD.Mar 29, 2013 · N122UX · Beech 1900D · Passenger/Crew DoorsSDR GLBA2013030500197Spar Web · damagedDURING A SCHEDULED ROUTINE INSPECTION, CHANGED AFT SPAR WEB. REPAIRED IAW EO 13-1900-55-006.Mar 4, 2013 · N122UX · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA2013011000149Pcb · failedPILOT 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.Jan 10, 2013 · N122UX · Beech 1900D · Landing Gear System WiringSDR GLBA201300146Line · inoperativePILOT 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 CHECJan 6, 2013 · N122UX · Beech 1900D · Hydraulic System, MainSDR GLBA2012122400140Eadi · odorPILOT 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.Dec 23, 2012 · N122UX · Beech 1900D · Navigation SystemSDR GLBA2012100800077Frame · crackedDURING 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.Oct 8, 2012 · N122UX · Beech 1900D · Fuselage Main, FrameSDR GLBA2012100400075Spar · damagedDURING 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 REPAIROct 4, 2012 · N122UX · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA2012100200074Frame · crackedDURING 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.Oct 2, 2012 · N122UX · Beech 1900D · Fuselage Main, FrameSDR GLBA2012100200073Pressure Blkhd · crackedDURING 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.Oct 2, 2012 · N122UX · Beech 1900D · Fuselage Main, BulkheadSDR GLBA2012091200054Spar Cap · crackedDURING 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 REPAIRSep 11, 2012 · N122UX · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2012091200053Angle · crackedDURING 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 REPAIRSep 11, 2012 · N122UX · Beech 1900D · Vertical Stabilizer Miscellaneous StructureSDR GLBA201208151Flow Divider · inoperativeAC PRODUCES STRANGE ODOR AFTER TAKEOFF AFTER BLEEDS ARE OPENED. MX REPLACED THE RT ENGINE FLOW DIVIDER, OPS CHECKED GOOD.Aug 13, 2012 · N122UX · Beech 1900D · Cabin Cooling SystemSDR GLBA201206123Actuator · leakingTHE 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.Jun 11, 2012 · N122UX · Beech 1900D · Landing Gear ActuatorSDR GLBA2012030502Structure · crackedDURING 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 REPAIRMar 5, 2012 · N122UX · Beech 1900D · Vertical StabilizerSDR GLBA20111213FWarning Light · false activationPILOT REPORTED THAT ON DPARTURE AUTOFEATHER ANNUNCIATOR ILLUMINATED. MX PERFORMED, OPS CHECKED IAW RUN WORKSHEET AND BMM 61-21-00, NO DEFECTS NOTED.Dec 12, 2011 · N122UX · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20111204ABlower · failedPILOT REPORTED THAT SMOKE IN CABIN AND COCKPIT. MX REPLACED THE FORWARD VENT BLOWER, IAW AIM 21-02, ALL CHECKED GOOD.Dec 4, 2011 · N122UX · Beech 1900D · Air Distribution FanSDR GLBA201112011Wire · damagedCABIN DOOR LIGHT ANNUNCIATOR CAME ON WHILE TAXIING. MX REPAIRED SMASHED WIRE IN DOOR.Nov 28, 2011 · N122UX · Beech 1900D · Door System WiringSDR GLBA20110915ADisplay · failedCAPT'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.Sep 15, 2011 · N122UX · Beech 1900D · Attitude and Direction Data SystemSDR GLBA20110909GSnubber · underservicedPILOT REPORTED THAT THE CABIN DOOR SNUBBER NEEDS SERVICE. MX SERVICED THE DOOR SNUBBER IAW BMM 12-10-00, OK FOR SERVICE.Sep 8, 2011 · N122UX · Beech 1900D · Passenger/Crew DoorsSDR GLBA20110909FCable · crackedPILOT 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.Sep 8, 2011 · N122UX · Beech 1900D · Passenger/Crew DoorsSDR GLBA200904152Computer · malfunctionedUNSCHEDULED 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.Apr 13, 2011 · N122UX · Beech 1900D · Rudder Control SystemSDR GLBA20110218FSkin · debondedDURING 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 EFeb 18, 2011 · N122UX · Beech 1900D · Passenger/Crew DoorsSDR GLBA20101101FSkin · tornMAJOR 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 Nov 1, 2010 · N122UX · Beech 1900D · Elevator, Plate/SkinSDR GLBA20100416JDoor Frame · crackedMAJOR 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. MATERIALSApr 15, 2010 · N122UX · Beech 1900D · Fuselage Main, StructureSDR GLBA20100416HDoor Frame · crackedMAJOR 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 UTILIZEDApr 15, 2010 · N122UX · Beech 1900D · Fuselage Main, StructureSDR GLBA20100416GSkin · crackedMAJOR 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.Apr 15, 2010 · N122UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20100416FDoor Frame · bentMAJOR 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-Apr 15, 2010 · N122UX · Beech 1900D · Fuselage Main, StructureSDR GLBA20100415FDoor Frame · crackedMAJOR 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 AFFECApr 14, 2010 · N122UX · Beech 1900D · Fuselage Main, StructureSDR GLBA20090731GSpar Cap · crackedMAJOR 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 ARJul 31, 2009 · N122UX · Beech 1900D · Wing SparSDR GLBA20090731FSkin · crackedDURING 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. MAINTENAJul 28, 2009 · N122UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20090212ATurnbuckle · obstructedIN 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 CFeb 12, 2009 · N122UX · Beech 1900D · Aileron Control SystemSDR GLB2008F00030Spar · damagedMAJOR 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" OUTSep 19, 2008 · N122UX · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLB2008F00029Stabilizer · damagedMAJOR 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 Sep 19, 2008 · N122UX · Beech 1900D · Horizontal Stabilizer StructureSDR GLB2008F00027Stabilizer · damagedMAJOR 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 Sep 19, 2008 · N122UX · Beech 1900D · Vertical StabilizerSDR GLBA20061088Actuator · wornENROUTE, 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 ACTUATORMar 15, 2008 · N122UX · Beech 1900D · Landing Gear ActuatorSDR GLBAActuator · wornSIGNIFICANT 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. LANDMar 15, 2008 · N122UX · Beech 1900D · Landing Gear ActuatorSDR GLBA20061075Frame · crackedFUSELAGE 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.Feb 25, 2008 · N122UX · Beech 1900D · Fuselage Main, FrameSDR GLBA20061076Frame · crackedFUSELAGE 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.Feb 25, 2008 · N122UX · Beech 1900D · Fuselage Main, FrameSDR GLBA20061069Fire Loop · faultyENG 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 Feb 13, 2008 · N122UX · Beech 1900D · Fire DetectionSDR GLBA20060893Skin · crackedDURING 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 5Feb 11, 2007 · N122UX · Beech 1900D · Fuselage Main, Plate/SkinSDR 20060893Skin · crackedDURING 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 STATIONFeb 11, 2007 · N122UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20060884Skin · crackedLT 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.Jan 12, 2007 · N122UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20060885Skin · crackedRT 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.Jan 12, 2007 · N122UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20060812Doubler · crackedLEFT AND RIGHT HEAVY DOUBLERS CRACKED AT FS 288.0 P/N 114-430002-7180 (RIGHT) AND 114-430002-7179 (LEFT). REPAIR PENDING.Aug 8, 2006 · N122UX · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA20060688Smoke · detectedSMOKE IN CABIN. SMOKE APPEARED TO DISSIPATE AFTER TURNING OFF MASTER SWITCH. INSPECTED ELECTRICAL SYSTEM, COULD NOT DUPLICATE.Mar 1, 2006 · N122UX · Beech 1900D · Air Distribution SystemSDR GLBA20060679Smoke · detectedREPORT OF SMOKE (ELECTRICAL) SMELL IN COCKPIT, FLIGHT DIRECTOR C/B POPPED, RESET CIRCUIT BREAKER, OPS CHECKED SYSTEM GOOD.Feb 17, 2006 · N122UX · Beech 1900D · Air Distribution SystemSDR GLBA20060669Actuator · intermittentLEFT 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.Feb 11, 2006 · N122UX · Beech 1900D · Landing Gear ActuatorSDR GLBA20060665Downlock Switch · out of adjustLEFT 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.Feb 6, 2006 · N122UX · Beech 1900D · Landing Gear Position and WarningSDR 20030828Frame · crackedDURING 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.Mar 30, 2005 · N122UX · Beech 1900D · Fuselage Main, Frame
Back to N122UX