# Service difficulty reports: N184UX

A list on [N184UX](https://openairdocs.org/aircraft/N184UX.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 · 81 reports

- [SDR TIMA2024071105007](https://openairdocs.org/sdr/TIMA2024071105007.md): Engine · power loss · Jul 5, 2024 · N184UX · Beech 1900D · Engine (Turbine/Turboprop)
  > AFTER DESCENDING AND LEVELING OFF LEFT ENGINE TORQUE NOT RISISNG PROPERLY AND INCORRECT ENGINE CONTROL/FEEL, PILOT NOTICED IMPROPER PWOER OUT OF LEFT ENGINE AND DECLARED EMERGENCY DUE TO PARITAL POWER ON LEFT ENGINE. PILOT WAS CLEARED TO LAND. LANDED SAFELY AN
- [SDR TIMA20221003011](https://openairdocs.org/sdr/TIMA20221003011.md): Engine · low torque · Sep 27, 2022 · N184UX · Beech 100BEECH · Engine Indicating System
  > NORMAL START, NORMAL RUNNUP. ADVANCED POWER ON RWY 28R AND MANIPULATED POWER LEVERS TO MATCH TORQUES. ROTATED AT VR AND NOTICED AN ABNORMAL SPLIT IN THE POSITION OF THE POWER LEVERS. SCANNED THE ENGINE INSTRUMENTS FOR ANY ABNORMALITIES AND FOUND THE LEFT ENGIN
- [SDR GLBA2016082500607](https://openairdocs.org/sdr/GLBA2016082500607.md): Bracket · worn · Aug 23, 2016 · N184UX · Beech 1900D · Propeller System
  > PILOT REPORTED THAT THE LEFT PROPELLER SEEMS LIKE IT TRIES TO AUTOFEATHER FURING FINAL. MAINTENANCE R & R THE BETA ARM LEVER IAW BMM 61-20-00 STEP 2 PN:3054890-01, RR BETA ARM BRACKET BY REMOVING THE 2 NUTS & INSTALLED THE NEW ONE IN REVERSE ORDER PN:3111379-
- [SDR GLBA2016031800575](https://openairdocs.org/sdr/GLBA2016031800575.md): Support · cracked · Mar 18, 2016 · N184UX · Beech 1900D · Fuselage Miscellaneous Structure
  > MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THE LT SIDEWALL SEAT TRACK SUPPORT, STRINGER 10L, CRACKED IN THE FLANGE BEND RADIUS, AT FS 327.63, 1" IN LENGTH. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAP
- [SDR GLBA2016030200574](https://openairdocs.org/sdr/GLBA2016030200574.md): Panel · cracked · Mar 2, 2016 · N184UX · Beech 1900D · Wing Miscellaneous Structure
  > MAJOR REPAIR DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE NUTPLATE PANEL FOR THE ACCESS DOOR 632IB, WS 148.2, RT WING LOWER SIDE, 1.4" IN LENGTH. WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.
- [SDR GLBA2016021700571](https://openairdocs.org/sdr/GLBA2016021700571.md): Bracket · worn · Feb 15, 2016 · N184UX · Beech 1900D · Trailing Edge Flaps
  > MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THE INBD ATTACH BOLT WORN INTO BRACKET ON THE RT INBD FLAP ACTUATOR. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.
- [SDR GLBA2016021500570](https://openairdocs.org/sdr/GLBA2016021500570.md): Frame · cracked · Feb 12, 2016 · N184UX · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND FUSELAGE FRAME FLANGE CRACKED, FROM THE BEND RADIUS TO THE EDGE OF THE FLANGE, FS 150.60 BETWEEN STRINGER 2R & 3R,.75" IN LENGTH. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RE
- [SDR GLBA2016021500569](https://openairdocs.org/sdr/GLBA2016021500569.md): Skin · dented · Feb 12, 2016 · N184UX · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION, FOUND A DENT IN THE FUSELAGE SKIN, BETWEEN FS 378.25 & 381.25, BELOW STRINGER 12L. DENT APPROX SIZE 2.7 X 2. MAJOR REPAIR.
- [SDR GLBA2016021500568](https://openairdocs.org/sdr/GLBA2016021500568.md): Skin · cracked · Feb 12, 2016 · N184UX · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION, FOUND THE BELLY SKIN AT FS 225.25, BETWEEN STRINGER 16 & 15R, CRACKED APPROX.2" IN LENGTH, EVIDENCE OF CORROSION FROM STRINGER 15R GOING INBD 4 FASTENERS. MAJOR REPAIR.
- [SDR GLBA2016021500567](https://openairdocs.org/sdr/GLBA2016021500567.md): Bracket · worn · Feb 12, 2016 · N184UX · Beech 1900D · Trailing Edge Flaps
  > MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THE OTBD ATTACH BOLT WORN INTO THE BRACKET OF THE RT INBD FLAP ACTUATOR. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.
- [SDR GLBA2016020900566](https://openairdocs.org/sdr/GLBA2016020900566.md): Skin · damaged · Feb 8, 2016 · N184UX · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND AT FS 281.00, BETWEEN STRINGERS 14L & 13L, A 3" LONG,.5" WIDE WARE IMPRESSION FROM THE HYD LINE & A SMALL PIN HOLE IN THE CTR. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETEN
- [SDR GLBA2015082000531](https://openairdocs.org/sdr/GLBA2015082000531.md): Snubber · detached · Aug 19, 2015 · N184UX · Beech 1900D · Passenger/Crew Doors
  > SIG EVENT, PILOT NOTED THAT THE CABIN DOOR SNUBBER DETACHED IN FLIGHT. LOCATED THE UPPER BOLT FOR THE AIRSTAIR DOOR SNUBBER ON THE FLOORBOARD. INSPECTED THREADS ON THE BOLT & RECEPTACLE, NO DEFECTS NOTED. REINSTALLED UPPER BOLT IAW AIM 12 15 0, NO FURTHER D
- [SDR GLBA2015010200489](https://openairdocs.org/sdr/GLBA2015010200489.md): Master Cylinder · leaking · Jan 1, 2015 · N184UX · Beech 1900D · Master Cylinder/Brake Valve
  > THE LT BRAKE PEDAL IS MUSHY & IT MUST BE FULLY DEPRESSED TO ACTIVATE THE BRAKES. FOUND EVIDENCE TO SUSPECT THAT THE CAPTAIN'S LT BRAKE MASTER CYLINDER, SN 4112, WAS BYPASSING INTERNALLY. THE CAPTAIN`S BRAKE MASTER CYLINDER WAS R & R IAW BMM 32-40-06. DURING
- [SDR GLBA2014123000487](https://openairdocs.org/sdr/GLBA2014123000487.md): Line · loose · Dec 29, 2014 · N184UX · Beech 1900D · Landing Gear Brake System
  > THE CAPTAIN`S LEFT BRAKE PEDAL WENT TO THE FLOOR. FOUND THE BRAKE LINE LOOSE AT CLUSTER FITTING BETWEEN 1 & 2 BRAKE. TIGHTENED BRAKE LINE & BLED BRAKES IAW TC 1900-3240.02 STEPS 6 - 9. OPS CHECKED GOOD.
- [SDR GLBA2014081800429](https://openairdocs.org/sdr/GLBA2014081800429.md): Engine · failed · Aug 15, 2014 · N184UX · Beech 1900D · Engine (Turbine/Turboprop)
  > PILOT REPORTED THAT AFTER REACHING CRUISE FLT LEVEL 240, NR 2 ENGINE FAILED WITH A BANG. LOST ALL POWER, PROP AUTO FEATHERED, RAN CHECK LIST, EMERGENCY DECLARED & DIVERTED. REMOVED AND REPLACED THE ENGINE R & R RT ENG ASSEMBLY IAW TC 1900-7100.00 REV 8. OP
- [SDR GLBA2013081600294](https://openairdocs.org/sdr/GLBA2013081600294.md): Skin · cracked · Aug 16, 2013 · N184UX · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION FOUND THE RT FUSELAGE BELLY SKIN CRACKED AT JUNCTION WITH WING SPAR AT FS 288, FWD SIDE OF WING SPAR,.9" IN LENGTH. REPAIRED IAW EO 13-1900-53-055.
- [SDR GLBA2013080200289](https://openairdocs.org/sdr/GLBA2013080200289.md): Frame · cracked · Aug 2, 2013 · N184UX · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE COCKPIT RT SIDEWALL FRAME AT FS 107 AT UPPER FASTENER,.5" IN LENGTH. REPAIRED IAW EO 13-1900-53-053.
- [SDR GLBA2013080200288](https://openairdocs.org/sdr/GLBA2013080200288.md): Longeron · cracked · Aug 2, 2013 · N184UX · Beech 1900D · Fuselage Main, Longeron/Stringer
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE COCKPIT RT SIDEWALL LONGERON AT FS 107,.5" IN LENGTH. REPAIRED IAW EO 13-1900-53-054.
- [SDR GLBA2013073000287](https://openairdocs.org/sdr/GLBA2013073000287.md): Stringer · damaged · Jul 29, 2013 · N184UX · Beech 1900D · Horizontal Stabilizer, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A HOLE IN THE STRINGER ON THE VERTICAL STAB, LT SIDE AT CSS-68 AND 29.75 PERCENT CHORD, HOLE APPROX.5" IN DIAMETER. REPAIRED IAW EO 13-1900-55-019.
- [SDR GLBA2013073000286](https://openairdocs.org/sdr/GLBA2013073000286.md): Rib · cracked · Jul 29, 2013 · N184UX · Beech 1900D · Wing, Rib/Bulkhead
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE RT INBD WING INBD RIB AT BL-29 AFT SIDE BY SPAR,.75 INCHE IN LENGTH. REPAIRED IAW EO 13-1900-57-014.
- [SDR GLBA2013073000284](https://openairdocs.org/sdr/GLBA2013073000284.md): Angle · cracked · Jul 29, 2013 · N184UX · Beech 1900D · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE A/S DOOR ANGLE AT FS 150.60 AT BOTH UPPER SNUBBER MOUNT NUTPLATES, TWO INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-051.
- [SDR GLBA2013073000283](https://openairdocs.org/sdr/GLBA2013073000283.md): Frame · cracked · Jul 29, 2013 · N184UX · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND THREE CRACKS IN THE FUSELAGE FRAME AT BS 183.5, BETWEEN S2-3R AND SECOND CRACK FOUND FIVE INCHES OTBD, AND THIRD CRACK ON OTHER SIDE OF FASTENER, 1.125 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-050.
- [SDR GLBA2013072600280](https://openairdocs.org/sdr/GLBA2013072600280.md): Valve · inoperative · Jul 26, 2013 · N184UX · Beech 1900D · Landing Gear Retraction/Extension System
  > PILOT REPORTED ON GEAR EXTENSION, INTRANSIT LIGHT ILLUMINATED MOMENTARILY, THEN GEAR HANDLE CIRCUIT BREAKER TRIPPED, LOST ALL GEAR INDICATIONS, FOLLOWED CHECKLIST, EXTENDED GEAR MANUALLY, THREE GREEN OBSERVED, LANDED WITHOUT FURTHER INCIDENT, EMERGENCY DECLAR
- [SDR GLBA2013072900282](https://openairdocs.org/sdr/GLBA2013072900282.md): Circuit Breaker · tripped · Jul 26, 2013 · N184UX · Beech 1900D · Landing Gear System Wiring
  > PILOT REPORTED THAT THE LANDING GEAR CIRCUIT BREAKER TRIPPED IN FLT, PERFORMED MANUAL EXTENTION. COULD NOT DUPLICATE.
- [SDR GLBA2013072900281](https://openairdocs.org/sdr/GLBA2013072900281.md): Landing Gear · failed · Jul 26, 2013 · N184UX · Beech 1900D · Landing Gear Retraction/Extension System
  > PILOT REPORTED THAT DURING AN OPS CHECK, FLIGHT TO TEST THE GEAR, THE GEAR FAILED TO EXTEND, 2 AMP CIRCUIT BREAKER TRIPS AT HANDLE, PUMPED GEAR DOWN MANUALLY. OPS CHECK FLIGHT UNSATISFACTORY.
- [SDR GLBA2013072500280](https://openairdocs.org/sdr/GLBA2013072500280.md): Relay · failed · Jul 24, 2013 · N184UX · Beech 1900D · Landing Gear Retraction/Extension System
  > DURING CRUISE, LOWERED LANDING GEAR HANDLE, HEARD NOTHING, INTRANSIT LIGHT WAS ON THEN WENT OUT AFTER 60 SECONDS, NOTICED LANDING GEAR HANDLE CIRCUIT BREAKER TRIPPED, RAN CHECKLIST, NO CHANGE, PUMPED GEAR DOWN, & DIVERTED. MX REPLACED THE LANDING GEAR HANDLE,
- [SDR GLBA2013060400256](https://openairdocs.org/sdr/GLBA2013060400256.md): Gearbox · failed · Jun 4, 2013 · N184UX · Beech 1900D · Air Distribution System
  > DURING CLIMBOUT EXPERIENCED SMOKE IN THE CABIN, DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE, FLAPS DID NOT EXTEND, SMOKE DISSAPATED AFTER FIVE MINUTES. R & R FLAP GEAR BOX MOTOR ASSY IAW MM 27-50-03, PN 100-524073-1. SN OFF 6245 ON 979. R & R RT INBD FL
- [SDR GLBA2013012100159](https://openairdocs.org/sdr/GLBA2013012100159.md): Bulb · inoperative · Jan 18, 2013 · N184UX · Beech 1900D · Emergency Lighting
  > PILOT REPORTED THAT THE CAPT'S SIDE EMERGENCY LIGHT IS INOPERATIVE. MX REPLACED LIGHT BULBS, OPS CHECKED GOOD.
- [SDR GLBA2012121000131](https://openairdocs.org/sdr/GLBA2012121000131.md): Bulb · inoperative · Dec 7, 2012 · N184UX · Beech 1900D · Emergency Lighting
  > PILOT REPORTED THAT THE INSTRUMENT EMERGENCY LIGHT IS INOPERATIVE. MX REPLACED THE BULB, OPS CHECKED GOOD.
- [SDR GLBA2012092400067](https://openairdocs.org/sdr/GLBA2012092400067.md): Angle · cracked · Sep 24, 2012 · N184UX · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND TWO CRACKS ON THE LT FWD SPAR CAP ANGLE ON THE VERTICAL STAB COMING DOWN TO THE FIRST FASTENER,.375" IN LENGTH, AND A SECOND CRACK NEXT TO THE SECOND FASTENER FROM THE TOP,.5" IN LENGTH. REPAIRED IAW FR-CO-02532,
- [SDR GLBA2012092400066](https://openairdocs.org/sdr/GLBA2012092400066.md): Spar Cap · cracked · Sep 24, 2012 · N184UX · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND CRACK ON THE RT FWD SPAR CAP ANGLE ON THE VERTICAL STAB COMING DOWN TO THE FIRST FASTENER,.375" IN LENGTH. REPAIRED IAW FR-CO-02532 REV 1, STEP 1. MAJOR REPAIR.
- [SDR GLBA2012082400039](https://openairdocs.org/sdr/GLBA2012082400039.md): Bulb · inoperative · Aug 23, 2012 · N184UX · Beech 1900D · Emergency Lighting
  > PILOT REPORTED THAT THE F/O EMERGENCY LIGHT BULB IS INOPERATIVE. MX REPLACED BULB, OPS CHECKED GOOD.
- [SDR GLBA2012042701](https://openairdocs.org/sdr/GLBA2012042701.md): Bulkhead · cracked · Apr 27, 2012 · N184UX · Beech 1900D · Fuselage Main, Bulkhead
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE FWD PRESSURE BULKHEAD ALONG THE OTBD ROW OF FASTENERS NEXT TO THE RT NOSE GEAR WEB AT FS 84.00,.375" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1
- [SDR GLBA2012042605](https://openairdocs.org/sdr/GLBA2012042605.md): Frame · cracked · Apr 25, 2012 · N184UX · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FRAME AT FS 150 AND STRINGER 9AL, AT NUTPLATE FOR A/S DOOR STRUT LWR MOUNT,.75" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-028. MAJOR REPAIR
- [SDR GLBA2012042604](https://openairdocs.org/sdr/GLBA2012042604.md): Frame · cracked · Apr 25, 2012 · N184UX · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FRAME AT FS 164 AND STRINGER 9AR AT CUTOUT,.35" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-026. MAJOR REPAIR.
- [SDR GLBA2012042603](https://openairdocs.org/sdr/GLBA2012042603.md): Frame · cracked · Apr 25, 2012 · N184UX · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE FUSELAGE FRAME AT FS 509 AND AFT GAS STRUT MOUNT AREA FROM CENTER OF THE UPPER INBD GAS STRUT NUTPLACE SCREW HOLES. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. E
- [SDR GLBA2012042602](https://openairdocs.org/sdr/GLBA2012042602.md): Bulkhead · cracked · Apr 25, 2012 · N184UX · Beech 1900D · Fuselage Main, Bulkhead
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE FWD PRESSURE BULKHEAD ALONG ROW OR FASTENERS NEXT TO THE LT NOSE GEAR WEB, FS 84.00, 7.25" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-029. MA
- [SDR GLBA2012022801](https://openairdocs.org/sdr/GLBA2012022801.md): Spar · cracked · Feb 28, 2012 · N184UX · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE HORIZONTAL FWD SPAR WEB JUST INBD OF RT HSS 00.0, APPROX.5" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTION IAW EO 12-1900-55-004. MAJOR REPAIR.
- [SDR GLBA20111116G](https://openairdocs.org/sdr/GLBA20111116G.md): Uplock Switch · inoperative · Nov 15, 2011 · N184UX · Beech 1900D · Landing Gear Position and Warning
  > WITH THE AUTOFEATHER SWITCH OFF, AUTOFEATHER OFF ANNUNCIATOR AND MAST CAUTION ANNUNCIATOR DO NOT ILLUMINATE. MX REPLACED THE LT UPLOCK SWITCH IAW EO 11-1900-32-002, OPS CHECKED GOOD.
- [SDR GLBA20111020G](https://openairdocs.org/sdr/GLBA20111020G.md): Propeller · malfunctioned · Oct 19, 2011 · N184UX · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT THE LT PROP WON'T MANUALLY FEATHER. MX INSPECTED THE LINKAGE AND RAN ENG, NO DEFECTS NOTED.
- [SDR GLBA201110181](https://openairdocs.org/sdr/GLBA201110181.md): Bulb · burned out · Oct 18, 2011 · N184UX · Beech 1900D · Emergency Lighting
  > EMERGENCY LIGHT UNDER GLARESHIELD ON CAPT SIDE INOPERATIVE FOUND DURING PREFLIGHT INSPECTION BY CREW. MX DETERMINED BULB WAS BURNED OUT AND REPLACED THE BULB.
- [SDR GLBA20111017J](https://openairdocs.org/sdr/GLBA20111017J.md): Handle · out of position · Oct 14, 2011 · N184UX · Beech 1900D · Emergency Exits
  > PILOT REPORTED THAT THE EMERGENCY HANDLE AT 6C IS PUSHED IN. MX RESEATED THE EMERGENCY DOOR IAW BMM 52-20-01, OK FOR SERVICE.
- [SDR GLBA20110929G](https://openairdocs.org/sdr/GLBA20110929G.md): Line · leaking · Sep 28, 2011 · N184UX · Beech 1900D · Engine Fuel Distribution
  > PILOT REPORTED THAT THERE IS A POSSIBLE FUEL LEAK ON THE RT ENGINE NACELLE INSIDE THE WHEEL WELL. MX REPLACED THE FUEL DRAIN LINES, LEAK CHECKED GOOD.
- [SDR GLBA20110926F](https://openairdocs.org/sdr/GLBA20110926F.md): Handle · damaged · Sep 25, 2011 · N184UX · Beech 1900D · Emergency Exits
  > PILOT REPORTED THAT THE EMERGENCY EXIT DOOR AT 6C HANDLE SEEMS TO BE DEPRESSED. MX REINSTALLED THE DOOR IAW BMM 52-26-00, SYS OK FOR SERVICE.
- [SDR GLBA20110908F](https://openairdocs.org/sdr/GLBA20110908F.md): Handle · unsecure · Sep 7, 2011 · N184UX · Beech 1900D · Emergency Exits
  > PILOT REPORTED THAT THE RT SIDE EMERGENCY DOOR HANDLE LOOKS NOT SECURED. MX RESECURED THE EMERGENCY EXIT DOOR REF 52-20-00.
- [SDR GLBA20110805F](https://openairdocs.org/sdr/GLBA20110805F.md): Skin · dented · Aug 5, 2011 · N184UX · Beech 1900D · Wing, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSP MX FOUND A DENT IN THE RT WING L/E AT WS 167.24 MEASURING 7" WIDE, 3" HIGH,.5" DEEP. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-57-008. MATERIALS UTILIZED ARE INCLUDED IN THE EO. MAJ
- [SDR GLBA20110613G](https://openairdocs.org/sdr/GLBA20110613G.md): Wire · chafed · Jun 12, 2011 · N184UX · Beech 1900D · Landing Gear System Wiring
  > PILOT REPORTED THAT WHEN GEAR WAS SELECT UP, GEAR FAILED TO RETRACT, LANDING GEAR CB TRIPPED, RETURNED TO DEPARTURE. MX RESECURED A LOOSE PCB AND REPAIRED A CHAFED WIRE, OPS CHECK GOOD.
- [SDR GLBA20101027G](https://openairdocs.org/sdr/GLBA20101027G.md): Frame · cracked · Oct 27, 2010 · N184UX · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A.5" CRACK IN THE LT HEAVY ANGLE IN THE BEND RADIUS AT FS 303.25. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-061. MATERIALS UTILIZED ARE INCLUDED IN THE
- [SDR GLBA20101027F](https://openairdocs.org/sdr/GLBA20101027F.md): Skin · debonded · Oct 27, 2010 · N184UX · Beech 1900D · Passenger/Crew Doors
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND THE AIRSTAIR DOOR DEBONDED AT THE HINDGE ATTACH AREA AND OUTER SKIN DEBONDED 3.5" TO 4" INWARD FROM EDGE OF DOOR. MX REPLACED THE AIRSTAIR DOOR IAW MM 52-10-03, OPS CHECK GOOD, COMPLIED WITH ALL RII REQ
- [SDR GLBA20100329G](https://openairdocs.org/sdr/GLBA20100329G.md): Circuit Board · deteriorated · Mar 28, 2010 · N184UX · Beech 1900D · Propeller Feathering/Reversing
  > SUSPECTED AUTOFEATHER - PILOTS REPORTED THAT THE NR 2 ENGINE AUTOFEATHER WAS CYCLING DURING FINAL APPROACH. MX R & R THE HIGH AND LOW PRESSURE SWITCHES IAW BMM 61-21-01. MX ADDITIONALLY R & R THE AUTOFEATHER PRINTED CIRCUIT BOARD IAW BMM 20-03-00. OPS CHECK

Next page: https://openairdocs.org/aircraft/N184UX/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 = 'N184UX' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N184UX/reports

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