# Service difficulty reports: N202UX

A list on [N202UX](https://openairdocs.org/aircraft/N202UX.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 · 77 reports

- [SDR GLBA2017022700635](https://openairdocs.org/sdr/GLBA2017022700635.md): Downlock Switch · inoperative · Feb 24, 2017 · N202UX · Beech 1900D · Landing Gear Position and Warning
  > PILOTS REPORTED THAT THEY RECEIVED A GPWS WARNING FOR AN UNSAFE GEAR CONDITION DURING A RETURN TO FIELD FOR A CABIN DOOR ANNUNCIATOR. THE CREW MANUALLY EXTENDED THE GEAR AND DECLARED AN EMERGENCY WITH THE TOWER. MAINTENANCE REMOVED AND REPLACED THE NLG DOWNLOC
- [SDR GLBA2017022400634](https://openairdocs.org/sdr/GLBA2017022400634.md): Shaft · worn · Feb 22, 2017 · N202UX · Beech 1900D · Passenger/Crew Doors
  > MAINTENANCE NOTED THAT THE PAX DOOR HANDLE WAS LOOSE. REMOVED AND REPLACED THE PAX DOOR HANDLE SHAFT AND ROLL PIN IAW AMM 52-10-05. OPS CHECKED GOOD.
- [SDR GLBA2016111700616](https://openairdocs.org/sdr/GLBA2016111700616.md): Cable · broken · Nov 16, 2016 · N202UX · Beech 1900D · Passenger/Crew Doors
  > SIG EVENT, PILOT REPORTED THAT THE LOWER FORWARD CABIN DOOR CABLE BROKEN (HANDRAIL CABLE). MAINTENANCE REMOVED AND REPLACED THE LOWER FORWARD MAIN CABIN DOOR CABLE REF 52-10-02, P/N 1440-43GLA.
- [SDR GLBA2016072600600](https://openairdocs.org/sdr/GLBA2016072600600.md): Bolt · dislodged · Jul 23, 2016 · N202UX · Beech 1900D · Passenger/Crew Doors
  > MAINTENANCE PERSONNEL NOTED THAT THE AIRSTAIR DOOR ACCUMULATOR TOP ATTACH BOLT FELL OUT OF THE HOUSING. MAINTENANCE ATTACHED THE AIRSTAIR DOOR SNUBBER TOP BOLT IAW TC 1900-5210.01.
- [SDR GLBA2016072600001](https://openairdocs.org/sdr/GLBA2016072600001.md): Bolt · unsecure · Jul 23, 2016 · N202UX · Beech 1900D · Passenger/Crew Doors
  > SIGNIFICANT EVENT, PILOT NOTED THAT THE CABIN DOOR SNUBBER TOP ATTACH BOLT FELL OUT. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR AND RETENTION OF THE PAPERWORK.
- [SDR GLBA2016070800593](https://openairdocs.org/sdr/GLBA2016070800593.md): Bolt · broken · Jul 5, 2016 · N202UX · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE ATTACHING BULT ON THE CABIN DOOR BROKE. MAINTENANCE REPLACED THE BOLT ON THE LOWER END OF THE CABIN DOOR STRUT IAW MM 52-10-01(1)(B) STEPS 9-10, OPS CHECKED GOOD.
- [SDR GLBA2016040700578](https://openairdocs.org/sdr/GLBA2016040700578.md): Skin · cracked · Apr 6, 2016 · N202UX · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR DURING A SCHEDULED INSPECTION, FOUND THE FUSELAGE BELLY SKIN CORRODED & CRACKED AT FS 213.25 & STRINGER 14R,.2" IN LENGTH. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.
- [SDR GLBA2015111600558](https://openairdocs.org/sdr/GLBA2015111600558.md): Bolt · unsecure · Nov 15, 2015 · N202UX · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE DOOR SNUBBER BOLT CAME OFF. APPLIED LOCTITE 242 TO THE BOLT THREADS & REINSTALLED THE BOLT IAW TC 1900-5210 01 STEP 13. OPERATIONAL CHECKED GOOD.
- [SDR GLBA2015032500507](https://openairdocs.org/sdr/GLBA2015032500507.md): Fan · malfunctioned · Mar 24, 2015 · N202UX · Beech 1900D · Air Distribution Fan
  > PILOT REPORTED THAT THERE WAS LIGHT SMOKE COMING FROM THE FLOOR VENTS. REPLACED THE AFT VENT BLOWER IAW AIM 21-07. OPERATIONS CHECKED GOOD.
- [SDR GLBA2014110400463](https://openairdocs.org/sdr/GLBA2014110400463.md): Shimmy Dampener · faulty · Nov 2, 2014 · N202UX · Beech 1900D · Shimmy Damper
  > DURING TAXI OUT, THE CREW NOTED THAT THE ACFT WOULD NOT STEER TO THE RT WITH MAX DIFFERENTIAL BRAKING POWER & NOSE WHEEL STEERING. TOWED THE ACFT BACK TO THE GATE & REPLACED THE NOSE SHIMMY DAMPER IAW BMM 32-50-00. AFTER RELEASE, THE ACFT FLEW & WHILE TAXIIN
- [SDR GLBA2014082900434](https://openairdocs.org/sdr/GLBA2014082900434.md): Frame · corroded · Aug 29, 2014 · N202UX · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION MAINTENANCE FOUND CORROSION ON THE FUSELAGE FRAME AT FS 198.25 BETWEEN STRINGERS 15L & 14L, UPPER SURFACE, AREA CORRODED 2.25 INCHES BY.75 INCHES. DEEPEST PITTED AREA IS APPROX.03 INCHES ALONG LE, DEEP PITTED SPOT TOWARD STRING
- [SDR GLBA2014082500432](https://openairdocs.org/sdr/GLBA2014082500432.md): Rib · cracked · Aug 25, 2014 · N202UX · Beech 1900D · Wing, Rib/Bulkhead
  > DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE RT WING INBD RIB AT BL 29 & WING SPAR, RIB FLANGE CRACKED AT JUNCTION WITH WING SPAR, APPROX 1 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-57-005. MA
- [SDR GLBA2014082600433](https://openairdocs.org/sdr/GLBA2014082600433.md): Repair · cracked · Aug 25, 2014 · N202UX · Beech 1900D · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE LT HEAVY CLOSING ANGLE REPAIR AT FS 288.00, IN THE BEND RADIUS OF THE REPAIR ANGLE,.65 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-030. MATERIALS
- [SDR GLBA2014082500431](https://openairdocs.org/sdr/GLBA2014082500431.md): Frame · cracked · Aug 25, 2014 · N202UX · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE FLANGE RADIUS ON THE FRAME AT FS 451 & STRINGER 10R.5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-029. MATERIALS UTILIZED ARE INCLUDED IN THE ENG
- [SDR GLBA2014052700415](https://openairdocs.org/sdr/GLBA2014052700415.md): Actuator · failed · May 25, 2014 · N202UX · Beech 1900D · Landing Gear Actuator
  > PILOT REPORTED THAT WHILE COMING IN ON FINAL SELECTED THE GEAR DOWN & AFTER THE LG CYCLED, THE LT GEAR FAILED TO ILLUMINATE DOWN & LOCKED, RAN CHECKLIST, FAILED TO RESOLVE SITUATION, CONTACTED DISPATCH & TOWER DECLARED EMERGENCY, PUMPED GEAR DOWN. MAINTENANCE
- [SDR GLBA2013122300363](https://openairdocs.org/sdr/GLBA2013122300363.md): Latch · lack of lube · Dec 20, 2013 · N202UX · Beech 1900D · Emergency Exits
  > PILOT REPORTED THAT THE EMERGENCY EXIT DOOR AT 6C, EXTERIOR LATCH IS NOT STOWED. R & R 6C EMERGENCY DOOR IAW AMM 52-20-00, OPS CHECKED GOOD. LUBRICATED LATCH IAW 52-20-01 STEPS 1B18 1B14 1B22.
- [SDR GLBA2013121300354](https://openairdocs.org/sdr/GLBA2013121300354.md): Unknown · odor · Dec 12, 2013 · N202UX · Beech 1900D · Air Distribution System
  > PILOT REPORTED FUEL LEAKING ON THE RT WING LOWER SURFACE AT THE WING ROOT AT THE MID CHORD, ALSO HAS A STRONG FUEL ODOR IN CABIN. MAINTENANCE INSPECTED AUX TANK, FOUND NO LEAKS.
- [SDR GLBA2013102200342](https://openairdocs.org/sdr/GLBA2013102200342.md): Indicator · malfunctioned · Oct 21, 2013 · N202UX · Beech 1900D · Propeller Indication System
  > PILOT REPORTED AFTER TAKE OFF, LT PROP RPM ROSE TO 1730 FOR 15 SECS, PULLED BACK PROP LEVERS AND CONTINUED TO CLIMB, LEVELED OFF AND TRIED TO SYNC PROPS, RECEIVED A VIBRATION, TURNED OFF PROP SYNC AND SYNC'D, NR 1 AT 1400 AND NR 2 AT 1550, STARTED LOSING PROP
- [SDR GLBA2012122100138](https://openairdocs.org/sdr/GLBA2012122100138.md): Spar · chafed · Dec 21, 2012 · N202UX · Beech 1900D · Elevator, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CHAFED SPAR.035 ON TOP AND BOTTOM FLANGES AT HSS 98.197 AND A.5" CRACK EXTENDING FROM A RIVET HOLE ON THE BACK WALL OF THE SPAR ON THE LT ELEVATOR. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-27-005. MAJOR RE
- [SDR GLBA2012113000124](https://openairdocs.org/sdr/GLBA2012113000124.md): Skin · cracked · Nov 30, 2012 · N202UX · Beech 1900D · Elevator, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND T/E DAMAGE.35" -.35" ON THE OTBD END OF THE LT ELEVATOR. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-27-005. MAJOR REPAIR.
- [SDR GLBA2012112800121](https://openairdocs.org/sdr/GLBA2012112800121.md): Longeron · cracked · Nov 28, 2012 · N202UX · Beech 1900D · Fuselage Main, Longeron/Stringer
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND TWO CRACKS COMING OUT OF A RIVET HOLE ON LONGERON UNDER FINGER DOUBLER AT FS 107,.5" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-072. MAJOR REPAIR.
- [SDR GLBA2012112800120](https://openairdocs.org/sdr/GLBA2012112800120.md): Structure · cracked · Nov 28, 2012 · N202UX · Beech 1900D · Vertical Stabilizer
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND TWO CRACKS COMING OUT OF RIVET HOLE, ONE CRACK COMING OUT OF ANOTHER RIVET HOLE ON THE LONGERON UNDER FINGER DOUBLER AT FS 107, 0.375" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-073. MAJOR REPAIR.
- [SDR GLBA2012112600116](https://openairdocs.org/sdr/GLBA2012112600116.md): Spar · cracked · Nov 26, 2012 · N202UX · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND THE LT VERTICAL FWD SPAR CAP ANGLE HAS A CRACK AT TWO RIVETS AT FSS 84.10 AND 20 PERCENT CHORD,.25" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-059. MAJOR REPAIR.
- [SDR GLBA2012112600115](https://openairdocs.org/sdr/GLBA2012112600115.md): Web · cracked · Nov 26, 2012 · N202UX · Beech 1900D · Horizontal Stabilizer Structure
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND THE HORIZONTAL STABILIZER AFT SPAR WEB HAS A CRACK PROTRUDING OUT OF THE ACCESS HOLE AT HSS 00.00,.5" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-058. MAJOR REPAIR.
- [SDR GLBA2012112600114](https://openairdocs.org/sdr/GLBA2012112600114.md): Angle · cracked · Nov 26, 2012 · N202UX · Beech 1900D · Vertical Stabilizer
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND THE VERTICAL STABILIZER RT FWD SPAR CAP ANGLE CRACKED BY TOP RIVET AT FSS 84.10 AND 20 PERCENT CHORD,.25" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO12-1900-55-060. MAJOR REPAIR.
- [SDR GLBA2012112600113](https://openairdocs.org/sdr/GLBA2012112600113.md): Frame · cracked · Nov 26, 2012 · N202UX · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND FUSELAGE FRAME AT FS 107 AND STRINGER 8R CRACKED AT INBD FLANGE AT UPPER FASTENER HOLE,.5" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-070. MAJOR REPAIR.
- [SDR GLBA2012112600112](https://openairdocs.org/sdr/GLBA2012112600112.md): Frame · cracked · Nov 26, 2012 · N202UX · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND FUSELAGE FRAME AT FS 107.00 AND STRINGER 8L CRACKED AT INBD FLANGE TO UPPER FASTENER HOLD,.5" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-071. MAJOR REPAIR.
- [SDR GLBA2012081300030](https://openairdocs.org/sdr/GLBA2012081300030.md): Skin · dented · Aug 11, 2012 · N202UX · Beech 1900D · Wing, Plate/Skin
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION FOUND A DENT AT WS 290.06 ON RT WING, 9" BY 4" AREA. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-57-009. MATERIALS UTILIZED ARE INCLUDED IN THE EO.
- [SDR GLBA2012061211](https://openairdocs.org/sdr/GLBA2012061211.md): Wire · broken · Jun 9, 2012 · N202UX · Beech 1900D · Landing Gear System Wiring
  > LANDING GEAR RELAY CIRCUIT BREAKER TRIPPED IN FLIGHT. CREW NOTICED ROUGHLY 10 MINUTES IN TO THE FLIGHT. MX REPAIRED A BROKEN WIRE BY SEAT 2A IAW WM 20-10-00, OPS CK GOOD.
- [SDR GLBA201206111](https://openairdocs.org/sdr/GLBA201206111.md): Relay · failed · Jun 8, 2012 · N202UX · Beech 1900D · Landing Gear Retraction/Extension System
  > ON SELECTING GEAR DOWN ON APPROACH. LANDING GEAR RELAY CIRCUIT BREAKER TRIPPED IMMEDIATELY. AFTER PERFORMING "FAILURE OF LANDING GEAR TO EXTEND NORMALLY" CHECKLIST, GEAR WAS DETERMINED UNSAFE. "LANDING GEAR MANUAL EXTENSION" CHECKLIST PERFORMED, LANDING G
- [SDR GLBA20111122F](https://openairdocs.org/sdr/GLBA20111122F.md): Drain · leaking · Nov 21, 2011 · N202UX · Beech 1900D · Fuel Boost Pump
  > THE FUEL PUMP FCU DRAIN IS DRIPPING ON THE LT ENGINE. MX BAGGED ALL DRAINS ON THE LEFT ENGINE, NO LEAKS NOTED.
- [SDR GLBA20111028F](https://openairdocs.org/sdr/GLBA20111028F.md): Unknown · odor · Oct 28, 2011 · N202UX · Beech 1900D · Air Distribution System
  > PILOT REPORTED A BURNED RUBBER ODOR IN COCKPIT. MX INSPECTED AND FOUND NO ODORS IN THE COCKPIT OR CABIN, INSPECTED WINDSHIELD HEAT SYS, NO DEFECTS FOUND, RAN ACFT, NO DEFECTS FOUND, OK FOR SERVICE.
- [SDR GLBA201110281](https://openairdocs.org/sdr/GLBA201110281.md): Unknown · odor · Oct 28, 2011 · N202UX · Beech 1900D · Air Distribution System
  > BURNED RUBBER SMELL IN COCKPIT.
- [SDR GLBA20111017G](https://openairdocs.org/sdr/GLBA20111017G.md): Pump · leaking · Oct 14, 2011 · N202UX · Beech 1900D · Engine Fuel Pump
  > "SUP" -MX REPORTED THAT THE LT HP FUEL PUMP WAS LEAKING. MX REPLACED THE FCU, OPS CK GOOD.
- [SDR GLBA20111005F](https://openairdocs.org/sdr/GLBA20111005F.md): Annunciator · no indication · Oct 3, 2011 · N202UX · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT THE AUTOFEATHER OFF ANNUNCIATOR IS NOT ILLUMINATING WHEN AUTOFEATHER SWITCH IS IN THE OFF POSITION. MX REPLACED LT UPLOCK SWITCH, OPS CHECKED GOOD IAW AIM MI 32-01.
- [SDR GLBA20110929F](https://openairdocs.org/sdr/GLBA20110929F.md): Pcb · inoperative · Sep 28, 2011 · N202UX · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT THE AUTOFEATHER OFF ANNUNCIATOR WILL NOT ILLUMINATE IN OFF OR TEST MODE. MX REPLACED THE PCB. OPS CHECKED GOOD.
- [SDR GLBA20110926H](https://openairdocs.org/sdr/GLBA20110926H.md): Bulb · inoperative · Sep 24, 2011 · N202UX · Beech 1900D · Landing Gear Position and Warning
  > PILOT REPORTED THAT THE H ON RT MAIN DOWN AND LOCKED ANNUNCIATOR DOES NOT ILLUMINATE. MX REPLACED THE BULB IAW BMM 33-10-00, OPS CHECKED GOOD.
- [SDR GLBA20110922F](https://openairdocs.org/sdr/GLBA20110922F.md): Line · leaking · Sep 21, 2011 · N202UX · Beech 1900D · Fuel Storage
  > PILOT REPORTED THAT FUEL WAS LEAKING FROM THE RT WING OR WHEEL WELL. MX TIGHTENED THE LINE ON THE RT FUEL VENT IAW BMM 28-20-01, LEAK CHECKED GOOD.
- [SDR GLBA20110902F](https://openairdocs.org/sdr/GLBA20110902F.md): Autofeather Sys · malfunctioned · Sep 1, 2011 · N202UX · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT THE PROP WENT INTO AUTOFEATHER ON FINAL, THEN CAME BACK OUT, FELT LIKE THE RT SIDE. MX TROUBLESHOT THE SYS IAW WITH THE RUNSHEET AND BMM 61-21-00 SEC 1(A), SYS OPS CHECKED GOOD, OK FOR SERVICE.
- [SDR GLBA20110824F](https://openairdocs.org/sdr/GLBA20110824F.md): Power Lever · split · Aug 23, 2011 · N202UX · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT WITH THE TORQUE SET AT 1000 LBS, RT PROP CYCLED IN & OUT OF FEATHER 3 TIMES WITH THE AFX ARMED. MX FOUND SPLIT IN THE POWER LEVERS, RIGGED LT DEADBAND IAW CH 7 AND OPS CK GOOD REF TC1900-RUN WORKSHEET.
- [SDR GLBA20110822J](https://openairdocs.org/sdr/GLBA20110822J.md): Pump · leaking · Aug 19, 2011 · N202UX · Beech 1900D · Engine Fuel Pump
  > PILOT REPORTED THAT THERE IS A FUEL LEAK FROM THE HIGH PRESSURE FUEL PUMP DRAIN ON THE LEFT ENGINE. MX REPLACED THE LEFT HIGH PRESSURE FUEL PUMP IAW 73-10-02 AND THE FCU IAW TC. 1900-7320.00, OK FOR SERVICE.
- [SDR GLBA20110725F](https://openairdocs.org/sdr/GLBA20110725F.md): Solenoid · dirty · Jul 24, 2011 · N202UX · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT THE RT ENGINE WENT INTO AUTOFEATHER DURING FLARE. MAINTENANCE CLEANED THE LOW PITCH STOP SOLENOID, PERFORMED AUTOFEATHER OPS CHECKED IAW 61-21-00, SYS OPS CHECKED GOOD.
- [SDR GLBA20110713G](https://openairdocs.org/sdr/GLBA20110713G.md): Skin · cracked · Jul 13, 2011 · N202UX · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE LT BELLY SKIN AT FS 288 & WING SPAR JUNCTION CRACKED, 1.1" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-048 MATERIALS
- [SDR GLBA20110713F](https://openairdocs.org/sdr/GLBA20110713F.md): Skin · loose · Jul 13, 2011 · N202UX · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE RT BELLY SKIN AT FS 288 & WING SPAR JUNCTION HAS A PATCH WITH LOOSE FASTENERS. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-049
- [SDR GLBA20110712K](https://openairdocs.org/sdr/GLBA20110712K.md): Frame · cracked · Jul 12, 2011 · N202UX · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE RH HEAVY ANGLE CRACKED IN THE BEND RADIUS AT FS 288, FWD LEADING EDGE OF ANGLE, 2" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO
- [SDR GLBA20110712J](https://openairdocs.org/sdr/GLBA20110712J.md): Frame · cracked · Jul 12, 2011 · N202UX · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE LH HEAVY ANGLE CRACKED IN THE BEND RADIUS AT FS 288, FWD EDGE OF ANGLE, 1.75" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900
- [SDR GLBA20110712G](https://openairdocs.org/sdr/GLBA20110712G.md): Frame · cracked · Jul 12, 2011 · N202UX · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE FUSELAGE FRAME AT FS 456 & STRINGER 10R IS CRACKED AT THE LOWER RADIUS OF THE CUTOUT,.2" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I
- [SDR GLBA20110712H](https://openairdocs.org/sdr/GLBA20110712H.md): Skin · corroded · Jul 12, 2011 · N202UX · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE FUSELAGE BELLY SKIN AT FS 213.25 AND STRINGER 15R CORRODED IN AN AREA OF 1" BY.75". MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-
- [SDR GLBA20110706N](https://openairdocs.org/sdr/GLBA20110706N.md): Ground Wire · broken · Jul 4, 2011 · N202UX · Beech 1900D · Extinguishing System
  > PILOT REPORTED THAT THE LT FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATED IN FLT. MX FOUND BROKEN GROUND WIRE MAKING INTERMITTENT CONNECTION. R & R JACK KNIFE SPLICE IAW AIM 14.3.0 OPS CHECKED SYS.
- [SDR GLBA20110112F](https://openairdocs.org/sdr/GLBA20110112F.md): Skin · damaged · Jan 12, 2011 · N202UX · Beech 1900D · Passenger/Crew Doors
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND THE AIRSTAIR DOOR DAMAGED FROM FS 150.1 TO 177.35, 2" WIDE & 22" LONG ON THE BOTTOM OF THE DOOR INSIDE AT HINGE. OPEN

Next page: https://openairdocs.org/aircraft/N202UX/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 = 'N202UX' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N202UX/reports

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