# Service difficulty reports: N100UX

A list on [N100UX](https://openairdocs.org/aircraft/N100UX.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 · 94 reports

- [SDR GLBA2017110900691](https://openairdocs.org/sdr/GLBA2017110900691.md): Hose · leaking · Nov 6, 2017 · N100UX · Beech 1900D · Fuel Storage
  > PILOTS REPORTED THAT THERE WAS A FUEL LEAK FROM LEFT WHEEL WELL ONTO THE LEFT OUTBOARD MAIN TIRE, A DROP EVERY 5 SECONDS. R & R THE HOSE WITH SERVICEABLE ONE IAW 28-20-00, LEAK CHECKED GOOD.
- [SDR GLBA2017100300685](https://openairdocs.org/sdr/GLBA2017100300685.md): Cable · torn · Oct 2, 2017 · N100UX · Beech 1900D · Passenger/Crew Doors
  > MAINTENANCE REPORTED THAT THE UPPER AFT AIRSTAIR DOOR CABLE WAS TORN. REMOVED AND REPLACED THE UPPER AFT AIRSTAIR DOOR CABLE IAW 52-10-02. P/N OFF/ON: 1440-40GLA, NSN.
- [SDR GLBA2016011900564](https://openairdocs.org/sdr/GLBA2016011900564.md): Cable · broken · Jan 16, 2016 · N100UX · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE FWD DOOR SNUBBER WAS INOPERATIVE. MX FOUND THE COUNTER BALANCE CABLE BROKEN, DISCONNECTED & REMOVED BOTH ENDS. INSTALLED NEW CABLE ASSEMBLY. OPS CHECKED GOOD.
- [SDR GLBA2014071400420](https://openairdocs.org/sdr/GLBA2014071400420.md): Tire · failed · Jul 13, 2014 · N100UX · Beech 1900D · Tire
  > PILOT STATED THAT THE TOWER CALLED & SAID THEY SAW DEBRIS AFTER TAKEOFF. GROUND OPS CONFIRMED PIECES OF A TIRE ON THE RUNWAY. DECLARED AN EMERGENCY & RETURNED TO THE FIELD, RT INBD TIRE HAD SEPARATED. MAINTENANCE REPLACED BOTH RT TIRES.
- [SDR GLBA2014031000400](https://openairdocs.org/sdr/GLBA2014031000400.md): Skin · cracked · Mar 9, 2014 · N100UX · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE SKIN AT THE RT FWD SPAR CAP AREA, FS 288.0, 1.5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-021.
- [SDR GLBA2014022800397](https://openairdocs.org/sdr/GLBA2014022800397.md): Frame · corroded · Feb 28, 2014 · N100UX · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION MX FOUND CORROSION AT FS 288.000 ON THE FRAME WHERE THE STRINGERS 16, 15R, 15L, 14R, & 14L ATTACHED, AREA OF 3 INCHES WIDE BY 2 INCHES. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-014.
- [SDR GLBA2014022800396](https://openairdocs.org/sdr/GLBA2014022800396.md): Stringer · corroded · Feb 28, 2014 · N100UX · Beech 1900D · Fuselage Main, Longeron/Stringer
  > DURING A SCHEDULED INSPECTION MX FOUND CORROSION AT FS 258.250 TO FS 288.000 ON STRINGER 14L AT FAYING SURFACE. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-013.
- [SDR GLBA2014022800395](https://openairdocs.org/sdr/GLBA2014022800395.md): Stringer · corroded · Feb 28, 2014 · N100UX · Beech 1900D · Fuselage Main, Longeron/Stringer
  > DURING A SCHEDULED INSPECTION MX FOUND CORROSION AT FS 258.250 TO FS 288.000 ON STRINGER 15L AT FAYING SURFACE. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-015.
- [SDR GLBA2014022800394](https://openairdocs.org/sdr/GLBA2014022800394.md): Stringer · corroded · Feb 28, 2014 · N100UX · Beech 1900D · Fuselage Main, Longeron/Stringer
  > DURING A SCHEDULED INSPECTION MX CORROSION AT FS 258.250 TO FS 288.000 AT STRINGER 16 ON FAYING SURFACE. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-016.
- [SDR GLBA2014022800393](https://openairdocs.org/sdr/GLBA2014022800393.md): Stringer · corroded · Feb 28, 2014 · N100UX · Beech 1900D · Fuselage Main, Longeron/Stringer
  > DURING A SCHEDULED INSPECTION MX FOUND CORROSION AT FS 258.250 TO FS 288.000 ON STRINGER 15R AT FAYING SURFACE. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-017.
- [SDR GLBA2014022800392](https://openairdocs.org/sdr/GLBA2014022800392.md): Stringer · corroded · Feb 28, 2014 · N100UX · Beech 1900D · Fuselage Main, Longeron/Stringer
  > DURING A SCHEDULED INSPECTION MX FOUND CORROSION AT FS 258.250 TO 288.000, STRINGER 14R AT FAYING SURFACE. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-018.
- [SDR GLBA2014022800390](https://openairdocs.org/sdr/GLBA2014022800390.md): Skin · torn · Feb 28, 2014 · N100UX · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION MX FOUND THE SKIN TORN ON THE BELLY AT FS 265.750 & STRINGER 14L, APPROXIMATELY 5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-020.
- [SDR GLBA2014021700385](https://openairdocs.org/sdr/GLBA2014021700385.md): Frame · cracked · Feb 17, 2014 · N100UX · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE FUSELAGE FRAME AT FS 183.250, BETWEEN STRINGERS 2R & 3R WHERE THE DUCT PASSES THROUGH THE FRAME,.5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 14-1900
- [SDR GLBA2014021300382](https://openairdocs.org/sdr/GLBA2014021300382.md): Frame · cracked · Feb 13, 2014 · N100UX · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION MX FOUND 2 CRACKS IN THE RT SIDE OF FS 107 & STRINGER 8R, FRAME ANGLE & LONGERON, FRAME CRACKED AT UPPER END OF FRAME IN BEND RADIUS. LONGERON CRACKED FROM LOWER EDGE TO LONGERON UPWARD THROUGH BEND RADIUS, 1.5 INCHES IN LENGTH.
- [SDR GLBA2014021300381](https://openairdocs.org/sdr/GLBA2014021300381.md): Skin · corroded · Feb 13, 2014 · N100UX · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION MX FOUND BELLY SKIN CORROSION AT FS 270 & STRINGER 16, 1.2 INCHES FWD & AFT DIRECTION BETWEEN STRINGER 16 FASTENERS. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-010.
- [SDR GLBA2014021300380](https://openairdocs.org/sdr/GLBA2014021300380.md): Frame · cracked · Feb 13, 2014 · N100UX · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE LT FUSELAGE AT FS 107 & STRINGER 8L FRAME AT THE UPPER END AT FRAME IN BEND RADIUS,.75 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-009.
- [SDR GLBA2014021200379](https://openairdocs.org/sdr/GLBA2014021200379.md): Rib · cracked · Feb 11, 2014 · N100UX · Beech 1900D · Wing, Rib/Bulkhead
  > DURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE RT WING INBD RIB FLANGE & DOUBLER AT JUNCTION WITH THE WING SPAR, RADIATES FROM THE OTBD EDGE OF THE FLANGE & DOUBLER INWARD TOWARD THE FLANGE BEND RADIUS, 1 INCH IN LENGTH. REPAIRED THE AFFECTED AREA AND
- [SDR GLBA2014021000378](https://openairdocs.org/sdr/GLBA2014021000378.md): Skin · cracked · Feb 10, 2014 · N100UX · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED INSPECTION MX FOUND 2 CRACKS IN THE FUSELAGE SKIN AT FS 150 & STRINGER 1, JUST TO THE RT OF STRINGER 1 LOCATION, CRACK RADIATES INBD & OTBD FROM FASTENER.55 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPEC
- [SDR GLBA2013103000346](https://openairdocs.org/sdr/GLBA2013103000346.md): Door Frame · cracked · Oct 30, 2013 · N100UX · Beech 1900D · Fuselage Main, Structure
  > DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE AFT LOWER CARGO DOOR FRAME AT FS 509.50 AND BETWEEN STRINGERS 10 - 11L, 2.5 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-077.
- [SDR GLBA2013070100267](https://openairdocs.org/sdr/GLBA2013070100267.md): Relay · inoperative · Jun 28, 2013 · N100UX · Beech 1900D · Landing Gear Retraction/Extension System
  > PILOT REPORTED THAT THE LANDING GEAR WOULD NOT EXTEND NORMALLY ON APPROACH, RAN CHECKLIST AND NOT HELP, MANUALLY PUMPED GEAR DOWN, ALL INDICATIONS NORMAL, AFTER LANDING FOUND LANDING GEAR RELAY CB POPPED. MX R & R TIME DELAY PCB, R & R GEAR MOTOR RELAY, R & R
- [SDR GLBA2013062800265](https://openairdocs.org/sdr/GLBA2013062800265.md): Relay · malfunctioned · Jun 27, 2013 · N100UX · Beech 1900D · Landing Gear Retraction/Extension System
  > LANDING GEAR WOULD NOT EXTEND NORMALLY ON APPROACH. RAN CHECKLISTS AND NO HELP, MANUALLY PUMPED GEAR DOWN. ALL INDICATIONS NORMAL. AFTER LANDING, FOUND LANDING GEAR RELAY CIRCUIT BREAKER TRIPPED. R & R LANDING GEAR MOTOR RELAY IAW AIM 12-15.0. R & R LANDIN
- [SDR GLBA2013030600198](https://openairdocs.org/sdr/GLBA2013030600198.md): Diode · failed · Mar 5, 2013 · N100UX · Beech 1900D · DC Power Distribution System
  > PILOT REPORTED THAT THERE WAS ELECTRICAL SMOKE COMING FROM THE FUEL GAUGE PANEL, RT FIRE WALL CIRCUIT BREAKER TRIPPED. MX REPLACED THE CR3 DIODE ON THE FUEL PANEL.
- [SDR GLBA2013021300175](https://openairdocs.org/sdr/GLBA2013021300175.md): Bulb · inoperative · Feb 12, 2013 · N100UX · Beech 1900D · Emergency Lighting
  > PILOT REPORTED THAT THE INSTRUMENTS EMERGENCY LIGHTS ON CAPS SIDE WILL NOT ILLUMINATE. MX REPLACED THE BULB, OPS CHECKED GOOD.
- [SDR GLBA2013011400151](https://openairdocs.org/sdr/GLBA2013011400151.md): Bulb · burned out · Jan 11, 2013 · N100UX · Beech 1900D · Emergency Lighting
  > PILOT REPORTED THAT THE CAPTAIN'S SIDE EMERGENCY LIGHT WILL NOT ILLUMINATE. MX REPLACED THE BULB, OPS CHECKED GOOD.
- [SDR GLBA2012081400032](https://openairdocs.org/sdr/GLBA2012081400032.md): Bulkhead · debonded · Aug 14, 2012 · N100UX · Beech 1900D · Fuselage Main, Bulkhead
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION FOUND THE FWD UPPER PRESSURE BULKHEAD AT FS 34.0 THE 2ND & 3RD BONDED STRAP FROM THE RT OTBD EDGE OF BULKHEAD HAS DEBONDED AREAS AT THE BOTTOM AREA OF STRAPS, THE 2ND STRAP DEBONDED AREA 2.3" X 1.3", 3RD STR
- [SDR GLBA2012081400031](https://openairdocs.org/sdr/GLBA2012081400031.md): Bulkhead · cracked · Aug 13, 2012 · N100UX · Beech 1900D · Fuselage Main, Bulkhead
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND LT UPPER FWD PRESSURE BULKHEAD AT FS 84.0 CRACKED AT FASTENER HOLE ALONG BOTTOM EDGE OF PRESSURE BULKHEAD, 5.75" FROM THE LT OTBD PRESS BULKHEAD EDGE, CRACK RADIATES UPWARD FROM FASTENER HOLE,.1875" IN LENGTH. REP
- [SDR GLBA2012080800029](https://openairdocs.org/sdr/GLBA2012080800029.md): Elevator · damaged · Aug 8, 2012 · N100UX · Beech 1900D · Elevator Tab Control System
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND THE LT ELEVATOR HAS DAMAGE ON THE T/E,.37" BY.15". REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-27-001. MATERIALS UTILIZED ARE INCLUDED IN THE EO.
- [SDR GLBA2012080700028](https://openairdocs.org/sdr/GLBA2012080700028.md): Spar Cap · cracked · Aug 7, 2012 · N100UX · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > DURING A SCHEDULED INSPECTION, FOUND TWO CRACKS IN THE RT SIDE OF THE VERTICAL STAB, RT FWD SPAR CAP ANGLE AT APPROX AREA VSS 84.10, 20 PERCENT. REPAIRED AFFECTED AREA IAW EO 12-1900-55-022. MAJOR REPAIR.
- [SDR GLBA2012080600027](https://openairdocs.org/sdr/GLBA2012080600027.md): Spar Cap · cracked · Aug 6, 2012 · N100UX · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE LT VERTICAL STAB, LT FWD SPAR CAP ANGLE AT APPROX FSS 84.10, 20 PERCENT CHORD VISIBLE, 1.25" IN LENGTH. REPAIRED AFFECTED AREA IAW EO 12-1900-55-021. MAJOR REPAIR.
- [SDR GLBA2012080300025](https://openairdocs.org/sdr/GLBA2012080300025.md): Stringer · corroded · Aug 3, 2012 · N100UX · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND CORROSION BETWEEN STRINGER 16 AT FS 243.25 AND 258.25, IN A 2.25" AREA. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-042. MATERIALS UTILIZED ARE INCLUDED IN THE EO.
- [SDR GLBA2012080300026](https://openairdocs.org/sdr/GLBA2012080300026.md): Rib · cracked · Aug 3, 2012 · N100UX · Beech 1900D · Wing, Rib/Bulkhead
  > DURING A SCHEDULED ROUTINE INSP FOUND A CRACK ON THE LT WING INBD AUX RIB FLANGE & ANGLE AT JUNCTION WITH LT WING FWD WING SPAR AT FS 288, 1.3" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-57-008. MATERIALS
- [SDR GLBA201208030024](https://openairdocs.org/sdr/GLBA201208030024.md): Skin · cracked · Aug 2, 2012 · N100UX · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND THE CENTER BELLY SKIN AT FS 303, 2" IB FROM RT EDGE, SKIN CRACKED, 1.25" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-041. MATERIALS UTILIZED ARE INCLUDED IN TH
- [SDR GLBA201208020023](https://openairdocs.org/sdr/GLBA201208020023.md): Bulkhead · cracked · Aug 2, 2012 · N100UX · Beech 1900D · Fuselage Main, Bulkhead
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND 9 CRACKS IN THE LT LOWER PRESSURE BULKHEAD RADIATING FROM THE DOUBLE ROW OF FASTENERS AT THE INBD EDGE OF THE BULKHEAD, 3" IN LENGTH. REPAIRED AFFECTED AREA IAW EO 12-1900-53-040. MAJOR REPAIR.
- [SDR GLBA201208020022](https://openairdocs.org/sdr/GLBA201208020022.md): Bulkhead · cracked · Aug 2, 2012 · N100UX · Beech 1900D · Fuselage Main, Bulkhead
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND CRACKS IN THE RT LOWER PRESSURE BULKHEAD RADIATING FROM FASTENERS AT THE INBD EDGE OF THE BULKHEAD, 8 CRACKS, 3.1" IN TOTAL LENGTH. REPAIRED AFFECTED AREA IAW EO 12-1900-53-040. MAJOR REPAIR.
- [SDR GLBA2012080100021](https://openairdocs.org/sdr/GLBA2012080100021.md): Skin · corroded · Aug 1, 2012 · N100UX · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND BELLY SKIN CORROSION AT FS 243.25, AT JUNCTION OF FRAME & STRINGER 16, AND AT FS 243.25, AT JUNCTION OF FRAME & STRINGER 15L. REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-039.
- [SDR GLBA2012061801](https://openairdocs.org/sdr/GLBA2012061801.md): Web · cracked · Jun 16, 2012 · N100UX · Beech 1900D · Horizontal Stabilizer Structure
  > DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE HORIZONTAL STAB AFT WEB AT HSS 0.00 IN THE LIGHTNING HOLE AT 2 O'CLOCK POSITION LOOKING FWD,.125" IN LENGTH. REPAIRED AFFECTED AREA IAW EO 12-1900-55-016. MAJOR REPAIR.
- [SDR GLBA2012052201](https://openairdocs.org/sdr/GLBA2012052201.md): Diaphragm · damaged · May 20, 2012 · N100UX · Beech 1900D · Pressure Regulator/Outflow Valve
  > PILOT REPORTED THAT DURING CLIMB OUT AND PASSING THROUGH 21,500" CABIN HIGH ANNC ILLUMINATED, DECLARED EMERGENCY, MASKS DEPLOYED, RETURNED TO DEPARTURE. MX R & R LT OUTFLOW VALUE DUE TO DAMAGE TO THE DIAPHRAM IAW BMM 21-30-01, OPS CHECKED GOOD IAW BMM 21-30-0
- [SDR GLBA20111212G](https://openairdocs.org/sdr/GLBA20111212G.md): Cable · broken · Dec 10, 2011 · N100UX · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE DOOR SNUBBER CABLE IS BROKEN. MX REPLACED THE CABLE IAW MM 52-10-01, OPS CHECKED GOOD.
- [SDR GLBA20110516F](https://openairdocs.org/sdr/GLBA20110516F.md): Check Valve · failed · May 14, 2011 · N100UX · Beech 1900D · Aircraft Fuel Distribution System
  > SIG EVENT - THE PILOT REPORTED THAT 600 LBS OF FUEL DRAINED FROM THE MAIN TANK TO THE AUX TANK (LT). MX REPAIRED BY REPLACING THE LT AUX FUEL LINE CHECK VALVE.
- [SDR GLBA20110307G](https://openairdocs.org/sdr/GLBA20110307G.md): Spar · worn · Mar 7, 2011 · N100UX · Beech 1900D · Wing Spar
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE LH WING REAR SPAR BOTTOM LEADING EDGE CHAFFED AT 2 LOCATIONS BY EXT PWR CABLE, OB CHAFF.4" IN LENGTH.1" DEEP, IB CHAFFR.3" IN LENGTH.05" DEEP. MAINTENANCE REPAIRED THE AFFECTED ARE
- [SDR GLBA20110308G](https://openairdocs.org/sdr/GLBA20110308G.md): Frame · cracked · Mar 4, 2011 · N100UX · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE CARGO DOOR AFT FUSELAGE FRAME CRACKED 1.5" IN LENGTH AT THE GAS STRUT MOUNT UPPER IB NUT PLATE, FS 509 BETWEEN STRINGERS 4L & 5L. REF SDR 20110308F. MAINTENANCE REPAIRED THE AFFECTED A
- [SDR GLBA20110308H](https://openairdocs.org/sdr/GLBA20110308H.md): Frame · cracked · Mar 4, 2011 · N100UX · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE CARGO DOOR FRAME AT THE FWD GAS STRUT MOUNT CRACKED IN TWO PLACES 1.5" IN LENGTH AT FS 456 BETWEEN STRINGERS 3L & 4L. REF SDR 20110308F. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERF
- [SDR GLBA20110304F](https://openairdocs.org/sdr/GLBA20110304F.md): Structure · damaged · Mar 4, 2011 · N100UX · Beech 1900D · Wing Main, Frame Structure
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE RT OB WHEEL WELL KEEL ATTACHING HOLES FOR OB FENDER BRACKET HAS ELONGATED HOLES. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-54
- [SDR GLBA20110304J](https://openairdocs.org/sdr/GLBA20110304J.md): Skin · cracked · Mar 4, 2011 · N100UX · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE UPPER FUSELAGE SKIN AT F.S. 288 AND STRINGER 1 IS CRACKED, CRACK RADIATES FORWARD FROM FASTENER.4" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INS
- [SDR GLBA20110304K](https://openairdocs.org/sdr/GLBA20110304K.md): Skin · cracked · Mar 4, 2011 · N100UX · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE UPPER SKIN CRACKED AROUND (7) FASTENERS AT FS 273 BETWEEN STRINGER 1 AND 2R, CRACKS RANGE FROM.4" TO.2" IN LENGTH. SOME FOUND WITH EDDY CURRENT. MAINTENANCE REPAIRED THE AFFECTED ARE
- [SDR GLBA20110304H](https://openairdocs.org/sdr/GLBA20110304H.md): Frame · cracked · Mar 4, 2011 · N100UX · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE RH FUSELAGE FRAME CRACKED.3" IN LENGTH AT STRINGER 9AR CUTOUT AT F.S. 177. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-014. MAT
- [SDR GLBA20110304G](https://openairdocs.org/sdr/GLBA20110304G.md): Frame · cracked · Mar 4, 2011 · N100UX · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE RH FUSELAGE FRAME CRACKED AT STRINGER CUTOUT F.S. 183 STRINGER 9AR,.4" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-0
- [SDR GLBA20110308F](https://openairdocs.org/sdr/GLBA20110308F.md): Mount · cracked · Mar 4, 2011 · N100UX · Beech 1900D · Cargo/Baggage Doors
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE CARGO DOOR GAS STRUT FWD MOUNT HAS 2 CRACKS APPROX 1.3" IN LENGTH, THE AFT GAS STRUT MOUNT HAS 1 CRACK APPROX.6" IN LENGTH.
- [SDR GLBA20110303H](https://openairdocs.org/sdr/GLBA20110303H.md): Frame · cracked · Mar 3, 2011 · N100UX · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUNTINE INSP MX FOUND THE RT SIDE WALL HEAVY ANGLE AT FS 303, CRACKED IN THE BEND RADIUS, APPROX 1" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-010. MATERIALS UTILIZED ARE INCLUDED IN
- [SDR GLBA20110303G](https://openairdocs.org/sdr/GLBA20110303G.md): Frame · cracked · Mar 3, 2011 · N100UX · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND THE LT HEAVY ANGLE CRACKED AT FS 303 APPROX 1" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-009. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEE

Next page: https://openairdocs.org/aircraft/N100UX/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 = 'N100UX' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N100UX/reports

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