# Service difficulty reports: N17541, cancelled Oct 24, 2012

A list on [N17541, cancelled Oct 24, 2012](https://openairdocs.org/deregistered/N17541-2012-10-24.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 · 73 reports

- [SDR 29GA94153071412](https://openairdocs.org/sdr/29GA94153071412.md): Skin · corroded · Jul 14, 2012 · N17541 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED SEVERE CORROSION AT FS 363.25 STRINGER 16. REMOVED DAMAGED SKIN AREA AND STRINGER 16 DAMAGE AND INSTALLED FUSELAGE SKIN DOUBLER REPAIR AND STRINGER 16 REPAIR ANGLE.
- [SDR 29GA94153062912](https://openairdocs.org/sdr/29GA94153062912.md): Skin · wrinkled · Jun 29, 2012 · N17541 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED BELLY SKIN WRINKLE AT BEACON LOCATION.
- [SDR 29GA94132012112A](https://openairdocs.org/sdr/29GA94132012112A.md): Powerpack · low · Jan 21, 2012 · N17541 · Beech 1900D · Hydraulic Pump (Electric/Engine), Main
  > FLIGHT: 4068 FKL/DUJ AFTER LANDING GEAR HANDLE IS MOVED UP GEAR IN TRANSIT LIGHT AND MOTOR DO NOT ACTUATE FOR 2.4 SECONDS AFTER THIS TIME GEAR RETRACTS AND EXTENDS AS NORMAL. COMPLIED WITH VISUAL INSPECTION OF LANDING GEAR, SERVICED LEVEL OF POWER PACK CYCLED
- [SDR 29GA94132011912A](https://openairdocs.org/sdr/29GA94132011912A.md): Unknown · low · Jan 19, 2012 · N17541 · Beech 1900D · Landing Gear System
  > FLIGHT: 4070 CLE/CLE AFTER DEPARTING AND PUTTING THE GEAR HANDLE UP NOTHING HAPPENED AFTER 1500 FEET LOOKED AT GEAR AND SAW GEAR RELAY CIRCUIT BREAKER WAS POPPED. COMPLIED WITH LANDING GEAR FILLING AND BLEEDING PROCEDURES OPERATIONAL CHECKS GOOD.
- [SDR 29GA2012010494153](https://openairdocs.org/sdr/29GA2012010494153.md): Skin · corroded · Jan 4, 2012 · N17541 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING SCHEDULED STRUCTURAL INSPECTION DISCOVERED AREA OF CORROSION THROUGH OUTER SKIN AT APPROXIMATELY FS 327.630 STRINGER 16-15R APPROXIMATELY. REMOVED DAMAGED SECTION OF SKIN AND INSTALLED INSERTION PATCH AND AN EXTERNAL DOUBLER REPAIR.
- [SDR 29GA94153010412A](https://openairdocs.org/sdr/29GA94153010412A.md): Skin · corroded · Jan 4, 2012 · N17541 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING SCHEDULED STRUCTURAL INSPECTION DISCOVERED AREA OF CORROSION THROUGH OUTER SKIN AT APPROXIMATELY FS 327.630 STRINGER 12L APPROXIMATELY. REMOVED DAMAGED SECTION OF SKIN AND INSTALLED INSERTION PATCH AND AN EXTERNAL DOUBLER REPAIR.
- [SDR 29GA94152122811A](https://openairdocs.org/sdr/29GA94152122811A.md): Handle · lack of lube · Dec 28, 2011 · N17541 · Beech 1900D · Emergency Exits
  > REPORT: DURING SCHEDULED ROUTINE C-2 INSPECTION DISCOVERED RIGHT FORWARD EMERGENCY EXIT DOOR OUTSIDE HANDLE STIFF (HARD TO OPEN. LUBRICATED RIGHT FORWARD EMERGENCY EXIT DOOR OUTSIDE HANDLE.
- [SDR 29GA94152112811A](https://openairdocs.org/sdr/29GA94152112811A.md): Handle · lack of lube · Nov 28, 2011 · N17541 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE C-1 INSPECTION DISCOVERED LEFT EMERGECNY EXIT OUTER HANDLE WILL NOT SPRING OPEN. LUBRICATED LEFT EMERGENCY EXIT OUTER HANDLE. OUTER HANDLE OPEN AND CLOSED NORMALLY.
- [SDR 29GA94153081511A](https://openairdocs.org/sdr/29GA94153081511A.md): Skin · cracked · Aug 15, 2011 · N17541 · Beech 1900D · Fuselage Main, Plate/Skin
  > REPORT: DURING SCHEDULED ROUTINE INSPECTION DISCOVERED AIRSTAIR DOOR LOWER COUNTER BALANCE BRACKET ATTACH POINT SKIN CRACK. REMOVED DAMAGED AREA AND INSTALLED REPAIR FILLER AND DOUBLER REPAIR.
- [SDR 29GA94153081211A](https://openairdocs.org/sdr/29GA94153081211A.md): Skin · cracked · Aug 12, 2011 · N17541 · Beech 1900D · Fuselage Main, Plate/Skin
  > REPORT: DURING SCHEDULED ROUTINE INSPECTION DISCOVERED AIRSTAIR DOOR LOWER COUNTER BALANCE BRACKET ATTACH POINT SKIN CRACK. REMOVED DAMAGED AREA AND INSTALLED REPAIR FILLER AND DOUBLER REPAIR.
- [SDR 29GA94132071911A](https://openairdocs.org/sdr/29GA94132071911A.md): Relay · shorted · Jul 19, 2011 · N17541 · Beech 1900D · Landing Gear Retraction/Extension System
  > FLIGHT 9257 EYW/FLL PILOT REPORTED LANDING GEAR RELAY POPPED WHEN EXTENDING GEAR. REPLACED LANDING GEAR RELAY OPERATIONAL CHECK OK.
- [SDR GUUA94132052311A](https://openairdocs.org/sdr/GUUA94132052311A.md): Switch · defective · May 23, 2011 · N17541 · Beech 1900D · Landing Gear Position and Warning
  > PILOT REPORTED ON GEAR RETRACTION LANDING GEAR HORN SOUNDED AND STAYED RED UNTIL LANDING GEAR WAS EXTENDED AGAIN. REPLACED LANDING GEAR WARNING HORN SWITCH.
- [SDR GUUA94161022511A](https://openairdocs.org/sdr/GUUA94161022511A.md): Annunciator · no indication · Feb 25, 2011 · N17541 · Beech 1900D · Propeller System
  > PILOT REPORTED WITH N1 AT 95 PERCENT "AFX DISABLE" ANNUNCIATOR WAS ILLUMINATED AND LT AFX WAS NOT ILLUMINATED. RERACKED ANNUNCIATOR FAULT DETECTION PCB AUTOFEATHER TEST OPS CHECK GOOD.
- [SDR GUUA94132022411A](https://openairdocs.org/sdr/GUUA94132022411A.md): Indication Sys · inoperative · Feb 24, 2011 · N17541 · Beech 1900D · Landing Gear Position and Warning
  > FLIGHT: 9131 TPA/TLH PILOT REPORTED DURING APPROACH NO GEAR SAFE INDICATION AND LANDING GEAR INDICATOR CIRCUIT BREAKER POPPED. RETURNED TO TPA LANDED WITHOUT INCIDENT. INSPECTED PC BOARD AND CONNECTORS PERFORMED LANDING GEAR SWING FIVE TIMES. VISUALLY INSPEC
- [SDR GUUA94171123010A](https://openairdocs.org/sdr/GUUA94171123010A.md): Bracket · cracked · Dec 30, 2010 · N17541 · Beech 1900D · Engine Cowling System
  > DURING MAGNETIC PARTICLE INSP, DISCOVERED ENGINE TRUSS COWL BRACKET WELD AREA CRACKED. PERFORMED WELD REPAIR TO ENGINE TRUSS COWL BRACKET WELD AREA.
- [SDR GUUA94152090910A](https://openairdocs.org/sdr/GUUA94152090910A.md): Handle · stiff · Sep 9, 2010 · N17541 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE INSP DISCOVERED LT EMERGENCY EXIT HANDLE STIFF TO OPERATE. LUBRICATED LT EMERGENCY EXIT HANDLE.
- [SDR GUUA94155071910C](https://openairdocs.org/sdr/GUUA94155071910C.md): Hinge Bracket · corroded · Jul 19, 2010 · N17541 · Beech 1900D · Elevator Structure
  > DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT ELEVATOR INBOARD HINGE BRACKET HAS CORROSION. REPLACED RIGHT ELEVATOR INBOARD HINGE BRACKET.
- [SDR GUUA94155071910B](https://openairdocs.org/sdr/GUUA94155071910B.md): Hinge Bracket · corroded · Jul 19, 2010 · N17541 · Beech 1900D · Elevator Structure
  > DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT ELEVATOR CENTER HINGE BRACKET EXFOLIATED. REPLACED RIGHT ELEVATOR CENTER HINGE BRACKET.
- [SDR GUUA94155071910A](https://openairdocs.org/sdr/GUUA94155071910A.md): Hinge Bracket · corroded · Jul 19, 2010 · N17541 · Beech 1900D · Elevator Structure
  > DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT ELEVATOR CENTER HINGE BRACKET EXFOLIATED. REPLACED RIGHT ELEVATOR CENTER HINGE BRACKET.
- [SDR GUUA94132060310A](https://openairdocs.org/sdr/GUUA94132060310A.md): Bulb · inoperative · Jun 3, 2010 · N17541 · Beech 1900D · Landing Gear Position and Warning
  > DURING APPROACH SELECTED LANDING GEAR DOWN HAD GREEN LIGHT INDICATION ON THE MAIN GEAR BUT NOT ON THE NOSEWHEEL. R & R LANDING GEAR INDICATOR BULBS.
- [SDR GUUA94153050410B](https://openairdocs.org/sdr/GUUA94153050410B.md): Shim · corroded · May 4, 2010 · N17541 · Beech 1900D · Fuselage Main, Structure
  > DURING SCHEDULED ROUTINE INSP DISCOVERED CORROSION FS 363 FWD AND AFT OF ANGLE BETWEEN STRINGERS 15L AND STRINGER 16. REMOVED AREA OF CORROSION AND REPLACED SECTION OF DAMAGED SHIM.
- [SDR GUUA94153050410A](https://openairdocs.org/sdr/GUUA94153050410A.md): Stringer · corroded · May 4, 2010 · N17541 · Beech 1900D · Fuselage Main, Structure
  > DURING SCHEDULED ROUTINE INSP DISCOVERED INTERIOR CORROSION APPROX FS 258, STRINGER 14L, FWD OF ANGLE AT SPLICE AREA OF STR 14L. REMOVED DAMAGED SECTION OF STRINGER AND SPLICED IN NEW STRINGER AND INSTALLED EXTERNAL DOUBLER REPAIRS.
- [SDR GUUA94152050410A](https://openairdocs.org/sdr/GUUA94152050410A.md): Handle · binding · May 4, 2010 · N17541 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE INSP DISCOVERED SEAT 6A EMERGENCY EXIT INTERIOR HANDLE IS HARD TO OPERATE. LUBRICATED SEAT 6A EMERGENCY EXIT INTERIOR AND EXTERIOR DOOR HANDLES. OPS CHECKS GOOD.
- [SDR GUUA94153043010](https://openairdocs.org/sdr/GUUA94153043010.md): Angle · cracked · Apr 30, 2010 · N17541 · Beech 1900D · Fuselage Miscellaneous Structure
  > DURING SCHEDULED ROUTINE INSP, DISCOVERED INTERIOR FUSELAGE ANGLE CRACKED AT FS 150 STR, 9AL AT AIRSTAIR DOOR TOP AFT ATTACH POINT OF LOWER BRACKET. REMOVED 2.25 INCHES OF DAMAGED ANGLE AND INSTALLED REPAIR ANGLE.
- [SDR GUUA94153043010A](https://openairdocs.org/sdr/GUUA94153043010A.md): Angle · cracked · Apr 30, 2010 · N17541 · Beech 1900D · Fuselage Miscellaneous Structure
  > DURING SCHEDULED ROUTINE INSP DISCOVERED INTERIOR FUSELAGE ANGLE CRACKED AT FS 150 STRINGER 9AL AT AIRSTAIR DOOR TOP AFT ATTACH POINT OF LOWER BRACKET. (OPEN)
- [SDR GUUA94152021810A](https://openairdocs.org/sdr/GUUA94152021810A.md): Panel · out of limits · Feb 18, 2010 · N17541 · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED CABIN DOOR HARD TO OPEN AFTER LANDING. TRIMMED CABIN DOOR INTERIOR PANEL AROUND PUSH BUTTON OPS CHECK GOOD.
- [SDR GUUA94129012410A](https://openairdocs.org/sdr/GUUA94129012410A.md): Line · leaking · Jan 24, 2010 · N17541 · Beech 1900D · Hydraulic System, Main
  > DURING FLIGHT HYD LOW LIGHT ILLUMINATED UPON LANDING GEAR EXTENSION, FOUND LARGE HYD FLUID PUDDLE UNDER WING. REPLACED HAND PUMP HYD RETURN LINE. LANDING GEAR OPS CHECK GOOD.
- [SDR GUUA94132011710A](https://openairdocs.org/sdr/GUUA94132011710A.md): Actuator · bypassing · Jan 17, 2010 · N17541 · Beech 1900D · Landing Gear Actuator
  > DURING FLIGHT LANDING GEAR MOTOR RECYCLING IN AIR ABOUT EVERY THREE TO FOUR MINUTES. REPLACED LT MLG ACTUATOR, OPS CHECK GOOD.
- [SDR GUUA94155121409B](https://openairdocs.org/sdr/GUUA94155121409B.md): Hinge · corroded · Dec 14, 2009 · N17541 · Beech 1900D · Rudder Structure
  > DURING SCHEDULED ROUTINE INSP, DISCOVERED RUDDER CTR HINGE HAS CORROSION. REPLACED RUDDER CTR HINGE.
- [SDR GUUA94155121409A](https://openairdocs.org/sdr/GUUA94155121409A.md): Hinge · corroded · Dec 14, 2009 · N17541 · Beech 1900D · Rudder Structure
  > DURING SCHEDULED ROUTINE INSP, DISCOVERED VERTICAL STABILIZER UPPER RUDDER HINGE HAS CORROSION. REPLACED VERTICAL STABILIZER UPPER RUDDER HINGE.
- [SDR GUUA94132112909A](https://openairdocs.org/sdr/GUUA94132112909A.md): Pressure Switch · out of adjust · Nov 29, 2009 · N17541 · Beech 1900D · Landing Gear Retraction/Extension System
  > PILOT REPORTED DELAY IN NOSE WHEEL EXTENSION 4 SECONDS AFTER MAINS. REPLACED HYD PRESSURE SWITCH AND ADJUSTED NLG DOWN POSITION SWITCH. LANDING GEAR OPS CHECK NORMAL.
- [SDR GUUA94157111409A](https://openairdocs.org/sdr/GUUA94157111409A.md): Access Panel · delaminated · Nov 14, 2009 · N17541 · Beech 1900D · Wing, Plate/Skin
  > DURING SCHEDULED ROUTINE MX DISCOVERED RT WING FUEL ACCESS PANEL 631DB LEAKING FUEL. INSTALLED EXTERNAL RING DOUBLER ON WING SKIN AT FUEL ACCESS PANEL 631DB, NO LEAKS NOTED.
- [SDR GUUA94157103109B](https://openairdocs.org/sdr/GUUA94157103109B.md): Spar · corroded · Oct 31, 2009 · N17541 · Beech 1900D · Wing Spar
  > DURING SCHEDULED X-RAY INSP OF LT WING COLLECTOR TANK FOUND SEVERAL SPOTS OF CORROSION ON LWR MAIN SPAR. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR STRAP.
- [SDR GUUA94157103109A](https://openairdocs.org/sdr/GUUA94157103109A.md): Stringer · corroded · Oct 31, 2009 · N17541 · Beech 1900D · Wing, Longeron/Stringer
  > DURING SCHEDULED X-RAY INSP DISCOVERED LT WING COLLECTOR TANK LWR SKIN AFT OF MAIN SPAR BONDED STR HAS MINOR SURFACE CORROSION. REMOVED CORROSION AND INSTALLED AN EXTERNAL REPAIR DOUBLER.
- [SDR GUUA94152081909A](https://openairdocs.org/sdr/GUUA94152081909A.md): Door · stuck · Aug 19, 2009 · N17541 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE INSP DISCOVERED RT AFT EMERGENCY EXIT WILL NOT COME OUT OF FRAME. (JAMMED) LUBRICATED RT AFT EMERGENCY EXIT. OPS CHECK GOOD.
- [SDR GUUA94155062209A](https://openairdocs.org/sdr/GUUA94155062209A.md): Hinge Bracket · corroded · Jun 22, 2009 · N17541 · Beech 1900D · Wing, Control Surface Attach Fittings
  > DURING SCHEDULED ROUTINE MX DISCOVERED RT ELEVATOR OTBD HINGE BRACKET EXFOLIATED. C/A: REPLACED RT ELEVATOR OTBD HINGE BRACKET.
- [SDR GUUA941062209A](https://openairdocs.org/sdr/GUUA941062209A.md): Hinge Bracket · corroded · Jun 22, 2009 · N17541 · Beech 1900D · Wing, Control Surface Attach Fittings
  > DURING SCHEDULED ROUTINE INSP, DISCOVERED RT ELEVATOR OTBD HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR OTBD HINGE BRACKET.
- [SDR GUUA94132041609A](https://openairdocs.org/sdr/GUUA94132041609A.md): Squat Switch · failed · Apr 16, 2009 · N17541 · Beech 1900D · Landing Gear Position and Warning
  > DURING TEST FLIGHT LT MAIN LANDING GEAR DID NOT EXTEND. MANUALLY EXTENDED LANDING GEAR. LT MAIN GEAR ILLUMINATED DOWN AND LOCKED. OBTAINED 3 GREEN DOWN AND LOCKED INDICATION. REPLACED LT MLG SQUAT SWITCH ASSY. TEST FLIGHT SATISFACTORY.
- [SDR GUUA94132040609A](https://openairdocs.org/sdr/GUUA94132040609A.md): Wire · chafed · Apr 6, 2009 · N17541 · Beech 1900D · Nacelle/Pylon System Wiring
  > DURING FLIGHT, DISCOVERED LANDING GEAR CIRCUIT BREAKER POPPED. REPAIRED CHAFED WIRE D6D22 ON TOP LT NACELLE.
- [SDR GUUA94132032909A](https://openairdocs.org/sdr/GUUA94132032909A.md): Pcb · failed · Mar 29, 2009 · N17541 · Beech 1900D · Landing Gear Position and Warning
  > PILOT REPORTED NO 3 GREEN GEAR INDICATION LIGHTS. REPLACED PCB A319. LANDING GEAR OPERATIONAL CHECK NORMAL.
- [SDR GUUA94132032908A](https://openairdocs.org/sdr/GUUA94132032908A.md): Pcb · damaged · Mar 29, 2009 · N17541 · Beech 1900D · Landing Gear Position and Warning
  > PILOT REPORTED NO 3 GREEN GEAR INDICATION LIGHTS. REPLACED PCB A319. LANDING GEAR OPS CHECK, NORMAL.
- [SDR GUUA94132032809A](https://openairdocs.org/sdr/GUUA94132032809A.md): Circuit Breaker · tripped · Mar 28, 2009 · N17541 · Beech 1900D · Landing Gear System Wiring
  > DURING APPROACH LANDING GEAR INDICATION CIRCUIT BREAKER POPPED AFTER SELECTING GEAR DOWN. RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. OPS CHECK FOUND TO BE WORKING OK. INSPECTED LANDING GEAR SYSTEMS UNABLE TO FIND ANY PROBLEM OPERATIONAL CHECK OK.
- [SDR GUUA94132022109B](https://openairdocs.org/sdr/GUUA94132022109B.md): Circuit Breaker · unknown · Feb 21, 2009 · N17541 · Beech 1900D · Landing Gear Position and Warning
  > FLIGHT: 9233 DURING FLIGHT LANDING GEAR INDICATOR CIRCUIT BREAKER POPPED UNABLE TO RESET. RETURNED TO FLL. REPLACED LANDING GEAR INDICATOR CIRCUIT BREAKER. LANDING GEAR OPERATIONAL CHECK NORMAL.TEST FLIGHT SATISFACTORY.
- [SDR GUUA94132022109A](https://openairdocs.org/sdr/GUUA94132022109A.md): Wire · broken · Feb 21, 2009 · N17541 · Beech 1900D · Landing Gear System Wiring
  > FLIGHT: 9270 DURING APPROACH LANDING GEAR INDICATOR CIRCUIT BREAKER POPPED AFTER GEAR EXTENSION. FOUND BROKEN BROKEN WIRE ON LEFT LANDING GEAR DOWN LOCK CONNECTOR. SPLICED BROKEN WIRE.LANDING GEAR OPERATIONAL CHECK NORMAL.
- [SDR GUUA94132022009A](https://openairdocs.org/sdr/GUUA94132022009A.md): Circuit Breaker · tripped · Feb 20, 2009 · N17541 · Beech 1900D · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, LANDING GEAR CIRCUIT BREAKER POPPED AFTER GEAR RETRACTED, RESET CIRCUIT BREAKER, STAYED IN THE REST OF THE FLIGHT. PERFORMED OPS CHECK OF LANDING GEAR. OPS CHECK GOOD. COULD NOT DUPLICATE.
- [SDR GUUA94152120908A](https://openairdocs.org/sdr/GUUA94152120908A.md): Door · out of rig · Dec 9, 2008 · N17541 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE MX DISCOVERED RT AFT EMERGENCY EXIT HARD TO OPEN. RERIGGED RT AFT EMERGENCY EXIT. OPS CHECK GOOD.
- [SDR GUUA94157120908A](https://openairdocs.org/sdr/GUUA94157120908A.md): Skin · corroded · Dec 9, 2008 · N17541 · Beech 1900D · Wing, Plate/Skin
  > DURING SCHEDULED ROUTINE MX DISCOVERED RT OTBD WING UPPER SKIN TRAILING EDGE HAD CORROSION AND DEBOND BETWEEN WS 139 THROUGH 158. REMOVED DAMAGED SKIN AND FABRICATED AND INSTALLED AN EXTERNAL REPAIR DOUBLER.
- [SDR GUUA11040801](https://openairdocs.org/sdr/GUUA11040801.md): Wire · broken · Nov 4, 2008 · N17541 · Beech 1900D · Landing Gear System Wiring
  > FLIGHT 5201 MIA/FLL - DURING APPROACH LEFT LANDING GEAR INDICATION LIGHTS DOES NOT SHOW LOCKED. CONTINUED TO FLL. LANDED WITHOUT INCIDENT. REPAIRED BROKEN WIRE AT LEFT MAIN LANDING GEAR CONNECTOR P273. OPERATIONAL CHECK NORMAL.
- [SDR GUUA10260801](https://openairdocs.org/sdr/GUUA10260801.md): Handle · lack of lube · Oct 26, 2008 · N17541 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT EMERGENCY EXIT DIFFICULT TO OPEN. LUBRICATED LEFT EMERGENCY EXIT HANDLE.
- [SDR GUUA05200801](https://openairdocs.org/sdr/GUUA05200801.md): Squat Switch · loose · May 20, 2008 · N17541 · Beech 1900D · Landing Gear Position and Warning
  > FLIGHT: 9140 AFTER TAKEOFF, LANDING GEAR WILL NOT RETRACT. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT RESECURED RT LANDING GEAR SQUAT SWITCH. LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHECK GOOD.

Next page: https://openairdocs.org/deregistered/N17541-2012-10-24/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 = 'N17541' AND deregistration_id = 'N17541-2012-10-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N17541-2012-10-24/reports

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