# Service difficulty reports: N16540, cancelled Dec 18, 2012

A list on [N16540, cancelled Dec 18, 2012](https://openairdocs.org/deregistered/N16540-2012-12-18.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 · 86 reports

- [SDR 29GA94032083012](https://openairdocs.org/sdr/29GA94032083012.md): Uplock Switch · out of adjust · Aug 30, 2012 · N16540 · Beech 1900D · Landing Gear Position and Warning
  > FLIGHT:4001 TLH/TPA GEAR UNSAFE LIGHT INTERMITTENTLY ILLUMINATES LIGHT AND HORN ACTIVATED IN CLIMBOUT WITH GEAR UP. ADJUSTED LEFT MAIN LANDING GEAR UPLOCK SWITCH, OPERATIONAL CHECK OK.
- [SDR 29GA94032070712A](https://openairdocs.org/sdr/29GA94032070712A.md): Powerpack · defective · Jul 7, 2012 · N16540 · Beech 1900D · Hydraulic Pump (Electric/Engine), Main
  > FLIGHT: 3979 PNS/PNS AFTER TAKEOFF LANDING GEAR DID NOT RETRACT. REPLACED HYDRAULIC POWER PACK, OPERATIONAL CHECK SATISFACTORY.
- [SDR 29GA201204110001](https://openairdocs.org/sdr/29GA201204110001.md): Switch · dirty · Apr 7, 2012 · N16540 · Beech 1900D · Landing Gear Position and Warning
  > IN FLIGHT, REDUCED POWER TO IDLE NO HORN NO GEAR LIGHTS. PERFORMED INSP OF LANDING GEAR HORN SYS AND INTRANSIT LIGHT SYS CLEANED DEBRIS FROM LANDING GEAR SWITCHES OPS CHECKED GOOD.
- [SDR 29GA94052012612B](https://openairdocs.org/sdr/29GA94052012612B.md): Handle · lack of lube · Jan 26, 2012 · N16540 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE C-2 INSPECTION DISCOVERED RIGHT FORWARD EMERGENCY EXIT OUTER HANDLE DOES NOT SPRING OPEN. LUBRICATED RIGHT FORWARD EMERGENCY EXIT OUTER HANDLE OPERATIONAL CHECK NORMAL.
- [SDR 29GA94052012612A](https://openairdocs.org/sdr/29GA94052012612A.md): Handle · lack of lube · Jan 26, 2012 · N16540 · Beech 1900D · Emergency Exits
  > REPORT: DURING SCHEDULED ROUTINE C-2 INSPECTION DISCOVERED RIGHT AFT EMERGENCY EXIT INNER AND OUTER HANDLE STIFF TO OPERATE. LUBRICATED RIGHT AFT EMERGENCY EXIT INNER AND OUTER HANDLE OPERATIONAL CHECK NORMAL.
- [SDR 29GA94032121611A](https://openairdocs.org/sdr/29GA94032121611A.md): Pressure Switch · defective · Dec 16, 2011 · N16540 · Beech 1900D · Landing Gear Position and Warning
  > FLIGHT: 4017 FLL/GGT PILOT REPORTED LANDING GEAR "3 GREEN" ILLUMINATED WITH GEAR HANDLE IN "UP" POSITION AIRSPEED EXCEEDED 200 KTS. REPLACED LANDING GEAR POWERPACK GEAR UP PRESSURE SWITCH. LANDING GEAR OPERATIONAL CHECK SATISFACTORY.
- [SDR 29GA94071081911A](https://openairdocs.org/sdr/29GA94071081911A.md): Truss · damaged · Aug 19, 2011 · N16540 · Beech 1900D · Engine Mount Section
  > REPORT: DURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS TUBES DAMAGED. PERFORMED ENGINE TRUSS REPAIR IN ACCORDANCE WITH FAA APPROVED DATA CONTAINED IN DRAWING 1005272-4,8110-3, DERT-510208-CE.
- [SDR 29GA94071081911](https://openairdocs.org/sdr/29GA94071081911.md): Truss · damaged · Aug 19, 2011 · N16540 · Beech 1900D · Engine Mount Section
  > REPORT: DURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS TUBES DAMAGED. PERFORMED ENGINE TRUSS REPAIR IN ACCORDANCE WITH FAA APPROVED DATA CONTAINED IN DRAWING 1005272-4,8110-3, DERT-510208-CE.
- [SDR 29GA94061072811A](https://openairdocs.org/sdr/29GA94061072811A.md): Switch · out of adjust · Jul 28, 2011 · N16540 · Beech 1900D · Propeller Feathering/Reversing
  > FLIGHT 9185 FPO/FLL PILOT REPORTED AUTOFEATHER CYCLES ON AND OFF ON APPROACH TO LANDING WITH 1000 LBS OF TORQUE ON LEFT AND RIGHT ENGINES. ADJUSTED AUTOFEATHER ARMING SWITCHES OPERATIONAL CHECK GOOD.
- [SDR GUUA94057050211C](https://openairdocs.org/sdr/GUUA94057050211C.md): Stringer · corroded · May 2, 2011 · N16540 · Beech 1900D · Wing, Longeron/Stringer
  > DURING SCHEDULED X-RAY INSP DISCOVERED RT WING FWD LOWER BONDED J STRINGER HAS CORROSION BETWEEN WS 114.25 AND 124.25. REMOVED CORROSION AND INSTALLED REPAIR STRAP.
- [SDR GUUA94057050211D](https://openairdocs.org/sdr/GUUA94057050211D.md): Spar · corroded · May 2, 2011 · N16540 · Beech 1900D · Wing Spar
  > DURING SCHEDULED X-RAY INSPECTION DISCOVERED RIGHT WING LOWER MAIN SPAR AREA OF CORROSION BETWEEN WS 124.25 TO WS 135.86. BLENDED OUT CORROSION AND INSTALLED REPAIR STRAP.
- [SDR GUUA94057050211B](https://openairdocs.org/sdr/GUUA94057050211B.md): Skin · corroded · May 2, 2011 · N16540 · Beech 1900D · Wing, Plate/Skin
  > DURING SCHEDULED X-RAY INSPECTION DISCOVERED LEFT WING FORWARD OF MAIN SPAR AREA OF CORROSION AT WS 124.25. REMOVED CORROSION FABRICATED AND INSTALLED EXTERNAL STRAP REPAIR.
- [SDR GUUA94057050211A](https://openairdocs.org/sdr/GUUA94057050211A.md): Stringer · corroded · May 2, 2011 · N16540 · Beech 1900D · Wing, Longeron/Stringer
  > DURING SCHEDULED X-RAY INSPECTION DISCOVERED LEFT WING LOWER BONDED SKIN FORWARD J STRINGER CORRODED TWO SPOTS BETWEEN WS 114.25 AND 124.25. REMOVED CORROSION FABRICATED AND INSTALLED INTERNAL STRAP REPAIR.
- [SDR GUUA94053041711B](https://openairdocs.org/sdr/GUUA94053041711B.md): Door Frame · cracked · Apr 17, 2011 · N16540 · Beech 1900D · Fuselage Main, Structure
  > DURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED AIRSTAIR DOOR FRAME CRACKED AT UPPER AND LOWER COUNTER BALANCE MOUNTS APPROXIMATELY FS 150.6 AND WL 105. REMOVED DAMAGED SECTION OF ANGLE AND INSTALLED NEW SECTION.
- [SDR GUUA94053041711A](https://openairdocs.org/sdr/GUUA94053041711A.md): Skin · corroded · Apr 17, 2011 · N16540 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING SCHEDULED ROUTINE STRUCTURAL INSP CORROSION FOUND BETWEEN FS 378.25 AND FS 393.25 BETWEEN STRINGERS 9AL AND 10L. REMOVED DAMAGED SKIN AND INSTALLED EXTERNAL REPAIR DOUBLER.
- [SDR GUUA94053032211A](https://openairdocs.org/sdr/GUUA94053032211A.md): Skin · corroded · Mar 22, 2011 · N16540 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED FUSELAGE BELLY SKIN EXFOLIATED IN ONE SPOT AT FS 349.00 JUST AFT OF VCS SERVICE DOOR. REMOVED DAMAGE SKIN AND STRINGER AND INSTALLED STRINGER REPAIR AND AN EXTERNAL DOUBLER REPAIR.
- [SDR GUUA94071121710A](https://openairdocs.org/sdr/GUUA94071121710A.md): Bracket · cracked · Dec 17, 2010 · N16540 · Beech 1900D · Engine Mount Section
  > DURING MAGNETIC PARTICLE INSP, DISCOVERED ENGINE TRUSS COWL BRACKET WELD AREAS CRACKED. PERFORMED WELD REPAIR TO ENGINE TRUSS COWL BRACKET WELD AREA CRACKS. FOUND DURING MAGNETIC PARTICLE INSP.
- [SDR GUUA94032062410A](https://openairdocs.org/sdr/GUUA94032062410A.md): Brake · faulted · Jun 24, 2010 · N16540 · Beech 1900D · Landing Gear Brake System
  > PILOT REPORTED AT TIMES WHEN APPLYING RT BRAKES PEDAL GOES ALL THE WAY TO THE FLOOR WITH NO BRAKE PRESSURE HAVE TO PUMP THE BRAKE TO GET PRESSURE. BLED BRAKES AND REMOVED TRAPPED AIR IN RT BRAKE SYS.
- [SDR GUUA94057053110A](https://openairdocs.org/sdr/GUUA94057053110A.md): Spar · damaged · May 31, 2010 · N16540 · Beech 1900D · Wing Spar
  > SPAR DAMAGED, ACFT REQUIRES D+ INSP ACFT COMPANY KIT 118-4014-0003. COMPLIED WITH D+ INSP COMPANY KIT 118-4014-0003.
- [SDR GUUA94032043010A](https://openairdocs.org/sdr/GUUA94032043010A.md): Brake Assy · weak · Apr 30, 2010 · N16540 · Beech 1900D · Landing Gear Brake System
  > PILOT REPORTED BRAKES ON LT SIDE OF ACFT SPONGY AND WEAK. REPLACED NR (1) BRAKE ASSY.
- [SDR GUUA94032042910A](https://openairdocs.org/sdr/GUUA94032042910A.md): Brake · weak · Apr 29, 2010 · N16540 · Beech 1900D · Landing Gear Brake System
  > PILOT REPORTED BRAKES FEEL WEAK. INSPECTED BRAKE SYS FOUND NO LEAKS. BLED BRAKE SYS TAXIED ACFT AND FOUND BRAKE SYS OPS CHECK GOOD NO DEFECTS NOTED.
- [SDR GUUA94032042610A](https://openairdocs.org/sdr/GUUA94032042610A.md): Brake Sys · contaminated · Apr 26, 2010 · N16540 · Beech 1900D · Landing Gear Brake System
  > FLIGHT: 9168 MIA/TPA PILOT REPORTED BRAKES FEEL WEAK. BLED ALL FOUR BRAKES, OPERATIONAL CHECK NORMAL.
- [SDR GUUA94027031410A](https://openairdocs.org/sdr/GUUA94027031410A.md): Torque Tube · corroded · Mar 14, 2010 · N16540 · Beech 1900D · Elevator Structure
  > DURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT ELEVATOR TORQUE TUBE EXFOLIATED. REPLACED LEFT ELEVATOR TORQUE TUBE.
- [SDR GUUA94052022210A](https://openairdocs.org/sdr/GUUA94052022210A.md): Door · stuck · Feb 22, 2010 · N16540 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE MX DISCOVERED RT FWD EMERGENCY EXIT HARD TO OPEN. REPOSITIONED RT FWD EMERGENCY EXIT INTERIOR PANEL.
- [SDR GUUA94053102309A](https://openairdocs.org/sdr/GUUA94053102309A.md): Spar · damaged · Oct 23, 2009 · N16540 · Beech 1900D · Fuselage Main, Frame
  > REPORT: DURING BELLY SKIN REPAIR DISCOVERED RIGHT MAIN SPAR HAS TWO ELONGATED FASTENER HOLES AT FS 288.00. COLD WORK FASTENER HOLES AND INSTALLED BLIND FASTENERS
- [SDR GUUA94057102309A](https://openairdocs.org/sdr/GUUA94057102309A.md): Spar · damaged · Oct 23, 2009 · N16540 · Beech 1900D · Wing, Plate/Skin
  > DURING BELLY SKIN REPAIR, DISCOVERED RT MAIN SPAR LWR FLANGE HAS 2 ELONGATED FASTENER HOLES AT FS288.00. COLD WORK FASTENER HOLES AND INSTALLED BLIND FASTENERS. PREVIOUSLY SUBMITTED OPEN UNDER CONTROL NR GUUA94053102309A UPDATED TO GUUA94057102309A
- [SDR GUUA94053102109A](https://openairdocs.org/sdr/GUUA94053102109A.md): Skin · corroded · Oct 21, 2009 · N16540 · Beech 1900D · Fuselage Main, Plate/Skin
  > DISCOVERED CTR BELLY SKIN CORROSION AT FS 327.63 BETWEEN STR 16 TO 15R OUT OF LIMITS REQUIRES REPAIR. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED AN EXTERNAL DOUBLER REPAIR.
- [SDR GUUA94053101309A](https://openairdocs.org/sdr/GUUA94053101309A.md): Skin · corroded · Oct 13, 2009 · N16540 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING SCHEDULED ROUTINE INSP RT BELLY SKIN HAS SKIN DEBONDING AT FS 288.00. REMOVED SURFACE CORROSION FROM SKIN REQUIRES REPAIR. REMOVED DAMAGED SKIN AND INSTALLED SKIN FILLER AND EXTERNAL DOUBLER REPAIR.
- [SDR GUUA94052101109A](https://openairdocs.org/sdr/GUUA94052101109A.md): Control Cable · frayed · Oct 11, 2009 · N16540 · Beech 1900D · Entrance Stairs
  > DURING SCHEDULED ROUTINE MX, DISCOVERED AIRSTAIR DOOR FWD UPPER CONTROL CABLE FRAYED. REPLACED AIRSTAIR DOOR FWD UPPER CONTROL CABLE. ACFT DOWN FOR STRUCTURAL INSP.
- [SDR GUUA94053100609A](https://openairdocs.org/sdr/GUUA94053100609A.md): Skin · corroded · Oct 6, 2009 · N16540 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT FUSELAGE HAS CORROSION BETWEEN STRINGERS 9L TO 10L AT F.S 408.25. REMOVED DAMAGED SKIN INSTALLED FILLERS AND SHIMS, FABRICATED AND INSTALLED AN EXTERNAL DOUBLER REPAIR.
- [SDR GUUA94053100509A](https://openairdocs.org/sdr/GUUA94053100509A.md): Skin · corroded · Oct 5, 2009 · N16540 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING SCHEDULED ROUTINE INSPECTION DISCOVERED SKIN BULGING AND SEVERAL RIVETS PULLED THROUGH SKIN AT LEFT EMERGENCY EXIT AFT CUT OUT FRAME. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED AN INTERNAL WEB REINFORCEMENT AND AN EXTERNAL DOUBLER REPAIR.
- [SDR GUUA94057093009D](https://openairdocs.org/sdr/GUUA94057093009D.md): Structure · corroded · Sep 30, 2009 · N16540 · Beech 1900D · Wing Main, Frame Structure
  > DURING SCHEDULED LEFT WING X-RAY INSPECTION DISCOVERED SMALL AREA OF CORROSION AREA 1 FWD BONDED STRINGER. CLEANED SURFACE CORROSION AT AREA 1 FOUND TO BE WITHIN ALLOWABLE LIMITS.
- [SDR GUUA94057093009C](https://openairdocs.org/sdr/GUUA94057093009C.md): Spar · corroded · Sep 30, 2009 · N16540 · Beech 1900D · Wing Spar
  > DURING SCHEDULED LEFT WING X-RAY INSPECTION DISCOVERED SMALL CORROSION SPOTS AREA 1 WING SPAR. BLENDED OUT CORROSION AND INSTALLED REPAIR STRAP.
- [SDR GUUA94057093009B](https://openairdocs.org/sdr/GUUA94057093009B.md): Stringer · corroded · Sep 30, 2009 · N16540 · Beech 1900D · Wing, Longeron/Stringer
  > DURING SCHEDULED RIGHT WING X-RAY INSPECTION DISCOVERED SMALL AREA OF CORROSION AREA 1 FWD BONDED STRINGER. REMOVED CORROSION FROM RIGHT WING AREA 1 FORWARD BONDED STRINGER FOUND TO BE WITHIN ALLOWABLE LIMITS.
- [SDR GUUA94057093009A](https://openairdocs.org/sdr/GUUA94057093009A.md): Spar · corroded · Sep 30, 2009 · N16540 · Beech 1900D · Wing Spar
  > DURING SCHEDULED RIGHT WING X-RAY INSPECTION DISCOVERED SMALL CORROSION SPOTS AREA 1 WING SPAR. BLENDED OUT CORROSION AND INSTALLED REPAIR STRAP.
- [SDR GUUA94057092409A](https://openairdocs.org/sdr/GUUA94057092409A.md): Skin · corroded · Sep 24, 2009 · N16540 · Beech 1900D · Wing, Plate/Skin
  > DURING SCHEDULED ROUTINE INSP DISCOVERED RT WING UPPER SKIN T/E CORROSION AND DEBOND BETWEEN WING STATIONS 123.988 THROUGH 196.06. REMOVED DAMAGED SKIN AND INSTALLED AN EXTERNAL REPAIR DOUBLER.
- [SDR GUUA94057060209A](https://openairdocs.org/sdr/GUUA94057060209A.md): Skin · corroded · Jun 2, 2009 · N16540 · Beech 1900D · Wing, Plate/Skin
  > DURING SCHEDULED ROUTINE INSP DISCOVERED RT WING UPPER SKIN AREA EXFOLIATED AT RWS 136.86. REMOVED DAMAGED SKIN AND INSTALLED AN EXTERNAL REPAIR DOUBLER.
- [SDR GUUA94052040409A](https://openairdocs.org/sdr/GUUA94052040409A.md): Door · stiff · Apr 4, 2009 · N16540 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE MX, DISCOVERED RT AFT EMERGENCY EXIT DIFFICULT TO OPEN. LUBRICATED RT AFT EMERGENCY EXIT INTERIOR AND EXTERIOR HANDLE.
- [SDR GUUA94057030709A](https://openairdocs.org/sdr/GUUA94057030709A.md): Skin · corroded · Mar 7, 2009 · N16540 · Beech 1900D · Wing Structure
  > DURING FUTHER INSPECTION OF SURFACE CORROSION DISCOVERED SEVERE CORROSION EXTENDS FROM WS 140.00 TO 190.00 APROXIMATELY. CUT OUT DAMAGED AREA AND INSTALLED AN EXTERNAL DOUBLER REPAIR.
- [SDR GUUA94055030609D](https://openairdocs.org/sdr/GUUA94055030609D.md): Spar Cap · corroded · Mar 6, 2009 · N16540 · Beech 1900 · Horizontal Stabilizer, Spar/Rib
  > DURING SCHEDULED ROUTINE INSP, DISCOVERED RT HORIZONTAL STABILIZER UPPER REAR SPAR CAP HAS EXFOLIATION. REPLACED RIGHT HORIZONTAL STABILIZER UPPER REAR SPAR CAP.
- [SDR GUUA94055030609C](https://openairdocs.org/sdr/GUUA94055030609C.md): Hinge Bracket · corroded · Mar 6, 2009 · N16540 · Beech 1900 · Elevator Miscellaneous Structure
  > DURING SCHEDULED ROUTINE INSP DISCOVERED RT ELEVATOR OTBD HINGE BRACKET HAS SURFACE CORROSION. REPLACED RT ELEVATOR OUTBOARD HINGE BRACKET.
- [SDR GUUA94055030609B](https://openairdocs.org/sdr/GUUA94055030609B.md): Hinge Bracket · corroded · Mar 6, 2009 · N16540 · Beech 1900 · Elevator Miscellaneous Structure
  > DURING SCHEDULED ROUTINE INSP DISCOVERED RT ELEVATOR CTR HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR CENTER HINGE BRACKET.
- [SDR GUUA94055030609A](https://openairdocs.org/sdr/GUUA94055030609A.md): Hinge Bracket · corroded · Mar 6, 2009 · N16540 · Beech 1900D · Elevator Miscellaneous Structure
  > DURING SCHEDULED ROUTINE INSP, DISCOVERED LT ELEVATOR OTBD HINGE BRACKET HAS SURFACE CORROSION. REPLACED LT ELEVATOR OUTBOARD HINGE BRACKET.
- [SDR GUUA10200801](https://openairdocs.org/sdr/GUUA10200801.md): Mechanism · dirty · Oct 20, 2008 · N16540 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED EMERGENCY EXIT DOOR 6A WILL NOT OPEN. CLEANED AND LUBRICATED EMERGENCY EXIT DOOR 6A LATCH MECHANISM. OPERATIONAL CHECK NORMAL.
- [SDR GUU2008F00030](https://openairdocs.org/sdr/GUU2008F00030.md): Snubber · unknown · Aug 9, 2008 · N16540 · Beech 1900D · Passenger/Crew Doors
  > FLIGHT 9237 GHB/FLL, PILOT REPORTED FORWARD DOOR HARD TO PULL. SERVICED AIRSTAIR DOOR SNUBBER. (S)
- [SDR GUU2008F00001](https://openairdocs.org/sdr/GUU2008F00001.md): Hydraulic System · low · Jul 4, 2008 · N16540 · Beech 1900D · Hydraulic System, Main
  > DURING APPROACH AFTER SELECTING THE LANDING GEAR DOWN THE "J" LOCK ENGAGED AND THE CIRCUIT BREAKER TRIPPED IMMEDIATELY. FOUND HYDRAULIC SYSTEM LOW SERVICED HYDRAULIC SYSTEM. OPERATIONAL CHECK NORMAL. (K)
- [SDR GUU2008F00014](https://openairdocs.org/sdr/GUU2008F00014.md): Landing Gear · malfunctioned · Jun 23, 2008 · N16540 · Beech 1900D · Landing Gear Retraction/Extension System
  > FLIGHT 9216, AFTER TAKEOFF, LANDING GEAR CIRCUIT BREAKER POPPER WHEN GEAR SELECTED UP. INSPECTED MLG PERFORMED OPERATIONAL CHECK. COULD NOT DUPLICATE. (A)
- [SDR GUUA94053042208A](https://openairdocs.org/sdr/GUUA94053042208A.md): Skin · corroded · Apr 22, 2008 · N16540 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING SCHEDULED ROUTINE MX DISCOVERED EXFOLIATION AT THE LWR FUSELAGE SKIN AT FS 438.250. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED AN EXTERNAL DOUBLER REPAIR.
- [SDR GUUA01230801](https://openairdocs.org/sdr/GUUA01230801.md): Circuit Breaker · popped · Jan 23, 2008 · N16540 · Beech 1900D · Landing Gear Retraction/Extension System
  > FLIGHT: 9167, DURING APPROACH WHEN SELECTING THE LANDING GEAR DOWN THE LANDING GEAR CB FOR THE MOTOR POPPED. INSPECTED THE LANDING GEAR SYS, PERFORMED LANDING GEAR EXTENSION AND RETRACTION, OPS CHECK NORMAL.
- [SDR GUUA10110702](https://openairdocs.org/sdr/GUUA10110702.md): Hinge · corroded · Oct 11, 2007 · N16540 · Beech 1900D · Rudder Structure
  > DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LOWER RUDDER HINGE ASSEMBLY EXFOLIATED. REPLACED LOWER RUDDER HINGE ASSEMBLY.

Next page: https://openairdocs.org/deregistered/N16540-2012-12-18/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 = 'N16540' AND deregistration_id = 'N16540-2012-12-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N16540-2012-12-18/reports

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