# Service difficulty reports: N87552, cancelled Dec 4, 2015

A list on [N87552, cancelled Dec 4, 2015](https://openairdocs.org/deregistered/N87552-2015-12-04.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 · 60 reports

- [SDR 29GA95231110811A](https://openairdocs.org/sdr/29GA95231110811A.md): Warning System · false activation · Nov 8, 2011 · N87552 · Beech 1900D · Central Warning
  > FLIGHT: 3998 TLH/FLL PILOT REPORTED BLANK RED ANNUNCIATOR WARNING PANEL ILLUMINATES IN TANDEM WITH LANDING GEAR HANDLE ANNUNCIATOR LIGHT. PERFORMED SEVERAL LANDING GEAR OPERATIONAL CHECKS COULD NOT DUPLICATE.
- [SDR GUUA95227052311A](https://openairdocs.org/sdr/GUUA95227052311A.md): Cable · worn · May 23, 2011 · N87552 · Beech 1900D · Elevator Tab Control System
  > PILOT REPORTED ELEVATOR TRIM VIBRATES TOWARDS A NOSE UP ATTITUDE AFTER BEING TRIMMED TO LEVEL FLIGHT ATTITUDE. REPLACED LT ELEVATOR TRIM DRUM AND CABLE, AND RT ELEVATOR TRIM TAB ELECTRIC TRIM SERVO MOTOR AND ACTUATOR.
- [SDR GUUA95252030211A](https://openairdocs.org/sdr/GUUA95252030211A.md): Skin · cracked · Mar 2, 2011 · N87552 · Beech 1900D · Passenger/Crew Doors
  > DURING SCHEDULED ROUTINE MX DISCOVERED SMALL CRACK ON AIRSTAIR DOOR OUTER SKIN AROUND DOOR HANDLE. DURING FURTHER INSPECTION DISCOVERED CORROSION ON OUTER AIRSTAIR DOOR SKIN REMOVED CORRODED OUTER SKIN AND CRACK AND INSTALLED FILLER AND DOUBLER REPAIR.
- [SDR GUUA95253010311A](https://openairdocs.org/sdr/GUUA95253010311A.md): Skin · chafed · Jan 3, 2011 · N87552 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING SCHEDULED ROUTINE INSP, DISCOVERED SKIN CHAFED AT FUSELAGE STA 258 AND BUTT LINE 29.5 ON THE LT SIDE OF THE ACFT. REPAIRED SKIN CHAFE BY INSTALLING COVER PATCH.
- [SDR GUUA95257010311A](https://openairdocs.org/sdr/GUUA95257010311A.md): Skin · corroded · Jan 3, 2011 · N87552 · Beech 1900D · Wing, Plate/Skin
  > DURING SCHEDULED ROUTINE INSP, DISCOVERED RT WING UPPER SKIN T/E CORROSION AND DEBOND BETWEEN WING STA 138.00 AND 160.25. REMOVED DAMAGED SKIN AND INSTALLED AN EXTERNAL DOUBLER REPAIR.
- [SDR GUUA95253122610A](https://openairdocs.org/sdr/GUUA95253122610A.md): Stringer · cracked · Dec 26, 2010 · N87552 · Beech 1900D · Fuselage Main, Longeron/Stringer
  > DURING SCHEDULED ROUTINE STRUCTURAL INSP DISCOVERED STR 10R CRACKED.25 INCH AT APPROX FS 451. REPAIRED 10R STR CRACK AREA. ACFT DOWN FOR STRUCTURAL INSP.
- [SDR GUUA95232073110A](https://openairdocs.org/sdr/GUUA95232073110A.md): Switch · failed · Jul 31, 2010 · N87552 · Beech 1900D · Landing Gear Position and Warning
  > PILOT REPORTED LANDING GEAR WARNING HORN WILL NOT SILENCE. REPLACED LANDING GEAR HORN SILENCE SWITCH (PN C2006) AND RELAY PCB A113 OPS CHECK NORMAL.
- [SDR GUUA95221072410A](https://openairdocs.org/sdr/GUUA95221072410A.md): Hydraulic System · leaking · Jul 24, 2010 · N87552 · Beech 1900D · Hydraulic System, Main
  > DURING FLIGHT, RTV SEALANT SMELL COMING FROM CAPTAINS OVERHEAD VENT, VARYING INTENSITY THROUGHTOUT THE FLIGHT. FOUND HYD OVERFILL LINE NOT THROUGH WING PANEL ALOWING HYD FLUID BUILD UP IN ACM AREA, CLEANED ACM AREA AND REINSTALLED HYD OVERFILL LINE PROPERLY.
- [SDR GUUA95221071910A](https://openairdocs.org/sdr/GUUA95221071910A.md): Unknown · odor · Jul 19, 2010 · N87552 · Beech 1900D · Air Distribution System
  > FLIGHT 9150 MHH/FLL WHEN AIRCRAFT DEPARTS INTO THE AIR AIRCRAFT WILL PRODUCE A BURNT SMELL COMING FROM EYEBALL AND FLOOR VENTS. OPENED FLOORBOARDS AND INSPECTED FOR CAUSE OF BURNT SMELL, NO CAUSE OF BURNT SMELL FOUND TURNED ON ALL SYSTEMS FOR 30 MINUTES AND N
- [SDR GUUA95221062610A](https://openairdocs.org/sdr/GUUA95221062610A.md): Unknown · odor · Jun 26, 2010 · N87552 · Beech 1900D · Air Distribution System
  > DURING FLIGHT NOTICED PLASTIC TYPE ODOR COMING FROM FLIGHT DECK. INVESTIGATED FLIGHT DECK FOR ODOR. NO ODOR NOTICED, RAN ENGINES FOR 45 MINUTES WITH ALL ELECTRICAL EQUIPMENT ON AND BLEEDS OPEN NO PLASTIC OR UNUSUAL ODOR NOTED.
- [SDR GUUA95234060310A](https://openairdocs.org/sdr/GUUA95234060310A.md): Altimeter · malfunctioned · Jun 3, 2010 · N87552 · Beech 1900D · Altimeter, Barometric/Encoder
  > AFTER LIFTOFF CAPTAINS ALTIMETER DIDN'T INDICATE ALTITUDE AND FLAG WAS DISPLAYED. REMOVED STRAIGHT FITTING FROM THE BACK OF THE ALTIMETER AND INSTALLED A 45 DEGREE FITTING TO PREVENT THE HOSE FROM KINKING. OPS CHECKS SATISFACTORY AT THIS TIME.
- [SDR GUUA95255022810B](https://openairdocs.org/sdr/GUUA95255022810B.md): Torque Tube · corroded · Feb 28, 2010 · N87552 · Beech 1900D · Elevator Structure
  > DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT ELEVATOR TORQUE TUBE EXFOLIATED. REPLACED RIGHT ELEVATOR TORQUE TUBE.
- [SDR GUUA95255022810A](https://openairdocs.org/sdr/GUUA95255022810A.md): Hinge Bracket · corroded · Feb 28, 2010 · N87552 · Beech 1900D · Elevator Structure
  > DURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT ELEVATOR OUTBOARD HINGE BRACKET HAS CORROSION. REPLACED LEFT ELEVATOR OUTBOARD HINGE BRACKET.
- [SDR GUUA95252100309B](https://openairdocs.org/sdr/GUUA95252100309B.md): Door · stiff · Oct 3, 2009 · N87552 · Beech 1900D · Entrance Stairs
  > FLIGHT: 9204, PILOT REPORTED AIRSTAIR DOOR DIFFICULT TO OPEN. PERFORMED OPERATIONAL FUNTIONAL CHECK NO DEFECTS NOTED.
- [SDR GUUA95252100309A](https://openairdocs.org/sdr/GUUA95252100309A.md): Door · stiff · Oct 3, 2009 · N87552 · Beech 1900D · Entrance Stairs
  > FLIGHT: 9160, PILOT REPORTED AIRSTAIR DOOR DIFFICULT TO OPEN. ADJUSTED AIRSTAIR DOOR FORWARD LOWER LATCH CAM OPERATIONAL CHECK GOOD.
- [SDR GUUA95271092809A](https://openairdocs.org/sdr/GUUA95271092809A.md): Truss · cracked · Sep 28, 2009 · N87552 · Beech 1900D · Engine Mount Section
  > DURING MAGNETIC PARTICLE INSP, DISCOVERED 2 ENGINE TRUSS TUBES HAVE WELD AREA CRACKS. PERFORMED WELD REPAIR TO ENG TRUSS TUBES WELD AREAS.
- [SDR GUUA95257082309A](https://openairdocs.org/sdr/GUUA95257082309A.md): Skin · corroded · Aug 23, 2009 · N87552 · Beech 1900D · Wing, Plate/Skin
  > DURING SCHEDULED ROUTINE INSP, DISCOVERED LT WING TOP SKIN SURFACE BETWEEN WS 147.74 AND WS 159.51 AT REAR SPAR HAS AREA OF BUCKLING SKIN SUSPECT CORROSION. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED REPAIR STRAP TO REAR SPAR CAP FLANGE FILLERS AND AN EXTER
- [SDR GUUA95253051109A](https://openairdocs.org/sdr/GUUA95253051109A.md): Skin · corroded · May 11, 2009 · N87552 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING SCHEDULED ROUTINE INSPECTION DISCOVERED CORROSION ON BELLY SKIN AT FUSELAGE STATION 340.75 STRINGER 15 RIGHT. REMOVED CORROSION FABRICATED AND INSTALLED EXTERNAL DOUBLER REPAIR.
- [SDR GUUA95255021609C](https://openairdocs.org/sdr/GUUA95255021609C.md): Mount · corroded · Feb 16, 2009 · N87552 · Beech 1900D · Elevator Structure
  > DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RIGHT ELEVATOR TORQUE TUBE MOUNT BASE EXFOLIATED. REPLACED RIGHT ELEVATOR TORQUE TUBE MOUNT BASE.
- [SDR GUUA95255021609B](https://openairdocs.org/sdr/GUUA95255021609B.md): Hinge Bracket · corroded · Feb 16, 2009 · N87552 · Beech 1900D · Rudder Miscellaneous Structure
  > DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED UPPER RUDDER HINGE BRACKET SHOW SIGNS OF EXFOLIATION. REPLACED UPPER RUDDER HINGE BRACKET.
- [SDR GUUA95255021609A](https://openairdocs.org/sdr/GUUA95255021609A.md): Hinge Bracket · corroded · Feb 16, 2009 · N87552 · Beech 1900D · Rudder Miscellaneous Structure
  > DURING SCHEDULED ROUTINE MX, DISCOVERED LOWER RUDDER HINGE BRACKET SHOW SIGNS OF EXFOLIATION. REPLACED LOWER RUDDER HINGE BRACKET.
- [SDR GUUA95252012109A](https://openairdocs.org/sdr/GUUA95252012109A.md): Door · stiff · Jan 21, 2009 · N87552 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE MX DISCOVERED RT AFT EMERGENCY EXIT HARD TO OPEN. LUBRICATED RT AFT EMERGENCY EXIT INTERIOR AND EXTERIOR HANDLES. OPS CHECK OK.
- [SDR GUUA95252011909A](https://openairdocs.org/sdr/GUUA95252011909A.md): Door · inoperative · Jan 19, 2009 · N87552 · Beech 1900D · Entrance Stairs
  > PILOT REPORTED AIRSTAIR DOOR DOES NOT FREE FALL ALL THE WAY DOWN. SERVICED AIRSTAIR DOOR STRUT. OPS CHECK GOOD.
- [SDR GUU2008F00054](https://openairdocs.org/sdr/GUU2008F00054.md): Cable Assy · defective · Sep 27, 2008 · N87552 · Beech 1900D · Passenger/Crew Doors
  > FLIGHT 9208 TPA/PNS PILOT DISCREPANCY. PILOT REPORTED UNABLE TO OPEN MAIN CABIN DOOR. C/A REPLACED UPPER AFT AIRSTAIR DOOR CABLE. OPS CHECK GOOD.
- [SDR GUU2008F00053](https://openairdocs.org/sdr/GUU2008F00053.md): Warning System · malfunctioned · Sep 24, 2008 · N87552 · Beech 1900D · Landing Gear Position and Warning
  > FLIGHT 99184 FLL/EYW PILOT DISCREPANCY. DURING APPROACH FLAPS AT 35 DEGREE SELECTION, LANDING GEAR UNSAFE LIGHT ILLUMINATED WITH 3 GREEN DOWN AND LOCKED LIGHT. CONTINUED TO EYW AND LANDED WITHOUT INCIDENT. C/A CHECKED SECURITY OF LANDING GEARS AND SWITCHES
- [SDR GUUA03150801](https://openairdocs.org/sdr/GUUA03150801.md): Downlock Switch · misinstalled · Mar 15, 2008 · N87552 · Beech 1900D · Landing Gear Position and Warning
  > FLIGHT:9253, DURING BOARDING LT (H) LIGHT AND LANDING GEAR HORN ARE BLINKING AND SOUNDING SIMULTANEOUSLY. ALL (3) GREEN LIGHTS ILLUMINATED WITH THE RED GEAR HANDLE LIGHT WITH GEAR HORN. INSTALLED MISSING BOLT ON LT DOWNLOCK SWITCH.
- [SDR GUUA12200702](https://openairdocs.org/sdr/GUUA12200702.md): Door · inoperative · Dec 20, 2007 · N87552 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT FWD EMERGENCY EXIT DOOR WILL NOT OPEN. READJUSTED RT FWD EMERGENCY EXIT.
- [SDR GUUA12200701](https://openairdocs.org/sdr/GUUA12200701.md): Door · inoperative · Dec 20, 2007 · N87552 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT EMERGENCY EXIT DOOR WILL NOT OPEN. ADJUSTED LT EMERGENCY EXIT DOOR.
- [SDR GUUA09280701](https://openairdocs.org/sdr/GUUA09280701.md): Bolt · unknown · Sep 28, 2007 · N87552 · Beech 1900D · Main Landing Gear
  > AFTER TAKEOFF AT TNT LT MAIN LANDING GEAR GREEN ANNUNCIATOR BLANK OUT AND RED HANDLE ILLUMINATED. RECYCLED LANDING GEAR TWO TIMES WITH SAME RESULTS.CONTINUED TO FLL. MANUALLY EXTENDED LANDING GEAR LANDED WITHOUT INCIDENT. INSPECTED LANDING GEAR SYSTEM INSTAL
- [SDR GUUA09120701](https://openairdocs.org/sdr/GUUA09120701.md): Hinge Bracket · corroded · Sep 12, 2007 · N87552 · Beech 1900D · Elevator Structure
  > DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT OB ELEVATOR HINGE BRACKET HAS CORROSION. REPLACED LT OB ELEVATOR HINGE BRACKET.
- [SDR GUUA95253053107A](https://openairdocs.org/sdr/GUUA95253053107A.md): Pressure Panel · cracked · May 31, 2007 · N87552 · Beech 1900D · Fuselage Main, Bulkhead
  > DURING INSP DISCOVERED CRACKED CEILING IN NOSE WHEEL WELL AT FS 89 WL 100.00 AT CENTER BUTT LINE. REMOVED DAMAGED AREA AND INSTALLED SHIM AND EXTERNAL REINFORCEMENT DOUBLER REPAIR.
- [SDR GUUA95253052907A](https://openairdocs.org/sdr/GUUA95253052907A.md): Bulkhead · cracked · May 29, 2007 · N87552 · Beech 1900D · Fuselage Main, Bulkhead
  > DURING INSP DISCOVERED RT FWD PRESSURE BULKHEAD CRACKED 2.5 INCHES HORIZONTALLY AND 1.0 INCH VERTICALLY AT STA 89.00. STOP DRILLED CRACKS AND INSTALLED AN EXTERNAL DOUBLER REPAIR.
- [SDR GUUA05110702](https://openairdocs.org/sdr/GUUA05110702.md): Uplock Switch · failed · May 11, 2007 · N87552 · Beech 1900D · Landing Gear Position and Warning
  > DURING APPROACH LANDING GEAR WOULD NOT EXTEND NORMALLY. MANUAL EXTENSION GOT SAFE FOR LT AND RT MAINS. LANDED WITHOUT A LOCKED NOSE GEAR. SHUTDOWN RT ENGINE AT 1,000 FEET AND LT ENGINE PRIOR TO TOUCHDOWN. REPLACED LT MAIN LANDING GEAR UP LOCK SWITCH AND SERVI
- [SDR GUUA05080701](https://openairdocs.org/sdr/GUUA05080701.md): Motor · inoperative · May 8, 2007 · N87552 · Beech 1900D · Landing Gear Retraction/Extension System
  > FLIGHT: 9159 VPS/TPA - DURING APPROACH, LANDING GEAR WOULD NOT COME DOWN WHEN EXTENDED. MANUALLY EXTENDED LANDIND GEAR. REPLACED LANDING GEAR POWER PACK MOTOR. OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY.
- [SDR GUUA05060701](https://openairdocs.org/sdr/GUUA05060701.md): Selector Valve · malfunctioned · May 6, 2007 · N87552 · Beech 1900D · Landing Gear Retraction/Extension System
  > FLIGHT: 9285 FLL/EYW - DURING APPROACH, LANDING GEAR DID NOT EXTEND WHEN SELECTED DOWN. MANUALLY EXTENDED LANDING GEAR. REPLACED SELECTOR VALVE. OPREATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY.
- [SDR GUUA05040702](https://openairdocs.org/sdr/GUUA05040702.md): Switch · malfunctioned · May 4, 2007 · N87552 · Beech 1900D · Landing Gear Retraction/Extension System
  > FLIGHT: 9197 TLH/TPA - DURING APPROACH, LANDING GEAR DID NOT COME DOWN ON THE FIRST ATTEMPT. REPLACED LANDING GEAR CONTROL. OPERATIONAL CHECK NORMAL.
- [SDR GUUA05020701](https://openairdocs.org/sdr/GUUA05020701.md): Circuit Board · failed · May 2, 2007 · N87552 · Beech 1900D · Landing Gear System Wiring
  > FLIGHT: 9216 PNS/TPA - DURING APPROACH, SECOND LANDING GEAR EXTENSION ATTEMPT GEAR EXTENDED AFTER 20 SECONDS. REPLACE TIME DELAY PC BOARD AND LANDING GEAR RELAY. OPERATIONAL CHECK NORMAL.
- [SDR GUUA04260701](https://openairdocs.org/sdr/GUUA04260701.md): Actuator · leaking · Apr 26, 2007 · N87552 · Beech 1900D · Landing Gear Actuator
  > FLIGHT:9133 TPA/EYW - DURING APPROACH LANDING GEAR HAD A SLIGHT DELAY WHEN PUT IN THE DOWN POSITION. REPLACED LEFT MAIN LANDING GEAR ACTUATOR. OPERATIONAL CHECK NORMAL.
- [SDR GUUA04190701](https://openairdocs.org/sdr/GUUA04190701.md): Uplock Switch · dirty · Apr 19, 2007 · N87552 · Beech 1900D · Landing Gear Position and Warning
  > FLIGHT: 9221 TLH/PBI - DURING FLIGHT, LANDING GEAR HANDLE LIGHTS ILLUMINATED. CLEANED BOTH MAIN LANDING GEAR UPLOCK SWITCHES. COULD NOT DUPLICATE.
- [SDR GUUA09030602](https://openairdocs.org/sdr/GUUA09030602.md): Warning Light · false indication · Sep 3, 2006 · N87552 · Beech 1900D · Indicating/Recording System
  > FLIGHT: 9166 NAS/FLL DURING FLIGHT LT AND RT DISCHARGE LIGHTS RANDOMLY ILLUMINATED. CHECKED CONECTIONS GOOD CONTACT COULD NOT DUPLICATE.
- [SDR GUUA95253042606A](https://openairdocs.org/sdr/GUUA95253042606A.md): Spar · cracked · Apr 26, 2006 · N87552 · Beech 1900D · Aircraft Structures
  > DURING SCHEDULED ROUTINE MX DISCOVERED 2.0 INCH CRACK IN SPAR AREA AT BL 30.62. STOP DRILLED CRACK AND INSTALLED REINFORCEMENT DOUBLER REPAIR.
- [SDR GUU2005F00044](https://openairdocs.org/sdr/GUU2005F00044.md): Bracket · corroded · Aug 17, 2005 · N87552 · Beech 1900D · Elevator Structure
  > AT SCHEDULED ROUTINE MAINTENANCE, RT ELEVATOR OB HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT ELEVATOR OB HINGE BRACKET. (K)
- [SDR GUU2005F00043](https://openairdocs.org/sdr/GUU2005F00043.md): Bracket · corroded · Aug 17, 2005 · N87552 · Beech 1900D · Elevator Structure
  > AT SCHEDULED ROUTINE MAINTENANCE, RT ELEVATOR CENTER HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT ELEVATOR CENTER HINGE BRACKET. (K)
- [SDR GUU2005F00019](https://openairdocs.org/sdr/GUU2005F00019.md): Brake · unresponsive · May 28, 2005 · N87552 · Beech 1900D · Landing Gear Brake System
  > LT TOE BRAKE DOES NOT WORK. HAVE TO PUMP UP PRESSURE. BLED LT BRAKE SYSTEM. OPS CHECK NORMAL. (K)
- [SDR GUU2005F00008](https://openairdocs.org/sdr/GUU2005F00008.md): Hinge Bracket · corroded · Mar 5, 2005 · N87552 · Beech 1900D · Horizontal Stabilizer Structure
  > AT SCHEDULED ROUTINE MAINTENANCE, LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LT OB ELEVATOR HINGE BRACKET. (K)
- [SDR 2004F00171](https://openairdocs.org/sdr/2004F00171.md): Blade · failed · Nov 18, 2003 · N87552 · Beech 1900D · Turbine Engine Compressor Section
  > DURING TAKEOFF, LOUD BANG OCCURRED ON LEFT ENGINE. ABORTED TAKEOFF. DEMATED POEWR SECIOTN FROM GAS GENERTOR AND DETERMINED THAT POWER TURBINE BLADES WERE BROKE OFF. REPLACED LEFT POWER SECTION MODULE AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. C
- [SDR 2004F00047](https://openairdocs.org/sdr/2004F00047.md): Turbine Blades · broken · Nov 18, 2003 · N87552 · Beech 1900D · Turbine Section
  > DURING TAKEOFF, LOUD BANG OCCURRED ON LT ENGINE. ABORTED TAKEOFF. SEPARATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES WERE BROKE OFF. REPLACED LEFT POWER SECITON MODULE AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR.
- [SDR 2003F00111](https://openairdocs.org/sdr/2003F00111.md): Warning System · activated · Jan 17, 2003 · N87552 · Beech 1900D · Landing Gear Position and Warning
  > FLT 9198 - MIA-TPA - AFTER LANDING, RED LIGHT IN LANDING GEAR HANDLE ILLUMINATED AND LANDING GEAR WARNING HORN WOULD NOT CEASE. RESECURED LANDING GEAR HANDLE LIGHT KNOB. OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY. (M)
- [SDR GUUA07270209](https://openairdocs.org/sdr/GUUA07270209.md): Switch · dirty · Jul 17, 2002 · N87552 · Beech 1900D · Autopilot System
  > YAW DAMPER DISENGAGES BOTH LEFT AND RIGHT, IN FLIGHTCLEANED CAPTAINS YOKE DISCONNECT SWITCH
- [SDR GUUA07270208](https://openairdocs.org/sdr/GUUA07270208.md): Trim Switch · dirty · Jul 16, 2002 · N87552 · Beech 1900D · Elevator Control System
  > ELECTRIC TRIM LOCKS TRIM IN POSITION. OPERATES NORMAL WHEN ELECTRIC TRIM IS DISENGAGEDCLEANED ELECTRIC TRIM SWITCH IN CAPTAINS YOKE

Next page: https://openairdocs.org/deregistered/N87552-2015-12-04/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 = 'N87552' AND deregistration_id = 'N87552-2015-12-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N87552-2015-12-04/reports

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