# Service difficulty reports: N38537

A list on [N38537](https://openairdocs.org/aircraft/N38537.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 · 71 reports

- [SDR 29GA93755101712](https://openairdocs.org/sdr/29GA93755101712.md): Channel · cracked · Oct 18, 2012 · N38537 · Beech 1900D · Vertical Stabilizer Miscellaneous Structure
  > DURING SCHEDULED INSPECTION FCD 55-09-19-02 FOUND CRACK IN HAT SECTION OF VERTICAL STABILIZER AREA C.
- [SDR 29GA93732082912](https://openairdocs.org/sdr/29GA93732082912.md): Downlock Switch · loose · Aug 29, 2012 · N38537 · Beech 1900D · Landing Gear Position and Warning
  > FLIGHT 3563 SDY/BIL RED LIGHT IN GEAR HANDLE COMES ON AND GEAR WARNING HORN ACTIVATES ON TOUCHDOWN WITH POWER LEVERS AT IDLE. TIGHTENED RIGHT MAIN LANDING GEAR DOWNLOCK SWITCH, OPERATIONAL CHECKS GOOD.
- [SDR 29GA2012082293753](https://openairdocs.org/sdr/29GA2012082293753.md): Skin · gouged · Aug 19, 2012 · N38537 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING SCHEDULED ROUTINE INSPECTION DISCOVERED AIRSTAIR DOOR FRAME INNER SKIN 2.0 INCH GOUGE DAMAGE AT FS 150 STRINGER 8. REMOVED DAMAGED SECTION OF SKIN AND INSTALLED COVER PATCH REPAIR.
- [SDR 29GA93753082012](https://openairdocs.org/sdr/29GA93753082012.md): Angle · cracked · Aug 19, 2012 · N38537 · Beech 1900D · Passenger/Crew Doors
  > DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT AIRSTAIR DOOR FORWARD ANGLE CRACKED APPROXIMATELY AT FS 150. REMOVED 2.0 INCH SECTION OF DAMAGED ANGLE AND INSTALLED REPAIR ANGLE.
- [SDR 29GA93753081912](https://openairdocs.org/sdr/29GA93753081912.md): Angle · cracked · Aug 19, 2012 · N38537 · Beech 1900D · Fuselage Miscellaneous Structure
  > DURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT HEAVY ANGLE CRACKED LESS THAN 2.25 INCHES AT FS 288. STOP DRILLED END OF CRACK AND INSTALLED REPAIR ANGLE.
- [SDR 29GA93732062712](https://openairdocs.org/sdr/29GA93732062712.md): Indication Sys · intermittent · Jun 27, 2012 · N38537 · Beech 1900D · Landing Gear Position and Warning
  > FLIGHT 3574 BIL/MLS NOSE WHEEL DID NOT GIVE DOWN AND LOCKED INDICATION UPON NORMAL EXTENSION ATTEMPTED EXTENSION A SECOND TIME AND WAS SUCCESSFUL. CYCLED GEAR FIVE TIMES NO FAILURES. REMOVED AND REPLACED GREEN GEAR INDICATION BLOCK CYCLED GEAR FIVE MORE TIME
- [SDR 29GA93761062811A](https://openairdocs.org/sdr/29GA93761062811A.md): Pressure Switch · malfunctioned · Jun 28, 2011 · N38537 · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTS, ON APPROACH, RT PROPELLER CYCLES IN AND OUT OF AUTOFEATHER. REPLACED RT AUTOFEATHER LOW PRESSURE SWITCH.
- [SDR GUUA93723060111A](https://openairdocs.org/sdr/GUUA93723060111A.md): Radio · shorted · Jun 1, 2011 · N38537 · Beech 1900D · HF Communications System
  > NR 2 COMM FAILED ACCOMPANIED BY SMOKE. INSPECTED WIRING BEHIND RADIO PANEL, NO DEFECTS NOTED. REPLACED COMM NR 2 RADIO, RAN UNIT FIFTEEN MINUTES, NO DEFECTS NOTED.
- [SDR GUUA93761022811A](https://openairdocs.org/sdr/GUUA93761022811A.md): Propeller · malfunctioned · Feb 28, 2011 · N38537 · Beech 1900D · Propeller Controlling System
  > DURING APPROACH RT ENG CYCLED BETWEEN 700 AND 1200 POUNDS OF TORQUE WITH ASSOCIATED RT AUTO FEATHER LIGHT. CHECKED AUTO FEATHER SWITCH SETTINGS AND PERFORMED MULTIPLE AUTOFEATHER TEST OPS CHECK NORMAL.
- [SDR GUUA93757011711C](https://openairdocs.org/sdr/GUUA93757011711C.md): Spar Cap · corroded · Jan 17, 2011 · N38537 · Beech 1900D · Wing Spar
  > DURING SCHEDULED X-RAY INSP DISCOVERED LT WING CORROSION AT LOWER FWD SPAR CAP NEAR FUEL DRAIN WS 125.5. REMOVED CORROSION FROM LEFT WING AT LOWER FORWARD SPAR CAP NEAR FULE DRAIN WS 125.5 AND INSTALLED AN EXTERNAL DOUBLER REPAIR.
- [SDR GUUA93757011711B](https://openairdocs.org/sdr/GUUA93757011711B.md): Spar Cap · corroded · Jan 17, 2011 · N38537 · Beech 1900D · Wing Spar
  > DURING SCHEDULED X RAY INSP DISCOVERED RT WING CORROSION AT LOWER FWD SPAR CAP NEAR FUEL DRAIN. REMOVED CORROSION FROM RIGHT WING LOWER FORWARD SPAR CAP COMPLIED WITH FLOURESCENT INSPECTION ON BLEND OUT AREA NO SIGNS OF CORROSION FOUND,ALL AREAS WITHIN LIMITS
- [SDR GUUA93757011711A](https://openairdocs.org/sdr/GUUA93757011711A.md): Stringer · corroded · Jan 17, 2011 · N38537 · Beech 1900D · Wing, Longeron/Stringer
  > DURING SCHEDULED X RAY INSP DISCOVERED RT WING CORROSION IN RT COLLECTOR TANK 1ST STRINGER AFT OF SPAR BPTH SIDES OF FLANGE 4 INCHES TO 6 INCHES FROM INBD RIB. REMOVED CORROSION INSTALLED REPAIR STRINGER AND DOUBLER REPAIRS TO FORWARD AND AFT FLANGES.
- [SDR GUUA93752120810A](https://openairdocs.org/sdr/GUUA93752120810A.md): Handle · binding · Dec 8, 2010 · N38537 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE INSP, DISCOVERED RT FWD EMERGENCY EXIT HANDLE DIFFICULT TO OPERATE. ADJUSTED UPPER STRIKER PLATES AND LOWER LUGS, OPS CHECK GOOD. ACFT DOWN FOR STRUCTURAL INSP.
- [SDR GUUA93753111510A](https://openairdocs.org/sdr/GUUA93753111510A.md): Skin · chafed · Nov 15, 2010 · N38537 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING SCHEDULED ROUTINE INSP, DISCOVERED LT EXTERNAL SKIN CHAFE, APPROX AT FS 259-281 WS 30. REPAIRED LT EXTERNAL SKIN CHAFE INSTALLED EXTERNAL DOUBLER 1.5 X 22 INCHES COVER PATCH.
- [SDR GUUA93753111410A](https://openairdocs.org/sdr/GUUA93753111410A.md): Door Frame · cracked · Nov 14, 2010 · N38537 · Beech 1900D · Fuselage Main, Structure
  > DURING SCHEDULED ROUTINE INSP, DISCOVERED UPPER AFT CARGO DOOR FRAME HAS A 2.0 INCH CRACK APPROX AT FS 509.5, STRINGER 14L. REPAIRED CRACKED "L" ANGLE BY REMOVING 47.0 INCHESS OF ANGLE AND INSTALLING INSERTION OF THE SAME MATERIAL AND A 9.5 INCH REINFORCEMENT
- [SDR GUUA93732103110A](https://openairdocs.org/sdr/GUUA93732103110A.md): Switch · inoperative · Oct 31, 2010 · N38537 · Beech 1900D · Landing Gear Retraction/Extension System
  > PILOT REPORTED LANDING GEAR HAD TO BE RETRACTED BY BYPASSING THE "J" HOOK. REPLACED LANDING GEAR SWITCH OPS CHECK SATISFACTORY.
- [SDR GUUA93732091210A](https://openairdocs.org/sdr/GUUA93732091210A.md): Annunciator · intermittent · Sep 12, 2010 · N38537 · Beech 1900D · Landing Gear Position and Warning
  > PILOT REPORTED CTR LANDING GEAR DOWN GREEN LIGHT INTERMITTENT. REPLACED CENTER LANDING GEAR DOWN GREEN LIGHT ANNUNCIATOR. OPS CHECK NORMAL.
- [SDR GUUA93727081210A](https://openairdocs.org/sdr/GUUA93727081210A.md): Torque Tube · corroded · Aug 12, 2010 · N38537 · Beech 1900D · Elevator Control System
  > DURING SCHEDULED ROUTINE INSP DISCOVERED LT ELEVATOR TORQUE TUBE HAS CORROSION. REPLACED LT ELEVATOR TORQUE TUBE.
- [SDR GUUA93734062410A](https://openairdocs.org/sdr/GUUA93734062410A.md): Altimeter · reads low · Jun 24, 2010 · N38537 · Beech 1900D · Altimeter, Barometric/Encoder
  > FLIGHT: 9174 AFTER TAKEOFF CAPTAINS ALTIMETER HAD A 300 FT SPLIT AT 11,000 FT AND 240 FT SPLIT ON LANDING. DECLARED AN EMERGENCY RETURNED TO TPA LANDED WITHOUT INCIDENT. REPLACED CAPTAINS ALTIMETER.
- [SDR GUUA93757061110A](https://openairdocs.org/sdr/GUUA93757061110A.md): Access Panel · delaminated · Jun 11, 2010 · N38537 · Beech 1900D · Wing, Plate/Skin
  > DURING SCHEDULED ROUTINE INSP DISCOVERED LT WING FUEL ACCESS PANEL 542CB LEAKS. REPAIRED DELAMINATED SKIN AT WING ACCESS PANEL 542CB.
- [SDR GUUA93757042810A](https://openairdocs.org/sdr/GUUA93757042810A.md): Panel · debonded · Apr 28, 2010 · N38537 · Beech 1900D · Wing, Plate/Skin
  > DURING SCHEDULED ROUTINE INSP DISCOVERED LT AND RT INTERNAL DOUBLERS FOR FUEL PANEL 532DB, 532FB, 631DB AND 642FB DEBONDED. REBONDED RING DOUBLERS AT FUEL PANELS 532DB, 532FB, 631DB AND 642FB.
- [SDR GUUA93732041810A](https://openairdocs.org/sdr/GUUA93732041810A.md): Switch · intermittent · Apr 18, 2010 · N38537 · Beech 1900D · Landing Gear Position and Warning
  > PILOT REPORTED GEAR WARNING SILENCE BUTTON DOES NOT SILENCE THE GEAR WARNING HORN. REPLACED GEAR WARNING SILENCE SWITCH, OPS CHECK GOOD.
- [SDR GUUA93732041110A](https://openairdocs.org/sdr/GUUA93732041110A.md): Warning Horn · malfunctioned · Apr 11, 2010 · N38537 · Beech 1900D · Landing Gear Position and Warning
  > PILOT REPORTED GEAR WARNING HORN STILL SOUNDS OCCASIONALLY WITH SILENCE BUTTON DEPRESSED. CLEANED AND RERACKED PCB CONNECTOR P273 OPS CHECK NORMAL.
- [SDR GUUA93757020710A](https://openairdocs.org/sdr/GUUA93757020710A.md): Skin · punctured · Feb 7, 2010 · N38537 · Beech 1900D · Wing, Plate/Skin
  > DURING SCHEDULED ROUTINE INSP DISCOVERED RT STUB WING TOP OF L/E HAS A DENT AND PUNTURED. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR.
- [SDR GUUA93721111509A](https://openairdocs.org/sdr/GUUA93721111509A.md): Line · leaking · Nov 15, 2009 · N38537 · Beech 1900D · Aircraft Fuel Distribution System
  > PILOT REPORTED VERY STRONG CHEMICAL ODOR INSIDE PLANE. REPLACED RT ENGINE PRESSURE FUEL LINE, OPS CHECK OK.
- [SDR GUUA93721111409A](https://openairdocs.org/sdr/GUUA93721111409A.md): Intake · contaminated · Nov 14, 2009 · N38537 · Beech 1900D · Engine Air Intake System
  > PILOT REPORTED CHEMICAL ODOR COMING FROM RT BLEED. FOUND RESIDUAL OIL AT RT ENG INTAKE CLEANED AREA OF OIL. PREVIOUSLY SUBMITTED CORRECTED DATE.
- [SDR GUUA93721110409A](https://openairdocs.org/sdr/GUUA93721110409A.md): Intake · contaminated · Nov 14, 2009 · N38537 · Beech 1900D · Engine Air Intake System
  > PILOT REPORTED CHEMICAL ODOR COMING FROM RT BLEED. FOUND RESIDUAL OIL AT RT ENG INTAKE. CLEANED AREA OF OIL.
- [SDR GUUA93732101009A](https://openairdocs.org/sdr/GUUA93732101009A.md): Socket · loose · Oct 10, 2009 · N38537 · Beech 1900D · Landing Gear Position and Warning
  > PILOT REPORTED UPPER LANDING GEAR WARNING LIGHT INTERMITTENT. SECURED LOOSE BULB AND SOCKET ON THE LANDING GEAR HANDLE.
- [SDR GUUA93727082709A](https://openairdocs.org/sdr/GUUA93727082709A.md): Horn · corroded · Aug 27, 2009 · N38537 · Beech 1900D · Elevator Control System
  > DURING SCHEDULED ROUTINE INSPECTION DISCOVERED LT ELEVATOR TRIM TAB HORN EXFOLIATED. REPLACED LT ELEVATOR TRIM TAB.
- [SDR GUUA93721080809A](https://openairdocs.org/sdr/GUUA93721080809A.md): Unknown · odor · Aug 8, 2009 · N38537 · Beech 1900D · Air Distribution System
  > UPON ARRIVAL, BURNING ODOR NOTICED IN COCKPIT AND CABIN. INSPECTED BLOWERS AND AVIONICS, RAN BOTH ENGINES WITH BLEEDS ON COULD NOT ODOR BURNING.
- [SDR GUUA93752072909A](https://openairdocs.org/sdr/GUUA93752072909A.md): Cover · unsecure · Jul 29, 2009 · N38537 · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED UNABLE TO LOCK MAIN CABIN DOOR PROPERLY. INSPECTED AND SECURED PLASTIC COVER ON DOOR. OPS CHECK GOOD.
- [SDR GUUA93757062409A](https://openairdocs.org/sdr/GUUA93757062409A.md): Skin · corroded · Jun 24, 2009 · N38537 · Beech 1900D · Wing, Plate/Skin
  > DURING SCHEDULED ROUTINE INSP DISCOVERED RT UPPER WING SKIN T/E CORROSION AND DEBOND BETWEEN WING STA 136.036 THROUGH 196.06. REMOVED DAMAGED SKIN AND INSTALLED EXTERNAL REPAIR DOUBLER.
- [SDR GUUA93757061709A](https://openairdocs.org/sdr/GUUA93757061709A.md): Stringer · corroded · Jun 17, 2009 · N38537 · Beech 1900D · Wing, Longeron/Stringer
  > DURING SCHEDULED INSP DISCOVERED LT WING COLLECTOR TANK AREA 1 J STRINGER HAS CORROSION.
- [SDR GUUA93757061709D](https://openairdocs.org/sdr/GUUA93757061709D.md): Spar · corroded · Jun 17, 2009 · N38537 · Beech 1900D · Wing Spar
  > DURING SCHEDULED INSP DISCOVERED LT WING FWD SPAR AFT FLANGE AREA 3 HAS CORROSION. REMOVED CORROSION AND INSTALLED REPAIR STRAP.
- [SDR GUUA93757061709C](https://openairdocs.org/sdr/GUUA93757061709C.md): Spar · corroded · Jun 17, 2009 · N38537 · Beech 1900D · Wing Spar
  > DURING SCHEDULE INSP DISCOVERED LT WING FWD FRONT SPAR AREA 2 HAS CORROSION. REMOVED CORROSION AND INSTALLED REPAIR STRAP.
- [SDR GUUA93757061709B](https://openairdocs.org/sdr/GUUA93757061709B.md): Spar · corroded · Jun 17, 2009 · N38537 · Beech 1900D · Wing Spar
  > DURING SCHEDULED INSP DISCOVERED LT WING COLLECTOR TANK AREA 1 FWD SPAR AFT FLANGE HAS CORROSION. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR STRAP.
- [SDR GUUA93757061409B](https://openairdocs.org/sdr/GUUA93757061409B.md): Skin · corroded · Jun 14, 2009 · N38537 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING SCHEDULED ROUTINE INSP, DISCOVERED RT FUSELAGE BELLY EXFOLIATED AT FS 303.25. REMOVED EXFOLIATED SKIN AND INSTALLED FILLER AND DOUBLER REPAIR.
- [SDR GUUA93757061409A](https://openairdocs.org/sdr/GUUA93757061409A.md): Skin · cracked · Jun 14, 2009 · N38537 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING SCHEDULED ROUTINE MX 2.25 INCH CRACK ON RT FUSELAGE BELLY AT FS 310.00. INSTALLED FILLER AND DOUBLER REPAIR.
- [SDR GUUA93732051809A](https://openairdocs.org/sdr/GUUA93732051809A.md): Line · cracked · May 18, 2009 · N38537 · Beech 1900D · Hydraulic System, Main
  > PILOT REPORTED LT BRAKE PEDAL GOES TO THE FLOOR. REMOVED AND REPLACED CRACKED HYD BRAKE LINE.
- [SDR GUUA93752051709A](https://openairdocs.org/sdr/GUUA93752051709A.md): Cable · broken · May 17, 2009 · N38537 · Beech 1900D · Passenger/Crew Doors
  > DURING SCHEDULED ROUTINE MX DISCOVERED FWD AIRSTAIR DOOR CAMS NOT MOVING. REPLACED FWD LOWER DOOR CABLE.
- [SDR GUUA93753050809A](https://openairdocs.org/sdr/GUUA93753050809A.md): Skin · cracked · May 8, 2009 · N38537 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING SCHEDULED ROUTINE INSP, DISCOVERED LT FUSELAGE BELLY SKIN HAS.75 INCH CRACK AT FS 260.750. STOP DRILLED CRACK AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER.
- [SDR GUUA93721041909A](https://openairdocs.org/sdr/GUUA93721041909A.md): Unknown · odor · Apr 19, 2009 · N38537 · Beech 1900D · Air Distribution System
  > FLIGHT: 9180, DURING FLIGHT, STRONG BURNING RUBBER ODOR WITH RT BLEED AIR VALVE OPEN, GOES AWAY WHEN VALVE IS CLOSED, HAPPENS ONLY IN FLIGHT. INSPECTED FUEL LINES,OIL LINES BYPASS AND THRU VALVE PERFORMED RUN UPS AT 90 PERCENT WITH BLEEDS ON NO DISCREPANCY FO
- [SDR GUUA93734041809A](https://openairdocs.org/sdr/GUUA93734041809A.md): Display · intermittent · Apr 18, 2009 · N38537 · Beech 1900D · Attitude and Direction Data System
  > DURING FLIGHT, CAPTAIN`S EADI FLICKERED A FEW TIMES, DISPLAY THEN SHRUNK FOLLOWED BY STRONG BURNING ODOR. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. REPAIRED BROKEN WIRE AT EFIS SCREEN COOLING FAN. OPS CHECK NORMAL.
- [SDR GUUA93755020109A](https://openairdocs.org/sdr/GUUA93755020109A.md): Hinge Bracket · corroded · Feb 1, 2009 · N38537 · Beech 1900D · Rudder Miscellaneous Structure
  > DURING SCHEDULED ROUTINE MX DISCOVERED RT ELEVATOR OTBD HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR OTBD HINGE BRACKET.
- [SDR GUUA937120908A](https://openairdocs.org/sdr/GUUA937120908A.md): Actuator · bypassing · Dec 9, 2008 · N38537 · Beech 1900D · Landing Gear Actuator
  > FLIGHT NR 9191 PNS/TPA DURING FLIGHT LANDING GEAR RELAY CIRCUIT BREAKER POPPED. REPLACED LT MLG ACTUATOR. OPS CHECK NORMAL.
- [SDR GUUA10130802](https://openairdocs.org/sdr/GUUA10130802.md): Door · malfunctioned · Oct 13, 2008 · N38537 · Beech 1900D · Passenger/Crew Doors
  > FLIGHT 9154 - MCO/MIA - PILOT REPORTED CHECK FORWARD CABIN DOOR FOR PROPER OPERATION APPEARS TO JAM. INSPECTED FORWARD CABIN DOOR. NO DEFECTS NOTED. OPERATIONAL CHECK NORMAL.
- [SDR GUUA03010803](https://openairdocs.org/sdr/GUUA03010803.md): Hinge Bracket · corroded · Mar 1, 2008 · N38537 · Beech 1900D · Elevator Structure
  > DURING SCHEDULED ROUTINE MAINT, DISCOVERED RT ELEVATOR CTR HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR CTR HINGE BRACKET.
- [SDR GUUA03010802](https://openairdocs.org/sdr/GUUA03010802.md): Hinge Bracket · corroded · Mar 1, 2008 · N38537 · Beech 1900D · Elevator Structure
  > DURING SCHEDULED ROUTINE MAINT, DISCOVERED LT ELEVATOR OB HINGE BRACKET EXFOLIATED. REPLACED LT ELEVATOR OB HINGE BRACKET.
- [SDR GUUA03010801](https://openairdocs.org/sdr/GUUA03010801.md): Hinge Bracket · corroded · Mar 1, 2008 · N38537 · Beech 1900D · Elevator Structure
  > DURING SCHEDULED ROUTINE MAINT DISCOVERED LT CTR ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED LT ELEVATOR CENTER HINGE BRACKET.
- [SDR GUUA02090801](https://openairdocs.org/sdr/GUUA02090801.md): Latch · broken · Feb 9, 2008 · N38537 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE MAINT, DISCOVERED RT AFT EMERGENCY EXIT DOOR TOP CAM BROKEN. REPLACED EMERGENCY EXIT ARM LATCH ASSY.

Next page: https://openairdocs.org/aircraft/N38537/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 = 'N38537' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N38537/reports

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