# Service difficulty reports: N81538, cancelled Aug 2, 2013

A list on [N81538, cancelled Aug 2, 2013](https://openairdocs.org/deregistered/N81538-2013-08-02.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 · 59 reports

- [SDR 29GA93832050412A](https://openairdocs.org/sdr/29GA93832050412A.md): Switch · out of adjust · May 4, 2012 · N81538 · Beech 1900D · Landing Gear Position and Warning
  > FLIGHT: 5201 TPA/GNV GEAR WARNING HORN AND GEAR UNSAFE LIGHT COMES ON WHEN LEFT POWER LEVER RETARDED TO 89.6 N1. ADJUSTED GEAR WARNING HORN MICRO-SWITCH OPERATIONAL CHECK GOOD. TEST FLIGHT SATISFACTORY.
- [SDR 29GA93832040912](https://openairdocs.org/sdr/29GA93832040912.md): Switch · out of adjust · Apr 9, 2012 · N81538 · Beech 1900D · Power Lever
  > FLIGHT 4009, PILOT REPORTED LANDING GEAR WARNING HORN COMES OFF AT 91% N1. ADJUSTED POWER LEVERS SWITCHES, TEST FLIGHT SATISFACTORY.
- [SDR 29GA93852032312A](https://openairdocs.org/sdr/29GA93852032312A.md): Handle · lack of lube · Mar 23, 2012 · N81538 · Beech 1900D · Emergency Exits
  > REPORT: DURING SCHEDULED ROUTINE INSPECTION DICOVERED RIGHT AFT EMERGENCY EXIT OUTER LATCH HANDLE CATCH WILL NOT SPRING OPEN. LUBRICATED RIGHT AFT EXIT OUTER DOOR HANDLE AND LATCH MECHANISM.
- [SDR 29GA93871021012A](https://openairdocs.org/sdr/29GA93871021012A.md): Attach Bracket · cracked · Feb 10, 2012 · N81538 · Beech 1900D · Engine Cowling System
  > DURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS COWLING ATTACH BRACKET WELD AREA CRACKS AND ENGINE MOUNT ATTACH POINTS WELD AREA CRACKS AND TRUSS TUBE CHAFE. PERFORMED WELD REPAIRS TO ENGINE TRUSS IN ACCORDANCE WITH FAA APPROVED DATA.
- [SDR 29GA93871020312A](https://openairdocs.org/sdr/29GA93871020312A.md): Truss · cracked · Feb 3, 2012 · N81538 · Beech 1900D · Engine Mount Section
  > DURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS COWLING ATTACH BRACKET WELD AREA CRACKS AND ENGINE MOUNT ATTACH POINTS WELD AREA CRACKS. PERFORMED WELD REPAIR TO ENGINE TRUSS ATTACH BRACKETS WELD AREAS AND ENGINE MOUNT ATTACH POINTS WELD AREAS IN
- [SDR 29GA93852101411B](https://openairdocs.org/sdr/29GA93852101411B.md): Handle · lack of lube · Oct 14, 2011 · N81538 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE C-3 INSPECTION DISCOVERED LEFT AFT EMERGENCY EXIT OUTER HANDLE DOES NOT SPRING OPEN. CLEANED AND LUBRICATED LEFT AFT EMERGENCY EXIT OUTER HANDLE OPERATIONAL CHECK GOOD.
- [SDR 29GA93852101411A](https://openairdocs.org/sdr/29GA93852101411A.md): Handle · lack of lube · Oct 14, 2011 · N81538 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE C-3 INSPECTION DISCOVERED RIGHT AFT EMERGENCY EXIT OUTER HANDLE DOES NOT SPRING OPEN. CLEANED AND LUBRICATED RIGHT AFT EMERGENCY EXIT OUTER HANDLE OPERATIONAL CHECK GOOD.
- [SDR GUUA93853051211A](https://openairdocs.org/sdr/GUUA93853051211A.md): Skin · cracked · May 12, 2011 · N81538 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING SCHEDULED ROUTINE MX LOWER FUSELAGE BELLY SKIN HAS A SMALL CRACK AND SIGNS OF CORROSION BETWEEN FS 456.00 AND 482.75 AT STRINGER 14R. REMOVED DAMAGED AREA AND INSTALLED SKIN FILLER REPAIR AND EXTERNAL DOUBLER REPAIR.
- [SDR GUUA93852040511A](https://openairdocs.org/sdr/GUUA93852040511A.md): Cable · broken · Apr 5, 2011 · N81538 · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED MAIN CABIN DOOR UPPER RT CAM LOCK WILL NOT ROTATE. DOOR WILL NOT OPEN OR LOCK PROPERLY. REPLACED AIRSTAIR DOOR FWD UPPER AND LOWER CABLES. OPS CHECK GOOD.
- [SDR GUUA93852012311A](https://openairdocs.org/sdr/GUUA93852012311A.md): Button · lack of lube · Jan 23, 2011 · N81538 · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED CABIN DOOR RELEASE BUTTON HARD TO PRESS. OPEN. CLEANED AND LUBRICATED INNER AIRSTAIR DOOR RELEASE BUTTON, OPS CHECK OK.
- [SDR GUUA93832122210A](https://openairdocs.org/sdr/GUUA93832122210A.md): Diode · inoperative · Dec 22, 2010 · N81538 · Beech 1900D · Landing Gear Position and Warning
  > DURING APPROACH, LANDING GEAR HANDLE LIGHTS INOPERATIVE. REPLACED DIODE AND SOCKET 14 ON CONNECTOR P200. OPS CHECK SATISFACTORY.
- [SDR GUUA93832120410A](https://openairdocs.org/sdr/GUUA93832120410A.md): Warning Horn · malfunctioned · Dec 4, 2010 · N81538 · Beech 1900D · Landing Gear Position and Warning
  > PILOT REPORTED LANDING GEAR WARNING HORN SOUNDS WITH TORQUE SET AT 2000 LBS. INSPECTED GEAR WARNING SWITCH NO DEFECT NOTED TEST FLIGHT PERFORMED MARKED PEDESTAL. TEST FLIGHT SATISFACTORY.
- [SDR GUUA93857092210A](https://openairdocs.org/sdr/GUUA93857092210A.md): Skin · damaged · Sep 22, 2010 · N81538 · Beech 1900D · Wing, Plate/Skin
  > FLIGHT 5401 PILOT REPORTED BIRD STRIKE ON RIGHT WING. REMOVED DAMAGED SECTION OF SKIN AT RIGHT WING OUTBOARD LEADING WS 189.0 AND INSTALLED A DOUBLER REPAIR AND SKIN FILLER.
- [SDR GUUA93832091310A](https://openairdocs.org/sdr/GUUA93832091310A.md): Annunciator · loose · Sep 13, 2010 · N81538 · Beech 1900D · Landing Gear Position and Warning
  > PILOT REPORTED NOSE GEAR LIGHT INOPERATIVE. PUSHED NOSE GEAR ANNUNCIATOR IN THE SOCKET.
- [SDR GUUA93853082710A](https://openairdocs.org/sdr/GUUA93853082710A.md): Skin · cracked · Aug 27, 2010 · N81538 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING SCHEDULED STRUCTURAL INSP, DISCOVERED CRACK IN SKIN 1.5 INCHES LONG AT APPROX FS 353 STRINGER 16. REMOVED DAMAGED SECTION OF SKIN, INSTALLED INSERTION PATCH AND EXTERNAL DOUBLER REPAIR.
- [SDR GUUA93852082510A](https://openairdocs.org/sdr/GUUA93852082510A.md): Cable · frayed · Aug 25, 2010 · N81538 · Beech 1900D · Entrance Stairs
  > DURING SCHEDULED STRUCTURAL INSP DISCOVERED AIRSTAIR DOOR AFT UPPER AND FORWARD UPPER CONTROL CABLES FRAYED. REPLACED UPPER AFT AND UPPER FORWARD AIRSTAIR DOOR CONTROL CABLES.
- [SDR GUUA93853082410B](https://openairdocs.org/sdr/GUUA93853082410B.md): Angle · cracked · Aug 24, 2010 · N81538 · Beech 1900D · Fuselage Miscellaneous Structure
  > DURING SCHEDULED ROUTINE INSP, DISCOVERED LT HEAVY ANGLE CRACKED AT FS 288 APPROX 1.875 INCHES LONG. STOP DRILLED END OF CRACK AND INSTALLED REPAIR ANGLE,CLIP AND FASTNERS AS REQUIRED.
- [SDR GUUA93853082410D](https://openairdocs.org/sdr/GUUA93853082410D.md): Stringer · corroded · Aug 24, 2010 · N81538 · Beech 1900D · Fuselage Main, Longeron/Stringer
  > DURING SCHEDULED STRUCTURAL INSPECTION DISCOVERED CORROSION AT FS 348 STRINGER 16. REMOVED DAMAGED SECTION OF STRINGER 16, AND INSTALLED NEW SECTION STRINGER SPLICE.
- [SDR GUUA93853082410C](https://openairdocs.org/sdr/GUUA93853082410C.md): Frame · cracked · Aug 24, 2010 · N81538 · Beech 1900D · Fuselage Main, Frame
  > DURING SCHEDULED ROUTINE MX DISCOVERED ASD ANGLE CRACKED AT FS 150 STRINGER 5L APPROX. REMOVED DAMAGED SECTION OF ANGLE AND INSTALLED FRAME ANGLE REPAIR.
- [SDR GUUA93853082410A](https://openairdocs.org/sdr/GUUA93853082410A.md): Stringer · corroded · Aug 24, 2010 · N81538 · Beech 1900D · Fuselage Main, Longeron/Stringer
  > DURING SCHEDULED ROUTINE INSP DISCOVERED CORROSION AT STR 15L APPROX FS 250 TO 258. REMOVED DAMAGED SECTION OF STRINGER 15L,INSTALLED NEW SECTION AND INSTALLED EXTERNAL DOUBLER REPAIR.
- [SDR GUUA93832050410A](https://openairdocs.org/sdr/GUUA93832050410A.md): Handle · inoperative · May 4, 2010 · N81538 · Beech 1900D · Landing Gear Selector
  > DURING FLIGHT WHEN PULLING POWER LEVER TO LESS OR AFT LANDING GEAR HANDLE WILL NOT ILLUMINATE IN FLIGHT OR ON THE GROUND. REPLACED LANDING GEAR HANDLE OPS CK NORMAL.
- [SDR GUUA93853040710A](https://openairdocs.org/sdr/GUUA93853040710A.md): Paint · peeling · Apr 7, 2010 · N81538 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING POST FLIGHT, FOUND PAINT PEELING OFF ON TOP OF ACFT. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED FILLER 4X5 INCHES AND AN EXTERNAL DOUBLER REPAIR.
- [SDR GUUA93861021410A](https://openairdocs.org/sdr/GUUA93861021410A.md): Pressure Switch · failed · Feb 14, 2010 · N81538 · Beech 1900D · Propeller Feathering/Reversing
  > DURING FINAL APPROACH RT ENGINE GOES IN AND OUT OF FEATHER MULTIPLE TIMES. REPLACED AUTOFEATHER HIGH PRESSURE SWITCH.
- [SDR GUUA93856072809A](https://openairdocs.org/sdr/GUUA93856072809A.md): Heater · odor · Jul 28, 2009 · N81538 · Beech 1900D · Windshield/Door Rain/Ice Removal
  > FLIGHT: 9146 TLH/PBI DURING FLIGHT WHEN RIGHT WINDSHIELD HEAT SELECTED A HOT WIRE ODOR NOTICED BY CREW. REPLACED RIGHT WINDSHIELD WIRE H31A8 TREMINAL,INSULATED AND SECURED.OPERATIONAL CHECK NORMAL.
- [SDR GUUA93854041209A](https://openairdocs.org/sdr/GUUA93854041209A.md): Keel · damaged · Apr 12, 2009 · N81538 · Beech 1900D · Nacelle/Pylon, Main Frame
  > LT NACELLE KEEL DAMAGED PREVIOUS REPAIR. AMENDED REPAIR BY BONDING REPAIR DOUBLERS IAW FAA APPROVED DATA.
- [SDR GUUA93832032909A](https://openairdocs.org/sdr/GUUA93832032909A.md): Switch · out of adjust · Mar 29, 2009 · N81538 · Beech 1900D · Power Lever
  > LANDING GEAR WARNING HORN IS ACTIVATED AT 79.5 TO 80 PERCENT, N1 WITH LT POWER LEVER AND 75 PERCENT, N1 WITH RT PWR LEVER. ADJUSTED LANDING GEAR POWER LEVER SWITCHES. TEST FLIGHT SATISFACTORY.
- [SDR GUUA93832020209A](https://openairdocs.org/sdr/GUUA93832020209A.md): Brake Sys · inoperative · Feb 2, 2009 · N81538 · Beech 1900D · Landing Gear Brake System
  > FLIGHT: 9173 EYW/FLL DURING TAXI CAPTAINS RT BRAKE PEDAL GOES TO THE FLOOR, AND CAPTAINS LT BRAKE GETTING 50 PERCENT. RETURNED TO EYW. BLED CAPTAINS AND FIRST OFFICERS LT AND RT BRAKE SYSTEMS. OPS CHECK GOOD.
- [SDR GUUA93832020109A](https://openairdocs.org/sdr/GUUA93832020109A.md): Master Cylinder · malfunctioned · Feb 1, 2009 · N81538 · Beech 1900D · Master Cylinder/Brake Valve
  > FLIGHT: 9171 TPA/MIA DURING TAXI CAPTAINS RIGHT BRAKE GOES FLAT. REPLACED RIGHT BRAKE PEDAL MASTER CYLINDER.
- [SDR GUUA93832122208A](https://openairdocs.org/sdr/GUUA93832122208A.md): Uplock Switch · defective · Dec 22, 2008 · N81538 · Beech 1900D · Landing Gear Position and Warning
  > DURING FLIGHT, LANDING GEAR HORN WILL NOT SILENCE EVEN THOUGH SILENCE BUTTON IS PUSHED. REPLACED LT LANDING GEAR UPLOCK SWITCH. OPS CHECK GOOD.
- [SDR GUUA93853121708A](https://openairdocs.org/sdr/GUUA93853121708A.md): Skin · corroded · Dec 17, 2008 · N81538 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING SCHEDULED ROUTINE MAINT, DISCOVERED SURFACE CORROSION ON FUSELAGE BELLY AT FS 327.630. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED AN EXTERNAL DOUBLER.
- [SDR GUUA93854112308A](https://openairdocs.org/sdr/GUUA93854112308A.md): Keelbeam · cracked · Nov 23, 2008 · N81538 · Beech 1900D · Nacelle/Pylon, Main Frame
  > AT SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT NACELLE KEEL HAS A.75 INCH CRACK. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLERS.
- [SDR GUU2008F00039](https://openairdocs.org/sdr/GUU2008F00039.md): Relay · inoperative · Aug 13, 2008 · N81538 · Beech 1900D · Landing Gear Retraction/Extension System
  > FLIGHT 9225 TPA/JAX, DURING APPROACH NOSE LANDING GEAR RELAY CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER AND RECYCLED GEAR. NOSE GEAR EXTENDED NORMALLY WITH THREE GREEN. REPLACED LANDING GEAR RELAY. OPERATIONAL CHECK NORMAL. (S)
- [SDR GUU2008F00004](https://openairdocs.org/sdr/GUU2008F00004.md): Brake Assy · weak · Jul 5, 2008 · N81538 · Beech 1900D · Landing Gear Brake System
  > AFTER LANDING, CAPTAINS RT BRAKE PEDAL LOST PRESSURE. GRAVITY BLED ALL BRAKES. OPS CHECK GOOD. (K)
- [SDR GUU2008F00009](https://openairdocs.org/sdr/GUU2008F00009.md): Light · loose · Jun 25, 2008 · N81538 · Beech 1900D · Landing Gear Selector
  > FLIGHT 9306, DURING APPROACH LIGHTS IN LANDING GEAR HANDLE INOPERATIVE. SECURED LIGHT ASSEMBLY ON LANDING GEAR HANDLE. (A)
- [SDR 938012108A](https://openairdocs.org/sdr/938012108A.md): Skin · cracked · Jan 21, 2008 · N81538 · Beech 1900D · Fuselage Main, Plate/Skin
  > AT SCHEDULED INSPECTION, DISCOVERED ONE INCH LATERAL CRACK IN FUSELAGE BELLY SKIN IN SPAR AREA AT BL 30.62. STOP DRILLED CRACK AND INSTALLED REINFORCEMENT DOUBLER REF SRM 53-90-18, (FUSELAGE SKIN CRACK REPAIR IN SPAR AREA).
- [SDR GUUA01210801](https://openairdocs.org/sdr/GUUA01210801.md): Skin · cracked · Jan 21, 2008 · N81538 · Beech 1900D · Fuselage Main, Plate/Skin
  > AT SCHEDULED INSPECTION, DISCOVERED A 1.0 INCH CRACK BETWEEN FS 230.75 AND 310.75 AT BL 30.62. STOP DRILLED CRACK AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER IAW SRM 53-90-18.
- [SDR GUUA08210701](https://openairdocs.org/sdr/GUUA08210701.md): Unknown · unknown · Aug 21, 2007 · N81538 · Beech 1900D · Landing Gear System
  > FLIGHT: 9142 MIA/EYW DURING APPROACH, LANDING GEAR CIRCUIT BREAKER POPPED WHEN GEAR HANDLE MOVED TO THE DOWN POSITION. CONTINUED TO EYW LANDED WITHOUT INCIDENT. PERFORMED LANDING GEAR OPERATIONAL CHECK SEVERAL TIMES UNABLE TO DUPLICATE.
- [SDR GUUA08140701](https://openairdocs.org/sdr/GUUA08140701.md): Attach Bracket · corroded · Aug 14, 2007 · N81538 · Beech 1900D · Rudder Structure
  > AT SCHEDULED INSPECTION DISCOVERED TOP RUDDER ATTACH BRACKET EXFOLIATED. REPLACED TOP RUDDER BRACKET.
- [SDR GUUA04170701](https://openairdocs.org/sdr/GUUA04170701.md): Actuator · slow · Apr 17, 2007 · N81538 · Beech 1900D · Landing Gear Actuator
  > FLIGHT: 9167, DURING APPROACH LANDING GEAR WOULD NOT EXTEND. MANUALLY EXTENDED LANDING GEAR. LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR POWER PACK MOTOR AND RT LANDING GEAR ACTUATOR. OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY.
- [SDR GUUA04270601](https://openairdocs.org/sdr/GUUA04270601.md): Switch · malfunctioned · Apr 27, 2006 · N81538 · Beech 1900D · Landing Gear Position and Warning
  > FLIGHT: 9188 VPS/TPA DURING APPROACH UNABLE TO SILENCE LANDING GEAR WARNING HORN. REPLACED LANDING GEAR WARNING SWITCH.
- [SDR GUU2005F00040](https://openairdocs.org/sdr/GUU2005F00040.md): Bracket · corroded · Jul 30, 2005 · N81538 · Beech 1900D · Elevator Miscellaneous Structure
  > AT SCHEDULED INSPECTION, RT ELEVATOR CENTER HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED RT ELEVATOR CENTER HINGE BRACKET. (K)
- [SDR 2005F00081](https://openairdocs.org/sdr/2005F00081.md): Brake Assy · malfunctioned · Apr 17, 2005 · N81538 · Beech 1900D · Landing Gear Brake System
  > RT BRAKE VERY SOFT. REQUIRED EXCESSIVE PUMPING TO CREATE PRESSURE AND INCREASE BRAKE EFFECTIVENESS. BLED LEFT AND RIGHT BRAKES. OPERATIONAL CHECK NORMAL. (M)
- [SDR GUU2005F00011](https://openairdocs.org/sdr/GUU2005F00011.md): Valve · failed · Feb 25, 2005 · N81538 · Beech 1900D · Landing Gear Brake System
  > FLT 9132 - EYW/TPA - DURING TAXI, RIGHT BRAKE LOCKED UP. REMOVED AND REPLACED RIGHT PARKING BRAKE VALVE. (M)
- [SDR GUU2005F00014](https://openairdocs.org/sdr/GUU2005F00014.md): Blade · failed · Feb 16, 2005 · N81538 · Beech 1900D · Turbine Section
  > DURING TAKEOFF ROLL, WITH LT ENGINE AT APPROXIMATELY 1,000 LBS OF TORQUE, UNUSUAL NOISE HEARD. LT ENGINE CEASED. ABORTED TAKEOFF. DETERMINED LT POWER SECTION SEIZED. REMOVED AND REPLACED LT ENGINE ASSEMBLY AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND RE
- [SDR 2005F00054](https://openairdocs.org/sdr/2005F00054.md): Engine · stopped · Feb 16, 2005 · N81538 · Beech 1900D · Engine (Turbine/Turboprop)
  > FLT 9133 - JAX - DURING TAKEOFF ROLL, WITH LEFT ENGINE AT APPROXIMATELY 1,000 LBS OF TORQUE, UNUSUAL NOISE HEARD. LEFT ENGINE CEASED. ABORTED TAKEOFF. DETERMINED LEFT POWER SECTION SEIZED. REMOVED AND REPLACED LEFT ENGINE ASSEMBLY AND ROUTED FAILED UNIT FO
- [SDR GUU2004F00015](https://openairdocs.org/sdr/GUU2004F00015.md): Brake Assy · worn · May 19, 2004 · N81538 · Beech 1900D · Landing Gear Brake System
  > DURING TAXI, RT SIDE BRAKING ACTION NOT ADEQUATE. REMOVED AND REPLACED NR 3 BRAKE ASSEMBLY. BLED BRAKES. OPERATIONAL CHECK NORMAL.
- [SDR GUU2004F00004](https://openairdocs.org/sdr/GUU2004F00004.md): Line · contaminated · May 4, 2004 · N81538 · Beech 1900D · Landing Gear Brake System
  > DURING TAXI, VERY POOR BRAKING ACTION ON RT PEDAL. BLED RT BRAKE SYSTEM. OPS CHECK NORMAL.
- [SDR GUU2004F00012](https://openairdocs.org/sdr/GUU2004F00012.md): Bracket · corroded · Mar 21, 2003 · N81538 · Beech 1900D · Elevator Structure
  > AT SCHEDULED ROUTINE MAINTENANCE, LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LT OB ELEVATOR HINGE BRACKET.
- [SDR GUU2002F00011](https://openairdocs.org/sdr/GUU2002F00011.md): Bolt · loose · May 21, 2002 · N81538 · Beech 1900D · Vertical Stabilizer
  > AT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQUE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM.
- [SDR C2XA01CL155](https://openairdocs.org/sdr/C2XA01CL155.md): Light · dirty · Jun 24, 2001 · N81538 · Beech 1900D · Landing Gear Position and Warning
  > CLE FLIGHT# 3108 THE CREW REPORTED THE NOSE GEAR LIGHT DID NOT ILLUMINATE WHEN THE GEAR WAS EXTENDED.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND CLEANED THE NOSE GEAR LIGHT SOCKET.OPERATIONAL CHECKS WERE GOOD.

Next page: https://openairdocs.org/deregistered/N81538-2013-08-02/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 = 'N81538' AND deregistration_id = 'N81538-2013-08-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N81538-2013-08-02/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.