# Service difficulty reports: N137H, cancelled Jul 19, 2005

A list on [N137H, cancelled Jul 19, 2005](https://openairdocs.org/deregistered/N137H-2005-07-19.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR SWIA200211212](https://openairdocs.org/sdr/SWIA200211212.md): Valve · malfunctioned · Sep 7, 2002 · N137H · Emb EMB120RT · APU Bleed Air System
  > APU CAUSES SMOKE IN COCKPIT & CABIN. FOUND LCV NOT OPENING CAUSING SMELL TO COME FROM PACKS. REPLACED APU LCV, OPS CHECK GOOD.
- [SDR SWIA200210789](https://openairdocs.org/sdr/SWIA200210789.md): Actuator · failed · Apr 16, 2002 · N137H · Emb EMB120RT · Trailing Edge Flap Actuator
  > DURING TAXI FLAPS WOULD NOT SET TO 15 DEGREES. RECEIVED A CONTROL FAULT MESSAGE FOR THE OUTBOARD FLAPS. INSTALLED SERVICEABLE OUTBOARD FLAP ACTUATOR (RIGHT) IAW MM 27-50-00. OPS CHECK GOOD.
- [SDR SWIA200210745](https://openairdocs.org/sdr/SWIA200210745.md): Relay · faulty · Mar 20, 2002 · N137H · Emb EMB120RT · Propeller Feathering/Reversing
  > ON ROTATION AT SJC RECEIVED AN AURAL WARNING TAKEOFF AUTO FEATHER. ABORTED TAKEOFF. FOUND K0161 RELAY TO BE SLOW. INSTALLED NEW RELAY AND OPERATED SYSTEM. OPS CHECKS GOOD AT THIS TIME.
- [SDR SWIA200210737](https://openairdocs.org/sdr/SWIA200210737.md): Control Valve · malfunctioned · Mar 15, 2002 · N137H · Emb EMB120RT · Airfoil Anti/De-ice System
  > INBOARD LEFT AND RIGHT STABILIZER DEICE AND INBOARD LEFT AND RIGHT WING DEICE REPEATEDLY FAIL ON BOTH TIMERS. RETURNED TO PDX. REMOVED AND REPLACED EJECTOR FLOW CONTROL VALVE IAW MM 30-20-04. OPS CHECKS GOOD.
- [SDR SWIA200210693](https://openairdocs.org/sdr/SWIA200210693.md): Relay · failed · Feb 27, 2002 · N137H · Emb EMB120RT · Central Warning
  > ON TAKEOFF ROLL, AMBER APU LIGHT AND AMBER POWER OFF LIGHT ILLUMINATED AND LEFT TORQUE GAUGE DROPPED TO ZERO. REPLACED RELAYS K129, K149, CB0266 AND WIRE W200-0214-24 WITH SERVICEABLE UNITS. RAN ENGINES. OPS CHECKS GOOD. NO DISCREPANCIES NOTED AT THIS TIME
- [SDR SWIA200210666](https://openairdocs.org/sdr/SWIA200210666.md): Relay · failed · Feb 25, 2002 · N137H · Emb EMB120RT · Electrical Power System
  > TEN MINUTES AFTER TAKEOFF, RIGHT TORQUE DROPPED TO ZERO AND POWER OFF AND APU LIGHT ILLUMINATED ON ANNUNCIATOR PANEL. APU WAS OFF. RETURNED TO SBA. REPLACED RELAY K0397 WITH SERVICEABLE UNIT. RAN AIRCRAFT FOR 45 MINUTES. OPS CHECK GOOD AT THIS TIME.
- [SDR SWIA200210633](https://openairdocs.org/sdr/SWIA200210633.md): Fcu · faulty · Feb 8, 2002 · N137H · Emb EMB120RT · Trailing Edge Flap Control System
  > CREW REPORTS OUTBOARD FLAPS DO NOT RETRACT WITH ASSOCIATED DISAGREEMENT. REMOVED AND REPLACED FCU AND ANNUNCIATOR. OPS CHECK GOOD IAW MM 27-50-05 & 27-50-06. (FCU) S/N OFF 0255. (ANNUNCIATOR) P/N ON 306900-1017, S/N OFF 0142.
- [SDR SWIA200210546](https://openairdocs.org/sdr/SWIA200210546.md): Flap · malfunctioned · Jan 5, 2002 · N137H · Emb EMB120RT · Trailing Edge Flap Control System
  > UPON SELECTING FLAPS TO 45 DEGREES, THE OUTBOARD FLAPS WENT TO 25 DEGREES ONLY. RECEIVED A FLAP DISAGREEMENT. FOLLOWED QRH PROCEDURE AGAIN, FLAP DISAGREEMENT. DIVERTED FROM SBP TO SMX. RESET FLAP ANNUNCIATOR. INSPECTED FLAPS, ROLLERS AND TRACKS, FOUND TO
- [SDR SWIA200110449](https://openairdocs.org/sdr/SWIA200110449.md): Computer · malfunctioned · Dec 14, 2001 · N137H · Emb EMB120RT · Integrated Flight System
  > CAPTAIN'S ADI WENT BLANK INTERMITTENTLY WITH ATT FLAG, SIMULTANEOUSLY A/P FAILED WITH RED FAILURE CAPTIONS ON CAPTAIN'S FCP AND AUTOPILOT PANEL WITH ASSOCIATED AUTOPILOT FAIL FLAG ON MAP. DIVERTED TO OXR IN VMC CONDITIONS 2255 Z. REINITIALIZED NR 1 AHARS. C
- [SDR SWIA200110248](https://openairdocs.org/sdr/SWIA200110248.md): Angle · cracked · Sep 6, 2001 · N137H · Emb EMB120RT · Fuselage, Stabilizer Attach Fittings
  > CRACK AND PULLED RIVET IN VERTICAL STABILIZER TO EMPENNAGE SUPPORT ANGLE LEFT SIDE. REPLACED LEFT L-FORWARD PROFILE PER PART II OF SB 120-053-0074 AND EMBRAER AUTHORIZATION GST-3216/01. P/N: SB120-53-0074 KIT 1.
- [SDR SWIA200110247](https://openairdocs.org/sdr/SWIA200110247.md): Shear Tie · cracked · Sep 6, 2001 · N137H · Emb EMB120RT · Fuselage Main, Structure
  > FORMER CRACKED JUST AFT OF PILOT'S DIRECT VISION WINDOW AFT CENTER. REMOVED AND REPLACED CRACKED BRACKET WITH NEW SERVICEABLE BRACKET OF SAME P/N FOR THIS LOCATION. ALL WORK PERFORMED IN ACCORDANCE WITH THE SRM 51-70-00. ALL CHECKS GOOD. P/N: 120-12545-00
- [SDR SWIA20019996](https://openairdocs.org/sdr/SWIA20019996.md): Brake Assy · failed · Jul 2, 2001 · N137H · Emb EMB120RT · Master Cylinder/Brake Valve
  > NR 2 BRAKE LOCKED UPON LANDING. REPLACED NR 2 BRAKE ASSEMBLY, ALSO BRAKE CONTROL VALVE. AIRCRAFT RESTORED TO NORMAL. ALL CHECKS GOOD.
- [SDR SWIA972645](https://openairdocs.org/sdr/SWIA972645.md): Annunciator · failed · Jun 18, 2001 · N137H · Emb EMB120RT · Trailing Flap Position Indicating System
  > ON CLIMB OUT FLAP ASYMMETRY AND CONTROL FAULT. FLAP HANDLE WAS IN UP POSITION. ALL PAIRS SHOWED IN DOWN POSITION. COMMAND BAR SHOWED DOWN. RETURNED TO FIELD. REPLACED FLAP ANNUNCIATOR IAW MM 27-50-05. OPS CHECK GOOD ON GROUND. P/N: 306900-1005 S/N ON:
- [SDR SWIA972634](https://openairdocs.org/sdr/SWIA972634.md): Handle · malfunctioned · Jun 14, 2001 · N137H · Emb EMB120RT · Trailing Edge Flap Control System
  > DURING CLIMB WITH FLAPS UP, WE GOT A FLAP/ADVANCED SWS ON MAP, WITH ASSYMETRY AND CONTROL FAULT, ALL LIGHT BARS INDICATING FULL FLAPS AND NOT FLASHING. FOLLOWED QRH PROCEDURES AND RESET. INSTALLED SERVICEABLE FLAP SELECT HANDLE, FLAPS CHECK GOOD 27-50-00. SN
- [SDR SWIA972613](https://openairdocs.org/sdr/SWIA972613.md): Annunciator · malfunctioned · Jun 3, 2001 · N137H · Emb EMB120RT · Trailing Flap Position Indicating System
  > FLAP DISAGREEMENT ON TAKEOFF, DURING RETRACTION. REPLACED FLAP ANNUNCIATOR UNIT PER MM 27-50-00. OPS CHECK GOOD ON GROUND. P/N: 306900-1017, S/N ON: 0010, S/N OFF: 0217. CHANGED ALL WORN FLAP ROLLERS (8) AND FLAP TRACKS (3). REPLACED RIGHT INBOARD FLAP
- [SDR SWIA972576](https://openairdocs.org/sdr/SWIA972576.md): Fastener · loose · May 9, 2001 · N137H · Emb EMB120RT · Fluid Service Doors
  > ABORTED TAKEOFF FOR RED DOOR LIGHT ON MAP AND SERVICE DOOR ON AT 80 KIAS. INBOARD FUEL SERVICE DOOR AFT FASTENER CAME LOOSE. SECURED FASTENER. OPS CHECKS GOOD.
- [SDR SWIA972439](https://openairdocs.org/sdr/SWIA972439.md): Flap Track · dirty · Mar 14, 2001 · N137H · Emb EMB120RT · Trailing Edge Flaps
  > FLAP DISAGREEMENT IN FLIGHT DURING FLAP RETRACTION. FOUND FLAP TRACKS AND ROLLERS DIRTY. CLEANED ALL TRACKS AND ROLLERS. OPERATED FLAPS NUMEROUS TIMES. OPS CHECK GOOD AT THIS TIME.
- [SDR SWIA972388](https://openairdocs.org/sdr/SWIA972388.md): Servo · worn · Feb 19, 2001 · N137H · Emb EMB120RT · Autopilot Main Servo
  > E002 INSPECTION - RIGHT YOKE MAKES GRINDING NOISE WHEN PULLED BACK (ELEVATOR SERVO CLUTCH) CONTROLS DISCONNECTED. FOUND ELEVATOR SERVO TO BE WORN TO LIMITS. REMOVED AND REPLACED ELEVATOR SERVO IAW MM 22-10-05 PG 6. PERFORMED INSPECTION IAW MM 22-10-05 PAGE
- [SDR SWIA972324](https://openairdocs.org/sdr/SWIA972324.md): Annunciator · malfunctioned · Feb 2, 2001 · N137H · Emb EMB120RT · Trailing Flap Position Indicating System
  > FLAP DISAGREEMENT AFTER FLAP RETRACTION AFTER TAKEOFF. DIVERTED TO FAT FROM MOD. REPLACED FLAP ANNUNCIATOR UNIT. OPS CHECK GOOD IAW EMB 120 MM 27-50-05. P/N ON 306900-1005, S/N ON 0212, P/N OFF 306900-1017, S/N OFF 0155.
- [SDR SWIA972158](https://openairdocs.org/sdr/SWIA972158.md): Relay · failed · Dec 10, 2000 · N137H · Emb EMB120RT · Landing Gear Selector
  > AFTER TAKE OFF FROM SBP THERE WAS A HEAVY VIBRATION FROM THE NOSE LANDING GEAR AREA. RETURNED TO SBP. PERFORMED NUMEROUS GEAR SWINGS AND FOUND GEAR DOORS WOULD ONLY CLOSE WHEN UP AND LOCKED HALF OF THE TIME. REMOVED AND REPLACED LANDING GEAR RELAY BOX IAW
- [SDR SWIA972058](https://openairdocs.org/sdr/SWIA972058.md): Window · out of adj · Oct 26, 2000 · N137H · Emb EMB120RT · Flight Compartment Windows
  > CAPTAINS DV WINDOWN WILL NOT OPEN. ADJUSTED CAPTAINS DV WINDOW IAW MM 52-22-01. OPS CHECKS NORMAL.
- [SDR SWIA972958](https://openairdocs.org/sdr/SWIA972958.md): Window · out of adj · Oct 26, 2000 · N137H · Emb EMB120RT · Flight Compartment Windows
  > CAPTAINS DV WINDOW WILL NOT OPEN. ADJUSTED CAPTAINS DV WINDOW IAW MM 52-22-01. OPS CHECKS NORMAL.
- [SDR SWIA971733](https://openairdocs.org/sdr/SWIA971733.md): Proximity Switch · failed · Mar 13, 2000 · N137H · Emb EMB120RT · Landing Gear Position and Warning
  > RETRACTING GEAR RED B NOSE AND GREEN B NOSE REMAIN ILLUMINATED. RETURNED TO FAT. INSPECTED NLG SYSTEM FORWARD PROXIMITY SENSORS AND FOUND THEM ADJUSTED WITHIN LIMITS AND UNABLE TO DUPLICATE DISCREPANCY. REPLACED LANDING GEAR RELAY BOX AS A PRECAUTION. (P/
- [SDR SWIA971606](https://openairdocs.org/sdr/SWIA971606.md): Switch · out of adjust · Nov 17, 1999 · N137H · Emb EMB120RT · Door Warning System
  > SERVICE DOOR LIGHT CAME ON AT ROTATION. RETURNED TO FIELD. FOUND OUTBOARD FUEL SERVICE DOOR SWITCH OUT OF ADJUSTMENT. ADJUSTED MICROSWITCH, OPS CHECK GOOD.
- [SDR SWIA971590](https://openairdocs.org/sdr/SWIA971590.md): Switch · out of adjust · Nov 1, 1999 · N137H · Emb EMB120RT · Door Warning System
  > SERVICE DOOR LIGHT ILLUMINATED AFTER TAKEOFF. RETURNED TO PDX. ADJUSTED SINGLE POINT REFUELING DOOR MICROSWITCH AS NECESSARY. LIGHT OPS CHECKS GOOD.
- [SDR SWIA971416](https://openairdocs.org/sdr/SWIA971416.md): Boot · failed · Feb 28, 1999 · N137H · Emb EMB120RT · Air Intake Anti/De-Ice System
  > RIGHT ENGINE AIR INLET DEICE BOOT FAILED IN FLIGHT. RETURNED TO PDX. SHOP AIR TESTED GOOD FROM BOTH AIR INPUTS. SWAPPED PRESSURE SWITCHES FROM LEFT TO RIGHT AND INSTALLED NEW TIMER FOR RIGHT INLET BOOT IAW MM 30-20-05. OPS CHECKS GOOD ON GROUND.
- [SDR COMA9810051](https://openairdocs.org/sdr/COMA9810051.md): Lamp · failed · Feb 27, 1998 · N137H · Emb EMB120RT · Emergency Lighting
  > ONE LAMP INOP AT FORWARD EMERGENCY FLOOR PATH LIGHTING. REPLACED LAMP.
- [SDR COMA9810045](https://openairdocs.org/sdr/COMA9810045.md): Ecu · malfunctioned · Feb 10, 1998 · N137H · Emb EMB120RT · Fuel Control/Turbine Engines
  > THE RIGHT PROPELLER RPM FLUCTUATED BETWEEN 100 AND 102.5 PERCENT AFTER TAKEOFF. DEFERRED THE RIGHT ENGINE ELECTRONIC CONTROL SYSTEM. AIRCRAFT RETURNED TO SERVICE.
- [SDR COMA9810035](https://openairdocs.org/sdr/COMA9810035.md): Actuator · malfunction · Jan 30, 1998 · N137H · Emb EMB120RT · Trailing Edge Flap Actuator
  > FLAP CONTROL FAULT WARNING. REPLACED THE LEFT HAND INBOARD FLAP ACTUATOR.
- [SDR COMA9810017](https://openairdocs.org/sdr/COMA9810017.md): Light · inoperative · Jan 6, 1998 · N137H · Emb EMB120RT · Emergency Lighting
  > RIGHT AFT EXTERIOR EMERGENCY LIGHT IS INOP. REPLACED LIGHT ASSY.
- [SDR COMA9710419](https://openairdocs.org/sdr/COMA9710419.md): Wire · shorted · Sep 28, 1997 · N137H · Emb EMB120RT · Overheat Detection
  > AVIONICS BAY OVERHEAT WARNING ON. REPAIRED OVERTEMP SENSOR WIRING (P/N W012-0203-20).
- [SDR COMA9710342](https://openairdocs.org/sdr/COMA9710342.md): Wire · overheated · Aug 2, 1997 · N137H · Emb EMB120RT · Electrical Power System Wiring
  > DURING SCHEDULED MAINTENANCE, BEHIND THE AIRCRAFTS MAIN CIRCUIT BREAKER PANEL, 35 CIRCUIT BREAKER WIRES WERE DISCOVERED WITH EVIDENCE OF OVERHEATING. REPLACED OVERHEATED WIRES AND TERMINAL ENDS.
- [SDR COMA9710272](https://openairdocs.org/sdr/COMA9710272.md): Eadi · malfunction · May 17, 1997 · N137H · Emb EMB120RT · Attitude Gyro and Indicating System
  > PILOTS EAD1 AND EHS1 HAVE NO BACKGROUND COLOR AND RED ATT AND HDG FLAPS. REPLACED THE NR 1 AHC-85.
- [SDR COMA9710188](https://openairdocs.org/sdr/COMA9710188.md): Relay Box · malfunctioned · Mar 24, 1997 · N137H · Emb EMB120RT · Landing Gear Retraction/Extension System
  > LANDING GEAR DID NOT RETRACT WHEN SELECTED UP AFTER TAKE OFF. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE LANDING GEAR RELAY BOX FOR TROUBLESHOOTING.
- [SDR COMA9610252](https://openairdocs.org/sdr/COMA9610252.md): Sensor · defective · Aug 21, 1996 · N137H · Emb EMB120RT · Landing Gear Position and Warning
  > THE RT MLG DOWN LOCK LIGHT REMAINED ON AFTER GEAR RETRACTION. REPLACED DEFECTIVE DOWN LOCK PROXIMITY SENSOR.
- [SDR COMA9610235](https://openairdocs.org/sdr/COMA9610235.md): Skin · corroded · Jul 31, 1996 · N137H · Emb EMB120RT · Fuselage Main, Plate/Skin
  > DURING INSPECTION, FOUND LOWER FUSELAGE SKIN TO BE CORRODED AT FRAME 22 BETWEEN STRINGERS 20 LT AND 20 RT, CUT OUT CORRODED AREA OF LOWER FUSELAGE SKIN FABRICATED AND INSTALLED A SERVICEABLE FILLER AND DOUBLER REPAIR. ALL WORK WAS DONE I/A/W EMB 120 S.B. 120-
- [SDR COMA9610087](https://openairdocs.org/sdr/COMA9610087.md): Seal · worn · Feb 20, 1996 · N137H · Emb EMB120RT · Cabin Cooling System
  > LEFT DUCT LEAK WARNING ILLUMINATED DURING FLIGHT. REPLACED WORN HEAT EXCHANGER SEAL.
- [SDR COMA9512028](https://openairdocs.org/sdr/COMA9512028.md): Potentiometer · defective · Dec 15, 1995 · N137H · Emb EMB120RT · Landing Gear Steering System
  > NOSE WHEEL STEERING IS ERRATIC AND PULLS HARD TO THE RIGHT. REPLACED THE FEED BACK POTENTIOMETER BOX.
- [SDR COMA9512023](https://openairdocs.org/sdr/COMA9512023.md): Manifold Assy · defective · Dec 12, 1995 · N137H · Emb EMB120RT · Landing Gear Steering System
  > NOSE WHEEL STEERING IS JERKY, DRIFTS TO ONE SIDE AND THEN JERKS BACK. ABNORMAL AMOUNT OF LEFT RUDDER REQUIRED FOR TAKEOFF. REPLACED THE NEW MANIFOLD ASSY.
- [SDR COMA9511975](https://openairdocs.org/sdr/COMA9511975.md): Tube Assy · cracked · Sep 27, 1995 · N137H · Emb EMB120RT · Aircraft Fuel Distribution System
  > FUEL LEAKING FROM LT ENGINE NACELLE. REPLACED CRACKED VENT VALVE FLOW LINE IN LT NACELLE.
- [SDR COMA9511959](https://openairdocs.org/sdr/COMA9511959.md): Fuel Heater · cracked · Sep 7, 1995 · N137H · Emb EMB120RT · Fuel Heater
  > FUEL LEAKING FROM RIGHT ENGINE NACELLE. REMOVED AND REPLACED RIGHT ENGINE FUEL HEATER WITH SERVICEABLE UNIT.
- [SDR COM11957](https://openairdocs.org/sdr/COM11957.md): Separator · broken · Aug 31, 1995 · N137H · Emb EMB120RT · Airfoil Anti/De-ice System
  > NR 2 ENGINE DUCT LEAK WARNING CAME ON DURING CLIMB, AIRCRAFT RETURNED TO MCO. REPLACED BROKEN WING DE-ICE BLEED AIR WATER SEPARATOR.
- [SDR COM11926](https://openairdocs.org/sdr/COM11926.md): Wheel Half · cracked · Jul 7, 1995 · N137H · Emb EMB120RT · Wheel/Ski/Float
  > WHEEL S/N 1566 WAS REMOVED FROM AIRCRAFT 1137 LEFT OUTBOARD GEAR, DUE TO THE TIRE BEING WORN TO LIMITS. WHEEL ASSY CAME THROUGH MCO TIRE SHOP. WHEEL WAS DUE EDDY CURRENT, UPON EDDY CURRENT ON WHEEL, FOUND A 2 INCH CRACK ON BEAD SEAT ON INNER WHEEL HALF. SEN
- [SDR COM11914](https://openairdocs.org/sdr/COM11914.md): Fuel Heater · leaking · Jun 11, 1995 · N137H · Emb EMB120RT · Engine Fuel/Oil Cooler
  > RT ENGINE IS LEAKING FUEL. REPLACED THE ENGINE FUEL HEATER.
- [SDR COM11908](https://openairdocs.org/sdr/COM11908.md): Thermostat · defective · May 30, 1995 · N137H · Emb EMB120RT · Cabin Cooling System
  > LEFT DUCT OVERHEAT WARNING ON. REPLACED THE LEFT DUCT THERMOSTAT.
- [SDR COM11829](https://openairdocs.org/sdr/COM11829.md): Fuel Flow Trans · defective · Mar 19, 1995 · N137H · Emb EMB120RT · Fuel Flow Indicating
  > RT ENGINE FUEL FLOW INDICATION FAILED DURING TAKEOFF. REPLACED FUEL FLOW TRANSMITTER.
- [SDR COM11771](https://openairdocs.org/sdr/COM11771.md): Frame · cracked · Feb 12, 1995 · N137H · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/Rib
  > DURING INSPECTION, FOUND RIGHT NACELLE HALF FRAME P/N 120-07881-004 TO BE CRACKED. REPAIRED PER EMB SRM. INSTALLED PER AERODESIGN REPORT NR 661-13 DATED 2-12-95.
- [SDR COM11770](https://openairdocs.org/sdr/COM11770.md): Frame · cracked · Feb 11, 1995 · N137H · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/Rib
  > DURING INSPECTION FOUND RIGHT NACELLE OUTBOARD HALF FRAME P/N 120-39739-002 TO BE CRACKED. REMOVED FRAME AND INSTALLED SERVICEABLE HALF FRAME P/N 120-48439-002. ORIGINAL FRAME THICKNESS 15.032 INCH NEW FRAME 15.040 INCH INSTALLED AS PER EMB 120 SRM AND AEROD
- [SDR COM11755](https://openairdocs.org/sdr/COM11755.md): Potentiometer · defective · Jan 30, 1995 · N137H · Emb EMB120RT · Landing Gear Steering System
  > COPILOTS NWS IS INOP. AIRCRAFT VEERS HARD LEFT. REPLACED THE NWS FEEDBACK POTENTIOMETER.
- [SDR COM11726](https://openairdocs.org/sdr/COM11726.md): Seal · leaking · Jan 9, 1995 · N137H · Emb EMB120RT · Turbine Engine Oil System
  > FLUID LEAKING FROM LEFT ENGINE. REPLACED THE CENTRIFUGAL BREATHER CARBON SEAL.

## 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 = 'N137H' AND deregistration_id = 'N137H-2005-07-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N137H-2005-07-19/reports

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