# Service difficulty reports: N393SW, cancelled Apr 20, 2011

A list on [N393SW, cancelled Apr 20, 2011](https://openairdocs.org/deregistered/N393SW-2011-04-20.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 · 53 reports

- [SDR SWIA201024861](https://openairdocs.org/sdr/SWIA201024861.md): Light · inoperative · Sep 1, 2010 · N393SW · Emb EMB120ER · Emergency Lighting
  > EMERGENCY MAIN CABIN DOOR LIGHT INOPERATIVE. (FLT 6417) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201024442](https://openairdocs.org/sdr/SWIA201024442.md): Light · inoperative · Jun 18, 2010 · N393SW · Emb EMB120ER · Emergency Lighting
  > EMERGENCY LIGHT ON CEILING AT ROW 10 INOP. (FLT 6260) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201024639](https://openairdocs.org/sdr/SWIA201024639.md): Firewall · cracked · May 28, 2010 · N393SW · Emb EMB120ER · Fuselage Main, Bulkhead
  > APU COMPARTMENT FORWARD FIREWALL SKIN IS CRACKED. (C-CHECK) REPAIRED PER SRM.
- [SDR SWIA201023980](https://openairdocs.org/sdr/SWIA201023980.md): Stringer · cracked · Apr 5, 2010 · N393SW · Emb EMB120ER · Wing, Longeron/Stringer
  > LEFT NR 2 FUEL PANEL FORWARD STRINGER IS CRACKED. (C CHECK) REPAIRED STRINGER WITH NEW SPLICE PER SRM.
- [SDR SWIA201023686](https://openairdocs.org/sdr/SWIA201023686.md): Flap · cracked · Feb 10, 2010 · N393SW · Emb EMB120ER · Trailing Edge Flaps
  > LEFT NACELLE FLAP OUTBOARD EDGE CRACKED. (C CHECK) REPLACED FLAP PER AMM.
- [SDR SWIA201023668](https://openairdocs.org/sdr/SWIA201023668.md): Roller · lack of lube · Feb 6, 2010 · N393SW · Emb EMB120ER · Passenger/Crew Doors
  > MAIN DOOR DIFFICULT TO OPEN. (FLT 6838) LUBED ROLLERS ON DOOR FRAME.
- [SDR SWIA201023604](https://openairdocs.org/sdr/SWIA201023604.md): Door · lack of lube · Jan 29, 2010 · N393SW · Emb EMB120ER · Passenger/Crew Doors
  > MAIN DOOR HARD TO OPEN AND CLOSE. (FLT 6195) LUBED DOOR.
- [SDR SWIA200923077](https://openairdocs.org/sdr/SWIA200923077.md): Control Column · obstructed · Nov 9, 2009 · N393SW · Emb EMB120ER · Control Column Section
  > AILERON ROLL CONTROL VERY STIFF. (FLT 6318)REMOVED FOD FROM BETWEEN YOKE AND COLUMN.
- [SDR SWIA200922015](https://openairdocs.org/sdr/SWIA200922015.md): Lamp · burned out · Jul 8, 2009 · N393SW · Emb EMB120ER · Emergency Lighting
  > FLT 6446, FORWARD FLOOR RED EMERGENCY LIGHT INOP. RELAMPED.
- [SDR SWIA200921714](https://openairdocs.org/sdr/SWIA200921714.md): Light · loose · May 30, 2009 · N393SW · Emb EMB120ER · Emergency Lighting
  > FLT 6072 - RED EMERGENCY PATH LIGHTING AT ROW 2 INOP. REPOSITIONED LIGHT.
- [SDR SWIA200819945](https://openairdocs.org/sdr/SWIA200819945.md): Fire Bottle · empty · Aug 8, 2008 · N393SW · Emb EMB120ER · Fire Bottle, Fixed
  > APU FIRE BOTTLE DISCHARGED. FLIGHT 5752. REPLACED APU FIRE BOTTLE ASSEMBLY WITH A SERVICEABLE ASSEMBLY. OPS CHECK GOOD.
- [SDR SWIA200819032](https://openairdocs.org/sdr/SWIA200819032.md): Stringer · cracked · Jan 2, 2008 · N393SW · Emb EMB120ER · Wing, Longeron/Stringer
  > RIGHT WING FUEL PANEL ACCESS HAS A CRACK ON STRINGER 8 BETWEEN FRAMES 8 AND 9. REPAIRED STRINGER IAW SRM 57-20-03.
- [SDR SWIA200819031](https://openairdocs.org/sdr/SWIA200819031.md): Stringer · cracked · Jan 2, 2008 · N393SW · Emb EMB120ER · Wing, Longeron/Stringer
  > RIGHT WING FUEL PANEL ACCESS HAS A CRACK ON STRINGER 10 BETWEEN FRAMES 8 AND 9. REPAIRED CRACKED AFT STRINGER IAW SRM 57-20-03.
- [SDR SWIA200718905](https://openairdocs.org/sdr/SWIA200718905.md): Wheel · broken · Nov 24, 2007 · N393SW · Emb EMB120ER · Wheel/Ski/Float
  > FLT 5552 - DURING POST FLIGHT, NOTICED NR 2 MAIN WHEEL ASSEMBLY APPEARED TO BE BROKEN. REPLACED BOTH LEFT WHEEL ASSEMBLIES, PN 3-1446-1 SN OFF 0538 PN 3-1446-1 SN OFF 777.
- [SDR SWIA200717836](https://openairdocs.org/sdr/SWIA200717836.md): Structure · cracked · Jan 2, 2007 · N393SW · Emb EMB120ER · Passenger/Crew Doors
  > PAX DOOR HAS A CRACK UNDER LOCK FASTENER FWD AND AFT STRINGER NEXT TO 3RD STEP, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CRACKED BRACKETS ON PAX DOOR SECURED IAW EMB 120 SRM 51-40-02.
- [SDR SWIA200717835](https://openairdocs.org/sdr/SWIA200717835.md): Buttstrap · corroded · Jan 2, 2007 · N393SW · Emb EMB120ER · Fuselage Main, Structure
  > FOUND CORROSION AT RIGHT AND CENTER BUTTSTRAPS NEAR LAV AREA, DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT AND CENTER BUTTSTRAPS NEAR LAV AREA IAW SRM 120 51-10-02 PG 3 SEC 3A.
- [SDR SWIA200717834](https://openairdocs.org/sdr/SWIA200717834.md): Buttstrap · corroded · Jan 2, 2007 · N393SW · Emb EMB120ER · Fuselage Main, Structure
  > FOUND CORROSION AT CARGO DOOR ENTRANCE BUTTSTRAP, DISCOVERED DURING C-CHECK INSPECTION. REPLACED BUTTSTRAP AT CARGO DOOR ENTRANCE IAW SRM 120 51-10-02 PG 3 SEC 3A.
- [SDR SWIA200717833](https://openairdocs.org/sdr/SWIA200717833.md): Buttstrap · corroded · Jan 2, 2007 · N393SW · Emb EMB120ER · Fuselage Main, Structure
  > FOUND CORROSION AT PASSENGER DOOR ENTRANCE BUTTSTRAP, DISCOVERED DURING C-CHECK INSPECTION. REPLACED BUTTSTRAP AT PASSENGER DOOR ENTRANCE IAW SRM 51-10-02 PG 3 SEC 3A.
- [SDR SWIA200717832](https://openairdocs.org/sdr/SWIA200717832.md): Frame · cracked · Jan 2, 2007 · N393SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/Rib
  > FOUND LEFT NACELLE FRAME 1 CRACKED AT INBOARD WEB, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW LEFT FRAME NR 1 IAW EMB 120 SRM 51-40-02, SB 120-54-0036 PART II AND RII 54-900-1000.
- [SDR SWIA200617384](https://openairdocs.org/sdr/SWIA200617384.md): Hmu · malfunctioned · Nov 11, 2006 · N393SW · Emb EMB120ER · Fuel Controlling System
  > RIGHT ENGINE SHUTDOWN AFTER LANDING AND EXITING RUNWAY. REPLACED LEFT HMU AND FUEL CONTROL UNIT IAW MM 73-21-00 AND MM 73-13-00. PERFORMED ENGINE RUNS IAW MM 71-00-00. OPERATIONAL CHECKS GOOD, HMU PN: 5009986-C SN OFF: 3116.
- [SDR SWIA200616493](https://openairdocs.org/sdr/SWIA200616493.md): Pulley · binding · Mar 27, 2006 · N393SW · Emb EMB120ER · Aileron Control System
  > PILOT REPORTED SLIGHT DETENT WHEN MOVING AILERONS THROUGH CENTER POSITION. REPLACED RIGHT AILERON WING BOX LOWER PULLEY IAW 27-00-01. REMOVED AILERON AUTOPILOT SERVO AND INSP CLUTCH FOR FREEDOM OF MOVEMENT FOUND GOOD. INSTALLED SERVO, CYCLED AILERONS THROUG
- [SDR SWIA200515690](https://openairdocs.org/sdr/SWIA200515690.md): Actuator · malfunctioned · Oct 16, 2005 · N393SW · Emb EMB120ER · Rudder Control System
  > RIGHT RUDDER JAMS AFTER ROTATION. REPLACED BLUE SYSTEM RUDDER ACTUATOR IAW EMB MM 27-22-00 AND 27-22-02. OPERATIONAL CHECK GOOD.
- [SDR SWIA200515438](https://openairdocs.org/sdr/SWIA200515438.md): Actuator · malfunctioned · Aug 15, 2005 · N393SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > FLAP DISAGREEMENT DURING FLAP RETRACTION ON AFTER LANDING CHECK. "INBD" LIGHTS FLASHING. REPLACED THE LEFT INBOARD FLAP ACTUATOR IAW MM 27-50-07. OPERATIONAL CHECK GOOD.
- [SDR SWIA200515177](https://openairdocs.org/sdr/SWIA200515177.md): Intercostal · cracked · Apr 4, 2005 · N393SW · Emb EMB120ER · Fuselage Miscellaneous Structure
  > CLIP CRACKED AT FRAME 12A JUST AFT LT DV WINDOW, ITEM FOUND AT C-CHECK INSPECTION. REPLACED INTERCOSTAL AT FRAME 12A AFT OF PILOT'S DV WINDOW PER EMB120 SRM 51-40-02.
- [SDR SWIA200414158](https://openairdocs.org/sdr/SWIA200414158.md): Actuator · malfunctioned · Nov 24, 2004 · N393SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > LEFT INBOARD FLAP DROOPS. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR IAW MM 27-50-00. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413992](https://openairdocs.org/sdr/SWIA200413992.md): Wire · chafed · Oct 21, 2004 · N393SW · Emb EMB120ER · Light System Wiring
  > EMERGENCY LIGHT C/B POPS WHEN TESTED. REPAIRED CHAFED WIRE AT EMERGENCY LIGHT BATTERY PACK NR 2. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413802](https://openairdocs.org/sdr/SWIA200413802.md): Actuator · malfunctioned · Sep 10, 2004 · N393SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > RT IB FLAP DOES NOT FULLY RETRACT. REPLACED RT IB FLAP ACTUATOR IAW MM 27-50-07. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413670](https://openairdocs.org/sdr/SWIA200413670.md): Actuator · malfunctioned · Aug 9, 2004 · N393SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > ON TAXI OUT, SELECTED FLAPS 15 DEGREES, THE LT IB FLAP WENT TO 45 DEGREES CAUSING AN ASYMMETRY. REPLACED LT IB FLAP ACTUATOR IAW MM 27-50-00. OPERATIONAL CHECK GOOD.
- [SDR SWIA200412926](https://openairdocs.org/sdr/SWIA200412926.md): Actuator · leaking · Feb 18, 2004 · N393SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > DURING APPROACH INTO MRY GOT A DISAGREEMENT WITH FLAP SELECTOR AT 25 FT THE NACELLE FLAPS WERE AT 0 DEGREES SHORTLY AFTER THE BLUE HYD QUANTITY AND PRESSURE WENT TO 0 AND ASSOCIATED LIGHTS. DIVERTED TO SFO. REPLACED LEAKING LEFT NACELLE FLAP ACTUATOR PER MM
- [SDR SWIA200312607](https://openairdocs.org/sdr/SWIA200312607.md): Wire · chafed · Oct 27, 2003 · N393SW · Emb EMB120ER · Fuel System Wiring
  > LEFT FORWARD FUEL BOOST PUMP HAS CHAFED WIRE. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED LEFT FORWARD FUEL BOOST PUMP IAW MM 28-21-02.
- [SDR SWIA200312554](https://openairdocs.org/sdr/SWIA200312554.md): Computer · malfunctioned · Oct 25, 2003 · N393SW · Emb EMB120ER · Autopilot System
  > AUTOPILOT FAILED WHEN SELECTED TO CAPTAIN'S SIDE. COMPUTER FLAG SHOWING ON CAPTAIN'S ADI. REPLACED CAPTAIN'S AUTOPILOT COMPUTER. OPS CHECK GOOD PER 22-11-00.
- [SDR SWIA200312298](https://openairdocs.org/sdr/SWIA200312298.md): Control Arm · loose · Aug 21, 2003 · N393SW · Emb EMB120ER · Fuel Controlling System
  > LEFT ENGINE DID NOT SHUTDOWN IN FUEL CUT OFF (1ST ATTEMPT). FOUND FUEL CUTOFF SERRATED ARM ON THE HMU TO PCU LOOSE. RETORQUED, SAFETIED AND RAN LT AND RT ENGINES. OPS CHECK GOOD.
- [SDR SWIA200311925](https://openairdocs.org/sdr/SWIA200311925.md): Power Supply · malfunctioned · Apr 29, 2003 · N393SW · Emb EMB120ER · Emergency Lighting
  > EMERGENCY EXIT LIGHTS OPERATE INTERMITTENTLY FROM F/A STATION AND FLIGHT DECK. REMOVED AND REPLACED AFT EMERGENCY LIGHT BATTERY IAW 33-50-00. OPS CHECK OK.
- [SDR SWIA200311924](https://openairdocs.org/sdr/SWIA200311924.md): Computer · malfunctioned · Apr 29, 2003 · N393SW · Emb EMB120ER · Autopilot Computer
  > CAPTAIN'S AUTOPILOT SPONTANEOUSLY DISENGAGES WITH CORRESPONDING RED A/P LIGHTS AND AURAL WARNING. CAPTAIN FLIGHT DIRECTOR AND F/O'S A/P OPERATE NORMALLY. REPLACED NR 1 APC-65B. OPS CHECK GOOD.
- [SDR SWIA200211463](https://openairdocs.org/sdr/SWIA200211463.md): Seal · dirty · Nov 12, 2002 · N393SW · Emb EMB120ER · Passenger/Crew Doors
  > MAIN CABIN DOOR DOES NOT CLOSE. THE RED HANDLES DO NOT MOVE, BUT THE DOOR GOES UP AND DOWN. CLEANED AND LUBRICATED CABIN DOOR SEAL AND LOCKING MECHANISM. OPS CHECKED GOOD.
- [SDR SWIA200211407](https://openairdocs.org/sdr/SWIA200211407.md): Pressure Switch · malfunctioned · Oct 26, 2002 · N393SW · Emb EMB120ER · Engine Oil Pressure
  > NR 1 ENGINE OIL PRESSURE LIGHT ILLUMINATED INFLIGHT FOR 2 MINUTES, WITH NORMAL OIL PRESSURE OF 63 PSID. ALL OTHER INDICATIONS ALSO NORMAL.REMOVED AND REPLACED NR 1 ENGINE LOW OIL PRESSURE SWITCH. CONDUCTED ENGINE RUN. NO LEAKS NOTED. CHECKS GOOD. NO LIGHT
- [SDR SWIA200211116](https://openairdocs.org/sdr/SWIA200211116.md): Actuator · defective · Aug 5, 2002 · N393SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > INBOARD FLAPS ARE CYCLING IN AND OUT 1 TO 2 LIGHT BARS AFTER LANDING WHEN FLAPS ARE RETRACTED. REMOVED & REPLACED RIGHT INBOARD FLAP ACTUATOR. OPS CHECK GOOD AND NO LEAKS NOTED.
- [SDR SWIA200211093](https://openairdocs.org/sdr/SWIA200211093.md): Engine · malfunctioned · Jul 30, 2002 · N393SW · Emb EMB120ER · Engine (Turbine/Turboprop)
  > WHILE EN ROUTE FROM SAN TO LAX, NR 1 ENGINE TORQUE BEGAN TO SURGE AND AIRCRAFT BEGAN TO YAW BACK AND FORTH. FOLLOWED QRH AND SELECT EEC MANUAL PER QRH. FOUR TO FIVE MINUTES LATER NR 1 ENGINE BEGAN TO SURGE AGAIN WITH WIDER PARAMETER SWINGS. ELECTRONIC FUEL
- [SDR SWIA200211051](https://openairdocs.org/sdr/SWIA200211051.md): Hmu · failed · Jul 13, 2002 · N393SW · Emb EMB120ER · Fuel Controlling System
  > AFTER START OF TAKEOFF ROLL, AURAL WARNING ENGINE CONTROL SOUNDED. REMOVED AND REPLACED LT HMU IAW EMB 120 MM 73-21-00. OPS CHECK GOOD.
- [SDR SWIA200211041](https://openairdocs.org/sdr/SWIA200211041.md): Governor · malfunctioned · Jul 11, 2002 · N393SW · Emb EMB120ER · Propeller Governor
  > LEFT ENGINE DID NOT ACCELERATE ABOVE 90 PERCENT NP ON TAKEOFF. ABORTED T/O. RAN UP ENGINES W/EEC ON & OFF WITH SIMILAR RESULTS. REMOVED AND REPLACED LT OVERSPEED GOVERNOR IAW HS 61-22-00. OPS CHECKS GOOD.
- [SDR SWIA200210705](https://openairdocs.org/sdr/SWIA200210705.md): Pcu · malfunctioned · Feb 28, 2002 · N393SW · Emb EMB120ER · Propeller Controlling System
  > NP AND TQ FLUCTUATE IN CLIMB AND ON APPROACH ON ENGINE NR 1. TQ 2 PERCENT, NP 0.8 PERCENT. INSTALLED SERVICEABLE LEFT PCU IAW MM 61-21-00. OPS CHECK GOOD. NO TORQUE FLUCTUATIONS OR LEAKS NOTED.
- [SDR SWIA200210686](https://openairdocs.org/sdr/SWIA200210686.md): Warning System · malfunctioned · Feb 28, 2002 · N393SW · Emb EMB120ER · Propeller Indication System
  > ABORTED TAKEOFF DUE TO AUTOFEATHER AURAL WARNING. STATIC TAKEOFF WAS ATTEMPTED WITH AUTOFEATHER ARMED AND THE POWER LEVERS ADVANCED AS QUICKLY AS POSSIBLE. PERFORMED EXTENSIVE GROUND RUNS OF BOTH ENGINES WITH EEC'S ON AND OFF. COULD NOT DUPLICATE AUTOFEATHE
- [SDR SWIA200210652](https://openairdocs.org/sdr/SWIA200210652.md): Sensor · reads high · Feb 13, 2002 · N393SW · Emb EMB120ER · Engine RPM Indicating System
  > LEFT EEC IS INOP. HOOKED UP EEC BREAKOUT BOX, FOUND NH SENSOR READING HIGH. REMOVED AND REPLACED LEFT NH SENSOR WITH A SERVICEABLE UNIT. TRIMMED LEFT ENGINE. OPS CHECK GOOD. NO LEAKS NOTED AT THIS TIME.
- [SDR SWIA200210624](https://openairdocs.org/sdr/SWIA200210624.md): Warning System · malfunctioned · Feb 4, 2002 · N393SW · Emb EMB120ER · Engine Fuel Indicating System
  > EEC AURAL WARNING ON TAKEOFF ROLL. ABORTED PER SOP. INSPECTED BOTH EEC SYSTEMS. RAN AIRCRAFT. EEC'S OPERATED NORMALLY AT VARIOUS POWER SETTINGS. NO DISCREPANCIES NOTED. OPS CHECK GOOD.
- [SDR SWIA200210500](https://openairdocs.org/sdr/SWIA200210500.md): Connector · loose · Jan 2, 2002 · N393SW · Emb EMB120ER · Fuel Control/Turbine Engines
  > AT BEGINNING OF TAKEOFF ROLL, NR 1 EEC FAILED. WHITE 'MAN' LIGHT, RED `EEC` LIGHT AND AURAL WARNING SOUNDED. ABORTED TAKEOFF. FOUND LOOSE CANNON PLUG TO 1.8 SENSOR. CLEANED, OHM'S CHECKED AND TIGHTENED CANNON PLUG. ALSO OHM'S CHECKED NH & NP SENSORS AND E
- [SDR SWIA200110264](https://openairdocs.org/sdr/SWIA200110264.md): Bushing · stiff · Oct 23, 2001 · N393SW · Emb EMB120ER · Control Column Section
  > AILERONS ARE VERY STIFF OUT OF NEUTRAL POSITION. PULLED AILERON DISCONNECT AND DETERMINED THE STIFFNESS IS COMING FROM THE F/O'S SIDE. REMOVED AND REPLACED BOTH BUSHINGS IN RIGHT AILERON CONTROL COLUMN IAW 27-11-01. RERIGGED COCKPIT LOOP IAW 27-10-01. OPS
- [SDR SWIA200110196](https://openairdocs.org/sdr/SWIA200110196.md): Engine · malfunctioned · Sep 21, 2001 · N393SW · Emb EMB120ER · Engine (Turbine/Turboprop)
  > ON CLIMB OUT OF SEA, 100 PERCENT NP & 84 PERCENT TQ, NP FLUCTUATIONS NOTED ON NR 2 ENGINE. NP SWIFTLY OSCILLATED BETWEEN 96 PERCENT TO 100.5 PERCENT, ACCOMPANIED WITH YAWING. PROP SYNC DESELECTED HAD NO EFFECT. TORQUE FLUCTUATIONS WERE APPROXIMATELY 2-3 PER
- [SDR SWIA200110110](https://openairdocs.org/sdr/SWIA200110110.md): Governor · leaking · Aug 19, 2001 · N393SW · Emb EMB120ER · Propeller Governor
  > OIL PRESSURE DROPPED IN FLIGHT. ALTERNATE LANDING IN SNA.FOUND OIL LEAKING FROM OVERSPEED GOVERNOR. REPLACED OVERSPEED GOVERNOR. PERFORMED OPS AND LEAK CHECK. OPS CHECK GOOD. NO LEAKS NOTED.
- [SDR SWIA971860](https://openairdocs.org/sdr/SWIA971860.md): Strap · broken · Jun 30, 2000 · N393SW · Emb EMB120ER · Nose/Tail Landing Gear
  > AFTER TAKEOFF AND GEAR RETRACTION ALOUD RATTLE (ALMOST KNOCKING) CAN BE HEARD FROM UNDER CENTER CONSOLE AND NOSE RETURNED TO SFO. REPAIRED BROKEN BONDING STRAP ON NOSE GEAR.
- [SDR SWIA971859](https://openairdocs.org/sdr/SWIA971859.md): Rccb · malfunctioned · Jun 29, 2000 · N393SW · Emb EMB120ER · DC Generating System
  > AFTER TAKEOFF AND GEAR UP A LOUD RAPID KNOCKING FROM UNDER NOSE OF AC INCREASE IN SPEED NOISE LOUDER ALONG WITH KNOCKING. THE OPPOSITE EFFECT WITH DECREASE IN SPEED WITH GEAR DOWN NOISE AND KNOCKING STOPPED. JACKED AC AND SWUNG GEAR, FOUND GASPER FAN RCCB C

Next page: https://openairdocs.org/deregistered/N393SW-2011-04-20/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 = 'N393SW' AND deregistration_id = 'N393SW-2011-04-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N393SW-2011-04-20/reports

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