# Service difficulty reports: N488AA, cancelled Sep 6, 2019

A list on [N488AA, cancelled Sep 6, 2019](https://openairdocs.org/deregistered/N488AA-2019-09-06.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 3 · 121 reports

- [SDR AALA20170103016](https://openairdocs.org/sdr/AALA20170103016.md): Swivel · detached · Dec 30, 2016 · N488AA · Doug DC982 · Emergency Equipment
  > AIRCRAFT NOT GROUNDED. R1 DOOR GIRT BAR IS NOT CONNECTED TO THE SLIDE COVER. RECONNECTED THE GIRT BAR SWIVEL TO SLIDE COVER IAW AMM 25-62-00. OPERATIONAL CHECK GOOD.
- [SDR AALA20161209007](https://openairdocs.org/sdr/AALA20161209007.md): Battery · faulted · Dec 8, 2016 · N488AA · Doug DC982 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHTS AT ROWS 23 THROUGH 27 CAME ON WITH EMERGENCY LIGHT SWITCH AND BATTERY OFF. AIRCRAFT GROUNDED. REMOVED AND REPLACED BATTERY ASSEMBLY B5-106 IAW AMM 33-53-00. OPERATIONAL CHECKED GOOD.
- [SDR AALA20161207013](https://openairdocs.org/sdr/AALA20161207013.md): Battery · faulty · Dec 6, 2016 · N488AA · Doug DC982 · Emergency Lighting
  > AIRCRAFT GROUNDED. OVERHEAD EMERGENCY EXIT LIGHTS ROW 23 THROUGH 27 COME ON WITH BATTERY SWITCH IN THE OFF POSITION. REMOVED AND REPLACED BATTERY ASSEMBLY IAW AMM 33-53-00. OPERATIONAL CHECK GOOD.
- [SDR AALA20161003003](https://openairdocs.org/sdr/AALA20161003003.md): Battery Pack · inoperative · Oct 1, 2016 · N488AA · Doug DC982 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHTS AT ROW 30 AND AFT GALLEY COME ON WITH ALL POWER REMOVED FROM AIRCRAFT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY ASSEMBLIES AT ROWS 25 AND 29 IAW AMM 33-53-00. OPERATIONAL CHECK GOOD IAW AMM 33-53-00. SEE ALSO AALA20161001003.
- [SDR AALA20161001003](https://openairdocs.org/sdr/AALA20161001003.md): Battery Pack · inoperative · Oct 1, 2016 · N488AA · Doug DC982 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHTS AT ROW 30 AND AFT GALLEY COME ON WITH ALL POWER REMOVED FROM AIRCRAFT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY ASSEMBLIES AT ROWS 25 AND 29 IAW AMM 33-53-00. OPERATIONAL CHECK GOOD IAW AMM 33-53-00.
- [SDR AALA20160510003](https://openairdocs.org/sdr/AALA20160510003.md): Battery Pack · discharged · May 9, 2016 · N488AA · Doug DC982 · Emergency Lighting
  > AIRCRAFT WAS NOT GNDED. EGRESS POWER SUPPLY, AB5-4 FAILS TO TEST. R & R AB5-4 EGRESS LIGHT POWER SUPPLY BATTERY PACK IAW AMM 33-60-98. SYS CHECKS NORMAL.
- [SDR AALA20160510002](https://openairdocs.org/sdr/AALA20160510002.md): Battery Pack · discharged · May 9, 2016 · N488AA · Doug DC982 · Emergency Lighting
  > AIRCRAFT WAS NOT GNDED. EGRESS POWER SUPPLY, AB5-3 FAILS TO TEST. R & R AB5-3 EGRESS LIGHT POWER SUPPLY BATTERY PACK IAW AMM 33-60-98. SYS CHECKED NORMAL.
- [SDR AALA20160327002](https://openairdocs.org/sdr/AALA20160327002.md): Tube · cracked · Mar 27, 2016 · N488AA · Doug DC982 · Air Distribution System
  > AIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB RECEIVED A TAIL COMPARTMENT TEMP HIGH WARNING. WARNING CEASED AFTER HP BLEED SWITCHES SELECTED OFF. FOUND CRACKED TUBE ON RT FLOW CONTROL VLV. R & R T
- [SDR AALA20160120001](https://openairdocs.org/sdr/AALA20160120001.md): Controller · failed · Jan 15, 2016 · N488AA · Doug DC982 · Brake Anti-Skid Section
  > AIRCRAFT WAS GNDED. DURING TAKEOFF, WHEEL NOT TURNING LIGHT ILLUMINATED. TAKEOFF ABORTED AT APPROX 60 KNOTS. ACCOMPLISHED TROUBLESHOOTING IAW AMM 32-43-00, FOUND CONTROL BOX FAIL. R & R ANTI-SKID CONTROL BOX IAW AMM 32-43-04. SYS CHECKED NORMAL.
- [SDR AALA20151227005](https://openairdocs.org/sdr/AALA20151227005.md): Adc · faulty · Dec 27, 2015 · N488AA · Doug DC982 · Air Data Computer
  > AIRCRAFT WAS GNDED. EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE 30,000 AUTOPILOT & AUTO THROTTLE DISCONNECTED. CAPTAIN HAD FAST & SLOW FAIL LIGHT ON MACH TRIM INOPERATIVE & UNRELIABLE AIRSPEED. R & R NR 1 AIR DATA COMPUTER IAW AM
- [SDR AALA20150808001](https://openairdocs.org/sdr/AALA20150808001.md): Heat Exchanger · leaking · Aug 8, 2015 · N488AA · Doug DC982 · Cabin Cooling System
  > AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB, PASSING FL180 THE TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. PERFORMED TAIL COMPARTMENT LEAK CHECK IAW MCM36-95-15 & FOUND THE PRIMARY HEAT EXCHANGER LEAKING AT THE UNIO
- [SDR AALA20150805010](https://openairdocs.org/sdr/AALA20150805010.md): Sensor · faulty · Aug 3, 2015 · N488AA · Doug DC982 · Pneumatic Indicating System
  > AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB, THE TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. R & R TUBE ASSEMBLY FROM TURBINE NOZZLE VLV TO EJECTOR INLET, BROKEN OFF, IAW AMM 21-20-06. R & R LT & RT TAIL COMPARTMENT HI
- [SDR AALA20150805009](https://openairdocs.org/sdr/AALA20150805009.md): Sensor · faulty · Aug 3, 2015 · N488AA · Doug DC982 · Pneumatic Indicating System
  > AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB, THE TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. R & R TUBE ASSEMBLY FROM TURBINE NOZZLE VLV TO EJECTOR INLET, BROKEN OFF, IAW AMM 21-20-06. R & R LT & RT TAIL COMPARTMENT HI
- [SDR AALA20150803010](https://openairdocs.org/sdr/AALA20150803010.md): Tube · broken · Aug 3, 2015 · N488AA · Doug DC982 · Engine Bleed Air System
  > AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB, THE TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. R & R TUBE ASSEMBLY FROM TURBINE NOZZLE VLV TO EJECTOR INLET, BROKEN OFF, IAW AMM 21-20-06. R & R LT & RT TAIL COMPARTMENT HI
- [SDR AALA20150727005](https://openairdocs.org/sdr/AALA20150727005.md): Panel · misaligned · Jul 25, 2015 · N488AA · Doug DC982 · Fuselage Miscellaneous Structure
  > VENTRAL STAIRWAY RUBS ON CEILING PANEL DURING UP & DOWN TRAVEL. REPAIRED VENTRAL STAIRWAY MOVABLE CEILING IAW AMM 53-20-06. TRIMMED OVERHEAD CEILING PANEL FOR CLEARANCE OF MOVEABLE CEILING, CAT WALK.
- [SDR AALA20140502009](https://openairdocs.org/sdr/AALA20140502009.md): Rib · cracked · May 2, 2014 · N488AA · Doug DC982 · Wing, Rib/Bulkhead
  > RIGHT HAND WING NR 4 SLAT TRACK INBD SUPPORT RIB CRACKED. INSTALLED DOUBLER REPAIR IAW EA MD80-57-034669.
- [SDR AALA20140502008](https://openairdocs.org/sdr/AALA20140502008.md): Rib · cracked · May 2, 2014 · N488AA · Doug DC982 · Wing, Rib/Bulkhead
  > LEFT HAND WING NR 4 SLAT TRACK INBD SUPPORT RIB CRACKED. INSTALLED DOUBLER REPAIR IAW EA MD80-57-034669.
- [SDR AALA20130508037](https://openairdocs.org/sdr/AALA20130508037.md): Transmitter · inoperative · May 8, 2013 · N488AA · Doug DC982 · Engine (Turbine/Turboprop)
  > LAX - INFLIGHT FAT-DFW. CREW REPORTED LEFT ENGINE COMPRESSOR STALL FOLLOWED BY SMOKE IN COCKPIT AND CABIN. EMERGENCY DECLARED FLIGHT DIVERTED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE PRESSURATION TRANSMITTER. SYSTEM
- [SDR AALA20121112001](https://openairdocs.org/sdr/AALA20121112001.md): Frame · worn · Nov 12, 2012 · N488AA · Doug DC982 · Fuselage Main, Frame
  > STATION 1380 LEFT SIDE FRAME WEB HAS WORN AREA FROM COCKPIT TEMP CONTROL VALVE. REMOVED DAMAGED MATERIAL AND INSTALLED FRAME WEB REPAIR AS PER AARD 53-10-00-28.
- [SDR AALA20121111004](https://openairdocs.org/sdr/AALA20121111004.md): Skin · dented · Nov 11, 2012 · N488AA · Doug DC982 · Fuselage Main, Plate/Skin
  > FUSELAGE DENTED WITH SCRATCH FROM STATIONS 170 TO 182 LONGERON 25 LEFT. INSTALLED DOUBLER PER SRM 53-04-03, FIGURE 8, SHEET 5.
- [SDR AALA20121111001](https://openairdocs.org/sdr/AALA20121111001.md): Web · corroded · Nov 11, 2012 · N488AA · Doug DC982 · Fuselage Miscellaneous Structure
  > RIGHT FORWARD SUBFLOOR CORRODED FROM STATIONS 160 TO 200 RIGHT BUTTLINE 50. INSTALLED SUBFLOOR REPAIR DOUBLER AT STATIONS 160 TO 200, RIGHT BUTTLINES 43 TO 57 PER AARD 53-20-00-16.
- [SDR AALA20121110005](https://openairdocs.org/sdr/AALA20121110005.md): Pan · corroded · Nov 10, 2012 · N488AA · Doug DC982 · Fuselage Miscellaneous Structure
  > FORWARD SERVICE DOOR JAMB PAN, LOWER END CORRODED FROM STATIONS 180 TO 190. ACCOMPLISHED REPAIR PER SRM 53-05-00 FIGURE 55.
- [SDR AALA20121108011](https://openairdocs.org/sdr/AALA20121108011.md): Bulkhead · cracked · Nov 8, 2012 · N488AA · Doug DC982 · Fuselage Main, Bulkhead
  > BULKHEAD SKIN IS CRACKED AROUND LOWER LEFT RADOME ALIGNMENT PIN. INSTALLED DOUBLER PER AARD 53-10-00-19.
- [SDR AALA20121107026](https://openairdocs.org/sdr/AALA20121107026.md): Shear Tie · cracked · Nov 7, 2012 · N488AA · Doug DC982 · Fuselage Internal Mounting Structure
  > SHEAR TIE CRACKED AT 1401 LONGERON 15 LEFT. INSTALLED NEW SHEAR TIE ANGLE PER AARD 51-00-05-1.
- [SDR AALA20121105017](https://openairdocs.org/sdr/AALA20121105017.md): Frame · cracked · Nov 5, 2012 · N488AA · Doug DC982 · Fuselage Main, Frame
  > THE 1485 CANT FRAME CRACKED BELOW STAIR RET ACTUATOR. INSTALLED FRAME SPLICE PER AARD 53-10-00-33.
- [SDR AALA20121105014](https://openairdocs.org/sdr/AALA20121105014.md): Fitting · corroded · Nov 5, 2012 · N488AA · Doug DC982 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO DOORWAY LOWER FORWARD CORNER FITTING. INSTALLED NEW CORNER FITTING AS PER AARD 51-00-05-1.
- [SDR AALA20121105005](https://openairdocs.org/sdr/AALA20121105005.md): Cusp Web · cracked · Nov 5, 2012 · N488AA · Doug DC982 · Fuselage Miscellaneous Structure
  > FOUND CRACK IN CUSP AT STATION 661 LEFT SIDE. REPLACED CUSP SHEET FROM STATIONS 598 TO 712 PER AARD 53-20-00-16.
- [SDR AALA20121104010](https://openairdocs.org/sdr/AALA20121104010.md): Membrane · corroded · Nov 4, 2012 · N488AA · Doug DC982 · Fuselage Miscellaneous Structure
  > RIGHT FORWARD SUBFLOOR CORRODED FROM STATIONS 160 TO 200, RIGHT BUTTLINE 50. INSTALLED DOUBLER PER AARD 53-20-00-16.
- [SDR AALA20121104009](https://openairdocs.org/sdr/AALA20121104009.md): Membrane · corroded · Nov 4, 2012 · N488AA · Doug DC982 · Fuselage Miscellaneous Structure
  > CORROSION FOUND AT STATIONS 148 TO 160, 6 INCHES RIGHT OF CENTERLINE ON SUBFLOOR. INSTALLED DOUBLER PER AARD 53-20-00-16.
- [SDR AALA20121104008](https://openairdocs.org/sdr/AALA20121104008.md): Angle · corroded · Nov 4, 2012 · N488AA · Doug DC982 · Fuselage Miscellaneous Structure
  > CUSP ANGLE CORRODED AT STATIONS 170 TO 210, FORWARD SERVICE DOOR AREA. ACCOMPLISHED SPLICE REPAIR PER SRM 53-05-00 FIGURE 55 AND BOEING DRAWING J060288.
- [SDR AALA20121104007](https://openairdocs.org/sdr/AALA20121104007.md): Pan · cracked · Nov 4, 2012 · N488AA · Doug DC982 · Fuselage Miscellaneous Structure
  > WINDOW PAN CRACKED, WINDOW 43, UPPER AFT AT STATION 1041. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.
- [SDR AALA20121104006](https://openairdocs.org/sdr/AALA20121104006.md): Membrane · corroded · Nov 4, 2012 · N488AA · Doug DC982 · Fuselage Miscellaneous Structure
  > CORROSION ON SUBFLOOR AT STATION 200 UNDER G-2 GALLEY OUTBOARD. INSTALLED DOUBLER PER AARD 53-20-00-16.
- [SDR AALA20121104004](https://openairdocs.org/sdr/AALA20121104004.md): Membrane · corroded · Nov 4, 2012 · N488AA · Doug DC982 · Fuselage Miscellaneous Structure
  > CORROSION ON SUB-FLOOR UNDER G-1 GALLEY DRAIN PAN. INSTALLED DOUBLER PER AARD 53-20-00-16.
- [SDR AALA20121104003](https://openairdocs.org/sdr/AALA20121104003.md): Cusp Web · cracked · Nov 4, 2012 · N488AA · Doug DC982 · Fuselage Miscellaneous Structure
  > FOUND CRACK IN CUSP AT STATION 581, LEFT SIDE. INSTALLED DOUBLER PER AARD 53-20-00-16.
- [SDR AALA20121104002](https://openairdocs.org/sdr/AALA20121104002.md): Cusp Web · corroded · Nov 4, 2012 · N488AA · Doug DC982 · Fuselage Miscellaneous Structure
  > CORROSION ON BOTTOM OF LEFT CUSP FROM STATIONS 554 TO 557. INSTALLED DOUBLER PER AARD 53-20-00-16.
- [SDR AALA20121102005](https://openairdocs.org/sdr/AALA20121102005.md): Door Frame · cracked · Nov 2, 2012 · N488AA · Doug DC982 · Service Doors
  > AFT SERVICE DOOR HAS A CRACK IN FRAME AT LOWER HINGE CUTOUT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER EA COMP-52-026822.
- [SDR AALA20121102003](https://openairdocs.org/sdr/AALA20121102003.md): Intercostal · cracked · Nov 2, 2012 · N488AA · Doug DC982 · Fuselage Miscellaneous Structure
  > AFT CARGO CEILING CENTER INTERCOSTAL IS CRACKED AT FWD SIDE OF FLOORBEAM AT STATION 1309. REPLACED INTERCOSTAL PER AARD 51-00-05-1.
- [SDR AALA20121030036](https://openairdocs.org/sdr/AALA20121030036.md): Skin · cracked · Oct 30, 2012 · N488AA · Doug DC982 · Fuselage Main, Plate/Skin
  > FUSE - SKIN CRACKED AT STATION 1309 ABOVE LONGERON 7 RIGHT. INSTALLED REPAIR DOUBLER PER SRM 53-04-03 FIGURE 9 AND SRM 51-01-00 PARAGRAPH 4.
- [SDR AALA20121030024](https://openairdocs.org/sdr/AALA20121030024.md): Cusp Web · cracked · Oct 30, 2012 · N488AA · Doug DC982 · Fuselage Miscellaneous Structure
  > CRACK IN CUSP AT STATION 581 LEFT SIDE. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.
- [SDR AALA20121030005](https://openairdocs.org/sdr/AALA20121030005.md): Skin · damaged · Oct 30, 2012 · N488AA · Doug DC982 · Trailing Edge Flaps
  > INBOARD FLAP, INBOARD WEDGE, GOUGED BOTTOM EDGE. REMOVED DAMAGE FROM LOWER SKIN PER SRM 57-01-00 FIGURE 5 SHEET 2. DAMAGE IS 22 INCHES FROM TRAILNG EDGE AND 20 INCHES FROM INBOARD EDGE. DYE PEN INSPECTION REVEALS NO CRACK INDICATION. INSTALLED PERMANENT FL
- [SDR AALA20120524001](https://openairdocs.org/sdr/AALA20120524001.md): Battery Pack · discharged · May 23, 2012 · N488AA · Doug DC982 · Emergency Lighting
  > FORWARD CABIN AND FLIGHT DECK EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD CABIN AND FLIGHT DECK EMERGENCY LIGHTS BATTERY PACK, OPS CHECK NORMAL.
- [SDR AALA20110523TUL05](https://openairdocs.org/sdr/AALA20110523TUL05.md): Structure · corroded · May 23, 2011 · N488AA · Doug DC982 · Fuselage Miscellaneous Structure
  > CORROSION UNDER STAINLESS DOUBLER ALONG BOTTOM EDGE OF DOOR SILL. INSTALLED DOUBLER PER AARD 53-10-00-3.
- [SDR AALA20100402DFW02](https://openairdocs.org/sdr/AALA20100402DFW02.md): Regulator · malfunctioned · Apr 2, 2010 · N488AA · Doug DC982 · Cabin Pressure Control System
  > DFW - CREW REPORTED FUMES AND SMOKE IN CABIN. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT PRESSURE REGULATOR AND ACCOMPLISHED BURN OUT OF HIGH PRESSURE PNEUMATIC DUCTING. SYSTEM GROUND CHECKED NORMA
- [SDR AALA20091001SFO03](https://openairdocs.org/sdr/AALA20091001SFO03.md): Regulator Valve · failed · Oct 1, 2009 · N488AA · Doug DC982 · Air Distribution System
  > CREW REPORTED SMELL OR ODOR IN CABIN AND COCKPIT AFTER TAKEOFF. RETURNED TO FAT AND LANDED WITHOUT INCIDENT. REPLACED LEFT AND RIGHT PRESSURE REGULATING VALVES. REPLACED BOTH COALESCER BAGS AND LEFT PNEUMATIC PILOT REGULATOR VALVE.
- [SDR AALA20090722LGA06](https://openairdocs.org/sdr/AALA20090722LGA06.md): Light · inoperative · Jul 21, 2009 · N488AA · Doug DC982 · Emergency Lighting
  > CEILING EMERGENCY LIGHT BETWEEN AFT LAVATORIES INOPERATIVE. REPLACED LAMP FOR CEILING EMERGENCY LIGHT BETWEEN AFT LAVATORIES. OPS CHECK NORMAL.
- [SDR AALA20090722LGA05](https://openairdocs.org/sdr/AALA20090722LGA05.md): Strap · missing · Jul 21, 2009 · N488AA · Doug DC982 · Emergency Lighting
  > FLASHLIGHT STRAP MISSING FROM FLASHLIGHT BY AFT GALLEY FLIGHT ATTENDANT SEAT. INSTALLED STRAP FOR FLASHLIGHT AT AFT GALLEY FLIGHT ATTENDANT SEAT.
- [SDR AALA20090722LGA04](https://openairdocs.org/sdr/AALA20090722LGA04.md): Strap · missing · Jul 21, 2009 · N488AA · Doug DC982 · Emergency Lighting
  > FLASHLIGHT STRAP MISSING FROM FLASHLIGHT OUTSIDE RIGHT LAVATORY. INSTALLED STRAP FOR FLASHLIGHT AT RIGHT LAVATORY.
- [SDR AALA20090722LGA03](https://openairdocs.org/sdr/AALA20090722LGA03.md): Strap · missing · Jul 21, 2009 · N488AA · Doug DC982 · Emergency Equipment
  > FLASHLIGHT STRAP MISSING FROM FLASHLIGHT BY AFT GALLEY FLIGHT ATTENDANT SEAT. REPLACED STRAP FOR FLASHLIGHT AT AFT GALLEY FLIGHT ATTENDANT SEAT.
- [SDR AALA20090722LGA02](https://openairdocs.org/sdr/AALA20090722LGA02.md): Battery Pack · not seated · Jul 21, 2009 · N488AA · Doug DC982 · Emergency Lighting
  > CEILING EMERGENCY LIGHTS INOPERATIVE FROM ROWS 23 TO ROW 29. RESEATED BATTERY PACK FOR CEILING EMERGENCY LIGHTS FROM ROWS 23 TO 29. OPS NORMAL.
- [SDR AALA20090722LGA01](https://openairdocs.org/sdr/AALA20090722LGA01.md): Battery Pack · not seated · Jul 21, 2009 · N488AA · Doug DC982 · Emergency Lighting
  > TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERY PACK IN TAIL COMPARTMENT. OPS CHECKS NORMAL.

Next page: https://openairdocs.org/deregistered/N488AA-2019-09-06/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 = 'N488AA' AND deregistration_id = 'N488AA-2019-09-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N488AA-2019-09-06/reports

---
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