# Service difficulty reports: N927DA, cancelled Apr 8, 2019

A list on [N927DA, cancelled Apr 8, 2019](https://openairdocs.org/deregistered/N927DA-2019-04-08.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 4 · 180 reports

- [SDR DALA2018072304608](https://openairdocs.org/sdr/DALA2018072304608.md): Charger · inoperative · Jul 23, 2018 · N927DA · Doug MD88 · Emergency Lighting
  > EMERGENCY PATH LIGHTING AT SEATS 13-23 INOP. R&R BATTERY CHAGER AT B5-211 PER 33-50 OPS CK NML.
- [SDR DALA2018011700260](https://openairdocs.org/sdr/DALA2018011700260.md): Reservoir · malfunctioned · Jan 17, 2018 · N927DA · Doug MD88 · Hydraulic Reservoir, Main
  > DURING CRUISE, RT HYD LOW PRESSURE MESSAGE ON OAP, RIGHT HYD QTY WENT UP TO 19 QTS. FOLLOWING QRH, REPRESSURIZED BELOW 10,000 FT. PRESSURE CAME UP TO 3000 PSI, QTY DOWN TO 10 QUARTS. PRESSURE WAS ZERO FOR 5 - 20 MINUTES. REPLACED THE RESERVOIR AND ENGINE DRIV
- [SDR DALA2017100207192](https://openairdocs.org/sdr/DALA2017100207192.md): Connector · disconnected · Sep 29, 2017 · N927DA · Doug MD88 · Light System Wiring
  > EMERGENCY LIGHTS INOPERATIVE SEATS 10D, 27D, AND 33D. CHECK LIGHTS AND WIRING. CONNECTED THE CONNECTORS. CHECKED GOOD.
- [SDR DALA2017052104053](https://openairdocs.org/sdr/DALA2017052104053.md): Shutoff Valve · leaking · May 20, 2017 · N927DA · Doug MD88 · Rudder Control System
  > DURING FLIGHT, CREW REPORTED RIGHT HYDRAULIC FLUID QUANTITY LOSS AND ACCOMPLISHED QRH PROCEDURE SECURING RIGHT HYDRAULIC SYSTEM PUMPS. ON APPROACH, ATTEMPTED TO RE-PRESSURIZE RIGHT HYDRAULIC SYSTEM PER QRH AND THE SYSTEM FAILED TO PRESSURIZE. ACCOMPLISHED ALTE
- [SDR DALA2017032302348](https://openairdocs.org/sdr/DALA2017032302348.md): Battery · discharged · Mar 23, 2017 · N927DA · Doug MD88 · Emergency Lighting
  > AIR STAIR EMER LIGHTS INOP. REPLACED BATTERIES AFT EMER LIGHT BATTERY PACK REF AMM 33-53.
- [SDR DALA2017030101645](https://openairdocs.org/sdr/DALA2017030101645.md): Pin · out of adjust · Feb 28, 2017 · N927DA · Doug MD88 · Aerodynamic Fairings
  > TAILCONE RELEASE MECHANISM CAM ASSY. PIN IS IMPROPERLY INDEXED ON SPLINE. REINDEXED CAM RELEASE PIN PER MD88 AMM 53-53-02-201, O.K. FOR SERVICE.
- [SDR DALA2017021201145](https://openairdocs.org/sdr/DALA2017021201145.md): Valve · failed · Feb 13, 2017 · N927DA · Doug MD88 · Cabin Pressure Control System
  > AFTER TAKEOFF AT 3000FT CABIN AND FLIGHT CREW NOTICED THAT AIRCRAFT WAS LOSING CABIN PRESSURE. AT 12,000FT MSL MAX CABIN ALTITUDE REACHED 10,500FT. CABIN ALTITUDE AND MASTER WARNING LIGHTS WERE ILLUMINATED ALONG WITH CABIN ALTITUDE WARNING HORN SOUNDING. ATB
- [SDR DALA2016121909973](https://openairdocs.org/sdr/DALA2016121909973.md): Slide · malfunctioned · Dec 18, 2016 · N927DA · Doug MD88 · Escape Slide
  > DOOR 1L OPENED BY FA WHILE ARMED. SLIDE DID NOT DEPLOY. INSPECTED SLIDE VERIFIED PARACHUTE PINS ARE INSTALLED. REINSTALLED SLIDE ON L1 DOOR PER AMDS CARD 2561-4964. OK FOR SERVICE.
- [SDR DALA2016042403283](https://openairdocs.org/sdr/DALA2016042403283.md): Skin · damaged · Apr 23, 2016 · N927DA · Doug MD88 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN BS 1174 AND LONGERON 1. EXTERNAL FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04-1, PAR 6 D, 3, COND 3, AMM 25-28-00-201, AMM 21-00-00-401, ETI 88-16 -175, REV 5, ER/A 545136-14 MA, REV ORIGINAL, AND PS 900-5-1, NR 04. REP
- [SDR DALA2016042303238](https://openairdocs.org/sdr/DALA2016042303238.md): Skin · corroded · Apr 22, 2016 · N927DA · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON INNER PRODUCTION DOUBLER BS 1309, OUTFLOW VALVE AREA. DUE TO EXCESIVE CORROSION DOUBLER WAS REPLACED IAW SRM 51-10-4M, 51-10-3, PAR 21 AND 14, 51-30-2 AND 51-30-5, AND DWG 5936021.
- [SDR DALA2016042303237](https://openairdocs.org/sdr/DALA2016042303237.md): Skin · corroded · Apr 22, 2016 · N927DA · Doug MD88 · Fuselage Main, Plate/Skin
  > CORRODED PREVIOUS REPAIR DOUBLER BETWEEN BS 200 TO 218, LONGERON 29LT TO 30 AT ELECTRONIC EQUIPMENT COMPARTMENT. REPAIR WAS ACCOMPLISHED IAW ER/A 545129-14, REV ORIGINAL AND ERI -88-16-171, REV 1, SECTION 1.
- [SDR DALA2016042303236](https://openairdocs.org/sdr/DALA2016042303236.md): Skin · damaged · Apr 22, 2016 · N927DA · Doug MD88 · Rudder, Plate/Skin
  > EXPOSED MATERIAL ON LT, RT SIDE AT RUDDER. DAMAGE AREA BOTH SIDE WERE REPAIRED IAW ERA NR 092613-14MA, REV "A", SRM 51-70-01A, PAR 23 AND ERA NR 545122-14, REV ORIGINAL.
- [SDR DALA2016042503249](https://openairdocs.org/sdr/DALA2016042503249.md): Skin · corroded · Apr 21, 2016 · N927DA · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE, SKIN, FS 200-218, L29-30L AT MODE S ANTENNA CORROSION REPAIR. ACCOMPLISH ER/A 545129-14, SECTION II.
- [SDR DALA2016042203231](https://openairdocs.org/sdr/DALA2016042203231.md): Structure · damaged · Apr 21, 2016 · N927DA · Doug MD88 · Rudder Structure
  > HINGE EDGE ON RUDDER LT/RT SIDE. EDGE ON RUDDER LT & RT SIDE WERE REPAIRED IAW SRM 51-70-4AD AND OPEN 2304653.
- [SDR DALA2016042103148](https://openairdocs.org/sdr/DALA2016042103148.md): Pan · cracked · Apr 20, 2016 · N927DA · Doug MD88 · Service Doors
  > CRACKED PAN ON AFT UPPER AT R1 DOOR. PAN WAS REPAIRED IAW SRM 52-03D, FIG 3.
- [SDR DALA2016042103147](https://openairdocs.org/sdr/DALA2016042103147.md): Beam · cracked · Apr 20, 2016 · N927DA · Doug MD88 · Service Doors
  > CRACKED BEAM NR 1 AFT EDGE AT FWD SERVICE DOOR. BEAM WAS REPLACED IAW SRM 51-30-2.
- [SDR DALA2016042103143](https://openairdocs.org/sdr/DALA2016042103143.md): Longeron · cracked · Apr 20, 2016 · N927DA · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 29L, BS 200. THE LONGERON WAS REPLACED IAW SRM 53-14-1, FIG 3, 51-30-2 AND 51-30.
- [SDR DALA2016042003140](https://openairdocs.org/sdr/DALA2016042003140.md): Beam · cracked · Apr 19, 2016 · N927DA · Doug MD88 · Service Doors
  > CRACKED BEAM NR 4 FWD EDGE AT FWD R1 DOOR. NR 4 BEAM WAS REPLACED IAW DWG 9911582, REV T, 51-30-1, 51-30-2, 51-30-4 AND 51-30-5.
- [SDR DALA2016042003135](https://openairdocs.org/sdr/DALA2016042003135.md): Skin · damaged · Apr 19, 2016 · N927DA · Doug MD88 · Rudder, Plate/Skin
  > EXPOSED MATERIAL ON LT & RT SIDE AT RUDDER. LT & RT SIDE AT RUDDER WERE REPAIRED IAW ER/A 092613-14MA, REV A, ER/A 545141-14, REV ORIGINAL.
- [SDR DALA2016042003134](https://openairdocs.org/sdr/DALA2016042003134.md): Skin · damaged · Apr 19, 2016 · N927DA · Doug MD88 · Fuselage Main, Plate/Skin
  > ASSESS DAMAGE ON FUSELAGE SKIN BS 484, BETWEEN LONGERON 23-24 RT, SPEED TAPE ID DATA. REPAIR WAS EVALUATED AND FOUND ACCOMPLISHED IAW INSTRUCTIONS OF SRM 53-04-2, FIG 2, SHEET 5, AS PERMANENT REPAIR.
- [SDR DALA2016042003131](https://openairdocs.org/sdr/DALA2016042003131.md): Beam · damaged · Apr 19, 2016 · N927DA · Doug MD88 · Service Doors
  > CRACKED PAN ON FWD EDGE AT NR 4BEAM FWD R1 SERVICE DOOR. BEAM WAS REPAIRED IAW SRM 52-03, FIG 3.
- [SDR DALA2016041903026](https://openairdocs.org/sdr/DALA2016041903026.md): Longeron · cracked · Apr 18, 2016 · N927DA · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON 4L BS 200. LONGERON WAS REPLACED IAW SRM 53-02, FIG 18, PAR 12, 51-30-5, AND CARD 5330-01204-02-03.
- [SDR DALA2016041903024](https://openairdocs.org/sdr/DALA2016041903024.md): Longeron · cracked · Apr 18, 2016 · N927DA · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 29R BS 180. LONGERON WAS REPLACED IAW SRM 53-02, FIG 18, SHEET 2, 51-30-2, 51-10-4, 51-30-5, PAR 7, FIG 10, PAR 14, 21.
- [SDR DALA2016041802991](https://openairdocs.org/sdr/DALA2016041802991.md): Longeron · cracked · Apr 17, 2016 · N927DA · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 29R BS 180 AT ELECTRONIC EQUIPMENT COMPARTMENT. LONGERON WAS REPLACED IAW SRM 53-02, FIG 18, SHEET 2, 51-30-2, 51-10-4, 51-30-5 PAR 7, FIG 10, PAR 14, 21.
- [SDR DALA2016041802989](https://openairdocs.org/sdr/DALA2016041802989.md): Cargo Track · cracked · Apr 17, 2016 · N927DA · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK ON LOWER SUPPORT OF TIE TRACK BETWEEN BS 1212 TO 1231 AND PROJECTION LONGERONS 28LT TO 27LT AT AFT CARGO COMPARTMENT. SUPPORT WAS REPLACED IAW SRM 53-05, FIG 4G, 51-10-3, PAR 21,14, 51-30-2, 51-30-5.
- [SDR DALA2016041702971](https://openairdocs.org/sdr/DALA2016041702971.md): Rib · cracked · Apr 15, 2016 · N927DA · Doug MD88 · Wing, Rib/Bulkhead
  > CRACKED RIB ON RT WING FIXED L/E BS XRS 324. THE RIB WAS REPAIRED IAW SRM 57-06 B, D, FIG 18.
- [SDR DALA2016041602963](https://openairdocs.org/sdr/DALA2016041602963.md): Support Fitting · corroded · Apr 14, 2016 · N927DA · Doug MD88 · Fuselage, Landing Gear Attach Fittings
  > CORROSION ON MLG SUPPORT FITTING LOWER AREA BS XCW=98.500. AREA WAS REPAIRED IAW SRM 57-03, FIG 34, 51-10-3, P 14-21 AND 51-30-5.
- [SDR DALA2016041502929](https://openairdocs.org/sdr/DALA2016041502929.md): Skin · damaged · Apr 14, 2016 · N927DA · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DAMAGED BETWEEN BS 1287- 1309, LONGERON 26L.
- [SDR DALA2016041402909](https://openairdocs.org/sdr/DALA2016041402909.md): Longeron · cracked · Apr 13, 2016 · N927DA · Doug MD88 · Fuselage Main, Longeron/Stringer
  > AD 98-13-35, REV 1: CRACK ON LONGERON 2 LT BS 160, AT CPAX COMPLETE WC 5330-01204-0205. 1ST EVAL, LONGERON NR 2 WAS REPAIRED IAW SRM 51-30-2, 53-02, FIG 18, 51-10-4, 51-10-3 PAR 14 AND 21, 51-30-5.
- [SDR DALA2016041302867](https://openairdocs.org/sdr/DALA2016041302867.md): Door Frame · corroded · Apr 12, 2016 · N927DA · Doug MD88 · Fuselage Main, Structure
  > CORROSION ON DOOR FRAME AT CARGO DOOR BS 650 - 690 LONGERON 28R. CORROSION WAS REMOVED AND REWORKED AREA WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 26, 21, 14. WITHIN LIMITS IAW SRM 53-05, FIG 123.
- [SDR DALA2016021501078](https://openairdocs.org/sdr/DALA2016021501078.md): Battery Pack · inoperative · Feb 14, 2016 · N927DA · Doug MD88 · Emergency Lighting
  > MAINTENANCE FOUND THE AFT CEILING EMERGENCY LIGHTS INOPERATIVE. BATTERIES WERE REPLACED AND THE LIGHTS CHECKED GOOD.
- [SDR DALA14017360927](https://openairdocs.org/sdr/DALA14017360927.md): Connector · disconnected · Mar 18, 2014 · N927DA · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT SEAT 27D/E IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A CONNECTOR IN THE WIRE HARNESS UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYS.
- [SDR DALA13051230927](https://openairdocs.org/sdr/DALA13051230927.md): Toggle · failed · Oct 8, 2013 · N927DA · Doug MD88 · Escape Slide
  > ACFT FAILED THE FUNCTIONAL CHECK OF TAILCONE RELEASE SYS WHEN A WORN TOGGLE ON THE SLIDE LANYARD PREVENTED THE SLIDE FROM DEPLOYING. THE TOGGLE WAS REPLACED, THE SYS WAS RETURNED OPERATIONAL STATUS, AND THE RII WAS COMPLETED.
- [SDR DALA13046470927](https://openairdocs.org/sdr/DALA13046470927.md): Battery Pack · inoperative · Sep 21, 2013 · N927DA · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MX FOUND THAT THE EMERGENCY EXIT SIGNS AT BOTH OF THE LT AND RT OVERWING DOORS WERE INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.
- [SDR DALA13046010927](https://openairdocs.org/sdr/DALA13046010927.md): Connector · damaged · Sep 18, 2013 · N927DA · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 19R IN THE CABIN WAS INOPERATIVE. MX FOUND A LOOSE PIN IN THE CONNECTOR AND RE-PINNED IT. THE SYS RETURNED TO NORMAL OPERATION.
- [SDR DALA13044350927](https://openairdocs.org/sdr/DALA13044350927.md): Power Supply · inoperative · Sep 12, 2013 · N927DA · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MX FOUND THAT MULTIPLE OVERHEAD EMERGENCY PATHWAY LIGHTS IN THE MID-CABIN WERE INOPERATIVE. MX REPLACED THE POWER SUPPLY AND RELAMPED AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA13002440927](https://openairdocs.org/sdr/DALA13002440927.md): Structure · cracked · Jan 16, 2013 · N927DA · Doug MD88 · Vertical Stabilizer
  > ON BOLT HOLE INSPECTION OF VERTICAL STAB, FOUND OVERSIZED HOLE WITH CRACK INDICATION. FOUND HOLE TO BE LARGER THAN.202" ALLOWABLE HOLE SIZE. OVERSIZED HOLE WAS REPAIRED IAW FINAL ER/A 510507-14AD REV ORIG ASSOCIATED ER/A 14-510507 ADDED FOR AC 0927.
- [SDR DALA13002410927](https://openairdocs.org/sdr/DALA13002410927.md): Release Mech · stuck · Jan 12, 2013 · N927DA · Doug MD88 · Aerodynamic Fairings
  > MX DISCOVERED THAT THE TAILCONE RELEASE SYS CAM WAS STUCK, CAM AND BLOCKS FOR THE RELEASE CABLE WERE WORN AND OUT OF RIG BEYOND ALLOWABLE LIMITS. THE MATING FLANGE WAS CRACKED AT MULTIPLE ALIGNMENT PIN POSITIONS. THE CABLE CAMS AND BLOCKS WERE REPLACED AND
- [SDR DALA13002450927](https://openairdocs.org/sdr/DALA13002450927.md): Structure · damaged · Jan 11, 2013 · N927DA · Doug MD88 · Vertical Stabilizer
  > ON BOLT HOLE INSPECTION OF VERTICAL STAB, FOUND THREE HOLES DAMAGED. DAMAGE CLEAN-UP RESULTED IN OVERSIZING HOLES LARGER THAN ALLOWED SIZE. OVERSIZED HOLES WERE REPAIRED IAW ER/A 510499-14AD, REV ORIG ASSOCIATED ER/A 14-510499 ADDED FOR AC 0927.
- [SDR DALA13002430927](https://openairdocs.org/sdr/DALA13002430927.md): Structure · cracked · Jan 11, 2013 · N927DA · Doug MD88 · Vertical Stabilizer
  > ON BOLT HOLE EC INSPECTION OF RT SIDE VERTICAL, 3 HOLE DOWN FROM COLLAR, FAULT FOUND OVERSIZED HOLE WITH CRACK INDICATION, CLEAN UP OF HOLE, NO HELP. FURTHER CLEANUP OF SUSPECTED HOLE WITH CRACK AND FOUND HOLE TO BE LARGER THAN.202" ALLOWABLE HOLE SIZE. OVE
- [SDR DALA13002420927](https://openairdocs.org/sdr/DALA13002420927.md): Attach Fitting · damaged · Jan 11, 2013 · N927DA · Doug MD88 · Vertical Stabilizer, Attach Fittings
  > COMPLETING BOLT HOLE EC OF VERTICAL STAB, FOUND 3 RT SIDE HOLES, THREAD CUT-DAMAGED INSIDE OF HOLES. REMOVED NUT PLATE CHANNEL & POLISHED HOLES. ACCOMPLISHED DVI OF REWORKED AREA, DAMAGE CONTAINED. ALL 3 HOLES ARE LARGER THAN THE.202" ALLOWABLE HOLE SIZE.
- [SDR DALA1245510927](https://openairdocs.org/sdr/DALA1245510927.md): Seat Track · corroded · Aug 13, 2012 · N927DA · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK STA 1155 LBL 22 HAS AREA OF CORROSION ON LT FLANGE AND BARE META. SEAT TRACK REPLACED ON NRC 7000098670001.
- [SDR DALA1245500927](https://openairdocs.org/sdr/DALA1245500927.md): Seat Track · corroded · Aug 13, 2012 · N927DA · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STA 1287-1309 LBL 22 HAS CORROSION ON TOP OF TRACK INSIDE CHANNEL IN 3 AREAS. SEAT TRACK REPLACED ON NRC7000098670001.
- [SDR DALA1245490927](https://openairdocs.org/sdr/DALA1245490927.md): Seat Track · corroded · Aug 13, 2012 · N927DA · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT STA 1174-1193 LBL 22 HAS 2 AREAS OF CORROSION ON LT FLANGE AND BARE METAL. SEAT TRACK REPLACED ON NRC 7000098670001.
- [SDR DALA1245480927](https://openairdocs.org/sdr/DALA1245480927.md): Seat Track · corroded · Aug 13, 2012 · N927DA · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 1271-1287 HAS CORROSION ON TOP OF TRACK AND INSIDE CHANNEL. SEAT TRACK REPLACED ON NRC 7000098670001.
- [SDR DALA1245470927](https://openairdocs.org/sdr/DALA1245470927.md): Seat Track · corroded · Aug 12, 2012 · N927DA · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 1250-1271 HAS CORROSION ON TOP OF TRACK AND DOWN IN CHANNEL. REPAIRED PER MD-88 SRM 51-30-1.
- [SDR DALA1245460927](https://openairdocs.org/sdr/DALA1245460927.md): Beam · corroded · Aug 12, 2012 · N927DA · Doug MD88 · Fuselage Main, Structure
  > MID CARGO LOWER BILGE BEAM HAS CORROSION AT BS 636 AND L29R. COMPLIED WITH ER/A 505651-14 REV ORIG.
- [SDR DALA1245450927](https://openairdocs.org/sdr/DALA1245450927.md): Skin · dented · Aug 12, 2012 · N927DA · Doug MD88 · Fuselage Main, Plate/Skin
  > RT FUSELAGE STA 1375 L-7R HAS A DENT JUST BELOW SKIN OVERLAP. ACCOMPLISHED ER/A 505309-14 REV ORIG.
- [SDR DALA1245430927](https://openairdocs.org/sdr/DALA1245430927.md): Seat Track · corroded · Aug 12, 2012 · N927DA · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK SECTION LBL 54 FS 266-797 HAS PITTING CORROSION AT CTR CHANNEL AND LUGS FS 790-797. REPLACED SEAT TRACK IAW SRM 53-05.
- [SDR DALA1245420927](https://openairdocs.org/sdr/DALA1245420927.md): Cusp Web · corroded · Aug 12, 2012 · N927DA · Doug MD88 · Fuselage Miscellaneous Structure
  > MAIN CABIN RT CUSP WEB LOWER SURFACE HAS CORROSION AT BS 933. WEB REPLACED ON NRC 210001.

Next page: https://openairdocs.org/deregistered/N927DA-2019-04-08/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 = 'N927DA' AND deregistration_id = 'N927DA-2019-04-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N927DA-2019-04-08/reports

---
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