# Service difficulty reports: N910DE, cancelled Nov 23, 2022

A list on [N910DE, cancelled Nov 23, 2022](https://openairdocs.org/deregistered/N910DE-2022-11-23.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 · 182 reports

- [SDR DALA2020033002059](https://openairdocs.org/sdr/DALA2020033002059.md): Lanyard · broken · Mar 30, 2020 · N910DE · Doug MD88 · Escape Slide
  > THE L1 DOOR SLIDE LANYARD WAS FOUND BROKEN. MAINTENANCE REPLACED THE SLIDE LANYARD FOR THE L1 DOOR PER MD88 AMM 25-62. (LP #7179212)
- [SDR DALA2020031601856](https://openairdocs.org/sdr/DALA2020031601856.md): Frame · cracked · Mar 15, 2020 · N910DE · Doug MD88 · Fuselage Main, Frame
  > CANTED FRAME CRACKED AT 2 O'CLOCK POSITION AND 7 O'CLOCK. REMOVED L/H LWR FRAME + UPPER FRAME, DRILLED UP THE NEW L/H LWR FRAME + BEGAN DRILLING NEW UPPER FRAME. PER MD88 SRM 53-15-4 FIG 3. ( P/N 596676841 + P/N 5966769-1) COMPLETED DRILLING UP UPPER FRAME. IN
- [SDR DALA2019122907587](https://openairdocs.org/sdr/DALA2019122907587.md): Skin · corroded · Dec 28, 2019 · N910DE · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION FOUND JUST AFT OF LAV SVC PANEL. CORROSION ALSO NOTED FURTHER AFT AT PRESSURE DOME AREA. SKIN IS BULGED AND SEPARATED AT SEAM. AREA MARKED. BLENDED CORROSION NEAR AFT LAV SVC PNL. FOUND TO BE WITHIN LIMITS PER MD88 SRM 53-04-1. RESTORED FINISH. CORRO
- [SDR DALA2019071104157](https://openairdocs.org/sdr/DALA2019071104157.md): Inlet · contaminated · Jul 11, 2019 · N910DE · Doug MD88 · APU Cowling/Containment
  > WHILE BOARDING FLIGHT LEADER AND CAPT SMELLED BURNING OIL ORDER IN COCKPIT AND FWD CABIN FOUND OIL AROUND APU NON REM DOORS. T/S PER NO GO ODI FOUND APU INLET CONTAMINATED PERFORMED DUCT BURN OUT PER WORK CARD 7100-2619 LEACK CHECK LEFT AND RIGHT PACK NO LEAKS
- [SDR DALA2019061293522](https://openairdocs.org/sdr/DALA2019061293522.md): Door Frame · cracked · Jun 7, 2019 · N910DE · Doug MD88 · Fuselage Main, Structure
  > R/H FWD MAIN LANDING GEAR WHEEL FRAME IS CRACKED. ACCOMPLISHED SEC I TIME LIMITED REPAIR PER ER/A 578803-14 REV ORIGINAL. ASSOCIATED ER/A 14-578803. REPLACED R/H MLG FWD DOOR JAMB PER RI SEC II REF BOEING DWG #5930584. LANDING GEAR DOOR OPS CHECK GOOD REF MD88
- [SDR DALA2019050902912](https://openairdocs.org/sdr/DALA2019050902912.md): Light · damaged · May 9, 2019 · N910DE · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHT ASSY DAMAGED AT 32D. REPLACED LIGHT ASSY AT 32D OPS NL REF AMM 33-52. (LP5800382)
- [SDR DALA2019032301882](https://openairdocs.org/sdr/DALA2019032301882.md): Connector · damaged · Mar 22, 2019 · N910DE · Doug MD88 · Light System Wiring
  > SEAT 13DE AND 21DE EMERGENCY PATH LIGHTS INOP. REPAIRED CONNECTORS, REF SWPM 20-90. NOW CHECKS GOOD. (LP5845377)
- [SDR DALA2019020420697](https://openairdocs.org/sdr/DALA2019020420697.md): Door Frame · corroded · Feb 1, 2019 · N910DE · Doug MD88 · Fuselage Main, Structure
  > AWR. CORROSION ON LWR DOOR JAMB BTW STA 399 TO 415 AT FWD CARGO COMPARTMENT. REPAIR ON LWR DOOR JAMB BTW STA 399 TO 415 AT FWD CARGO COMPARTMENT WAS PERMORMED PER DC9MD80 SRM 53-05 FIG. 44A, ETI-88-19-006 REV. 1 AND ERA 575056-14 REV. ORIG. (LP0927609)
- [SDR DALA2019012900611](https://openairdocs.org/sdr/DALA2019012900611.md): Spacer · corroded · Jan 28, 2019 · N910DE · Doug MD88 · Fuselage Miscellaneous Structure
  > AWR. INITIAL INSPECTION. CORROSION ON SPACER IN LWR BEAM PREVIOUS REPAIR AT AFT CARGO DOOR CUT OUT LWR AREA. CORROSION LEVEL 2. SPACER ON BEAM PREVIOUS REPAIR AT AFT CARGO DOOR WAS REPLACED PER SRM 53-05 FIG 123. (LP0922716)
- [SDR DALA2019010500062](https://openairdocs.org/sdr/DALA2019010500062.md): Cooling Fan · odor · Jan 4, 2019 · N910DE · Doug MD88 · Air Distribution Fan
  > BURNING SMELL WHEN INSTR COOLING FAN RUNNING PULL C/B ODOR GOES AWAY. C/W NO GO ODI PREV 2172 PER AMDS W/C 2120-2367. VERIFIED INST COOLING FAN IS BAD CAUSING THE NOISE AND BURNING SMELL IN COCKPIT. APU INLET IS CLEAN. REMOVED AND REPLACED INST COOLING FAN REF
- [SDR DALA2018072504672](https://openairdocs.org/sdr/DALA2018072504672.md): Battery · discharged · Jul 25, 2018 · N910DE · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTS DOOR 2 LEFT INOP. REMOVED AND REPLACED TWO EMERGENCY 'D' CELL BATTERIES FOR THE OVER EMERGENCY LIGHTS AT DOOR 2L. OPERATIONAL CHECK GOOD IAW AMM 33-50. P/N AD4002P.
- [SDR DALA2018033002038](https://openairdocs.org/sdr/DALA2018033002038.md): Actuator · failed · Mar 30, 2018 · N910DE · Doug MD88 · Landing Gear Actuator
  > DURING CLIMB OUT, A NOISE AND VIBRATION FROM NOSE GEAR AREA INCREASED WITH AIRSPEED. RETURNED TO DEPARTURE. RIGHT NOSE GEAR DOOR FOUND OPEN. REPLACED RIGHT DOOR MECHANICAL ACTUATOR IAW AMM. NOSE GEAR SWING CHECK PERFORMED.
- [SDR DALA2018030801468](https://openairdocs.org/sdr/DALA2018030801468.md): Wire · shorted · Mar 6, 2018 · N910DE · Doug MD88 · Electrical Power System Wiring
  > ACARS PRINTER WIRE BUNDLE SHORTING ON AIRCRAFT STRUCTURE. PULLED & COLLARED ACARS PRINTER C/B F18. REMOVED ACARS PRINTER. FOUND 4 WIRES SHORTING TO GROUND. REPAIRED WIRING PER SOPW AND WDM 23-24-01 SH 1 PG 2. REROUTED WIRE BUNDLE TO MAKE CANNON PLUG ACCESSIBLE
- [SDR DALA2017042503376](https://openairdocs.org/sdr/DALA2017042503376.md): Cable · frayed · Apr 25, 2017 · N910DE · Doug MD88 · Aerodynamic Fairings
  > DURING TAILCONE INSPECTION FOUND CABLE FRAYED. R & R TAILCONE CABLE IAW AMM 53-53-0.
- [SDR DALA2016123010145](https://openairdocs.org/sdr/DALA2016123010145.md): Shaft · worn · Dec 30, 2016 · N910DE · Doug MD88 · Passenger/Crew Doors
  > WEAR ON L1 MECHANISM DOOR SHAFT ASSY P/N4915850-1. REPLACED SHAFT ASSY PER MD 88 AMM 26-62-00-201, 52-11-01-201 (LP# 2828265)
- [SDR DALA2016123010142](https://openairdocs.org/sdr/DALA2016123010142.md): Longeron · cracked · Dec 29, 2016 · N910DE · Doug MD88 · Fuselage Main, Longeron/Stringer
  > AFT ACCESORIES COMPARTMENT CRACK LONGERON 12R, BS 1431 BULKHEAD. REPAIRED IAW ETI-88-16-462 REV. 1 AND ER/A 552834-14.
- [SDR DALA2016122910128](https://openairdocs.org/sdr/DALA2016122910128.md): Housing · worn · Dec 28, 2016 · N910DE · Doug MD88 · Cargo/Baggage Doors
  > WEAR ON AFT CARGO DOOR HANDLE HOUSING. HOUSING WAS REMPLACED IAW SRM 51-30-2 AND 51-30-5.
- [SDR DALA2016122710084](https://openairdocs.org/sdr/DALA2016122710084.md): Pan · cracked · Dec 26, 2016 · N910DE · Doug MD88 · Cargo/Baggage Doors
  > CRACKED PAN BELOW STOP FITTING NR 2 ON FWD CARGO DOOR FWD EDGE. REPAIRED IAW ETI-88-16-480 REV. 2 AND ER/A 552866-14.
- [SDR DALA2016122410060](https://openairdocs.org/sdr/DALA2016122410060.md): Door Frame · cracked · Dec 23, 2016 · N910DE · Doug MD88 · Fuselage Main, Structure
  > CRACKED FWD DOOR JAMB CHANNEL BS 937 AND RBL 5. RH MLG JAMB CHANNEL WAS REPAIRED IAW ERA 552882-14.
- [SDR DALA2016122310040](https://openairdocs.org/sdr/DALA2016122310040.md): Doubler · corroded · Dec 22, 2016 · N910DE · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON AFT LAVATORY SERVICE PANEL INNER DOUBLER. THE DOUBLER WAS REPLACED IAW ER/A 552849-14 REV: ORIGINAL.
- [SDR DALA2016122210028](https://openairdocs.org/sdr/DALA2016122210028.md): Pan · cracked · Dec 21, 2016 · N910DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED PAN BELOW STOP FITTING NR 2 ON FWD CARGO COMPARTMENT DOOR FWD EDGE. CRACKED PAN WAS REPAIRED IAW ER/A 552873-14 REV: ORIGINAL, MESSAGE 16-0778-08B AND ETI-88-16-483 REV: NR 3.
- [SDR DALA2016122210027](https://openairdocs.org/sdr/DALA2016122210027.md): Pan · cracked · Dec 21, 2016 · N910DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACK ON INNER PAN FWD LOWER CORNER AT FWD SERVICE DOOR. INNER PAN FWD LOWER CORNER AT FWD SERVICE DOOR WAS REPAIRED IAW ETI 88-16-483 REV.3 AND ER/A 552873-14 REV. ORIGINAL.
- [SDR DALA2016122110002](https://openairdocs.org/sdr/DALA2016122110002.md): Frame · cracked · Dec 20, 2016 · N910DE · Doug MD88 · Fuselage Main, Frame
  > AFT ACCESORIES COMPARTMENT, CRACK ON FRAME BS 1485 BETWEEN LONGERONS 15 - 16L. THE FRAME WAS REPAIRED IAW ER/A 552836-14 REV. ORIGINAL. MESSAGE 16-0739-04B AND ETI -88-16-464 REV.ORIGINAL.
- [SDR DALA2016122109995](https://openairdocs.org/sdr/DALA2016122109995.md): Floor Panel · cracked · Dec 20, 2016 · N910DE · Doug MD88 · Fuselage Floor Panel
  > CRACKED CHANNEL ON CABIN FLOOR PANEL 769G. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-05 PAR. 145 FIG.
- [SDR DALA2016122009971](https://openairdocs.org/sdr/DALA2016122009971.md): Former · cracked · Dec 19, 2016 · N910DE · Doug MD88 · Fuselage Main, Frame
  > FUSELAGE, CRACKED FORMER STA Y=907 AND X=-60 AT RT FILLET PANEL. FORMER WAS REPAIRED PER SRM 53-01 FIG 2.
- [SDR DALA2016121909968](https://openairdocs.org/sdr/DALA2016121909968.md): Hinge · damaged · Dec 18, 2016 · N910DE · Doug MD88 · Cargo/Baggage Doors
  > C2 CARGO DOOR, ELONGATED HOLES ON CARGO DOOR HINGES C2. HOLES WERE REWORKED PER ERA 497387-14MA REV B AND DOORS HINGES WAS REMOVED /INSTALLED PER AMM 52-31-02-201.
- [SDR DALA2016121909939](https://openairdocs.org/sdr/DALA2016121909939.md): Frame · cracked · Dec 18, 2016 · N910DE · Doug MD88 · Fuselage Main, Frame
  > AFT ACCESSORIES COMPARTMENT: CRACK ON FRAME STA Y=1485 CANT LONG 7R TO 9R. AREA WAS REPAIRED PER SRM 53-03 FIG. 49 AND SRM 51-30-2, 51-30-5 AND 51-30-1.
- [SDR DALA2016121909938](https://openairdocs.org/sdr/DALA2016121909938.md): Hinge · damaged · Dec 18, 2016 · N910DE · Doug MD88 · Fuselage, Door Hinge
  > ELONGATED HOLES ON HINGES AT AFT UPPER INBOARD SIDE OF THE FUSELAGE DOOR CARGO JAM. HINGES AT AFT UPPER INBOARD SIDE OF THE FUSELAGE DOOR CARGO JAMB WERE REPLACED PER SRM 51-30-5 AND DWG 9957945 REV J.
- [SDR DALA2016121809937](https://openairdocs.org/sdr/DALA2016121809937.md): Skin · corroded · Dec 17, 2016 · N910DE · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON TWO HOLES ON LWR ACCESS CUTOUT ADJACENT TO STRINGER 12 AT XRS=210 AT LT WING. LWR ACCESS CUT OUT WAS REPAIRED PER ER/A 552851-14AD REV ORIGINAL AND ETI 88-16-474 REV 1 REPAIR, APPROVAL IS LIMITED TO 67,000 TOTAL CYCLES ONLY.
- [SDR DALA2016121809936](https://openairdocs.org/sdr/DALA2016121809936.md): Floor Panel · cracked · Dec 17, 2016 · N910DE · Doug MD88 · Fuselage Floor Panel
  > CRACKED CABIN FLOOR PANEL NR: 389A, 693A, 617G, 1079E, 256E AND 389G. FLOOR PANELS 256E, 389G AND 1079E WERE REPAIRED PER SRM 53-05 PAR 145 FIG 131C. FLOOR PANEL 617G WAS REPAIRED PER SRM 53-01 FIG 4. FLOOR PANEL 693A WAS REPLACED PER SRM 51-10-4. FLOOR PANEL
- [SDR DALA2016121809934](https://openairdocs.org/sdr/DALA2016121809934.md): Floor Panel · cracked · Dec 17, 2016 · N910DE · Doug MD88 · Fuselage Floor Panel
  > CRACK ON GENERATION FLOOR PANEL NR: 541F, 927E, 1079A, 389A, 769A AND 256A. FLOOR PANELS 541F, 927E AND 256A WERE REPAIRED PER SRM 53-05 PAR 145 FIG 131B AND 131C. FLOOR PANEL 769A WAS REPAIRED PER SRM 53-01 FIG 4. FLOOR PANEL 1079A WAS REPAIRED PER SRM 51-20-
- [SDR DALA2016121909969](https://openairdocs.org/sdr/DALA2016121909969.md): Skin · punctured · Dec 16, 2016 · N910DE · Doug MD88 · Cargo/Baggage Doors
  > PUNCTURE ON FWD CARGO COMPARTMENT DOOR INNER SKIN. FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER. ERA 094625-14.
- [SDR DALA2016121909941](https://openairdocs.org/sdr/DALA2016121909941.md): Bulkhead · corroded · Dec 16, 2016 · N910DE · Doug MD88 · Fuselage Main, Bulkhead
  > AFT ACCESSORY COMPARTMENT: CORROSION ON BULKHEAD, INTERCOSTALS, RT/LT CAP AND RT/LT BEAM AT AFT STAIRWAY WALKING BRIDGE. DUE EXCESSIVE CORROSION BULKHEAD NR 2 WAS REPLACED PER SRM 51-30-2.
- [SDR DALA2016121709926](https://openairdocs.org/sdr/DALA2016121709926.md): Intercostal · cracked · Dec 16, 2016 · N910DE · Doug MD88 · Fuselage Miscellaneous Structure
  > AFT ACCESSORIES COMPARTMENT: CRACK ON INTERCOSTAL BTW STA Y=1485 CANT TO Y=1497 CANT BTW LONG PROJECTION 18L TO 22L. INTERCOSTAL WAS REPLACED PER DWG 9917701 REV AND SRM 51-30-2 AND 51-30-5.
- [SDR DALA2016121609909](https://openairdocs.org/sdr/DALA2016121609909.md): Cargo Track · corroded · Dec 16, 2016 · N910DE · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO BAY HAS CORROSION ON THE RT CARGO TRACK BETWEEN BS 1007 - 1155, AND BS 1212 - 1322. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-1 AND DWG 5936660 REV. BZ.
- [SDR DALA2016121609896](https://openairdocs.org/sdr/DALA2016121609896.md): Support · corroded · Dec 15, 2016 · N910DE · Doug MD88 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT: CORROSION ON ZEE SUPPORT ABOVE RT CARGO TRACK BETWEEN BS 1117 TO 1155. THE SUPPORT WAS REPLACED IAW SRM 51-30-1, 51-30-5 AND DWG 5936660 REV:BZ.
- [SDR DALA2016121609900](https://openairdocs.org/sdr/DALA2016121609900.md): Access Panel · corroded · Dec 15, 2016 · N910DE · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON SECONDARY ACCESS PANEL 1410C. THE ACCESS PANELS WAS REPLACED IAW 51-10-3.
- [SDR DALA2016121609899](https://openairdocs.org/sdr/DALA2016121609899.md): Access Panel · corroded · Dec 15, 2016 · N910DE · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON FUEL ACCESS PANEL 1333C. INSTALLED A NEW ACCESS PANEL IAW AMM 28-00-00.
- [SDR DALA2016121609898](https://openairdocs.org/sdr/DALA2016121609898.md): Frame · cracked · Dec 15, 2016 · N910DE · Doug MD88 · Fuselage Main, Frame
  > AFT ACCESORIES COMPARTMENT HAD A CRACK ON FRAME BS 1510. THE FRAME WAS REPLACED IAW SRM 51-30-02.
- [SDR DALA2016121609897](https://openairdocs.org/sdr/DALA2016121609897.md): Floor Panel · corroded · Dec 15, 2016 · N910DE · Doug MD88 · Fuselage Floor Panel
  > CORROSION ON FLOOR PANEL. REPAIRED IAW ER/A 504469-14MA.
- [SDR DALA2016121509885](https://openairdocs.org/sdr/DALA2016121509885.md): Splice · cracked · Dec 14, 2016 · N910DE · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED SPLICE BS 988 AND LBL 7. REPAIRED IAW ER/A 413026-14MA.
- [SDR DALA2016121509880](https://openairdocs.org/sdr/DALA2016121509880.md): Skin · bulged · Dec 14, 2016 · N910DE · Doug MD88 · Trailing Edge Flaps
  > PROTUBERANCE ON LOWER SKIN OF RT WING OUTBD FLAP OUTBD GUIDE VANE AT XV2=321. REPAIRED IAW SRM 57-03 D PAR. 11 (LP#2808044)
- [SDR DALA2016121509879](https://openairdocs.org/sdr/DALA2016121509879.md): Finger Doubler · corroded · Dec 14, 2016 · N910DE · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON THE FINGER DOUBLER BETWEEN BS 1193 - 1309, LONGERONS 25 - 26L. FINGER DOUBLER WAS REPLACED IAW SRM 53-34-0 FIG, 3 AND 51-10-1 FIG 36.
- [SDR DALA2016121409850](https://openairdocs.org/sdr/DALA2016121409850.md): Door · cracked · Dec 14, 2016 · N910DE · Doug MD88 · Wing Main, Frame Structure
  > RT WING HAS A CRACKED INBD FLIGHT SPOILER BUTTE DOOR XRS 184. REPAIR THE DOOR IAW SRM 51-70-4 FIG.1 (SHEET 1).
- [SDR DALA2016121409849](https://openairdocs.org/sdr/DALA2016121409849.md): Frame · cracked · Dec 13, 2016 · N910DE · Doug MD88 · Fuselage Main, Frame
  > AFT ACCESORIES BAY HAS A CRACK ON THE FRAME LOWER CAP BS 1431 LONGERONS 11 & 12R. THE FRAME WAS REPAIRED IAW ER/A 552832-14 REV. ORIGINAL AND ETI-88-16-460 REV. 2.
- [SDR DALA2016121409847](https://openairdocs.org/sdr/DALA2016121409847.md): Cargo Track · corroded · Dec 13, 2016 · N910DE · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO BAY HAS CORROSION ON THE LT CARGO TRACK BS 1007 - 1322. REPLACED IAW SRM 51-30-2 AND 51-30-5.
- [SDR DALA2016121409845](https://openairdocs.org/sdr/DALA2016121409845.md): Doubler · corroded · Dec 13, 2016 · N910DE · Doug MD88 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY HAS CORROSION ON A PREVIOUS REPAIR DOUBLER AT LOWER DOOR FRAME PAN BS 370 TO 427. THE REPAIR DOUBLERS WAS REPLACED IAW ER/A 526949-14 REV.ORIG. AND ER/A 383732-14 REV.ORIG.
- [SDR DALA2016121309794](https://openairdocs.org/sdr/DALA2016121309794.md): Frame · corroded · Dec 12, 2016 · N910DE · Doug MD88 · Fuselage Main, Frame
  > AFT ACCESORIES COMPARTMENT, CORROSION ON FRAME BS 1393 LBL 3 TO LBL 10, BETWEEN LONGERONS 25 - 28L. AREA WAS REPAIRED IAW SRM 51-70-5 FIG 1.
- [SDR DALA2016121209787](https://openairdocs.org/sdr/DALA2016121209787.md): Skin · not reported · Dec 10, 2016 · N910DE · Doug MD88 · Wing, Plate/Skin
  > DURING NDT INSPECTION, A DISCREPANT AREA WAS FOUND (SEVEN DIFFERENT FASTENERS OF PSE) ON LOWER SKIN REAR SPAR BTW XRS=163 TO 168 AT LT WING. ATTENDED WITH ER/A NR 552817-14AD REV ORIGINAL.
- [SDR DALA2016121209786](https://openairdocs.org/sdr/DALA2016121209786.md): Skin · not reported · Dec 10, 2016 · N910DE · Doug MD88 · Wing, Plate/Skin
  > DURING NDT INSPECTION, A DISCREPANT AREA WAS FOUND (SEVEN DIFFERENT FASTENERS OF PSE) ON LOWER SKIN REAR SPAR BTW XRS=163 TO 168 AT RT WING. ATTENDED WITH ER/A NR 552817-14AD REV ORIGINAL.

Next page: https://openairdocs.org/deregistered/N910DE-2022-11-23/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 = 'N910DE' AND deregistration_id = 'N910DE-2022-11-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N910DE-2022-11-23/reports

---
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