# Service difficulty reports: N911DL, cancelled Dec 30, 2024

A list on [N911DL, cancelled Dec 30, 2024](https://openairdocs.org/deregistered/N911DL-2024-12-30.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 · 195 reports

- [SDR DALA2019083105108](https://openairdocs.org/sdr/DALA2019083105108.md): Socket · burned · Aug 30, 2019 · N911DL · Doug MD88 · Passenger Compartment Lighting
  > FWD LAV FLUORESCENT LIGHT BURNED OUT ODOR OF BURNED INSULATION OR BALLAST. C/W NO GO ODI CHECKLIST 2172 C/W JIC 2120-2367 FOUND F/C LAV AFT LIGHT UPPER SOCKET ASSEMBLY WITH HEAT DAMAGE R/R SOCKET ASSY IAW WSPM 20-31 NO SMOKE/ODOR PRESENT CHKS GOOD OK FOR SVC.
- [SDR DALA2019080104519](https://openairdocs.org/sdr/DALA2019080104519.md): Unknown · odor · Jul 31, 2019 · N911DL · Doug MD88 · Air Distribution System
  > ON ENGINE SHUT DOWN, AND APU ON, FUEL ODOR IN FLIGHT DECK. FLT ATTENDANT IN FRONT SMELLED FUEL. INSPECTED FOR FUEL LEAKS ENGINES AND APU COMP NO SMELLS OR FUEL LEAKS NOTICED. COMPLETED NO GO ODI CHECK LISHT 21-72 MD88 AMDS CARD 2120-2367. NO ODORS PRESENT COMP
- [SDR DALA2019072004353](https://openairdocs.org/sdr/DALA2019072004353.md): Structure · cracked · Jul 19, 2019 · N911DL · Doug MD88 · Fuselage Miscellaneous Structure
  > TWO CRACKS DETECTED AT AFT LOWER CORNER OF FWD CARGO DOOR CUTOUT. ONE SURFACE AND ONE SUBSURFACE. (MARKED). NRC 002-0005:5230-2466/001 00003 COMPLIED WITH ER/A 579800-14AD REV O. (LP #1180107)
- [SDR DALA2019021500959](https://openairdocs.org/sdr/DALA2019021500959.md): Wire · broken · Feb 15, 2019 · N911DL · Doug MD88 · Light System Wiring
  > FOUND EMERGENCY LIGHT OUT AT ROW 16. REPINED BROKEN WIRES ON EMERGENCY LIGHT ROW 16 REF MD88 SWPM 20-14. OPS CHECK GOOD. (LP5529603)
- [SDR DALA2019020400702](https://openairdocs.org/sdr/DALA2019020400702.md): Bottle · empty · Feb 2, 2019 · N911DL · Doug MD88 · Escape Slide
  > DURING SERVICE CHECK FOUND L1 DOOR SLIDE BOTTLE GAGE IN THE RED NO GO ZONE. R/R L1 DOOR SLIDE PER WORK CARD 2561-4964. A/C OK FOR SVC. SLIDE, EVAC, FO OFF 97-2561-9-0001 01778 ON 09-2561-9-0011 02128. (LP4809848)
- [SDR DALA2018103106350](https://openairdocs.org/sdr/DALA2018103106350.md): Battery · discharged · Oct 31, 2018 · N911DL · Doug MD88 · Emergency Lighting
  > ROW 10-15 CEILING EMER LIGHT OUT. R+R ROW 10-15 CEILING EMER LIGHT BATTERYS PER AMM 33-53. OPS CHECK GOOD. (LP4814589)
- [SDR DALA2018092605762](https://openairdocs.org/sdr/DALA2018092605762.md): Smoke Detector · malfunctioned · Sep 25, 2018 · N911DL · Doug MD88 · Smoke Detection
  > AFT LEFT LAV SMOKE DETECTOR CHIRPING. REPLACED LEFT AFT SMOKE DETECTOR - CKS OK - REF MD88 AMM 26-17. (LP4698953)
- [SDR DALA2018082985339](https://openairdocs.org/sdr/DALA2018082985339.md): Acoustic Liner · damaged · Aug 26, 2018 · N911DL · Doug MD88 · Turbine Engine Compressor Section
  > FLT 2179, RETURNED TO DEPARTURE, DUE TO THE NR 2 ENGINE COMPRESSOR STALL, SHORTLY AFTER TAKE-OFF. MAINTENANCE FOUND DAMAGE TO ACOUSTIC PANELS AND BLEED DUCTS IN COLD STREAM AROUND BLEED VALVES. THE ENGINE WAS REPLACED.
- [SDR DALA2018031301578](https://openairdocs.org/sdr/DALA2018031301578.md): Lens · missing · Mar 12, 2018 · N911DL · Doug MD88 · Emergency Lighting
  > EMERGENCY EXIT SIGNS INOPERATIVE, LOCATIONS 25E, ACARS TEXT FRC25600125E INTERIOR. FOUND OVERWING EXIT DOOR LIGHT UPPER LENS COVER MISSING. INSTALLED NEW COVER. OK FOR SVC.
- [SDR DALA2017110607953](https://openairdocs.org/sdr/DALA2017110607953.md): Lens · missing · Nov 5, 2017 · N911DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHT RED LENS MISSING AT GALLEY AISLE INTERIOR. SECURED THE RED LENS.
- [SDR DALA2017092507063](https://openairdocs.org/sdr/DALA2017092507063.md): Fan · failed · Sep 24, 2017 · N911DL · Doug MD88 · Air Distribution Fan
  > SMOKE AND FUMES DETECTED CLIMBING OUT OF 11,000 FT. DIVERTED. SMOKE ORIGINATED AT ROW 27ABC TO FWD CABIN. FOLLOWED NO GO ODI. TROUBLESHOT IAW AMDS 2120-2367. FOUND CABIN RECIRCULATION FAN NOT RUNNING. ALL THREE CIRCUIT BREAKERS PHASES TRIPPED. REPLACED TH
- [SDR DALA2017081106134](https://openairdocs.org/sdr/DALA2017081106134.md): Attach Bolt · corroded · Aug 10, 2017 · N911DL · Doug MD88 · Trailing Edge Flaps
  > RUSTED RT FLAP HINGE FITTING ATTACH BOLT STA XW= 251 AT RT WING. RUST WAS REMOVED PER SRM 51-10-03 PARA 26 VOL II AND SERVICEABLE FLAP HINGE AT RT WING STA 251 WAS INSTALLED PER AMM 57-40-01-201.
- [SDR DALA2017081106132](https://openairdocs.org/sdr/DALA2017081106132.md): Support Fitting · corroded · Aug 10, 2017 · N911DL · Doug MD88 · Trailing Edge Flaps
  > CORROSION ON FLAP HINGE SUPPORT STA XW 251 AT LEFT WING REAR SPAR. LT WING FLAP HINGE SUPPORT FITTING WAS REPAIRED, BUSHING WERE FABRICATED AND INSTALLED PER CMM 27-50-5 PAR 2 I AND HINGE WAS INSTALLED PER AMM 57-40-01-201.
- [SDR DALA2017081006106](https://openairdocs.org/sdr/DALA2017081006106.md): Panel · corroded · Aug 10, 2017 · N911DL · Doug MD88 · Auxiliary Power Unit (APU) Doors
  > CORROSION ON THE AFT LAVATORY SERVICE PANEL. THE LAVATORY SERVICE PANEL WAS REPLACED IAW SRM 51-10-4, 51-10-3, 51-30-2, 51-30-5, AND 51-30-1.
- [SDR DALA2017080806039](https://openairdocs.org/sdr/DALA2017080806039.md): Hinge · corroded · Aug 7, 2017 · N911DL · Doug MD88 · Trailing Edge Flaps
  > CORROSION AROUND STUD HOLES ON RT WING FLAP HINGE SUPPORT NR 3. DUE TO EXCESSIVE DAMAGE ON HINGE. THE HINGE WAS REPLACED.
- [SDR DALA2017080605985](https://openairdocs.org/sdr/DALA2017080605985.md): Skin · cracked · Aug 5, 2017 · N911DL · Doug MD88 · Fuselage Main, Plate/Skin
  > TWO CRACKS WERE FOUND OF 0.064" AND 0.096" LENGTH ON THE FUSELAGE SKIN BS 1418, LONGERONS 1 AND 2R. REPAIRED IAW ER/A 559536-14 AD, REV ORG, AND ETI-88-17-200, REV 1.
- [SDR DALA2017081106135](https://openairdocs.org/sdr/DALA2017081106135.md): Vane · cracked · Aug 3, 2017 · N911DL · Doug MD88 · Trailing Edge Flaps
  > CRACK ON UPPER INBD CIRCULAR PANEL AT LT OTBD FLAP OTBD FIXED VANE CIRCULAR PANEL ON TOP SURFACE IAW NRC 00935. THE FLAP OTBD FIXED VANE WAS REPLACED IAW AMM 27-51-03.
- [SDR DALA2017080405951](https://openairdocs.org/sdr/DALA2017080405951.md): Skin · nicked · Aug 3, 2017 · N911DL · Doug MD88 · Trailing Edge Flaps
  > NICK ON LOWER SKIN INBD EDGE ON RT OUTBD FIXED GUIDE VANE OUTBD FLAP. RT OUTBD FIXED GUIDE VANE OUTBD FLAP WAS REPAIRED PER SRM 57-03 D PAR 11.
- [SDR DALA2017080305950](https://openairdocs.org/sdr/DALA2017080305950.md): Vane · delaminated · Aug 2, 2017 · N911DL · Doug MD88 · Trailing Edge Flaps
  > HIDDEN DAMAGE DELAMINATION BELOW RUB STRIP ON LT OUTBD FIXED GUIDE VANE INBD FLAP. LT WING INBD FLAP OUTBD FIXED GUIDE VANE WAS REPAIRED PER SRM 57-03 D PARAGRAPH 11 FIG 11.
- [SDR DALA2017080305886](https://openairdocs.org/sdr/DALA2017080305886.md): Doubler · corroded · Aug 2, 2017 · N911DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON PREVIOUS REPAIR DOUBLER STA Y=234 BTW LONGERON 26-25 RT SIDE AT FWD CARGO COMPARTMENT. PREVIOUS DOUBLER REPAIR STA Y=234 BTWN LONG 26 AND 25 RT SIDE WAS REPLACED AS PERMANENT REPAIR PER ETI- 88-17-203 REV 3 AND ER/A 559546-14 REV ORIG SECTION I.
- [SDR DALA2017080305885](https://openairdocs.org/sdr/DALA2017080305885.md): Spar Cap · cracked · Aug 2, 2017 · N911DL · Doug MD88 · Elevator, Spar/Rib
  > A CRACK OF 4.400" WAS FOUND ON LT ELEVATOR SPAR CAP BETWEEN XE=133.411 AND XE=137.811. LT ELEVATOR SPAR CAP BTW XE=133.411 AND XE= 137.811 WAS REPAIRED PER ETI-88-17-197 REV 3 AND ER/A 559522-14 REV ORG SECTION I PERMANENT REPAIR.
- [SDR DALA2017080305884](https://openairdocs.org/sdr/DALA2017080305884.md): Doubler · worn · Aug 2, 2017 · N911DL · Doug MD88 · Trailing Edge Flaps
  > WORN LEADING EDGE REPAIR DOUBLER ON RT OUTBOARD FLAP INBOARD GUIDE VANE. RT OUTBOARD FLAP INBOARD GUIDE VANE WAS REPAIRED PER SRM 57-03 D.
- [SDR DALA2017080305883](https://openairdocs.org/sdr/DALA2017080305883.md): Panel · cracked · Aug 2, 2017 · N911DL · Doug MD88 · Leading Edge Devices
  > CRACK ON SLAT PANEL NR 3 CENTER HINGE SUPPORT, RT WING. SLAT PANEL NR 3 RT WING WAS REMOVED PER AMM 27-80-01 S/N REMOVED 0022 AND SERVICEABLE SLAT PANEL 3 S/N DL51 RW MUST BE INSTALLED AND ADJUSTED UNDER JIC 2700-4224-RH-03 JOB 000-0003.
- [SDR DALA2017080305882](https://openairdocs.org/sdr/DALA2017080305882.md): Skin · cracked · Aug 2, 2017 · N911DL · Doug MD88 · Wing, Plate/Skin
  > CRACKS ON 7 HOLES ON LT WING LWR ACCESS DOOR CUTOUT XRS = 189.0 TO 214.0. CRACKS ON 7 HOLES ON LT WING LWR ACCESS DOOR CUTOUT XRS = 189.0 TO 214.0 WERE REPAIRED PER ETI-88-17-199 REV 1 AND ER/A 559533-14AD REV ORIGINAL WITH LOG 0144928.
- [SDR DALA2017080205861](https://openairdocs.org/sdr/DALA2017080205861.md): Access Panel · cracked · Aug 1, 2017 · N911DL · Doug MD88 · Wing, Plate/Skin
  > CRACKS ON THE RT WING LOWER ACCESS DOOR CUTOUT XRS 189 TO 214. REPAIRED IAW ETI-88-17-199, REV 1, AND ER/A 559533-14AD, REV ORIGINAL.
- [SDR DALA2017080205860](https://openairdocs.org/sdr/DALA2017080205860.md): Access Panel · cracked · Aug 1, 2017 · N911DL · Doug MD88 · Wing, Plate/Skin
  > CRACKS ON THE LT WING LOWER ACCESS DOOR CUTOUT XRS 189 TO 214. REPAIRED IAW ETI-88-17-199, REV 1, AND ER/A 559533-14AD, REV ORIGINAL.
- [SDR DALA2017080105857](https://openairdocs.org/sdr/DALA2017080105857.md): Web · corroded · Jul 31, 2017 · N911DL · Doug MD88 · Entrance Stairs
  > CORROSION ON WEB ABOVE STEP NR 5 OF VENTRAL STAIRWAY DOOR STRUCTURE AT AFT ACCESSORY COMPARTMENT. THE WEB ON THE STEP WAS REPAIRED IAW SRM 53-01, FIG 4, SHT 4.
- [SDR DALA2017080105818](https://openairdocs.org/sdr/DALA2017080105818.md): Doubler · cracked · Jul 31, 2017 · N911DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CRACKS (2 EAS) 1)0..250" 2)0.125" WERE FOUND AT EXTERNAL DOUBLER THAT COVERS THE SKIN ADJACENT TO THE UPPER DOOR STOP ADJUST HOLES ON AFTER UPPER DOOR JAMB CORNER AT FWD PASSENGER DOOR BS 200. EXTERNAL DOUBLER THAT COVERS THE SKIN ADJACENT TO THE UPPER DOOR ST
- [SDR DALA2017080105817](https://openairdocs.org/sdr/DALA2017080105817.md): Intercostal · cracked · Jul 31, 2017 · N911DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 937, RBL 7 IN THE RT WHEEL WELL. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-02, 51-30-05, AND DWG:9936368, REV AW.
- [SDR DALA2017080105816](https://openairdocs.org/sdr/DALA2017080105816.md): Cargo Track · cracked · Jul 31, 2017 · N911DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CRACKED CARGO TRACK LT FWD BS 1003 AND 1265. THE CARGO TRACK WAS REPLACED IAW SRM 51-10-4, 51-30-05, 51-30-02, AND 51-10-3 PAR.14, 21, & 38.
- [SDR DALA2017073105780](https://openairdocs.org/sdr/DALA2017073105780.md): Intercostal · corroded · Jul 30, 2017 · N911DL · Doug MD88 · Fuselage Miscellaneous Structure
  > PARTS RACK, CORROSION ON INNER INTERCOSTALS (3E/A) AT VENTRAL STAIRWAY MOVABLE CEILING. INTERCOSTAL WERE REPLACED PER SRM 51-30-2 AND DWG 9911993 REV CJ / BW.
- [SDR DALA2017073005777](https://openairdocs.org/sdr/DALA2017073005777.md): Doubler · worn · Jul 29, 2017 · N911DL · Doug MD88 · Fuselage Main, Structure
  > WEAR ON DOUBLER PRODUCTION OUT OF LIMITS AT LT WW AFT DOOR JAMB STA Y= 941 X=55. REPLACED DOOR JAMB SRM 51-30-2, 51-30-05,51-30-1,51-10-3 PAR. 21 AND 14 DWG 5930584 REV BY.
- [SDR DALA2017073005775](https://openairdocs.org/sdr/DALA2017073005775.md): Frame · cracked · Jul 29, 2017 · N911DL · Doug MD88 · Fuselage Main, Frame
  > CRACKS ON FRAME STA Y=1463 CANT FWD FACE BTW LONGS 17L AND 18L AT AFT ACCESSORY COMPARTMENT. FRAME STA Y 1463 CANT BTW LONGS 17L AND 18L WAS REPAIRED PER SRM 53-01 FIG 2.
- [SDR DALA2017072805725](https://openairdocs.org/sdr/DALA2017072805725.md): Frame · cracked · Jul 27, 2017 · N911DL · Doug MD88 · Fuselage Main, Frame
  > CRACKED FRAME BS 1474 FWD FACE BETWEEN LONGERONS 17L AND 18L AT AFT ACCESSORY COMPARTMENT. THE FRAME WAS REPAIRED IAW SRM 53-01 FIG. 1.
- [SDR DALA2017072805724](https://openairdocs.org/sdr/DALA2017072805724.md): Access Panel · corroded · Jul 27, 2017 · N911DL · Doug MD88 · Wing, Plate/Skin
  > CORRODED COUNTERSINKS ON FUEL ACCESS PANEL. THE ACCESS PANEL ARE OUT OF LIMITS AND REPLACED IAW SRM 51-22-2A PAR. 6.
- [SDR DALA2017072805723](https://openairdocs.org/sdr/DALA2017072805723.md): Access Panel · corroded · Jul 27, 2017 · N911DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON COUNTERSINK ON FUEL TANK ACCESS PANEL 1436C. THE ACCESS PANEL FOUND OUT OF LIMITS AND REPLACED IAW SRM 51-22-2A PAR 6.
- [SDR DALA2017072805722](https://openairdocs.org/sdr/DALA2017072805722.md): Access Panel · corroded · Jul 27, 2017 · N911DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON UPPER SURFACE ON FUEL TANK ACCES PANEL 1307C. THE ACCESS PANEL IS OUT OF LIMITS AND WAS REPLACED IAW SRM 51-22-2A PAR. 6.
- [SDR DALA2017072805727](https://openairdocs.org/sdr/DALA2017072805727.md): Fitting · corroded · Jul 27, 2017 · N911DL · Doug MD88 · Fuselage Main, Attach Fittings
  > CORROSION ON THE FRAME FITTING BS 1271, BETWEEN RBL 54 AND 60. A NEW FITTING INSTALLED IAW SRM 51-30-1 AND 51-30-5.
- [SDR DALA2017072805728](https://openairdocs.org/sdr/DALA2017072805728.md): Angle · corroded · Jul 26, 2017 · N911DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON INNER ANGLES LT BS 1437 TO 1443, SIDE OF VENTRAL STAIRWAY MOVABLE CEILING. AREA WAS REPAIRED IAW SRM 53-01, FIG 2.
- [SDR DALA2017072705713](https://openairdocs.org/sdr/DALA2017072705713.md): Floor Support · cracked · Jul 26, 2017 · N911DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKS ON FLOOR SUPPORT BL 0, BETWEEN BS 1309 AND 1287. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-2, 51-30-5, AND DWG 9936580, REV BW.
- [SDR DALA2017072605704](https://openairdocs.org/sdr/DALA2017072605704.md): Access Panel · damaged · Jul 25, 2017 · N911DL · Doug MD88 · Wing, Plate/Skin
  > ELONGATE HOLES AND TOOL DAMAGE ON THE FUEL TANK ACCESS PANEL. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A, PAR 6.
- [SDR DALA2017072605703](https://openairdocs.org/sdr/DALA2017072605703.md): Access Panel · damaged · Jul 25, 2017 · N911DL · Doug MD88 · Wing, Plate/Skin
  > ELONGATE HOLES AND TOOL DAMAGE ON THE FUEL TANK ACCESS PANEL. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A, PAR 6.
- [SDR DALA2017072605702](https://openairdocs.org/sdr/DALA2017072605702.md): Panel · cracked · Jul 25, 2017 · N911DL · Doug MD88 · Leading Edge Devices
  > CRACKS FOUND ON THE LT WING SLAT PANELS 4 & 3 BOTH AT CENTER HINGES. THE SLAT PANELS WERE REPLACED.
- [SDR DALA2017072605699](https://openairdocs.org/sdr/DALA2017072605699.md): Vane · nicked · Jul 25, 2017 · N911DL · Doug MD88 · Trailing Edge Flaps
  > NICKS ON LOWER SKIN AT THE RT INBD FIXED GUIDE VANE INBD FLAP. THE GUIDE VANE WAS REPAIRED IAW SRM 57-03D, PAR 11.
- [SDR DALA2017072605698](https://openairdocs.org/sdr/DALA2017072605698.md): Access Panel · corroded · Jul 25, 2017 · N911DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON SETTLEMENT AREA AND COUNTERSINK ON FUEL TANK ACCESS PANEL NR 1409C. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A, PAR 6, CONDITION III.
- [SDR DALA2017072605697](https://openairdocs.org/sdr/DALA2017072605697.md): Access Panel · corroded · Jul 25, 2017 · N911DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON SETTLEMENT AREA AND COUNTERSINK ON THE FUEL TANK ACCESS PANEL NR 1303C. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A, PAR 6, CONDITION III.
- [SDR DALA2017072505693](https://openairdocs.org/sdr/DALA2017072505693.md): Fitting · cracked · Jul 24, 2017 · N911DL · Doug MD88 · Cargo/Baggage Doors
  > CRACKED FITTING BS 408 UPPER SECTION AT FWD CARGO DOOR. THE FITTING WAS REPLACED IAW SRM 51-30-02, AND 51-30-05.
- [SDR DALA2017072505652](https://openairdocs.org/sdr/DALA2017072505652.md): Spar Cap · cracked · Jul 24, 2017 · N911DL · Doug MD88 · Horizontal Stabilizer, Spar/Rib
  > CRACK ON UPPER HOLE IN THE HORIZONTAL STABILIZER RT REAR CAP. REPAIRED IAW DWG SR09550027, REV F, AND SRM 51-30-1, 51-302 AND 51-30-5.
- [SDR DALA2017072405643](https://openairdocs.org/sdr/DALA2017072405643.md): Fitting · corroded · Jul 23, 2017 · N911DL · Doug MD88 · Fuselage Main, Attach Fittings
  > CORROSION ON FITTINGS, AT FLOOR PANEL 160G. NEW FITTINGS WERE INSTALLED.
- [SDR DALA2017072405634](https://openairdocs.org/sdr/DALA2017072405634.md): Ferrule · damaged · Jul 23, 2017 · N911DL · Doug MD88 · Fuselage Floor Panel
  > DAMAGE FERRULES ON FLOOR PANELS NR 465C, 541C,160B, 160E, 256C, 200B, 693C,886C, 1003C, 1003D, 1003. COMPOSITES. FLOOR PANELS NR: 465C, 541C, 160E, 256C, 200B, 693C, 886C, 1003C, 1003D AND 1003E WERE REPLACED FERRULES PER AMM 53-20-01-201. FLOOR PANEL NR 160B

Next page: https://openairdocs.org/deregistered/N911DL-2024-12-30/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 = 'N911DL' AND deregistration_id = 'N911DL-2024-12-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N911DL-2024-12-30/reports

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