# Service difficulty reports: N954DL, cancelled Jan 24, 2020

A list on [N954DL, cancelled Jan 24, 2020](https://openairdocs.org/deregistered/N954DL-2020-01-24.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 · 94 reports

- [SDR DALA201902010662](https://openairdocs.org/sdr/DALA201902010662.md): Windshield Wiper · detached · Jan 29, 2019 · N954DL · Doug MD88 · Windshield/Door Rain/Ice Removal
  > WINSHIELD WIPER ON CO-PILOT SIDE FELL OFF AIRPLANE ON APPROCH. R/R WIPER ARM AND BLADE PER MD 88 AMM 30-43. OPS CK. NML. OK FOR SERV. (LP3759244)
- [SDR DALA2019010900110](https://openairdocs.org/sdr/DALA2019010900110.md): Oven · smoke · Jan 8, 2019 · N954DL · Doug MD88 · Buffet/Galleys
  > OVEN NEEDS TO BE CLEANED. BAD SMELL LIKE CLEANER AND SMOKE WHEN COOKING. C/W SMOKE/ODOR T/S PER W/C 2120-2367. VERIFIED FWD GALLEY OVEN INTERIOR SMELL AS SOURCE OF SMELL. REPLACED FWD GALLEY OVEN PER AMM 25-30. C/W ALL ODI REQUIREMENTS PER W/C 2120-2367. OVEN,
- [SDR DALA2018072304607](https://openairdocs.org/sdr/DALA2018072304607.md): Wire · shorted · Jul 23, 2018 · N954DL · Doug MD88 · Light System Wiring
  > SEAT EMERGENCY LIGHTS INOP FROM 31ED AFT TO TAILCONE AREA. FOUND WIRE L982U14 GROUNDING OUT/CHAFFED AT LIGHT ASSY L2-848. REPAIRED WIRE AND REPLACED FUSE AT BATTERY PACK B5-212 PER SWPM CH.20. CKS GOOD. OK FOR SVC.
- [SDR DALA2018072404636](https://openairdocs.org/sdr/DALA2018072404636.md): Floor Panel · damaged · Jul 22, 2018 · N954DL · Doug MD88 · Fuselage Floor Panel
  > CABIN CARPET (AISLE AND CROSS-AISLE) WORN/TORN/FRAYED/MISSING. AC FLOORING SOFT BETWEEN 10ABC AND 10DE AND 4AB AND 4CB / INTERIOR. FOUND DAMAGE TO EXTEND WITHIN 3" OF PANEL EDGE. REMOVED SEAT ROW 10ABC FOR ACCESS. REMOVED FLOOR PANEL 9936585-2. FABRICATED NEW
- [SDR DALA2018071204451](https://openairdocs.org/sdr/DALA2018071204451.md): Wire · broken · Jul 12, 2018 · N954DL · Doug MD88 · Light System Wiring
  > EMERGENCY LIGHT ON SEAT 34D INOP. REPAIRED BROKEN WIRING IAW AMM 20-50. OPS CHECK GOOD.
- [SDR DALA2018070604389](https://openairdocs.org/sdr/DALA2018070604389.md): Power Supply · inoperative · Jul 6, 2018 · N954DL · Doug MD88 · Emergency Lighting
  > ON SVC CK, FOUND SEATS 31-36 EMERGENCY LIGHT AND AFT STAIRS EMERGENCY LIGHTS INOP. T/S PER AMM 33-50-00-001. FOUND EMERGENCY LIGHT BATTERY PACK B5-212 POWER SUPPLY INOP. REPLACED POWER SUPPLY ASSY IAW AMM 33-53. OPS CK NML. OK FOR SVC.
- [SDR DALA2018080304839](https://openairdocs.org/sdr/DALA2018080304839.md): Skin · corroded · Jun 29, 2018 · N954DL · Doug MD88 · Fuselage Main, Plate/Skin
  > REPAIR OF CORROSION AT AFT LAV SERVICE PANEL CUTOUT, STA 1322 BETWEEN L-21L AND L-22L. REPAIRED AFT LAV SERVICE PANEL CUTOUT PER ER/A 569781-14.
- [SDR DALA2018070304327](https://openairdocs.org/sdr/DALA2018070304327.md): Skin · cracked · Jun 29, 2018 · N954DL · Doug MD88 · Fuselage Main, Plate/Skin
  > FOUND SKIN CRACK AT LWR FWD CORNER OF AFT LAV PAN. REPAIRED PER ERA 569781-14 REV ORIGINAL.
- [SDR DALA2018043002898](https://openairdocs.org/sdr/DALA2018043002898.md): Frame · cracked · Apr 29, 2018 · N954DL · Doug MD88 · Aerodynamic Fairings
  > TAIL CONE ATTACH CANTED FRAME BS 1310 WAS FOUND CRACKED, TWO AREAS 2:00 & 7:00 O`CLOCK. REPLACED THE FRAME IAW DRAWING 5966769.
- [SDR DALA2018043002891](https://openairdocs.org/sdr/DALA2018043002891.md): Support Angle · cracked · Apr 29, 2018 · N954DL · Doug MD88 · Aerodynamic Fairings
  > TAIL CONE LT UPPER LOCK BAYONET RECEPTACLE, UPPER SUPPORT ANGLE CRACKED. REPLACED THE SUPPORT ANGLE IAW DWG 9911957.
- [SDR DALA2018030901514](https://openairdocs.org/sdr/DALA2018030901514.md): Battery Pack · inoperative · Mar 3, 2018 · N954DL · Doug MD88 · Emergency Lighting
  > TAIL COMPARTMENT CENTER STAIR LIGHT INOPERATIVE. FOUND BATTERY PACK INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-50.
- [SDR DALA2018012200325](https://openairdocs.org/sdr/DALA2018012200325.md): Battery Pack · inoperative · Jan 20, 2018 · N954DL · Doug MD88 · Smoke Detection
  > RIGHT AFT LAVATORY, CREW REPORTED A CHIRPING NOISE. REPLACED THE LAVATORY SMOKE DETECTOR BATTERY. OPS CHECKED GOOD IAW AMM 26-13.
- [SDR DALA2017101807628](https://openairdocs.org/sdr/DALA2017101807628.md): Wire · broken · Oct 18, 2017 · N954DL · Doug MD88 · Light System Wiring
  > SEAT 22DE EMERGENCY LIGHT INOPERATIVE. FOUND A WIRE BROKEN AT THE SEAT FRAME, TERMINATED THE WIRE AS REQUIRED.
- [SDR DALA2017011600365](https://openairdocs.org/sdr/DALA2017011600365.md): Skin · cracked · Jan 15, 2017 · N954DL · Doug MD88 · Fuselage Main, Plate/Skin
  > TWO CRACKS WERE FOUND ON FUSELAGE SKIN AT THE BS 1437 AND BETWEEN LONGERON 3 AND 4L. THE SKIN WAS REPAIRED IAW ETI-88-17-005 REV 2 AND ER/A 552912-14 REV. ORIG.
- [SDR DALA2017011600363](https://openairdocs.org/sdr/DALA2017011600363.md): Skin · cracked · Jan 15, 2017 · N954DL · Doug MD88 · Fuselage Main, Plate/Skin
  > A CRACK WAS FOUND ON THE SKIN AT BS 1437 BETWEEN LONGERONS 1 - 2L. THE SKIN WAS REPAIRED IAW ETI-88-17-005 REV 2 AND ER/A 552912-14 REV. ORIG.
- [SDR DALA2017011600362](https://openairdocs.org/sdr/DALA2017011600362.md): Frame · cracked · Jan 15, 2017 · N954DL · Doug MD88 · Fuselage Main, Frame
  > DURING BHEC INSPECTION, A CRACK WAS FOUND ON CAP AT BS 1437 BETWEEN LONGERONS 1-2L. THE CAP WAS REPAIRED IAW ETI-88-17-003 REV. 3 AND ER/A 552910-14 REV. ORIGINAL.
- [SDR DALA2017011600371](https://openairdocs.org/sdr/DALA2017011600371.md): Floor Support · corroded · Jan 14, 2017 · N954DL · Doug MD88 · Fuselage Miscellaneous Structure
  > PAX CABIN. CORROSION ON FLOOR SUPPORT BETWEEN BS 160 TO 200 AT LBL 54. THE FLOOR SUPORT WAS REPLACED IAW SRM 53-14-1 FIGURE 11 AND 51-30-5.
- [SDR DALA2017011400321](https://openairdocs.org/sdr/DALA2017011400321.md): Static Port · damaged · Jan 13, 2017 · N954DL · Doug MD88 · Pitot/Static System
  > RT ALTERNATE STATIC PORT WAVINESS IS OUT OF LIMITS ON CRITICAL AREA. (MAX 0.006 IN - HAS 0.010 IN) WAVINESS CAUSED BY A PREVIOUS BLEND OUT. REPAIRED PER SRM 53-04 FIG 12C(SHEET 5).
- [SDR DALA2017011100241](https://openairdocs.org/sdr/DALA2017011100241.md): Skin · dented · Jan 10, 2017 · N954DL · Doug MD88 · Trailing Edge Flaps
  > SKIN DENTED ON MID VANE OF LT WING TE FLAP. REPAIRED IAW SRM 57-03D P.11, AND 51-70-2D.
- [SDR DALA2017011100240](https://openairdocs.org/sdr/DALA2017011100240.md): Pan · corroded · Jan 10, 2017 · N954DL · Doug MD88 · Fuselage Main, Structure
  > CORROSION ON PAN OF CARGO LOWER DOOR FRAME BS 370 - 427. THE PAN WAS REPAIRED IAW SRM 53-05 PAR 55A FIG.44A.
- [SDR DALA2017010900213](https://openairdocs.org/sdr/DALA2017010900213.md): Doubler · corroded · Jan 8, 2017 · N954DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERNAL DOUBLER AROUND AFT LAVATORY SERVICE PANEL CUT OUT. DAMAGE AREA WAS ACCOMPLISHED PER ERA 552906-14 REV. ORG. AND ETI-88-17-001 REV. 2.
- [SDR DALA2017010900211](https://openairdocs.org/sdr/DALA2017010900211.md): Skin · corroded · Jan 8, 2017 · N954DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON FUSELAGE SKIN AROUND AFTER LAVATORY SERVICE PANEL. REPAIRED IAW ERA 552906-14 REV. ORG. AND ETI-88-17-001 REV. 2.
- [SDR DALA2017010800207](https://openairdocs.org/sdr/DALA2017010800207.md): Longeron · corroded · Jan 7, 2017 · N954DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY HAS CORROSION ON LONGERON 28R AND BS 1287. THE LONGERON WAS REPAIRED IAW SRM 53-02 PAR 13 FIG 19.
- [SDR DALA2017010700203](https://openairdocs.org/sdr/DALA2017010700203.md): Skin · cracked · Jan 6, 2017 · N954DL · Doug MD88 · Nacelle/Pylon, Plate/Skin
  > CRACKED LT PYLON UPPER SKIN. TRAILING EDGE PYLON LH WAS REMOVED AND INSTALLED IAW SRM 51-30-1. HFEC INSPECTION WAS ACCOMPLISHED.
- [SDR DALA2017010600134](https://openairdocs.org/sdr/DALA2017010600134.md): Door Frame · corroded · Jan 5, 2017 · N954DL · Doug MD88 · Fuselage Main, Structure
  > MID CARGO COMPARTMENT, CORROSION ON DOOR JAMB BTW STA Y= 636 AND STA Y= 693 BTW LONGERON 28R AND 27R. DOUBLER WAS REPLACED PER SRM 53-05 PAR 140 FIG 123.
- [SDR DALA2017010500125](https://openairdocs.org/sdr/DALA2017010500125.md): Fitting · cracked · Jan 4, 2017 · N954DL · Doug MD88 · Service Doors
  > CRACKED AFT EDGE CLIP ON BEAM NR 1 AT FWD SERVICE DOOR. CRACK CLIP WAS REPLACED FOR ONE NEW PER SRM 51-30-05.
- [SDR DALA2017010500072](https://openairdocs.org/sdr/DALA2017010500072.md): Longeron · cracked · Jan 4, 2017 · N954DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > PAX CABIN, CRACKED LONGERON 3L ON STA Y=160 AT CABIN CROWN. LONGERON SECTION WAS REPAIRED PER 53-02 PAR 12 FIG 18 AND INSTALLED PER SRM 51-30-5, 51-30-2.
- [SDR DALA2017010500071](https://openairdocs.org/sdr/DALA2017010500071.md): Beam · cracked · Jan 4, 2017 · N954DL · Doug MD88 · Passenger/Crew Doors
  > CRACKED AFT EDGE BEAM NR 2 ON MAIN ENTRANCE DOOR. BEAM NR 2 WAS REPAIRED PER SRM 52-05 REPAIR 69 FIGURE 83.
- [SDR DALA2017010300031](https://openairdocs.org/sdr/DALA2017010300031.md): Beam · cracked · Jan 2, 2017 · N954DL · Doug MD88 · Passenger/Crew Doors
  > CRACKED FWD EDGE BEAM NR 1 AT MAIN ENTRANCE DOOR. THE BEAM WAS REPAIRED IAW SRM 52-05 FIG.98 SHEET 3.
- [SDR DALA2016060804487](https://openairdocs.org/sdr/DALA2016060804487.md): Liner · debonded · Jun 7, 2016 · N954DL · Doug MD88 · Nacelle/Pylon Structure
  > PERFORMED DUE TO REPORT OF RT ENGINE COMPRESSOR STALL. FOUND ACOUSTIC LINER DIS-BONDED FRONT OF ENGINE NEAR THE BLEED VALVES. THE ENGINE WAS REPLACED.
- [SDR DALA2016060604362](https://openairdocs.org/sdr/DALA2016060604362.md): Floorboard · damaged · Jun 6, 2016 · N954DL · Doug MD88 · Fuselage Floor Panel
  > ALLEY FLOOR IS DEPRESSED SLIGHTLY APPROXIMATELY 12" X 18" LOCATED JUST INBD OF THE 2L DOOR THERE IS A SLIGHT RISE IN THE FLOOR ALONG THE INBOARD EDGE. R & R FLOORBOARD INBD OF 2R DOOR AND REPLACED GALLEY MATERIAL.
- [SDR DALA2016060604360](https://openairdocs.org/sdr/DALA2016060604360.md): Cable · damaged · Jun 6, 2016 · N954DL · Doug MD88 · Aerodynamic Fairings
  > TAILCONE KEVLAR CABLE DAMAGED. REPLACED KEVLAR CABLE REF. AMDS CARD 5350-01077-0101.
- [SDR DALA2016053104189](https://openairdocs.org/sdr/DALA2016053104189.md): Turbine · failed · May 29, 2016 · N954DL · Doug MD88 · Turbine Section
  > RETURNED TO DEPARTURE DUE TO A RT ENGINE TURBINE FAILURE DURING CLIMB AT AT 800-1000 FT. RT ENGINE WAS SHUTDOWN IFSD. CREW NOTED MAXIMUM EGT 800DEG. MAINTENANCE FOUND TURBINE DAMAGE AND AN ENGINE CHANGE WAS REQUIRED. ENGINE WAS REPLACED AND SUBSEQUENT CHEC
- [SDR DALA2016052404134](https://openairdocs.org/sdr/DALA2016052404134.md): Battery Pack · discharged · May 24, 2016 · N954DL · Doug MD88 · Emergency Lighting
  > AFT CEILING LIGHTS, EMERGENCY, INOPERATIVE. CHANGED BATTERY'S AD2013-1A, 2 EACH. OPS CHECK GOOD.
- [SDR DALA2016042603272](https://openairdocs.org/sdr/DALA2016042603272.md): Target · damaged · Apr 25, 2016 · N954DL · Doug MD88 · Landing Gear Position and Warning
  > AFTER EXTENDING THE LANDING GEAR IN PREPARATION FOR LANDING, CREW REPORTED MLG DOOR OPEN LIGHT ILLUMINATED. ACCOMPLISHED QRH PROCEDURE AND PERFORMED AN ALTERNATE GEAR EXTENSION RESULTING IN BOTH MAIN GEAR DOORS CONTACTING THE RUNWAY DURING LANDING. MAINTENANC
- [SDR DALA2016042003119](https://openairdocs.org/sdr/DALA2016042003119.md): Pump · failed · Apr 19, 2016 · N954DL · Doug MD88 · Hydraulic Pump (Electric/Engine), Main
  > RIGHT HYDRAULIC QTY DROPPED TO 2 QTS AND AFTER GEAR AND FLAPS WERE LOWERED QTY WENT TO 0 QTS. FOLLOWED BY PRESSURE DROPPING TO 0 PSI. REPLACED RT ENGINE DRIVEN HYD PUMP.
- [SDR DALA2016031101874](https://openairdocs.org/sdr/DALA2016031101874.md): Wire Harness · damaged · Mar 10, 2016 · N954DL · Doug MD88 · Light System Wiring
  > THE FLIGHT CREW FOUND 1 RED EMERGENCY LIGHT INOPERATIVE AT SEAT ROW 24DE. MCO MAINTENANCE REPLACED THE HARNESS ASSY AND THE LIGHT CHECKED OK.
- [SDR DALA2016021801248](https://openairdocs.org/sdr/DALA2016021801248.md): Control Box · failed · Feb 17, 2016 · N954DL · Doug MD88 · Brake Anti-Skid Section
  > RIGHT OTBD ANTI-SKID LIGHT ILLUNINATED ON OAP AFTER GEAR WAS LOWERED. CREW DECLARED EMERGENCY. REPLACED ANTI-SKID CONTROL BOX AND RIGHT OTBD A/S TRANSDUCER.
- [SDR DALA2015092405808](https://openairdocs.org/sdr/DALA2015092405808.md): Skin · corroded · Sep 20, 2015 · N954DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING WALK AROUND FOUND FUSELAGE SKIN PILLOWED AND CRACKED AT BS 610 AND STR 28R. REMOVED MID CARGO SLANT AND FLOOR PANEL FWD OF DOORWAY TO GET ACCESS TO CORROSION. REINSTALLED CARGO SLANT PANEL AND FLOOR PANEL FWD OF DOOR WAY IAW AMM 25-52. REPAIRED IAW ER
- [SDR DALA2015031002109](https://openairdocs.org/sdr/DALA2015031002109.md): Oven · odor · Mar 9, 2015 · N954DL · Doug MD88 · Buffet/Galleys
  > ON CLIMBOUT A STRONG ELECTRICAL ODOR WAS NOTICED THROUGHOUT CABIN AND COCKPIT IAW SMOKE AND FUMES CHECKLIST. TURNED GALLEY POWER OFF AND ELECTRICAL ODOR DISSIPATED. CONTINUED FLIGHT WITH GALLEY POWER OFF. PERFORMED PNEUMATIC DISTRIBUTION CABIN SMOKE/ODOR TRO
- [SDR DALA2015012000442](https://openairdocs.org/sdr/DALA2015012000442.md): Wire Harness · damaged · Jan 16, 2015 · N954DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS AT 24DE TO BE INOPERATIVE. MAINTENANCE REPLACED THE PIGTAIL LIGHT ASSEMBLY AT SEAT 20DE AND THE OPS CHECK WAS GOOD.
- [SDR DALA14021040954](https://openairdocs.org/sdr/DALA14021040954.md): Battery Pack · inoperative · Apr 5, 2014 · N954DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS IN COCKPIT AND AT DOORS L1 & R1 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECKED GOOD.
- [SDR DALA14021030954](https://openairdocs.org/sdr/DALA14021030954.md): Battery Pack · inoperative · Apr 5, 2014 · N954DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS AT ROWS 11-20 AND 27 & AFT WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND OPS CHECKED GOOD.
- [SDR DALA13069770954](https://openairdocs.org/sdr/DALA13069770954.md): Connector · damaged · Dec 16, 2013 · N954DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT SEAT 27D INOPERATIVE. MAINTENANCE REPLACED THE CONNECTOR WIRES AND THE SYSTEM RETURNED TO NORMAL OPERATION.
- [SDR DALA13034490954](https://openairdocs.org/sdr/DALA13034490954.md): Lanyard · missing · Jul 8, 2013 · N954DL · Doug MD88 · Escape Slide
  > INSPECTION DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE IN THE TAILCONE HAD THE LANYARD PULLED FROM ITS OUTER PROTECTIVE SLEEVE. THE TAILCONE SLIDE LANYARD WAS REPLACED.
- [SDR DALA13033740954](https://openairdocs.org/sdr/DALA13033740954.md): Frame · cracked · Jun 28, 2013 · N954DL · Doug MD88 · Fuselage Main, Frame
  > BS 1437. STR 1, FRAME CRACKED. REMOVED FASTENERS, STRIPPED DAMAGE AREA, COMPLETED NDT INSPECTION AT AREA IAW NDT SPM 06-10-01. CUT OUT DAMAGE AREA, FABRICATED, AND INSTALLED REPAIR PARTS IAW SRM 53-03 FIG 4.
- [SDR DALA13032730954](https://openairdocs.org/sdr/DALA13032730954.md): Skin · damaged · Jun 28, 2013 · N954DL · Doug MD88 · Passenger/Crew Doors
  > L1 DOOR EXTERNAL LOWER SKIN PREVIOUS REPAIR DAMAGE ALONG LENGTH OF DOOR. REMOVED DOUBLER AND INSTALLED NEW ONE. REPAIR ALL IAW SRM 52-05D, FIG 37, 51-10-3, AMM 52-11-02 & PSM 900-5-1, NR 4.
- [SDR DALA13031860954](https://openairdocs.org/sdr/DALA13031860954.md): Cusp Web · corroded · Jun 20, 2013 · N954DL · Doug MD88 · Fuselage Miscellaneous Structure
  > RT SIDE CUSP WEB BETWEEN BS 1174 AND 1193, RBL-58 CORRODED. BLENDED TWO AREAS OF CORROSION, BS 1174-1193 RT IAW ER/A 508307-14MA, REV A. MATERIAL REMAINING IS.010 IAW SRM 53-14-3 FIG 12, SHEET 1 AND 2. FOUND TO BE OUT OF LIMITS IAW ER/A 508307MA, REV A.
- [SDR DALA13031850954](https://openairdocs.org/sdr/DALA13031850954.md): Cusp Web · corroded · Jun 20, 2013 · N954DL · Doug MD88 · Fuselage Main, Frame
  > RT SIDE CUSP WEB BETWEEN BS 1193 AND 1212, RBL-58 CORRODED. BLENDED CORROSION FROM FS 1202-1206 RT IAW ERA 508307-14MA, REV A. CORROSION AF FS 1202 TO 1206 RT GOES THROUGH MATERIAL WITH ZERO MATERIAL REMAINING. FOUND TO BE OUT OF LIMITS IAW ER/A 508307-14M
- [SDR DALA13029260954](https://openairdocs.org/sdr/DALA13029260954.md): Cusp Web · corroded · Jun 12, 2013 · N954DL · Doug MD88 · Fuselage Miscellaneous Structure
  > RIGHT SIDE CUSP WEB BS 1110, RBL 58 CORRODED. REPAIRED IAW SRM 53-05, FIG 131A-2, 51-30-5, 51-30-2.

Next page: https://openairdocs.org/deregistered/N954DL-2020-01-24/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 = 'N954DL' AND deregistration_id = 'N954DL-2020-01-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N954DL-2020-01-24/reports

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