# Service difficulty reports: N988DL, cancelled Feb 12, 2021

A list on [N988DL, cancelled Feb 12, 2021](https://openairdocs.org/deregistered/N988DL-2021-02-12.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 · 199 reports

- [SDR DALA2019051603065](https://openairdocs.org/sdr/DALA2019051603065.md): Light · inoperative · May 16, 2019 · N988DL · Doug MD88 · Emergency Lighting
  > EMERGENCY ESCAPE PATH LIGHT INOP AT 11D. REPL LIGHT ASSY PER AMM 33-53. OPS CHECK GOOD. (LP5504375)
- [SDR DALA2019031701761](https://openairdocs.org/sdr/DALA2019031701761.md): Skin · cracked · Mar 16, 2019 · N988DL · Doug MD88 · Fuselage Main, Plate/Skin
  > ON WALK AROUND FOUND 2 CRACKS LEFT SIDE STA 1265.603 6" ABOVE AFT AIRSTAIR DOOR CUTOUT. INSTALLED PERM REPAIR PER SRM 53-01 PAGE 12 FIG 2. (LP5835229)
- [SDR DALA2019012400493](https://openairdocs.org/sdr/DALA2019012400493.md): Screw · missing · Jan 22, 2019 · N988DL · Doug MD88 · Exterior Lighting
  > AFT LEFT WING POSITION LIGHT ASSY LENS COVER MISSING RETAINING SCREW. REPLACED LEFT WING AFT POSITION LIGHT ASSY PER AMM 33-43. SDR REPORTED DUE TO POSSIBILITY THAT PART MAY DEPARTED FROM THE AIRCRAFT DURING FLIGHT. (LP4809128)
- [SDR DALA2018111406618](https://openairdocs.org/sdr/DALA2018111406618.md): Lamp · inoperative · Nov 14, 2018 · N988DL · Doug MD88 · Emergency Lighting
  > SEAT 19 E/D EMER LIGHT INOP. RELAMPED SEAT 19 E/D. CHECKS GOOD. (LP4807188)
- [SDR DALA2018090705495](https://openairdocs.org/sdr/DALA2018090705495.md): Skin · cracked · Sep 6, 2018 · N988DL · Doug MD88 · Fuel Storage
  > FUEL LEAKING FROM LT CENTER TANK. POSSIBLE SKIN CRACK LEFT OF CENTER KEEL BEAM. CRACK INDICATION IN LWR SKIN AT APPROX STA 883 STR 17 BY HFEC IAW MDC 93KO393 NDT SPM PART 6-10-01.001. REPAIR IN REF TO ERA 571124-14AD REV O AND ERA 571160-14 REV O.
- [SDR DALA2018090705494](https://openairdocs.org/sdr/DALA2018090705494.md): Stringer · cracked · Sep 6, 2018 · N988DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > STRINGER 17 LT IS CRACKED AT APPROX LBL15 AT THE O/B END OF THE 5935874-501 FITTING. REPAIRED IN REF TO ERA 571124-14AD REV O AND ERA 571160-14 REV O.
- [SDR DALA2018090705493](https://openairdocs.org/sdr/DALA2018090705493.md): Skin Panel · cracked · Sep 6, 2018 · N988DL · Doug MD88 · Fuselage Main, Plate/Skin
  > SKIN CRACKED FROM EOP THRU FASTENER AND OUT THE OTHER SIDE. LOWER AFT SKIN PANEL P/N 5930503-105 AT STA 883 STRINGER 17. CENTER LT FUEL TANK. APPROX 2 INCHES. REPAIRED IN REF TO ERA 571124-14AD REV O AND ERA 571160-14 REV O.
- [SDR DALA2018090705492](https://openairdocs.org/sdr/DALA2018090705492.md): Skin Panel · cracked · Sep 6, 2018 · N988DL · Doug MD88 · Fuselage Main, Plate/Skin
  > SKIN CRACKED AT FASTENER LOWER FWD SKIN PANEL P/N 5930503-103 AT STA 883 STRINGER 17. CENTER LT FUEL TANK. DIRECTLY FWD OF AFT SKIN CRACK REF NRC. REPAIRED IN REF TO ERA 571124-14AD REV O AND ERA 571160-14 REV O.
- [SDR DALA2017090106521](https://openairdocs.org/sdr/DALA2017090106521.md): Skin · gouged · Aug 31, 2017 · N988DL · Doug MD88 · Leading Edge Devices
  > LEFT WING L/E SLAT NR 3 EXTERNAL SKIN HAS A GOUGE NEXT TO THE END. REMOVED DAMAGE AND EVALUATED, ORIGINAL.100 LOSS.024, REMAINING.076, AND FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-01. REPAIRED AREA IAW ERA 556444-14, REV O.
- [SDR DALA2017083106471](https://openairdocs.org/sdr/DALA2017083106471.md): Strut · damaged · Aug 30, 2017 · N988DL · Doug MD88 · Nose/Tail Landing Gear Strut/Axle
  > DURING NLG SHOCK STRUT SEAL REPLACEMENT, FOUND METERING PIN AND INNER TUBE DAMAGED. REMOVED AND REPLACED NLG METERING PIN, SUPPORT TUBE, RESTRICTOR SUPPORT ASSY HEAD AND LOWER STRUT PISTON ASSY IAW CMM 32-21-04 AND AMDS.
- [SDR DALA2017083106476](https://openairdocs.org/sdr/DALA2017083106476.md): Stand Off · cracked · Aug 28, 2017 · N988DL · Doug MD88 · Fuselage Main, Attach Fittings
  > AUX HYD PUMP POWER CABLE RT WW WIRING STANDOFF SUPPORT BRACKET CRACKED. LOCATED JUST I/B OF THE HYD SERVICE ACCESS PANEL. REMOVED AND INSTALLED THE STAND OFF IAW SRM 51-30-01.
- [SDR DALA2017083006458](https://openairdocs.org/sdr/DALA2017083006458.md): Attach Fitting · cracked · Aug 28, 2017 · N988DL · Doug MD88 · Fuselage Main, Attach Fittings
  > AFT ACCESSORY BAY LT AFT SIDE OF CANTED FRAME 1463 ATTACH CLIP IS CRACKED AROUND INBD FASTENER L7L INSIDE OF LOUVER PANEL REF AA 5310-01456-01.
- [SDR DALA2017030501778](https://openairdocs.org/sdr/DALA2017030501778.md): Lamp · inoperative · Mar 2, 2017 · N988DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHT AT SEAT 17EF IS INOPERATIVE. REPLACED THE LAMPS, OPS CHECKED GOOD IAW AMM 33-53.
- [SDR DALA2017012300583](https://openairdocs.org/sdr/DALA2017012300583.md): Terminal · loose · Jan 21, 2017 · N988DL · Doug MD88 · Passenger Compartment Lighting
  > DURING CRUISE, THE FLIGHT ATTENDANTS DETECTED AN ELECTRICAL ODOR MOST NOTICEABLE AT THE AFT FLIGHT ATTENDANT JUMP SEAT POSITION. THE CREW PERFORMED QRH SMOKE/ODOR PROCEDURE AND DIVERTED TO TPA. MAINTENANCE TROUBLESHOT PER WORK CARD 2120-2367 AND FOUND AFT LEFT
- [SDR DALA2017010200027](https://openairdocs.org/sdr/DALA2017010200027.md): Battery Pack · discharged · Jan 1, 2017 · N988DL · Doug MD88 · Emergency Lighting
  > DURING PREFLIGHT, FOUND EMERGENCY LIGHTS ON AND BATTERIES DEAD LIGHTS WILL COME ON FOR 5 SECONDS THEN DIE. REPLACED THE BATTERY PACKS IAW WORK CARD 3350-7353. EMERGENCY LIGHTS CHECKED GOOD IAW AMM 33-53-00.
- [SDR DALA2016122910134](https://openairdocs.org/sdr/DALA2016122910134.md): Coffeemaker · odor · Dec 28, 2016 · N988DL · Doug MD88 · Buffet/Galleys
  > ENROUTE, DIVERTED DUE TO FLIGHT ATTENDANTS REPORTING AN ELECTRICAL ODOR IN THE FIRST CLASS CABIN. MAINTENANCE FOUND A FORWARD GALLEY COFFEEMAKER HOT PLATE WAS BURNING COFFEE AND CAUSING ELECTRICAL ODOR. THE COFFEE MAKER WAS DEFERRED PER NEF (LP# 9480325) AN
- [SDR DALA2016122109998](https://openairdocs.org/sdr/DALA2016122109998.md): Duct · cracked · Dec 20, 2016 · N988DL · Doug MD88 · Cabin Cooling System
  > VERTICAL RAM AIR INLET DUCT SKIN LEFT SIDE CRACKED DORSAL FIN AREA. CRACK 7" LONG. IAW ENGINEERING PERFORMED DETAILED VISUAL INSP OF CRACK AND SURROUNDING AREA. STOP DRILLED CRACK IAW INSTRUCTIONS.
- [SDR DALA2016122109996](https://openairdocs.org/sdr/DALA2016122109996.md): Duct · cracked · Dec 20, 2016 · N988DL · Doug MD88 · Cabin Cooling System
  > VERTICAL RAM AIR INLET DUCT SKIN CRACKED. REPAIRED IAW SRM 55-05 FIG 3 AND RI 553770-14 REV ORIG.
- [SDR DALA2016121309852](https://openairdocs.org/sdr/DALA2016121309852.md): A/C Pack · failed · Dec 11, 2016 · N988DL · Doug MD88 · Cabin Cooling System
  > THE RIGHT PACK CYCLED TWICE AND SHUTDOWN AND THEN SMOKE WAS REPORTED IN THE AFT CABIN. THE COCKPIT AND CABIN TEMPERATURE SELECTORS WHERE BOTH FOUND IN THE MANUAL FULL HOT POSITION. OVERHEATING OF THE RIGHT PACK WAS SUSPECTED. VERIFICATION OF THE RIGHT ACM'S A
- [SDR DALA2016080805861](https://openairdocs.org/sdr/DALA2016080805861.md): Wire · broken · Aug 8, 2016 · N988DL · Doug MD88 · Light System Wiring
  > AFT CATWALK LOWER CENTER EMERGENCY LIGHT INOPERATIVE. CRIMPED BROKEN WIRE AT CONNECTOR IAW SWPM 20 AND WDM 3351. OPS CHECKED NORMAL.
- [SDR DALA2015080204801](https://openairdocs.org/sdr/DALA2015080204801.md): Floorbeam · corroded · Jul 31, 2015 · N988DL · Doug MD88 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM, BS 1338 BETWEEN X -13 TO -17. FLOORBEAM WAS REPAIRED IAW ER/A 397783-14MA, REV ORIGINAL.
- [SDR DALA2016111108828](https://openairdocs.org/sdr/DALA2016111108828.md): Angle · corroded · Jul 29, 2015 · N988DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEB ANGLE BS 685 - 690 BETWEEN RBL 54 TO 60. AREA WAS REPAIRED IAW ER/A.
- [SDR DALA2015073004752](https://openairdocs.org/sdr/DALA2015073004752.md): Tab · not reported · Jul 29, 2015 · N988DL · Doug MD88 · Standard Practices/Structures
  > BUSHING GEARED TAB ATTACH POINTS WERE REPLACED. FITTING ON GEARED TAB ATTACH POINTS WAS REMOVED AND NEW FITTING WAS DRILLED, TREATED, PAINTED AND INSTALLED IAW CMM 27-30-1, AMM 20-30-01-201, SRM 51-10-4, 51-10-3, PAR 21 AND 14 AND 51-30-2. FREE PLAY WAS CORR
- [SDR DALA2015073004755](https://openairdocs.org/sdr/DALA2015073004755.md): Bushing · corroded · Jul 28, 2015 · N988DL · Doug MD88 · Elevator, Tab Structure
  > FREEPLAY AND CORROSION ON BUSHING OF CONTROL TAB ATTACH POINTS AT RT ELEVATOR. CONTROL TAB ATTACH POINTS WERE REPLACED IAW CMM 27-30-1. FITTING ON BS XET=48.293 WAS REMOVED IAW AMM 20-30-01-201 NEW FITTING WAS DRILLED, TREATED, PAINTED AND INSTALLED IAW SRM
- [SDR DALA2015072904743](https://openairdocs.org/sdr/DALA2015072904743.md): Finger Doubler · corroded · Jul 28, 2015 · N988DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON INNER FINGER DOUBLER BETWEEN BS 1291 - 1295, LONGERONS 25 - 26L. THE FINGER DOUBLER WAS REPAIRED IAW SRM 51-30-2, 53-04, FIG 12E, 51-10-1, FIG 36 AND 51-10-3, PAR 14, 21.
- [SDR DALA2016111108827](https://openairdocs.org/sdr/DALA2016111108827.md): Skin · corroded · Jul 27, 2015 · N988DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON LOWER INTERCOSTAL AT AFT LAVATORY SERVICE PANEL, BETWEEN BS 1322 TO 1338, LONGERONS 21 - 22L. THE INTERCOSTAL WAS REPLACED IAW SRM.
- [SDR DALA2015072904738](https://openairdocs.org/sdr/DALA2015072904738.md): Door Frame · corroded · Jul 27, 2015 · N988DL · Doug MD88 · Fuselage Main, Structure
  > CORROSION ON LOWER DOOR FRAME. REPAIRED IAW SRM 53-05, FIG 123, SRM 51-10-3, PAR 14, 21, AND SRM 51-30-5.
- [SDR DALA2015072804732](https://openairdocs.org/sdr/DALA2015072804732.md): Rib · cracked · Jul 27, 2015 · N988DL · Doug MD88 · Vertical Stabilizer, Spar/Rib
  > CRACKED RIBS ON FIXED L/E OF VERTICAL STABILIZER. RIBS WERE R & R IAW SRM 55-02 D, FIG 27 AND 51-30-5 TO 51-30-2 AND DWGS 9911881, ID, 2 REV C. AND 9911882: ID 2, REV B.
- [SDR DALA2015072804730](https://openairdocs.org/sdr/DALA2015072804730.md): Doubler · worn · Jul 27, 2015 · N988DL · Doug MD88 · Fluid Service Doors
  > WORN INNER DOUBLER OF AFT LAVATORY SERVICE PANEL.
- [SDR DALA2015072804729](https://openairdocs.org/sdr/DALA2015072804729.md): Doubler · worn · Jul 27, 2015 · N988DL · Doug MD88 · Fluid Service Doors
  > WORN INNER DOUBLER OF AFT LAVATORY SERVICE PANEL. DOUBLER WAS BLENDED OUT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1. THE DOUBLER WAS REPLACED IAW DWG 5911423, ITEM 43, REV: CD, SRM 51-30-2 AND 51-30-5.
- [SDR DALA2015072804728](https://openairdocs.org/sdr/DALA2015072804728.md): Tray · corroded · Jul 27, 2015 · N988DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT LAVATORY SERVICE PANEL TRAY. EXCESSIVE CORROSION ON PANEL TRAY WAS REPLACED IAW DWG 5914792, ITEM 3, REV: AG AND SRM 51-10-4, 51-30-2 AND 51-30-5.
- [SDR DALA2016111108826](https://openairdocs.org/sdr/DALA2016111108826.md): Cargo Track · corroded · Jul 26, 2015 · N988DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON THE LEFT CARGO TRACK BETWEEN BS 1007 TO 1322 IN THE AFT CARGO COMPARTMENT. A NEW CARGO TRACK WAS INSTALLED IAW SRM.
- [SDR DALA2015072704720](https://openairdocs.org/sdr/DALA2015072704720.md): Finger Doubler · corroded · Jul 26, 2015 · N988DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON THE FINGER DOUBLER BETWEEN LONGERONS 25-26L BS 1209 - 1212, 1228 - 1231. THE FINGER DOUBLER WAS REPAIRED IAW SRM 53-04, FIG 12E, 51-30-2, 51-30-5 AND 51-10-3, PAR 38.
- [SDR DALA2015072704719](https://openairdocs.org/sdr/DALA2015072704719.md): Finger Doubler · cracked · Jul 26, 2015 · N988DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CRACKED FINGER DOUBLER BETWEEN LONGERON 25-26L BS 1174 - 1193. THE FINGER DOUBLER WAS REPAIRED IAW SRM 53-04, FIG 12E, 51-30-2, 51-30-5 AND 51-10-3, PAR 38.
- [SDR DALA2015072904740](https://openairdocs.org/sdr/DALA2015072904740.md): Skin · corroded · Jul 25, 2015 · N988DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION BETWEEN DOUBLER AND SKIN AT AFT LAVATORY SERVICE PANEL, BETWEEN BS 1307 - 1322, LONGERONS 21-22L. REPAIRED IAW ETI 88-15-248, REV 2 AND ER/A 536500-14, REV:ORIG.
- [SDR DALA2015072704722](https://openairdocs.org/sdr/DALA2015072704722.md): Skin · dented · Jul 25, 2015 · N988DL · Doug MD88 · Trailing Edge Flaps
  > DENTS FOUND ON REPAIR OF INBD GUIDE VANE LOWER SURFACE ON LT WING INBD FLAP. THE REPAIR WAS REPLACED IAW SRM 57-03D.
- [SDR DALA2015072704721](https://openairdocs.org/sdr/DALA2015072704721.md): Frame · cracked · Jul 25, 2015 · N988DL · Doug MD88 · Fuselage Main, Frame
  > CRACKS FOUND ON FRAME, BS 1510. THE FRAME WAS REPLACED IAW DWG 9911843, REV SRM 51-30-2, 51-10-4, AND 51-10-3.
- [SDR DALA2015072704718](https://openairdocs.org/sdr/DALA2015072704718.md): Hinge · cracked · Jul 25, 2015 · N988DL · Doug MD88 · Fuselage, Door Hinge
  > A CRACK WAS FOUND ON AFT VENTRAL DOOR UNDER UPPER HINGE FITTING. REPAIRED IAW SRM 51-30-2 AND 51-30-1, 51-10-3, PAR 14/21, 51-01, PAR 4 CAP 21 AND 52-05D, FIG 34.
- [SDR DALA2015072604717](https://openairdocs.org/sdr/DALA2015072604717.md): Skin · dented · Jul 25, 2015 · N988DL · Doug MD88 · Trailing Edge Flaps
  > DENTS FOUND ON PREVIOUS REPAIR OF MID GUIDE VANE ON THE LT WING OTBD FLAP. A NEW DOUBLER WAS INSTALLED IAW SRM 57-03, PARR II.
- [SDR DALA2015072604716](https://openairdocs.org/sdr/DALA2015072604716.md): Pan · cracked · Jul 25, 2015 · N988DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED INNER PAN BELOW STOP FITTING NR 3 IN FWD CARGO BAY AFT EDGE. REPAIR WAS ACCOMPLISHED IAW SRM 52-05D, FIG 50. CRACK LONG 0.150".
- [SDR DALA2015072604715](https://openairdocs.org/sdr/DALA2015072604715.md): Longeron · corroded · Jul 25, 2015 · N988DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CORROSION ON PREVIOUS REPAIR OF LONGERON 29L BETWEEN BS 1231 - 1250. THE REPAIR WAS REPLACED IAW SRM 51-30-5, PAR 13, SRM 53-02, FIG 19, AND SRM 51-10-3, PAR 21, 14 AND 38.
- [SDR DALA2015072604714](https://openairdocs.org/sdr/DALA2015072604714.md): Intercostal · cracked · Jul 25, 2015 · N988DL · Doug MD88 · Fuselage Miscellaneous Structure
  > A CRACK WAS FOUND ON THE INTERCOSTAL BETWEEN LONGERONS 27-28L. BS 1309 - 1322. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, AND 51-10-3, PAR 14 AND 21.
- [SDR DALA2015072604713](https://openairdocs.org/sdr/DALA2015072604713.md): Frame · cracked · Jul 25, 2015 · N988DL · Doug MD88 · Fuselage Main, Frame
  > CRACKED FRAME BS 1451, BETWEEN LONGERONS 1-3L. THE FRAME WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, AND 51-10-3 PAR 14,21.
- [SDR DALA2015072604712](https://openairdocs.org/sdr/DALA2015072604712.md): Cargo Track · corroded · Jul 25, 2015 · N988DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON THE RT CARGO TRACK BETWEEN BS 1212 - 1322, UPPER AND LOWER SURFACES. THE CARGO TRACK WAS REMOVED AND REPLACED IAW IAW SRM 51-10-3, PAR 21, 14, AND 51-30-1.
- [SDR DALA2015072604711](https://openairdocs.org/sdr/DALA2015072604711.md): Cargo Track · corroded · Jul 25, 2015 · N988DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RT CARGO TRACK BETWEEN BS 1007 - 1155, UPPER AND LOWER SURFACES. DAMAGE CARGO TRACK WAS REMOVED, AND A NEW CARGO TRACK WAS DRILLED, TREATED AND PAINTED. THE CARGO TRACK WAS INSTALLED IAW SRM 51-30-1,51-10-4, AND 51-10-3 PAR 21,14.
- [SDR DALA2015072504707](https://openairdocs.org/sdr/DALA2015072504707.md): Rib · cracked · Jul 24, 2015 · N988DL · Doug MD88 · Vertical Stabilizer, Spar/Rib
  > CRACKED RIBS ON FIXED L/E OF VERTICAL STABILIZER, THE RIBS WERE REPAIRED AND REPLACED IAW SRM 55-02D, FIG 27 AND 51-30-5 TO 51-30-2 AND DWG 9911881, ID, 2 REV. C AND 9911882. ID, 2, REV B.
- [SDR DALA2015072504705](https://openairdocs.org/sdr/DALA2015072504705.md): Longeron · corroded · Jul 24, 2015 · N988DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 22L BETWEEN BS 1287 - 1309 IN CARGO BAY. THE LONGERON WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-3, PAR 14 AND 21.
- [SDR DALA2015072504704](https://openairdocs.org/sdr/DALA2015072504704.md): Skin · damaged · Jul 24, 2015 · N988DL · Doug MD88 · Rudder, Tab Structure
  > DAMAGED METALLIZED SKIN ON RUDDER CONTROL TAB. METALLIZED SKIN WAS REPAIRED IAW SRM 51-70-1A, PAR 23 AND JIC 2000-8149-16.
- [SDR DALA2016111108825](https://openairdocs.org/sdr/DALA2016111108825.md): Skin · corroded · Jul 23, 2015 · N988DL · Doug MD88 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN & INTERNAL DOUBLER AT THE AFT LAV WASTE PANEL BS 1307-1322, L21 - 22L, WERE CORRODED AND REQUIRED REPAIR DOUBLERS.
- [SDR DALA2015072304588](https://openairdocs.org/sdr/DALA2015072304588.md): Longeron · cracked · Jul 22, 2015 · N988DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK FOUND ON LONGERON 6L BS 693. THE LONGERON WAS REPAIRED IAW ER/A 536506-14 REV. ORIGINAL.

Next page: https://openairdocs.org/deregistered/N988DL-2021-02-12/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 = 'N988DL' AND deregistration_id = 'N988DL-2021-02-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N988DL-2021-02-12/reports

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