# Service difficulty reports: N977DL, cancelled Sep 6, 2019

A list on [N977DL, cancelled Sep 6, 2019](https://openairdocs.org/deregistered/N977DL-2019-09-06.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 5 · 239 reports

- [SDR DALA2019032901995](https://openairdocs.org/sdr/DALA2019032901995.md): Cable · burned · Mar 27, 2019 · N977DL · Doug MD88 · Electrical Power System Wiring
  > DURING WAKE UP CHECK LIST AMP INDICATION NO SHOW. ELECTRICAL CABLE P44A24 AND C/B WERE FOUND BURNED, CABLE AND C/B B1-171 WERE REPLACED PER MD88 SWPM 20-10-06 AMD AMM 24-00-00. TEST WAS PERFORMED PER AMM 24-30-02 TEST OK. (LP4883756)
- [SDR DALA2019032801990](https://openairdocs.org/sdr/DALA2019032801990.md): Fastener · loose · Mar 27, 2019 · N977DL · Doug MD88 · Vertical Stabilizer, Plate/Skin
  > AWR. IN REFERENCE AMDS 5530-01045-05 STEP 2 LOOSE FASTENERS WAS FOUND ON VERTICAL STABILIZER LEADING EDGE STA ZFS: 52.26. FASTENERS ON VERTICAL STABILIZER LEADING EDGE STA ZFS: 52.26 WERE REPLACED PER ETI-88-19-028 REV.2 AND ERA 576759-14AD REV. ORIGINAL. SECT
- [SDR DALA2019032901993](https://openairdocs.org/sdr/DALA2019032901993.md): Skin · damaged · Mar 26, 2019 · N977DL · Doug MD88 · Vertical Stabilizer, Plate/Skin
  > STABILIZERS VERTICAL FIXED LE SKIN, ZFS. ELONGATED HOLES. DTA MONITOR INSPECTION LOG REFERENCE ER/A 576759-14AD SECTION II REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS. DISCONTINUE REVENUE SERVICE ON OR BEFORE THE NEXT 24 MONTHS PENDING A DAMAGE TOLER
- [SDR DALA2019032601911](https://openairdocs.org/sdr/DALA2019032601911.md): Doubler · cracked · Mar 25, 2019 · N977DL · Doug MD88 · Wing, Plate/Skin
  > INITIAL INSPECTION: CRACK ON DOUBLER REPAIR OF LEADING EDGE BTW XRS= 190 AND XRS= 210 LT WING. DOUBLER REPAIR OF LEADING EDGE BTW XRS= 190 AND XRS= 210 LT WING WAS REPLACED PER ETI-88-19-026 REV. ORIGINAL AND ER/A 532516-14 REV A SECTION III. (LP1001760)
- [SDR DALA2019032501887](https://openairdocs.org/sdr/DALA2019032501887.md): Spacer · corroded · Mar 24, 2019 · N977DL · Doug MD88 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION AT SPACER OF THE CENTER LOWER CARGO DOOR JAMB BEAM. (CORROSION LEVEL 2): SPACER WAS REPLACED PER SRM 53-05 FIG 123A (SHEET1). (LP1000032)
- [SDR DALA2019032301883](https://openairdocs.org/sdr/DALA2019032301883.md): Doubler · worn · Mar 22, 2019 · N977DL · Doug MD88 · Passenger/Crew Doors
  > INITIAL INSPECTION: WEAR ON REPAIR DOUBLER AT EXT USELAGE SKIN FWD PASSENGER DOOR ( L1) PROJECTION LONG 16/ 15L AT FUSELAGE. REPAIR DOUBLER AT EXT FUSELAGE SKIN FWD PASSENGER DOOR, PROJECTION LONG 16/ 15L WAS REPLACED PER SRM 52-05 PAR. 17 FIG. 20A. (LP09970
- [SDR DALA2019032201843](https://openairdocs.org/sdr/DALA2019032201843.md): Skin · worn · Mar 21, 2019 · N977DL · Doug MD88 · Trailing Edge Flaps
  > WEAR AT UPPER PREVIOUS REPAIR SKIN ON INTERNAL VANE GUIDE AT OUTBOARD FLAP RT WING. INTERNAL VANE GUIDE AT OUTBOARD FLAP RT WING WAS REPAIRED PER SRM 57-03D. (LP0995827)
- [SDR DALA2019031801764](https://openairdocs.org/sdr/DALA2019031801764.md): Spacer · corroded · Mar 17, 2019 · N977DL · Doug MD88 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION AT SPACER OF THE AFT LOWER CARGO DOOR JAMB BEAM. (CORROSION LEVEL 2): SPACER OF THE AFT LOWER CARGO DOOR JAMB BEAM WAS REPLACED PER SRM 53-05 FIG. 123. (LP0990137)
- [SDR DALA2019020400703](https://openairdocs.org/sdr/DALA2019020400703.md): Bulb · inoperative · Feb 3, 2019 · N977DL · Doug MD88 · Emergency Lighting
  > 23D SEAT EMERGENCY LIGHT OUT. R/R BULB AT SEAT 23D PER STANDARD PRACTICE. (LP4807909)
- [SDR DALA2019012100375](https://openairdocs.org/sdr/DALA2019012100375.md): Skin · cracked · Jan 20, 2019 · N977DL · Doug MD88 · Fuselage Main, Plate/Skin
  > FOUND CRACK AT STA. 1474 LEFT SIDE FWD OF TAILCONE SLIDE HANDLE. REPAIRED PER SRM 53-01 FIG 2 SHEET 3. (LP5088564)
- [SDR DALA2018111506633](https://openairdocs.org/sdr/DALA2018111506633.md): Bottle · low pressure · Nov 15, 2018 · N977DL · Doug MD88 · Escape Slide
  > DURING SVC, FOUND L1 DOOR SLIDE BOTTLE PRESSURE IN RED ''NO GO'' STATUS. R/R L1 DOOR SLIDE PER W/C 2561-4964. ACFT OK FOR SVC. (LP5055352)
- [SDR DALA2018100405889](https://openairdocs.org/sdr/DALA2018100405889.md): Light · inoperative · Oct 4, 2018 · N977DL · Doug MD88 · Emergency Lighting
  > FOUND LT OVERWING EXIT UPPER EMERGENCY LIGHT INOP. RELAMPED OVERWING EXIT EMERGENCY LIGHT IAW AMM 33-50. OPS CK NML. (LP3740096)
- [SDR DALA2018080644858](https://openairdocs.org/sdr/DALA2018080644858.md): Charger · inoperative · Aug 4, 2018 · N977DL · Doug MD88 · Emergency Lighting
  > AFT CABIN EMERGENCY LIGHT ON THE CEILING FROM ROW 32 AND BACK WERE INOPERATIVE. FOUND THE CHARGER NOT CHARGING THE BATTERY PACK. REPLACED THE CHARGER IAW AMM 33-51. LIGHTS TESTED GOOD.
- [SDR DALA2017122708913](https://openairdocs.org/sdr/DALA2017122708913.md): Floor Panel · damaged · Dec 26, 2017 · N977DL · Doug MD88 · Fuselage Floor Panel
  > FLT CREW REPORTS SOFT SPOT IN GALLEY FLOOR BETWEEN G1 AND G3. FLOOR PANEL REF IPC 53-21-00-02J AND REPLACED NICKEL MAT. OK FOR SVC.
- [SDR DALA2017060104397](https://openairdocs.org/sdr/DALA2017060104397.md): Pump · malfunctioned · May 30, 2017 · N977DL · Doug MD88 · Fuel Boost Pump
  > ON TAKEOFF ROLL CENTER FUEL PRESS LO LIGHT ILLUMINATED. CB J21 AND J23 WERE FOUND POPPED ON CLIMBOUT. T/S PER MM REF 28-20-07-101 THRU STEP 4 - WIRING CK AT TERMINAL STRIP S3-10 CKS OK. REF WDM 28-21-00 RANG LT AND RT BOOST PUMPS PHASES A B C TO GRD AND PHASE
- [SDR DALA2017050103519](https://openairdocs.org/sdr/DALA2017050103519.md): Wire · arced · Apr 29, 2017 · N977DL · Doug MD88 · Ice/Rain Protection System Wiring
  > ON DESCENT INTO ATL TURNED ON W/S ANTI-FOG SWITCH. RECEIVED A QUICK FLASH IN COCKPIT, POPPING SOUND, EFIS FLICKERED MOMENTARILY. HAD ELECTRICAL BURNING SMELL FOR ABOUT 10 SECONDS, NO SMOKE, DISSIPATED QUICKLY. EVERYTHING NORMAL AFTER INCIDENT. PERFORMED 2120-2
- [SDR DALA2017040702855](https://openairdocs.org/sdr/DALA2017040702855.md): Connector · broken · Apr 7, 2017 · N977DL · Doug MD88 · Light System Wiring
  > EMERGENCY LIGHT INOPERATIVE AT SEAT 31 AB. REPLACED A BROKEN CONNECTOR IAW SWPM 20. OPS CHECKED GOOD.
- [SDR DALA2017030901904](https://openairdocs.org/sdr/DALA2017030901904.md): Light · malfunctioned · Mar 7, 2017 · N977DL · Doug MD88 · Emergency Lighting
  > AFT EMERGENCY LIGHTS ILLUMINATED WITH POWER REMOVED FROM ACFT. PERFORMED EMERGENCY LIGHT CHECK IAW AMM 33-53. RECYCLED ARM SWITCH WITH POWER OFF, OPS CHECKED GOOD.
- [SDR DALA2017020701007](https://openairdocs.org/sdr/DALA2017020701007.md): Frame · cracked · Feb 6, 2017 · N977DL · Doug MD88 · Fuselage Main, Frame
  > FRAME BS 1451 CRACKED AT LONGERON 1.. REPAIRED IAW ERA 554841-14 REV ORIG.
- [SDR DALA2017020600997](https://openairdocs.org/sdr/DALA2017020600997.md): Bulkhead · damaged · Feb 5, 2017 · N977DL · Doug MD88 · Fuselage Main, Bulkhead
  > RIGHT AFT PRESSURE BULKHEAD LOWER SHEAR ANGLE DAMAGED. REPAIRED IAW ERA 554877-14 REV ORIG.
- [SDR DALA2017020600996](https://openairdocs.org/sdr/DALA2017020600996.md): Bulkhead · damaged · Feb 5, 2017 · N977DL · Doug MD88 · Fuselage Main, Bulkhead
  > LEFT AFT PRESSURE BULKHEAD LOWER SHEAR ANGLE DAMAGED. REPAIRED IAW PRI 554877-14 REV 0 AND COMPLIED WITH ERA 554877-14 REV ORIG.
- [SDR DALA2017020500988](https://openairdocs.org/sdr/DALA2017020500988.md): Frame · cracked · Feb 4, 2017 · N977DL · Doug MD88 · Fuselage Main, Frame
  > FRAME BS 1437 FWD SIDE HAS A 2 INCH LONG CRACK THRU THREE FASTENER HOLES, RBL 7. REPAIRED IAW PRI 554290-14 REVISIONS 1, 2, AND 3 AND COMPLY WITH ERA 554290-14 REVISION ORIGINAL.
- [SDR DALA2017020500987](https://openairdocs.org/sdr/DALA2017020500987.md): Frame · cracked · Feb 4, 2017 · N977DL · Doug MD88 · Fuselage Main, Frame
  > FRAME BS 1437, FWD SIDE HAS A 2 INCH LONG CRACK, LBL 7. REPAIRED IAW PRI 554290-14, REVISIONS 1, 2, AND 3 AND COMPLIED WITH ERA 554290-14 REVISION ORIGINAL.
- [SDR DALA2017020400950](https://openairdocs.org/sdr/DALA2017020400950.md): Shear Tie · cracked · Feb 3, 2017 · N977DL · Doug MD88 · Fuselage Internal Mounting Structure
  > TAIL INTERIOR, CROWN SHEAR TIE HAS 2 CRACKS, BS 1437, RBL 8. REPAIR PER DWG 9953016.
- [SDR DALA2017020300881](https://openairdocs.org/sdr/DALA2017020300881.md): Skin · cracked · Feb 2, 2017 · N977DL · Doug MD88 · Fuselage Main, Plate/Skin
  > TAIL SKIN HAS A CRACK BETWEEN TWO RIVETS AT BS 1437, LONGERON 4 & 5L. REPAIRED IAW PRI 554872-14 REV 0RIGINAL AND COMPLIED WITH ERA 554872-14 REV ORIGINAL.
- [SDR DALA2016122010001](https://openairdocs.org/sdr/DALA2016122010001.md): Wire · broken · Dec 20, 2016 · N977DL · Doug MD88 · Emergency Lighting
  > FOUND EMERGENCY LIGHT INOPERATIVE. REPAIRED BROKEN WIRES AT SEAT 31ED IAW SWPM. OK FOR SERVICE.
- [SDR DALA2016101207190](https://openairdocs.org/sdr/DALA2016101207190.md): Vane · damaged · Oct 11, 2016 · N977DL · Doug MD88 · Trailing Edge Flaps
  > HOLE IN INBD FIXED VANE, OTBD SECTION OF RT WING TE FLAP. REMOVED AND REPLACED THE VANE IAW AMM 27-51-03 P 201.
- [SDR DALA2016101107176](https://openairdocs.org/sdr/DALA2016101107176.md): Tab · damaged · Oct 10, 2016 · N977DL · Doug MD88 · Rudder, Tab Structure
  > RUDDER CONTROL TAB HAS FLAME SPRAY MISSING IN CRITICAL AREAS. REMOVED & REPLACED RUDDER CONTROL TAB IAW WORK CARD 2720-4321. OK FOR SERVICE.
- [SDR DALA2016042003141](https://openairdocs.org/sdr/DALA2016042003141.md): Wire · broken · Apr 19, 2016 · N977DL · Doug MD88 · Light System Wiring
  > MSP MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 17DE, 22DE, AND 33DE. BROKEN WIRES WERE FOUND AND REPAIRED UNDER 17R, 22E AND 33E. ALL LIGHTS CHECKED OK.
- [SDR DALA2016040802712](https://openairdocs.org/sdr/DALA2016040802712.md): Tab · damaged · Apr 7, 2016 · N977DL · Doug MD88 · Elevator, Tab Structure
  > LEFT ELEVATOR ANTI-FLOAT TAB HAS LIGHTNING STRIKE. REPLACED TAB IAW AMDS CARD 2730-4382.
- [SDR DALA2015102606485](https://openairdocs.org/sdr/DALA2015102606485.md): Wire Harness · damaged · Oct 26, 2015 · N977DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT SEAT 12D WAS INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.
- [SDR DALA2015022601663](https://openairdocs.org/sdr/DALA2015022601663.md): None · none · Feb 25, 2015 · N977DL · Doug MD88 · Standard Practices/Structures
  > INADECUATE RIVETS ON STA 435 AND BETWEEN LONGERON 20 TO 24RT. FASTENERS WERE REMOVED. AREA WAS TREATED AND PAINTED AND NEW FASTENERS WERE INSTALLED IAW SRM 51-30-5, 51-10-3, PAR 14 AND 21. REPAIR WAS ACCOMPLISHED IAW ER/A 532510-14, REV ORIGINAL AND ETI-88-
- [SDR DALA2015022601660](https://openairdocs.org/sdr/DALA2015022601660.md): Doubler · corroded · Feb 25, 2015 · N977DL · Doug MD88 · Fuselage Main, Plate/Skin
  > THE AFT LAV CUTOUT DOUBLER WAS CORRODED AND REPAIRED, 532435-14.
- [SDR DALA2015022601667](https://openairdocs.org/sdr/DALA2015022601667.md): Panel · corroded · Feb 24, 2015 · N977DL · Doug MD88 · Fluid Service Doors
  > CORROSION WAS FOUND ON INTERNAL DOUBLER AT FWD LAVATORY SERVICE PANEL BTW STA Y= 282 TO 287 AND LONGS 20LH TO 22LH. REPAIR WAS PERFORMED WITH ER/A 473507-14 REV "A". (LP1836669)
- [SDR DALA2015022301584](https://openairdocs.org/sdr/DALA2015022301584.md): Door Frame · cracked · Feb 22, 2015 · N977DL · Doug MD88 · Fuselage Main, Structure
  > CONTINUED CRACK ON AFTER TO PREVIOUS REPAIR AT DOOR JAMB AT STA Y=46, X=29 AT NOSE WHEEL WELL STRUCTURE. DOOR JAMB WAS REPAIRED IAW ETI-88-15-033, REV 4 AND ER/A 531399-14, REV ORIGINAL.
- [SDR DALA2015022301583](https://openairdocs.org/sdr/DALA2015022301583.md): Angle · corroded · Feb 22, 2015 · N977DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP ANGLE IN STA Y=646, Y=655 AND Y=674 ON X=-60 RT SIDE AT PAX CABIN STRUCTURE. REPAIR WAS PERFORMED WITH ER/A 532529-14, REV ORIG.
- [SDR DALA2015022301582](https://openairdocs.org/sdr/DALA2015022301582.md): Slat Track · cracked · Feb 22, 2015 · N977DL · Doug MD88 · Leading Edge Devices
  > CRACKED LOWER EDGE CUT OUT SLAT TRACK NR 7 LT WING. L/E OUTER WING SKIN WAS REPAIRED IAW ETI-88-15-063, REV 3 AND ER/A 532516-14, REV ORIGINAL.
- [SDR DALA2015022301580](https://openairdocs.org/sdr/DALA2015022301580.md): Access Panel · cracked · Feb 22, 2015 · N977DL · Doug MD88 · Vertical Stabilizer
  > CRACKED SETTLEMENT AREA, BOTH SIDES OF ACCESS PANEL 6301B AT DORSAL FIN L/E. DORSAL ANGLES WERE REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, 51-10-3 PARA 14 & 21, AND DWG 5912188 REV BD.
- [SDR DALA2015022201570](https://openairdocs.org/sdr/DALA2015022201570.md): Door Frame · corroded · Feb 21, 2015 · N977DL · Doug MD88 · Fuselage Main, Structure
  > CORROSION ON LOWER DOOR JAMB, BETWEEN STA Y=638 TO Y=893 ON LONGERON 28 AT CTR CARGO COMPARTMENT. PREVIOUS REPAIR SPACER WAS REPLACED IAW SRM 53-05, FIG 123A.
- [SDR DALA2015022201565](https://openairdocs.org/sdr/DALA2015022201565.md): Access Panel · corroded · Feb 21, 2015 · N977DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON COUNTERSINK AT LT MAIN FUEL TANK ACCESS PLATE NR 1311C. ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0120.
- [SDR DALA2015022201564](https://openairdocs.org/sdr/DALA2015022201564.md): Access Panel · corroded · Feb 21, 2015 · N977DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON COUNTERSINK AT LT MAIN FUEL TANK ACCESS PLATE NR 1335C. ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0120.
- [SDR DALA2015022201563](https://openairdocs.org/sdr/DALA2015022201563.md): Track · corroded · Feb 21, 2015 · N977DL · Doug MD88 · Fuselage Miscellaneous Structure
  > SEVERAL CORROSION POINTS ON RT TIE TRACK FROM STA Y=1212 TO 1320 AFT CARGO COMPARTMENT THE TRACK WAS REPLACED IAW 51-30-1 AND DWG 5936660, REV BZ.
- [SDR DALA2015022201562](https://openairdocs.org/sdr/DALA2015022201562.md): Track · corroded · Feb 21, 2015 · N977DL · Doug MD88 · Fuselage Miscellaneous Structure
  > SEVERAL CORROSION POINTS ON LT TIE TRACK FROM STA Y=1174 TO 1320 AFT CARGO COMPT. TIE TRACK WAS REPLACED IAW SRM 51-30-1 AND DWG 593666, REV BZ.
- [SDR DALA2015022201537](https://openairdocs.org/sdr/DALA2015022201537.md): Frame · corroded · Feb 21, 2015 · N977DL · Doug MD88 · Fuselage Main, Frame
  > SEVERAL CORROSION POINTS ON FRAME AT STA Y=1250 BETWEEN LONGS 27L TO 27R AFT CARGO COMPT CORROSION WAS REMOVED; MEASURED AND FOUND OUT OF LIMITS IAW SRM 51-10-3 PAR 26 AND 53-01, FIG 1, BETWEEN L-28 TO L-28R. UT WAS ACCOMPLISHED ORIGINAL THICKNESS IS 0.063" A
- [SDR DALA2015022101530](https://openairdocs.org/sdr/DALA2015022101530.md): Floor Support · cracked · Feb 20, 2015 · N977DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT AT STA Y=1136 BETWEEN LONGERONS 27L TO 26L AFT CARGO COMPT. FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-2 AND ER/A 413029-14MA, REV "D".
- [SDR DALA2015022101529](https://openairdocs.org/sdr/DALA2015022101529.md): Structure · worn · Feb 20, 2015 · N977DL · Doug MD88 · Trailing Edge Flaps
  > WEAR ON UPPER SURFACE ALSO UPPER/INBD EDGE AT OTBD FLAP/OTBD VANE RT WING. UPPER SURFACE ALSO UPPER/INBD EDGE AT OTBD FLAP/OTBD VANE RT WING WERE REPAIRED IAW ER/A 521199-14MA REV ORIGINAL AND SRM 57-03D.
- [SDR DALA2015022101522](https://openairdocs.org/sdr/DALA2015022101522.md): Floor Panel · unknown · Feb 20, 2015 · N977DL · Doug MD88 · Fuselage Floor Panel
  > INITIAL REPAIR AS REQUIRED PAX CABIN FLOOR PANELS FROM STA Y=120 TO 1338 BETWEEN X=- 44 TO X= 44. FLOOR PANELS NRS 160A, 160E, 160F, 148A, 148B, 148D, 148C, 200C, 160D, 160B, 200E, 826C, 826F, 927B, 927D, 617E, 389F, 769E, 160C, 200D, 826D, 886C, 120E, 617C,
- [SDR DALA2015022101520](https://openairdocs.org/sdr/DALA2015022101520.md): Rib · cracked · Feb 20, 2015 · N977DL · Doug MD88 · Vertical Stabilizer, Spar/Rib
  > CRACKED RIBS AT VERTICAL STABILIZER L/E STA ZFS 23.500 AND STA ZFS 17.656. CRACKED RIBS WERE REPAIRED IAW SRM 55-02, FIG 27.
- [SDR DALA2015022101518](https://openairdocs.org/sdr/DALA2015022101518.md): Rib · cracked · Feb 20, 2015 · N977DL · Doug MD88 · Vertical Stabilizer, Spar/Rib
  > CRACKED RIBS AT VERTICAL STABILIZER L/E. CRACKED RIBS WERE REPAIRED IAW SRM 55-02, FIG 27.
- [SDR DALA2015022101517](https://openairdocs.org/sdr/DALA2015022101517.md): Web · cracked · Feb 20, 2015 · N977DL · Doug MD88 · Fuselage Main, Structure
  > CRACKED LOWER DOOR JAMB WEB AT STA Y=1217 APPROXIMATELY BETWEEN PROJECTION LONGERONS 28R AND 27R AFT CARGO COMPT WEB WAS REMOVED. NEW WEB WAS DRILLED, TREAT AND PAINTED AND WAS INSTALLED IAW DWG 5936442, REV "A" SRM 51-10-3, PAR 21 AND 14; 51-10-4, 51-30-1, 5

Next page: https://openairdocs.org/deregistered/N977DL-2019-09-06/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 = 'N977DL' AND deregistration_id = 'N977DL-2019-09-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N977DL-2019-09-06/reports

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