# Service difficulty reports: N973DL, cancelled Dec 30, 2024

A list on [N973DL, cancelled Dec 30, 2024](https://openairdocs.org/deregistered/N973DL-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 3 · 144 reports

- [SDR DALA2020020500890](https://openairdocs.org/sdr/DALA2020020500890.md): Battery Pack · inoperative · Feb 5, 2020 · N973DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTS ROWS 10,11, AND 12 INOP. CHANGED BATTERIES IN PACK. CKS GOOD PER MD88 AMM 33-53. (LP6483407)
- [SDR DALA2020012700599](https://openairdocs.org/sdr/DALA2020012700599.md): Battery Pack · inoperative · Jan 27, 2020 · N973DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTS AT EXIT ROW 24 UPPER INOP. R/R BATTERIES AT PACK B5-125. OPS NML. REF MD88 AMM 33-53. (LP7223878)
- [SDR DALA2020012500594](https://openairdocs.org/sdr/DALA2020012500594.md): Frame · cracked · Jan 24, 2020 · N973DL · Doug MD88 · Fuselage Main, Frame
  > CRACK DETECTED ON UPPER CANTED FRAME AT 2 0'CLOCK. REMOVED UPPER CANTED FRAME AND DRILLED REPLACEMENT CANTED FRAME. (398826). INSTALLED REPLACEMENT FRAME IAW BOEING DRAWING 9911843. (LP1460279)
- [SDR DALA2020012500593](https://openairdocs.org/sdr/DALA2020012500593.md): Frame · cracked · Jan 24, 2020 · N973DL · Doug MD88 · Fuselage Main, Frame
  > CRACK DETECTED ON LOWER CANTED FRAME AT 7O'CLOCK. REMOVED LEFT CANTED FRAME. DRILLED UP REPLACEMENT CANTED FRAME. BEGAN INSTALLING LEFT CANTED FRAME. COMPLETED LEFT CANTED. (LP1460270)
- [SDR DALA2020012500592](https://openairdocs.org/sdr/DALA2020012500592.md): Intercostal · cracked · Jan 24, 2020 · N973DL · Doug MD88 · Fuselage Miscellaneous Structure
  > INTERCOSTAL PN-9911875-3 FOUND CRACKED WHILE REPLACING CANTED FRAME. REMOVED INTERCOSTAL.(359111). REPLACED INTERCOSTAL IAW BOEING DRAWING 9911875. (LP1460281)
- [SDR DALA2020011300210](https://openairdocs.org/sdr/DALA2020011300210.md): Smoke Detector · inoperative · Jan 12, 2020 · N973DL · Doug MD88 · Smoke Detection
  > AFT RT LAV SMOKE DET INOP. REMOVED AND REPLACED AFT RT LAV SMOKE DET. (LP7223839)
- [SDR DALA2019112906961](https://openairdocs.org/sdr/DALA2019112906961.md): Bulb · burned out · Nov 27, 2019 · N973DL · Doug MD88 · Passenger Compartment Lighting
  > AFTER FLIGHT F/A REPORTED LEFT AFT LAV SMOKE DETECTOR WENT OFF IN FLIGHT. ONE PAX REPORTED SMELLING SOMETHING. IN FLIGHT F/A REPORTED WHAT PAX SAID I ASKED FOR DETAILS, SHE SAID SHE SMELLED NOTHING; AND NO REPORT OF ALARM. ONLY AFTER WE DEPLANED DID SHE TELL M
- [SDR DALA2019112306863](https://openairdocs.org/sdr/DALA2019112306863.md): Smoke Detector · false activation · Nov 23, 2019 · N973DL · Doug MD88 · Smoke Detection
  > AFT LEFT LAV SMOKE DETECTOR WENT OFF FOR SEVERAL SECONDS ENROUTE. NO SMOKE OR FIRE PRESENT. R/R AFT LEFT LAV SMOKE DECTECTOR PER MD 88 AMM 26-13. OPS CHECK GOOD.
- [SDR DALA2019042902689](https://openairdocs.org/sdr/DALA2019042902689.md): Smoke Detector · missing · Apr 28, 2019 · N973DL · Doug MD88 · Smoke Detection
  > FWD LAV SMOKE DETECTOR IS MISSING. RPLCD FWD LAV SMOKE DETECTOR PER MD88 AMM 26-13. ALL CHKS GOOD. (LP5675132)
- [SDR DALA2019022701257](https://openairdocs.org/sdr/DALA2019022701257.md): Cam · out of position · Feb 26, 2019 · N973DL · Doug MD88 · Aerodynamic Fairings
  > TAIL CONE CAM ARM FOR SLIDE LANYARD IS NOT POSITIONED CORRECTLY. ADJUSTED CAM PER MD88 AMM 53-53-02. (LP0960759)
- [SDR DALA2019022601211](https://openairdocs.org/sdr/DALA2019022601211.md): Tab · damaged · Feb 26, 2019 · N973DL · Doug MD88 · Rudder, Tab Structure
  > RUDDER TAB HAS PAINT CHIPPING INTO COMPOSITE. REPLACED WITH SERVICEABLE RUDDER TAB IAW DELTA WORK CARDS 2720-4438 AND 2720-4321 TAB, RUDDER OFF 88-5554-9-0002 00094 ON 88-5554-9-0002 00542. (LP0959946)
- [SDR DALA2019022601209](https://openairdocs.org/sdr/DALA2019022601209.md): Rudder · damaged · Feb 25, 2019 · N973DL · Doug MD88 · Rudder, Plate/Skin
  > DURING PAINT VISIT -RUDDER MISSING DAMAGED FLAME SPRAY. REMOVED AND REPLACED RUDDER PER MD88 AMM 27-20-01. REMOVE & INSTALL MISTAKENLY ACCOMPLISHED ON LOG 5318866. (LP5318867)
- [SDR DALA201902110871](https://openairdocs.org/sdr/DALA201902110871.md): Skin · cracked · Feb 9, 2019 · N973DL · Doug MD88 · Vertical Stabilizer, Plate/Skin
  > INITIAL INSPECTION: CRACK ON VERTICAL STABILIZER LEADINGEDGE SKIN RH SIDE STA ZFS 17.65. VERTICAL STABILIZER LEADINGEDGE SKIN RH SIDE STA ZFS 17.65 WAS REPAIRED PER ER/A 575282-14 REV. ORIG. AND ETI-88-19-008 REV.1. PERFORM GENERAL VISUAL INSPECTION EVERY "C"
- [SDR DALA201902110870](https://openairdocs.org/sdr/DALA201902110870.md): Access Panel · corroded · Feb 9, 2019 · N973DL · Doug MD88 · Fuselage Main, Plate/Skin
  > INITIAL INSPECTION: CORROSION ON AFT LAVATORY ACCESS PANEL BTW STA Y 1309 -1322 AND BTW LOG 20LH -21LH FUS. CORROSION LEVEL 2. AFT LAVATORY ACCESS PANEL,SKIN AND INTERNAL DOUBLER WERE REPAIRED PER ER/A 473500-14 REV. A SECTION II AND ETI-88-19-009 REV.3. PERFO
- [SDR DALA2019021109866](https://openairdocs.org/sdr/DALA2019021109866.md): Longeron · corroded · Feb 8, 2019 · N973DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > INITIAL INSPECTION: CORROSION AT LONGERON 29RH BTW STA Y=1270 TO Y=1290.(C3). SECTION OF LONGERON 29RH BTW STA Y=1270 TO Y=1290. WAS REPAIRED AND REPLACED PER DC9/MD80, SRM 53-02 FIG. 18. CORROSION LEVEL 2. PERMANENT REPAIR. (LP0936794)
- [SDR DALA2019020800848](https://openairdocs.org/sdr/DALA2019020800848.md): Jackscrew · corroded · Feb 7, 2019 · N973DL · Doug MD88 · Stabilizer Control System
  > INITIAL INSPECTION: AD. RII. AA WORKCARD. CORROSION ON HORIZONTAL STABILIZER ACTUATOR JACKSCREW UPPER SIDE. HORIZONTAL STABILIZER JACKSCREW ASSEMBLY P/N 5910962-71 S/N: DCA2042 WAS REPLACED FOR SERVICEABLE P/N 5910962-57 S/N: DCA1689 UNDER AMDS 2742-4540. JACK
- [SDR DALA2019020600808](https://openairdocs.org/sdr/DALA2019020600808.md): Door Frame · cracked · Feb 5, 2019 · N973DL · Doug MD88 · Fuselage Main, Structure
  > INITIAL INSPECTION: CRACK ON FWD OUTBD DOORJAMB STA 946 AT RH MLG WHEEL WELL. FWD OUTBD DOORJAMB STA 946 AT RH MLG WHEEL WELL WAS REPAIRED PER DC9/MD80 SRM 53-05 FIG 113. (LP0933140)
- [SDR DALA2018090205396](https://openairdocs.org/sdr/DALA2018090205396.md): Light · inoperative · Sep 2, 2018 · N973DL · Doug MD88 · Emergency Lighting
  > RED EMERGENCY FLOOR LIGHT INOP FWD OF F/C COAT CLOSET. RELAMPED PER AMM 33-53. OPS CHECK GOOD.
- [SDR DALA2018062604202](https://openairdocs.org/sdr/DALA2018062604202.md): Unknown · fumes · Jun 9, 2018 · N973DL · Doug MD88 · Air Distribution System
  > AFTER LANDING AND STARTING THE APU, SMELLED FUMES COMING FROM THE COCKPIT EYE BALL VENTS. WE IMMEDIATELY SHUT THE AIR OFF. APU AND INLET DRY NO SIGNS OF FUEL CONTAMINATION. OPENED APU DOORS VERIFIED NOT CONTAMINATED. CKD FUEL DRAINS, NO FUEL. PRESSURIZED FUE
- [SDR DALA2018011900300](https://openairdocs.org/sdr/DALA2018011900300.md): Tab · missing · Jan 19, 2018 · N973DL · Doug MD88 · Elevator, Tab Structure
  > WHILE INSPECTING FLIGHT CONTROLS, FOUND LEFT ELEVATOR INBD TAB OTBD EDGE REPAIR MISSING. REMOVED AND REPLACED LEFT ELEVATOR CONTROL TAB IAW JIC 2730-4634-LH.
- [SDR DALA2017060604490](https://openairdocs.org/sdr/DALA2017060604490.md): Roller · missing · May 24, 2017 · N973DL · Doug MD88 · Landing Gear Door Retract Section
  > DURING GEAR EXTENSION, THE GEAR DOOR LIGHT REMAINED ILLUMINATED. IAW QRH 14.3, THE ALTERNATE GEAR EXTEND PROCEDURE WAS PERFORMED FOR LANDING. MAINTENANCE FOUND THE LEFT GEAR DOOR UP LATCH ROLLER AND ATTACHING HARDWARE MISSING. THE ROLLER AND HARDWARE WAS REPL
- [SDR DALA2017042403318](https://openairdocs.org/sdr/DALA2017042403318.md): Unknown · odor · Apr 23, 2017 · N973DL · Doug MD88 · Air Distribution System
  > AT FL250, TURNED ON THE WING ANTI-ICE DUE TO RIME ICE BUILD UP, IMMEDIATELY SMELLED A STRONG CHEMICAL ODOR. THE FLIGHT ATTENDANTS DETECTED THE ODOR. LASTED CONTINUOUSLY FOR THE 10 MINUTES OR SO THE WING ANTI-ICE WAS ACTIVE. ONCE TURNED OFF, THE ODOR
- [SDR DALA2017020200908](https://openairdocs.org/sdr/DALA2017020200908.md): Seat · detached · Feb 1, 2017 · N973DL · Doug MD88 · Passenger Compartment Equipment
  > ROW 13ABC SEATS CAME DETACHED AT THE FLOOR ON THE FRONT. ENTIRE ROW TIPPED BACK ON TAKEOFF. ADJUSTED AND SECURED SEAT ROW IAW AMM 25-23. ALL OPS NORMAL.
- [SDR DALA2017011900483](https://openairdocs.org/sdr/DALA2017011900483.md): Strap · cracked · Jan 18, 2017 · N973DL · Doug MD88 · Escape Slide
  > EVACUATION SLIDE OF TAILCONE THE CONTAINER FORWARD HOLD-DOWN STRAPS WERE FOUND CRACKED DUE TO CORROSION. HOLD DOWN STRAPS WERE REPLACED IAW AMM 25-62-01.
- [SDR DALA2017011600376](https://openairdocs.org/sdr/DALA2017011600376.md): Frame · cracked · Jan 14, 2017 · N973DL · Doug MD88 · Fuselage Main, Frame
  > CRACKED FRAME BS 1485 BETWEEN LONGERONS 15 AND 16L. THE FRAME WAS REPAIRED IAW ERA 552911-14 REV. ORIGINAL AND ETI-88-17-004 REV.2.
- [SDR DALA2017011200260](https://openairdocs.org/sdr/DALA2017011200260.md): Frame · damaged · Jan 11, 2017 · N973DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > ELONGATED HOLES AT FRAME BS 1361 LONGERON 9 AND 10L. REPAIRED IAW SRM 53-03 FIG. 4 AND 51-30-5.
- [SDR DALA2017011100256](https://openairdocs.org/sdr/DALA2017011100256.md): Cusp Web · corroded · Jan 10, 2017 · N973DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP WEB BS 845 AND BTW LBL 54 AND 58. THE CUSP WEB WAS REPARIED IAW SRM 53-05 FIG 131A-13.
- [SDR DALA2015101706233](https://openairdocs.org/sdr/DALA2015101706233.md): Attach Fitting · corroded · Oct 16, 2015 · N973DL · Doug MD88 · Horizontal Stabilizer, Attach Fittings
  > LEFT OTBD HORIZONTAL STABILIZER ATTATCH FITTING HAS WEAR ON OTBD FACE AND PITTING IN BORE. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 032-0001, 5510-01074-16/001, 00008. REPLACED PLATES REF ER/A 540306-14, REV ORIG
- [SDR DALA2015101506173](https://openairdocs.org/sdr/DALA2015101506173.md): Attach Fitting · corroded · Oct 14, 2015 · N973DL · Doug MD88 · Horizontal Stabilizer, Attach Fittings
  > BOTH INBD ATTACH FITTINGS FOR HORIZONTAL STABILIZER HAVE PITTED BORES. REPACED PLATES REF ERA 540306-14, REV O.
- [SDR DALA2015101506172](https://openairdocs.org/sdr/DALA2015101506172.md): Attach Fitting · worn · Oct 14, 2015 · N973DL · Doug MD88 · Horizontal Stabilizer, Attach Fittings
  > RIGHT OTBD HORIZONTAL STABILIZER ATTATCH FITTING HAS WEAR ON OTBD FACE AND PITTING IN BORE. REPLACED PLATES, REF ERA 540306-14, REV O.
- [SDR DALA2015101306092](https://openairdocs.org/sdr/DALA2015101306092.md): Spar Cap · cracked · Oct 12, 2015 · N973DL · Doug MD88 · Horizontal Stabilizer, Spar/Rib
  > RT HORIZONTAL STABILIZER AFT UPPER SPAR CAP CRACKED AT AFT BARREL NUT HOLE (MKD). REF NOTES AMDS 5510-01098-01B, ITEM 7. FOR DETAILS SEE JOB 00 - WORK PACKAGE. REPLACE HORIZONTAL STAB ASSY ON TASK CARDS: 5510-4135, 2730-4182, 2730-4831, 2730-4590-LT, 2730-4
- [SDR DALA2015061103669](https://openairdocs.org/sdr/DALA2015061103669.md): Compressor · stalled · Jun 1, 2015 · N973DL · Doug MD88 · Turbine Engine Compressor Section
  > FLIGHT RETURNED TO DEPARTURE FOLLOWING A COMPRESSOR STALL AND RESULTING HIGH EGT IN THE NR 2 ENGINE. THE CREW SHUTDOWN THE NR 2 ENGINE AND LANDED UNEVENTFULLY ON 1 ENGINE. MAINTENANCE HAS REPLACED THE ENGINE.
- [SDR DALA2014121606545](https://openairdocs.org/sdr/DALA2014121606545.md): Skin · dented · Dec 11, 2014 · N973DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DENT ON EXTERNAL FUSELAGE SKIN REPAIR DOUBLER BS 402-403 BETWEEN LONGERONS 25 -26L. AREA REPAIRED IAW ER/A 365087-14, REV C.
- [SDR DALA2014121006515](https://openairdocs.org/sdr/DALA2014121006515.md): Slide · unserviceable · Dec 8, 2014 · N973DL · Doug MD88 · Escape Slide
  > MAINTENANCE DISCOVERED THAT THE TAILCONE EVACUATION SLIDE WAS INADEQUATELY WRAPPED. MAINTENANCE INSTALLED A SERVICABLE TAILCONE EVACUATION SLIDE. RII WAS SATISFACTORY.
- [SDR DALA2014121006497](https://openairdocs.org/sdr/DALA2014121006497.md): Release Mech · damaged · Dec 7, 2014 · N973DL · Doug MD88 · Aerodynamic Fairings
  > DURING CHECK, MAINTENANCE FOUND THE TAILCONE RELEASE MECHANISM TO BE DAMAGED. MAINTENANCE REPLACED THE RELEASE MECHANISM FITTING AND CRANK ASSY.
- [SDR DALA2014120906451](https://openairdocs.org/sdr/DALA2014120906451.md): Skin · dented · Dec 7, 2014 · N973DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DENT ON EXTERNAL FUSELAGE SKIN REPAIR DOUBLER BS 402-403 BETWEEN LONGERONS 25 -26L. REPAIRED IAW ER/A 365087-14, REV C.
- [SDR DALA2014120706449](https://openairdocs.org/sdr/DALA2014120706449.md): Floorbeam · corroded · Dec 6, 2014 · N973DL · Doug MD88 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM BS 1322, X 18, X 26L. DAMAGE REPAIRED IAW SRM 53-05, FIG 79A, SH 1.
- [SDR DALA2014120806450](https://openairdocs.org/sdr/DALA2014120806450.md): Structure · cracked · Dec 5, 2014 · N973DL · Doug MD88 · Fuselage Main, Structure
  > CORROSION AND CRACK AROUND OF SETTLEMENT AREA OF LT APU DOOR. CORROSION WAS REMOVED IAW SRM 51-10-3, PAR 26. FASTENERS WERE REMOVED IAW SRM 51-30-2, NEW REPAIR DOUBLERS WERE FABRICATED IAW SRM 52-05D, FIG 9 NEW REPAIR DOUBLERS WERE TREATED AND PAINTED IAW
- [SDR DALA2014120606448](https://openairdocs.org/sdr/DALA2014120606448.md): Frame · cracked · Dec 5, 2014 · N973DL · Doug MD88 · Fuselage Main, Frame
  > CANTED FRAME BS 1485 CRACKED AT LT AFT SIDE OTBD OF LIGHT ASSY. DAMAGE WAS REMOVED IAW SRM 53-030, FIG 48. REPAIR FABRICATED IAW SRM 53-030, FIG 8 AND INSTALLED IAW SRM 53-030, FIG 48.
- [SDR DALA2016111008680](https://openairdocs.org/sdr/DALA2016111008680.md): Frame · corroded · Dec 4, 2014 · N973DL · Doug MD88 · Fuselage Main, Frame
  > CORROSION ON FRAME BS 1287, BETWEEN LONGERONS 29 TO 30L. THE FRAME WAS REPAIRED IAW SRM 53-03 D FIG 2A,
- [SDR DALA2014120506419](https://openairdocs.org/sdr/DALA2014120506419.md): Skin · damaged · Dec 4, 2014 · N973DL · Doug MD88 · Wing, Plate/Skin
  > CRACKED REPAIR DOUBLER AND ELONGATED HOLES ON INTERNAL STRUCTURE AT LT WING INBD BUTE DOOR AFT EDGE. REPAIR WAS REMOVED, AND A NEW DOUBLER WAS FABRICATED, TREATED, PAINTED, AND INSTALLED IAW SRM 51-30-2 AND 51-30-5, 57-01, FIG 3 AND 51-10-3, PAR 14 AND 21.
- [SDR DALA2016111008677](https://openairdocs.org/sdr/DALA2016111008677.md): Floorbeam · corroded · Dec 2, 2014 · N973DL · Doug MD88 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED BS 1307, X 22. REPAIRED THE FLOORBEAM.
- [SDR DALA2014120306414](https://openairdocs.org/sdr/DALA2014120306414.md): Skin · damaged · Dec 2, 2014 · N973DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DAMAGE ON FUSELAGE SKIN BELOW RUB STRIPS AREA FROM BS 1117 - 1079 BETWEEN LONGERONS 25-30.. CORROSION WAS REMOVED IAW SRM 51-10-3, PAR 26. AREAS WITHIN LIMITS WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14-21.
- [SDR DALA2014120306413](https://openairdocs.org/sdr/DALA2014120306413.md): Pan · cracked · Dec 2, 2014 · N973DL · Doug MD88 · Passenger/Crew Doors
  > CRACK BEYOND PREVIOUS STOP DRILL ON FWD UPPER CORNER AT DOOR PAN OF FWD PASSENGER DOOR. DOOR PAN WAS REPLACED IAW SRM 52-05D, 51-30-1, 51-30-2, 51-30-4.
- [SDR DALA2014120306411](https://openairdocs.org/sdr/DALA2014120306411.md): Intercostal · corroded · Dec 2, 2014 · N973DL · Doug MD88 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CORRODED BETWEEN BS 1271-1287 BL 0. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-10-3, PAR 21,14, 26, 38; 51-30-2, 51-30-5, ER/A 511165-14, REV B, AMM 20-30-01-201, DWG 9936580.
- [SDR DALA2014121206517](https://openairdocs.org/sdr/DALA2014121206517.md): Frame · cracked · Dec 1, 2014 · N973DL · Doug MD88 · Fuselage Main, Frame
  > CANT FRAME BS 1485 CRACKED AT LT AFT SIDE OF OTBD LIGHT ASSY. DAMAGE WAS REMOVED IAW SRM 53-03, FIG 48. REPAIR FABRICATED IAW SRM 53-03, PAR 48. REPAIR DRILLED AND TRIMED IAW SRM 53-03, FIG 48. REPAIR TREATED AND PAINTED IAW SRM 51-10-3, PAR 21 AND 14. RE
- [SDR DALA2014120106337](https://openairdocs.org/sdr/DALA2014120106337.md): Frame · corroded · Nov 30, 2014 · N973DL · Doug MD88 · Fuselage Main, Frame
  > CORROSION ON FRAME, BS 1287 BETWEEN LONGERONS 29 - 30L. FRAME REPAIRED IAW SRM 53-03 D, FIG 2A.
- [SDR DALA2014120106336](https://openairdocs.org/sdr/DALA2014120106336.md): Cargo Track · corroded · Nov 30, 2014 · N973DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RT CARGO TRACK BS 1212-1322. THE CARGO TRACK WAS REMOVED, AND CORROSION WAS REMOVED. A NEW CARGO TRACK WAS DRILLED, TREATED, PAINTED, AND INSTALLED IAW SRM 51-30-1, 51-10-3, PAR 26,14,21 AND 38, SRM 53-05, FIG 4C, SRM 51-10-4, 51-30-1 AND NDT
- [SDR DALA2014120106335](https://openairdocs.org/sdr/DALA2014120106335.md): Frame · corroded · Nov 30, 2014 · N973DL · Doug MD88 · Fuselage Main, Frame
  > CORROSION ON FRAME BS 1380 BETWEEN LONGERONS 26 - 30R. FRAME REPLACED IAW SRM 51-30-2 AND 51-30-5 AND DWG 9912246-REV DE.
- [SDR DALA2014120106334](https://openairdocs.org/sdr/DALA2014120106334.md): Intercostal · corroded · Nov 30, 2014 · N973DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL BETWEEN BS 1145-1155 AND L28-29R. THE INTERCOSTAL WAS R&R IAW SRM 51-30-2, 51-30- 5, 51-10-3 PAR 14, 21, 26, 38 ER/A 511165-14 MA, REV B, 51-10-4.

Next page: https://openairdocs.org/deregistered/N973DL-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 = 'N973DL' AND deregistration_id = 'N973DL-2024-12-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N973DL-2024-12-30/reports

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