# Service difficulty reports: N946DL, cancelled Sep 16, 2019

A list on [N946DL, cancelled Sep 16, 2019](https://openairdocs.org/deregistered/N946DL-2019-09-16.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 · 201 reports

- [SDR DALA2018112006701](https://openairdocs.org/sdr/DALA2018112006701.md): Smoke Detector · malfunctioned · Nov 19, 2018 · N946DL · Doug MD88 · Smoke Detection
  > LAVATORY SMOKE DETECTOR WILL NOT TURN OFF LOCATIONS 203. REPLACED DETECTOR, OK FOR SVC REF AMM 26-17. (LP0833638)
- [SDR DALA2018052503602](https://openairdocs.org/sdr/DALA2018052503602.md): Battery · discharged · May 25, 2018 · N946DL · Doug MD88 · Emergency Lighting
  > ON SERVICE CHECK- EMERGENCY LIGHTS AT L1, R1, AND COCKPIT OVERHEAD DID NOT REMAIN ON. REPLACED EMERGENCY LIGHT BATTERIES IN FWD DROP DOWN PNL. OPS CHECKS GOOD AMM 33-53.
- [SDR DALA2018052203497](https://openairdocs.org/sdr/DALA2018052203497.md): Skin · corroded · May 21, 2018 · N946DL · Doug MD88 · Fuselage Main, Plate/Skin
  > AFT LAVATORY SERVICE PANEL LOWER FWD CORNER, IS SUSPECTED OF BEING CORRODED. REPAIRED IAW ERA 568545-14 REV. A.
- [SDR DALA2018052203494](https://openairdocs.org/sdr/DALA2018052203494.md): Skin · corroded · May 21, 2018 · N946DL · Doug MD88 · Fuselage Main, Plate/Skin
  > THE FUSELAGE LAVATORY SERVICE CUTOUT SKIN, BS 1322, LONGERON 22L FOUND CORRODED. COMPLIED WITH STEPS 1 THROUGH 23 OF PRI 568545-14, REV. 5. STEPS 1 THROUGH 23 OF ERA 568545-14 REV A. MATCH THOSE OF PRI 568545-14, REV. 5. ERA 568545-14 REV. A COMPLIED WITH.
- [SDR DALA2018012700456](https://openairdocs.org/sdr/DALA2018012700456.md): Wire Harness · defective · Jan 27, 2018 · N946DL · Doug MD88 · Light System Wiring
  > SEAT 30DE EMERGENCY LIGHT INOP. REPLACED SEAT MOUNTED LIGHT HARNESS, REF AMM 33-53 CHECKS GOOD.
- [SDR DALA2017061804798](https://openairdocs.org/sdr/DALA2017061804798.md): Battery · discharged · Jun 18, 2017 · N946DL · Doug MD88 · Emergency Lighting
  > ON SVC CK FOUND OVERHEAD EMERGENCY LIGHTS INOP ROW 17-21. REPLACED EMER LIGHT BATTERIES AT ROW 17 OPS CHECK GOOD.
- [SDR DALA2017012000552](https://openairdocs.org/sdr/DALA2017012000552.md): Lamp · inoperative · Jan 20, 2017 · N946DL · Doug MD88 · Emergency Lighting
  > LEFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-50, OK FOR SERVICE.
- [SDR DALA2016092006740](https://openairdocs.org/sdr/DALA2016092006740.md): Battery · discharged · Sep 20, 2016 · N946DL · Doug MD88 · Emergency Lighting
  > CEILING EMERGENCY LIGHTS OUT AT ROWS 23, 24, AND 25. REPLACED BATTERIES IN POWER SUPPLY AT ROW 25, SN-22718. OPS CHECK OK. REF AMM 33-53-00-401.
- [SDR DALA2016051904020](https://openairdocs.org/sdr/DALA2016051904020.md): Battery Pack · inoperative · May 18, 2016 · N946DL · Doug MD88 · Emergency Lighting
  > CEILING EMERGENCY LIGHTS OUT AT SEATS 22C, 24C, 24D, AND 25C. REPLACED BOTH BATTERIES IN POWER PACK. REF AMM 33-53-00. OPS CHECK OK. PN ON 2 AD-4002P BATTERIES.
- [SDR DALA2016051603960](https://openairdocs.org/sdr/DALA2016051603960.md): Battery Pack · inoperative · May 14, 2016 · N946DL · Doug MD88 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHTS ROW 16-19 INOPERATIVE. R & R BATTERIES IAW AMM 33-53-00. OPS CHECKED GOOD.
- [SDR DALA2016031101868](https://openairdocs.org/sdr/DALA2016031101868.md): Skin · cracked · Mar 10, 2016 · N946DL · Doug MD88 · Vertical Stabilizer, Plate/Skin
  > VERTICAL STABILIZER HAS A CRACK ON TOP L/E. REMOVED DAMAGED SKIN BETWEEN STOP DRILLS. TRIMMED OUT DAMAGED AREA. HFEC IAW SPM 6-10-01.001. FABRICATED AND INSTALLED INTERNAL DOUBLER AND FILLER IAW PRI 544417-14, REV O. IDENTIFIED REPAIR IAW 900-5-1, NR 4. R
- [SDR DALA2015091405620](https://openairdocs.org/sdr/DALA2015091405620.md): Wire · broken · Sep 12, 2015 · N946DL · Doug MD88 · Emergency Lighting
  > MAINTENANCE FOUND CATWALK MARKER FOR EMERGENCY LIGHTS INOPERATIVE. BROKEN WIRES WERE FOUND AT QUICK DISCONNECT AND RETERMINATED.
- [SDR DALA2015090605457](https://openairdocs.org/sdr/DALA2015090605457.md): Frame · cracked · Sep 1, 2015 · N946DL · Doug MD88 · Fuselage Main, Frame
  > DURING SERVICE CHECK, FOUND T-SHAPED CRACK ON FORWARD EDGE OF GEAR OPENING RT SIDE. REPLACED FRAME FWD RT SIDE MAIN WHEEL WELL IAW DWG 5930584, OPS CHECKED, DOOR CHECKED GOOD.
- [SDR DALA2015032702454](https://openairdocs.org/sdr/DALA2015032702454.md): Lanyard · frayed · Mar 27, 2015 · N946DL · Doug MD88 · Escape Slide
  > MAINTENANCE FOUND L-1 DOOR SLIDE LANYARD FRAYED AND IN POOR CONDITION. THE L1 DOOR SLIDE WAS REPLACED.
- [SDR DALA2014093005357](https://openairdocs.org/sdr/DALA2014093005357.md): Latch · failed · Sep 29, 2014 · N946DL · Doug MD88 · Aerodynamic Fairings
  > DURING THE TAILCONE RELEASE SYSTEM OPS CHECK, MAINTENANCE FOUND THAT THERE WAS EXCESSIVE TENSION IN THE RELEASE CABLE SYSTEM. THE TAILCONE UPPER RT LATCH PIN HUNG ON THE DROP. MAINTENANCE REPLACED THE LATCH AND CLEANED AND LUBED THE CABLE CONDUITS AND TAILCO
- [SDR DALA2014093005336](https://openairdocs.org/sdr/DALA2014093005336.md): Skin · cracked · Sep 29, 2014 · N946DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CRACK IN SKIN TWO INCHES FWD OF BS 1338, LONGERON 3L. ACCOMPLISHED REPAIR IAW ERA 529397-14AD, REV ORIGINAL SEC I.
- [SDR DALA2014093005335](https://openairdocs.org/sdr/DALA2014093005335.md): Skin · cracked · Sep 29, 2014 · N946DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CRACK DISCOVERED AT BS 1338, LONGERON 3L ON SKIN ONE INCH FWD. 0.125 INCH IN LENGTH. ACCOMPLISHED REPAIR IAW ERA 529397-14AD, REV ORIGINAL SEC I.
- [SDR DALA2014093005337](https://openairdocs.org/sdr/DALA2014093005337.md): Stringer Fitting · cracked · Sep 28, 2014 · N946DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 3L END FITTING CRACKED AT BS 1338, VERIFIED WITH EDDY CURRENT. REPAIRED IAW PRI 529458-14, REV 0, BY REPLACEMENT OF END FITTING.
- [SDR DALA2014082604738](https://openairdocs.org/sdr/DALA2014082604738.md): Frame · cracked · Aug 14, 2014 · N946DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE DISCOVERED THAT THE TAILCONE RELEASE MECHANISM ALIGNMENT PIN FRAME WAS CRACKED OUT OF ALLOWABLE LIMITS. THE CANTED FRAME WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS.
- [SDR DALA2014081404509](https://openairdocs.org/sdr/DALA2014081404509.md): Angle · cracked · Aug 14, 2014 · N946DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE DISCOVERED THAT THE TAILCONE LOCK PAD ANGLES WERE CRACKED BEYOND ALLOWABLE LIMITS. THE TAILCONE ASSEMBLY WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII WAS SATISFACTORY.
- [SDR DALA2014081504622](https://openairdocs.org/sdr/DALA2014081504622.md): Bayonet · loose · Aug 12, 2014 · N946DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE DISCOVERED THAT FOUR OF THE BAYONETS FOR THE TAILCONE RELEASE SYSTEM WERE LOOSE BEYOND ALLOWABLE LIMITS. THE BAYONETS ATTACHMENT HARDWARE WAS REMOVED, REINSTALLED, AND PROPERLY SECURED.
- [SDR DALA14019430946](https://openairdocs.org/sdr/DALA14019430946.md): Battery Pack · inoperative · Mar 27, 2014 · N946DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT ALL OF THE OVERHEAD EMERGENCY LIGHT IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN 2 OF THE POWER SUPPLIES AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA13054830946](https://openairdocs.org/sdr/DALA13054830946.md): Power Supply · inoperative · Oct 21, 2013 · N946DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 22, 24, & 25 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA13017310946](https://openairdocs.org/sdr/DALA13017310946.md): Skin · corroded · Apr 16, 2013 · N946DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON FUSELAGE SKIN, BS 647 BETWEEN L29-30L. REPAIRED IAW ER/A 512876-14 REV ORIG
- [SDR DALA13017300946](https://openairdocs.org/sdr/DALA13017300946.md): Tee Fitting · damaged · Apr 16, 2013 · N946DL · Doug MD88 · Fuselage Main, Attach Fittings
  > DAMAGED TEE FITTING BS 1338 L29-30R AT AFT PRESSURE BULKHEAD. TEE FITTING REPLACED IAW SR09530001, REV J AND SRM 53-03, FIG 37 AND ER/A 512881-14, REV ORIG.
- [SDR DALA13017290946](https://openairdocs.org/sdr/DALA13017290946.md): Skin · damaged · Apr 16, 2013 · N946DL · Doug MD88 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKES ON LT WINDOW BELT FWD LOWER CORNER AND ALSO MID LOWER SECTION BETWEEN BS 1003-1022. REPAIRED IAW ER/A 512849. REV ORIGINAL.
- [SDR DALA13017260946](https://openairdocs.org/sdr/DALA13017260946.md): Skin · damaged · Apr 15, 2013 · N946DL · Doug MD88 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON LT WINDOW BELT FWD LOWER CORNER BETWEEN BS 731-750. REPAIR ON LT WINDOW BELT FWD LOWER CORNER BETWEEN BS 731-750 WAS ACOMPLISHED WHITH 1 EXTERNAL REPAIR DOUBLER IAW ER/A 512848-14 REV ORIGINAL;
- [SDR DALA13017000946](https://openairdocs.org/sdr/DALA13017000946.md): Skin · damaged · Apr 15, 2013 · N946DL · Doug MD88 · Fuselage Main, Plate/Skin
  > LIGHTING STRIKE ON RT WINDOW BELT AFT LOWER CORNER BETWEEN BS 579 - 598. REPAIRED IAW ER/A 512847-14, REV ORIGINAL.
- [SDR DALA13016580946](https://openairdocs.org/sdr/DALA13016580946.md): Frame · corroded · Apr 14, 2013 · N946DL · Doug MD88 · Fuselage Main, Frame
  > CORROSION ON FRAME BS 1332 BETWEEN LONGERONS 22-24R AT AFT CARGO COMPARTMENT (C3). CORROSION WAS REMOVED AND NEW FRAME WAS INSTALLED DWG 9958238 REV CF AND SRM 51-30-2 AND SRM 51-30-5.
- [SDR DALA13016500946](https://openairdocs.org/sdr/DALA13016500946.md): Doubler · cracked · Apr 12, 2013 · N946DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CRACK ON INTERNAL DOUBLER AT BS 424.625 BETWEEN LONGERON 26-27R ON LOWER AFTER DOOR JAMB CORNER AT FWD CARGO COMPARTMENT. AREA DAMAGE WAS REMOVED AND PARTS OF REPAIR WERE TREATED AND PAINTED IAW ER/A 512878-14, REV ORIGINAL REPAIR WAS PERFORMED IAW ER/A 5128
- [SDR DALA13016530946](https://openairdocs.org/sdr/DALA13016530946.md): Cusp Web · corroded · Apr 11, 2013 · N946DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON LT CUSP WEB UPPER AND LOWER SURFACE BS 655-666 BTW X=54 TO X=60 AT PAX CABIN. AREA DAMAGE WAS REPAIRED IAW SRM 53-05 FIG 131A-14 DUE TO AREA OUT LIMITS.
- [SDR DALA13016520946](https://openairdocs.org/sdr/DALA13016520946.md): Skin · cracked · Apr 11, 2013 · N946DL · Doug MD88 · Wing, Plate/Skin
  > CRACK OF 0.0109" APPROX ON INTERNAL SURFACE OPEN HOLE CLOSE TO STRINGER 15, XCW=202.716 AT LT LOWER ACCESS DOOR CUT OUT. REPAIR WAS ACCOMPLISHED WITH ER/A NR 512852-14 AD REV ORIG WITH PLUG REPAIR.
- [SDR DALA13016400946](https://openairdocs.org/sdr/DALA13016400946.md): Cusp Web · corroded · Apr 11, 2013 · N946DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON MEMBRANE CUSP WEB X=50-60 BS 595. REMOVED CORROSION, REMOVED AREA OF OUT LIMITS, FABRICATE DOUBLER AND RING DOUBLERS, AND PERFORM REPAIR. CORROSION LEVEL 2.
- [SDR DALA13016390946](https://openairdocs.org/sdr/DALA13016390946.md): Seat Track · corroded · Apr 11, 2013 · N946DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LT SEAT TRACK X=54 FROM BS 857-859 AT PAX CABIN. SEAT TRACK REPAIRED IAW SRM 53-05, FIG 4A.
- [SDR DALA13016380946](https://openairdocs.org/sdr/DALA13016380946.md): Seat Track · corroded · Apr 10, 2013 · N946DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LT SEAT TRACK X=54 FROM BS 1214-1295 AT PAX CABIN.
- [SDR DALA13016370946](https://openairdocs.org/sdr/DALA13016370946.md): Seat Track · corroded · Apr 10, 2013 · N946DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LT SEAT TRACK X=54 BETWEEN BS 1174 - 1212 AT PAX CABIN. REMOVED SEAT TRACK AND CORROSION, MEASURE DRILLED NEW SEAT TRACK IAW SRM 51-10-3 PAR 26, 21, 14, 38, 53-05, FIG 4B1 AND 51-30-2, 51-30-1.
- [SDR DALA13016150946](https://openairdocs.org/sdr/DALA13016150946.md): Cargo Track · corroded · Apr 10, 2013 · N946DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON (LT) TIE TRACK BTW STA Y=1117-1222 AT AFT CARGO COMPARTMENT (C3) REF. NEW TIE TRACK BTW STA Y 1117-1222 WAS REPLACED IAW SRM 53-24-00 AND 51-30-1 AND 51-30-2.
- [SDR DALA13016040946](https://openairdocs.org/sdr/DALA13016040946.md): Skin · corroded · Apr 10, 2013 · N946DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON INNER FUSELAGE SKIN PREVIOUS REPAIR DOUBLER BETWEEN STA Y=610 TO Y=628 LONG, 28RY AND 29 LT REF (T0 277241). REPAIR FILLER WAS REMOVED IAW SRM MD-88 51-30-5. FABRICATED AND INSTALLED, AND PROTECTED AGAINST CORROSION IAW SRM 51-10-3 PAR 14-21 AND
- [SDR DALA13016030946](https://openairdocs.org/sdr/DALA13016030946.md): Cusp Web · corroded · Apr 10, 2013 · N946DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION OUT OF LIMITS ON CUSP WEB UPPER/ LOWER SURFACE BETWEEN 895-900 AND 1072-1087 X=-54 TO X=-60. IN REF NRC 153 ZONE 58 AND CUSP WEB WERE REPAIRED IAW SRM 53-05, FIG 231A. CORROSION LEVEL 2.
- [SDR DALA13016420946](https://openairdocs.org/sdr/DALA13016420946.md): Intercostal · corroded · Apr 9, 2013 · N946DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL FROM BS 1322 TO 1338 BETWEEN LONGERON 21 - 22L AT AFT CARGO COMPARTMENT. INTERCOSTAL REPLACED IAW DWG 5911423, REV CC AND THESE WERE DRILLED, TREATED, AND INSTALLED IAW SRM 51-30-2, 51-10-3.
- [SDR DALA13016140946](https://openairdocs.org/sdr/DALA13016140946.md): Cusp Web · corroded · Apr 9, 2013 · N946DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON LT FLOOR CUSP WEB UPPER AND LOWER SURFACE X=54 TO X=60 AT STA Y=693-712 PAX CABIN (CFS) REF. (T0 276219). REMOVE AREA DAMAGED, FABRICATED REPAIR PARTS, AND REPAIR WEB IAW SRM 53-05 FIG 31A-8. CORROSION LEVEL 2. (LP #0818374)
- [SDR DALA13016110946](https://openairdocs.org/sdr/DALA13016110946.md): Support · cracked · Apr 9, 2013 · N946DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED LT SLANT PANEL SUPPORT IN STA Y=1117 BETWEEN LONGS 26L AND 27L AT AFT CARGO COMPARTMENT. (C3) REF (T0 276564). SUPPORT WAS REMOVED, FABRICATED AND REPLACED IAW ER/A 413029-14 MA REV C, ASSOCIATED ER/A 41-302914 ADDED FOR AC 0946.
- [SDR DALA13016100946](https://openairdocs.org/sdr/DALA13016100946.md): Cargo Track · corroded · Apr 9, 2013 · N946DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RT TIE TRACK FROM STA Y=1212 TO 1287 OF AFT CARGO COMPARTMENT. (C3) (MRB 53-139-05) (REF 336,ZONE 57) (T0 276486). TIE TRACK WAS REMOVED, CORROSION WAS REMOVED, MEASURED (OUT OF LIMITS) NEW TIE TRACK WAS DRILLER, TREATED AND PAINTED AND INSTALLED
- [SDR DALA13016090946](https://openairdocs.org/sdr/DALA13016090946.md): Cargo Track · corroded · Apr 9, 2013 · N946DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON THE TRACK LT SIDE FROM STA Y=1212 TO Y=1287. ALSO CRACK ON SAME LT TIE TRACK STA Y=1260 OF AFT CARGO COMPARTMENT. (C3) (MRB 53-139-05) (REF 335,ZONE 57) (T0 276485). TIE TRACK WAS REMOVED NEW TIE TRACK WAS INSTALLED IAW SRM 51-30-1.
- [SDR DALA13016060946](https://openairdocs.org/sdr/DALA13016060946.md): Frame · corroded · Apr 9, 2013 · N946DL · Doug MD88 · Fuselage Main, Frame
  > CORROSION ON FRAME 1380 STA X=13 AND X=-13. REF. (T0 276519). FRAME TEE WAS REPLACE IAW DWG 9912246, REV DE (FRAME TEE WAS REMOVED AND NEW FRAME TEE WAS INSTALLED) IAW SRM 51-30-2, 51-30-5. CORROSION LEVEL 2.
- [SDR DALA13015800946](https://openairdocs.org/sdr/DALA13015800946.md): Skin · corroded · Apr 9, 2013 · N946DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON PREVIOUS REPAIR FILLER BS 617-623 BETWEEN L29 AND 30R CARGO COMPARTMENT INNER SKIN. DAMAGED FILLER REPLACED IAW ER/A 457687-14, REV "B".
- [SDR DALA13016080946](https://openairdocs.org/sdr/DALA13016080946.md): Cusp Web · corroded · Apr 8, 2013 · N946DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON RT FLOOR CUSP WEB UPPER AND LOWER SURFACE X=-54 TO X=-60 AT STA Y=1098-1117, 1117-1120, 1136-1147, 1147-1155, 1155-1174 PAX CABIN. (CFS) (MRB 53-037-01)(REF 154, ZONE 58) (T0 276209). REMOVE CORROSION, MEASURE, REMOVE SEAT TRACK, CUSP WEB FITTINGS
- [SDR DALA13016070946](https://openairdocs.org/sdr/DALA13016070946.md): Cusp Web · corroded · Apr 8, 2013 · N946DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON LT CUSP WEB BETWEEN STA Y=1161-1174 AND X=44 TO X=60 AT PAX CABIN IN REF NRC (T0 276378) AND CARD 251. REF NRC NR 618, ZONE 58 (T0 277205). AREA OUT LIMITS WAS REPAIRED IAW SRM 53-05, FIG 131A-21 DUE TO AREA OUT LIMITS REF NRC 251.
- [SDR DALA13015780946](https://openairdocs.org/sdr/DALA13015780946.md): Strap · corroded · Apr 8, 2013 · N946DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAPS ABOVE LONGERON 23L BETWEEN BS 1239-1309, AFT CARGO COMPARTMENT. STRAPS WERE REMOVED AND INSTALLED IAW SRM 51-30-2.
- [SDR DALA13015770946](https://openairdocs.org/sdr/DALA13015770946.md): Cusp Web · corroded · Apr 8, 2013 · N946DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION OUT OF LIMITS ON RT CUSP WEB FROM BS 660-663. DAMAGED REMOVED AND DOUBLER AND FILLER FABRICATED AND AREA WAS REPAIRED IAW SRM 51-70-4, FIG 1.

Next page: https://openairdocs.org/deregistered/N946DL-2019-09-16/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 = 'N946DL' AND deregistration_id = 'N946DL-2019-09-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N946DL-2019-09-16/reports

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