# Service difficulty reports: N984DL, cancelled Nov 9, 2020

A list on [N984DL, cancelled Nov 9, 2020](https://openairdocs.org/deregistered/N984DL-2020-11-09.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 · 250 reports

- [SDR DALA2019062803910](https://openairdocs.org/sdr/DALA2019062803910.md): Connector · disconnected · Jun 28, 2019 · N984DL · Doug MD88 · Light System Wiring
  > EMEG LIGHTS INOP BETWEEN ROW 13 & 23. RECONNECTED CONNECTOR AT FLOOR AT SEAT 13 ED OPS CK GOOD. (LP5917986)
- [SDR DALA2019031501702](https://openairdocs.org/sdr/DALA2019031501702.md): Bracket · broken · Mar 14, 2019 · N984DL · Doug MD88 · Hydraulic Pump, Auxiliary
  > WHILE WORKING JOB CARD 0591-0301 FOUND AUX HYD PUMP WIRE HARNESS BRACKET BROKE. REF EA 09-457000-03AD FIG 2 ITEM 7. INSTALLED BRACKET TO WIRE HARNESS PER EA 09-457000-03AD FIG 2. A/C OK FOR SVC. BRACKET 9D0062-3S10-12. SDR REPORTED DUE TO BEING AD RELATED. (LP
- [SDR DALA2018032401860](https://openairdocs.org/sdr/DALA2018032401860.md): Fire Warning · false activation · Mar 23, 2018 · N984DL · Doug MD88 · Fire Detection
  > RIGHT ENGINE LOOP B LIGHT ILLUMINATED DURING FLIGHT PER QRH LOOP A SELECTED. NORMAL FIRE TEST LOOP DETECTOR LEFT IN A POSITION FOR REMAINDER OF THE FLIGHT. SELECTED RT ENG FIRE LOOP TO BOTH AND RAN TEST OPS NORMAL NO FAULT NO HISTORY OK FOR SVC.
- [SDR DALA2017082306345](https://openairdocs.org/sdr/DALA2017082306345.md): Battery Pack · not reported · Aug 22, 2017 · N984DL · Doug MD88 · Emergency Lighting
  > OVERWING EMERGENCY EVACUATION LIGHT BATTERY PACK OPS CHECK. REPLACED OVERWING EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK IAW AMM 33-53-00 PERFORMED SATISFACTORY OPS CHECK.
- [SDR DALA2017082106306](https://openairdocs.org/sdr/DALA2017082106306.md): Bearing · nicked · Aug 18, 2017 · N984DL · Doug MD88 · Elevator Structure
  > LEFT ELEVATOR NR 1 HINGE BEARING NICKED. REMOVED THE HINGE BEARING HOUSING IAW OVERHAUL MANUAL 27-30-1. REMOVED AND REPLACED THE BEARING AND REINSTALLED HINGE HOUSING IAW CMM 27-30-1 AND SOPM 20-10-7.
- [SDR DALA2017081806298](https://openairdocs.org/sdr/DALA2017081806298.md): Seal · damaged · Aug 17, 2017 · N984DL · Doug MD88 · Horizontal Stabilizer Structure
  > ON INSTALLATION OF LEFT ELEVATOR TO HORIZONTAL STAB, DAMAGE WAS FOUND ON THE AFT SPAR REAR CAP, XE225. REPAIRED LT HORIZONTAL STAB T/E SPAR SEAL IAW ER/A 398032-14MA.
- [SDR DALA2017081706296](https://openairdocs.org/sdr/DALA2017081706296.md): Cusp Web · cracked · Aug 16, 2017 · N984DL · Doug MD88 · Fuselage Miscellaneous Structure
  > ON REMOVAL OF THE RT SIDE FLOOR WEB, A CRACK WAS NOTICED AT FWD CORNER CUT OUT. REPAIRED THE CUSP WEB AT BS 807 IAW SRM 53-05, PAR 144, FIG 131A-21, DWG 9910151, REV BU, REV CH, AND DWG 9930538 REV CE.
- [SDR DALA2017062604970](https://openairdocs.org/sdr/DALA2017062604970.md): Wire · damaged · Jun 25, 2017 · N984DL · Doug MD88 · Electrical Power System Wiring
  > ACFT DIVERTED, DURING CLIMB OUT, PASSING THROUGH 26K, A STRONG ACRID ODOR BECAME APPARENT IN THE COCKPIT. FLIGHT ATTENDANTS REPORTED SAME ODOR IN CABIN. BEGAN DESCENT DIVERSION. AFTER APPROXIMATELY 1-1.5 MINUTES BOTH OIL TEMP HIGH LIGHTS ILLUMINATED. THROTT
- [SDR DALA2017060704535](https://openairdocs.org/sdr/DALA2017060704535.md): Structure · punctured · Jun 7, 2017 · N984DL · Doug MD88 · Leading Edge Devices
  > DURING A SERVICE CHECK, FOUND A DENT WITH A PUNCTURE ON BACKSIDE OF RT NR 1 SLAT, 45 INCHES FROM INBOARD, 2.25 X 1.87 L X.195 DEEP. REMOVED AND REPLACED THE SLAT IAW AMDS CARD 2700-4224-RH-01.
- [SDR DALA2017012300562](https://openairdocs.org/sdr/DALA2017012300562.md): Skin · cracked · Jan 22, 2017 · N984DL · Doug MD88 · Horizontal Stabilizer, Plate/Skin
  > HORIZONTAL STABILIZER UPPER RT AFT SKIN PANEL CRACKED. DRILLED END CRACK 0.250 DRILLED IAW SR09550028. ENLARGE STOP DRILL IAW SR09550028 STEP 42. HFEC INSP AREA IAW NDTM 06-1001.001 NO DEFECTS NOTED. ALODINED & PRIMED. SEALED AREA REINSTALLED FILLER AND APPLI
- [SDR DALA2017012300572](https://openairdocs.org/sdr/DALA2017012300572.md): Cam · no test · Jan 21, 2017 · N984DL · Doug MD88 · Aerodynamic Fairings
  > TAILCONE RELEASE MECHANISM CAM FAILS TORQUE CHECK IAW STEP 12 OF AMDS 5350-01077-0101. ADJUSTED IAW AMM 53-53-02-201, OPS CHECKED GOOD, OK FOR SERVICE IAW AMDS 5350-01077-0101.
- [SDR DALA2017010400078](https://openairdocs.org/sdr/DALA2017010400078.md): Apu · contaminated · Jan 2, 2017 · N984DL · Doug MD88 · APU Core Engine
  > DURING THE BOARDING PROCESS, THE CREW NOTIFIED MAINTENANCE OF A BURNING SMELL IN THE CABIN. THE APU WAS RUNNING AND THE PACKS WERE BEING OPERATED TO WARM THE CABIN. MAINTENANCE FOUND THE APU INLET CONTAMINATED WITH DE-ICE FLUID. THE APU INLET AND DOOR ASSEMBLY
- [SDR DALA2016120109436](https://openairdocs.org/sdr/DALA2016120109436.md): Fastener · damaged · Dec 1, 2016 · N984DL · Doug MD88 · Fuselage Miscellaneous Structure
  > 1R DOOR GIRT BAR HOLDER DETACHED FROM DOOR. ACARS INBD WRITE UP. REPLACED FASTENERS ON GIRT BAR HOLDER. CKS GOOD.
- [SDR DALA2015081604983](https://openairdocs.org/sdr/DALA2015081604983.md): Cusp Web · corroded · Aug 15, 2015 · N984DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEB BS 715-718 BETWEEN X -54 TO -60 AT CABIN PAX IN REF CARD 149, ZONE 201. REPAIR WAS ACCOMPLISHED IAW SRM 53-05, FIG 131A -13.
- [SDR DALA2015072804733](https://openairdocs.org/sdr/DALA2015072804733.md): Vane · damaged · Jul 27, 2015 · N984DL · Doug MD88 · Trailing Edge Flaps
  > AFTER LANDING, WHEN FLAPS WERE RAISED TO 0 THE RT FLAP INDICATOR READS 5 AND LT FLAP INDICATOR READS 0, FELT SLIGHT BINDING WHEN ATTEMPTING TO RETRACT SLATS SO LT FLAPS OUT. INBD AND OTBD FLAP VANE GUIDE OF INBD FLAP WERE REPLACED FOR A SERVICIABLE FLAP VAN
- [SDR DALA2015072504706](https://openairdocs.org/sdr/DALA2015072504706.md): Heater Blanket · corroded · Jul 24, 2015 · N984DL · Doug MD88 · Airfoil Anti/De-ice System
  > CORROSION ON RT WING HEATER BLANKET AROUND FUEL ACCESS PANEL CUTOUT. THE HEATER BLANKET WAS REPLACED IAW AMM 30-80-02-401. TESTED THE HEATER BLANKET, FOUND OK IAW AMM 30-80-02-501.
- [SDR DALA2015072404640](https://openairdocs.org/sdr/DALA2015072404640.md): Bushing · corroded · Jul 23, 2015 · N984DL · Doug MD88 · Wing Main, Frame Structure
  > CORROSION ON REPAIR BUSHINGS AND ELONGATED BUSHINGS ON RT HEATER BLANKET T/E. DAMAGE BUSHINGS WERE REPLACED IAW ER/A 537709-14AD, REV "A" AND EA: 09-070683-03, AD REV L. MAJOR REPAIR.
- [SDR DALA2015072404637](https://openairdocs.org/sdr/DALA2015072404637.md): Skin · corroded · Jul 23, 2015 · N984DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION FOUND BETWEEN FUSELAGE SKIN AND INBD DOUBLER AT AFT WASTE LAVATORY SERVICE PANEL. CORROSION WAS REMOVED IAW ETI-88-15-224, REV 1 AND ER/A 536427-14, REV ORIGINAL.
- [SDR DALA2015072404630](https://openairdocs.org/sdr/DALA2015072404630.md): Skin · cracked · Jul 23, 2015 · N984DL · Doug MD88 · Fuselage Main, Plate/Skin
  > A 0.187 INCH CRACK ON FUSELAGE SKIN, BS 1418 BETWEEN LONGERONS 2 - 3L AND A CRACK OF 0.531" BETWEEN LONGERON 1 AND 2R. FUSELAGE SKIN WAS REPAIRED IAW ER/A 536455-14AD, REV ORIGINAL AND ETI 88-15-204, REV 2.
- [SDR DALA2015072304585](https://openairdocs.org/sdr/DALA2015072304585.md): Angle · cracked · Jul 22, 2015 · N984DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED SPLICE ANGLE ON CANTED FRAME STA Y=1463 AND RBL 18. REPAIRED IAW ERA 536514-14, REV.
- [SDR DALA2015072304581](https://openairdocs.org/sdr/DALA2015072304581.md): Trunnion · corroded · Jul 22, 2015 · N984DL · Doug MD88 · Wing, Landing Gear Attach Fittings
  > CORROSION AND BLEND OUTS IN LT RETRACT ACTUATOR SUPPORT FITTING BUSHING BORE. CORROSION ON BUSHING BORE WAS REWORKED WITH FINAL DIMENTION: ID 2.2735" WITHIN LIMITS IAW DWG SR09570087, REV B FPI WAS ACCOMPLISHED LT RETRACT ACTUATOR SUPPORT FITTING BUSHING BORE
- [SDR DALA2015072304580](https://openairdocs.org/sdr/DALA2015072304580.md): Trunnion · corroded · Jul 22, 2015 · N984DL · Doug MD88 · Wing, Landing Gear Attach Fittings
  > CORROSION IN RT RETRACT ACTUATOR SUPPORT FITTING BUSHING BORE. CORROSION ON BUSHING BORE WAS REWORKED WITH FINAL DIMENTION ID 2.377" WITHIN LIMITS IAW DWG SR09570087, REV B, FPI WAS ACCOMPLISHED RT RETRACT ACTUATOR SUPPORT FITTING BUSHING BORE NO CRACKS WERE
- [SDR DALA2015072204555](https://openairdocs.org/sdr/DALA2015072204555.md): Frame · cracked · Jul 21, 2015 · N984DL · Doug MD88 · Fuselage Main, Frame
  > CRACKED FRAME BS 1497. FRAME WAS REPAIRED IAW ER/A 536485-14, REV ORIGINAL AND ETI-88-15-234, REV 2.
- [SDR DALA2015072204547](https://openairdocs.org/sdr/DALA2015072204547.md): Pan · cracked · Jul 21, 2015 · N984DL · Doug MD88 · Passenger/Crew Doors
  > CRACKED PAN ON PAX DOOR BETWEEN BEAM 8 AND FWD EDGE. THE DOOR WAS REPAIRED IAW SRM 52-05D, FIGURE 18A.
- [SDR DALA2015072104509](https://openairdocs.org/sdr/DALA2015072104509.md): Cargo Track · corroded · Jul 20, 2015 · N984DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON THE LT CARGO TRACK BS 1193 - 1250. THE CARGO TRACK WAS REPLACED.
- [SDR DALA2015072104503](https://openairdocs.org/sdr/DALA2015072104503.md): Intercostal · cracked · Jul 20, 2015 · N984DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BETWEEN BS 1271 - 1288. THE INTERCOSTAL WAS REMOVED IAW SRM 51-30-2, FABRICATED IAW DWG 9936580, REV BT, AND INSTALLED IAW SRM 51-30-2.
- [SDR DALA2015072004495](https://openairdocs.org/sdr/DALA2015072004495.md): Beam · corroded · Jul 19, 2015 · N984DL · Doug MD88 · Fuselage Main, Structure
  > CORROSION FOUND ON THE BEAM BETWEEN BS 685 - 690 OF THE MID CARGO LOWER DOOR FRAME. THE BEAM WAS REPAIRED IAW SRM 53-05, FIG 123. MAJOR REPAIR.
- [SDR DALA2015072004490](https://openairdocs.org/sdr/DALA2015072004490.md): Longeron Splice · corroded · Jul 19, 2015 · N984DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CORROSION ON THE LONGERON SPLICE, BS 1287 - 1309, LONGERON 30. THE LONGERON SPLICE WAS REPLACED IAW SRM 51-10-4, 51-10-3 PAR 14 AND 21, 51-30-2 AND 51-30-5.
- [SDR DALA2015071904487](https://openairdocs.org/sdr/DALA2015071904487.md): Access Panel · corroded · Jul 18, 2015 · N984DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON THE COUNTERSINK AND SETTLEMENT AREA OF THE FUEL ACCESS PANEL 1335C. THE CORROSION WAS REMOVED AND FOUND OUT OF LIMITS. THE ACCESS PANLE WAS REPLACED IAW SRM 51-22-2A.
- [SDR DALA2015071904482](https://openairdocs.org/sdr/DALA2015071904482.md): Finger Doubler · corroded · Jul 18, 2015 · N984DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON FUSELAGE SKIN FINGER DOUBLER BELOW LONGERON 26L, BS 579 - 598. THE FINGER DOUBLER WAS REPLACED IAW SRM 51-30-2, SRM 51-30-5, SRM 51-10-4, AND SRM 51-10-3 PAR 14, 21 & 33.
- [SDR DALA2015071904475](https://openairdocs.org/sdr/DALA2015071904475.md): Intercostal · cracked · Jul 18, 2015 · N984DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BELOW HYD MANUAL PUMP AT LT MLG WHEEL WELL. THE INTERCOSTAL WAS REMOVED, REPAIRED, AND INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-3 PAR.21 AND 14, 51-10-2 AND 53-01.
- [SDR DALA2015071904474](https://openairdocs.org/sdr/DALA2015071904474.md): Angle · cracked · Jul 18, 2015 · N984DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE BEHIND LT SIDE WALL SUPPORT AT BS 1007, Z -6. THE ANGLE WAS REPAIRED IAW SRM 53-01, 51-30-2, 53-01, FIG 2, 51-10-3 PAR 14 AND 21.
- [SDR DALA2015071904473](https://openairdocs.org/sdr/DALA2015071904473.md): Intercostal · corroded · Jul 18, 2015 · N984DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL FROM BS 1380 - 1390 LONGERON 26L. THE INTERCOSTAL WAS REPLACED IAW SRM 53-14-4, FIG 1, NDT SPM 04-00-07, FIG 3, PAR 5, SH 1 AND 2.
- [SDR DALA2015071904472](https://openairdocs.org/sdr/DALA2015071904472.md): Angle · cracked · Jul 18, 2015 · N984DL · Doug MD88 · Vertical Stabilizer
  > CRACKED ANGLE BETWEEN VSS 2 - 26 TO -15 AT VERTICAL STABILIZER INNER STRUCTURE. THE ANGLE WAS REPLACED IAW SRM 51-30-05, 51-30-2, 51-10-3 PAR 21 AND 14 SRM 51-10-2 AND DWG 5912188, REV BD.
- [SDR DALA2015071804467](https://openairdocs.org/sdr/DALA2015071804467.md): Beam · corroded · Jul 17, 2015 · N984DL · Doug MD88 · Fuselage Main, Structure
  > CORROSION ON THE UPPER DOOR FRAME BEAM BETWEEN BS 1174 - 1193 IN THE AFT CARGO BAY. THE BEAM WAS REPLACED IAW SRM 51-30-5, 51-10-4 AND 51-10-3 PARA 21, 14 AND 36.
- [SDR DALA2015071804466](https://openairdocs.org/sdr/DALA2015071804466.md): Door Frame · corroded · Jul 17, 2015 · N984DL · Doug MD88 · Fuselage Main, Structure
  > CORROSION ON LOWER DOOR FRAME IN THE FWD CARGO BAY. REPAIRED IAW SRM 53-05, FIG 44A.
- [SDR DALA2015071804465](https://openairdocs.org/sdr/DALA2015071804465.md): Doubler · cracked · Jul 17, 2015 · N984DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CRACKED INNER PRODUCTION DOUBLER, BS 693 BETWEEN LONGERONS 23-24R. THE DOUBLER WAS REWORKED IAW SRM 53-05, FIG 109. TREATED AND PAINTED IAW SRM 51-10-3, PAR 14, 21.
- [SDR DALA2015071704444](https://openairdocs.org/sdr/DALA2015071704444.md): Door Frame · cracked · Jul 16, 2015 · N984DL · Doug MD88 · Fuselage Main, Structure
  > CRACK ON UPPER DOOR FRAME FOR THE RT AFT OVERWING EMERGENCY DOOR. THE DOOR FRAME WAS REPAIRED IAW SRM 53-05, FIG 32 AND 51-01, PAR 4, 21.
- [SDR DALA2015071704436](https://openairdocs.org/sdr/DALA2015071704436.md): Tab · dented · Jul 16, 2015 · N984DL · Doug MD88 · Elevator, Tab Structure
  > RT ELEVATOR GEARED TAB, DENTED ON UPPER SURFACE. THE TAB WAS REPAIRED IAW SRM 55-04.
- [SDR DALA2015071704431](https://openairdocs.org/sdr/DALA2015071704431.md): Longeron · corroded · Jul 16, 2015 · N984DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON LONGERON 24L BETWEEN BS 1338 - 1380. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.
- [SDR DALA2015071704430](https://openairdocs.org/sdr/DALA2015071704430.md): Frame · cracked · Jul 16, 2015 · N984DL · Doug MD88 · Fuselage Main, Frame
  > WEAR AND A CRACK WAS FOUND ON FRAME BS 1343 LONGERONS 26L - 26R. THE FRAME WAS REPAIRED IAW ERA 094719-14MA, REV A.
- [SDR DALA2015071504376](https://openairdocs.org/sdr/DALA2015071504376.md): Floor Panel · delaminated · Jul 14, 2015 · N984DL · Doug MD88 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL IN CABIN PAX. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.
- [SDR DALA2015071504375](https://openairdocs.org/sdr/DALA2015071504375.md): Rib · cracked · Jul 14, 2015 · N984DL · Doug MD88 · Vertical Stabilizer, Spar/Rib
  > CRACKED RIB XFS 30.00 IN VERTICAL STABILIZER L/E INNER STRUCTURE. RIB REMOVED IAW SRM 51-30-2 AND 51-30-5 AND A NEW RIB WAS DRILLED IAW SRM 51-10-4, AND REPAIRED IAW SRM 55-02, FIG 27. NEW RIB INSTALLED IAW SRM 51-30-2 AND 51-30-5.
- [SDR DALA2015071404356](https://openairdocs.org/sdr/DALA2015071404356.md): Frame · corroded · Jul 14, 2015 · N984DL · Doug MD88 · Fuselage Main, Frame
  > CORROSION ON FRAME AND FRAME CLIP AT BS 1287 BETWEEN LONGERONS 28LT AND 28RT IN AFT CARGO COMPARTMENT. SUMMARY CORROSION WAS REMOVED IAW SRM 51-10-3 THEN NDT SPM 04-00-01 WITH AN ORIGINAL THICK OF 0.063" ON FRAME 1287 AND REM. THICK 0.004 AND IT IS OUT OF LIM
- [SDR DALA2015071404355](https://openairdocs.org/sdr/DALA2015071404355.md): Rib · cracked · Jul 14, 2015 · N984DL · Doug MD88 · Vertical Stabilizer, Spar/Rib
  > CRACKED LT RIB BS ZFS 36.50 AT VERTICAL STABILIZER L/E INNER STRUCTURE. RIB WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, 51-10-3, PAR 14, 21.
- [SDR DALA2015071404354](https://openairdocs.org/sdr/DALA2015071404354.md): Rib · cracked · Jul 14, 2015 · N984DL · Doug MD88 · Vertical Stabilizer, Spar/Rib
  > CRACKED RIB STA ZFS 49.62 AT VERTICAL STABILIZER. L/E INNER STRUCTURE, RIBS WERE REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-3 PAR 14, 21 51-10-4.
- [SDR DALA2015071304335](https://openairdocs.org/sdr/DALA2015071304335.md): Cusp Web · damaged · Jul 13, 2015 · N984DL · Doug MD88 · Fuselage Miscellaneous Structure
  > WAVINESS IN LEFT CUSP WEB BETWEEN X 44 - 54, BS 1174 - 1250. CUSP WEB WAS REPAIRED IAW SRM 51-30-1, SRM 51-30-2, SRM 53-05, FIG 131A-6, SRM 51-10-3, PAR 14 & 21 AND SRM 51-30-5.
- [SDR DALA2015071304334](https://openairdocs.org/sdr/DALA2015071304334.md): Seat Track · worn · Jul 13, 2015 · N984DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > WEAR ON THE LEFT SEAT TRACK X 44 BETWEEN BS 1188 - 1196. THE SEAT TRACK WAS REPLACED IAW SRM 51-30-1, SRM 53-05, FIG 4B-1, NDT SPM 04-00-07, PAR 5, FIG 3 SH-1AND 2, SRM 53-05, FIG 4F, SRM 51-10-4, SRM 51-10-3, PAR 14 AND 21, AND SRM 51-30-5.
- [SDR DALA2015071404353](https://openairdocs.org/sdr/DALA2015071404353.md): Door Frame · corroded · Jul 13, 2015 · N984DL · Doug MD88 · Fuselage Main, Structure
  > CORROSION ON REPAIR OF LWR DOOR JAMB AT AFT CARGO COMPARTMENT. DOUBLER WAS REPLACE IAW SRM 53-05, FIG 123. PRIMARY STRUCTURE.
- [SDR DALA2015071304331](https://openairdocs.org/sdr/DALA2015071304331.md): Intercostal · cracked · Jul 12, 2015 · N984DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL AT BS 886 - 905 LONGERON 17L. THE INTERCOSTAL WAS REPAIRED IAW SRM 53-01, FIG 2.

Next page: https://openairdocs.org/deregistered/N984DL-2020-11-09/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 = 'N984DL' AND deregistration_id = 'N984DL-2020-11-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N984DL-2020-11-09/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.