# Service difficulty reports: N986DL, cancelled Apr 25, 2022

A list on [N986DL, cancelled Apr 25, 2022](https://openairdocs.org/deregistered/N986DL-2022-04-25.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 · 233 reports

- [SDR DALA2019102706182](https://openairdocs.org/sdr/DALA2019102706182.md): Charger · inoperative · Oct 27, 2019 · N986DL · Doug MD88 · Emergency Lighting
  > OVERWING EXIT LIGHTS ABOVE FWD OVERWING DOORS LT AND RT SIDE INOP. REPLACED BATTERIES IN BATTERY CHARGER FOR EMERGENCY LIGHTS. CKS GOOD. (LP6641857)
- [SDR DALA2019082104888](https://openairdocs.org/sdr/DALA2019082104888.md): Line · loose · Aug 20, 2019 · N986DL · Doug MD88 · Extinguishing System
  > NR 2 ENGINE FIRE SUPPRESSION LINE LOOSE IN PYLON. TIGHTENED JAM NUT FOR NO. 2 ENG FIRE SUPPRESSION LINE.
- [SDR DALA2019022801286](https://openairdocs.org/sdr/DALA2019022801286.md): Vane · damaged · Feb 28, 2019 · N986DL · Doug MD88 · Trailing Edge Flaps
  > RT OB FLAP CENTER FLAP VANE DAMAGED. REMOVED RT OB FLAP CENTER VANE PER AMM 27-51. INSTALLED NEW O/B FLAP CENTER VANE IAW AMM 27-51. (LP5311566)
- [SDR DALA2018111976674](https://openairdocs.org/sdr/DALA2018111976674.md): Structure · damaged · Nov 16, 2018 · N986DL · Doug MD88 · Service Doors
  > FOUND BOTTOM OF R1 DOOR DAMAGED AND SEAL TORN. RMVD R1 DOOR AND COMP. STEPS B 1-2 OF INST. PER MD88 M/M 52-41. COMP. INST OF R1 DOOR PER MD 88 M/M 52-41 CKS GOOD. RMVD AND RE-INST R1 DOOR SLIDE PER AMDS 2561-4964. RII C/W. (LP4755951)
- [SDR DALA2018100305851](https://openairdocs.org/sdr/DALA2018100305851.md): Wire · loose · Sep 28, 2018 · N986DL · Doug MD88 · Electrical Power System Wiring
  > AT GATE SRQ APU GEN FELL OFF LINE, RESETS NO HELP, NO VOLTS OR FREQ. FOUND GEN FEED WIRE 3X4D2N LOOSE AND BURNED ALSO GEN. TERMINAL BURNED OFF. RMVD APU & GEN. INST. APU GEN. PER M/M 24-20. RE-INST APU PER M/M 49-10 APU LK CKS & OPS CKS. (LP0761874)
- [SDR DALA2018082205196](https://openairdocs.org/sdr/DALA2018082205196.md): Cam Lock · missing · Aug 21, 2018 · N986DL · Doug MD88 · Auxiliary Power Unit (APU) Doors
  > LEFT APU DOOR MISSING ONE CAMLOCK. INSTALLED THE CAMLOCK IAW CMM 52-44-2. OK FOR SERVICE. REPORTED DUE TO POSSIBILITY THAT CAM LOCK COULD HAVE DEPARTED THE AIRCRAFT IN FLIGHT.
- [SDR DALA2018071604491](https://openairdocs.org/sdr/DALA2018071604491.md): Turbine · damaged · Jul 16, 2018 · N986DL · Doug MD88 · Turbine Section
  > THE CREW RETURNED THE AIRCRAFT TO ATL AFTER EXPERIENCING A COMPRESSOR STALL IN THE NR 1 ENGINE DURING CLIMB. THE ENGINE WAS KEPT RUNNING AT IDLE AND THE QRH WAS COMPLIED WITH. STATION CFR SAW FLAMES (IN THE ENGINE ONLY) SO THE FLIGHT CREW PULLED THE FIRE HANDL
- [SDR DALA2017111008038](https://openairdocs.org/sdr/DALA2017111008038.md): Door Frame · cracked · Nov 10, 2017 · N986DL · Doug MD88 · Fuselage Main, Structure
  > LEFT WHEEL WELL BS 937 MLG DOOR FRAME CRACKED. COMPLIED WITH HFEC IAW ERA 497265-14MA, TWO CRACKS COMING FROM PREVIOUS STOP DRILLS. REMOVED THE MLG DOOR FRAME, AND INSTALLED A NEW MLG DOOR FRAME IAW ERA 497265-14 MA, SECTION III.
- [SDR DALA2017111008037](https://openairdocs.org/sdr/DALA2017111008037.md): Vane · debonded · Nov 9, 2017 · N986DL · Doug MD88 · Trailing Edge Flaps
  > FLAP VANE HAS AREA OF DEBONDING AT JUNCTION OF INBD AND OTBD FLIGHT SPOILERS. REPLACED THE FLAP VANE ASSY IAW AMM 27-51-03.
- [SDR DALA2017111008036](https://openairdocs.org/sdr/DALA2017111008036.md): Vane · debonded · Nov 9, 2017 · N986DL · Doug MD88 · Trailing Edge Flaps
  > FLAP VANE HAS AN AREA OF DEBONDING, AFT OF GROUND SPOILER PANEL. REPLACED THE FLAP VANE IAW AMM 27-51-03
- [SDR DALA2017111008040](https://openairdocs.org/sdr/DALA2017111008040.md): Vane · debonded · Oct 30, 2017 · N986DL · Doug MD88 · Trailing Edge Flaps
  > RT FLAP VANE JUST AFT OF GROUND SPOILER HAS AREA OF DISBOND. REMOVE AND REPLACED FLAP FIXED VANE IAW AMM 27-51-03 AND ERA 563105-14, REV ORG.
- [SDR DALA2017021301167](https://openairdocs.org/sdr/DALA2017021301167.md): Battery · discharged · Feb 11, 2017 · N986DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTS AFT TAIL UPPER DO NOT TURN ON. CHANGED BATTERIES PACK AFT RIGHT LAV. OPERATIONAL CHECK OK.
- [SDR DALA2016122510089](https://openairdocs.org/sdr/DALA2016122510089.md): Support · damaged · Dec 25, 2016 · N986DL · Doug MD88 · Fuselage Miscellaneous Structure
  > RIGHT NLG STEERING ACTUATOR DAMAGED RIGHT SIDE NLG SUPPORT WEB. INSTALLED REPAIR IAW SRM 53-05 REPAIR 47A STEP (B) (3) (B).
- [SDR DALA2016120909773](https://openairdocs.org/sdr/DALA2016120909773.md): Battery Pack · discharged · Dec 9, 2016 · N986DL · Doug MD88 · Emergency Lighting
  > CABIN CEILING EMERGENCY STANDBY LIGHT INOP FROM ROW 22 TO 26. REPLACED BATTERY PACK IN THE OVERHEAD BIN 24 RT. LIGHT CHECKS NORMAL.
- [SDR DALA2016113009419](https://openairdocs.org/sdr/DALA2016113009419.md): Battery · discharged · Nov 30, 2016 · N986DL · Doug MD88 · Emergency Lighting
  > EMERGENCY POWER CEILING LIGHTS INOP AT ROW 22-26, 33 AND 36. REMOVED & REPLACED 4 EA BATTERY PACK BATTERIES. CEILING LIGHTS AT 22-26 & 33-36. OPS CCK GOOD.
- [SDR DALA2016041102771](https://openairdocs.org/sdr/DALA2016041102771.md): Actuator · inoperative · Apr 9, 2016 · N986DL · Doug MD88 · Cabin Pressure Control System
  > PRESSURIZATION AUTO INOPERATIVE. MANUAL SYS WAS MARGINAL. MOVE INDICATOR 2" WITH NO CHANGE IN RATE. THEN.2500" WOULD GIVE 100 FPM. PERFORMED BITE OF BOTH AUTO PRESSURE CONTROLLERS. AC MOTOR FAULTS ON BOTH 1 AND 2. C/W AMDS W/C 2132-01033-01 AND T/S IAW TSM 2
- [SDR DALA2016022301329](https://openairdocs.org/sdr/DALA2016022301329.md): B-Nut · leaking · Feb 22, 2016 · N986DL · Doug MD88 · Turbine Engine Oil System
  > LEFT OIL PRESSURE LOW AT 24,000. FOLLOWED BY ZERO OIL QTY. SHUTDOWN LT ENGINE IN FLIGHT. FOUND LOOSE B-NUT AT 8 O`CLOCK POSITION, RT ABOVE STARTER. OIL LINE IS DISCONNECTED. REPLACED IAW AMDS W/C 7100-4682-LT.
- [SDR DALA2016021601089](https://openairdocs.org/sdr/DALA2016021601089.md): Battery Pack · inoperative · Feb 15, 2016 · N986DL · Doug MD88 · Emergency Lighting
  > MAINTENANCE FOUND THE OVERHEAD EMERGENCY LIGHTS AT BOTH FORWARD OVERWING EXIT DOORS INOPERATIVE. THE BATTERIES WERE REPLACED AND THE LIGHTS TESTED OK.
- [SDR DALA2016021201014](https://openairdocs.org/sdr/DALA2016021201014.md): Warning Horn · false activation · Feb 11, 2016 · N986DL · Doug MD88 · Ice/Rain Protection System
  > DURING TAKEOFF AND LANDING WITH ENGINE ANTI-ICE ON, NO WING ANTI-ICE SMOKE ALARMS IN BOTH AFT LAVS CAME ON, THEN SILENCED AFTER SEVERAL MINUTES. AT FL 360 WITH ONLY ENGINE ANTI-ICE ON, GOT RT AIR CONDITIONING SUPPLY TEMP HIGH ANNUNCIATION WITH SOME CABIN SMOK
- [SDR DALA2015111506966](https://openairdocs.org/sdr/DALA2015111506966.md): Skin · dented · Nov 14, 2015 · N986DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DENT ON PREVIOUS DOUBLER REPAIR, BS 238 BETWEEN LONG 17 - 18L ON OUTER FUSELAGE SKIN. REPAIRED IAW ER/A 273447-14, REV E.
- [SDR DALA2015111406964](https://openairdocs.org/sdr/DALA2015111406964.md): Skin · damaged · Nov 13, 2015 · N986DL · Doug MD88 · Fuselage Main, Plate/Skin
  > ELONGATED HOLE ON INTERNAL FUSELAGE SKIN, BELLY DRAIN HOLE, BS 1210 BETWEEN LONGERONS 29 - 30L. REPAIRED IAW ETI-88-15-373, REV 1 AND ER/A 539904-14, REV ORIG.
- [SDR DALA2015111406963](https://openairdocs.org/sdr/DALA2015111406963.md): Skin · cracked · Nov 13, 2015 · N986DL · Doug MD88 · Trailing Edge Flaps
  > CRACK ON SKIN SURFACE AT LT INBD FLAP OTBD GUIDE VANE APPROXIMATELY ON BS XRS=121-TO XRS =124. DAMAGE AREA WAS REPAIRED IAW ERA NR 539946-14, REV ORIGINAL.
- [SDR DALA2015111406962](https://openairdocs.org/sdr/DALA2015111406962.md): Door Frame · corroded · Nov 13, 2015 · N986DL · Doug MD88 · Fuselage Main, Structure
  > CORROSION ON PAN AT C1 CARGO DOOR JAMB FROM, BS 370 TO 427. BOTH SURFACES. C1 CARGO DOOR JAMB WAS REPAIRED IAM ER/A 539907-14, REV ORIGINAL.
- [SDR DALA2015111406960](https://openairdocs.org/sdr/DALA2015111406960.md): Frame · unknown · Nov 13, 2015 · N986DL · Doug MD88 · Fuselage Main, Frame
  > LOWER CHORD SPLICE ROUND ON BS 1338 BETWEEN LONGERONS 26-27L AND 26-27R. AREA WAS REPAIRED IAW ETI-88-15-372 REV 1 AND ER/A 539897-14, REV.
- [SDR DALA2015111306939](https://openairdocs.org/sdr/DALA2015111306939.md): Frame · cracked · Nov 12, 2015 · N986DL · Doug MD88 · Fuselage Main, Frame
  > CRACK ON FRAME BS 1174, LONGERON 5L. THE FRAME WAS REPAIRED IAW SRM 51-30-2 AND 51-30-5 AND ETI 88-15-393 AND ER/A 539932-14, REV ORIGINAL.
- [SDR DALA2015111306938](https://openairdocs.org/sdr/DALA2015111306938.md): Longeron · cracked · Nov 12, 2015 · N986DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 12R, BS 1437. THE LONGERON WAS ATTENDED WITH ER/A 539936-14, REV ORIG.
- [SDR DALA2015111306937](https://openairdocs.org/sdr/DALA2015111306937.md): Floor Support · cracked · Nov 12, 2015 · N986DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED CHANNEL ON FLOOR PANEL NR 256A, 465E AND 541F AT CABIN PASSENGER FLOOR PANELS WERE REPAIRED IAW SRM 53-05, FIG 131B.
- [SDR DALA2015111206933](https://openairdocs.org/sdr/DALA2015111206933.md): Spar Cap · cracked · Nov 11, 2015 · N986DL · Doug MD88 · Elevator, Spar/Rib
  > CRACK WAS FOUND OF 4.000" ON ELEVATOR SPAR CAP OF THE LT ELEVATOR BETWEEN BS XE=136 AND XE=140. SM, CARD 35, ZONE 60. CRACK WAS REPAIRED IAW ER/A 539903-14, REV ORIGINAL. PERFORM DECAL INSPECTION CONDITION IAW TOPP 30-10-70, PAGE 13, PARAGRAPH I. RII COMPLE
- [SDR DALA2015111206902](https://openairdocs.org/sdr/DALA2015111206902.md): Skin · cracked · Nov 11, 2015 · N986DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON FUSELAGE SKIN INTERNAL DOUBLER BETWEEN BS 1309-1322 AND LONGERONS 20-23L. REPAIRED IAW ER/A 508134-14, REV B.
- [SDR DALA2015111206901](https://openairdocs.org/sdr/DALA2015111206901.md): Skin · cracked · Nov 11, 2015 · N986DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CRACK OF 0.150" LENGTH ON FUSELAGE SKIN, BS 1418 BETWEEN LONGERON 2-3 LT, SM, CARD 2, ZONE 65. DAMAGE WAS REPAIRED IAW ER/A 539886-14, AD REV: ORIGINAL. REPAIR APPROVAL IS LIMITED TO 75,000 TOTAL CYCLES ONLY. ADDITIONAL E/A, ER/A REVISION, IS REQUIRED FOR
- [SDR DALA2015111106876](https://openairdocs.org/sdr/DALA2015111106876.md): Blanket · cracked · Nov 10, 2015 · N986DL · Doug MD88 · Airfoil Anti/De-ice System
  > CRACK ON T/E OF RT WING HEATER BLANKET STATION APPROXIMATELY XW=91.155. RT WING HEATER BLANKET WAS REPAIRED IAW ER/A 494597-14AD MA, REV A.
- [SDR DALA2015111106875](https://openairdocs.org/sdr/DALA2015111106875.md): Web · cracked · Nov 10, 2015 · N986DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACK AND CORROSION ON VENTRAL STAIRWAY MOVABLE CEILING SKIN AT AFT SECTION. REPAIR WAS ACCOMPLISHED IAW ETI 88-15-389, REV 1 AND ER/A 539926-14, REV ORIGINAL.
- [SDR DALA2015111106871](https://openairdocs.org/sdr/DALA2015111106871.md): Slide · damaged · Nov 10, 2015 · N986DL · Doug MD88 · Escape Slide
  > QRO MAINTENACE FOUND THAT THE L1 DOOR SLIDE PACK LACING WAS MISSING. A NEW LACING WAS INSTALLED IAW AES PACKING INSTRUCTIONS.
- [SDR DALA2016111608838](https://openairdocs.org/sdr/DALA2016111608838.md): Skin · corroded · Nov 9, 2015 · N986DL · Doug MD88 · Fuselage Main, Plate/Skin
  > AFT LAVATORY SERVICE DOOR CUTOUT SKIN & DOUBLER CORRODED REPAIR. REPAIRED IAW ER/A.
- [SDR DALA2015110906822](https://openairdocs.org/sdr/DALA2015110906822.md): Intercostal · corroded · Nov 8, 2015 · N986DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION OUT LIMITS ON INTERCOSTAL BETWEEN LONGERON 27 LT AND LONGERON 28LT, FROM BS Y=1309 TO Y=1322 AT AFT CARGO COMPARTMENT. NEW INTERCOSTAL WAS REPLACED DUE TO EXCESSIVE DAMAGE IAW SRM 51-30-2, 51-10-4, 51-10-3, PAR 21 AND 14, 51-30-5 AND DWG 9936718.
- [SDR DALA2015110906821](https://openairdocs.org/sdr/DALA2015110906821.md): Cargo Track · corroded · Nov 8, 2015 · N986DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON TIE TRACK BETWEEN Y=1155 TO Y=1003 RT SIDE AT AFT CARGO COMPARTMENT. DUE TO EXCESSIVE DAMAGE, TIE TRACK WILL BE REPLACED. NEW TRACK WAS DRILLED IAW SRM 51-10-4 NEW TRACK WAS INSTALLED IAW SRM 51-30-1.
- [SDR DALA2015110906816](https://openairdocs.org/sdr/DALA2015110906816.md): Cargo Track · corroded · Nov 8, 2015 · N986DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RT TIE TRACK BETWEEN BS 1212 -- 1309 AT AFT CARGO COMPARTMENT. TIE TRACK WAS REPLACED IAW SRM 51-30-1 AND SRM 51-10-4, CORROSION WAS FOUND EXCESSIVE DUE TO TIE TRACK WAS REPLACED.
- [SDR DALA2015110906823](https://openairdocs.org/sdr/DALA2015110906823.md): Frame · damaged · Nov 7, 2015 · N986DL · Doug MD88 · Fuselage Main, Frame
  > DAMAGE AT FRAME BS 1287 BETWEEN LONGERONS 11-12R. DAMAGE WAS BLENDED OUT, FOUND AREA OUT LIMITS, AND REPAIRED IAW SRM 53-01 AND 53-01 AND 51-30-2.
- [SDR DALA2015110806812](https://openairdocs.org/sdr/DALA2015110806812.md): Duct · cracked · Nov 7, 2015 · N986DL · Doug MD88 · Air Distribution System
  > CRACK ON Y DUCT INLET FLANGE. CRACK ON WYE DUCT WAS WELDED IAW ER/A 503276-14MA REV C AND REA WORKED AREA WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21.
- [SDR DALA2015110806809](https://openairdocs.org/sdr/DALA2015110806809.md): Pan · cracked · Nov 7, 2015 · N986DL · Doug MD88 · Cargo/Baggage Doors
  > CRACK ON INNER PAN BETWEEN BEAM 1-2 AT MID CARGO COMPARTMENT DOOR FWD EDGE. CRACK ON INNER PAN BETWEEN BEAM 1-2 WAS REPAIRED IAW ETI-88-15-387, REV ORIGINAL AND ERA 539925-14, REV ORIGINAL.
- [SDR DALA2015110806808](https://openairdocs.org/sdr/DALA2015110806808.md): Cargo Track · corroded · Nov 7, 2015 · N986DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LT TIE TRACK BETWEEN BS Y=1212 TO Y=1309 AT AFT CARGO COMPARTMENT. TIE TRACK WAS REPLACED DUE TO EXCESSIVE DAMAGE IAW SRM 51-30-1, 51-30-5, 51-10-4, 51-10-3 PAR 14 AND 21 AND DWG 5936660.
- [SDR DALA2015110806804](https://openairdocs.org/sdr/DALA2015110806804.md): Frame · corroded · Nov 6, 2015 · N986DL · Doug MD88 · Fuselage Main, Frame
  > CORROSION ON PREVIOUS REPAIR PARTS OF FRAME BETWEEN LONGERON 28LT TO LONG 28RT BS 1309 AT AFT CARGO COMPARTMENT. REPAIR INSTALLED AND CIC WAS APPLIED IAW SRM 51-30-5, 51-10-4, 53-03, FIG 2A, 51-10-3, PAR 14, 21, 38 F.
- [SDR DALA2015110706799](https://openairdocs.org/sdr/DALA2015110706799.md): Skin · cracked · Nov 6, 2015 · N986DL · Doug MD88 · Vertical Stabilizer, Plate/Skin
  > CRACK ON VERTICAL STABILIZER SKIN LT SIDE BETWEEN BS XFS=12 TO XFS=17, JUST UP TO RAM AIR DUCT. VERTICAL STABILIZER SKIN LT SIDE BETWEEN XFS=12-17 WAS REPAIRED IAW 55-01, FIG 2, 51-10-3, PARA 14, 21, 51-30-8.
- [SDR DALA2015110706798](https://openairdocs.org/sdr/DALA2015110706798.md): Pan · cracked · Nov 6, 2015 · N986DL · Doug MD88 · Cargo/Baggage Doors
  > CRACK INNER PAN BETWEEN FWD UPPER CORNER AND BEAM5 OF MID CARGO COMPARTMENT DOOR. CRACK ON INNER PAN BETWEEN FWD UPPER CORNER AND BEAM NR 5 WAS REPAIRED IAW SRM 52-03D, FIG 8 HFEC WAS PERFORMED AND NO CRACK WERE FOUND.
- [SDR DALA2015110606769](https://openairdocs.org/sdr/DALA2015110606769.md): Tab · damaged · Nov 6, 2015 · N986DL · Doug MD88 · Elevator, Tab Structure
  > ELONGATED BORES ON HINGE FITTING OF CONTROL TAB AT LT ELEVATOR BS XET=80. FITTING BRACKET ASSY ELEVATOR TAB LT WAS REPLACED IAW SRM 51-10-2.
- [SDR DALA2015110806806](https://openairdocs.org/sdr/DALA2015110806806.md): Cargo Track · corroded · Nov 5, 2015 · N986DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON TIE TRACK BETWEEN Y=1222 TO Y=1003 LT SIDE AT AFT CARGO COMPARTMENT. TIE TRACK WAS REPLACED IAW SRM 51-30-1, 51-10-4, 51-10-3 PAR 14 AND 21 AND 51-30-5.
- [SDR DALA2015110706800](https://openairdocs.org/sdr/DALA2015110706800.md): Floor Panel · delaminated · Nov 5, 2015 · N986DL · Doug MD88 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL BETWEEN BS 826 - 1003 IN PAX CABIN. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201, REPLACED IAW AMM 53-20-01-201, AND DWG 9936639, REV- P.
- [SDR DALA2015110606770](https://openairdocs.org/sdr/DALA2015110606770.md): Web · worn · Nov 5, 2015 · N986DL · Doug MD88 · Fuselage Main, Plate/Skin
  > WEAR ON TITANIUM WEB BS 1344 BETWEEN LONGERONS 27L & 27R. REPAIRED, AND INSTALLED IAW SRM 51-30-2 AND ER/A 094719-14MA, REV A.
- [SDR DALA2015110606766](https://openairdocs.org/sdr/DALA2015110606766.md): Longeron · cracked · Nov 5, 2015 · N986DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 11L AT BS 1380. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18, 51-10-3, PAR 21 AND 14.
- [SDR DALA2015110606765](https://openairdocs.org/sdr/DALA2015110606765.md): Longeron · cracked · Nov 5, 2015 · N986DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 13 LT ON BS 1380 AFT ACCESSORIES COMPARTMENT. CRACKED LONGERON 13 LT ON BS 1380 WAS REPLACED IAW SRM 53-14-4, 51-30-2, 51-10-3, PAR 21 AND 14 AND 51-30-5.

Next page: https://openairdocs.org/deregistered/N986DL-2022-04-25/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 = 'N986DL' AND deregistration_id = 'N986DL-2022-04-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N986DL-2022-04-25/reports

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