# Service difficulty reports: N985DL, cancelled Dec 17, 2022

A list on [N985DL, cancelled Dec 17, 2022](https://openairdocs.org/deregistered/N985DL-2022-12-17.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 4 · 172 reports

- [SDR DALA2019061703577](https://openairdocs.org/sdr/DALA2019061703577.md): Light · inoperative · Jun 16, 2019 · N985DL · Doug MD88 · Emergency Lighting
  > EMERGENCY ESCAPE PATH LIGHT INOP AT 16D. REPL LIGHT ASSY OPS CHECK GOOD REF MD88 AMM 33-53. (LP4629489)
- [SDR DALA2018101506040](https://openairdocs.org/sdr/DALA2018101506040.md): Smoke Detector · defective · Oct 12, 2018 · N985DL · Doug MD88 · Smoke Detection
  > AFT LAV SMOKE DETECTER RT GOING OFF. AFT RT LAV SMOKE DETECTOR NOT TESTING REPLACED SAME OPS NORMAL. (LP4822100)
- [SDR DALA2018100205820](https://openairdocs.org/sdr/DALA2018100205820.md): Fairing · missing · Sep 29, 2018 · N985DL · Doug MD88 · Trailing Edge Flaps
  > LEFT WING NR 2 FLAP SECONDARY INB FAIRING MISSING. LT WING NR 2 FLAP SECONDARY INB FAIRING FWD TO CDL 57-50-03. REPORTED DUE TO POSSIBILITY THAT PART MAY HAVE DEPARTED THE AIRCRAFT DURING FLIGHT. (LP5352438)
- [SDR DALA2018090405403](https://openairdocs.org/sdr/DALA2018090405403.md): Instrument Panel · unsecure · Aug 31, 2018 · N985DL · Doug MD88 · Instrument Panel
  > REJECTED TAKEOFF AT 100KNTS DUE TO COPILOTS INSTRUMENT PANEL COMING OUT. MAINTENANCE SECURED PANEL AND PERFORMED A HIGH ENERGY STOP INSPECTION. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR DALA2018080604863](https://openairdocs.org/sdr/DALA2018080604863.md): Battery Pack · malfunctioned · Aug 4, 2018 · N985DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE FROM ROW 31 AFT. AFTER TESTING FROM AFT BATTERY PACK, ALL LIGHTS OPS NORMAL.
- [SDR DALA2018073004753](https://openairdocs.org/sdr/DALA2018073004753.md): Connector · loose · Jul 29, 2018 · N985DL · Doug MD88 · Light System Wiring
  > DURING SVC CK, FOUND SEAT 14 AISLE EMERGENCY LIGHT OUT. FOUND LOOSE CONNECTOR UNDER SEAT. RESECURED CONNECTOR. CKS GOOD.
- [SDR DALA2018073004752](https://openairdocs.org/sdr/DALA2018073004752.md): Battery Pack · discharged · Jul 29, 2018 · N985DL · Doug MD88 · Emergency Lighting
  > DURING SVC CK, FOUND CEILING EMERGENCY LIGHTS OUT AT ROWS 16-20. REMOVED AND REPLACED BATTERY PACK AT ROW 17DC PER AMM 33-53. LIGHTS CK GOOD.
- [SDR DALA2018032201838](https://openairdocs.org/sdr/DALA2018032201838.md): Lug · cracked · Mar 21, 2018 · N985DL · Doug MD88 · Stabilizer Actuator
  > HORIZONTAL STABILIZER JACKSCREW ACTUATOR GEAR BOX, LEFT ATTACH POINT TO HORIZONTAL STAB, AFT LUG IS CRACKED. COMPLETED JACKSCREW ASSY INSTALLATION AND OP'S CHECK PER 2742-4540 AND AMM 27-40-01.
- [SDR DALA2018031601726](https://openairdocs.org/sdr/DALA2018031601726.md): Nut Plate · broken · Mar 15, 2018 · N985DL · Doug MD88 · Vertical Stabilizer Miscellaneous Structure
  > VERTICAL STABILIZER TIP, HORSESHOE ANGLE (AROUND TOP OF THS JACKSCREW MOTOR) FOR TOP CAP ATTACHMENT, MISSING/BROKEN NUTPLATES AT BOTH AFT ENDS. INSTALLED NUT PLATES REF SRM 51-30-02.
- [SDR DALA2018010800126](https://openairdocs.org/sdr/DALA2018010800126.md): Lamp · inoperative · Jan 8, 2018 · N985DL · Doug MD88 · Emergency Lighting
  > SEAT 31ED EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-00, OPS CHECKED GOOD.
- [SDR DALA2017061804796](https://openairdocs.org/sdr/DALA2017061804796.md): Skin Panel · cracked · Jun 17, 2017 · N985DL · Doug MD88 · Horizontal Stabilizer, Plate/Skin
  > LFEC INSPECTION OF HORIZONTAL STABILIZER RT UPPER CENTER SKIN PANEL PER STEP 5. OF WORKCARD SHOWS A CRACK INDICATION FROM AFT EDGE OF SKIN FORWARD APPROXIMATELY 1" IN LENGTH. REPAIRED PER ERA 559453-14AD.
- [SDR DALA2017061504747](https://openairdocs.org/sdr/DALA2017061504747.md): Cable · worn · Jun 14, 2017 · N985DL · Doug MD88 · Aerodynamic Fairings
  > UPPER LEFT TAILCONE LATCH RELEASE CABLE IS WORN. REPLACED CABLE ASSY IAW AMM 20-10-17.
- [SDR DALA2017040502752](https://openairdocs.org/sdr/DALA2017040502752.md): Connector · damaged · Apr 5, 2017 · N985DL · Doug MD88 · Landing Gear System Wiring
  > LEFT INBOARD AND LEFT OUTBOARD ANTI-SKID AMBER MESSAGES INFLIGHT. CREW DECLARED EMERGENCY. FOUND CONNECTOR TO P1-1148 WITH PUSHED PINS. REPLACED THE CONNECTOR AND SYSTEM CHECKED GOOD.
- [SDR DALA2017031402014](https://openairdocs.org/sdr/DALA2017031402014.md): Battery Pack · inoperative · Mar 14, 2017 · N985DL · Doug MD88 · Emergency Lighting
  > FOUND LEFT AND RIGHTT BS 875 OVERWING FWD EMERGENCY EXIT LIGHTS OUT. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-53. OPS CHECKED NORMAL.
- [SDR DALA2017011600386](https://openairdocs.org/sdr/DALA2017011600386.md): Unknown · odor · Jan 15, 2017 · N985DL · Doug MD88 · Air Distribution System
  > AT ALTITUDE 310, FLIGHT ATTENDANTS REPORTED A STRONG ELECTRICAL ODOR FROM FORWARD PART OF FIRST CLASS. TURNED OFF SIDE PANEL LIGHTS AND ODOR DISSAPATED AFTER 5-10 MINS. COMPLIED WITH JIC 2120-2367 THROUGH STEP 6. COMPLETED DUCT BURNOUT. NO ODOR PRESENT. APU
- [SDR DALA2016112109005](https://openairdocs.org/sdr/DALA2016112109005.md): Receptacle · worn · Nov 19, 2016 · N985DL · Doug MD88 · Aerodynamic Fairings
  > DURING TAILCONE CHECK, FOUND FOUR TAILCONE RECEPTICALS WORN AND LOOSE. REMOVED AND REPLACED THE RECEPITCALS IAW SRM 51-30-02.
- [SDR DALA2016112008996](https://openairdocs.org/sdr/DALA2016112008996.md): Receptacle · lack of lube · Nov 19, 2016 · N985DL · Doug MD88 · Aerodynamic Fairings
  > DURING TAILCONE FUNCTIONAL CHECK, THE TAILCONE DID NOT DROP PROPERLY WITH AFT CABIN DOOR OPENED IN THE ARMED POSITION. FOUND RECEPTICALS DRY WITH LITTLE LUBE. CLEANED AND LUBED RECEPTICALS. PERFORMED SUCCESSFUL TEST OF AFT CABIN DOOR PER AMDS 5350-010077-0101.
- [SDR DALA2016110208193](https://openairdocs.org/sdr/DALA2016110208193.md): Light · inoperative · Nov 1, 2016 · N985DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHT AISLE (13D) INOP. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-50. OPS CK OK.
- [SDR DALA2016082606215](https://openairdocs.org/sdr/DALA2016082606215.md): Bottle · low pressure · Aug 25, 2016 · N985DL · Doug MD88 · Escape Slide
  > L2 SLIDE BOTTLE PRESSURE LOW. R & R L2 SLIDE AMDS CARD 2561-4002, MPN D29985-103, SN OFF 0980. ALL RII STEPS HAVE BEEN ACCOMPLISH IAW AMDS 2561-4002.
- [SDR DALA2016071105206](https://openairdocs.org/sdr/DALA2016071105206.md): Wire · damaged · Jul 9, 2016 · N985DL · Doug MD88 · Light System Wiring
  > SEAT 12E EMERGENCY LIGHT INOPERATIVE. REPAIRED SEAT FRAME WIRING. OPS CKS GOOD. REF SWPM 20-10.
- [SDR DALA2016032502306](https://openairdocs.org/sdr/DALA2016032502306.md): Trim Tab · damaged · Mar 25, 2016 · N985DL · Doug MD88 · Elevator, Tab Structure
  > LIGHTNING STRIKE DAMAGE TO RT OTBD ELEVATOR TRIM TAB. ANTI-FLOAT TAB REPLACED ON AMDS WC 2730-4382.
- [SDR DALA2015101406135](https://openairdocs.org/sdr/DALA2015101406135.md): Floor Panel · punctured · Oct 11, 2015 · N985DL · Doug MD88 · Fuselage Floor Panel
  > A PUNCTURE IN AFT CARGO BAY FLOOR JUST FWD OF DOOR. INSTALLED A REPAIR IAW SRM 53-05.
- [SDR DALA2015061503839](https://openairdocs.org/sdr/DALA2015061503839.md): Bearing · damaged · Jun 14, 2015 · N985DL · Doug MD88 · Fuselage, Landing Gear Attach Fittings
  > CORROSION AND SCRATCHES ON RT MLG ACTUATOR SUPPORT FITTING BUSHING AND BEARINGS. ACTUATOR SUPPORT FITTING BUSHING AND BEARING ON RT MLG WERE R & R UNDER CARD 10, ZONE 18 AND CARD 5740-01139-04B. RII COMPLETED.
- [SDR DALA2015061503835](https://openairdocs.org/sdr/DALA2015061503835.md): Bushing · damaged · Jun 14, 2015 · N985DL · Doug MD88 · Fuselage, Landing Gear Attach Fittings
  > CORROSION AND SCRATCHES ON LT MLG ACTUATOR SUPPORT FITTING BUSHING AND BEARING. ACTUATOR SUPPORT FITTING BUSHING AND BEARING ON LT MLG INSTALLED UNDER CARD 5740-01139-04A, JOB 089-0001 AND CMM 20-10-7. BEARING AND BUSHING WERE REPLACED ON CARD 11, A/C ZONE 17
- [SDR DALA2015061503830](https://openairdocs.org/sdr/DALA2015061503830.md): Access Panel · damaged · Jun 14, 2015 · N985DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON PREVIOUS REPAIR BUSHINGS AT LT WING SETTLEMENT AREA OF ACCESS PANEL 1357C. ACCESS PANEL WAS REPAIRED.
- [SDR DALA2015061503829](https://openairdocs.org/sdr/DALA2015061503829.md): Access Panel · damaged · Jun 14, 2015 · N985DL · Doug MD88 · Wing, Plate/Skin
  > MISSING REPAIR BUSHING ON CUTOUT FUEL ACCESS RT WING. BUSHING AND CUTOUT ACCESS PANEL WAS REPAIR IAW ETI-88-15-186, REV 1, ER/A 534394-14 REV ORIGINAL.
- [SDR DALA2015061403801](https://openairdocs.org/sdr/DALA2015061403801.md): Fitting · corroded · Jun 13, 2015 · N985DL · Doug MD88 · Fuselage, Landing Gear Attach Fittings
  > CORROSION WAS FOUND ON THE LT MLG ACTUATOR SUPPORT FITTING BEARING BORE. THE AREA WAS REPAIRED IAW ER/A 534421-14AD REV ORIGINAL AND A NEW BEARING WAS REPLACED.
- [SDR DALA2015061503771](https://openairdocs.org/sdr/DALA2015061503771.md): Access Panel · corroded · Jun 11, 2015 · N985DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON COUNTERSINK SETTLEMENT AREA AND UPPER SURFACE ON FUEL ACCESS PANEL 1409C ON THE RT WING. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.
- [SDR DALA2015061103768](https://openairdocs.org/sdr/DALA2015061103768.md): Longeron · corroded · Jun 11, 2015 · N985DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 22L BS 1338 IN AFT CARGO BAY. REPLACED THE LONGERON IAW SRM 51-30-5.
- [SDR DALA2015061103756](https://openairdocs.org/sdr/DALA2015061103756.md): Intercostal · corroded · Jun 10, 2015 · N985DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL STA Y=769-788 BETWEEN LONGERONS 27-28RT. THE INTERCOSTAL WAS REPLACED IAW DWG 9915554, REV J, SRM 51-10-4, 51-30-1, 51-30-2, 51-30-5, AND 51-10-3 PAR 14-21.
- [SDR DALA2015061103750](https://openairdocs.org/sdr/DALA2015061103750.md): Beam · corroded · Jun 10, 2015 · N985DL · Doug MD88 · Fuselage Main, Structure
  > CORROSION ON LOWER FWD FLANGE BS 652-671 AND VERTICAL FACE BS 644 AT MID CARGO COMPARTMENT DOOR FRAME BEAM REF ORNRC 154 ZONE 100 MRB 53-018-02, CARD 219, ZONE 100. MID CARGO DOOR JAMB BEAM WAS REPAIRED IAW SRM 53-05, FIG 123A, OPTION 2 AND ER/A 534411-14 REV
- [SDR DALA2015061103740](https://openairdocs.org/sdr/DALA2015061103740.md): Longeron · corroded · Jun 10, 2015 · N985DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 23L BETWEEN BS 1136 - 1250. THE LONGERON WAS REPLACED IAW SRM 53-01 FIG 18 51-30-2, 51-30-5, AND 51-10-3, PAR 38.
- [SDR DALA2015061103751](https://openairdocs.org/sdr/DALA2015061103751.md): Intercostal · cracked · Jun 9, 2015 · N985DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL Y=37 AND X=11, X=-11 AT NLG WHEEL WELL. LT INTERCOSTAL WAS REPAIRED IAW 51-01, PAR 4, STEP 21 AND DOUBLER WAS FABRICATED IAW SRM 53-14-1, 51-10-2, DOUBLER WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 21/14.
- [SDR DALA2015061003734](https://openairdocs.org/sdr/DALA2015061003734.md): Longeron · cracked · Jun 9, 2015 · N985DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON 20L BS 1003. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 22, 51-30-3, 51-10-3 PAR 14, 21, 38.
- [SDR DALA2015061003733](https://openairdocs.org/sdr/DALA2015061003733.md): Longeron · cracked · Jun 9, 2015 · N985DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON 20R BS 1003. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 22, 51-30-5, 51-10-3 PAR 14,21,38.
- [SDR DALA2015061003729](https://openairdocs.org/sdr/DALA2015061003729.md): Access Panel · corroded · Jun 9, 2015 · N985DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 1466C AT RT WING. CORROSION WAS REMOVED IAW SRM 51-22-2A AND COUNTERSINK HOLES WERE MEASURED MAX DIAMETER ALLOWABLE IS 0.660" AND MAX DIAMETER MEASURED IS 0.670" IN 3 ADJACENT HOLES THEREFORE OUT OF LIMITS IAW SRM
- [SDR DALA2015061003728](https://openairdocs.org/sdr/DALA2015061003728.md): Shear Tie · cracked · Jun 9, 2015 · N985DL · Doug MD88 · Fuselage Internal Mounting Structure
  > SHEAR TIE BS 1437 BETWEEN LONGERONS 16 - 17R IS CRACKED. THE SHEAR TIE WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.
- [SDR DALA2015061003727](https://openairdocs.org/sdr/DALA2015061003727.md): Shear Tie · cracked · Jun 9, 2015 · N985DL · Doug MD88 · Fuselage Internal Mounting Structure
  > SHEAR TIE ON BS 1446 LONGERONS 17 - 18L IS CRACKED. THE SHEAR TIE WAS REPLACED IAW SRM 53-14-4, FIG. 3.
- [SDR DALA2015061003736](https://openairdocs.org/sdr/DALA2015061003736.md): Tab · dented · Jun 9, 2015 · N985DL · Doug MD88 · Elevator Structure
  > DENT ON ANTI-FLOAT TAB UPPER SURFACE AT RT ELEVATOR. ANTI-FLOAT TAB WAS REPAIRED IAW SRM 55-04 PAR 2.
- [SDR DALA2015061003688](https://openairdocs.org/sdr/DALA2015061003688.md): Skin · corroded · Jun 9, 2015 · N985DL · Doug MD88 · Horizontal Stabilizer, Plate/Skin
  > CORROSION ON BARREL NUT HOLE NR 13 AT LT HORIZONTAL STABILIZER STA XH=6.625. DAMAGE ON BARREL NUT HOLE WAS REPAIRED IAW ETI-88-15-173, REV 1 AND ER/A 534422-14, REV ORIGINAL.
- [SDR DALA2015062203890](https://openairdocs.org/sdr/DALA2015062203890.md): Floor Panel · damaged · Jun 8, 2015 · N985DL · Doug MD88 · Fuselage Floor Panel
  > DAMAGE ON FERRUL AND PUNCTURE ON PAX CABIN FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201 AND INSTALLED IAW AMM 53-20-01-201.
- [SDR DALA2015060903683](https://openairdocs.org/sdr/DALA2015060903683.md): Longeron · cracked · Jun 8, 2015 · N985DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 16L, BS 1437. THE LONGERON WAS REPLACED IAW SRM 53-14-4, FIG 4 AND DWG 5910228, REV KF AND SRM 51-30-5.
- [SDR DALA2015061103708](https://openairdocs.org/sdr/DALA2015061103708.md): Frame · cracked · Jun 7, 2015 · N985DL · Doug MD88 · Fuselage Main, Frame
  > CRACKED FRAME BS 1485. REPAIRED IAW SRM 53-03, PAR 38, FIG 43.
- [SDR DALA2015061003730](https://openairdocs.org/sdr/DALA2015061003730.md): Intercostal · cracked · Jun 7, 2015 · N985DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL ON BS 1338 LONGERON 3R, AFT FACE. REPAIRED THE INTERCOSTAL IAW SRM 53-01.
- [SDR DALA2015061003738](https://openairdocs.org/sdr/DALA2015061003738.md): Access Panel · corroded · Jun 7, 2015 · N985DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE 1460C AT RT WING, CARD 205, ZONE 00. CORROSION ON ACCESS DOOR 1460C WAS REMOVED IAW SRM 51-10-03 AND COUNTERSINK HOLES WERE MEASURED AND MAX DIAMETER MEASURED IS 0.578", 6 HOLES THERFORE WAS FOUND OUT OF LIMITS IAW
- [SDR DALA2015060903678](https://openairdocs.org/sdr/DALA2015060903678.md): Cusp Web · corroded · Jun 7, 2015 · N985DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON RT CUSP WEB BETWEEN X=-54 TO X=-60, BS 579- 598. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13, 51-30-5, AND 51-10-3 PARR 14, 21. UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07, PARR 5, FIG 3, SHT 1, 2. AND FOUND OUT OF LIMITS IAW ER/A 511
- [SDR DALA2015060803673](https://openairdocs.org/sdr/DALA2015060803673.md): Longeron · cracked · Jun 7, 2015 · N985DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON 8 BS 1309. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18 AND SRM 51-10-3 PAR 14, 21 SRM 51-30-2, SRM 51-30-5.
- [SDR DALA2015061003689](https://openairdocs.org/sdr/DALA2015061003689.md): Skin · damaged · Jun 7, 2015 · N985DL · Doug MD88 · Fuselage Main, Plate/Skin
  > PERFORM REPAIR ON FUSELAGE SKIN Y=237 BETWEEN. LONGERONS 18-20L, REF MON 88, CARD 220 ZONE 00. PERMANENT REPAIR WAS PERFORMED IAW SRM 53-04-5, FIG 3, CLASS I AND UNDER MONITOR NR 88. PERFORM DECAL INSPECTION ON PREVIOUS REPAIR AT EVERY "C" CHECK IAW TOPP
- [SDR DALA2015062203889](https://openairdocs.org/sdr/DALA2015062203889.md): Cusp Web · corroded · Jun 6, 2015 · N985DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON DOUBLER OF REPARATION ON CUSP WEB BETWEEN STA Y=984 TO Y=1003 AND X=-54 TO X=-60, RT SIDE. CUSP WEB WAS REPLACED IAW SRM 53-05, 51-30-2, 51-30-5 AND 51-10-3 PAR 14, 21.
- [SDR DALA2015061103701](https://openairdocs.org/sdr/DALA2015061103701.md): Access Panel · corroded · Jun 6, 2015 · N985DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE 1311C AT LT WING. REPLACED THE ACCESS PANEL.

Next page: https://openairdocs.org/deregistered/N985DL-2022-12-17/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 = 'N985DL' AND deregistration_id = 'N985DL-2022-12-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N985DL-2022-12-17/reports

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