# Service difficulty reports: N919DL, cancelled Jan 14, 2019

A list on [N919DL, cancelled Jan 14, 2019](https://openairdocs.org/deregistered/N919DL-2019-01-14.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 2 · 79 reports

- [SDR DALA2018021300877](https://openairdocs.org/sdr/DALA2018021300877.md): A/C Pack · shutdown · Feb 12, 2018 · N919DL · Doug MD88 · Cabin Cooling System
  > SMOKE - COLD TEMPERATURE IN DSM. WHILE AT GATE DURING BOARDING PLACED RIGHT PACK TO "ON". RT PACK OVER TEMP SHUTDOWN WITH SMOKE IN AFT CABIN. SMOKE DISSIPATED AFTER RT PACK WAS SHUTDOWN. ONLY 15 PASSENGERS WERE DEPLANED PER THE FLIGHT CREW REPORT AND NONE REPO
- [SDR DALA2017111508159](https://openairdocs.org/sdr/DALA2017111508159.md): Battery Pack · inoperative · Nov 15, 2017 · N919DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTS OVERWING INOPERATIVE. R & R THE BATTERIES IN B5105 IAW AMM 33-53. OPS CHECKED GOOD.
- [SDR DALA2017083106479](https://openairdocs.org/sdr/DALA2017083106479.md): Battery Pack · inoperative · Aug 23, 2017 · N919DL · Doug MD88 · Emergency Lighting
  > BOTH FWD OVERWING LIGHTED EXIT SIGNS INOPERATIVE.. INSTALLED NEW BATTERIES IAW AMM 33-53-00/401. ALL CHECKED OK.
- [SDR DALA2017072805726](https://openairdocs.org/sdr/DALA2017072805726.md): Connector · failed · Jul 28, 2017 · N919DL · Doug MD88 · Engine Oil System Wiring
  > DIVERTED DUE TO NR 1 ENGINE OIL PRESSURE HIGH. NR 1 THROTTLE AT IDLE WITH OIL PRESSURE IN RANGE. MAINTENANCE REPLACED THE SYSTEMS DISPLAY PANEL, PLUG P1-813, OIL PRESSURE TRANSMITTER. TAKEOFF POWER RUNS CONFIRMED OIL PRESSURE NOW NORMAL.
- [SDR DALA2017072105596](https://openairdocs.org/sdr/DALA2017072105596.md): Door Frame · corroded · Jul 20, 2017 · N919DL · Doug MD88 · Fuselage Main, Structure
  > CORROSION ON THE LOWER DOOR FRAME BEAM BS 1154 TO 1211. CORROSION WAS REMOVED IAW SRM 51-10-3, PAR 26, 21 AND 14. FOUNE WITHIN LIMITS IAW SRM 53-05, FIG 123, AND NDT SPM 04-00-07, FIG 3 PAR 5, SHEET 1-2.
- [SDR DALA2017030901906](https://openairdocs.org/sdr/DALA2017030901906.md): Spring · failed · Mar 8, 2017 · N919DL · Doug MD88 · Flight Compartment Equipment
  > DURING TAKEOFF ROLL AND AFTER ROTATION, THE CAPTAIN'S SEAT ROLLED BACK TO THE FULL AFT POSITION. REPLACED LOCK RETURN SPRING.
- [SDR DALA2016100707098](https://openairdocs.org/sdr/DALA2016100707098.md): Spar Cap · cracked · Oct 6, 2016 · N919DL · Doug MD88 · Wing Spar
  > RT WING REAR SPAR LOWER CAP PER W/C 5710-0110-05A SHOWS A CRACK INDICATION AT 6:30 POSITION TOTAL LENGTH OF CRACK TO BE DETERMINED AFTER DISASSEMBLY PER W/C 57-10-0110-05B. HFEC INSPECTION WAS ACCOMPLISHED ON RH WING REAR SPAR LOWER CAP ONE CRACK WAS FOUND (L
- [SDR DALA2016100607084](https://openairdocs.org/sdr/DALA2016100607084.md): Skin · corroded · Oct 5, 2016 · N919DL · Doug MD88 · Wing, Plate/Skin
  > CORROSION ON RIGHT HEATER BLANKET SKIN AROUND THE FUEL ACCESS 1410C. HEATER BLANKET PANEL WAS REPLACED AND SYSTEM OPS TEST WAS PERFORMED IAW AMM 30-80-02.
- [SDR DALA2016100607083](https://openairdocs.org/sdr/DALA2016100607083.md): Spar Cap · cracked · Oct 5, 2016 · N919DL · Doug MD88 · Wing Spar
  > HFEC INSPECTION OF RT WING REAR SPAR LOWER CAP IAW W/C 5710-0110-05A SHOW A CRACK INDICATION AT 6:30 POSITION. REPAIRED IAW CARD 5710-01110-06, DRAWING J060271-510 REV. T, AND ER/A 550317-14 AD REV. ORG.
- [SDR DALA2016092506825](https://openairdocs.org/sdr/DALA2016092506825.md): Access Panel · punctured · Sep 24, 2016 · N919DL · Doug MD88 · Wing, Plate/Skin
  > HIDDEN DAMAGE: PUNCTURE ON SECONDARY ACCESS COVER 3070-100, LT WING. SECONDARY ACCESS COVER NR 3070-100 AT LT WING WAS EVALUATED AND IT WAS FOUND OUT OF LIMITS, SECONDARY ACCESS COVER NR 3070-100 WAS REPLACED IAW ERA 530866-14AD MA, REV ORIGINAL.
- [SDR DALA2016092406822](https://openairdocs.org/sdr/DALA2016092406822.md): Beam · cracked · Sep 23, 2016 · N919DL · Doug MD88 · Fuselage Main, Structure
  > INITIAL: CRACKED BEAM 1, FORWARD EDGE, APPROXIMATELY STA Y=172 AT FORWARD SERVICE DOOR. DAMAGED BEAM NR 1WAS REPLACED IAW SRM 51-30-1, 51-30-2 AND 51-30-5.
- [SDR DALA2016051603962](https://openairdocs.org/sdr/DALA2016051603962.md): Connector · disconnected · May 14, 2016 · N919DL · Doug MD88 · Light System Wiring
  > EMERGENCY LIGHT OUT SEAT 29ED. RECONNECTED WIRE CLIP CONNECTOR AT ROW 29ED. OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR DALA2015121407589](https://openairdocs.org/sdr/DALA2015121407589.md): Pin · backed out · Dec 11, 2015 · N919DL · Doug MD88 · Escape Slide
  > DURING INSPECTION, FOUND L1 DOOR SLIDE DEPLOYMENT PINS OUT. REPLACED 1L DOOR SLIDE AND COMPLIED WITH REQUIRED INSPECTIONS.
- [SDR DALA2015040802685](https://openairdocs.org/sdr/DALA2015040802685.md): Battery Pack · inoperative · Apr 7, 2015 · N919DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY CEILING LIGHTS FROM ROWS 23-25 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECK WAS GOOD.
- [SDR DALA2015021701283](https://openairdocs.org/sdr/DALA2015021701283.md): Battery Pack · inoperative · Feb 15, 2015 · N919DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT THE FORWARD OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD.
- [SDR DALA2014100905487](https://openairdocs.org/sdr/DALA2014100905487.md): Sleeve · worn · Oct 8, 2014 · N919DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE DISCOVERED THAT THE KEVLAR SLEEVE OVER THE RELEASE CABLE FOR THE TAILCONE WAS WORN OUT OF ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.
- [SDR DALA2014100405443](https://openairdocs.org/sdr/DALA2014100405443.md): Floorbeam · corroded · Oct 3, 2014 · N919DL · Doug MD88 · Fuselage Main, Floor Beam
  > CORROSION ON UPPER SURFACE FLOORBEAM AT BS 427 FWD CARGO BAY. REPLACED FLOORBEAM IAW SRM 51-30-2, 51-10-4.
- [SDR DALA14022770919](https://openairdocs.org/sdr/DALA14022770919.md): Battery Pack · inoperative · Apr 10, 2014 · N919DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN FOR THE AFT OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD.
- [SDR DALA13010580919](https://openairdocs.org/sdr/DALA13010580919.md): Power Supply · inoperative · Mar 6, 2013 · N919DL · Doug MD88 · Emergency Lighting
  > DURING LINE MX CHECK, THE OVERWING EMERGENCY EXIT IDENTIFIER LIGHTS WERE FOUND TO BE INOPERATIVE. THE POWER SUPPLY BATTERIES WERE REPLACED AND THE EMERGENCY LIGHTS OPERATION CHECKED OK.
- [SDR DALA13004820919](https://openairdocs.org/sdr/DALA13004820919.md): Battery Pack · inoperative · Jan 29, 2013 · N919DL · Doug MD88 · Emergency Lighting
  > FLIGHT DISCOVERED THAT THE EMERGENCY LIGHTS IN THE COCKPIT HAD BECOME INOPERATIVE. MX REPLACED THE ASSOCIATED BATTERY PACK AND THE LIGHTS RETURNED TO NORMAL OPERATION.
- [SDR DALA12008740919](https://openairdocs.org/sdr/DALA12008740919.md): Structure · stuck · Sep 27, 2012 · N919DL · Doug MD88 · Fuselage Structure (General)
  > MX FOUND THE AFT STAIRWAY CATWALK BINDING IN THE HALF-WAY UP POSITION DURING TROUBLESHOOTING.
- [SDR DALA1240430919](https://openairdocs.org/sdr/DALA1240430919.md): Wire Harness · damaged · Jul 5, 2012 · N919DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 34D IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.
- [SDR DALA1217050919](https://openairdocs.org/sdr/DALA1217050919.md): Stop Fitting · cracked · Mar 19, 2012 · N919DL · Doug MD88 · Cargo/Baggage Doors
  > DURING HMV A CRACKED STOP FITTING WAS FOUND ON STA Y=636 AT BEAM NR 5 AND CRACKED PAN BELOW SAME STOP FITTING. AT MID CARGO COMPARTMENT DOOR CRACKED PAN WAS REPAIRED IAW MD88 SRM 52-05 FIG 50 AND THE STOP FITTING WAS REPLACED.
- [SDR DALA1216460919](https://openairdocs.org/sdr/DALA1216460919.md): Doubler · corroded · Mar 17, 2012 · N919DL · Doug MD88 · Fuselage Miscellaneous Structure
  > DURING HMV CORROSION WAS FOUND ON REPAIR DOUBLER STA Y=636-655 BETWEEN PROJECTION OF LONG 29RT AND 30 AT MID CARGO COMPARTMENT. CORROSION ON REPAIR DOUBLER STA Y=636-655. DOUBLER REPAIR INSTALLED IAW DC9/MD80 SRM 51-30-02 AND 51-30-05 AND ERA 455102-14 REV OR
- [SDR DALA1216370919](https://openairdocs.org/sdr/DALA1216370919.md): Skin · damaged · Mar 16, 2012 · N919DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV LIGHTNING STRIKES WERE FOUND ON WINDOWS BELT FRAMES SKIN AT UPPER AFT CORNER STA 461 AND 1094 AT FUSELAGE SKIN. DOUBLER REPAIR INSTALLED IAW ERA501075-14 REV.
- [SDR DALA1216210919](https://openairdocs.org/sdr/DALA1216210919.md): Skin · corroded · Mar 15, 2012 · N919DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV CORROSION WAS FOUND ON EXTERNAL FUSELAGE SKIN FROM STA Y=731 TO Y=807 BETWEEN LONG 16RT AND 21RT. FUSELAGE SKIN WAS BLENDED OUT AND WITHIN LIMITS REF MD88 SRM 53-04 PARA 57.
- [SDR DALA1215760919](https://openairdocs.org/sdr/DALA1215760919.md): Beam · corroded · Mar 14, 2012 · N919DL · Doug MD88 · Fuselage Miscellaneous Structure
  > DURING HMV CORROSION WAS FOUND ON AFT CARGO COMPARTMENT LWR DOORJAMB BEAM LWR CAP BTW STA Y=1155 TO Y=1212. BLEND OUT BEAM AND LESS THAN 25% REMOVED SO BEAM WAS REPAIRED IAW MD88 SRM 53-05 FIG 123 SHEET 2 SECTION C-C.
- [SDR DALA1215950919](https://openairdocs.org/sdr/DALA1215950919.md): Skin · corroded · Mar 13, 2012 · N919DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV CORROSION WAS FOUND BELOW SETTLEMENT AREA OF RUBSTRIP FRON STA Y=726 TO Y=788 BETWEEN LONG 16RT TO 21RT. REF MD88 SRM 53-04D PARA 57 FOR REPAIR. BLENDED AREA WITHIN LIMITS IAW DC9/MD80 SRM 53-04 PAR 57.
- [SDR DALA1215940919](https://openairdocs.org/sdr/DALA1215940919.md): Skin · corroded · Mar 13, 2012 · N919DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV CORROSION WAS FOUND BELOW SETTLEMENT AREA OF RUBSTRIP FROM STA Y=799 TO Y=830 BETWEEN LONG 26LT TO 30 REF MD88 SRM 53-04D PARA 57 FOR REPAIR. BLENDED ARE WITHIN LIMITS IAW DC9/MD80 SRM 53-04 PAR 57.
- [SDR DALA1215910919](https://openairdocs.org/sdr/DALA1215910919.md): Skin · corroded · Mar 13, 2012 · N919DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV CORROSION WAS FOUND BELOW SETTLEMENT AREA OF RUB STRIP FROM STA Y=995 TO Y=1032 LONG 18RT REF MD88 SRM 53-04D PARA 57 FOR REPAIR. BLENDED AREA WITHIN LIMITS IAW SG 09530014 PAR 5A AND DC9/MD80 SRM 53-04 PAR 57.
- [SDR DALA1215900919](https://openairdocs.org/sdr/DALA1215900919.md): Skin · corroded · Mar 13, 2012 · N919DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV CORROSION WAS FOUND BELOW SETTLEMENT AREA OF RUB STRIP FROM STA Y=1060 TO Y=1136 BETWEEN LONG 26RT TO 30 REF MD88 SRM 53-04D PARA 57 FOR REPAIR. BLENDED AREA WITHIN LIMITS IAW DC9/MD80 SRM 53-04 PAR 57.
- [SDR DALA1215960919](https://openairdocs.org/sdr/DALA1215960919.md): Skin · corroded · Mar 13, 2012 · N919DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV CORROSION WAS FOUND ON EXTERNAL FUSELAGE SKIN FROM STA Y=1060 TO Y=1131 BETWEEN LONGS 18LT AND 30 REF MD88 SRM 53-04D PARA 57 FOR REPAIR. BLENDED AREA, WITHIN LIMITS IAW DC9/MD80 SRM 53-04 PAR 57.
- [SDR DALA1215890919](https://openairdocs.org/sdr/DALA1215890919.md): Skin · corroded · Mar 13, 2012 · N919DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV CORROSION WAS FOUND BELOW SETTLEMENT AREA OF RUB STRIP FROM STA Y=758 TO Y=830 BTW LONG 26RT TO 30RT REF MD88 SRM 53-04D PARA 57 FOR REPAIR. BLENDED AREA WITHIN LIMITS IAW SG 09530014 PAR 5A AND SRM 53-04 PAR 57.
- [SDR DALA1215920919](https://openairdocs.org/sdr/DALA1215920919.md): Skin · corroded · Mar 13, 2012 · N919DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV CORROSION WAS FOUND ON OUTER FUSELAGE SKIN AT RUBSTRIP AREA FROM STA Y=728 BTW LONGS 23RT TO 24RT AND STA Y=757-826 LONG 27RT TO 30 REF MD88 SRM 53-04D PARA 57 FOR REPAIR. BLENDED AREA WITHIN LIMITS, IAW SG 09530014 PAR 5A AND SRM 5-04 PAR 57.
- [SDR DALA1215930919](https://openairdocs.org/sdr/DALA1215930919.md): Skin · corroded · Mar 13, 2012 · N919DL · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV CORROSION WAS FOUND BELOW SETTLEMENT AREA OF RUBSTRIP FROM STA Y=1071 TO Y=1136 BETWEEN LONG 20LT TO 30LT REF MD88 SRM 53-04D PARA 57 FOR REPAIR.
- [SDR DALA1212550919](https://openairdocs.org/sdr/DALA1212550919.md): Tee Fitting · damaged · Mar 3, 2012 · N919DL · Doug MD88 · Fuselage Main, Bulkhead
  > DRILL MARKS WERE FOUND ON AFT PRESSURE BULKHEAD TEE LOWER SECTION STAY=1338 BTW PROJECTION OF LONGERON 29L-29R AT AFT CARGO COMPARTMENT REF MD 88 SRM 53-03 FIG 37 FOR REPAIR (NRC TO241646). NEW SECTION OF TEE AND REPAIR PARTS INSTALLED IAW DC9/MD88 SRM 53-03D
- [SDR DALA1218280919](https://openairdocs.org/sdr/DALA1218280919.md): Plate · corroded · Feb 28, 2012 · N919DL · Doug MD88 · Wing, Plate/Skin
  > DURING HMV CORROSION WAS FOUND BELOW SETTLEMENT RUB STRIP AREA ON FUEL ACCESS PLATE NBR 1335C UPPER LT WING WILL BE ATTENDED WITH AN ERA. CORR ON SETTLEMENT AREA FUEL ACCESS 1335C REPAIR ACCOMPLISHED IAW ERA 501079-14 REV ORIG.
- [SDR DALA1217930919](https://openairdocs.org/sdr/DALA1217930919.md): Skin · damaged · Feb 18, 2012 · N919DL · Doug MD88 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON LT WINDOW BELT FRAME SKIN AT AFT LWR EDGE STA Y=518 AT FUSELAGE SKIN. BLENDOUT REWORK ACCOMPLISHED IAW ERA 501075-14 REV ORIG.
- [SDR DALA1217910919](https://openairdocs.org/sdr/DALA1217910919.md): Skin · damaged · Feb 18, 2012 · N919DL · Doug MD88 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKES ON WINDOW BELT FRAME SKIN AT LWR AFT CORNER EDGE STA Y=479,888,742-745. LIGHTNING STRIKE TO WINDOW BELT STA 421, 479, 888, 742-745 BLENDOUT REWORK ACCOMPLISHED IAW ERA 501075-14 REV ORIG.
- [SDR DALA1217720919](https://openairdocs.org/sdr/DALA1217720919.md): Frame · damaged · Feb 18, 2012 · N919DL · Doug MD88 · Fuselage Main, Frame
  > DURING HMV LIGHTNING STRIKE WAS FOUND ON RT WINDOW BELT FRAME AT FWD UPPER CORNER BETWEEN STA Y=845 TO Y=864. LIGHTNING STRIKE RT WINDOW BELT FRAME. REPAIR PERFORMED IAW ERA 501072-14 REV ORIG.
- [SDR DALA1218290919](https://openairdocs.org/sdr/DALA1218290919.md): Spar · corroded · Feb 13, 2012 · N919DL · Doug MD88 · Horizontal Stabilizer, Spar/Rib
  > DURING HMV CORROSION WAS FOUND ON BARREL NUT HOLES NR 1 AND 4 FROM FWD SPAR TO REAR SPAR STA XH=27 RT HORIZONTAL STAB ERA WAS ISSUED FOR BARREL NUT HOLES CORROSION ON HORIZONTAL STAB BARREL NUT HOLES CORROSION REMOVED AND BUSHING REPAIR INSTALLED AT 1 AND 4 HO
- [SDR DALA1217920919](https://openairdocs.org/sdr/DALA1217920919.md): Skin · damaged · Feb 5, 2012 · N919DL · Doug MD88 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKES ON WINDOW BELT FRAME SKIN AT FWD LOWER CORNER STA Y=931,469. BLENDOUT REWORK ACCOMPLISHED IAW ERA 501075-14 REV ORIG.
- [SDR DALA1153940919](https://openairdocs.org/sdr/DALA1153940919.md): Battery · discharged · Sep 15, 2011 · N919DL · Doug MD88 · Emergency Lighting
  > DURING SERVICE CHECK MAINTENANCE FOUND OVERHEAD EMERGENCY LIGHTS INOP IN COCKPIT, R1, AND R2 DOORS. MAINTENANCE REPLACED BATTERIES PER AMM 33-53. OPERATION OF LIGHTS NOW CHECKS GOOD.
- [SDR DALA1148160919](https://openairdocs.org/sdr/DALA1148160919.md): Connector · damaged · Aug 13, 2011 · N919DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHTS FROM ROW 27 AFT INOPERATIVE. MAINTENANCE REPLACED LIGHT CONNECTOR DUE TO PULLED WIRE. OPERATION OF LIGHTS NOW CHECKS OK.
- [SDR DALA1144400919](https://openairdocs.org/sdr/DALA1144400919.md): Pin · pulled · Jul 23, 2011 · N919DL · Doug MD88 · Escape Slide
  > MAINTENANCE FOUND THE L1 DOOR SLIDE PIN PULLED WHILE PERFORMING MAINTENANCE ON SLIDE. MAINTENANCE CONTINUED WITH REMOVAL, REPLACEMENT, AND CHECK OF THE L1 DOOR SLIDE PER MAINTENANCE MANUAL.
- [SDR DALA1125310919](https://openairdocs.org/sdr/DALA1125310919.md): Power Supply · inoperative · Apr 8, 2011 · N919DL · Doug MD88 · Emergency Lighting
  > DURING SERVICE CHECK MAINTENANCE FOUND EMERGENCY PATHWAY LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD AND AFT SEATING POWER SUPPLIES AND ONE BATTERY PACK. OPERATION CHECKS GOOD AND THE AIRCRAFT OKAY FOR SERVICE.
- [SDR DALA1167760919](https://openairdocs.org/sdr/DALA1167760919.md): Structure · damaged · Feb 14, 2011 · N919DL · Doug MD88 · Fuselage Miscellaneous Structure
  > LIGHTNING STRIKE AT FS 506 LONGERON 1. REPAIRED IAW ERA 32223-14.
- [SDR DALA1106530919](https://openairdocs.org/sdr/DALA1106530919.md): Structure · damaged · Jan 27, 2011 · N919DL · Doug MD88 · Vertical Stabilizer
  > LOWER FIXED L/E NUMEROUS HOLES WORN. REPAIRED IAW SRM 55-03D, FIG 30.
- [SDR DALA1050180919](https://openairdocs.org/sdr/DALA1050180919.md): Light · miswired · Nov 28, 2010 · N919DL · Doug MD88 · Emergency Lighting
  > CREW NOTED EMERGENCY LIGHTS IN OVERHEAD COCKPIT PANEL REMAIN ON WITH SWITCH IN OFF POSITION. MX FOUND WHEN THE L1 ENTRY LIGHT SWITCH IS TURNED OFF AT PANEL, EMERGENCY LIGHTS WILL EXTINGUISH. ALSO FOUND WRONG BULBS INSTALLED IN ALL 3 POSITIONS. VERIFIED WIRES
- [SDR DALA1026630919](https://openairdocs.org/sdr/DALA1026630919.md): Light · inoperative · Oct 9, 2010 · N919DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK MX FOUND EMERGENCY LIGHTS AT SEAT 23D INOPERATIVE. MX REPLACED THE LIGHT ASSY AT 23D. OPERATION OF LIGHTS NOW CHECK OK.

Next page: https://openairdocs.org/deregistered/N919DL-2019-01-14/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 = 'N919DL' AND deregistration_id = 'N919DL-2019-01-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N919DL-2019-01-14/reports

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