# Service difficulty reports: N919DE, cancelled Aug 22, 2019

A list on [N919DE, cancelled Aug 22, 2019](https://openairdocs.org/deregistered/N919DE-2019-08-22.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 3 · 140 reports

- [SDR DALA2018061904117](https://openairdocs.org/sdr/DALA2018061904117.md): Door · unsecure · Jun 19, 2018 · N919DE · Doug MD88 · Service Doors
  > CONDITIONED AIR GROUND CONNECT DOOR, FORWARD CONDITIONED AIR DOOR FELL OFF. DEFER FWD AC DOOR PER CDL 53-30-04A. DISP GRANTED. PLAC INSTALLED. (IN FWD CLOSET).
- [SDR DALA2018022601127](https://openairdocs.org/sdr/DALA2018022601127.md): Battery Pack · discharged · Feb 24, 2018 · N919DE · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTS BETWEEN ROW 22-25 CEILING INOP. REPL BATTERY PACK PER AMM 33-53. OPS CHECK GOOD.
- [SDR DALA2018021500930](https://openairdocs.org/sdr/DALA2018021500930.md): Battery · discharged · Feb 15, 2018 · N919DE · Doug MD88 · Emergency Lighting
  > FWD GALLEY EMERGENCY LIGHTS INOP. R&R BATTERIES IN FORWARD GALLEY LOC B5-23 PER AMM 33-53 OP CKS GOOD OK FOR SVC.
- [SDR DALA2017092107002](https://openairdocs.org/sdr/DALA2017092107002.md): Tab · damaged · Sep 12, 2017 · N919DE · Doug MD88 · Rudder, Tab Structure
  > COMPOSITE EXPOSED ON RUDDER TAB. REMOVED THE TAB IAW AMDS 2720-4438 AND INSTALLED A NEW TAB IAW AMDS 2720-4321.
- [SDR DALA2017040502753](https://openairdocs.org/sdr/DALA2017040502753.md): Battery Pack · inoperative · Apr 4, 2017 · N919DE · Doug MD88 · Emergency Lighting
  > FOUND OVERWING EXIT LIGHTS INOPERATIVE. REPLACED THE BATTERIES IAW AMM 33-53, LIGHTS CHECKED GOOD.
- [SDR DALA2017020200878](https://openairdocs.org/sdr/DALA2017020200878.md): Fan · failed · Feb 1, 2017 · N919DE · Doug MD88 · Air Distribution Fan
  > FLT LEVEL 340, FLIGHT ATTENDANT REPORTED ELECTRICAL SMELL WITH A HAZE IN THE CABIN. AFTER THE SMELL REACHED THE COCKPIT, ELECTRICAL, WE DIVERTED TO CAE. FOUND RECIRC FAN BAD. FWD TO MEL 21-00-43 AND PLA. C/W (M) PROCEDURES.
- [SDR DALA2016110708340](https://openairdocs.org/sdr/DALA2016110708340.md): Wire · chafed · Nov 4, 2016 · N919DE · Doug MD88 · Light System Wiring
  > AFT EMERGENCY LIGHT INOPERATIVE. FOUND CHAFED WIRE IN SERVICE LOOP. REMOVED THE PORTION OF WIRE AND SPLICED IAW AMM 20-50. LIGHTS OPERATE NORMAL.
- [SDR DALA2016102407529](https://openairdocs.org/sdr/DALA2016102407529.md): Battery Pack · discharged · Oct 24, 2016 · N919DE · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHT INOP FROM ROW 31 TO TAIL. REPLACED BATTERY PACK. OPS CKS GOOD.
- [SDR DALA2016100307009](https://openairdocs.org/sdr/DALA2016100307009.md): Fuse · blown · Oct 1, 2016 · N919DE · Doug MD88 · Emergency Lighting
  > AFT SECTION EMERG LIGHTS INOP. REPLACED FUSE IN BATTERY PACK. OPS CK GOOD. REF WDM 33-51.
- [SDR DALA2016092606837](https://openairdocs.org/sdr/DALA2016092606837.md): Fuse · blown · Sep 24, 2016 · N919DE · Doug MD88 · Emergency Lighting
  > FOUND DURING SERVICE CHECK, AFT CABIN AND TAIL COMPARTMENT EMERGENCY LIGHTS WILL NOT TEST. REPLACED BLOWN FUSE AT POWER SUPPLY B5-212, POSITION 9, IAW WDM 33-51-14. CHECKS OK.
- [SDR DALA2015092805843](https://openairdocs.org/sdr/DALA2015092805843.md): Battery Pack · inoperative · Sep 27, 2015 · N919DE · Doug MD88 · Emergency Lighting
  > MAINTENANCE FOUND THE COCKPIT EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACKS WERE REPLACED.
- [SDR DALA2015083105340](https://openairdocs.org/sdr/DALA2015083105340.md): Door · no test · Aug 30, 2015 · N919DE · Doug MD88 · Emergency Exits
  > LEFT AFT OVERWING EMERGENCY EXIT DOOR FAILED EXTERIOR DOOR HANDLE RELEASE TEST IAW W/C 5200-2643. DOOR RELEASES AS SOON AS EXTERIOR HANDLE TAB PRESSED WHILE HANDLE WAS IN THE STOWED POSITION. REPLACED AND RIGGED THE DOOR IAW AMM 52-21-00.
- [SDR DALA2015083105339](https://openairdocs.org/sdr/DALA2015083105339.md): Container · cracked · Aug 30, 2015 · N919DE · Doug MD88 · Escape Slide
  > DURING INSPECTION, MAINTENANCE FOUND TAILCONE EVACUATION SLIDE BASE PLATE CRACKED AT COVER ATTACH POINTS. THE CONTAINER ASSY WAS REPLACED IAW AMDS WORKCARD 2561-4001.
- [SDR DALA2015082705259](https://openairdocs.org/sdr/DALA2015082705259.md): Frame · cracked · Aug 26, 2015 · N919DE · Doug MD88 · Fuselage Main, Frame
  > AFT FUESLAGE TAIL CONE AREA FRAME BS 1463, S25R FOUND A THREE INCH CRACK ON FRAME. REPAIRED IAW SRM 53-03D, FIG 38A.
- [SDR DALA2016041402903](https://openairdocs.org/sdr/DALA2016041402903.md): Skin · damaged · Mar 21, 2015 · N919DE · Doug MD88 · Wing, Plate/Skin
  > REMOVED RT WINGTIP ASSY IAW AMM 57-20. REPLACED RT WING TIP ASSY IAW AMM 57-20-02. OPS CHECKED GOOD. COMPLIED WITH ER/A 534223-14, REV ORIGINAL.
- [SDR DALA2015030902031](https://openairdocs.org/sdr/DALA2015030902031.md): Pin · seized · Mar 7, 2015 · N919DE · Doug MD88 · Aerodynamic Fairings
  > DURING TAILCONE RELEASE SYS FUNCTIONAL CHECK, MAINTENANCE FOUND THE INTERIOR TAILCONE RELEASE CABLE RELEASE PIN SEIZED. MAINTENANCE R & R THE RELEASE CABLE RELEASE PIN. OPS CHECKED OK. LP1853095.
- [SDR DALA2015030902030](https://openairdocs.org/sdr/DALA2015030902030.md): Cable · worn · Mar 7, 2015 · N919DE · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE FOUND KEVLAR CABLE ASSY WORN FOR TAILCONE ASSY. MAINTENANCE REPLACED THE KEVLAR CABLE ASSY, CHECKS OK. LP1853081.
- [SDR DALA2014092205208](https://openairdocs.org/sdr/DALA2014092205208.md): Battery Pack · inoperative · Sep 20, 2014 · N919DE · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY OVERHEAD LIGHTING AT THE OVERWING EXIT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-104 AND THE LIGHTS RETURNED TO AN OPERATIONAL STATE.
- [SDR DALA14030359019](https://openairdocs.org/sdr/DALA14030359019.md): Cable · detached · May 15, 2014 · N919DE · Doug MD88 · Emergency Equipment
  > THE CREW DISCOVERED THE 1L DOOR GIRT BAR WIRE CABLE WAS NOT ATTACHED TO THE GIRT BAR. MAINTENANCE REINSTALLED THE GIRT BAR CABLE AND THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR DALA13044299019](https://openairdocs.org/sdr/DALA13044299019.md): Skin · damaged · Sep 12, 2013 · N919DE · Doug MD88 · Fuselage Main, Plate/Skin
  > WINDOW BELT FRAME FOUND CRACKED AT PREVIOUS LIGHTNING STRIKE BLEND. BS 541 TO 560 AREA C. NDT CONFIRMED 06-10-01-001. WORK ACCOMPLISHED ON PRI 518567-14. REPAIR COMPLETED.
- [SDR DALA13044279019](https://openairdocs.org/sdr/DALA13044279019.md): Skin · cracked · Sep 11, 2013 · N919DE · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED MX, A.7500 INCH SKIN CRACK WAS FOUND AT BS 1310, APPROXIMATELY 2.5 INCHES ABOVE THE EDGE OF THE SKIN PANEL NEAR LONGERON 7R. REPAIRED IAW ER/A 518476-14, SECT 1.
- [SDR DALA13034489019](https://openairdocs.org/sdr/DALA13034489019.md): Battery Pack · inoperative · Jul 11, 2013 · N919DE · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT DOOR L1 AND THE FIRST CLASS CABIN WERE INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA13024039019](https://openairdocs.org/sdr/DALA13024039019.md): Pin · loose · May 21, 2013 · N919DE · Doug MD88 · Escape Slide
  > DURING ROUTINE INSPECTION, THE INSPECTOR NOTED THAT THE NR 1 LEFT DOOR SLIDE PACKING PIN WAS LOOSE. THE SLIDE WAS REPLACED IAW AMM 25-62 AND THE REQUIRED INSPECTION WAS COMPLETED.
- [SDR DALA12012279019](https://openairdocs.org/sdr/DALA12012279019.md): Cabin Pressure · multiple fail · Nov 4, 2012 · N919DE · Doug MD88 · Cabin Pressure Control System
  > CREW REPORTED THAT THE ACFT COMPLETELY LOSS PRESSURIZATION NEAR THE TOP OF DESCENT. PASSENGER OXYGEN MASKS DID DEPLOYED AND AN EMERGENCY DESCENT TO 10K WAS DECLARED AND EXECUTED. MX FOUND CABIN PRESSURE CONTROLLER NR 2, LT PACK FLOW CONTROL VALVE, LT TRIM VAL
- [SDR DALA12011019019](https://openairdocs.org/sdr/DALA12011019019.md): Battery Pack · inoperative · Oct 23, 2012 · N919DE · Doug MD88 · Emergency Lighting
  > DURING SERVICE CHECK, MX FOUND EMERGENCY PATHWAY LIGHTS INOPERATIVE FROM ROW 1 THROUGH 11 AND LT AND RT FORWARD ENTRY DOOR EXIT SIGNS OUT. REMOVED AND REINSTALLED BATTERY PACK. ALL LIGHTS OPERATIONS CHECKED GOOD.
- [SDR DALA12009699019](https://openairdocs.org/sdr/DALA12009699019.md): Lanyard · loose · Oct 9, 2012 · N919DE · Doug MD88 · Emergency Equipment
  > PILOT FOUND CABLE HANGING FROM FORWAD FO SIDE GALLEY DOOR. MX SECURED R1 DOOR GIRT BAR LANYARD. ACFT OK FOR SERVICE.
- [SDR DALA1242629019](https://openairdocs.org/sdr/DALA1242629019.md): Skin · damaged · Jul 22, 2012 · N919DE · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV, LIGHTNING STRIKES WERE FOUND ON FWD AND AFT EDGES OF LT WINDOW BELT FRAME BS 617-636. WINDOW BELT FRAME WAS BLENDED OUT AFT EDGES AND WITHIN LIMITS PER SRM 53-05 FIG 111. THE FWD EDGE WAS REPAIRED IAW ERA 504342-14 REV ORIG.
- [SDR DALA1242619019](https://openairdocs.org/sdr/DALA1242619019.md): Skin · damaged · Jul 22, 2012 · N919DE · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV, LIGHTNING STRIKES WERE FOUND ON AFT UPPER CORNER OF LT WINDOW BELT FRAME BS 617-636. WINDOW BELT FRAME AFT UPPER CORNER LOWER OUT OF CRITICAL ZONE 1 IS WITHIN LIMIT PER SRM 53-05 FIG 111. THE AFT UPPER CORNER UPPER BLENDED OUT AND REPAIRED IAW ER
- [SDR DALA1243019019](https://openairdocs.org/sdr/DALA1243019019.md): Skin · dented · Jul 21, 2012 · N919DE · Doug MD88 · Fuselage Main, Plate/Skin
  > FOUND DENT TO FUSELAGE, APPROXIMATELY 2 FEET AFT OF L1 DOOR COMPLIED WITH PERMANENT REPAIR TO FUSELAGE DENT PER SRM 53-04-5.
- [SDR DALA1242489019](https://openairdocs.org/sdr/DALA1242489019.md): Skin · damaged · Jul 20, 2012 · N919DE · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV, LIGHTNING STRIKE WAS FOUND ON WINDOW BELT FWD EDGE BS 788-807. WINDOW BELT WAS BLENDED OUT AND REPAIR DOUBLER INSTALLED IAW ERA 504370-14 REV ORIG.
- [SDR DALA1242479019](https://openairdocs.org/sdr/DALA1242479019.md): Skin · damaged · Jul 20, 2012 · N919DE · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV, LIGHTNING STRIKE WAS FOUND ON LT WINDOW BELT FWD EDGE BS 826-845. WINDOW BELT WAS BLENDED OUT AND REPAIR DOUBLER INSTALLED IAW ERA 504370-14 REV ORIG.
- [SDR DALA1242469019](https://openairdocs.org/sdr/DALA1242469019.md): Skin · damaged · Jul 20, 2012 · N919DE · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV, LIGHTNING STRIKE WAS FOUND ON WINDOW BELT FRAME AFT LOWER CORNER BTW BS 693-674 RT SIDE. WINDOW BELT FRAME WAS BLENDED OUT AND REPAIR DOUBLER INSTALLED IAW ERA 504353-14 REV ORIG.
- [SDR DALA1242459019](https://openairdocs.org/sdr/DALA1242459019.md): Beam · corroded · Jul 20, 2012 · N919DE · Doug MD88 · Fuselage Main, Structure
  > DURING HMV, CORROSION WAS FOUND ON MID CARGO COMPARTMENT LOWER BEAM BS 636-693 (C2). BEAM WAS BLENDED OUT AND BS 655 AND 674 WAS OUT OF LIMITS. THE AREA WAS CUT OUT FILLER AND Z REPAIR INSTALLED IAW SRM 53-05 FIG 123.
- [SDR DALA1242439019](https://openairdocs.org/sdr/DALA1242439019.md): Skin · damaged · Jul 20, 2012 · N919DE · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV, LIGHTNING STRIKES WERE FOUND ON LT WINDOW BELT FRAME FWD UPPER CORNER. ALSO, AFT UPPER CORNER BS 655-674. WINDOW BELT FRAME WAS BLENDED OUT AND REPAIR DOUBLER INSTALLED IAW ERA 504352-14 REV ORIG.
- [SDR DALA1242429019](https://openairdocs.org/sdr/DALA1242429019.md): Skin · damaged · Jul 20, 2012 · N919DE · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV, LIGHTNING STRIKE WAS FOUND ON LT WINDOW BELT FRAME AFT LOWER CORNER BS 807-826. WINDOW BELT FRAME WAS BLENDED OUT AND REPAIR DOUBLER WAS INSTALLED BS 788-845 IAW ERA 504370-14 REV ORIG.
- [SDR DALA1242419019](https://openairdocs.org/sdr/DALA1242419019.md): Skin · damaged · Jul 20, 2012 · N919DE · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV, LIGHTNING STRIKES WERE FOUND ON LT WINDOW BELT FRAME LOWER AFT CORNER. ALSO LOWER FORWARD CORNER BS 541-560 WINDOW BELT FRAME WAS BLENDED OUT IAW ERA 504357-14 REV ORIG.
- [SDR DALA1242409019](https://openairdocs.org/sdr/DALA1242409019.md): Skin · damaged · Jul 20, 2012 · N919DE · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV, LIGHTNING STRIKES WERE FOUND ON WINDOW BELT FRAME ON FWD LOWER CORNER. ALSO ON AFT UPPER CORNER BTW BS 1193 AND 1212. WINDOW BELT FRAME WAS BLENDED OUT IAW ERA 504357-14 REV ORIG.
- [SDR DALA1242399019](https://openairdocs.org/sdr/DALA1242399019.md): Skin · corroded · Jul 20, 2012 · N919DE · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV, CORROSION WAS FOUND ON FUSELAGE SKIN IN BS 782 BETWEEN LONGERON 28R-29R. FUSELAGE SKIN WAS BLENDED OUT AND REPAIR DOUBLER INSTALLED IAW 53-04 PARA 57.
- [SDR DALA1242389019](https://openairdocs.org/sdr/DALA1242389019.md): Skin · corroded · Jul 20, 2012 · N919DE · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV, CORROSION WAS FOUND ON FUSELAGE SKIN BS 803 AND LONGERON 29R. FUSELAGE SKIN WAS BLENDED OUT AND DOUBLER REPAIR INSTALLED IAW MD88 SRM 53-04 PARA 57.
- [SDR DALA1242319019](https://openairdocs.org/sdr/DALA1242319019.md): Angle · damaged · Jul 19, 2012 · N919DE · Doug MD88 · Fuselage Miscellaneous Structure
  > DURING HMV, TOOLING MARKS WERE FOUND ON PRESSURE DOME LOWER TEE ANGLE AT BS 1338 BETWEEN LONGERON 26 LT AND 26 RT. REMOVED DAMAGE TEE ANGLE BETWEEN LONGERON 25 LT AND 25 RT AND INSTALLED REPAIR SPLICES TEE ANGLE IAW SRM 53-03 FIG 37.
- [SDR DALA1242309019](https://openairdocs.org/sdr/DALA1242309019.md): Structure · corroded · Jul 19, 2012 · N919DE · Doug MD88 · Fuselage Main, Structure
  > DURING HMV, CORROSION WAS FOUND ON REPAIR SPLICE OF LONGERON 28 LT AND 29 LT BTW STA Y=1250-1271 AT AFT CARGO COMPARTMENT LONGERON 28L WAS ATTENDED ON NRC 254176 AND REPAIR SPLICE OF LONGERON 29LH BTW Y=1250-1271 WAS REPLACED IAW SRM 53- 02 FIG 18.
- [SDR DALA1242299019](https://openairdocs.org/sdr/DALA1242299019.md): Skin · cracked · Jul 19, 2012 · N919DE · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV, CRACKED FUSELAGE SKIN WAS FOUND BTW BS 1497 - 1501 LONGERONS 17-18L. DAMAGE AREA WAS CUT OUT AND SHIM DOUBLER REPAIR INSTALLED IAW SRM 53-04-3 FIG 2.
- [SDR DALA1242089019](https://openairdocs.org/sdr/DALA1242089019.md): Longeron · corroded · Jul 18, 2012 · N919DE · Doug MD88 · Fuselage Main, Longeron/Stringer
  > DURING HMV, CORROSION WAS FOUND ON LONGERON 24 LT STA Y=1290, LONGERON WAS REMOVED FROM BS 1275-1328. REPAIR LONGERONS AND SPLICES INSTALLED IAW SRM 53-02 FIG 18.
- [SDR DALA1242079019](https://openairdocs.org/sdr/DALA1242079019.md): Longeron · corroded · Jul 18, 2012 · N919DE · Doug MD88 · Fuselage Main, Longeron/Stringer
  > DURING HMV, CORROSION WAS FOUND ON LONGERON 27 LT FROM BS 1257-1330 AND LONGERON 28 LT. DAMAGE SECTION WAS REMOVED BS 1204-1330 AND REPAIRED IAW SRM 53-02 FIG 18.
- [SDR DALA1242069019](https://openairdocs.org/sdr/DALA1242069019.md): Skin · corroded · Jul 18, 2012 · N919DE · Doug MD88 · Fuselage Main, Plate/Skin
  > DURING HMV, CORROSION WAS FOUND ON FUSELAGE SKIN BELOW WING TO FUSELAGE FILLET PANEL RUBSTRIPS ON BS 727-826 BETWEEN LONGERONS 16-30L AND BS 826-864 BETWEEN LONGERONS 17-19L. BLENDED FUSELAGE SKIN AND WITHIN LIMITS TO LEAVE AS IS IAW SRM 53-04 PARA 57.
- [SDR DALA1242059019](https://openairdocs.org/sdr/DALA1242059019.md): Longeron · corroded · Jul 18, 2012 · N919DE · Doug MD88 · Fuselage Main, Longeron/Stringer
  > DURING HMV, CORROSION WAS FOUND ON LONGERON 22 LT BTW BS 1277 TO 1335. DAMAGE LONGERON WAS REMOVED AND REPAIR LONGERON AND SPLICE INSTALLED IAW SRM 53-02 FIG 18.
- [SDR DALA1242049019](https://openairdocs.org/sdr/DALA1242049019.md): Longeron · corroded · Jul 18, 2012 · N919DE · Doug MD88 · Fuselage Main, Longeron/Stringer
  > DURING HMV, CORROSION WAS FOUND ON LONGERON 23L IN BS 1287 AT AFT CARGO COMPARTMENT. DAMAGE LONGERON WAS REMOVED7 AND REPAIR SPLICE INSTALLED IAW SRM 53-02 FIG 18.
- [SDR DALA1240879019](https://openairdocs.org/sdr/DALA1240879019.md): Longeron · damaged · Jul 9, 2012 · N919DE · Doug MD88 · Fuselage Main, Longeron/Stringer
  > DURING HMV, WEAR WAS FOUND ON STRAP AND LONGERON 8 RT AT BS 1401-1418. DAMAGED LONGERON 8 RT STA Y=1406-1429 AND SPLICE WAS REMOVED AND REPAIRED. PARTS INSTALLED IAW SRM 53-02 FIG 18.
- [SDR DALA1240489019](https://openairdocs.org/sdr/DALA1240489019.md): Skin · dented · Jul 8, 2012 · N919DE · Doug MD88 · Fuselage Main, Plate/Skin
  > DENT ON FUSELAGE AFT OF L1 DOOR APPROXIMATELY 2 FT AFT OF DOOR AT STA Y=239. REPAIRED FUSELAGE SKIN IAW WITH SRM 53-04-5 AND ERA 483596-14 REV ORIG.
- [SDR DALA1159329019](https://openairdocs.org/sdr/DALA1159329019.md): Floor Support · corroded · Oct 21, 2011 · N919DE · Doug MD88 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ANGLE CORRODED RBL 44 AT STA 148 AND 160. INSTALLED FLOOR SUPPORT ANGLE AT RBL 44 AT STA 148 - 160 IAW DC9/MD80 SRM 51-10-4 PG 1 MD80 SRM 51-30-5 PG 3 TORQUE WRENCH NR 11-750 DUE 11-19-11.

Next page: https://openairdocs.org/deregistered/N919DE-2019-08-22/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 = 'N919DE' AND deregistration_id = 'N919DE-2019-08-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N919DE-2019-08-22/reports

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