# Service difficulty reports: N945DL, cancelled Nov 9, 2020

A list on [N945DL, cancelled Nov 9, 2020](https://openairdocs.org/deregistered/N945DL-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 4 · 151 reports

- [SDR DALA2018081305013](https://openairdocs.org/sdr/DALA2018081305013.md): Battery Pack · inoperative · Aug 13, 2018 · N945DL · Doug MD88 · Emergency Lighting
  > RT OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERIES. OPS CHECKED GOOD.
- [SDR DALA2018080104804](https://openairdocs.org/sdr/DALA2018080104804.md): Light · inoperative · Jul 31, 2018 · N945DL · Doug MD88 · Emergency Lighting
  > SEAT EMER LIGHT INOP 20DE. R&R EMER LIGHT AS PASS SEAT 20 DE PER AMM 33-53 OPS CK GOOD.
- [SDR DALA2018062304169](https://openairdocs.org/sdr/DALA2018062304169.md): Csd · damaged · Jun 19, 2018 · N945DL · Doug MD88 · Alternator-Generator Drive
  > LT CSD OIL PRES LOW AND LT GEN OFF LIGHTS ILLUMINATED - FOLLOWED QRH - DISCONNECTED CSD. ACCORDING TO MCC NOTIFICATION, AN EMERGENCY WAS DECLARED. REMOVED CSD & GEN. FOUND CSD SHAFT TO THE GEAR BOX SHEERED. REPLACED CSD & REINSTALLED GEN IAW AMM 24-10. SYSTE
- [SDR DALA2017100907379](https://openairdocs.org/sdr/DALA2017100907379.md): Battery Pack · inoperative · Oct 7, 2017 · N945DL · Doug MD88 · Emergency Lighting
  > DURING A LINE CHECK, NOTED SIGNS ABOVE FWD EMERERGENCY EXIT DOORS INOPERATIVE. BATTERIES WERE REPLACED AND OPERATION WAS NORMAL.
- [SDR DALA2017100207233](https://openairdocs.org/sdr/DALA2017100207233.md): Wire · broken · Sep 29, 2017 · N945DL · Doug MD88 · Light System Wiring
  > SEAT 18D EMERGENCY LIGHT INOPERATIVE. FOUND A BROKEN WIRE. PINNED THE CONNECTOR PLUG. OP CHECKED IAW 33-50. (LP3478308)
- [SDR DALA2017080205864](https://openairdocs.org/sdr/DALA2017080205864.md): Battery Pack · inoperative · Aug 2, 2017 · N945DL · Doug MD88 · Emergency Lighting
  > CEILING EMERGENCY LIGHTS INOPERATIVE ROWS 1-4, AND 17-20. INSTALLED BATTERIES IN THE B5-100 & B5-102 POWER SUPPLIES IAW AMM 33-53. OPS CHECKED GOOD.
- [SDR DALA2017031602117](https://openairdocs.org/sdr/DALA2017031602117.md): Wire · broken · Mar 15, 2017 · N945DL · Doug MD88 · Light System Wiring
  > SEAT 29 DE, SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. FOUND A WIRE BROKEN AT CONTACT PIN IN CONNECTOR AT SEAT FRAME. TERMINATED THE WIRE IAW SWPM 20-90-03. CHECKED GOOD.
- [SDR DALA2017011200272](https://openairdocs.org/sdr/DALA2017011200272.md): Structure · dented · Jan 11, 2017 · N945DL · Doug MD88 · Wing, Plate/Skin
  > DENT ON L/E VORTILON YW=85, XRS=160. REPAIRED IAW RM 57-09D PAR. 33 AND ERA 401563-14 REV. ORIGINAL.
- [SDR DALA2016122910132](https://openairdocs.org/sdr/DALA2016122910132.md): Diode · damaged · Dec 28, 2016 · N945DL · Doug MD88 · DC Generating System
  > STRONG BURNING ODOR IN COCKPIT IMMEDIATELY AFTER TAKE OFF. NO SMOKE OR VISIBLE FUMES. NO ODORS IN CABIN AREA. ODOR DISSIPATED AFTER 3 OR 4 MINUTES. NO ABNORMAL COCKPIT INDICATIONS. FOUND TRANSFORMER RECITIFER DIODES DISCOLORED. REPLACED BOTH DIODES IAW AM
- [SDR DALA2016101907352](https://openairdocs.org/sdr/DALA2016101907352.md): Packing · damaged · Oct 18, 2016 · N945DL · Doug MD88 · Escape Slide
  > DAMAGE PACKING OF TAIL CONE EVACUATION SLIDE. THE SLIDE WAS REPLACED AND WAS INSTALLED IAW CARD 5350-4644, JOB 001-0195.
- [SDR DALA2016101807338](https://openairdocs.org/sdr/DALA2016101807338.md): Frame · cracked · Oct 17, 2016 · N945DL · Doug MD88 · Fuselage Main, Frame
  > CRACK ON WEB AT STA Y=1463 CANT BTW 10HRS AND 11HRS POSITION IN AFT ACCESSORY COMPARTMENT. DAMAGE AREA WAS REPAIRED PER SRM 53-03D FIG 38A, 51-30-2 & 51-30-5, 51-10-3 PAR 21 AND 14.
- [SDR DALA2016101407239](https://openairdocs.org/sdr/DALA2016101407239.md): Pan · cracked · Oct 13, 2016 · N945DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACK ON INTERNAL PAN BS 162 BTWEEN UPPER EDGE AND BEAM 1 AT MAIN ENTRANCE DOOR. HFEC INSPECTION WAS ACCOMPLISHED ON INTERNAL PAN. ONE CRACK OF 2.340 WAS FOUND. STOP DRILL WAS PERFORMED, HFEC WAS ACCOMPLISHED AFTER STOP DRILL AND NO CRACKS WERE FOUND. INTERNAL
- [SDR DALA2016101307232](https://openairdocs.org/sdr/DALA2016101307232.md): Angle · cracked · Oct 12, 2016 · N945DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE BS 195 BELOW OF BEAM 1 AT FWD SERVICE DOOR. THE ANGLE WAS REPLACED IAW SRM 51-30-5 AND DWG 9911579 REV L.
- [SDR DALA2016101207181](https://openairdocs.org/sdr/DALA2016101207181.md): Longeron · cracked · Oct 11, 2016 · N945DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERON 3L BS 160. THE LONGERON WAS REPLACED IAW SRM 53-02 FIG.18.
- [SDR DALA2016101207180](https://openairdocs.org/sdr/DALA2016101207180.md): Beam · cracked · Oct 11, 2016 · N945DL · Doug MD88 · Passenger/Crew Doors
  > CRACK ON BEAM NR 6 BS 177 AT MAIN ENTRANCE DOOR. THE BEAM WAS REPAIRED IAW ERA 413018-14 MA REV ORIG.
- [SDR DALA2016101207179](https://openairdocs.org/sdr/DALA2016101207179.md): Web · cracked · Oct 11, 2016 · N945DL · Doug MD88 · Passenger/Crew Doors
  > CRACK ON INTERNAL WEB BS 192 OF THE L1 DOOR. THE WEB WAS REPAIRED IAW SRM 52-01 FIGURE 4.
- [SDR DALA2016101107149](https://openairdocs.org/sdr/DALA2016101107149.md): Spacer · corroded · Oct 10, 2016 · N945DL · Doug MD88 · Fuselage Main, Structure
  > CORROSION ON SPACER OF LOWER BEAM BS 642 AT MID CARGO COMPARTMENT DOOR FRAME. THE SPACER WAS REPLACED IAW 53-05 FIG 123.
- [SDR DALA2016101107148](https://openairdocs.org/sdr/DALA2016101107148.md): Beam · cracked · Oct 10, 2016 · N945DL · Doug MD88 · Passenger/Crew Doors
  > CRACK ON BEAM NR 8 (AFT EDGE) AT MAIN ENTRANCE DOOR. BEAM WAS REPAIRED IAW SRM 52-05 FIG. 95 SHEET 3.
- [SDR DALA2016101107147](https://openairdocs.org/sdr/DALA2016101107147.md): Spacer · corroded · Oct 10, 2016 · N945DL · Doug MD88 · Fuselage Main, Structure
  > CORROSION ON SPACER AT AFT CARGO BAY LOWER DOOR FRAME. SPACER WAS REPLACED IAW SRM 53-05 FIG 123 SHEET 5 AND 51-30-5, 51-30-4.
- [SDR DALA2016062805026](https://openairdocs.org/sdr/DALA2016062805026.md): Strut · defective · Jun 28, 2016 · N945DL · Doug MD88 · Nose/Tail Landing Gear Strut/Axle
  > NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO DEPARTURE. MAINTENANCE FOUND THE NOSE STRUT COMPRESSED COMPLETELY. THE CREW INDICATED THE RIDE WAS HARSH DURING TAXI OUT. UPON DISASSEMBLY, THE SHOCK STRUT METERING PIN WAS DETERMINED TO BE BYPASSING.
- [SDR DALA2016062104805](https://openairdocs.org/sdr/DALA2016062104805.md): Battery Pack · discharged · Jun 21, 2016 · N945DL · Doug MD88 · Emergency Lighting
  > SEAT 2B AND 34E OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTER PACKS PER AMM 33-53-00.
- [SDR DALA2016040502649](https://openairdocs.org/sdr/DALA2016040502649.md): Battery Pack · inoperative · Apr 1, 2016 · N945DL · Doug MD88 · Emergency Lighting
  > FIRST CLASS CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-100.
- [SDR DALA2016032802379](https://openairdocs.org/sdr/DALA2016032802379.md): Pin · gouged · Mar 26, 2016 · N945DL · Doug MD88 · Aerodynamic Fairings
  > THE TAILCONE RELEASE OPS CHECK FAILED. MSP MAINTENANCE FOUND A T-PIN GOUGED AND REPLACED IT.
- [SDR DALA2016032802378](https://openairdocs.org/sdr/DALA2016032802378.md): Pin · gouged · Mar 26, 2016 · N945DL · Doug MD88 · Aerodynamic Fairings
  > ON SHIP 945, MSP MAINTENANCE FOUND THE UPPER LT TAIL CONE RELEASE LOCK PIN GOUGED. THE LOCK PIN WAS REPLACED BY MSP MAINTENANCE.
- [SDR DALA2015111907076](https://openairdocs.org/sdr/DALA2015111907076.md): Battery Pack · inoperative · Nov 18, 2015 · N945DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN ROWS 31 TO THE BACK OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.
- [SDR DALA2015111907075](https://openairdocs.org/sdr/DALA2015111907075.md): Fuse · inoperative · Nov 18, 2015 · N945DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN ROWS 31 THROUGH TO THE TAIL COMPARTMENT WERE INOPERATIVE. MAINTENANCE REPLACED THE FAILED FUSE AT THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.
- [SDR DALA2015111707030](https://openairdocs.org/sdr/DALA2015111707030.md): Power Supply · inoperative · Nov 14, 2015 · N945DL · Doug MD88 · Emergency Lighting
  > MAINTENANCE FOUND THE EMERGENCY LIGHTS FROM SEAT ROWS 31 AND AFT TO BE INOPERATIVE. THE B5-212 POWER SUPPLY WAS REPLACED. THE LIGHTS TESTED GOOD.
- [SDR DALA2015111006847](https://openairdocs.org/sdr/DALA2015111006847.md): Wire · chafed · Nov 9, 2015 · N945DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS FROM ROWS 30 AND AFT IN THE CABIN WERE INOPERATIVE. MAINTENANCE FOUND A WIRE CHAFING IN A SEAT TRACK, REPAIRED THE WIRE INSULATION, AND REPLACED THE BLOWN FUSE.
- [SDR DALA2015102006259](https://openairdocs.org/sdr/DALA2015102006259.md): Fuse · failed · Oct 20, 2015 · N945DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT ALL OF THE EMERGENCY LIGHTING FROM ROW 31 AND AFT IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE FAILED FUSE AT THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA2015101206073](https://openairdocs.org/sdr/DALA2015101206073.md): Power Supply · inoperative · Oct 10, 2015 · N945DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN ROWS 31-38 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA2015092905868](https://openairdocs.org/sdr/DALA2015092905868.md): Battery Pack · inoperative · Sep 28, 2015 · N945DL · Doug MD88 · Emergency Lighting
  > MAINTENANCE FOUND AFT OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. BATTERIES WERE REPLACED.
- [SDR DALA2015082805272](https://openairdocs.org/sdr/DALA2015082805272.md): Battery Pack · inoperative · Aug 28, 2015 · N945DL · Doug MD88 · Emergency Lighting
  > ACFT MAINTENANCE FOUND SEAT SHROUD EMERGENCY LIGHTS INOPERATIVE ON SEAT ROWS 31 AND AFT. UPPER FUSE IN EMERGENCY LIGHT BATTERY LIGHT CHARGER ABOVE SEAT ROW 35R WAS REPLACED AND NOW ALL EMERGENCY LIGHTS CK OK.
- [SDR DALA2015081805016](https://openairdocs.org/sdr/DALA2015081805016.md): Wire · pulled · Aug 18, 2015 · N945DL · Doug MD88 · Light System Wiring
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 24DE IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND WIRES PULLED OUT OF THE CONNECTOR. THE CONNECTOR WAS REPLACED AND THE SYSTEM RETURNED TO NORMAL OPERATION.
- [SDR DALA2015080704844](https://openairdocs.org/sdr/DALA2015080704844.md): Battery Pack · inoperative · Aug 3, 2015 · N945DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT ROWS 31-35 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA2015072704727](https://openairdocs.org/sdr/DALA2015072704727.md): Battery Pack · inoperative · Jul 24, 2015 · N945DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE AFT CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA2015072104514](https://openairdocs.org/sdr/DALA2015072104514.md): Battery Pack · inoperative · Jul 18, 2015 · N945DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT ROWS 31-36 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND A FAULTY LIGHT ASSY WHICH WAS BLOWING FUSES. A SATISFACTORY FUNCTIONAL CHECK WAS PERFORMED AND THE ACFT RETURNED TO SERVICE
- [SDR DALA2015062403974](https://openairdocs.org/sdr/DALA2015062403974.md): Fuse · inoperative · Jun 22, 2015 · N945DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT SEAT 31DE IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED A BAD FUSE ON THE BATTERY PACK AND THE SYSTEM RETURNED TO NORMAL OPERATION.
- [SDR DALA2015061503773](https://openairdocs.org/sdr/DALA2015061503773.md): Power Supply · inoperative · Jun 13, 2015 · N945DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT ROWS 31-36 WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.
- [SDR DALA2014122506768](https://openairdocs.org/sdr/DALA2014122506768.md): Battery Pack · inoperative · Dec 24, 2014 · N945DL · Doug MD88 · Emergency Lighting
  > DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS ABOVE THE OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS. OPS CHECKED GOOD.
- [SDR DALA2014120406421](https://openairdocs.org/sdr/DALA2014120406421.md): Line · leaking · Dec 4, 2014 · N945DL · Doug MD88 · Hydraulic System, Main
  > DURING INITIAL CLIMBOUT, CREW REPORTED A HOT HYDRAULIC ODOR BEING EMITTED FROM THE AIR CONDITIONING SYSTEM. BOTH THE FORWARD AND THE REAR LAVATORY SMOKE DETECTORS SOUNDED. ODOR DISSIPATED AND ALARMS SILENCED QUICKLY BUT THEN IT ALL REPEATED DURING APPROACH F
- [SDR DALA2014100905486](https://openairdocs.org/sdr/DALA2014100905486.md): Release Cable · out of rig · Oct 7, 2014 · N945DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE DISCOVERED THAT THE TAILCONE RELEASE CABLE WAS OUT OF ALLOWABLE RIG LIMITS AS IT DID NOT CLEAR THE CONDUIT BY THE SPECIFIED.2". THE CABLE CLAMPS WERE ADJUSTED AND THE SYS WAS RIGGED BACK INTO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.
- [SDR DALA2014100905485](https://openairdocs.org/sdr/DALA2014100905485.md): Cam · worn · Oct 7, 2014 · N945DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE DISCOVERED THAT THE TAILCONE RELEASE MECHANISM CAM BASE WAS WORN OUT OF ALLOWABLE LIMITS. THE CAM BASE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS.
- [SDR DALA2014100905484](https://openairdocs.org/sdr/DALA2014100905484.md): Conduit · worn · Oct 7, 2014 · N945DL · Doug MD88 · Aerodynamic Fairings
  > MAINTENANCE DISCOVERED THAT THE LT AND RT SIDE CONDUIT FOR THE RELEASE CABLE OF THE TAILCONE WAS WORN OUT OF ALLOWABLE LIMITS. THE CONDUIT TUBE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.
- [SDR DALA2014100805482](https://openairdocs.org/sdr/DALA2014100805482.md): Service Panel · corroded · Oct 7, 2014 · N945DL · Doug MD88 · Fluid Service Doors
  > AFT LAVATORY SERVICE PANEL HAS BULGING CORROSION AT THE LOWER FWD CORNER. CUTOUT SKIN AND INTERNAL DOUBLER TO REMOVE AREAS OF CORROSION. REPAIRED IAW PRI 529587-14, REV 0, 1, AND 2. ALL STEPS ACCOMPLISHED. COMPLIED WITH ER/A 529587-14, REV ORIG.
- [SDR DALA2014100805481](https://openairdocs.org/sdr/DALA2014100805481.md): Spar · cracked · Oct 7, 2014 · N945DL · Doug MD88 · Vertical Stabilizer, Spar/Rib
  > VERTICAL STABILIZER LT SIDE FRONT SPAR CRACKED BELOW ZFS 52.267. REPAIRED IAW ER/A 529591-14AD, REVISION ORIGINAL.
- [SDR DALA2014100805480](https://openairdocs.org/sdr/DALA2014100805480.md): Angle · damaged · Oct 7, 2014 · N945DL · Doug MD88 · Vertical Stabilizer
  > DURING C-CHECK, ELONGATED HOLES WERE FOUND COMMON TO THE LT ANGLE OF THE VERTICAL STABILIZER FRONT SPAR. FOUR OF THE HOLES ARE THE FIRST, FOURTH, FIFTH, AND SIXTH ABOVE ZFS=52. ONE OF THE HOLES IS THE FOURTH HOLE BELOW ZFS=52. ER/A 529591-14AD SECT I WA
- [SDR DALA2014100805479](https://openairdocs.org/sdr/DALA2014100805479.md): Frame · cracked · Oct 7, 2014 · N945DL · Doug MD88 · Fuselage Main, Frame
  > CANTED FRAME WEB AT BS 1485, HAS A.3750 INCH LONG CRACK AT RIVET, NEAR 8:00 O`CLOCK POSTION, WHERE TAIL INTERIOR TAIL CONE RELEASE HANDLE SUPPORT ANGLE ATTACHES. REPAIRED IAW SRM 51-70-05.
- [SDR DALA2014100705478](https://openairdocs.org/sdr/DALA2014100705478.md): Bulkhead Web · cracked · Oct 6, 2014 · N945DL · Doug MD88 · Fuselage Main, Bulkhead
  > TAIL INTERIOR CANTED BULKHEAD, BS 1463, WEB CRACKED ON FWD SIDE 23" OTBD OF ACFT CENTER LINE RT SIDE- HFEC CONFIRMED ENDS MARKED. COMPLIED WITH PRI 529613-14, REV 1 AND REPAIRED IAW ER/A 529613-14, REV ORIGINAL.
- [SDR DALA2014100605426](https://openairdocs.org/sdr/DALA2014100605426.md): Panel · out of tolerance · Oct 6, 2014 · N945DL · Doug MD88 · Aerodynamic Fairings
  > DURING TAILCONE RELEASE FUNCTIONAL CHECK, AFT ENTRANCE DOOR ROD FAILED TO PUNCTURE DECAL AND EXTEND. FOUND INTERFERENCE FROM DECORATIVE DOOR PANEL AROUND CAM ARM ASSY. TRIMMED DECORATIVE DOOR PANEL FOR CLEARANCE. OPS CHECKED GOOD IAW AMM 53-53-00-501 AND AM
- [SDR DALA14015090945](https://openairdocs.org/sdr/DALA14015090945.md): Battery Pack · inoperative · Mar 5, 2014 · N945DL · Doug MD88 · Emergency Lighting
  > FLIGHT CREW CONFIRMED THAT THE EMERGENCY LIGHT SYSTEM DID NOT ILLUMINATE ANY LIGHTS WHEN TESTED AND WAS INOPERATIVE WITH THE SWITCH IN ARM AND ONLY GROUND POWER AS A SOURCE DURING INITIAL POWER-UP. MAINTENANCE REPLACED ALL EMERGENCY LIGHT BATTERY PACKS AND TH

Next page: https://openairdocs.org/deregistered/N945DL-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 = 'N945DL' AND deregistration_id = 'N945DL-2020-11-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N945DL-2020-11-09/reports

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