# Service difficulty reports: N910DL, cancelled Feb 12, 2021

A list on [N910DL, cancelled Feb 12, 2021](https://openairdocs.org/deregistered/N910DL-2021-02-12.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 6 · 269 reports

- [SDR DALA2019100605736](https://openairdocs.org/sdr/DALA2019100605736.md): Connector · disconnected · Oct 6, 2019 · N910DL · Doug MD88 · Light System Wiring
  > EPLS SEAT LIGHTS INOP AT ROW 4 AND 36. RESEATED CONNECTORS OPS CHECK GOOD MD88 AMM 33-53.(LP5588793)
- [SDR DALA2019100405681](https://openairdocs.org/sdr/DALA2019100405681.md): Smoke Detector · malfunctioned · Oct 3, 2019 · N910DL · Doug MD88 · Smoke Detection
  > AFT LT LAVATORY SMOKE DETECTOR CHIRPING. REMOVED AND REPLACED THE SMOKE DETECTOR, OPS CHECKED NORMAL, OK FOR SERVICE.
- [SDR DALA2019092905576](https://openairdocs.org/sdr/DALA2019092905576.md): Apu · odor · Sep 28, 2019 · N910DL · Doug MD88 · APU Start/Ignition System
  > "NO GO" ODI PREVENTION - DRIVER DO NOT DISPATCH THE AIRCRAFT" - W/O MCC APPROVAL" - ON TAXI OUT APU AUTO S/D THEN PASS NOTED A ODD SMOKE/SMELL IN THE CABIN. CREW ALSO NOTED WEIRD SMELL BUT ATTRIBUTED TO THE APU S/D. C/W AMDS CARD 2120-2367 PER NO GO ODI PREVEN
- [SDR DALA2019062403763](https://openairdocs.org/sdr/DALA2019062403763.md): Engine · surges · Jun 23, 2019 · N910DL · Doug MD88 · Engine (Turbine/Turboprop)
  > ON ARRIVAL AT 10K, STARTED A DESCENT TO 5K. PLANE STARTED TO GET SLOW, WENT TO V.S. TRP WAS IN CR. THROTTLE BURST CAUSED N1 EXCEEDENCE ON BOTH ENGINES. 104.5 FOR 2 SEC ON LEFT. 102.5 FOR 1 SEC ON RIGHT. NBR 1 ENG REPLACED. REPLACED NR 2 ENGINE
- [SDR DALA2019012700538](https://openairdocs.org/sdr/DALA2019012700538.md): Connector · unsecure · Jan 26, 2019 · N910DL · Doug MD88 · Light System Wiring
  > EMERGENCY ESCAPE PATH LIGHT AT ROW 4 BOTH LIGHTS INOP. FOUND HARNESS CONNECTOR ON SEAT 4C FOR EMERGENCY LIGHTS NOT SECURE RECONNECTED CONNECTOR IAW AMM 33-53 AND 20-50 OPS CK GOOD. (LP5245470)
- [SDR DALA2019011000149](https://openairdocs.org/sdr/DALA2019011000149.md): Skin · cracked · Jan 10, 2019 · N910DL · Doug MD88 · Fuselage Main, Plate/Skin
  > FOUND BELLY SKIN CRACK AND CORROSION AFT OF NR 4 RADAR ALTIMETER ANTENNA NEAR STA 723 AND STR L29 - L30. REPAIRED PER ERA 574357-14 REV O. (LP0897799)
- [SDR DALA2018122407363](https://openairdocs.org/sdr/DALA2018122407363.md): Battery Pack · inoperative · Dec 21, 2018 · N910DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTS IN CEILING PANELS BETWEEN ROWS 22-31 NOT ILLUMINATING. REPLACED BATTERIES TO CHARGERS PER MD88 AMM 33-53. (LP5243663)
- [SDR DALA2018121307160](https://openairdocs.org/sdr/DALA2018121307160.md): Structure · cracked · Dec 12, 2018 · N910DL · Doug MD88 · Service Doors
  > FWD SERVICE DOOR UPPER FWD CORNER HAS CRACK INDICATION AT ONE FASTENER MARKED. REF AMDS 5240-2344 STEP 1. REPAIRED PER SRM SRM 53-05 FIGURE 176. (LP0861915)
- [SDR DALA2018112006700](https://openairdocs.org/sdr/DALA2018112006700.md): Unknown · odor · Nov 19, 2018 · N910DL · Doug MD88 · Air Distribution System
  > EXHAUST FUMES SMELLED AT AFT FA JUMPSEAT RIGHT AFTER TAKEOFF AFT LEFT LAV SMOKE DETECTOR ACTIVATED. SMELL WENT AWAY IN LESS THAN ONE MIN. AND SMOKE DETECTOR STOPPED SOUNDING. R/R APU PER MD88 AMM 49-10. APU STARTS OK APU OK FOR SERVICE. REMOVED CROSS OVER DUCT
- [SDR DALA2018111986679](https://openairdocs.org/sdr/DALA2018111986679.md): Unknown · odor · Nov 16, 2018 · N910DL · Doug MD88 · Air Distribution System
  > AT DEPARTURE AFTER AFT AIRSTAIRS CLOSED AFT LAV SMOKE DETECTOR ACTIVATED AND EXHAUST SMELL NOTICED AFT CABIN APU AIR ON AND EXTERNAL AIR SOURCE ALSO ON. C/W ODI PREVENTION T/S PER ATA 2172 NO/GO ODI C/W WORK CARDS 2120-2367 AND 7100-2619 REF NO GO ODI LOG 0829
- [SDR DALA2018102906330](https://openairdocs.org/sdr/DALA2018102906330.md): Hydraulic Line · leaking · Oct 27, 2018 · N910DL · Doug MD88 · Hydraulic System, Main
  > FUME EVENT ON CLIMBOUT AND DESCENT AT 12K ALTITUDE BOTH TIMES WITH ENG A/I USAGE. AFT LAV, CAPT SIDE, FIRE ALARM ACTIVATED. WENT OUT AFTER 5 MINS. NO SMOKE OF FIEW REPORTED. FOUND APU AIR INLET CONTAMINATED WITH HYD FLUID. LEFT THRUST REVERSER CNTL VALVE UPPER
- [SDR DALA2018091305578](https://openairdocs.org/sdr/DALA2018091305578.md): Battery · discharged · Sep 13, 2018 · N910DL · Doug MD88 · Emergency Lighting
  > ON SVC CHK FOUND LEFT AND RIGHT AFT OVERWING EXIT SIGN IDENTIFIERS LAMPS INOP. REMOVED AND REPLACED BATTERY PACK SUPPLY BATTERIES PER AMM 33-53. OPS CHK GOOD.
- [SDR DALA2018080204821](https://openairdocs.org/sdr/DALA2018080204821.md): Hydraulic Line · unsecure · Aug 1, 2018 · N910DL · Doug MD88 · Hydraulic System, Main
  > FLIGHT ATTENDANT REPORTED SMOKE/FUMES IN THE AFT CABIN. MAINTENANCE FOUND AND REPAIRED A HYDRAULIC LEAK AT THE LEFT THRUST REVERSER ISOLATION VALVE BY SECURING THE RETURN LINE. NO-GO ODI PREVENTION PROCEDURES WERE COMPLIED WITH.
- [SDR DALA2018073104805](https://openairdocs.org/sdr/DALA2018073104805.md): Service Panel · damaged · Jul 30, 2018 · N910DL · Doug MD88 · Wing, Plate/Skin
  > FUEL DOOR OPEN ON ARRIVAL/FUEL DOOR DAMAGED. REMOVED AND REPLACED FUEL SERVICE PANEL DOOR IAW AMM 57-30. OPS CHECK GOOD. C/W ERA 570489-14 REV ORG. SECTION 1 TIME LIMITED REPAIR. C/W TERMINATING REPAIR AT NEXT CCK AND INITIAL INSPECTION WITHIN 7 DAYS. CORRECTE
- [SDR DALA2018072304604](https://openairdocs.org/sdr/DALA2018072304604.md): Panel · cracked · Jul 20, 2018 · N910DL · Doug MD88 · Leading Edge Devices
  > CRACK INDICATION ON COVE PANEL AT CENTER ATTACH POINT. NR 2 LT SLAT REP REF RC 2700-4224-LH-02.
- [SDR DALA2018072304603](https://openairdocs.org/sdr/DALA2018072304603.md): Structure · cracked · Jul 20, 2018 · N910DL · Doug MD88 · Wing Miscellaneous Structure
  > ON WALK AROUND FOUND 2 INCH CRACK LT WING NR 2 UNDER NR 2 SLAT.
- [SDR DALA2018021300857](https://openairdocs.org/sdr/DALA2018021300857.md): Seat Track · damaged · Feb 11, 2018 · N910DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > WHILE TROUBLESHOOTING A FAULT, FOUND ELECTRICAL ARC DAMAGE ON THE SEAT TRACK AT BS 279. REPAIRED THE SEAT TRACK IAW PRI 565645-14, REV 0.
- [SDR DALA2018021100814](https://openairdocs.org/sdr/DALA2018021100814.md): Seat Track · damaged · Feb 10, 2018 · N910DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > DUE PRI 565645-14 REV 0. MD-88 / FUSELAGE / AUXILIARY STRUCTURE / SEAT TRACK STA 279, LBL 54.5 / DAMAGED FROM AN ARCING FEEDER CABLE. C/W PRI 565645-14 REV 0. C/W ERA 565645-14 REV 0. (LP0420138)
- [SDR DALA2018012900468](https://openairdocs.org/sdr/DALA2018012900468.md): Generator · failed · Jan 26, 2018 · N910DL · Doug MD88 · AC Generator-Alternator
  > DECLARED EMERGENCY DUE TO REPORTED TOTAL LOSS OF ELECTRICAL POWER. UPON ARRIVAL IT WAS DETERMINED THAT THE RT GEN HAD FAILED ALONG WITH THE A/C CROSS TIE LOCK OUT MESSAGE. T/S THE RT GENERATOR SYSTEM AND THE A/C CROSS TIE SYSTEM. R&R R2-216 AND R2-45 AMM 24-2
- [SDR DALA2017100507315](https://openairdocs.org/sdr/DALA2017100507315.md): Shear Tie · cracked · Oct 4, 2017 · N910DL · Doug MD88 · Fuselage Main, Bulkhead
  > LEFT AND RIGHT AFT PRESSURE BULKHEAD SPLICES ON FWD SHEAR ANGLE TAB ONLY HAVE TWO FASTENERS ON THE ONE SIDE OF THE CUT(EXAMPLE 2+4)SPLICES ARE AT 26LT AND 27LT AND 26RT AND 27RT. ALSO TWO FASTENERS HAVE CRACK INDICATIONS ON 26RT FWD OF APB 11 INCHES. C/W ERA
- [SDR DALA2017100407252](https://openairdocs.org/sdr/DALA2017100407252.md): Frame · cracked · Oct 3, 2017 · N910DL · Doug MD88 · Fuselage Main, Frame
  > CRACK IN FRAME STRUCTURE 1485 LEFT. REPAIRED PER ERA 562285-14 REV ORIG.
- [SDR DALA2017041302983](https://openairdocs.org/sdr/DALA2017041302983.md): Power Supply · malfunctioned · Apr 12, 2017 · N910DL · Doug MD88 · Emergency Lighting
  > DURING RAMP CHECK, COCKPIT OVERHEAD EMERGENCY LIGHT ON DIM WITH SWITCH ON OR OFF POSITION. REPLACED POWER SUPPLY IAW WDM 33-51-12.
- [SDR DALA2017011100261](https://openairdocs.org/sdr/DALA2017011100261.md): Cap · displaced · Jan 11, 2017 · N910DL · Doug MD88 · APU Oil System
  > AT THE GATE JUST PRIOR TO DEPARTURE, WHEN THE AIR-CONDITIONING SUPPLY SWITCHES WERE PLACED ON, THE FLIGHT ATTENDANTS NOTICED HAZE AND SMOKE ODOR IN THE AFT CABIN. MAINTENANCE FOUND THE APU OIL CAP OFF AND OIL AROUND THE APU RAM AIR DOOR INLET. APU AND INLET C
- [SDR DALA2016102607734](https://openairdocs.org/sdr/DALA2016102607734.md): Battery Pack · inoperative · Oct 25, 2016 · N910DL · Doug MD88 · Emergency Lighting
  > FWD OVERWING, OVERHEAD EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERIES AS REQUIRED IAW AMM 33-50. OPS CHECKED GOOD.
- [SDR DALA2016053004221](https://openairdocs.org/sdr/DALA2016053004221.md): Power Supply · inoperative · May 28, 2016 · N910DL · Doug MD88 · Emergency Lighting
  > DURING SERVICE CHECK FOUND NUMEROUS EMERGENCY LIGHTS INOPERATIVE THROUGH CABIN & TAIL AREA. REPLACED POWER SUPPLY BATTERIES AND LAMP IAW WDM 33-51-13. OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR DALA2015091105554](https://openairdocs.org/sdr/DALA2015091105554.md): Access Panel · corroded · Sep 10, 2015 · N910DL · Doug MD88 · Fuselage Main, Structure
  > CORROSION ON HEATER BLANKET SKIN AROUND OF SETTLEMENT SECONDARY ACCESS PANELS NR 1303C AND 1307C AT LT WING. HEATER BLANKET WAS REPAIRED IAW ER/A 537748-14AD, REV ORIGINAL.
- [SDR DALA2015091005535](https://openairdocs.org/sdr/DALA2015091005535.md): Bushing · corroded · Sep 9, 2015 · N910DL · Doug MD88 · Wing Main, Frame Structure
  > ACFT HAS CORROSION ON BUSHINGS OF T/E RT WING UPPER SKIN FROM AFT BOLTS HEATER BLANKET. REPAIR WAS ACCOMPLISHED IAW ER/A 537750-14, AD REV. A AND ETI-88-15-291, REV. 2.
- [SDR DALA2015091005533](https://openairdocs.org/sdr/DALA2015091005533.md): Fastener · missing · Sep 9, 2015 · N910DL · Doug MD88 · Vertical Stabilizer
  > LOOSE AND MISSING FASTENERS, TWO ROWS ABOVE AND TWO ROWS BELOW THE SPLICE AT ZFS=52.267, LT/RT SIDE. FASTENERS WERE REMOVED AND FASTENERS WERE INSTALLED IAW SRM 51-30-1, REPAIR WAS ACCOMPLISHED IAW ETI-88-15-319, REV 2, ERA 477118-14AD, REV B.
- [SDR DALA2015090805476](https://openairdocs.org/sdr/DALA2015090805476.md): Cap · cracked · Sep 7, 2015 · N910DL · Doug MD88 · Fuselage Miscellaneous Structure
  > OUTER CAP HAS A CRACK BETWEEN LONGERONS 1 - 2L, BS 1437. LOWER OUTER CAP WAS REPAIRED IAW ER/A NR 537773-14, REV ORIGINAL.
- [SDR DALA2015090505445](https://openairdocs.org/sdr/DALA2015090505445.md): Skin · cracked · Sep 4, 2015 · N910DL · Doug MD88 · Fuselage Main, Plate/Skin
  > ACFT HAS FIVE CRACKS, WERE FOUND ON FUSELAGE SKIN: RT SIDE.- 0.250", 0.180" AND 0.100" AT BS Y=1418 AND BETWEEN LONGERON 2 AND 3 AND LT SIDE-0.125" AND 0.100" AT BS Y=1418 AND BETWEEN LONGERON 2 AND 3. FUSELAGE SKIN WAS REPAIRED IAW ER/A 537744-14 AD REV A A
- [SDR DALA2015090405421](https://openairdocs.org/sdr/DALA2015090405421.md): Frame · cracked · Sep 4, 2015 · N910DL · Doug MD88 · Fuselage Main, Frame
  > A CRACK WAS FOUND ON SPLICE OF CANTED FRAME BETWEEN BS 1463 AND LONGERON 18R. REPAIRED IAW ETI-88-15-311, REV 1 AND ER/A 537771-14, REV ORIGINAL.
- [SDR DALA2015090405420](https://openairdocs.org/sdr/DALA2015090405420.md): Frame · cracked · Sep 4, 2015 · N910DL · Doug MD88 · Fuselage Main, Frame
  > A CRACK WAS FOUND ON SPLICE OF CANTED FRAME BS 1463 AND LONGERON 18L. CRACK WAS ATTENDED ETI-88-15-311, REV 1 AND ERA 537771-14, REV ORIGINAL.
- [SDR DALA2015090405424](https://openairdocs.org/sdr/DALA2015090405424.md): Skin · cracked · Sep 3, 2015 · N910DL · Doug MD88 · Wing, Plate/Skin
  > CRACK ON RT WING FIXED L/E XRS=406. RT WING FIXED L/E WAS REPAIRED IAW ER/A 537770-14. REV ORIGINAL AND ETI 88-15-310.
- [SDR DALA2015090405416](https://openairdocs.org/sdr/DALA2015090405416.md): Web · cracked · Sep 3, 2015 · N910DL · Doug MD88 · Fuselage Miscellaneous Structure
  > A CRACK WAS FOUND ON WEB ON BS 1437 BETWEEN LONGERONS 1 AND 2L. WEB REPAIRED IAW ETI NR 88-15-317, REV 1 AND ER/A 537778-14 REV ORIGINAL.
- [SDR DALA2015090405415](https://openairdocs.org/sdr/DALA2015090405415.md): Skin · not reported · Sep 3, 2015 · N910DL · Doug MD88 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BS 210, LONGERON 5L. REPAIRED IAW ER/A 518525-14AD, SEC III, REV A.
- [SDR DALA2015090405414](https://openairdocs.org/sdr/DALA2015090405414.md): Skin · corroded · Sep 3, 2015 · N910DL · Doug MD88 · Fuselage Main, Plate/Skin
  > HAS A BULGE ON FUSELAGE SKIN BETWEEN BS 218 AND LONGERONS 29-30R. THE SKIN WAS REPAIRED IAW ETI88-15-295, REV 1 AND ER/A 537751-14, REV ORIGINAL.
- [SDR DALA2015090105376](https://openairdocs.org/sdr/DALA2015090105376.md): Flange · cracked · Aug 31, 2015 · N910DL · Doug MD88 · Turbine Engine Compressor Section
  > FOUND A CRACK ON FLANGE J1 AT RT ENGINE 6 RT SIDE POSITION. THE ENGINE WAS REPLACED.
- [SDR DALA2015090105365](https://openairdocs.org/sdr/DALA2015090105365.md): Frame · cracked · Aug 31, 2015 · N910DL · Doug MD88 · Fuselage Main, Frame
  > FOUND A CRACK ON FRAME BS 1455, LONGERON 1. THE FRAME WAS REPLACED IAW SRM 51-30-2 AND 51-30-5 AND DWG 99860.0, REV L.
- [SDR DALA2015090105362](https://openairdocs.org/sdr/DALA2015090105362.md): Cargo Track · corroded · Aug 31, 2015 · N910DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION ON LT CARGO TRACK BETWEEN BS 1222 - 1322, UPPER AND LOWER SURFACES. THE CARGO TRACK WAS REPLACED IAW SRM 53-24-0D, DWG 5936660 REV B2, AND SRM 51-30-1.
- [SDR DALA2015090105361](https://openairdocs.org/sdr/DALA2015090105361.md): Cargo Track · corroded · Aug 31, 2015 · N910DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION ON LT CARGO TRACK BETWEEN BS 1003 - 1098, UPPER AND LOWER SURFACES,. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-1, 51-30-5, SRM 53-24-0D AND DWG DWGS936660, REV B2.
- [SDR DALA2015090105357](https://openairdocs.org/sdr/DALA2015090105357.md): Longeron · cracked · Aug 31, 2015 · N910DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > ACFT HAS A CRACK ON LONGERON 3R BS 1437. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.
- [SDR DALA2015090105356](https://openairdocs.org/sdr/DALA2015090105356.md): Longeron · cracked · Aug 31, 2015 · N910DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > ACFT HAS CRACK ON LONGERON 4R BS 1437. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.
- [SDR DALA2015090105355](https://openairdocs.org/sdr/DALA2015090105355.md): Longeron · cracked · Aug 31, 2015 · N910DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > ACFT HAS A CRACK ON LONGERON 4L BS 1437 IN AFT ACCESSORIES COMPARTMENT. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18, 51-10-3, 51-30-5, AND 51-10-4.
- [SDR DALA2015090705469](https://openairdocs.org/sdr/DALA2015090705469.md): Angle · cracked · Aug 30, 2015 · N910DL · Doug MD88 · Vertical Stabilizer
  > CRACKED LT AND RT INTERNAL DORSAL ANGLES BETWEEN JOIN OF VERTICAL STABILIZER L/E AND FUSELAGE SKIN BS 1418. THE ANGLE WAS REPLACED IAW SRM 51-30-2 AND DWG 5912188, REV BD.
- [SDR DALA2015083105342](https://openairdocs.org/sdr/DALA2015083105342.md): Floor Panel · corroded · Aug 30, 2015 · N910DL · Doug MD88 · Fuselage Floor Panel
  > CORROSION FOUND ON COCKPIT FLOOR PANEL. THE FLOOR PANEL WAS REMOVED IAW SRM 51-30-1. THE FLOOR PANEL WAS REPLACED.
- [SDR DALA2015083005314](https://openairdocs.org/sdr/DALA2015083005314.md): Cargo Track · corroded · Aug 30, 2015 · N910DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON RT CARGO TRACK BETWEEN BS 1212 - 1322. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-1.
- [SDR DALA2015083005313](https://openairdocs.org/sdr/DALA2015083005313.md): Frame · cracked · Aug 30, 2015 · N910DL · Doug MD88 · Fuselage Main, Frame
  > CRACKED FRAME BETWEEN LONGERONS 1 - 2L BS 1437. THE FRAME WAS REPLACED IAW SRM 51-30-5.
- [SDR DALA2015083005312](https://openairdocs.org/sdr/DALA2015083005312.md): Cap · cracked · Aug 30, 2015 · N910DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CRACKED UPPER CAP BETWEEN LONGERONS 1 - 2L BS 1437. CAP WAS REPLACED IAW SRM 51-30-5.
- [SDR DALA2015083005311](https://openairdocs.org/sdr/DALA2015083005311.md): Channel · cracked · Aug 30, 2015 · N910DL · Doug MD88 · Fuselage Floor Panel
  > CRACKED CHANNEL ON FLOOR PANEL. CHANNEL REPAIRED IAW SRM 53-05, FIG 131B AND 51-70-1.
- [SDR DALA2015083005320](https://openairdocs.org/sdr/DALA2015083005320.md): Scuff Plate · cracked · Aug 29, 2015 · N910DL · Doug MD88 · Cargo/Baggage Doors
  > CRACKED SCUFF PLATE AT CARGO DOOR. THE SCUFF PLATE WAS REPAIRED IAW ER/A 491023-14MA, REV A.

Next page: https://openairdocs.org/deregistered/N910DL-2021-02-12/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 = 'N910DL' AND deregistration_id = 'N910DL-2021-02-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N910DL-2021-02-12/reports

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