# Service difficulty reports: N996DL, cancelled Apr 25, 2022

A list on [N996DL, cancelled Apr 25, 2022](https://openairdocs.org/deregistered/N996DL-2022-04-25.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 5 · 230 reports

- [SDR DALA2019102506151](https://openairdocs.org/sdr/DALA2019102506151.md): Cover · damaged · Oct 14, 2019 · N996DL · Doug MD88 · Passenger Compartment Equipment
  > PASSENGER FINGER STUCK UNDER ARMREST IN RELEASE HOLE. SEAT 4C ARMREST CAP COVER DAMAGED. REPAIRED SEAT 4C ARMREST/ ARMCAP PER MD88 AMM 25-23 OPS CK NORMAL OK FOR SERVICE. (LP6605044)
- [SDR DALA2019061703581](https://openairdocs.org/sdr/DALA2019061703581.md): Battery Pack · inoperative · Jun 17, 2019 · N996DL · Doug MD88 · Emergency Lighting
  > FWD GALLEY CEILING EXIT LIGHTS INOP. REPLACED BATTERIES IN POWER SUPPLY IN FWD DROPDOWN CEILING IAW MD88 AMM 33-50. OPS CHECK GOOD.
- [SDR DALA2019021400949](https://openairdocs.org/sdr/DALA2019021400949.md): Spar · cracked · Feb 13, 2019 · N996DL · Doug MD88 · Vertical Stabilizer, Spar/Rib
  > VERTICAL STABILIZER LHS FORWARD SPAR ZFS=52.267 CRACK. C/W PRI 575390-14AD REV 0,1,2 C/W ERA 575390-14AD REV 0. (LP0943396)
- [SDR DALA2019021300938](https://openairdocs.org/sdr/DALA2019021300938.md): Spar · cracked · Feb 13, 2019 · N996DL · Doug MD88 · Vertical Stabilizer, Spar/Rib
  > FOUND CRACK INDICATION ON FIRST LOWER HOLE LEFT SIDE VERT STAB L/E. REMOVED VERIFIED CRACK IN SPAR FLANGE. C/W ERA 575390-14AD REV ORIG SECT I, TIME LIMITED REPAIR.
- [SDR DALA2019021200918](https://openairdocs.org/sdr/DALA2019021200918.md): Bracket · cracked · Feb 12, 2019 · N996DL · Doug MD88 · Rudder Control System
  > CAPTAIN SIDE RUDDER PEDAL BRACKET ASSY CRACKED. CONTACT PLANNING TO ATTACH EM 2720-01088-0701. REPLACED CAPT'S RUDDER PEDAL BRACKET ASSY. PER AMDS W/C 2720-10188-0701. (LP0941511)
- [SDR DALA2019021100876](https://openairdocs.org/sdr/DALA2019021100876.md): Battery Pack · inoperative · Feb 9, 2019 · N996DL · Doug MD88 · Emergency Lighting
  > EMER LIGHTS INOP CELLING ROW 11-15. CHANGED BATTERIES PER MD88 AMM 33-53. OPS CK SAT. (LP5603144)
- [SDR DALA2019100905789](https://openairdocs.org/sdr/DALA2019100905789.md): Fairing · missing · Jan 19, 2019 · N996DL · Doug MD88 · Trailing Edge Flaps
  > RT WING MOST INBOARD FLAP FAIRING - MISSING O/B SECONDARY FAIRING. INSTALLED RT FLAP SECONDARY FAIRING IAW ERA 580914-14. (LP5053442)
- [SDR DALA2019010900109](https://openairdocs.org/sdr/DALA2019010900109.md): Light · inoperative · Jan 9, 2019 · N996DL · Doug MD88 · Emergency Lighting
  > SEATS 11D, E EMERGENCY LIGHTS INOP AT ISLE. RE LAMP BULBS IAW MM 33-53 LIGHT CKS OK. (LP5053403)
- [SDR DALA2018122407371](https://openairdocs.org/sdr/DALA2018122407371.md): Door · open · Dec 21, 2018 · N996DL · Doug MD88 · Landing Gear Door Retract Section
  > RT MAIN GEAR LIGHT ILLUMINATED RED/UNSAFE WITH GEAR HANDLE UP AFTER T.O. ALSO AMBER GEAR DOOR OPEN LIGHT ILLUMINATED. VERBAL FROM FLT CREW, TOWER COMFIRMED GEAR DOOR STATED OPEN. ALSO SUSPECT FLOWN ENTIRE FLIGHT W/GEAR DOOR OPEN. (LP4808728)
- [SDR DALA2018102306241](https://openairdocs.org/sdr/DALA2018102306241.md): Tail Cone · unwanted deploy · Oct 23, 2018 · N996DL · Doug MD88 · Aerodynamic Fairings
  > WHILE PERFORMING MEET & GREET WALK AROUND AFT TAIL CONE DEPLOYED. TAIL CONE DROPPED DUE TO AFT ENTRY DOOR ACTIVATON PLACARD PUNCTURED, ARM OVER AFT DOOR DEPLOYED. SLIDE DID NOT DEPLOY DUE TO IT BEING PINED. INSTALLED TAIL CONE PER CARD 5350-9645 JOB #000-001:
- [SDR DALA2018103106352](https://openairdocs.org/sdr/DALA2018103106352.md): Tray · stuck · Oct 18, 2018 · N996DL · Doug MD88 · Passenger Compartment Equipment
  > IN ARM REST TRY TABLE AT 10C STUCK IN DOWN POSITION PASSENGER MANAGED TO OPEN 1 TIME AND WHILE ATTEMPTING TO CLOSE/STORE HE CUT HIS FINGER. OPS CHECK NORMAL. TRAY TABLE STOWS AND COMES OUT NORMALLY AT LOC. 10C. SDR REPORTED DUE TO PASSENGER GETTING INJURED. (L
- [SDR DALA2018092405722](https://openairdocs.org/sdr/DALA2018092405722.md): Engine · making metal · Sep 20, 2018 · N996DL · Doug MD88 · Engine (Turbine/Turboprop)
  > THE FLIGHT CREW DIVERTED THE AIRCRAFT TO IAD AFTER THE FAILURE OF THE NR 2 ENGINE DURING CLIMB OUT OF RIC. MAINTENANCE FOUND METAL IN THE TAIL PIPE WITH TURBINE DAMAGE. THE NR 2 ENGINE WAS REPLACED.
- [SDR DALA2018082105160](https://openairdocs.org/sdr/DALA2018082105160.md): Battery Pack · inoperative · Aug 21, 2018 · N996DL · Doug MD88 · Emergency Lighting
  > ALL F/C EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY PACK, OPS CHECKED GOOD IAW AMM 33-50.
- [SDR DALA2018081205012](https://openairdocs.org/sdr/DALA2018081205012.md): Unknown · unknown · Aug 10, 2018 · N996DL · Doug MD88 · Emergency Lighting
  > FWR LT AND RT EXIT EMERGENCY LIGHTS OVER WING INOPERATIVE. CYCLED SYSTEM POWER AND EMERGENCY LIGHTS OPS CHECK GOOD ON SEVERAL ATTEMPTS IAW MM 33-51.
- [SDR DALA2018041102333](https://openairdocs.org/sdr/DALA2018041102333.md): Connector · damaged · Apr 10, 2018 · N996DL · Doug MD88 · Light System Wiring
  > SEAT 17D EMERGENCY LIGHT INOPERATIVE. REPLACED THE CONNECTER AT SEAT 17D. EMERGENCY LIGHT CHECKED GOOD IAW AMM 33-53-00.
- [SDR DALA2018040302144](https://openairdocs.org/sdr/DALA2018040302144.md): Heater Blanket · damaged · Apr 3, 2018 · N996DL · Doug MD88 · Airfoil Anti/De-ice System
  > NDT INSPECTION OF THE RIGHT WING HEATER BLANKET, AFTER INSTALLATION SHOWS A VOID ALONG AFT INBOARD EDGE APPROX. 0.5 INCH WIDE X 8 INCHES LONG. THE HEATER BLANKET WAS REMOVED AND REPLACED IAW PRI 567147-14, REV 0 THRU 7.
- [SDR DALA2018032801996](https://openairdocs.org/sdr/DALA2018032801996.md): Battery Pack · inoperative · Mar 28, 2018 · N996DL · Doug MD88 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE 25A AND 25E. REPLACED THE BATTERY PACK IAW AMM 33-57, CHECKED NORMAL.
- [SDR DALA2018022801283](https://openairdocs.org/sdr/DALA2018022801283.md): Skin Panel · debonded · Feb 27, 2018 · N996DL · Doug MD88 · Wing, Plate/Skin
  > LT WING UPPER PANEL FWD OF AILERON HAS AREA OF DISBOND BULGING MARKED. REPLACED PANEL ASSY REF BACDWG 5910515-507 INSTALL.
- [SDR DALA2018022301103](https://openairdocs.org/sdr/DALA2018022301103.md): Lanyard · disconnected · Feb 22, 2018 · N996DL · Doug MD88 · Escape Slide
  > TAILCONE SLIDE DEPLOYMENT LANYARD DISCONNECTED. CONNECTED THE TAILCONE SLIDE DEPLOYMENT LANYARD.
- [SDR DALA2018021500929](https://openairdocs.org/sdr/DALA2018021500929.md): Angle · cracked · Feb 15, 2018 · N996DL · Doug MD88 · Fuselage Miscellaneous Structure
  > RIGHT MAIN GEAR WHEEL WELL, CRACK IN OUTBOARD AFT ANGLED, CORNER OF WHEEL WELL PREVIOUSLY REPAIRED. REPAIRED JAM PER ERA 520687-14MA REV A.
- [SDR DALA2018021300874](https://openairdocs.org/sdr/DALA2018021300874.md): Skin · cracked · Feb 13, 2018 · N996DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CRACK IN FUSELAGE, AFT LEFT SIDE, 20 INCHES FWD OF TAIL JETTISON HANDLE. INSTALLED REPAIR DOUBLER REF SRM 53-01, FIG 4 SHT 4.
- [SDR DALA2017122908973](https://openairdocs.org/sdr/DALA2017122908973.md): Smoke Detector · false activation · Dec 27, 2017 · N996DL · Doug MD88 · Smoke Detection
  > RIGHT AFT LAVATORY SMOKE DETECTOR SOUNDED CONTINUOUSLY AFTER SINK FLOODED. SWAPPED WITH LEFT LAVATORY SMOKE DETECTOR. R & R THE LT LAVATORY SMOKE DETECTOR IAW AMM 26-13. OPS CHECKED GOOD.
- [SDR DALA2017100407265](https://openairdocs.org/sdr/DALA2017100407265.md): Wire Harness · damaged · Oct 4, 2017 · N996DL · Doug MD88 · Light System Wiring
  > SEAT 18D EMERGENCY LIGHT INOPERATIVE. REPLACED SEAT WIRING HARNESS AND LAMP IAW AIM 33-53. OPS NORMAL.
- [SDR DALA2017090206543](https://openairdocs.org/sdr/DALA2017090206543.md): Windshield · arced · Sep 1, 2017 · N996DL · Doug MD88 · Windshield/Door Rain/Ice Removal
  > DURING FINAL APPROACH, FIRST OFFICER`S WINDSHIELD HEAT UNIT ARCED AND SPARKED VISUAL AND AURAL SPARK BOTH WINDSHIELD ANTI- FOG AND ANTI-ICE SWITHES ON, NO CIRCUIT BREAKERS TRIPPED, NO SCORCH MARKS NOTED. PERFORMED AN OPERATIONAL CHECK OF THE WINDSHIELD ANT
- [SDR DALA2017082206346](https://openairdocs.org/sdr/DALA2017082206346.md): Megaphone · inoperative · Aug 17, 2017 · N996DL · Doug MD88 · Emergency Equipment
  > AFT MEGAPHONE INOP. RPLD BATTERIES. NO HELP. INSTALLED NEW MEGAPHONE. OK FOR SVC.
- [SDR DALA2017080806072](https://openairdocs.org/sdr/DALA2017080806072.md): Switch · sparks · Aug 7, 2017 · N996DL · Doug MD88 · Windshield/Door Rain/Ice Removal
  > AFTER LANDING, TURNED ON WINDSHIELD ANTI-FOG. SPARKS BRIEFLY EMITTED FROM ELEMENT ON FIRST OFFICER`S WINDSHIELD SWITCH, PLACED OFF. OPS CHECKED THE FIRST OFFICER'S WINDSHIELD ANTI-FOG IAW AMM 30-41. OPS CHECKED NORMAL.
- [SDR DALA2017080405961](https://openairdocs.org/sdr/DALA2017080405961.md): Transmitter · failed · Aug 4, 2017 · N996DL · Doug MD88 · Engine Oil Pressure
  > CREW DECLARED AN EMERGENCY DUE TO THE RIGHT ENGINE OIL PRESSURE READING HIGH. MAINTENANCE REPLACED THE OIL PRESSURE REGULATING VALVE, THE OIL PRESSURE TRANSMITTER, AND THE OIL PRESSURE TRANSMITTER CONNECTOR PLUG. THE AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR DALA2017080105819](https://openairdocs.org/sdr/DALA2017080105819.md): Slide · no test · Jul 31, 2017 · N996DL · Doug MD88 · Escape Slide
  > TAILCONE SLIDE FAILED THE DEPLOYMENT TEST. THE TAILCONE DROPPED NORMALLY, LT FWD HOLD DOWN STRAP DID NOT RELEASE ON SLIDE. THE SLIDE WAS REPLACED.
- [SDR DALA2017050203521](https://openairdocs.org/sdr/DALA2017050203521.md): Wire Harness · inoperative · May 2, 2017 · N996DL · Doug MD88 · Light System Wiring
  > EMERGENCY LIGHT AT 15ED INOPERATIVE. INSTALLED A NEW HARNESS IAW AMM 33-53. OPS NORMAL.
- [SDR DALA2017010400077](https://openairdocs.org/sdr/DALA2017010400077.md): Light · inoperative · Jan 4, 2017 · N996DL · Doug MD88 · Emergency Lighting
  > SEAT ROW 23 EMERGENCY LIGHT INOP. INSTALLED NEW LIGHT PER MD88 MM 33-52.
- [SDR DALA2016101307238](https://openairdocs.org/sdr/DALA2016101307238.md): Battery Pack · inoperative · Oct 12, 2016 · N996DL · Doug MD88 · Emergency Lighting
  > MULTIPLE FIRST CLASS EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED & REPLACED THE BATTERIES. OPS CHECKED GOOD.
- [SDR DALA2016021301066](https://openairdocs.org/sdr/DALA2016021301066.md): Angle · damaged · Feb 12, 2016 · N996DL · Doug MD88 · Fuselage Miscellaneous Structure
  > ELONGATED HOLES ON ANGLE BS 1338 BETWEEN LONGERON 27-26 LT/RT SIDE AT C3. CLIP WAS REPAIRED IAW ETI-88-16-021, REV 5 AND ER/A 541622-14, REV ORIGINAL.
- [SDR DALA2016021301061](https://openairdocs.org/sdr/DALA2016021301061.md): Splice · corroded · Feb 12, 2016 · N996DL · Doug MD88 · Fuselage Main, Structure
  > CORROSION ON SPLICE, BS 1338 BETWEEN OF 28RT TO 28LT. SPLICE DOUBLER WAS REPLACED IAW SRM 51-30-5, 51-30-2 AND DWG 9915561, REV CG.
- [SDR DALA2016021301060](https://openairdocs.org/sdr/DALA2016021301060.md): Stringer · cracked · Feb 12, 2016 · N996DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > ONE CRACK WAS FOUND ON STR 17R. STRINGER WAS REPAIRED IAW ER/A 541614-14 AD REV ORIGINAL AND ER/A 541616-14, REV ORIGINAL.
- [SDR DALA2016021301059](https://openairdocs.org/sdr/DALA2016021301059.md): Stringer · cracked · Feb 12, 2016 · N996DL · Doug MD88 · Fuselage Main, Longeron/Stringer
  > ONE CRACK WAS FOUND ON STRINGER 17L. STRINGER WAS REPAIRED IAW ER/A 541614-14 AD, REV ORIGINAL AND ER/A 541616-14, REV ORIGINAL.
- [SDR DALA2016021201013](https://openairdocs.org/sdr/DALA2016021201013.md): Bulkhead · dented · Feb 11, 2016 · N996DL · Doug MD88 · Fuselage Main, Bulkhead
  > DENTED FWD BULKHEAD, BS 37, X=0 TO X=-2 AND Z=-18 IN NLG COMPARTMENT. REPAIRED IAW ER/A 543140-14, REV ORIG AND ETI 88-16-047, REV 1.
- [SDR DALA2016021201003](https://openairdocs.org/sdr/DALA2016021201003.md): Door Frame · cracked · Feb 11, 2016 · N996DL · Doug MD88 · Fuselage Main, Structure
  > CRACKED FRAME ON BS 1485 CANT BELOW OF PASSENGER AFT ENTRANCE DOOR STAIRWAY ACTUATING CYLINDER. FRAME WAS REPAIRED IAW SRM 53-03D, FIG 43.
- [SDR DALA2016021000968](https://openairdocs.org/sdr/DALA2016021000968.md): Frame · corroded · Feb 9, 2016 · N996DL · Doug MD88 · Fuselage Main, Frame
  > CORROSION ON FRAME BS 1250 ON LONGERON 30 AT C3. FRAME WAS REPAIRED IAW SRM 53-03"D", FIG 2A SHEET 3.
- [SDR DALA2016020900938](https://openairdocs.org/sdr/DALA2016020900938.md): Cusp Web · corroded · Feb 8, 2016 · N996DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON RT CUSP WEB FROM 503 TO 598, X=54 TO X=60 AT CABIN FLOOR STRUCTURE. CUSP WEB WAS REPLACED IAW SRM 51-30-2 AND DWG 9930538, REV CF DUE EXCESSIVE CORROSION.
- [SDR DALA2016020800920](https://openairdocs.org/sdr/DALA2016020800920.md): Structure · damaged · Feb 7, 2016 · N996DL · Doug MD88 · Horizontal Stabilizer Structure
  > SCRATCHES AND CORROSION ON LT & RT INBD AND OTBD HINGE PIVOT BORE AT HORIZONTAL STABILIZER. LT & RT INBD AND OTBD HINGE PIVOT BORE WAS REPAIRED IAW SRM 55-02D PAR 7B ETI-88-16-042 REV 1 AND ER/A 543136-14, FINAL 1D.
- [SDR DALA2016020800922](https://openairdocs.org/sdr/DALA2016020800922.md): Skin · damaged · Feb 7, 2016 · N996DL · Doug MD88 · Vertical Stabilizer, Plate/Skin
  > SUNKEN FASTENERS 9 EA AT REMOVABLE L/E SECOND ROW ABOVE BS ZFS=52.267 VERTICAL STABILIZER. VERTICAL STABILIZER WAS REPAIRED IAW SRM 55-03D, PAR 28, FIG 30, 55-03, PAR 27, FIG 29, 51-10-3, PAR 14/21, 51-10-2, 51-10-4 AND 51-30-5 AND AMDS 55-30-01045-08.
- [SDR DALA2016020800921](https://openairdocs.org/sdr/DALA2016020800921.md): Rib · cracked · Feb 7, 2016 · N996DL · Doug MD88 · Horizontal Stabilizer, Spar/Rib
  > CRACK OF 0.625" OF LENGTH ON HORIZONTAL STABILIZER CENTER SECTION RT RIB HINGE PIVOT BEARING LUG. RIB WAS REPLACED IAW AMM 20-10-14, 55-10-00-201, PARA 8B, 7B AND CARD 5500-01011-08, JOB 184-0001.
- [SDR DALA2016020700915](https://openairdocs.org/sdr/DALA2016020700915.md): Cargo Track · corroded · Feb 6, 2016 · N996DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LT CARGO TRACK SPLICES, BS 1212 AT C3. DUE TO EXCESSIVE CORROSION CARGO TRACK SPLICES WERE REPLACED IAW SRM 51-10-2 AND 51-30-5, DWG 5936660, REV: BZ ORIGINAL.
- [SDR DALA2016020500894](https://openairdocs.org/sdr/DALA2016020500894.md): Web · damaged · Feb 4, 2016 · N996DL · Doug MD88 · Fuselage Miscellaneous Structure
  > ELONGATED HOLE ON WEB BS 370 BETWEEN LONGERONS 26-27 RT, AT C1. REPAIR WAS ACCOMPLISHED IAW INSTRUCTIONS OF ER/A 541621-14, REV:ORIGINAL AND ETI 88-16-020, REV 3.
- [SDR DALA2016020500888](https://openairdocs.org/sdr/DALA2016020500888.md): Cargo Track · corroded · Feb 4, 2016 · N996DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > ELONGATED HOLES ON LT TIE TRACK FROM BS X=712 TOY=785 C2. TIE TRACK WAS ATTENDED IAW ERA 543139-14, REV ORIGINAL AND ETI-88-16-046, REV: 1.
- [SDR DALA2016020500886](https://openairdocs.org/sdr/DALA2016020500886.md): Doubler · corroded · Feb 4, 2016 · N996DL · Doug MD88 · Fuselage Main, Plate/Skin
  > CORROSION ON INNER PRODUCTION DOUBLER BS 1231-1250 BETWEEN LONGERONS 28 - 29 RT. REPAIRED IAW ETI-88-16-003, REV 2 AND ER/A 541601-14, REV ORI.
- [SDR DALA2016020300825](https://openairdocs.org/sdr/DALA2016020300825.md): Cusp Web · corroded · Feb 2, 2016 · N996DL · Doug MD88 · Fuselage Miscellaneous Structure
  > CORROSION ON LT CUSP WEB FROM BS 1174- 1179 ALSO BS 1242-1250 BETWEEN X=44- X=60 AT CABIN FLOOR STRUCTURE. DUE TO EXCESSIVE CORROSION CUSP WEB WAS REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-5.
- [SDR DALA2016020300824](https://openairdocs.org/sdr/DALA2016020300824.md): Fitting · cracked · Feb 2, 2016 · N996DL · Doug MD88 · Fuselage Main, Attach Fittings
  > CRACKED FITTING INTO CENTER FUEL TANK BS 886, X=0, JUST ABOVE LONGERON 18, REF CARD 124, ZONE 10. FITTING INTO CENTER FUEL TANK BS 886, X=0 WAS REPLACED IAW SRM 51-30-5, 51-10-4, 51-10-3, PAR 14 AND 21.
- [SDR DALA2016020100781](https://openairdocs.org/sdr/DALA2016020100781.md): Frame · corroded · Jan 31, 2016 · N996DL · Doug MD88 · Fuselage Main, Frame
  > CORROSION ON PREVIOUS REPAIR FRAME, BS 1309 BETWEEN LONGERONS 29 LT TO 28 RT. REPAIR WAS ACCOMPLISHED IAW SRM 53-03, D, FIG 2A.
- [SDR DALA2016020100780](https://openairdocs.org/sdr/DALA2016020100780.md): Cargo Track · corroded · Jan 31, 2016 · N996DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LT TIE TRACK BETWEEN BS 1060 TO 1211 AT C3. NEW TIE TRACK WAS DRILLED IAW SRM 51-10-4. DRILLED NEW TIE TRACK WAS TREATED AND PAINTED IAW SRM 51-10-3 PAR 14, 21, 38. NEW TIE TRACK WAS INSTALLED IAW SRM 51-30-1 AND 51-30-2.

Next page: https://openairdocs.org/deregistered/N996DL-2022-04-25/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 = 'N996DL' AND deregistration_id = 'N996DL-2022-04-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N996DL-2022-04-25/reports

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