# Service difficulty reports: N244WA, cancelled Jun 13, 2007

A list on [N244WA, cancelled Jun 13, 2007](https://openairdocs.org/deregistered/N244WA-2007-06-13.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 · 69 reports

- [SDR DL73S050805](https://openairdocs.org/sdr/DL73S050805.md): Floorbeam · cracked · Dec 16, 2005 · N244WA · Boeing 737247 · Fuselage Main, Floor Beam
  > THE RBL 24.8 FLOORBEAM HAD A PREVIOUS CHANNEL REPAIR INSTALLED THAT DOES NOT COMPLY WITH A RECENT AD. CHANNEL REPLACED PER ER/A 452157-14AD.
- [SDR DL73S050804](https://openairdocs.org/sdr/DL73S050804.md): Floorbeam · cracked · Dec 16, 2005 · N244WA · Boeing 737247 · Fuselage Main, Floor Beam
  > THE OVERWING FLOORBEAM AT LBL 24.8 WAS PREVIOUSLY REPAIRED WITH A CHANNEL THAT DID NOT MEET THE REQUIREMENTS OF A RECENT AD. REPLACED THE C-CHANNEL REPAIR WITH A NEW CHANNEL.
- [SDR DL73S050566](https://openairdocs.org/sdr/DL73S050566.md): Engine · malfunctioned · Sep 26, 2005 · N244WA · Boeing 737247 · Engine (Turbine/Turboprop)
  > MOMENTS AFTER ADDING T/O POWER HEARD A LOUD BOOM FROM RT SIDE OF A/C. ABORTED T/O APPROX 20 KTS. PAX REPORTED ORANGE FLAME FROM NR 2 ENG EXHAUST. SHUTDOWN NR 2 ENG AFTER CLEAR OF RUNWAY. NO ABNORMAL ENG INDICATIONS, NO FIRE INDICATION. INSP NR 2 INTAKE AN
- [SDR DL73S040966](https://openairdocs.org/sdr/DL73S040966.md): Connector · shorted · Oct 14, 2004 · N244WA · Boeing 737247 · Buffet/Galleys
  > AFT GALLEY NR 2 COFFEEMAKER C/B POPPED. LATER TRASH CAN FILLED UP WITH WATER. WATER SUPPLY SHUT OFF. REMOVED BOTH COFFEEMAKERS. FOUND ARCING ON NR 2 COFFEEMAKER CANNON PLUG. TURNED WATER SUPPLY ON. CANNOT FIND SOURCE OF LEAK. REPLACED BOTH COFFEEMAKERS
- [SDR DL73S040580](https://openairdocs.org/sdr/DL73S040580.md): Odor · detected · Jun 21, 2004 · N244WA · Boeing 737247 · Air Distribution System
  > EN ROUTE AT 33,000 FT STRONG ELEC ODOR IN THE VICINITY OF THE COPILOTS CIRCUIT PANEL. NO SMOKE. INSPECTED AREA AND RAN ENGINES/PACKS. UNABLE TO DUPLICATE.
- [SDR DL73S040544](https://openairdocs.org/sdr/DL73S040544.md): Skin · scratched · Jun 10, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRATCHES WERE FOUND ON THE LOWER FUSELAGE SKIN AT THE STR 14L LAP SPLICE BETWEEN STA 345 AND 360. REPAIRED PER ERA 090265-14.
- [SDR DL73S040543](https://openairdocs.org/sdr/DL73S040543.md): Skin · scratched · Jun 10, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRATCH WAS FOUND ON THE LOWER SKIN AT THE S14 SKIN LAP FROM STA 259-312. REPAIRED PER ERA 089694-14.
- [SDR DL73S040522](https://openairdocs.org/sdr/DL73S040522.md): Skin · damaged · Jun 10, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRIBE MARKS ON THE FUSELAGE SKIN AT STRINGER 10R BETWEEN STA 986 T0 1016. AREA REPAIRED IAW ER/A 089689-14.
- [SDR DL73S040521](https://openairdocs.org/sdr/DL73S040521.md): Door Frame · unknown · Jun 10, 2004 · N244WA · Boeing 737247 · Fuselage Main, Structure
  > FASTENER INSTALLATION REQUIRED RADIUS BLOCKS AND OVERSIZED FASTENER WHILE PERFORMING EO 03-055852-03AD AT THE FWD SERVICE DOOR CUTOUT AFT FRAME. VA 72553AD ISSUED AND 8110-3 RECEIVED PROVIDING APPROVAL.
- [SDR DL73S040520](https://openairdocs.org/sdr/DL73S040520.md): Skin · torn · Jun 10, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > TEAR IN THE UPPER FUSELAGE SKIN ADJACENT TO THE STR 25 R LAP JOINT. DAMAGE TO BE INCORPORATED INTO LAP SPLICE REPAIR. AREA REPAIRED IN ACCORDANCE WITH ERA 090580-14.
- [SDR DL73S040519](https://openairdocs.org/sdr/DL73S040519.md): Skin · damaged · Jun 10, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRIBE MARK DAMAGE AT STR 16L FROM STA 540 - 727. REPAIRED IN ACCORDANCE WITH ER/A 090576-14.
- [SDR DL73S040518](https://openairdocs.org/sdr/DL73S040518.md): Skin · damaged · Jun 10, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRIBE MARKS FOUND AT S16R BETWEEN BS 540 AND 727. DAMAGE REMOVED AND REPAIRED PER ERA 090575-14.
- [SDR DL73S040517](https://openairdocs.org/sdr/DL73S040517.md): Skin · damaged · Jun 10, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE S4R LAP SPLICE, LOWER SKIN, BETWEEN BS 259.5 AND 360. ISSUED REPAIR 089821-14.
- [SDR DL73S040516](https://openairdocs.org/sdr/DL73S040516.md): Skin · damaged · Jun 10, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRIBE MARKS WERE NOTED IN THE S10R LAP, LOWER SKIN, BETWEEN BS 540 AND 727. ISSUED REPAIR VIA 089765-14.
- [SDR DL73S040515](https://openairdocs.org/sdr/DL73S040515.md): Skin · damaged · Jun 10, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRIBE MARKS WERE FOUND IN THE LOWER SKIN OF THE S19L LAP BETWEEN BS 360 AND 540. ISSUED REPAIR VIA ERA 090436-14.
- [SDR DL73S040541](https://openairdocs.org/sdr/DL73S040541.md): Flap Track · stripped · Jun 9, 2004 · N244WA · Boeing 737247 · Trailing Edge Flaps
  > RIGHT WING O/B FLAP O/B TRACK CARRIAGE STOP ATTACH HOLES WEAR: 2 HOLES THAT ATTACH MAIN FLAP CARRIAGE STOP TO O/B FLAP O/B TRACK ASSY WERE STRIPPED IN TRACK. O/S BOLTS WERE INSTALLED ER/A 090836-14, REVISION INITIAL.
- [SDR DL73S040540](https://openairdocs.org/sdr/DL73S040540.md): Flap Track · stripped · Jun 9, 2004 · N244WA · Boeing 737247 · Trailing Edge Flaps
  > RIGHT WING O/B FLAP I/B TRACK CARRIAGE STOP ATTACH HOLES WEAR: 2 BOLT HOLES THAT ATTACH MAIN CARRIAGE STOP TO O/B FLAP I/B TRACK ASSY WERE STRIPPED IN TRACK. O/S BOLTS WERE INSTALLED ER/A 090835-14, REVISION INITIAL.
- [SDR DL73S040539](https://openairdocs.org/sdr/DL73S040539.md): Skin · damaged · Jun 9, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 360 - FS 440 S19R LAP SPLICE LOWER SKIN DAMAGE BELOW LAP SPLICE. REPAIR DOUBLERS INSTALLED ER/A 090445-14, REVISION INITIAL.
- [SDR DL73S040538](https://openairdocs.org/sdr/DL73S040538.md): Skin · damaged · Jun 9, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 259-360 S19R LAP SPLICE LOWER SKIN DAMAGE BELOW THE LAP SPLICE ALONG S19R BETWEEN FS 259 AND FS 360. REPAIR DOUBLERS INSTALLED ER/A 089739-14, REVISION INITIAL.
- [SDR DL73S040537](https://openairdocs.org/sdr/DL73S040537.md): Skin · damaged · Jun 9, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 908 - FS 1016 S4R LAP SPLICE LOWER SKIN DAMAGE BELOW LAP SPLICE AT S4R BETWEEN FS 908 AND FS 1016. REPAIR DOUBLERS INSTALLED ER/A 090115-14, REV A.
- [SDR DL73S040536](https://openairdocs.org/sdr/DL73S040536.md): Skin · scratched · Jun 9, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 727, S16L - BL 0 FILLET PANEL PERIMETER + FS 770-908, S20L LAP SPLICE REPAIR OF SCRIBE MARKS, TOOLING DAMAGE BELOW THE LAP SPLICE ALONG S20L BETWEEN FS 727 AND FS 908 AND ALONG THE EDGE OF THE FILLET PANEL AFT OF THE WING. REPAIR DOUBLERS WER
- [SDR DL73S040535](https://openairdocs.org/sdr/DL73S040535.md): Skin · scratched · Jun 9, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRIBE MARK DAMAGE WAS FOUND DUE TO METAL PAINT SCRAPER USE ON THE LOWER SKIN AT THE STRINGER 14L LAP SPLICE, LOCATED BETWEEN FUSELAGE STA 259 AND 312. REPAIRED PER ERA 089672-14.
- [SDR DL73S040531](https://openairdocs.org/sdr/DL73S040531.md): Skin · damaged · Jun 9, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > DAMAGE ON FUSELAGE SKIN ALONG THE TRAILING EDGE WING-TO-BODY FAIRING. REPAIRED IAW ERA 090712-14.
- [SDR DL73S040529](https://openairdocs.org/sdr/DL73S040529.md): Skin · scratched · Jun 9, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRATCHES IN THE FUSELAGE SKIN AT STRINGER 10L BETWEEN STATION 345 AND 360. REPAIR IAW ERA 090206-14.
- [SDR DL73S040528](https://openairdocs.org/sdr/DL73S040528.md): Skin · damaged · Jun 9, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SKIN AT STATION 178 AND WL 195 SUFFERED DAMAGE AND REQUIRED OVERSIZE FASTENERS THRU THE STATION 178 BULKHEAD CHORD AND AN EDGE TRIM. REPAIRED IAW ERA 089942-14AD.
- [SDR DL73S040527](https://openairdocs.org/sdr/DL73S040527.md): Bulkhead · corroded · Jun 9, 2004 · N244WA · Boeing 737247 · Fuselage Main, Bulkhead
  > STATION 1016 BULKHEAD WEB, STIFFENERS AND CHORDS CORRODED AT BL 0. CHORD SUFFERED DAMAGE AT BL 0 DURING COURSE OF REPAIR. AREA REPAIRED IAW ERA 089856-14AD.
- [SDR DL73S040526](https://openairdocs.org/sdr/DL73S040526.md): Skin · scratched · Jun 9, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRATCHES ON THE FUSELAGE SKIN AT STRINGER 19L FROM STATIONS 259 - 360. AREA REPAIRED IN ACCORDANCE WITH ERA 090232-14.
- [SDR DL73S040542](https://openairdocs.org/sdr/DL73S040542.md): Fitting · corroded · Jun 8, 2004 · N244WA · Boeing 737247 · Horizontal Stabilizer, Attach Fittings
  > HORIZONTAL STABILIZERS ATTACH FITTINGS LUGS AND CLEVIS LUGS CORROSION: CORROSION BLENDED AND O/S BUSHINGS INSTALLED ER/A 090581-14AD, REVISION INITIAL.
- [SDR DL73S040377](https://openairdocs.org/sdr/DL73S040377.md): Skin · damaged · Apr 27, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRIBE MARKS WERE NOTED IN THE LOWER SKIN OF THE S10L LAP JOINT BETWEEN BS 360 AND 540. DAMAGE WAS REMOVED AND REPAIRED IAW ERA 090052-14.
- [SDR DL73S040375](https://openairdocs.org/sdr/DL73S040375.md): Skin · damaged · Apr 27, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRIBE MARKS WERE NOTED IN THE LOWER SKIN OF THE S10R LAP JOINT BETWEEN BS 908 AND 960. DAMAGE WAS REMOVED AND THE AREA REPAIRED PER ERA 089670-14.
- [SDR DL73S040358](https://openairdocs.org/sdr/DL73S040358.md): Skin · damaged · Apr 19, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S10R FROM BS 360 THROUGH BS 540. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089757-14.
- [SDR DL73S040357](https://openairdocs.org/sdr/DL73S040357.md): Skin · damaged · Apr 19, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S10R FROM BS 727 THROUGH BS 908. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089716-14.
- [SDR DL73S040356](https://openairdocs.org/sdr/DL73S040356.md): Skin · damaged · Apr 19, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S10L FROM BS 727 THROUGH BS 908. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089715-14.
- [SDR DL73S040355](https://openairdocs.org/sdr/DL73S040355.md): Skin · damaged · Apr 19, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S4L FROM BS 360 THROUGH BS 540. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089714-14.
- [SDR DL73S040354](https://openairdocs.org/sdr/DL73S040354.md): Skin · damaged · Apr 19, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S4R FROM BS 360 THROUGH BS 540. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089713-14.
- [SDR DL73S040353](https://openairdocs.org/sdr/DL73S040353.md): Skin · damaged · Apr 19, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S4R FROM BS 727 THROUGH BS 908. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089712-14.
- [SDR DL73S040352](https://openairdocs.org/sdr/DL73S040352.md): Skin · damaged · Apr 19, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S14R FROM BS 360 THROUGH BS 540. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089710-14.
- [SDR DL73S040351](https://openairdocs.org/sdr/DL73S040351.md): Skin · damaged · Apr 19, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S4L FROM BS 727 THROUGH BS 908. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089708-14.
- [SDR DL73S040350](https://openairdocs.org/sdr/DL73S040350.md): Skin · damaged · Apr 19, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > SCRIBE MARKS WERE NOTED IN THE LOWER SKIN AT THE LAP SPLICE LOCATED AT S14L FROM BS 360 THROUGH BS 540. DAMAGE WAS REMOVED AND REPAIRED PER INSTRUCTIONS CONTAINED IN ERA 089703-14.
- [SDR DL73S040344](https://openairdocs.org/sdr/DL73S040344.md): Skin · damaged · Apr 16, 2004 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN LAP JOINTS AND BUTT JOINTS WERE FOUND WITH SEVERAL AREAS OF SCRIBE MARK DAMAGE IN THE PRESSURIZED FUSELAGE AREA BETWEEN FS 360 & 1016, IN THE UPPER PORTION BETWEEN STRINGERS 14L & 14R. THE DAMAGE LAP JOINTS ARE CUT AND REMOVED AND REPAIRED W
- [SDR DL73K021406](https://openairdocs.org/sdr/DL73K021406.md): Regulator Valve · leaking · Dec 3, 2002 · N244WA · Boeing 737247 · Pneumatic Distribution System
  > AIR TURNBACK FROM FLL TO BDL, RETURNED TO FLL. BLEED TRIP OFF NR 1 ENG ON TAKEOFF ROLL. REPLACED PRESSURE REGULATOR BLEED LINES FOR LEAKING.
- [SDR DL73K021178](https://openairdocs.org/sdr/DL73K021178.md): Gasper Fan · failed · Oct 8, 2002 · N244WA · Boeing 737247 · Air Distribution Fan
  > ON ARRIVAL PBI CREW OFF FLT 2309 REPORTED UNIDENTIFIABLE ODOR THROUGHOUT THE AIRCRAFT. AIRCRAFT WAS CARRYING HUMAN REMAINS, AND CREW SUSPECTED THIS TO BE THE SOURCE OF THE ODOR. BOTH MTC AND GROUND CREW INSPECTED CARGO COMPARTMENTS AND FOUND CLEAN. GRD CREW
- [SDR DL73K020234](https://openairdocs.org/sdr/DL73K020234.md): Smoke Detector · inoperative · Feb 26, 2002 · N244WA · Boeing 737247 · Smoke Detection
  > FORWARD LAVATORY SMOKE DETECTOR INOPERATIVE. REPLACED FORWARD LAVATORY SMOKE DETECTOR.
- [SDR DL73K020118](https://openairdocs.org/sdr/DL73K020118.md): Frame · cracked · Jan 30, 2002 · N244WA · Boeing 737247 · Fuselage Main, Frame
  > INSPECTION OF THE FS 178 BULKHEAD PER AD 2000-05-29, REVEALED A CRACK IN THE LT SIDE CHORD NEAR WL 207. THE DAMAGED SECTION OF CHORD WAS CUT OUT AND A NEW SECTION SPLICED IN. THE WORK WAS ACCOMPLISHED IN ACCORDANCE WITH BAC S/B 737-53A1173 AND ER/A 382503-14
- [SDR DL73K011956](https://openairdocs.org/sdr/DL73K011956.md): Apu · failed · Dec 19, 2001 · N244WA · Boeing 737247 · APU Core Engine
  > DURING TAXI OUT, APU DROPPED OFF LINE. TOWER CONFIRMED SMOKE AND FLAME COMING FROM APU AREA. CREW ACCOMPLISHED APU FIRE CHECKLIST. REPLACED APU AND APU FIRE BOTTLE.
- [SDR DL73K011320](https://openairdocs.org/sdr/DL73K011320.md): Hinge Pin · out of position · Aug 12, 2001 · N244WA · Boeing 737247 · Passenger/Crew Doors
  > PILOT REP - LOUD SQUEAL FROM L1 ENTRY DOOR UPPER HINGE AREA. FOUND UPPER HINGE/SEAL FLOATING BRACKET HINGE PIN OFF. REINSTALLED PIN AND HINGE. PRESS A/C TO 4.5 DIFF PRESS CKS OK
- [SDR DL73K011296](https://openairdocs.org/sdr/DL73K011296.md): Skin · cracked · Aug 5, 2001 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN WAS FOUND WITH A 1 INCH CRACK AT STRINGER 19L AT FS 767. THE CRACK WAS JUST ABOVE THE WAFFLE DOUBLER AT THE STRINGER. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL DOUBLER PER THE B737 SRM AND ER/A 381488-14.
- [SDR DL73K010539](https://openairdocs.org/sdr/DL73K010539.md): Skin · cracked · Apr 1, 2001 · N244WA · Boeing 737247 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WITH A 3 INCH CRACK JUST BELOW STRINGER 18 RT AT APPROXIMATELY FS 760. THE CRACK LOCATION WAS FWD OF AN EXISTING REPAIR FOR SIMILAR CRACKING. THE NEW CRACK WAS REMOVED WITH A 3 INCHES X 1.5 INCHES CUTOUT AND THE EXISTINGREPAIR REM
- [SDR DL73K010220](https://openairdocs.org/sdr/DL73K010220.md): Controller · failed · Feb 7, 2001 · N244WA · Boeing 737247 · Windshield/Door Rain/Ice Removal
  > DUE TO F/OS WINDSHIELD CRACKED IN FLT. REPLACED WINDSHIELD HEAT CONTROLLER, OPS CK OK.
- [SDR DL73K010215](https://openairdocs.org/sdr/DL73K010215.md): Window · cracked · Feb 7, 2001 · N244WA · Boeing 737247 · Flight Compartment Windows
  > FIRST OFFICERS FRONT WINDOW CRACKED AT FL 310. REMOVED AND REPLACED F/OS R-1 WINDOW AND WINDOW HEAT CONTROLLER.

Next page: https://openairdocs.org/deregistered/N244WA-2007-06-13/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 = 'N244WA' AND deregistration_id = 'N244WA-2007-06-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N244WA-2007-06-13/reports

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