# Service difficulty reports: N304DL, cancelled Jul 22, 2011

A list on [N304DL, cancelled Jul 22, 2011](https://openairdocs.org/deregistered/N304DL-2011-07-22.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR DL73S050593](https://openairdocs.org/sdr/DL73S050593.md): Tire · damaged · Sep 5, 2005 · N304DL · Boeing 737232 · Tire
  > ON WALK AROUND, FOUND NR 3 MAIN TIRE FAILURE CAUSING DAMAGE TO RT INBD FLAP AND RT GEAR INBD TRAILING EDGE FORE FLAP. CLOSE OUT PANEL. REPLACED TIRE AND REPAIRED DAMAGE.
- [SDR DL73S041136](https://openairdocs.org/sdr/DL73S041136.md): Adc · contaminated · Dec 24, 2004 · N304DL · Boeing 737232 · Air Data Computer
  > AFTER DE-ICING AUTOTHROTTLES DISARMED DURING T/O, NO RE-ENGAGE AT ACCEL PDC CADC FAIL MSG, MACH TRIM FAIL LIGHT. DURING CLIMB CAPTS A/S AND ALTM OFF MSG AFTER LVL OFF. AT FL 290 APPROX 5 MIN CABIN ALT WARN HORN DIFF PRESS 6 PSI, CABIN ALT 10K. FOLLOWED QRH
- [SDR DL73S041081](https://openairdocs.org/sdr/DL73S041081.md): Power Supply · inoperative · Dec 4, 2004 · N304DL · Boeing 737232 · Emergency Lighting
  > ON L/O CHECK, FOUND FWD CABIN EMERGENCY PATH LIGHTS INOP. REPLACED FWD CABIN EMERGENCY LIGHTS POWER SUPPLY. CHECKS GOOD.
- [SDR DL73S040372](https://openairdocs.org/sdr/DL73S040372.md): Bulkhead · cracked · Apr 23, 2004 · N304DL · Boeing 737232 · Fuselage Main, Bulkhead
  > INSPECTION OF THE AFT P-DOME WEB PER AD 99-08-23 REVEALED CRACKS IN THE WEB COMMON TO THE BULKHEAD Y-CHORD NEAR STRINGER 5R. THE CRACKED AREA OF WEB WAS REMOVED WITH A SINGLE CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER. THE REPAIR WAS ACCOMPLISHED PE
- [SDR DL73S040359](https://openairdocs.org/sdr/DL73S040359.md): Skin · cracked · Apr 17, 2004 · N304DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WITH A CRACK AT FS 727B+2 ALONG THE BONDED DOUBLER LINE JUST BELOW STRINGER 18L. THE CRACK IS TYPICAL OF BAC S/B 737-53-1065. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PE
- [SDR DL73S040346](https://openairdocs.org/sdr/DL73S040346.md): Skin · cracked · Apr 15, 2004 · N304DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > INSPECTION OF THE STRINGER 10R SKIN LAP JOINT FROM FS 360 TO 540 PER AD 2003-08-15, REVEALED A SINGLE CRACK AT FS 370. THE CRACK WAS REMOVED WITH A 1 X 4.25 INCH CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM 53-30-3 AND PER ER/A 0
- [SDR DL73S040345](https://openairdocs.org/sdr/DL73S040345.md): Skin · cracked · Apr 14, 2004 · N304DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > INSPECTION OF THE STRINGER 4L SKIN LAP JOINT BETWEEN FS 540 & 727 PER AD 2003-08-15, REVEALED 15 CRACK INDICATIONS. THE ENTIRE LAP JOINT WAS CUT OUT AND REPLACED WITH ALUMINUM REPAIR DOUBLERS PER BAC S/B 737-53A1177 AND ER/A 089523-14AD.
- [SDR DL73S040320](https://openairdocs.org/sdr/DL73S040320.md): Skin · cracked · Apr 7, 2004 · N304DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > INSPECTION OF THE STRINGER 4R SKIN LAP JOINT PER AD 2003-08-15, REVEALED A TOTAL OF 9 CRACKED FASTENER HOLES AT THREE LOCATIONS IN THE JOINT. THE CRACKS WERE REMOVED WITH CUTOUTS OF 15.5 X 1 INCH AND TWO CUTOUTS OF 7.25 X 1 INCH. THE CUTOUTS WERE REPAIRED WI
- [SDR DL73S040319](https://openairdocs.org/sdr/DL73S040319.md): Skin · cracked · Apr 7, 2004 · N304DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > INSPECTION OF THE STRINGER 10L LAP JOINT BETWEEN FS 360 & 540 REVEALED A CRACKED FASTENER HOLE AT FS 380. THE CRACKED HOLE WAS REMOVED WITH A 1 X 4 INCH CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER BAC 737 SRM 53-30-3, FIG 42. THE REPAIR
- [SDR DL73S040318](https://openairdocs.org/sdr/DL73S040318.md): Skin · cracked · Apr 7, 2004 · N304DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > INSPECTION OF THE STRINGER 14L SKIN LAP JOINT PER AD 2003- 08-15, REVEALED A CRACKED FASTENER HOLE AT FS 500A+10 & ANOTHER AT FS 500B+15. THE CRACKS WERE REMOVED WITH SKIN CUTOUTS (1 X 4 & 1 X 7 INCH RESPECTIVELY). THE CUTOUTS WERE REPAIRED WITH ALUMINUM DO
- [SDR DL73S040283](https://openairdocs.org/sdr/DL73S040283.md): Frame · corroded · Mar 30, 2004 · N304DL · Boeing 737232 · Fuselage Main, Frame
  > CORROSION ON AFT SIDE OF FORMER STA 827 O/B OF STR 27R. INSTALLED PERMANENT REPAIR PER SRM 53-10-4 FIG 6. COMPLETED AND SENT SSI DATA RETRIEVAL.
- [SDR DL73S031132](https://openairdocs.org/sdr/DL73S031132.md): Skin · dented · Dec 24, 2003 · N304DL · Boeing 737232 · Wing, Plate/Skin
  > DAMAGE FOUND ON LOWER SKIN PANEL OF RIGHT WING AT STA 525 NEAR OUTBOARD TIP. REPAIRED PER ERA 426849-14.
- [SDR DL73S030885](https://openairdocs.org/sdr/DL73S030885.md): Switch · broken · Sep 29, 2003 · N304DL · Boeing 737232 · Passenger Compartment Lighting
  > ELECTRICAL SMELL COMING FROM FWD FLIGHT ATTENDANT INTERPHONECOMM PANEL. FOUND CABIN SIDEWALL LIGHT SWITCH AT FWD F/A PANEL BROKEN AND SHORTING. REPLACED SWITCH, CHECKS OK.
- [SDR DL73S030643](https://openairdocs.org/sdr/DL73S030643.md): Engine · bird ingestion · Jul 14, 2003 · N304DL · Boeing 737232 · Engine (Turbine/Turboprop)
  > IRREG: ON T/O DETECTED SMELL IN COCKPIT AND CABIN. RETURN TO CVG. FOUND EVIDENCE OF BIRD STRIKE NR 1 ENG. INSP ENG AND ENG BLEED DUCTS. PERFORMED DUCT BURNOUT AND REPLD. WATER SEPARATOR BAGS.
- [SDR DL73S030431](https://openairdocs.org/sdr/DL73S030431.md): Valve · stuck · May 6, 2003 · N304DL · Boeing 737232 · Air Distribution System
  > IR: 20KFT CABIN ALTITUDE HORN WENT OFF.CBN ALT AT 11 KFT. STARTED DESCENT SWITCHED TO STBY CBN WOULD NOT PRESS. MANUAL MODE ALSO INOP. REPLACED E & E COOLING EXHAUST VALVE. ALSO FOUND LEFT ENGINE 450 DEG THERMOSTAT SENSE LINE BACKED OFF. TIGHTENED SAME,RAN
- [SDR DL73K020299](https://openairdocs.org/sdr/DL73K020299.md): Floorbeam · cracked · Mar 11, 2002 · N304DL · Boeing 737232 · Fuselage Main, Floor Beam
  > CENTER WING / LONGITUDINAL OVERWING FLOORBEAM / BL 24.82 / FS 678: CHORD AND WEB CRACK REPAIR INSPECTION OF THE LBL & RBL 24.82 LONGITUDINAL FLOORBEAMS PER AD 2001-17-18 REVEALED TYPICAL CRACKS IN THE BEAM WEB, WEB DOUBLER, AND UPPER CHORD AT FS 678 AT THE
- [SDR DL73K020271](https://openairdocs.org/sdr/DL73K020271.md): Bulkhead · cracked · Mar 7, 2002 · N304DL · Boeing 737232 · Fuselage Main, Bulkhead
  > INSPECTION OF THE FS 178 BULKHEAD PER AD 2000-05-29 REVEALED A SMALL CRACK IN THE LEFT SIDE CHORD AT WL 207 AND ANOTHER AT WL 195. THE LT CHORD WAS CUT AT WL 212 AND A NEW LOWER SECTION INSTALLED PER THE REQUIREMENTS OF BAC S/B 737-53A1173. THE WORK WAS DOCU
- [SDR DL73K020251](https://openairdocs.org/sdr/DL73K020251.md): Frame · cracked · Mar 4, 2002 · N304DL · Boeing 737232 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR WAS FOUND WITH CRACKED LOWER FOWARD AND AFT CORNER FRAMES, FORWARD AND AFT LOWER STOP BEAMS. REPAIRED.
- [SDR DL73K011361](https://openairdocs.org/sdr/DL73K011361.md): Flashlight · inoperative · Aug 19, 2001 · N304DL · Boeing 737232 · Emergency Equipment
  > DURING L/O FOUND EMERGENCY FLASHLIGHT AT AFT-LOWER STATION INOP.
- [SDR DL73K011204](https://openairdocs.org/sdr/DL73K011204.md): Skin · cracked · Jul 20, 2001 · N304DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > FUSELAGE / SKIN ASSY / AFT ENTRY DOOR (L2) / LWR FWD CORNER:CRACK REPAIR THE LOWER FORWARD CORNER OF THE AFT ENTRY DOOR CUTOUT WAS FOUND WITH A TYPICAL CRACK THROUGH THE SKIN AND UNDERLYING BEAR STRAP. THE CRA
- [SDR DL73K011199](https://openairdocs.org/sdr/DL73K011199.md): Skin · cracked · Jul 19, 2001 · N304DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN AT LOWER FORWARD CORNER OF L-2 DOOR CUTOUT WITH 0.75 INCH CRACK. ALSO FOUND BEARSTRAP AT THAT LOCATION WITH 1.5 INCH CRACK. REPAIRED PER SRM 53-30-3.
- [SDR DL73K010407](https://openairdocs.org/sdr/DL73K010407.md): Controller · failed · Mar 12, 2001 · N304DL · Boeing 737232 · Windshield/Door Rain/Ice Removal
  > ELECTRIAL CONNECTOR TO RIGHT FWD WINDOW BEGAN SMOKING, TURNED OFF WINDOW HEAT SMOKE STOPPED. / REPLACED R1 WINDOW AND WINDOW HEAT CONTROLLER PER M/M. OPNL TEST OF WINDOW HEAT GOOD
- [SDR DL73K001955](https://openairdocs.org/sdr/DL73K001955.md): Line · damaged · Oct 7, 2000 · N304DL · Boeing 737232 · Hydraulic System, Main
  > ENGINE HYD PUMP NR 2 PRESSURE LIGHT ON SYSTEM. REPLACED NR 2 ENGINE HYD PUMP AND HYD PRESS LINE. REPLACED FILTERS AND INSP A SYSTEM RETURN MODULE, ALL NORMAL. FLUSHED LINES, NO CONTAMINATION FOUND. RAN ENGINES, CHECKS NORMAL.
- [SDR DL73K001896](https://openairdocs.org/sdr/DL73K001896.md): Skin · cracked · Sep 27, 2000 · N304DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN AND BONDED DOUBLER WAS FOUND WITH A TYPICAL CRACK IN THE LOWER HINGE CUTOUT OF THE AFT GALLEY DOOR CUTOUT. THE CRACK WAS REMOVED WITH A 1 X 1.5 INCH CUTOUT. THE CUTOUT WAS LOCALLY REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND STEEL TRI
- [SDR DL73K001884](https://openairdocs.org/sdr/DL73K001884.md): Skin · cracked · Sep 26, 2000 · N304DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > A 4 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN NEAR FS 520 AND STRINGER 16L. THE SKIN WAS CUT OUT TO REMOVE THE CRACK. THE CUT OUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER. THE REPAIR WAS INSTALLED PER ER/A 378705-14.
- [SDR DL73K000897](https://openairdocs.org/sdr/DL73K000897.md): Attach Fitting · corroded · May 5, 2000 · N304DL · Boeing 737232 · Horizontal Stabilizer, Attach Fittings
  > THE HORIZONTAL STABILIZER REAR SPAR ATTACH LUGS WERE FOUND CORRODED. THE DAMAGE WAS REMOVED AND OVERSIZED BUSHINGS WERE INSTALLED PER ERA 334311-14 AT HMV.
- [SDR DL73K000896](https://openairdocs.org/sdr/DL73K000896.md): Fitting · corroded · May 5, 2000 · N304DL · Boeing 737232 · Fuselage, Landing Gear Attach Fittings
  > CORROSION WAS FOUND ON THE LHS MLG SIDE STRUT SUPPORT FITTING. THE BORE WAS OVERSIZED AND A BUSHING INSTALLED PER ERA 334372-14 AT HMV.
- [SDR DL73K000895](https://openairdocs.org/sdr/DL73K000895.md): Attach Fitting · corroded · May 5, 2000 · N304DL · Boeing 737232 · Fuselage Main, Attach Fittings
  > SEVERAL OF THE FIN ATTACHMENT LUGS WERE FOUND CORRODED AT THE AFT SPAR. THE CORROSION WAS REMOVED AND THE BUSHINGS WERE RE-MANUFACTURED PER ERA 334313-14 AT HMV.
- [SDR DL73K000894](https://openairdocs.org/sdr/DL73K000894.md): Stringer · cracked · May 5, 2000 · N304DL · Boeing 737232 · Fuselage Main, Longeron/Stringer
  > A 4 INCH CRACK WAS FOUND IN THE OUTBOARD SKIN FLANGE OF THE S27R KEEL CHORD AT FS 727A. THE EXISTING FACTORY SPLICE ANGLES WERE MODIFIED TO REPAIR THE DAMAGE PER ERA 334332-14 AT HMV.
- [SDR DL73K000893](https://openairdocs.org/sdr/DL73K000893.md): Bulkhead · cracked · May 5, 2000 · N304DL · Boeing 737232 · Fuselage Main, Bulkhead
  > THE WEB OF THE FS 178 BULKHEAD WAS FOUND CRACKED AT RBL 1 AND WL 190. THE CRACK WAS REMOVED BY A 1.0 X 2.0 CUTOUT AND A DOUBLER WAS INSTALLED PER ERA 334328-14.
- [SDR DL73K000892](https://openairdocs.org/sdr/DL73K000892.md): Stringer · cracked · May 5, 2000 · N304DL · Boeing 737232 · Fuselage Main, Longeron/Stringer
  > CRACKS WERE DISCOVERED ON THE WEB OF STR 18AL AT FS 727. ERA 334331-14 REPAIRS THE DAMAGE SIMILIARLY TO THAT OF S/B 737-53-1170. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL73K000891](https://openairdocs.org/sdr/DL73K000891.md): Frame · misinstalled · May 5, 2000 · N304DL · Boeing 737232 · Fuselage Main, Frame
  > THE FS 440 FRAME INSTALLATION DID NOT MATCH THE CONFIGURATION FOUND IN S/B 737-53-1125. THE S/B REQUIRES INSTALLATION OF.2187 INCH FASTENERS AND THE FACTORY INSTALLATION INSTALLS.25 INCH FASTENERS. ERA 334319-14 ADDRESSES THIS CONDITION AND INSTALLS
- [SDR DL73K000890](https://openairdocs.org/sdr/DL73K000890.md): Skin · cracked · May 5, 2000 · N304DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WITH A.375 INCH CRACK AT THE R2 DOOR UPPER HINGE CUTOUT. THE DAMAGE WAS LIMITED TO THE SKIN ONLY. THE DAMAGE WAS REPAIRED PER ERA 259665-14 AT HMV.
- [SDR DL73K000889](https://openairdocs.org/sdr/DL73K000889.md): Skin · corroded · May 5, 2000 · N304DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > CORROSION WAS FOUND ON THE FUSELAGE SKIN AT FS 967 BETWEEN STR 27L AND 27R. THE FRAME SHEAR TIE AND STR 27R WAS ALSO CORRODED AT THIS LOCATION. THE STRINGER WAS REPAIRED PER B737-200 SRM 53-10-3, FIGURE 1, THE FRAME SHEAR TIE REPLACED AND THE SKIN WAS REPA
- [SDR DL73K000860](https://openairdocs.org/sdr/DL73K000860.md): Floorbeam · cracked · Apr 27, 2000 · N304DL · Boeing 737232 · Fuselage Main, Floor Beam
  > CRACKING FOUND IN BL 0 LONGITUDINAL FLOORBEAM WEB AFT OF STA 717. RESULTED IN TRIMOUT OF BEAM WEB BETWEEN STA 700 AND 721. CORRECTIVE ACTION: ER/A 334337-14.
- [SDR DL73K000729](https://openairdocs.org/sdr/DL73K000729.md): Keelbeam · corroded · Apr 16, 2000 · N304DL · Boeing 737232 · Fuselage Main, Keel
  > THE LOWER SKIN OF THE KEEL BEAM WAS FOUND CORRODED BETWEEN FS 661 AND FS 727. THE SKIN PANEL WAS REMOVED AND REPLACED PER ERA 334318-14 AT HMV.
- [SDR DL73K991714](https://openairdocs.org/sdr/DL73K991714.md): Battery · discharged · Jul 31, 1999 · N304DL · Boeing 737232 · Emergency Lighting
  > EMERGENCY LIGHT AT 18D AND 2R DOOR ON. REPLACED CHARGER RACK AND BATTERY.
- [SDR DL73K990709](https://openairdocs.org/sdr/DL73K990709.md): Stringer · corroded · Mar 31, 1999 · N304DL · Boeing 737232 · Fuselage Main, Longeron/Stringer
  > STR 26R AT FS 978 CORRODED. REPAIRED PER SRM 53-10-3.
- [SDR DL73K990708](https://openairdocs.org/sdr/DL73K990708.md): Stringer · corroded · Mar 31, 1999 · N304DL · Boeing 737232 · Fuselage Main, Longeron/Stringer
  > STR 27 LT AT FS 988 CORRODED. REPAIRED PER SRM 53-10-3.
- [SDR DL73K990707](https://openairdocs.org/sdr/DL73K990707.md): Stringer · corroded · Mar 31, 1999 · N304DL · Boeing 737232 · Fuselage Main, Longeron/Stringer
  > STR 27 LT AT FS 948 CORRODED. REPAIRED PER SRM 53-10-3.
- [SDR DL73K990696](https://openairdocs.org/sdr/DL73K990696.md): Stringer · corroded · Mar 30, 1999 · N304DL · Boeing 737232 · Fuselage Main, Longeron/Stringer
  > STRINGER 27L FS 1006 HAD CORROSION. REPAIRED PER SRM 53-10-3 FIG 1.
- [SDR DL73K990077](https://openairdocs.org/sdr/DL73K990077.md): Wire · shorted · Jan 12, 1999 · N304DL · Boeing 737232 · Light System Wiring
  > LEFT AND RIGHT FWD DOORS EMERGENCY LIGHT EXIT IDENTIFIERS DO NOT ILLUMINATE WHEN TESTED. POWER SUPPLY FUSE BLOWN DUE TO LEFT LIGHT ASSY WIRE SHORTED. REPLACED FUSE IN POWER SUPPLY AND REPLACED LEFT LIGHT ASSY.
- [SDR DL73K981548](https://openairdocs.org/sdr/DL73K981548.md): Bulb · failed · Jul 24, 1998 · N304DL · Boeing 737232 · Emergency Lighting
  > R2 SLIDE LIGHT INOP. RELAMPED.
- [SDR DL73K971568](https://openairdocs.org/sdr/DL73K971568.md): Coalescer Bag · dirty · Aug 10, 1997 · N304DL · Boeing 737232 · Humidity Control System
  > UPON LIFTOFF NOTICED ACRID SMOKE SMELL AND CABIN FUMES, VERIFIED BY F/A'S. RETURNED FOR IMMEDIATE LANDING, OVERWEIGHT 110, BRAKE APPLICATION 90 KTS. INSPECTED AC FOR SOURCE OF SMELL, NO DEFECTS NOTED. PERFORMED T/O PWR RUN AND NOTICED LIGHT SMELL FROM RT EN
- [SDR DL73K970138](https://openairdocs.org/sdr/DL73K970138.md): Controls · stiff · Jan 23, 1997 · N304DL · Boeing 737232 · Aileron Control System
  > AILERONS STIFF, NO BINDING FELT BUT RESISTANCE TO CONTROL WHEEL MOVEMENT GREATER THAN NORMAL. REPLACED 'A' AND 'B' SYSTEMS RETURN FILTERS, CHECKED ROLL FORCE TRANSMITTER AND VISUALLY INSPECTED PULLEYS AND CABLES.
- [SDR DL73S962054](https://openairdocs.org/sdr/DL73S962054.md): Battery Pack · discharged · Sep 5, 1996 · N304DL · Boeing 737232 · Emergency Lighting
  > EMER EXIT LIGHTS ABOVE 1B AND 2C REMAINED ILLUM WITH SWITCH IN ARMED POSITION. REPLACED OVHD BATT PACK AND PWR SUPPLY CKS OK.
- [SDR DL73S960252](https://openairdocs.org/sdr/DL73S960252.md): Blkhd Web · cracked · Jan 30, 1996 · N304DL · Boeing 737232 · Fuselage Main, Bulkhead
  > REF. E.O. 03-069482-12 ME-04 OPN. 0445.1, 2 INCH CRACK AND 1 INCH CRACK IN BS 178 BULKHEAD WEB AT RT BL 5.7 INBOARD OF VERTICAL STIFFENER..50 INCH CRACK IN 178 BULKHEAD WEB AT RT BL 5.7 OUTBOARD OF VERTICAL STIFFENER. TWO.25 INCH CRACKS AND 1 INCH CRACK IN
- [SDR DL73S953421](https://openairdocs.org/sdr/DL73S953421.md): Floor Beam · cracked · Aug 10, 1995 · N304DL · Boeing 737232 · Wing, Center Box
  > THE BL0.07 FLOOR BEAM OF THE WING CENTER SECTION IS COMPLETELY CRACKED. THE WEB AND WEB DOUBLER ARE CRACKED APPROXIMATELY 2.0 INCHES IN LENGTH IN THE SAME LOCATION. THE ORIGINAL 65-45410-104 ANGLE IS REINSTALLED TO REPAIR DAMAGE. REPAIRS ACCOMPLISHED PER DL

## 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 = 'N304DL' AND deregistration_id = 'N304DL-2011-07-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N304DL-2011-07-22/reports

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