# Service difficulty reports: N605DL, cancelled Nov 7, 2022

A list on [N605DL, cancelled Nov 7, 2022](https://openairdocs.org/deregistered/N605DL-2022-11-07.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 · 86 reports

- [SDR IXXA20190329888](https://openairdocs.org/sdr/IXXA20190329888.md): Battery · discharged · Mar 26, 2019 · N605DL · Boeing 757232 · Emergency Equipment
  > JUMPSEAT FLASHLIGHT BATTERY DEAD. REMOVED AND REPLACED BATTERY FLASHLIGHT IAW AMM 25-64-00. OPERATIONAL CHECK SATISFACTORY.
- [SDR IXXA20171031321](https://openairdocs.org/sdr/IXXA20171031321.md): Battery Pack · discharged · Oct 30, 2017 · N605DL · Boeing 757232 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS EGRESS INOP. REMOVED AND REPLACED EGRESS BATTERY PACK. SYSTEMS OPERATIONAL CHECK SATISFACTORY. NO FURTHER DEFECTS NOTED. AIRCRAFT RELEASED TO SERVICE.
- [SDR IXXA20170131015](https://openairdocs.org/sdr/IXXA20170131015.md): Stringer · corroded · Jan 21, 2017 · N605DL · Boeing 757232 · Fuselage Main, Longeron/Stringer
  > STRINGER 29L BETWEEN BS 1400 - 1410 HAS SEVERAL SPOTS OF CORROSION. REPAIRED THE STRINGER IAW SRM 53-60-12, REPAIR 1, FIGURE 201.
- [SDR IXXA20170131011](https://openairdocs.org/sdr/IXXA20170131011.md): Stringer · corroded · Jan 17, 2017 · N605DL · Boeing 757232 · Fuselage Main, Longeron/Stringer
  > AFT EXTERNAL FUSELAGE AT BS 1455, STRINGER 29L HAS PULLED RIVETS AND EVIDENCE OF CORROSION. REMOVED AND REPLACED THE STRINGER IAW REA 47247FAB01 AND SRM 53-00-03 FIGURE 201 DETAIL 11.
- [SDR IXXA20170131009](https://openairdocs.org/sdr/IXXA20170131009.md): Attach Bracket · cracked · Jan 17, 2017 · N605DL · Boeing 757232 · Fuselage Main, Attach Fittings
  > BRACKET CRACKED ON FORWARD SIDE OF COOLING FANS JUST AFT OF AND BELOW OUTFLOW VALVE. REMOVED AND REPLACED COOL FAN ATTACH BRACKET P/N 214N3057-3 USING 2024-T3.080. P.O. #0089089 IN ACCORDANCE WITH BOEING DRAWING 214N3057 AND B757 SRM 51-40-02 PARAGRAPH 7.
- [SDR IXXA20170123007](https://openairdocs.org/sdr/IXXA20170123007.md): Skin · cracked · Jan 17, 2017 · N605DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. SKIN CRACKED AT STATION 1641 APPROXIMATELY 2" FROM RIVET HEAD TO FORWARD UPPER CORNER OF OUTFLOW VALVE CUTOUT. REPAIRED DAMAGED SKIN AND INTERNAL DOUBLER IN ACCORDANCE WITH ENGINEERING DOCUMENT REA 47247REA04.
- [SDR IXXA20170131013](https://openairdocs.org/sdr/IXXA20170131013.md): Shear Tie · corroded · Jan 16, 2017 · N605DL · Boeing 757232 · Fuselage Internal Mounting Structure
  > SHEAR TIE CORRODED AT BS 1640 STRINGER 22 - 23L. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-40-02 PARAGRAPH 4 AND 7, DRAWING 146N8711 AND ENGINEERING DOCUMENT 47247REA04.
- [SDR IXXA20170131012](https://openairdocs.org/sdr/IXXA20170131012.md): Shear Tie · corroded · Jan 16, 2017 · N605DL · Boeing 757232 · Fuselage Internal Mounting Structure
  > SHEAR TIE CORRODED AT BS 1640 STRINGER 23-24L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02 PARAGRAPH 4 & 7, DRAWING 146N8711 AND ENGINEERING DOCUMENT REA47247REA04.
- [SDR IXXA20170131010](https://openairdocs.org/sdr/IXXA20170131010.md): Shear Tie · cracked · Jan 16, 2017 · N605DL · Boeing 757232 · Fuselage Internal Mounting Structure
  > SHEAR TIE CRACKED STATION 1640 BETWEEN STRINGER 24L - 25L. FOUND DURING EDDY CURRENT HOLE SCAN. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02 PARAGRAPH 4 AND 7, DRAWING 140N7002 AND ENGINEERING DOCUMENT 7247REA04.
- [SDR IXXA20170127008](https://openairdocs.org/sdr/IXXA20170127008.md): Skin · deformed · Jan 9, 2017 · N605DL · Boeing 757232 · Fuselage Main, Plate/Skin
  > SKIN PANEL FORWARD OF RT WINDSCREEN JUST AFT OF RADOME HAS PREVIOUS DEFORMATION WITH INTERIM REMEDY. REPAIRED DEFORMED SKIN IAW REA 47247REA03.
- [SDR IXXA20151008116](https://openairdocs.org/sdr/IXXA20151008116.md): Bushing · worn · Oct 8, 2015 · N605DL · Boeing 757232 · Passenger/Crew Doors
  > MAIN ENTRY DOOR SAGGING AT TOP & STRIKING. NR 1 ROLLER LOCK APPEARS OUT OF ADJUSTMENT. FOUND SWING ARM BUSHING & BOLTS WORN & OUT OF RIG. R & R SWING ARM BUSHINGS & BOLTS IAW PRECISION MM 52-12-00. PERFORMED PRESS CHECK OF ACFT AMM 21-31-00. SYSTEMS CHECK
- [SDR IXXA20150518081](https://openairdocs.org/sdr/IXXA20150518081.md): Stop Fitting · misaligned · May 16, 2015 · N605DL · Boeing 757232 · Passenger/Crew Doors
  > UPPER LATCH ROLLER STOP ON L1 DOOR MISALIGNED. REALIGNED L1 DOOR UPPER LATCH ROLLER STOP IAW AMM 52-11-00. OPERATIONAL CHECKED SATISFACTORY. NO FURTHER DEFECTS NOTED. ACFT RELEASED TO SERVICE.
- [SDR FOTR20150307049](https://openairdocs.org/sdr/FOTR20150307049.md): Crease Beam · corroded · Mar 7, 2015 · N605DL · Boeing 757232 · Fuselage Main, Structure
  > MAIN CABIN STA 1580-1622, RBL 62 CREASE BEAM HAS CORROSION. REPAIRED ON FAS NR66383, W/O N605DL-01-01.
- [SDR FOTR20150307048](https://openairdocs.org/sdr/FOTR20150307048.md): Stringer · corroded · Mar 7, 2015 · N605DL · Boeing 757232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO STRINGER 18L HAS CORROSION, STA 1695. REPAIRED ON FAS NR 66474, W/O N605DL-01-01.
- [SDR FOTR20150306047](https://openairdocs.org/sdr/FOTR20150306047.md): Stringer Clip · corroded · Mar 6, 2015 · N605DL · Boeing 757232 · Fuselage Main, Attach Fittings
  > AFT CARGO BS 1320, STRINGER CLIP HAS CORROSION S26L. REPLACED ON FAS NR 66486, W/O N605DL.
- [SDR FOTR20150303047](https://openairdocs.org/sdr/FOTR20150303047.md): Stringer · corroded · Mar 3, 2015 · N605DL · Boeing 757232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO S26L HAS CORROSION STA 1370. REPAIRED ON FAS NR 66482, W/O N605DL-01-01.
- [SDR FOTR20150303046](https://openairdocs.org/sdr/FOTR20150303046.md): Stringer Clip · corroded · Mar 3, 2015 · N605DL · Boeing 757232 · Fuselage Main, Attach Fittings
  > AFT CARGO STA 1340, STRINGER CLIP HAS CORROSION S26L. REPLACED ON FAS NR 66483, W/O N605DL-01-01.
- [SDR FOTR20150303045](https://openairdocs.org/sdr/FOTR20150303045.md): Stringer · corroded · Mar 3, 2015 · N605DL · Boeing 757232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO STA 1335 S26L HAS CORROSION. REPAIRED ON FAS NR 66485, W/O N605DL-01-01.
- [SDR FOTR20150303044](https://openairdocs.org/sdr/FOTR20150303044.md): Shear Tie · corroded · Mar 3, 2015 · N605DL · Boeing 757232 · Fuselage Internal Mounting Structure
  > AFT CARGO STA 1300, LBL8 SHEAR TIE HAS CORROSION, REPLACED ON FAS NR 66435, W/O N605DL-01-01.
- [SDR FOTR20150303043](https://openairdocs.org/sdr/FOTR20150303043.md): Frame · corroded · Mar 3, 2015 · N605DL · Boeing 757232 · Fuselage Main, Frame
  > AFT CARGO STA 1520 FRAME HAS CORRSION BETWEEN S27R AND S27L. REPLACED ON FAS NR 66455, W/O N605DL-01-01.
- [SDR FOTR20150303042](https://openairdocs.org/sdr/FOTR20150303042.md): Shear Tie · corroded · Mar 3, 2015 · N605DL · Boeing 757232 · Fuselage Internal Mounting Structure
  > AFT CARGO COMPARTMENT, STA 1300, FRAME SHEAR TIE CORRODED NEAR STRINGER 28L. REPLACED ON FAS NR 66740, W/O N605DL-01-01.
- [SDR FOTR20150221041](https://openairdocs.org/sdr/FOTR20150221041.md): Keelbeam · corroded · Feb 21, 2015 · N605DL · Boeing 757232 · Fuselage Main, Keel
  > RT W/W KEEL BEAM HAS CORROSION ON CHORD IN AFT INBD CORNER STA 1140-1180 BL0. REPAIRED ON FAS NR 66172, W/O N605DL-01-01.
- [SDR FOTR20150221040](https://openairdocs.org/sdr/FOTR20150221040.md): Seat Track · corroded · Feb 21, 2015 · N605DL · Boeing 757232 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK, LBL 45, BS 1075-1180, HAS NUMEROUS LOCATIONS OF GOUGES AND CORROSION. REPLACED.
- [SDR FOTR20150221039](https://openairdocs.org/sdr/FOTR20150221039.md): Seat Track · damaged · Feb 21, 2015 · N605DL · Boeing 757232 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK, RBL 45 BS 900-1080, HAS NUMEROUS LOCATIONS OF GOUGES AND CORROSION. REPLACED.
- [SDR FOTR20150216038](https://openairdocs.org/sdr/FOTR20150216038.md): Seat Track · failed · Feb 16, 2015 · N605DL · Boeing 757232 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN BS 1320, RBL 48 SEAT TRACK HAS CORROSION. REPAIRED ON FAS NR 66387, W/O N605DL-01-01.
- [SDR FOTR20150216037](https://openairdocs.org/sdr/FOTR20150216037.md): Seat Track · failed · Feb 16, 2015 · N605DL · Boeing 757232 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK, RBL 45, BS 1080-1180, HAS NUMEROUS LOCATIONS OF GOUGES AND CORROSION. REPLACED ON FAS NR 66736, W/O N605DL-01-01.
- [SDR FOTR20150212036](https://openairdocs.org/sdr/FOTR20150212036.md): Seat Track · corroded · Feb 12, 2015 · N605DL · Boeing 757232 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK, RBL 25, STA 1075-1180 HAS NUMEROUS LOCATIONS OF GOUGES AND CORROSION. REPLACED ON FAS NR 66737, W/O N605DL-01-01.
- [SDR FOTR20150209035](https://openairdocs.org/sdr/FOTR20150209035.md): Seat Track · cracked · Feb 9, 2015 · N605DL · Boeing 757232 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CRACK SEAT TRACK AT RBL 24 AND BS 640 IN FWD CARGO COMPARTMENT. VIEW LOOKING UP IN FWD CARGO, REPLACED ON FAS NR 66622, W/O N605DL-01-01.
- [SDR FOTR20150209034](https://openairdocs.org/sdr/FOTR20150209034.md): Shear Tie · corroded · Feb 9, 2015 · N605DL · Boeing 757232 · Fuselage Internal Mounting Structure
  > AFT CARGO BS 1360, LBL8 SHEAR TIE HAS CORROSION. REPLACED ON FAS NR 66439, W/O N605DL-01-01.
- [SDR FOTR20150203033](https://openairdocs.org/sdr/FOTR20150203033.md): Shear Tie · corroded · Feb 3, 2015 · N605DL · Boeing 757232 · Fuselage Internal Mounting Structure
  > AFT CARGO BS 1460 AT S23R SHEAR TIE HAS CORROSION. THE SHEAR TIE WAS REPLACED.
- [SDR FOTR20150203032](https://openairdocs.org/sdr/FOTR20150203032.md): Shear Tie · cracked · Feb 3, 2015 · N605DL · Boeing 757232 · Fuselage Internal Mounting Structure
  > MAIN CABIN BS 1480 SHEAR TIE CRACKED AT S14L. THE SHEAR TIE WAS REPLACED.
- [SDR FOTR20150203031](https://openairdocs.org/sdr/FOTR20150203031.md): Shear Tie · cracked · Feb 3, 2015 · N605DL · Boeing 757232 · Fuselage Internal Mounting Structure
  > MAIN CABIN BS 1520, SHEAR TIE CRACKED AT STR 14L.
- [SDR FOTR20150203030](https://openairdocs.org/sdr/FOTR20150203030.md): Seat Track · corroded · Feb 3, 2015 · N605DL · Boeing 757232 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK HAS CORROSION RBL 48, BS 1538. THE SEAT TRACK WAS REPLACED.
- [SDR FOTR20150203029](https://openairdocs.org/sdr/FOTR20150203029.md): Seat Track · corroded · Feb 3, 2015 · N605DL · Boeing 757232 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK HAS CORROSION, BS 1180-1200, RBL 48. THE SEAT TRACK WAS REPLACED.
- [SDR FOTR20150203028](https://openairdocs.org/sdr/FOTR20150203028.md): Seat Track · corroded · Feb 3, 2015 · N605DL · Boeing 757232 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK HAS CORROSION BS 1180 - 1200, LBL 48. THE SEAT TRACK WAS REPLACED.
- [SDR IXXA20130823030](https://openairdocs.org/sdr/IXXA20130823030.md): Unknown · unknown · Aug 23, 2013 · N605DL · Boeing 7572Y0 · Cabin Pressure Control System
  > DURING CRUISE, AT FL370, CABIN ALTITUDE BEGAN TO CLIMB AT 800 FT PER MINUTE. SLOWED CLIMB RATE USING MANUAL. DESCENDED TO FL 330, CABIN ALTITUDE STABILIZED AND HELD IN AUTO. PRESSURIZED ACFT ON GROUND WITH NO LEAKS NOTED. SWAPPED POSITIONS OF THE NR 1 AND N
- [SDR IXXA20130822029](https://openairdocs.org/sdr/IXXA20130822029.md): Seal · leaking · Aug 22, 2013 · N605DL · Boeing 757232 · Cargo/Baggage Doors
  > DURING CRUISE AT FL 390, MAIN DECK CARGO DOOR DEVELOPED A SQUEAL AND CABIN ALTITUDE BEGAN TO CLIMB. DESCENDED TO FL 330, DOOR STILL SQUEALED BUT CABIN ALTITUDE STABILIZED. PRESSURIZED ACFT TO 7 PSI DIFFERENTIAL AND FOUND SEAL ON MAIN CARGO DOOR LEAKING WHE
- [SDR IXXA20130718042](https://openairdocs.org/sdr/IXXA20130718042.md): Frame · corroded · Jul 18, 2013 · N605DL · Boeing 7572Y0 · Fuselage Main, Frame
  > TOP FLANGE OF FRAME IS CORRODED AT BS 1460 BETWEEN S26-27R. REPAIRED FRAME IAW SRM 53-00-07, REPAIR NR 5.
- [SDR IXXA20130718041](https://openairdocs.org/sdr/IXXA20130718041.md): Angle · cracked · Jul 18, 2013 · N605DL · Boeing 757232 · Fuselage Main, Structure
  > TWO CRACKS IN THE INNER ANGLE OF THE AFT LOWER CARGO DOOR JAMB AT BS 1440 BY THE NR 6 DOOR STOP. FABRICATED THE CHORD SPLICE SECTION FROM 7075-T6511 EXTRUSION. ANNEAL AND FORM THE REPAIR SPLICE TO CONTOUR AND HEAT TREAT TO T-6. FABRICATED REPAIR WEB FROM 707
- [SDR IXXA20130718040](https://openairdocs.org/sdr/IXXA20130718040.md): Floorbeam · corroded · Jul 18, 2013 · N605DL · Boeing 7572Y0 · Fuselage Main, Floor Beam
  > FLOORBEAM HAS CORROSION AROUND MULTIPLE FASTENER HOLES AT BS 1020 LBL 24.5 TO 45.5. REMOVED CORROSION FROM UPPER FLANGE AND FOUND TO BE OUT OF LIMITS. FABRICATED TWO REPAIR DOUBLERS IAW SRM 51-70-11, FIG 1 & DWG 114N5080. FABRICATED TWO FILLERS IAW SRM 51-7
- [SDR IXXA20130718039](https://openairdocs.org/sdr/IXXA20130718039.md): Cover Plate · corroded · Jul 18, 2013 · N605DL · Boeing 7572Y0 · Fuselage Miscellaneous Structure
  > CORROSION WAS DISCOVERED ON THE COVER PLATE COMMON TO A HAT SECTION INTERCOSTAL MEMBER AT BS 1020, LBL 0 TO LBL 24.5. CORROSION REMOVAL RENDERED THE COVER PLATE UNSERVICEABLE. FABRICATED COVER PLATE. CORROSION PROTECT AND APPLY SURFACE FINISH TO FABRICATED C
- [SDR IXXA20130718038](https://openairdocs.org/sdr/IXXA20130718038.md): Attach Angle · corroded · Jul 18, 2013 · N605DL · Boeing 757232 · Horizontal Stabilizer Structure
  > HORIZONTAL STABILIZER T/E PANEL ATTACHING FLANGE IS CORRODED IN SEVERAL AREAS BETWEEN THE RT STABILIZER STA 96 TO 200. REMOVED AREAS OF CORROSION FROM UPPER BEAM CAP IAW SRM 55-10-13, DETAIL II. PERFORMED HFEC INSPECTION OF THE BLENDED SURFACES IAW NDTM.
- [SDR IXXA20130718037](https://openairdocs.org/sdr/IXXA20130718037.md): Angle · corroded · Jul 18, 2013 · N605DL · Boeing 757232 · Horizontal Stabilizer Structure
  > CORROSION WAS FOUND ON THE UPPER CHORD OF THE HORIZONTAL STABILIZER ON RIB NR 5 STA 128. DAMAGE WAS BLENDED TO A MAX OF.015" DEEP AND WAS BEYOND SRM LIMITS. REPAIRED DAMAGE IAW SRM 51-70-12.
- [SDR IXXA20130718036](https://openairdocs.org/sdr/IXXA20130718036.md): Seat Track · cracked · Jul 18, 2013 · N605DL · Boeing 757232 · Fuselage, Seat/Cargo Attach Fittings
  > F/O FORWARD OTBD SEAT TRACK CRACKED 0.50" AT FORWARD STOP. R & R F/O FORWARD OTBD SEAT TRACK IAW AMM 20-11-00.
- [SDR IXXA130718ILN035S](https://openairdocs.org/sdr/IXXA130718ILN035S.md): Attach Angle · corroded · Jul 18, 2013 · N605DL · Boeing 757232 · Horizontal Stabilizer Structure
  > HORIZONTAL STABILIZER T/E PANEL ATTACHING FLANGE IS CORRODED AT THE RT STABILIZER STA 104. BLENDED, TREATED AND PAINTED CORROSION AREAS. REMOVED AND REINSTALLED T/E PANELS ON RT HORIZONTAL STABILIZER UPPER SURFACE IAW SRM 51-40-02.
- [SDR IXXA20130529020O](https://openairdocs.org/sdr/IXXA20130529020O.md): Safety Valve · inoperative · May 29, 2013 · N605DL · Boeing 757232 · Landing Gear Retraction/Extension System
  > EICAS MESSAGE "GEAR DOOR" AND RT MLG DOOR OPEN UPON TAXI IN. DURING TROUBLESHOOTING THE RT GEAR DOOR WILL NOT FULLY CLOSE USING THE COCKPIT GEAR HANDLE OR THE SECONDARY SWITCH ON THE FUSELAGE. THE LT MLG DOOR AND THE NLG DOOR BOTH FUNCTION CORRECTLY. R & R
- [SDR IXXA20130514018O](https://openairdocs.org/sdr/IXXA20130514018O.md): Actuator · malfunctioned · May 14, 2013 · N605DL · Boeing 7572Y0 · Landing Gear Door Actuator
  > EICAS MESSAGE GEAR DOOR DISPLAYED AND DOORS AMBER LIGHT ON WITH LANDING GEAR INDICATING DOWN. ACCOMPLISHED FIM PROCEDURE 32-30 FAULT TREE 803. R & R THE RT MLG DOOR ACTUATOR IAW AMM 32-32-12. THE RT MLG DOOR SEQUENCE VALVE IAW AMM 32-32-05, AND THE RT MLG
- [SDR IXXA20130509017O](https://openairdocs.org/sdr/IXXA20130509017O.md): Warning Light · false activation · May 9, 2013 · N605DL · Boeing 757232 · Landing Gear Position and Warning
  > EXTENSION AND RETRACTION: EICAS MESSAGE GEAR DOOR DISPLAYED AND DOORS AMBER LIGHT ON WITH LANDING GEAR INDICATING DOWN. CYCLED MAIN GEAR DOORS IAW AMM 32-12-00. NO EICAS MESSAGE PRESENT. MAIN GEAR DOORS OPERATE NORMALLY. NO DEFECTS NOTED.
- [SDR IXXA20130501013O](https://openairdocs.org/sdr/IXXA20130501013O.md): Warning Light · false activation · May 1, 2013 · N605DL · Boeing 757232 · Landing Gear Position and Warning
  > EXTENSION AND RETRACTION EICAS MESSAGE GEAR DOOR DISPLAYED AND DOORS AMBER LIGHT ON WITH LANDING GEAR INDICATING DOWN. RT GEAR DOOR ONLY. CYCLED MAIN GEAR DOORS IAW AMM 32-12-00. NO EICAS MESSAGE PRESENT. MAIN GEAR DOORS OPERATE NORMALLY ON THE GROUND. NO
- [SDR IXXA20130312005](https://openairdocs.org/sdr/IXXA20130312005.md): Sensor · loose · Mar 12, 2013 · N605DL · Boeing 7572Y0 · Door Warning System
  > MAIN CARGO DOOR INDICATOR LIGHT ILLUMINATED ABOVE FLIGHT LEVEL 390. COMPLETED QRH CHECKLIST AND DESCENDED TO FL350. LIGHT WENT OUT. FOUND AFT LOCK SENSOR LOOSE. SECURED SENSOR AND OPS CHECK OF DOOR INDICATION IAW PRECISION CONTROLS MM 52-50-00. CYCLED DOOR

Next page: https://openairdocs.org/deregistered/N605DL-2022-11-07/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 = 'N605DL' AND deregistration_id = 'N605DL-2022-11-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N605DL-2022-11-07/reports

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