# Service difficulty reports: N783CA, cancelled Aug 16, 2022

A list on [N783CA, cancelled Aug 16, 2022](https://openairdocs.org/deregistered/N783CA-2022-08-16.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 4 · 156 reports

- [SDR ASOA2018122875361](https://openairdocs.org/sdr/ASOA2018122875361.md): Floor Support · corroded · Dec 27, 2018 · N783CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/H CABIN FLOOR SILL AND DOUBLER HAS CORROSION FS 449.85 TO 559.00(10 LOCATIONS).C/A:REPAIRED CORROSION L/H SILL AND DOUBLER (10 LOCATIONS) I.A.W BOMBARDIER REO 601R-53-41-666 REV C, DATED 2012-11-06 AND EXPRESSJET EC/TC REO 601R-53-41-666 REV. E AND EXPRESSJE
- [SDR ASOA2018110855315](https://openairdocs.org/sdr/ASOA2018110855315.md): Floor Support · corroded · Nov 5, 2018 · N783CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > REF: CO# 7315618 JOB# 7731568 OP# 35: R/H CABIN FLOOR SILL DOUBLER AND FLOOR SILL HAS CORROSION IN MULTIPLE AREAS FROM F.S. 409+128 TO F.S. 559.00. C/A: REPAIRED DAMAGE I.A.W. EXPRESSJET EC/TC REP 601R-53-41-666 REV.E, DATED 2013-10-23, EXPRESSJET EC/TC REO 60
- [SDR ASOA2018110835314](https://openairdocs.org/sdr/ASOA2018110835314.md): Former · cracked · Nov 3, 2018 · N783CA · Cndair CL6002B19 · Passenger/Crew Doors
  > REF: CO#7579618 JOB#7757961 OP#147 FOUND PAX DOOR AFT INNER FORMER TO BE CRACKED FOUND FWD INNER FORMER TO BE CRACKED. C/A:REPAIRED PAX DOOR FWD AND AFT INNER FORMER IAW CARD# REO 601R-52-11-2635 AND 601R-52-11-402.
- [SDR ASOA201811085313](https://openairdocs.org/sdr/ASOA201811085313.md): Bulkhead · cracked · Oct 31, 2018 · N783CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REF: CO# 7315618 JOB# 7731565 OP# 10: F.S.621 REAR PRESSURE BULKHEAD HAS 8 AREAS THAT FAILED THE NDT INSPECTION.C/A:REPAIRED F.S.621 REAR PRESSURE BULKHEAD IAW BOMBARDIER REO 601R-53-61-1240.
- [SDR ASOA201810285294](https://openairdocs.org/sdr/ASOA201810285294.md): Post · damaged · Oct 29, 2018 · N783CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INBOARD VERTICAL POST AT FS409+128, LBL18, FOUND DAMAGE ON THE 2ND TO THE BOTTOM HOLE. COMPLIED WITH EC/TC REO 601R-53-41-889 AND REO 601R-53-41-889, REV C, DATED 2018-01-03.
- [SDR ASOA201810285295](https://openairdocs.org/sdr/ASOA201810285295.md): Post · damaged · Oct 28, 2018 · N783CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INBOARD VERTICAL POST AT FS409+128, LBL18, FOUND DAMAGE ON THE 2ND TO THE BOTTOM HOLE. COMPLIED WITH EC/TC REO 601R-53-41-2384 AND REO 601R-53-41-2384, DATED 2018-10-19.
- [SDR ASOA201810205303](https://openairdocs.org/sdr/ASOA201810205303.md): Intercostal · corroded · Oct 20, 2018 · N783CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STRINGER 26R BETWEEN FS349 AND FS364 IS CORRODED. REPAIRED IAW EA30-2018-226.
- [SDR ASOA201810205291](https://openairdocs.org/sdr/ASOA201810205291.md): Skin · dented · Oct 20, 2018 · N783CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT ON FUSELAGE LT SIDE BELOW NR 2 AND NR 3 WINDOWS AT WL60. REPAIRED IAW SRM 53-00-31 REPAIR 8 FIGURE 203. FS 409.00+9.0 TO FS 409.00+16 BETWEEN STRINGERS 20L AND 21L. THIS REPAIR HAS SDIR REQUIREMENTS AS STATED IN SRM 53-00-31 PAGES 201 AND 203.
- [SDR ASOA201810205283](https://openairdocs.org/sdr/ASOA201810205283.md): Skin · corroded · Oct 20, 2018 · N783CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AREA OF LIGHT CORROSION UNDER NR 2 DME ANTENNA. REPAIRED CORROSION UNDER NR 2 DME ANTENNA IAW STS EA 32-2018-200 AND EA 32-2018-200.
- [SDR ASOA201810205282](https://openairdocs.org/sdr/ASOA201810205282.md): Skin · dented · Oct 20, 2018 · N783CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT ON FUSELAGE LT SIDE BELOW NR 2 AND NR 3 WINDOWS AT WL60. REPAIRED IAW SRM 53-00-31. REPAIR 8 FIGURE 203 FS 409.00+9.0 TO FS 409.00+16 BETWEEN STR 20L AND 21L.
- [SDR ASOA2018122095351](https://openairdocs.org/sdr/ASOA2018122095351.md): Hinge · gouged · Oct 19, 2018 · N783CA · Cndair CL6002B19 · Fuselage, Door Hinge
  > REF: CO# 7315618 JOB# 7731561 OP# 101: PAX DOOR HINGE ON FUSELAGE SIDE IS GOUGED FROM MIGRATED ROLL PIN. C/A: BLENDED DAMAGE IAW ECTC REO 601R-53-21-814 TYPE IV REPAIR.
- [SDR ASOA2018102595278](https://openairdocs.org/sdr/ASOA2018102595278.md): Skin · chafed · Oct 19, 2018 · N783CA · Cndair CL6002B19 · Wing, Plate/Skin
  > REF: CO 7315618 JOB 7731561 OP 44 CENTER WING LOWER SKIN CHAFED AT LWS 45.00, RWS 45.0 FS 499.00. C/A: REPAIRED IAW REO 601R-57-21-880 REV. D AND EC/TC REO601R-57-21-880.
- [SDR ASOA2018102595277](https://openairdocs.org/sdr/ASOA2018102595277.md): Intercostal · corroded · Oct 19, 2018 · N783CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > REF: CO 7315618 JOB 7731568 OP 10 INTERCOSTAL FS 349.00 TO 364.00 AT STRINGER 26L IS CORRODED. C/A:REMOVED AND INSTALLED A NEW SERVICABLE INTERCOSTAL P/N 601R31049-119 IAW SRM 51-40-11, 51-42-06, AND 51-42-21.
- [SDR ASOA201810185276](https://openairdocs.org/sdr/ASOA201810185276.md): Skin · corroded · Oct 18, 2018 · N783CA · Cndair CL6002B19 · Wing, Plate/Skin
  > WING PLANK HOLES HAVE PITTING CORROSION. REPAIRED WING PLANK ACCESS HOLE 640BB IAW REO 601R-57-21-030 REV L AND EC/TC EO600-57-81 REV K.
- [SDR ASOA2018102485275](https://openairdocs.org/sdr/ASOA2018102485275.md): Rib · corroded · Oct 18, 2018 · N783CA · Cndair CL6002B19 · Rudder, Spar/Rib
  > REF: CO 7315618 JOB 7731568 OP 36: RUDDER BOTTOM RIB P/N 600-22032 HAS EVIDENCE OF CORROSION. C/A:REPAIRED DAMAGE IAW SRM 51-21-06, 55-40-00, 51-25-01, STS EA 32-2018-208 AND EC/TC EA 32-2018-208 WO#559076.
- [SDR ASOA2018102465274](https://openairdocs.org/sdr/ASOA2018102465274.md): Frame · corroded · Oct 16, 2018 · N783CA · Cndair CL6002B19 · Fuselage Main, Frame
  > REF: CO 7315618 JOB 7731568 OP 28: FRAME 333.00 IS CORRODED ON THE FLANGE AT STRINGER 26L. C/A:REMOVED AND REPLACED FRAME AT F.S. 333.00 IAW SRM 51-42-06, 51-42-21, 51-40-11 AND SRM TR51-42.
- [SDR ASOA2018110845312](https://openairdocs.org/sdr/ASOA2018110845312.md): Angle · corroded · Oct 14, 2018 · N783CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > REF: CO#7579618 JOB#7757968 OP#32 F.S. 280 J-ANGLE IS CORRODED.C/A REMOVED UNSERVICABLE ANGLE, LOCATED AND DRILLED NEW SERVICEABLE ANGLE IAW CRJ200 SRM 51-40-11. INSTALLED NEW SERVICABLE ANGLE IAW EXPRESSJET REO 601R-53-11-3340 REV A DATED 2018-10-23.
- [SDR ASOA2018102345273](https://openairdocs.org/sdr/ASOA2018102345273.md): Door Sill · corroded · Oct 14, 2018 · N783CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > REF: CO 7315618 JOB 7731568 OP 42: RT FLOOR SILL RBL 45.00 F.S. 559+16 TO F.S. 559+21 HAS CORROSION ON UPPER SURFACE. C/A:REPAIRED DAMAGE I.A.W. EC/TC REO 601R-53-00-526 01 REV.0, DATED 2013-05-29.
- [SDR ASOA201810235272](https://openairdocs.org/sdr/ASOA201810235272.md): Door Sill · corroded · Oct 14, 2018 · N783CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > REF: CO 7315618 JOB 7731568 OP 34: LT FLOOR SILL HAS MULTIPLE AREAS OF CORROSION FROM F.S. 559.00 TO F.S. 559+48. C/A:REPAIRED DAMAGE I.A.W. EC/TC REO 601R-53-00-526 REV.0, DATED 2013-05-29.
- [SDR ASOA2018102345271](https://openairdocs.org/sdr/ASOA2018102345271.md): Bearing · worn · Oct 14, 2018 · N783CA · Cndair CL6002B19 · Rudder Miscellaneous Structure
  > REF: CO 7315618 JOB 7731561 OP 117: LOWER CENTER RUDDER BEARING WORN. C/A:COMPLIED WITH EC/TC RIL 0602 REV.G, DATED 2018-10-08.
- [SDR ASOA2018102335270](https://openairdocs.org/sdr/ASOA2018102335270.md): Bulkhead · cracked · Oct 13, 2018 · N783CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REF: CO 7315618 JOB 7731565 OP 28: WHILE ACCOMPLISHING REO 601R-53-61-1240, IT WAS FOUND THAT THE CRACK AT RBL 27.50 EXTENDS ABOVE THE CUTOUT LIMITATIONS OF REO 601R-53-61-1240. DEVIATION TO REO 601R-53-61-1240 REQUIRED. C/A:COMPLIED WITH REO 601R-53-61-6727 R
- [SDR ASOA2018102303526](https://openairdocs.org/sdr/ASOA2018102303526.md): Frame · corroded · Oct 3, 2018 · N783CA · Cndair CL6002B19 · Fuselage Main, Frame
  > REF: CO 7315618 JOB 7731568 OP 8: F.S. 319.00 FRAME IS CORRODED BETWEEN STRINGER 25R AND 25L. C/A:REMOVED AND REPLACED FRAME SECTOR I.A.W. SRM 51-42-06, 51-42-21, AND 51-40-11.
- [SDR ASOA201809215290](https://openairdocs.org/sdr/ASOA201809215290.md): Frame · corroded · Sep 21, 2018 · N783CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 394.00 FRAME IS CORRODED BETWEEN STR 25L AND 25R. C/W CARD NR EA 32-2018-215 BLENDED TO REMOVE CORROSION, INSPECTED, VERIFIED REMAINING THICKNESS BY UT. RESTORED FINISH.
- [SDR SWIA201844166](https://openairdocs.org/sdr/SWIA201844166.md): Bpsu · failed · Jan 16, 2018 · N783CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL WARNING. REPLACED BPSU, IAW AMM. OPS CHECKED GOOD.
- [SDR SWIA201642426](https://openairdocs.org/sdr/SWIA201642426.md): Engine · failed · Aug 7, 2016 · N783CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > DURING APP BASE LEG RIGHT ENGINE N1 FLUCTUATED AND NOTABLE A/C ENGINE VIBRATION @ 58 N1. VIBRATION STOPPED. DECLARED EMERGENCY WITH ATC. ON TAXI IN ENG TEMP WENT TO MAX TEMP OIL PRESSURE ZERO SHUT ENG DOWN. R&R THE RT ENGINE IAW AMM. OPS CHECK AND LEAK CH
- [SDR SWIA201642424](https://openairdocs.org/sdr/SWIA201642424.md): Floor Support · corroded · Jul 12, 2016 · N783CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR SUPPORT BEAM AT OTBD LBL 9.00 BETWEEN FS 589.00 AND FS 605.00 HAS CORROSION. R & R PART IAW SRM.
- [SDR SWIA201642423](https://openairdocs.org/sdr/SWIA201642423.md): Skin · gouged · Jul 8, 2016 · N783CA · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING APRON SKIN GOUGE. ALL STEPS COMPLETED OF PERMANENT REPAIR. COMPLIED WITH IAW REO.
- [SDR SWIA201642422](https://openairdocs.org/sdr/SWIA201642422.md): Skin · dented · Jul 6, 2016 · N783CA · Cndair CL6002B19 · Emergency Exits
  > CREW ESCAPE HATCH UPPER LT CORNER HAS A DENT ON OUTER SKIN. COMPLIED WITH STS EA AND ALL STEPS COMPLETED OF PERMANENT REPAIR.
- [SDR SWIA201642421](https://openairdocs.org/sdr/SWIA201642421.md): Floor Support · corroded · Jul 1, 2016 · N783CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT FS 349.00 HAS CORROSION OTBD SIDE OF LBL 27.00. C/W PERMANENT REPAIR OF FLOOR SUPPORT BEAM AT FS 349.00 OTBD SIDE OF LBL 27.00 IAW SRM AND STS-EA.
- [SDR SWIA201642415](https://openairdocs.org/sdr/SWIA201642415.md): Skin · chafed · Jul 1, 2016 · N783CA · Cndair CL6002B19 · Trailing Edge Flaps
  > REPLACE RT INBD FLAP VANE CENTER L/E PN 601R14303-52 FOUND CHAFED. REMOVED AND INSTALLED SERVICEABLE RT INBD FLAP, CENTER L/E IAW SRM.
- [SDR SWIA201642420](https://openairdocs.org/sdr/SWIA201642420.md): Floor Support · corroded · Jun 29, 2016 · N783CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT LBL 9.00 OTBD FLANGE HAS CORROSION BETWEEN FS 621.00 AND FS 589.00. THE FLOORBEAM WAS REMOVED AND A NEW PN: 601R35031-3 WAS INSTALLED IAW REO.
- [SDR SWIA201642419](https://openairdocs.org/sdr/SWIA201642419.md): Floor Support · corroded · Jun 29, 2016 · N783CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT LBL 27.00 INBD AND OTBD FLANGE HAS CORROSION BETWEEN FS 621.00 AND FS 574.00. R & R LBL 27 FLOORBEAM CAP FROM FS 574 TO FS 621 WITH NEW CAP IAW SRM AND REO.
- [SDR SWIA201642418](https://openairdocs.org/sdr/SWIA201642418.md): Door Sill · corroded · Jun 29, 2016 · N783CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT LT SILL HAS CORROSION BETWEEN FS 621.00 AND FS 574.00. C/W PERMANENT REPAIR IAW REO AND SRM.
- [SDR SWIA201642417](https://openairdocs.org/sdr/SWIA201642417.md): Angle · corroded · Jun 29, 2016 · N783CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT AT FS 621.00 HAS CORROSION AT ANGLE STR 17 LT SIDE. INSTALLED NEW ANGLE IN CARGO COMPARTMENT AT FS 621, STR 17L IAW SRM.
- [SDR SWIA201642416](https://openairdocs.org/sdr/SWIA201642416.md): Skin · chafed · Jun 29, 2016 · N783CA · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE L/E CHAFED AT OTBD L/E. REPLACED RT INBD FLAP OTBD L/E IAW SRM.
- [SDR SWIA201642414](https://openairdocs.org/sdr/SWIA201642414.md): Skin · chafed · Jun 29, 2016 · N783CA · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE L/E CHAFED AT INBD L/E. REPLACED L/E PN 601R14303-54 IAW SRM.
- [SDR SWIA201642413](https://openairdocs.org/sdr/SWIA201642413.md): Skin · chafed · Jun 29, 2016 · N783CA · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE L/E CHAFED AT OTBD L/E. REMOVED AND INSTALLED NEW LT INBD FLAP, FLAP VANE OTBD L/E SKIN IAW SRM.
- [SDR SWIA201642412](https://openairdocs.org/sdr/SWIA201642412.md): Skin · chafed · Jun 29, 2016 · N783CA · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBD FLAP VANE L/E CHAFED AT CENTER L/E. REPLACED LT INBD FLAP VANE CENTER L/E IAW SRM.
- [SDR SWIA201642411](https://openairdocs.org/sdr/SWIA201642411.md): Skin · chafed · Jun 29, 2016 · N783CA · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE L/E CHAFED AT INBD L/E. REMOVED AND INSTALLED NEW SERVICEABLE INBD VANE CAP ON LT INBD FLAP IAW SRM.
- [SDR SWIA201642410](https://openairdocs.org/sdr/SWIA201642410.md): Plate · corroded · Jun 27, 2016 · N783CA · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR PROTECTOR PLATE HAS CORROSION ON BOTTOM SIDE OF UPPER FLANGE AROUND SCREW HOLES. INSTALLED NEW SERVICE DOOR PROTECTOR PLATE IAW SRM.
- [SDR SWIA201642409](https://openairdocs.org/sdr/SWIA201642409.md): Structure · dented · Jun 27, 2016 · N783CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MINOR DENT BETWEEN FS 409.00+48 & FS 409.00+64 AND STR 21L & 22L. WORKED OUT DENT AND REMOVED ALL SIGNS OF DENT IAW STS EA.
- [SDR SWIA201642408](https://openairdocs.org/sdr/SWIA201642408.md): Skin · dented · Jun 27, 2016 · N783CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SMALL DENT 6" FWD OF EXTERNAL POWER RECEPTABLE DOOR 1.25" X 1" DIA APPROXIMATELY.005" DEEP LOCATED RT SIDE OF ACFT 6" FWD OF EXTERNAL POWER RECEPTACLE DOOR. REPAIRED DENT IAW STS EA. OPS, RIG CHECKS GOOD.
- [SDR SWIA201642407](https://openairdocs.org/sdr/SWIA201642407.md): Skin · corroded · Jun 27, 2016 · N783CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PANEL 832AL ON PASSENGER DOOR HAS CORROSION ON SKIN AROUND NUTPLATE HOLES. UNDER PANEL 832AL ON PASSENGER DOOR SKIN REPAIRED IAW STS EA.
- [SDR SWIA201439485](https://openairdocs.org/sdr/SWIA201439485.md): Oil System · low · Oct 10, 2014 · N783CA · Cndair CL6002B19 · APU Oil System
  > APU OIL PRESSURE CAUTION MESSAGE DURING FLIGHT. SERVICED APU WITH OIL. OPERATED APU FOR EXTENDED PERIOD. OPS CHECKED GOOD IAW AMM.
- [SDR SWIA201438230](https://openairdocs.org/sdr/SWIA201438230.md): Angle · corroded · Jun 10, 2014 · N783CA · Cndair CL6002B19 · Passenger/Crew Doors
  > CORROSION FOUND ON PAX DOOR KICK ANGLE. C-CHECK, RECEIVED AND INSTALLED NEW PAX DOOR SILL KICK ANGLE IAW SRM.
- [SDR SWIA201438231](https://openairdocs.org/sdr/SWIA201438231.md): Bracket · corroded · Jun 9, 2014 · N783CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR SILL, AFT HINGE ARM CUT OUT CORRODED. C-CHECK, INSTALLED PAX DOOR SILL AFT HINGE ARM CUT OUT BRACKET IAW SRM.
- [SDR SWIA201438232](https://openairdocs.org/sdr/SWIA201438232.md): Skin · cracked · Jun 8, 2014 · N783CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LEFT AFT LATCH CUT OUT IN THE TRU SKIN WAS FOUND CRACKED. C-CHECK, R & R LT FWD TRU BAY SKIN, DOOR LAND IAW SRM.
- [SDR SWIA201438234](https://openairdocs.org/sdr/SWIA201438234.md): Floorbeam · cracked · Jun 7, 2014 · N783CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM ANGLE CRACKED AT BS 484 AND RBL 36, WL 73.5. C-CHECK, R & R FLOORBEAM ANGLE IAW REO.
- [SDR SWIA201438233](https://openairdocs.org/sdr/SWIA201438233.md): Floorbeam · cracked · Jun 7, 2014 · N783CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM ANGLE CRACKED AT BS 484 AND RBL 9, WL 73.5. C-CHECK, REPLACED FLOORBEAM ANGLE IAW REO.
- [SDR SWIA201438240](https://openairdocs.org/sdr/SWIA201438240.md): Hinge · gouged · Jun 6, 2014 · N783CA · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR PIANO HINGE HALF, DOOR SIDE, LUGS NR 1 AND NR 8, AFT TO FWD, HAVE LIGHT GOUGES. C-CHECK, BLENDED CHAFED AREAS ON PAX DOOR PIANO HINGE, DOOR SIDE, LUGS NR 1 AND NR 8 IAW REO AND SRM.

Next page: https://openairdocs.org/deregistered/N783CA-2022-08-16/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 = 'N783CA' AND deregistration_id = 'N783CA-2022-08-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N783CA-2022-08-16/reports

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