# Service difficulty reports: N976EV, cancelled Sep 9, 2024

A list on [N976EV, cancelled Sep 9, 2024](https://openairdocs.org/deregistered/N976EV-2024-09-09.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 · 72 reports

- [SDR ASOA2014021109967](https://openairdocs.org/sdr/ASOA2014021109967.md): Floor Support · corroded · Feb 3, 2014 · N976EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THE LT FLOOR SUPPORT BETWEN BS 559+48 - 559+80 CORRODED AROUND NUT PLATES AND IN OPEN AREAS. BLENDED CORROSION IAW REO 601R-53-00-526.
- [SDR ASOA2014021109966](https://openairdocs.org/sdr/ASOA2014021109966.md): Seat Track · corroded · Feb 3, 2014 · N976EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL 9 BETWEEN BS 409 - 409+128 CORRODED. R & R SEAT TRACK IAW AMM 53-01-11.
- [SDR ASOA2014021109965](https://openairdocs.org/sdr/ASOA2014021109965.md): Seat Track · corroded · Feb 3, 2014 · N976EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL 9 BETWEEN BS 409-409+128 CORRODED. R & R SEAT TRACK IAW AMM 53-01-11 & 53-01-11-400-802.
- [SDR ASOA2014021109964](https://openairdocs.org/sdr/ASOA2014021109964.md): Seat Track · corroded · Feb 3, 2014 · N976EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL 9 BETWEEN BS 364 - 394 CORRODED. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR ASOA2014021109963](https://openairdocs.org/sdr/ASOA2014021109963.md): Seat Track · corroded · Feb 3, 2014 · N976EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL 9 BETWEEN BS 364 - 394 CORRODED. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR ASOA2014021109962](https://openairdocs.org/sdr/ASOA2014021109962.md): Frame · corroded · Feb 3, 2014 · N976EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 589 CORRODED AT S25R. REMOVED CORROSION IAW SRM 51-21-06-00.
- [SDR ASOA2014021109961](https://openairdocs.org/sdr/ASOA2014021109961.md): Frame · corroded · Feb 3, 2014 · N976EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 605, CORRODED FROM S25LT, 25RT. REMOVED CORROSION IAW SRM 51-21-06 AND 53-27-00. MAJOR REPAIR.
- [SDR ASOA2013121809656](https://openairdocs.org/sdr/ASOA2013121809656.md): Windshield · cracked · Nov 27, 2013 · N976EV · Cndair CL6002B19 · Flight Compartment Windows
  > PILOT'S WINDSHIELD CRACKED ENROUTE, ACFT DIVERTED. R & R WINDSHIELD IAW AMM 56-11-01. OPS & LEAK CHECKED GOOD.
- [SDR ASOA2013060703797](https://openairdocs.org/sdr/ASOA2013060703797.md): Bulkhead · cracked · May 15, 2013 · N976EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621, BULKHEAD FAILS NDT WITH AN INDICATION AT CARGO TRACK LBL 27.5 WL 130.0 GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW EC/TC REO 601R-53-61-1541 AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-1541, REV D.
- [SDR ASOA2013060303743](https://openairdocs.org/sdr/ASOA2013060303743.md): Bulkhead · cracked · May 15, 2013 · N976EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 BULKHEAD FAILS NDT WITH AN INDICATION AT CARGO TRACK LBL 27.5 WL 130.0 GREATER THAN 50 PERCENT SCREEN HEIGHT. COMPLIED WITH EC/TC REO 601R-53-61-1541 AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-1541, REV D, DATED: 10/31/2011.
- [SDR ASOA2013060303742](https://openairdocs.org/sdr/ASOA2013060303742.md): Isolator · broken · May 14, 2013 · N976EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 PRESSURE BULKHEAD FWD FACE HAS 8 BROKEN ISOLATORS AS MARKED WITH ORANGE TAPE. REMOVED 8 BROKEN ISOLATORS AND REPLACED WITH SERVICEABLE PARTS IAW SRM 51-42-10.
- [SDR ASOA2013020102946](https://openairdocs.org/sdr/ASOA2013020102946.md): Door · binding · Jan 28, 2013 · N976EV · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR DIFFICULT TO OPEN FROM THE OUTSIDE. CLEANED EXCESSIVE LUBRICATION FROM OUTER HANDLE. COMPLIED WITH OPS TEST OF THE SERVICE DOOR. OPS CHECK GOOD. ACFT OK FOR SERVICE. REF AMM 52-41-00.
- [SDR ASOA2013013102930](https://openairdocs.org/sdr/ASOA2013013102930.md): Handle · unknown · Jan 27, 2013 · N976EV · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR HANDLE DIFFICULT TO OPEN. PERFORMED OPS CHECK AT SERVICE DOOR IAW AMM 52-11-00. OPS CHECKED GOOD, NO DEFECT NOTED.
- [SDR ASOA2012091702225](https://openairdocs.org/sdr/ASOA2012091702225.md): Sensor · out of adjust · Sep 13, 2012 · N976EV · Cndair CL6002B19 · Landing Gear Position and Warning
  > RT GEAR DISAGREE MESSAGE AFTER TAKE OFF. RAN QRH PROCEDURE AND LANDED WITHOUT ISSUE WITH 3 GREEN INDICATED. ACFT RETURNED TO DEPARTURE, EMERGENCY DECLARED. ADJUSTED PROXIMITY SENSOR. PS11GA (PS7GA) AND TARGET ON UPLOCK LATCH IAW AMM 32-32-05. OPS CHECKED
- [SDR ASOA2012080302033](https://openairdocs.org/sdr/ASOA2012080302033.md): Bpsu · failed · Jul 31, 2012 · N976EV · Cndair CL6002B19 · Trailing Edge Flap Control System
  > AFTER TAKEOFF, FLAPS FAILED AT 8 DEGREES. COMPLIED WITH QRH. EMERGENCY DECLARED, ACFT RETURNED TO DEPARTURE. R & R RT BPSU IAW AMM 27-51-10. R & R FECU IAW AMM 27-51-05. OPS CHECKED GOOD
- [SDR ASOA2012080302029](https://openairdocs.org/sdr/ASOA2012080302029.md): Control Unit · failed · Jul 30, 2012 · N976EV · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT 0 ON APPROACH, SKEW DETECTION SYS DEACTIVATED. EMERGENCY DECLARED. REMOVED AND REPLACED RT BPSU AND FECU. OPS CHECKED GOOD.
- [SDR ASOA201102397](https://openairdocs.org/sdr/ASOA201102397.md): Lamp · burned out · Dec 19, 2011 · N976EV · Cndair CL6002B19 · Emergency Lighting
  > PAX DOOR EMERGENCY INOPERATIVE. RELAMPED PAX DOOR OUTER EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR ASOA201101116](https://openairdocs.org/sdr/ASOA201101116.md): Lamp · burned out · Jun 2, 2011 · N976EV · Cndair CL6002B19 · Emergency Lighting
  > EXTERIOR RT AFT EMERGENCY LIGHT IS INOP. R & R EXTERIOR RT AFT EMERGENCY LIGHT LAMP IAW MM 33-51-21-000-810 AND 33-51-21-400-801. OPS CHECKED GOOD.
- [SDR ASOA201101067](https://openairdocs.org/sdr/ASOA201101067.md): Floorbeam · corroded · May 19, 2011 · N976EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLIGHT DECK FLOOR SUPPORT ANGLE AT FS 280 IS CORRODED. LOCATED AND DRILLED NEW FLOOR SUPPORT FOR FLIGHT DECK FS 280 ANGLE IAW SRM 51-42-06. INSTALLED ANGLE. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702.
- [SDR ASOA201101055](https://openairdocs.org/sdr/ASOA201101055.md): Floorbeam · corroded · May 19, 2011 · N976EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION AROUND FASTENER HOLES IN CARGO BAY ON FLOORBEAM. REMOVED CORROSION ON FLOORBEAM IAW SRM 51-21-06. FOUND OUT OF LIMITS IAW SRM 53-00-00. REMOVED FLOORBEAM IAW SRM 51-42-06. LOCATED, DRILLED, COUNTERSUNK IAW SRM 51-42-06. INSTALLED NEW FLOORBEAM
- [SDR ASOA201101054](https://openairdocs.org/sdr/ASOA201101054.md): Cargo Track · corroded · May 19, 2011 · N976EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AROUND FASTENER HOLES IN CARGO BAY ON RBL 27 FROM FS 605 TO FS 621. FINAL DRILLED, SEALED AND INSTALLED NEW SEAT RAIL IAW SRM 51-42-21, 51-45-06, 51-42-22, 51-23-00, 51-41-04 & REO 601R-53-61-4064. LOCATED CARGO TRACK CAD IAW SRM 51-40-11. REO 601R
- [SDR ASOA201101053](https://openairdocs.org/sdr/ASOA201101053.md): Cargo Track · corroded · May 19, 2011 · N976EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON 1 CARGO BAY SEAT RAIL AND 3 ANCHOR PLATES AND ATTACHING HARDWARE AT LBL 27. REMOVED SEVERELY CORRODED FASTENERS & 1 EA SEAT TRACK, 3 EA ANCHOR PLATES. INSTALLED ALL NEW PARTS & HARDWARE IAW SRM 51-41-02. THIS REPAIR IS CLASSIFIED AS A MINOR RE
- [SDR ASOA201101035](https://openairdocs.org/sdr/ASOA201101035.md): Seat Track · corroded · May 19, 2011 · N976EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON CARGO BAY SEAT RAIL AND 2 ANCHOR PLATES AT LBL 18 AND ATTACHING HARDWARE. REMOVED SEVERELY CORRODED SCREWS & TRACKS, ANCHOR PLATES. INSTALLED NEW PART AND HARDWARE, TRACK, 2 EA ANCHOR PLATES IAW SRM 51-41-02. THIS REPAIR IS CLASSIFIED AS A MINO
- [SDR ASOA201101034](https://openairdocs.org/sdr/ASOA201101034.md): Floor Support · corroded · May 19, 2011 · N976EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION IN CARGO BAY ON RT FLOOR SUPPORT FROM FS 559+80 - 621. REPAIRED IAW REO 601R-53-61-4074, REV.
- [SDR ASOA201101033](https://openairdocs.org/sdr/ASOA201101033.md): Seat Track · corroded · May 19, 2011 · N976EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON 1 CARGO BAY SEAT RAIL AT RBL 27 AND ATTACHMENT HARDWARE. REMOVED CORRODED SCREWS & CORRODED SEAT RAIL, INSTALLED NEW SEAT RAIL & NEW HARDWARE IAW SRM 51-41-02. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.
- [SDR ASOA201101032](https://openairdocs.org/sdr/ASOA201101032.md): Seat Track · corroded · May 19, 2011 · N976EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON 2 CARGO BAY SEAT RAILS AT RBL 18 AND ATTACHING HARDWARE. REMOVED CORRODED SCREWS & TRACK SEGMENT. INSTALL NEW TRACK WITH NEW HARDWARE IAW SRM 51-41-02. REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.
- [SDR ASOA201100990](https://openairdocs.org/sdr/ASOA201100990.md): Post · cracked · May 16, 2011 · N976EV · Cndair CL6002B19 · Fuselage Main, Structure
  > FS 409+128 VERT POST BL 0 FAILS NDT WITH AN INDICATION IN LT AFT CHANNEL ON UPPER END. GREATER THAN 50 PERCENT SCREEN HEIGHT APPROX.1 LONG. REMOVED POST, LOCATED AND DRILLED NEW POST IAW SRM 51-42-06. INSTALLED POST IAW SRM 51-42-06 AND REO 601R-53-41889.
- [SDR ASOA201100989](https://openairdocs.org/sdr/ASOA201100989.md): Post · cracked · May 16, 2011 · N976EV · Cndair CL6002B19 · Fuselage Main, Structure
  > FS 409+128 VERTICAL POST, RBL 18 FAILS NDT WITH AN INDICATION IN OTBD AFT CHANNEL ON UPPER END. GREATER THEN 50 PERCENT SCREEN HEIGHT APPROX 1" LONG. REMOVED POST IAW SRM 51-42-06 AND INSTALLED SERVICEABLE POST IAW SRM 51-42-06 AND 51-42-22 AND REO 601R-53-41
- [SDR ASOA201100988](https://openairdocs.org/sdr/ASOA201100988.md): Angle · cracked · May 16, 2011 · N976EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR SUPPORT BEAM AFT LOWER ANGLE IS CRACKED APPROX.3" IN LENGTH. REMOVED CRACKED ANGLE AND REPLACED WITH NEW. INSTALLED NEW ANGLE IAW SRM 51-42-21. MINOR REPAIR.
- [SDR ASOA201100987](https://openairdocs.org/sdr/ASOA201100987.md): Floor Support · corroded · May 16, 2011 · N976EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT AROUND NUTPLATES LBL 27, FS 574.00-621.00. REMOVED FLOOR SUPPORT AND MATCHED DRILL NEW FLOOR SUPPORT IAW SRM 51-42-06, 51-42-21. INSTALLED NEW FLOOR SUPPORT IAW REO 601R-53-61-3778.
- [SDR ASOA201100986](https://openairdocs.org/sdr/ASOA201100986.md): Isolator · cracked · May 16, 2011 · N976EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621.0 BULKHEAD CARGO PANEL NUTPLATE ISOLATORS MISSING OR BROKEN 3 EA, 1 AT LBL 9, 2ND FROM FLOOR, 1 AT RBL 9 2ND FROM FLOOR, AND 1 AT LBL 27, 4TH UP FROM FLOOR. R & R ISOLATORS AND REINSTALLED ISOLATOR BRACKETS IAW SRM 51-42-06. THIS REPAIR IS CLASSIFIED
- [SDR ASOA201100985](https://openairdocs.org/sdr/ASOA201100985.md): Floorbeam · corroded · May 16, 2011 · N976EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RIGHT FS 349 FLOORBEAM CORRODED ON OTBD END AT SERVICE DOOR ENTRANCE. REPAIRED IAW REO 601R-53-21-1286.
- [SDR ASOA201100984](https://openairdocs.org/sdr/ASOA201100984.md): Angle · cracked · May 16, 2011 · N976EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 484, ANGLE AT OBS OF LBL 27 IS CRACKED. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE CLIP (PN 601R31171-17) AT FS 484 OTBD SIDE OF LBL 27 WITH 8 EA NEW HI-LITES IAW SRM CH 51-42-21. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW SOP 5702. THIS REP
- [SDR ASOA201100983](https://openairdocs.org/sdr/ASOA201100983.md): Angle · cracked · May 16, 2011 · N976EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 484, ANGLE AT OBS OF RBL 27 IS CRACKED. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE CLIP (PN 601R31171-9) AT FS 484 OTBD SIDE OF RBL 27 WITH 8 EA NEW HI-LITES IAW SRM CH 51-42-21. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS
- [SDR ASOA201100964](https://openairdocs.org/sdr/ASOA201100964.md): Web · cracked · May 13, 2011 · N976EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280.0 WEB IS CRACKED OTBD OF LBL 9, RBL 9. REPAIRED IAW REO 601R-53-11-926, REV B.
- [SDR ASOA201100960](https://openairdocs.org/sdr/ASOA201100960.md): Intercostal · cracked · May 11, 2011 · N976EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FS 621.00-625.30 INTERCOSTAL AT S14R IS CRACKED NEAR RADIUS APPROX.7" LONG. R & R CRACKED INTERCOSTAL IAW SRM 51-42-21. CLASSIFIED AS A MINOR REPAIR.
- [SDR ASOA201001318](https://openairdocs.org/sdr/ASOA201001318.md): Control Unit · failed · Sep 12, 2010 · N976EV · Cndair CL6002B19 · Drag Control System
  > "SPOILERONS" MESSAGE IN FLIGHT(EMERGENCY DECLARED). R & R NR 2 SECU IAW AMM 27-61-05. OPS CHECK GOOD, NO DEFECT NOTED AT THIS TIME. (CLOSED)
- [SDR ASOA20100001](https://openairdocs.org/sdr/ASOA20100001.md): Ecu · failed · Dec 26, 2009 · N976EV · Cndair CL6002B19 · Landing Gear Position and Warning
  > IAW FIM 32-50-00 R & R NWS ECU IAW AMM 32-51-10. OPS CHECK GOOD. (CLOSED)
- [SDR ASOA201000001](https://openairdocs.org/sdr/ASOA201000001.md): Steering Sys · inoperative · Dec 26, 2009 · N976EV · Cndair CL6002B19 · Landing Gear Steering System
  > AFTER T/O RECEIVED "STEERING INOP" CAUTION MESSAGE. RETURNED TO DEPARTURE. STEERING RESET ON GROUND. (EMERGENCY DECLARED -- ACFT RETURNED TO DEPARTURE AFTER T/O).
- [SDR ASOA200901338](https://openairdocs.org/sdr/ASOA200901338.md): Light · inoperative · Dec 1, 2009 · N976EV · Cndair CL6002B19 · Emergency Lighting
  > LT EXTERIOR NR 4 EMERGENCY LIGHT INOP.
- [SDR ASOA200901337](https://openairdocs.org/sdr/ASOA200901337.md): Light · inoperative · Dec 1, 2009 · N976EV · Cndair CL6002B19 · Emergency Lighting
  > RT EXTERIOR NR 2 EMERGENCY LIGHT INOP.
- [SDR ASOA200901336](https://openairdocs.org/sdr/ASOA200901336.md): Light · inoperative · Dec 1, 2009 · N976EV · Cndair CL6002B19 · Emergency Lighting
  > NR 4 CEILING EMERGENCY LIGHT INOP.
- [SDR ASOA200900746](https://openairdocs.org/sdr/ASOA200900746.md): Light · inoperative · Jul 5, 2009 · N976EV · Cndair CL6002B19 · Emergency Lighting
  > FWD OVERWING EMERGENCY LIGHT INOP.
- [SDR ASOA200900654](https://openairdocs.org/sdr/ASOA200900654.md): Wire · broken · Jun 11, 2009 · N976EV · Cndair CL6002B19 · Light System Wiring
  > WARDROBE LOWER EMERGENCY LIGHT WIRE HAS END BROKEN OFF.
- [SDR ASOA200900626](https://openairdocs.org/sdr/ASOA200900626.md): Post · damaged · May 29, 2009 · N976EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT FS 409.0+128 O/B VERTICAL POST LBL 18.0 HAS AN INDICATION NOTED APPROX.2 INCHES IN LENGTH 50 PERCENT FSH AT WL 69.0. FAILED NDT INSPECTION. REMOVED LBL 18 POST IAW CRJ SRM 51-42-06. FABRICATED OUTBOARD REPLACEMENT POST USING 7075-0.063" PO 104141/3 IAW
- [SDR ASOA200900593](https://openairdocs.org/sdr/ASOA200900593.md): Bulkhead · damaged · May 27, 2009 · N976EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > JOB 8760125 OPERATION 198 REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL FITTING HAS AN INDICATION NOTED APPROX.2" IN LENGTH 70% FSH. FAILED NDT INSPECTION. REPAIRED PER EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETED AND THE REPAIR C/W THE REQUIREMENTS
- [SDR ASOA200900590](https://openairdocs.org/sdr/ASOA200900590.md): Seat Track · corroded · May 26, 2009 · N976EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK RBL 9, FS 399.5 HAS CORROSION AROUND SCREW HOLES. REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-11 AND AMM 53-01-11-420-001B.
- [SDR ASOA200900589](https://openairdocs.org/sdr/ASOA200900589.md): Seat Track · corroded · May 26, 2009 · N976EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK RBL 9, FS 364 HAS CORROSION AROUND SCREW HOLES. REMOVED SEAT TRACK & INSTALLED NEW FLOOR SEAT TRACK IAW AMM 53-01-11.
- [SDR ASOA200900580](https://openairdocs.org/sdr/ASOA200900580.md): Bulkhead · damaged · May 23, 2009 · N976EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > RT FS 559 BULKHEAD WEB HAS AN INDICATION NOTED AT WL 59.10 I/B OF RBL 18.0 APPROX.3" IN LENGTH 70% FSH. FAILED NDT INSPECTION. COMPLIED WITH REPAIR AT FS 559 BULKHEAD LT AND RT WHEEL WELL IAW REO 601R-53-41-260 REV.C, STEPS 1-14. PAINTED RT BULKHEAD REPAIRED
- [SDR ASOA200900578](https://openairdocs.org/sdr/ASOA200900578.md): Drag Angle · cracked · May 23, 2009 · N976EV · Cndair CL6002B19 · Passenger/Crew Doors
  > JOB 8760121 OPERATION 139 PAX DOOR AFT DRAG ANGLE IS CRACKED 1.25"L JUST ABOVE THE DOOR ASSIST CABLE PULLEY. REPAIRED PAX DOOR CRACKED AFT DRAG ANGLE PRE-EXISTING REPAIR IAW REO 601R-52-11-513 REV.A.

Next page: https://openairdocs.org/deregistered/N976EV-2024-09-09/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 = 'N976EV' AND deregistration_id = 'N976EV-2024-09-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N976EV-2024-09-09/reports

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