# Service difficulty reports: N923EV

A list on [N923EV](https://openairdocs.org/aircraft/N923EV.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 3 · 118 reports

- [SDR SWIA202054581](https://openairdocs.org/sdr/SWIA202054581.md): Acm · odor · Dec 8, 2020 · N923EV · Cndair CL6002B19 · Cabin Cooling System
  > STRONG BURNING SMELL (LIKE BURNT RUBBER) AFTER WE ADVANCED THROTTLES AND TOOK OFF FROM TWF. ALL INDICATIONS WERE NORMAL. FLIGHT 4234-FILED CLOSED. THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 21955715 WITH THE FOLLOWING CORRECTIVE ACTION: "FIM TASK COMPLET
- [SDR SWIA2019102346605](https://openairdocs.org/sdr/SWIA2019102346605.md): Frame · corroded · Oct 23, 2019 · N923EV · Cndair CL6002B19 · Fuselage Main, Frame
  > * L/H FS 513.00 FRAME HAS SMALL SPOT OF CORROSION APPROX. 1" ABOVE PRESSURE FLOOR SILL AT AFT INB CORNER OF FRAME. (C-CHECK) RO: 10/22/19. PERFORMED BLEND OUT OF CORROSION AT L/H FS 513.00 FRAME 1.0" ABOVE PRESSURE FLOOR SILL I/B CORNER. IAW SRM. FOUND TO BE
- [SDR SWIA2019102346594](https://openairdocs.org/sdr/SWIA2019102346594.md): Angle · cracked · Oct 23, 2019 · N923EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS280 LBL9 I/B ANGLE CRACKED IN RADIUS, TOP OF ANGLE. (C-CHECK) RO: 10/22/19. FABRICATED NEW ANGLE AND REPLACED IAW REO.
- [SDR SWIA2019061445982](https://openairdocs.org/sdr/SWIA2019061445982.md): Panel · damaged · May 20, 2019 · N923EV · Cndair CL6002B19 · Fuselage Main, Structure
  > 2 ADDITIONAL FASTENER HOLES ELONGATED (APPROX..225") FOR RH KIDNEY PANEL (132AL). LOCATED ON FWD EDGE OF CUTOUT JUST BELOW STR20R. (C-CHECK) RO: 06/14/2019 REPAIRED 2 ADDITIONAL FASTENER HOLES IAW REO.
- [SDR SWIA2019061445989](https://openairdocs.org/sdr/SWIA2019061445989.md): Frame · corroded · May 19, 2019 · N923EV · Cndair CL6002B19 · Fuselage Main, Frame
  > F.S. 605.00 IS CORRODED ON FORWARD FLANGE BETWEEN STRINGER 26R AND 25L. (C-CHECK) RO: 06/14/2019 REMOVED AND REPLACED FS605 FRAME SECTOR IAW SRM.
- [SDR SWIA2019061445987](https://openairdocs.org/sdr/SWIA2019061445987.md): Attach Fitting · corroded · May 16, 2019 · N923EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FLOOR BEAM ATTACH FITTING ON FORWARD FACE OF F.S.621.00, LBL 9.00 IS CORRODED. (C-CHECK) RO: 06/14/2019 REMOVED AND INSTALLED NEW SERVICABLE FLOOR BEAM ATTACH FITTING ON FORWARD FACE OF F.S. 621.00 LBL 9.00 IAW SRM.
- [SDR SWIA2019061445983](https://openairdocs.org/sdr/SWIA2019061445983.md): Stringer · cracked · May 16, 2019 · N923EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L IS CRACKED AT AFT END OF PAX DOOR UPPER SILL. (C-CHECK) RO: 06/14/2019 REPAIRED STRINGER 3L IAW REO AND SRM.
- [SDR SWIA2019061445992](https://openairdocs.org/sdr/SWIA2019061445992.md): Skin · cracked · May 12, 2019 · N923EV · Cndair CL6002B19 · Wing, Plate/Skin
  > L/H LOWER WING PLANK HAS ONE INDICATION NOTED ON EDGE OF CUT OUT AT TOP CORNER FOR ACCESS PANEL 550EB ON I/B SIDE OF HOLE.100" LONG BY 80%FSH. (C-CHECK) RO: 06/14/2019 REPAIRED LH LOWER WING PLANK HOLE FOR ACCESS PANEL 550EB IAW REO.
- [SDR SWIA2019061445984](https://openairdocs.org/sdr/SWIA2019061445984.md): Post · cracked · May 10, 2019 · N923EV · Cndair CL6002B19 · Fuselage Main, Structure
  > FS409+128 VERTICAL POST @ BL0 RH SIDE HAS AN INDICATION.1" LONG BY 55% FSH IN THE UPPER AFT RADIUS AT WL69. (C-CHECK) RO: 06/14/2019. REMOVED AND REPLACED 409 +128 BL0 POST IAW REO AND SRM.
- [SDR SWIA2019061445990](https://openairdocs.org/sdr/SWIA2019061445990.md): Hinge Fitting · chafed · May 8, 2019 · N923EV · Cndair CL6002B19 · Trailing Edge Flaps
  > HINGE BOX UNDER PANEL 695AB IS CHAFED FROM TO LONG OF A SCREW INSTALLED AT THE FORWARD INBOARD LOWER FAIRING MOUNT. CHAFE IS APPROXIMATELY.005" DEEP WITH HIGH METAL. (C-CHECK) RO: 06/14/2019 REPAIRED FLAP HINGE BOX IAW REO.
- [SDR SWIA2019061445988](https://openairdocs.org/sdr/SWIA2019061445988.md): Bulkhead Web · cracked · May 5, 2019 · N923EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS621 RPB WEB HAS 3EA AREAS OF CRACK INDICATIONS NOTED IN THE HEEL LINE AREA OF VERTICAL POSTS, 1 AT RBL27 WL102 TO WL113 70%FSH, 1 AT BL0 WL126 TO WL134 50%FSH, AND 1 AT BL0 WL108 TO WL113 60%FHS. (C-CHECK) RO: 06/14/2019 REPAIRED THE 3 CRACK INDICATIONS ON F
- [SDR SWIA2019406145993](https://openairdocs.org/sdr/SWIA2019406145993.md): Frame · corroded · May 4, 2019 · N923EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 364 FRAME SECTOR IS CORRODED FROM STGR 25L TO STGR 25R. (C-CHECK) RO: 06/14/2019 REMOVED AND REPLACED FS 364 LOWER FRAME SECTOR IAW SRM.
- [SDR SWIA2019061445991](https://openairdocs.org/sdr/SWIA2019061445991.md): Frame · corroded · May 4, 2019 · N923EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 349 FRAME SECTOR IS CORRODED FROM STGR 25L TO STGR 25R. (C-CHECK) RO: 06/14/2019 REMOVED AND REPLACED FS349 LOWER FRAME SECTOR IAW SRM.
- [SDR SWIA2019061445986](https://openairdocs.org/sdr/SWIA2019061445986.md): Intercostal · corroded · May 4, 2019 · N923EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CORRODED AT STGR 27L BETWEEN FS 349 AND FS 364. REMOVED AND REPLACED INTERCOSTAL IAW SRM.
- [SDR SWIA2019061445985](https://openairdocs.org/sdr/SWIA2019061445985.md): Support Angle · corroded · May 4, 2019 · N923EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SEAL SUPPORT ANGLE IS CORRODED. (C-CHECK) RO: 06/14/2019 REPAIRED SERVICE DOOR IAW REO.
- [SDR SWIA2018091845088](https://openairdocs.org/sdr/SWIA2018091845088.md): Shutoff Valve · failed · Sep 18, 2018 · N923EV · Cndair CL6002B19 · Cabin Cooling System
  > WHILE CLIMBING THE RIGHT PACK (ONLY OPERATIONAL PACK) SHUT OFF AND AIRCRAFT BECAME UNPRESSURIZED. EMERGENCY DESCENT WAS COMPLIED WITH. RETURNED TO FIELD. NO PACK HI TEMP OR HI PRESS CAUTION MESSAGES OBSERVED. (FLT 4832) FO: 09/18/2018. CLOSED REMOVED AND REPLA
- [SDR SWIA201743333](https://openairdocs.org/sdr/SWIA201743333.md): Bulkhead · cracked · Apr 27, 2017 · N923EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB FWD FACE HAS TWO INDICATIONS NOTED AT LBL 36.2, WL 76 APPROX 1 INCH IN LENGTH, LBL 27.5, WL76 APPROXIMATELY 4 INCHES IN LENGTH BOTH FAILED ULTRASOUND INSPECTION. REPAIRED THE PRESSURE BULKHEAD IAW REO.
- [SDR SWIA201743332](https://openairdocs.org/sdr/SWIA201743332.md): Bulkhead Web · cracked · Apr 12, 2017 · N923EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 280 LOWER BULKHEAD WEB IS CRACKED JUST OUTBOARD OF LBL 9. REPAIRED THE BULKHEAD WEB IAW REO.
- [SDR ASOA2015101913933](https://openairdocs.org/sdr/ASOA2015101913933.md): Bulb · burned out · Oct 19, 2015 · N923EV · Cndair CL6002B19 · Emergency Lighting
  > FWD OVERWING EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY EXIT BULB IAW AMM 33-51-21. OPS CK GOOD.
- [SDR ASOA2015080413447](https://openairdocs.org/sdr/ASOA2015080413447.md): Door · unknown · Aug 4, 2015 · N923EV · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR IS DIFFICULT TO OPEN FROM THE OUTSIDE. PERFORMED OPS CHECK OF SERVICE DOOR IAW AMM 52-41-00, NO FURTHER DEFECTS NOTED.
- [SDR ASOA2015070713283](https://openairdocs.org/sdr/ASOA2015070713283.md): Window Frame · cracked · Jun 17, 2015 · N923EV · Cndair CL6002B19 · Fuselage Main, Structure
  > CRACK FOUND ON LT WINDSHIELD SIDE POST SUPPORT. REMOVED ALL FASTENERS COMMON TO ANGLE 601R34032-21 IAW SRM 51-42-06 AND REMOVED ANGLE 601R 34032-21. PERMANENTLY INSTALLED ALL FASTENERS IN NEW SERVICEABLE ANGLE IAW SRM 51-42-06, DWG 601R34032, DWG 601R34032.
- [SDR ASOA2015070713282](https://openairdocs.org/sdr/ASOA2015070713282.md): Skin · corroded · Jun 17, 2015 · N923EV · Cndair CL6002B19 · Wing, Plate/Skin
  > 650EB FUEL TANK LAND HAS CORROSION. COMPLIED WITH ECTC EO 600-57-81.
- [SDR ASOA2015070713281](https://openairdocs.org/sdr/ASOA2015070713281.md): Skin · corroded · Jun 16, 2015 · N923EV · Cndair CL6002B19 · Wing, Plate/Skin
  > 640BB FUEL TANK LAND HAS CORROSION. COMPLIED WITH ECTC REO 600-57-81.
- [SDR ASOA2015070713280](https://openairdocs.org/sdr/ASOA2015070713280.md): Skin · corroded · Jun 16, 2015 · N923EV · Cndair CL6002B19 · Wing, Plate/Skin
  > 640DB FUEL TANK LAND HAS CORROSION. REPAIRED IAW ECTC EO 600-57-81.
- [SDR ASOA2015070713279](https://openairdocs.org/sdr/ASOA2015070713279.md): Skin · corroded · Jun 16, 2015 · N923EV · Cndair CL6002B19 · Wing, Plate/Skin
  > 650 BB FUEL ACCESS PANEL LAND HAS CORROSION. REPAIRED IAW ECTC EO 600-57-81.
- [SDR ASOA2015070713278](https://openairdocs.org/sdr/ASOA2015070713278.md): Door Sill · corroded · Jun 12, 2015 · N923EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR SILL CORRODED AROUND SCREW HOLES AT BS 574 - 621, LBL 70. BLENDED THE DOOR SILL IAW SRM 51-21-06. AREA EXCEEDS ALLOWABLE LIMITS OF EC/TC REO 601R-53-00-526. REPAIRED IAW REO 601R-53-61-5506.
- [SDR ASOA2015070713277](https://openairdocs.org/sdr/ASOA2015070713277.md): Bracket · corroded · Jun 12, 2015 · N923EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKET AT BS 349 AND STR 17R. REMOVED THE BRACKET IAW SRM 51-42-21. INSTALLED A NEW BRACKET IAW SRM 51-42-21-00.
- [SDR ASOA2015070713276](https://openairdocs.org/sdr/ASOA2015070713276.md): Seat Track · corroded · Jun 11, 2015 · N923EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED BS 394 - 439, RBL 9. FABRICATED A NEW SEAT TRACK IAW GREO 601R-53-00-485, REV A. R & R THE SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR ASOA2015070713275](https://openairdocs.org/sdr/ASOA2015070713275.md): Seat Track · corroded · Jun 11, 2015 · N923EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED AT BS 364- 394 LBL 9. R & R THE SEAT TRACK IAW AMM 53-01-11-04 AND 53-01-11-944-001, 53-01-11-000-802, 53-01-11-400-802.
- [SDR ASOA2015070713274](https://openairdocs.org/sdr/ASOA2015070713274.md): Seat Track · corroded · Jun 11, 2015 · N923EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED AT BS 364 - 394, RBL 9. FABRICATED A NEW SEAT TRACK IAW GREO 601R-53-00-485, REV A. R & R THE SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR ASOA2015070713273](https://openairdocs.org/sdr/ASOA2015070713273.md): Floorbeam · corroded · Jun 11, 2015 · N923EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION FOUND ON FLOORBEAM AT BS 409, RBL 9. BLENDED THE FLOORBEAM IAW SRM 51-21-06. BLENDED AREAS ARE WITHIN LIMITS IAW REO 601-53-00-005.
- [SDR ASOA2015070713272](https://openairdocs.org/sdr/ASOA2015070713272.md): Floorbeam · corroded · Jun 11, 2015 · N923EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION FOUND ON FLOORBEAM AT FS 409, RBL 9. BLENDED THE FLOORBEAM IAW SRM 51-21-06. FOUND OUT OF LIMITS IAW REO 601R-53-00-005.
- [SDR ASOA2015070713271](https://openairdocs.org/sdr/ASOA2015070713271.md): Floorbeam · corroded · Jun 11, 2015 · N923EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION FOUND ON FLOORBEAM BS 409, RBL 9. BLENDED THE FLOORBEAM IAW SRM 51-21-06.
- [SDR ASOA2015070713270](https://openairdocs.org/sdr/ASOA2015070713270.md): Floorbeam · corroded · Jun 11, 2015 · N923EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION FOUND ON FLOORBEAM AT FS 409, RBL 9. BLENDED THE FLOORBEAM IAW SRM 51-21-06. AND FOUND WITHIN LIMITS IAW REO 601R-53-00-005, FIG 1.
- [SDR ASOA2015070713269](https://openairdocs.org/sdr/ASOA2015070713269.md): Seat Track · corroded · Jun 11, 2015 · N923EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED BS 394 - 439, LBL 9. CORROSION FOUND TO BE BEYOND LIMITS IAW SRM 53-21-44. REMOVED DAMAGED SEAT TRACK IAW AMM 53-01-11-020-001. FABRICATED A NEW SEAT TRACK IAW GREO 601RE-53-00-485 REV A, COMPLIED WITH REO 601R-53-00-485 REV A. INSTAL
- [SDR ASOA2015070713268](https://openairdocs.org/sdr/ASOA2015070713268.md): Frame · corroded · Jun 10, 2015 · N923EV · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION FOUND ON FRAME BS 349 STR 26R-25L. REMOVED CORROSION IAW SRM 53-00-00.
- [SDR ASOA2015070713267](https://openairdocs.org/sdr/ASOA2015070713267.md): Floor Panel · cracked · Jun 8, 2015 · N923EV · Cndair CL6002B19 · Fuselage Floor Panel
  > LEFT SIDE FWD EQUIPMENT COMPARTMENT, TRU, FLOOR PAN CRACKED BETWEEN OUTER SKIN EDGE AND BREAK PRESSURE GOUGES BRACKET. REPAIRED ELECTRICAL BAY FLOOR AT FS 193.00 IAW GREO 601R-53-11-111.
- [SDR ASOA2015070713266](https://openairdocs.org/sdr/ASOA2015070713266.md): Latch · failed · Jun 6, 2015 · N923EV · Cndair CL6002B19 · Emergency Exits
  > RT OVERWING EMERGENCY EXIT DOOR IS DIFFICULT TO OPEN. REMOVED RT OVERWING EXIT DOOR LATCH MECHANISM TO FOM IAW AMM 52-21-02-000-801. ADJUSTED RT OVERWING EMERGENCY EXIT DOOR LATCH MECH REF CMM 52-21-02. REINSTALLED LATCH MECH REF AMM TASK 52-21-02-400-801 O
- [SDR ASOA2013110809378](https://openairdocs.org/sdr/ASOA2013110809378.md): Sign · missing · Nov 7, 2013 · N923EV · Cndair CL6002B19 · Emergency Lighting
  > EXIT SIGN PANEL MISSING IN THE EXIT ROW. SECURED EXIT SIGN BACK INTO PLACE IAW AMM 25-60-01. OK FOR SERVICE.
- [SDR ASOA2013062808528](https://openairdocs.org/sdr/ASOA2013062808528.md): Lamp · burned out · Jun 24, 2013 · N923EV · Cndair CL6002B19 · Emergency Lighting
  > FWD BULKHEAD LOWER EMERGENCY FLOOD LIGHT HAS INOPERATIVE LAMPS. REPLACED LAMPS FWD BULKHEAD LOWER EMERGENCY FLOOD LIGHT IAW AMM 33-51-19, OP'S CHECK GOOD.
- [SDR ASOA2013041203375](https://openairdocs.org/sdr/ASOA2013041203375.md): Post · cracked · Mar 26, 2013 · N923EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND FS 409.00+128 VERT POST AT RBL 18 INBD AND OTBD SIDES HAVE INDICATIONS NOTED AT AFT FLANGE RADIUS WL 69 APPROX.2" IN LENGTH X 50 PERCENT FSH BOTH FAILED NDT. R & R DAMAGED INBD AND OTBD RBL 18 FS 409+128 POST IAW REO 601R-53-41-889.
- [SDR ASOA2013041203374](https://openairdocs.org/sdr/ASOA2013041203374.md): Bulkhead · cracked · Mar 25, 2013 · N923EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND FS 621.00 RPB WEB HAS AN INDICATION NOTED AT LBL 27.5 WL 130 (CARGO DOOR TRACK) APPROX 1" LONG X 100 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW SRM 51-42-06 AND REO 601R-53-61-1541, REV D DATED 10/31/2011.
- [SDR ASOA2013041203373](https://openairdocs.org/sdr/ASOA2013041203373.md): Bulkhead · cracked · Mar 25, 2013 · N923EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND FS 621.00 RPB WEB HAS AN INDICATION NOTED AT LBL 46 WL 108 (CARGO DOOR LINTEL FITTING) APPROX.5" LONG X 100 PERCENT FSH. FAILED NDT INSPECTION. UPON REPAIR OF FS 621 LINTEL FOUND PN 600-35013-39 TO HAVE A DRILL START. REMOVED PART IAW SMM 51-42-21.
- [SDR ASOA2013041203372](https://openairdocs.org/sdr/ASOA2013041203372.md): Angle · cracked · Mar 25, 2013 · N923EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AT FS 473.15, RBL 27.00, INTERCOSTAL INBD AFT NESTING ANGLE IS CRACKED. REQUIRES REPLACEMENT. R & R ANGLE IAW SRM 51-42-10, 51-40-11 AND 51-42-21.
- [SDR ASOA2013041203371](https://openairdocs.org/sdr/ASOA2013041203371.md): Cargo Track · corroded · Mar 20, 2013 · N923EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO COMPARTMENT FLOOR TRACKS AND TIE DOWNS ARE CORRODED AND REQUIRE REPLACEMENT. R & R CARGO FLOOR TRACKS IAW SRM 51-41-04.
- [SDR ASOA2013041203370](https://openairdocs.org/sdr/ASOA2013041203370.md): Floor Support · corroded · Mar 20, 2013 · N923EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO COMPARTMENT FLOOR SILL AT LBL 45 HAS CORROSION FROM FS 574.00 TO 621.00. R & R CARGO DOOR SILL WITH NEW SERVICEABLE SILL PLATE IAW REPAIR REO 601R-53-61-1574, REV A.
- [SDR ASOA2013041203369](https://openairdocs.org/sdr/ASOA2013041203369.md): Seat Track · corroded · Mar 20, 2013 · N923EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT FLOOR SEAT TRACK CORRODED BETWEEN FS 409+126 AND FS 559+4, RBL 9. REMOVED CORRODED RT FLOOR SEAT TRACK BETWEEN FS 409+126 AND FS 559+4 RBL 9 IAW SRM 51-41-02. LOCATED AND DRILLED HOLES FOR NEW SERVICEABLE SEAT TRACK IAW SRM 51-40-11 P/N 601R31032-75. INS
- [SDR ASOA2013041103365](https://openairdocs.org/sdr/ASOA2013041103365.md): Seat Track · corroded · Mar 20, 2013 · N923EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED BETWEEN FS 399.5 AND 409+126, RBL 9.0. R & R TRACK IAW AMM 53-01-11-400-802.
- [SDR ASOA2013041103364](https://openairdocs.org/sdr/ASOA2013041103364.md): Seat Track · corroded · Mar 20, 2013 · N923EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED BETWEEN FS 364 AND 399.50, RBL 9. R & R SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR ASOA2013041103363](https://openairdocs.org/sdr/ASOA2013041103363.md): Angle · cracked · Mar 19, 2013 · N923EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT FS 621-625 INTERCOSTAL ANGLE CRACKED AT STR 14L. REMOVED INTERCOSTAL ANGLE IAW SRM 51-42-06. INSTALLED SERVICEABLE INTERCOSTAL ANGLES AT STRINGER 14L FROM FS 621-625 IAW REO 601R-53-61-422 AND SRM 51-42-21.

Next page: https://openairdocs.org/aircraft/N923EV/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 = 'N923EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N923EV/reports

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