# Service difficulty reports: N927EV

A list on [N927EV](https://openairdocs.org/aircraft/N927EV.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 5 · 208 reports

- [SDR REXA2022111002450](https://openairdocs.org/sdr/REXA2022111002450.md): None · inoperative · Nov 3, 2022 · N927EV · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTED EXIT SIGN INOP BY PAX DOOR "REMOVED AND REPLACED FLOOR LEVEL EXIT SIGN IAW CRJ200 AMM 33-51-10 OPS TEST GOOD P/N ON/OFF 6020-6 "
- [SDR REXA2022060801079](https://openairdocs.org/sdr/REXA2022060801079.md): None · cracked · May 29, 2022 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DETAILED INSPECTION OF THE FS 409.0 +128 FRAME AND CAP AFT ANGLES AT STR21 LEFT AND RIGHT. CRACKS WERE FOUND AT THE BOTTOM OF THE LBL27 VERTICAL POST ON THE IB SIDE. THE CRACK ORIGINATES FROM THE BOTTOM OF THE POST BENEATH THE BOTTOM MOST RIVET AND MOVES UPWA
- [SDR REXA2022060801078](https://openairdocs.org/sdr/REXA2022060801078.md): None · cracked · May 29, 2022 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DETAILED INSPECTION OF THE FS 409.0 +128 FRAME AND CAP AFT ANGLES AT STR21 LEFT AND RIGHT. CRACKS WERE FOUND AT THE BOTTOM OF THE LBL27 VERTICAL POST ON THE OB SIDE. THE CRACK ORIGINATES FROM THE BOTTOM OF THE POST BENEATH THE BOTTOM MOST RIVET AND MOVES UPWA
- [SDR REXA2022060801077](https://openairdocs.org/sdr/REXA2022060801077.md): None · cracked · May 29, 2022 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DETAILED INSPECTION OF THE FS 409.0 +128 FRAME AND CAP AFT ANGLES AT STR21 LEFT AND RIGHT, A CRACK WAS FOUND AT THE BOTTOM OF THE LBL18 VERTICAL POST ON THE OB SIDE. THE CRACK WAS FOUND AT THE THE BOTTOM OF THE LBL18 VERTICAL POST ON THE OB SIDE. THE CRACK OR
- [SDR REXA2022060801076](https://openairdocs.org/sdr/REXA2022060801076.md): None · cracked · May 29, 2022 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DETAILED INSPECTION OF THE FS 409.0 +128 FRAME AND CAP AFT ANGLES AT STR21 LEFT AND RIGHT, A CRACK WAS FOUND AT THE BOTTOM OF THE RBL27 VERTICAL POST ON THE IB SIDE. THE CRACK ORIGINATES FROM THE BOTTOM OF THE POST UNDERNEATH THE BOTTOM MOST RIVET AND MOVES U
- [SDR REXA2022051700953](https://openairdocs.org/sdr/REXA2022051700953.md): None · inoperative · May 12, 2022 · N927EV · Cndair CL6002B19 · Cabin Pressure Control System
  > R PACK HI-PRESS CROSSING FL230, NOTICED ALT INCREASING RAPIDLY, STARTED OUR DESCEND THEN GOT CABIN ALT CAUTION, THEN WARNING ON OUR WAY TO 8000. RH PACK R/R IAW CRJ 200 AMM 21-51-10. OPS CHECK RH PACK OPS CHECK GOOD
- [SDR REXA2022040500563](https://openairdocs.org/sdr/REXA2022040500563.md): Light · inoperative · Apr 2, 2022 · N927EV · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS FOUND NOT ILLUMINATED DURING PREFLIGHT INSPECTION FOUND FLOOR PROX EXIT SIGN DS11LY HAD SWAPPED CONNECTIONS W- FLOOR LEVEL FLOODLIGHT DS3LY NEAR SERVICE DOOR. RESTORED CORRECT CONNECTION IAW AMM 33-51-10, 33-51-19 AND WM 33-51-00. OPS CHE
- [SDR REXA2021070100483](https://openairdocs.org/sdr/REXA2021070100483.md): Light · inoperative · Jul 1, 2021 · N927EV · Cndair CL6002B19 · Emergency Lighting
  > FWD EMER LIGHT OVER RIGHT WING INOPERATIVE. REMOVED AND REPLACED RH EMER LIGHT IAW AMM 33-51-21. BM1-0006-002
- [SDR REXA2021050600298](https://openairdocs.org/sdr/REXA2021050600298.md): Bulkhead · damaged · May 1, 2021 · N927EV · Cndair CL6002B19 · Fuselage Main, Structure
  > R/H 9G BULKHEAD HAS 20EA AREAS OF DAMAGE AROUND POTTED INSERTS. REPAIRED RH 9G BULKHEAD IAW MHIRJ ENGINEERING ORDER CL-600-2B19-53-L06720 REV IR, DATED 4/15/2021.
- [SDR REXA2021050600297](https://openairdocs.org/sdr/REXA2021050600297.md): Bulkhead · damaged · May 1, 2021 · N927EV · Cndair CL6002B19 · Fuselage Main, Structure
  > CENTER 9G BULKHEAD HAS 6EA AREAS OF DAMAGE AROUND PUTTED INSERTS REPAIRED CENTER 9G BULKHEAD IAW MHIRJ ENGINEERING ORDER CL-600-2B19-53-L06719 REV IR, DATED 4/15/2021.
- [SDR REXA2021050600296](https://openairdocs.org/sdr/REXA2021050600296.md): Bulkhead · damaged · May 1, 2021 · N927EV · Cndair CL6002B19 · Fuselage Main, Structure
  > L/H 9G BULKHEAD HAS 19EA AREAS OF DAMAGE AROUND POTTED INSERTS. REPAIRED RH 9G BULKHEAD IAW MHIRJ ENGINEERING ORDER CL-600-2B19-53-L06718 REV IR, DATED 4/15/2021.
- [SDR REXA2021050600295](https://openairdocs.org/sdr/REXA2021050600295.md): Frame · corroded · Apr 27, 2021 · N927EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 333 STR 22R FWD SIDE OF FRAME HAS CORROSION AROUND RIVETS. REMOVED AND REPLACED FRAME SECTOR IAW CRJ 200 SRM 51-40-11,51-42-06 AND 51-42-20.
- [SDR REXA2021050600292](https://openairdocs.org/sdr/REXA2021050600292.md): Seat Track · corroded · Apr 23, 2021 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/H SIDE SEAT RAIL IS CORRODED BETWEEN FS 559+16 TO FS 559+32 REMOVED AND REPLACE SIDE SEAT RAILS FS 559+16 - 559+32 IAW MHI REO 601R-53-00-005 REV C 19-3-21 AND CRJ 200 AMM 53-01-11-000/400-802
- [SDR REXA2021051100324](https://openairdocs.org/sdr/REXA2021051100324.md): Handle · failed · Apr 21, 2021 · N927EV · Cndair CL6002B19 · Emergency Exits
  > R/H OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST, HANDLE SHOULD RELEASE WITH 20-40 LBS OF FORCE, REQUIRED 50 LBS. LUBRICATED AND CORRECTLY PERFORMED FUNCTIONAL TEST OF RH OVERWING EMER EXIT IAW CRJ 200 AMM 12-20-52-640-802, 52-21-00-720-801. TEST GOOD. NO D
- [SDR REXA2021050600294](https://openairdocs.org/sdr/REXA2021050600294.md): Seat Track · corroded · Apr 15, 2021 · N927EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > L/H SIDE SEAT RAIL IS CORRODED BETWEEN FS 409+16 TO FS 409+32 REMOVED AND REPLACE SIDE SEAT RAILS FS 409+16 - 409+32 IAW MHI REO 601R-53-00-005 REV C 19-3-21 AND CRJ 200 AMM 53-01-11-000/400-802
- [SDR REXA2021050600293](https://openairdocs.org/sdr/REXA2021050600293.md): Seat Track · corroded · Apr 15, 2021 · N927EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > R/H SIDE SEAT RAIL IS CORRODED BETWEEN FS 559 TO FS 559+16 REMOVED AND REPLACE SIDE SEAT RAILS FS 559 - 559+16 IAW MHI REO 601R-53-00-005 REV C 19-3-21 AND CRJ 200 AMM 53-01-11-000/400-802
- [SDR REXA2021050600291](https://openairdocs.org/sdr/REXA2021050600291.md): Support Beam · cracked · Apr 14, 2021 · N927EV · Cndair CL6002B19 · Fuselage Main, Structure
  > CARGO DOOR SUPPORT BEAM BOTTOM CLIP ON THE FS 621 BULKHEAD IS CRACKED REMOVED AND REPLACE CLIP IAW CRJ 200 SRM 51-40-11 AND 51-42-21.
- [SDR REXA2020071300598](https://openairdocs.org/sdr/REXA2020071300598.md): Light · inoperative · Jul 11, 2020 · N927EV · Cndair CL6002B19 · Emergency Lighting
  > FWD EMERGENCY CEILING FLOOD LIGHT INOPERATIVE. REMOVED AND REPLACED CHARGER 1 FOR EMERGENCY LIGHTS, OPS CHECK GOOD, IAW CRJ200 AMM 33-51-05.
- [SDR REXA2020012730051](https://openairdocs.org/sdr/REXA2020012730051.md): Charger · inoperative · Jan 23, 2020 · N927EV · Cndair CL6002B19 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHTS FWD OF PASSENGER EXIT AND SERVICE DOOR INOP REMOVED AND REPLACED BATTERY PACK AT PS1LF. DID NOT FIX. REMOVED AND REPLACED CAHRGER ASSY. OPS CHECK GOOD IAW CRJ 200 AMM 33-51-04 AND CRJ 200 AMM 33-51-05. BATTERY P/N OFF 2013-1A S/N OFF
- [SDR REXA2019111871638](https://openairdocs.org/sdr/REXA2019111871638.md): Battery Pack · inoperative · Nov 17, 2019 · N927EV · Cndair CL6002B19 · Emergency Lighting
  > DURING ROUTINE CHECK FOUND BOTH FWD EXTERIOR EMERGENCY LIGHTS OUT NEXT TO PAX DOOR AND SERVICE DOOR REMOVED AND REPLACED #1 EMRGENCY BATTERY IAW JOB CARD 33-900-701 AND CHARGER IAW AMM 33-51-05. OPS CHECK GOOD NO FURTHER DEFECTS NOTED AT THIS TIME. BATTERY PO
- [SDR REXA2019082171247](https://openairdocs.org/sdr/REXA2019082171247.md): Lamp · inoperative · Aug 17, 2019 · N927EV · Cndair CL6002B19 · Emergency Lighting
  > FOUND RH FORWARD (OUTSIDE) EMERGENCY LIGHT INOP DURING ROUTINE CHECK. REPLACED THE LAMP IAW AMM 33-51-21 OPS CHECK GOOD.
- [SDR REXA2019070901090](https://openairdocs.org/sdr/REXA2019070901090.md): Light · inoperative · Jul 9, 2019 · N927EV · Cndair CL6002B19 · Emergency Lighting
  > CEILING EMERGENCY EXIT LIGHT AT ROW 7 WILL NOT ILLUMINATE. REPLACED CEILING EMERGENCY CALL LIGHT @ ROW 7 IAW MEL 33-51-14. OPS CK GOOD, OK FOR SERVICE.
- [SDR REXA2019062801019](https://openairdocs.org/sdr/REXA2019062801019.md): Floorbeam · corroded · Jun 28, 2019 · N927EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LBL 27 I/B FLOOR LANDING HAS CORROSION BETWEEN FS 559+112 AND FS 574, IN THE CARGO BAY. REPAIRED LBL27 FLOORBEAM LANDING IAW EA CRJ 253-09319 REV IR THIS IS A MAJOR REPAIR.
- [SDR REXA2019062301022](https://openairdocs.org/sdr/REXA2019062301022.md): Light · inoperative · Jun 23, 2019 · N927EV · Cndair CL6002B19 · Emergency Lighting
  > THIS IS SUPPLEMENTAL INFORMATION TO A PRIOR SUBMISSION. PART NUMBER WAS RECEIVED THAT WAS REPLACED AFTER THIS EVENT. LT AFT EMER EXIT EMER LIGHT NOT COMING ON. REMOVED AND REPLACED LIGHT BULB AT LT AFT EXTERIOR EMER LIGHT IAW CMM 33-52-06 OPS TEST ACCOMPLISHED
- [SDR REXA2019061801018](https://openairdocs.org/sdr/REXA2019061801018.md): Channel · cracked · Jun 18, 2019 · N927EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > AFT ACCY. COMPT.SYSTEM-2 HYD. MANIFOLD MOUNTING STRUCTURE CRACKED AT LOWER AFT CORNER. REMOVED/REPLACED MOUNTING STRUCTURE IAW SRM 51-42-06 LK AND OPS CK GOOD IAW AMM 12-00-06-863-801.
- [SDR REXA2019061801016](https://openairdocs.org/sdr/REXA2019061801016.md): Angle · cracked · Jun 18, 2019 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR PANEL LANDING AT FS 621 IS CRACKED JUST I/B OF THE LH FOOR SILL, IN THE CARGO BAY. REPAIRED FLOOR PANEL LANDING @ FS 621 IAW REO 601R-53-61-117.
- [SDR REXA2019061801000](https://openairdocs.org/sdr/REXA2019061801000.md): Rib · corroded · Jun 18, 2019 · N927EV · Cndair CL6002B19 · Nacelle/Pylon, Frame/Spar/Rib
  > RT PYLON O/B RIB HAS CORROSION AND PITS AROUND AFT MOUNT INNER RACE CUT-OUT. REPAIRED RT PYLON RIB IAW REO 601R-54-50-036 AND 601R-71-22-026 GAP CHECK GOOD IAW REO 601R-71-22-026 THIS IS A MAJOR REPAIR.
- [SDR REXA2019061800999](https://openairdocs.org/sdr/REXA2019061800999.md): Rib · corroded · Jun 18, 2019 · N927EV · Cndair CL6002B19 · Nacelle/Pylon, Frame/Spar/Rib
  > LT PYLON O/B RIB HAS CORROSION AND PITS AROUND AFT ENGINE MOUNT INNER RACE CUT OUT. REPAIRED LT PYLON RIB IAW REO 601R-54-50-036 AND 601R-71-22-026 GAP CHECK GOOD IAW REO 601R-71-22-026 THIS IS A MAJOR REPAIR.
- [SDR REXA2019061701012](https://openairdocs.org/sdr/REXA2019061701012.md): Rib · cracked · Jun 17, 2019 · N927EV · Cndair CL6002B19 · Elevator, Spar/Rib
  > DURING REPLACEMENT OF THE LT ELEVATOR SHEAR PINS FOUND ELEVATOR LEADING EDGE ACCESS PANEL SUPPORT RIB CRACKED. REMOVED/REPLACED LT SUPPORT RIB IAW SRM 51-42-21 AND 51-42-06.
- [SDR REXA2019061601017](https://openairdocs.org/sdr/REXA2019061601017.md): Channel · cracked · Jun 16, 2019 · N927EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > AFT ACCY. COMPT.SYSTEM-1 HYD. MANIFOLD MOUNTING STRUCTURE CRACKED AT FORWARD END. REPAIRED MOUNTING STRUCTURE IAW SRM 51-71-12 AND RESTORED FINISH IAW SRM 51-25-16 LK AND OPS CK GOOD IAW AMM 12-00-06-863-801.
- [SDR REXA2019061601006](https://openairdocs.org/sdr/REXA2019061601006.md): Floorbeam · corroded · Jun 16, 2019 · N927EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > THERE IS CORROSION AT RBL9 AT FS409+112 ON FLOORBEAM. REPAIRED FLOORBEAM AT FS409+112 AND RBL9 IAW SRM 53-00-43.
- [SDR REXA2019061601002](https://openairdocs.org/sdr/REXA2019061601002.md): Access Panel · cracked · Jun 16, 2019 · N927EV · Cndair CL6002B19 · Engine Cowling System
  > LT ENGINE LOWER PCU ACCESS PANEL 432AC IS SUSPECTED TO BE CRACKED. REMOVED AND REPLACED LOUVERS ON PANEL 432AC IAW CMM 20-42-10. APPLIED FINISH COAT IAW CMM 20-25-16.
- [SDR REXA2019061501014](https://openairdocs.org/sdr/REXA2019061501014.md): Seat Track · corroded · Jun 15, 2019 · N927EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK LT #2 HAS CORROSION. REMOVED/REPLACED SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2019061501011](https://openairdocs.org/sdr/REXA2019061501011.md): Mount Fitting · nicked · Jun 15, 2019 · N927EV · Cndair CL6002B19 · Engine Mount Section
  > RT PYLON FWD ENGINE MOUNT FITTING AFT UPPER LUG IS NICKED AT THE AFT UPPER EDGE. REPAIRED IAW REO 601R-54-51-203 THIS IS A MAJOR REPAIR.
- [SDR REXA2019061501010](https://openairdocs.org/sdr/REXA2019061501010.md): Threshold · corroded · Jun 15, 2019 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR THRESHOLD HAS SEVERAL SPOTS OF CORROSION. EVALUATED SERVICE DOOR THRESHOLD, PLACE FOUND TO BE OUT OF LIMITS. RECEIVED NEW SERVICE DOOR THRESHOLD, LOCATED AND DRILLED NEW SRM 51-42-06.
- [SDR REXA2019061501008](https://openairdocs.org/sdr/REXA2019061501008.md): Hinge · cracked · Jun 15, 2019 · N927EV · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR THRESHOLD, HINGES HAVE CORROSION AND AND CRACKS. LOCATED AND DRILLED NEW HINGES IAW SRM TR 51-42. INSTALLED ON NEW THRESHOLD PLATE IAW SRM 51-42-06.
- [SDR REXA2019061501007](https://openairdocs.org/sdr/REXA2019061501007.md): Skin · cracked · Jun 15, 2019 · N927EV · Cndair CL6002B19 · Passenger/Crew Doors
  > WHILE REMOVING CORROSION ON INNER SKIN FOUND SKIN CRACKED FWD UPPER CORNER. REPAIRED SKIN ON FWD UPPER CORNER OF PAX DOOR IAW EA CRJ252-09290.
- [SDR REXA2019061501005](https://openairdocs.org/sdr/REXA2019061501005.md): Floorbeam · corroded · Jun 15, 2019 · N927EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RBL 27 IB AND OB FLOOR PANEL LANDINGS HAS CORROSION SPOTS BETWEEN FS 589 THRU FS 610, IN THE CARGO BAY. REMOVED & REPLACED RBL 27 FLOORBEAM CAP FS589 TO FS 610 IAW SRM 51-42-21 & 51-42-22.
- [SDR REXA2019061501004](https://openairdocs.org/sdr/REXA2019061501004.md): Skin · gouged · Jun 15, 2019 · N927EV · Cndair CL6002B19 · Trailing Edge Flaps
  > RT IB FLAP LOWER SKIN HAS GOUGE OB OF PATCH ON IB END. REMOVED PREVIOUS REPAIR DOUBLER, CUTOUT ADDITIONAL GOUGE DAMAGE AND INSTALLED NEW REPAIR DOUBLER WITH FILLERS IAW SRM 57-52-00 FIG 202.
- [SDR REXA2019061401003](https://openairdocs.org/sdr/REXA2019061401003.md): Seat Track · corroded · Jun 14, 2019 · N927EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK RT #2 HAS CORROSION. REMOVED AND REPLACED RT #2 SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2019061401001](https://openairdocs.org/sdr/REXA2019061401001.md): Yoke · nicked · Jun 14, 2019 · N927EV · Cndair CL6002B19 · Engine Mount Section
  > RT ENGINE YOKE HAS NICK ON THE IB FWD EDGE. REPAIRED IAW REO 601R-71-21-078.
- [SDR REXA2019061400998](https://openairdocs.org/sdr/REXA2019061400998.md): Seat Track · corroded · Jun 14, 2019 · N927EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT AISLE SEAT STICK #4 TRACK HAS CORROSION SPOTS BETWEEN FS 559 THRU FS 559+80, IN THE CABIN. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2019061400994](https://openairdocs.org/sdr/REXA2019061400994.md): Seat Track · corroded · Jun 14, 2019 · N927EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK LT #1 HAS CORROSION. REMOVED AND REPLACED IAW AMM 53-01-11.
- [SDR REXA2019061200989](https://openairdocs.org/sdr/REXA2019061200989.md): Seat Track · corroded · Jun 12, 2019 · N927EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT AISLE SEAT STICK # 4 TRACK HAS CORROSION SPOTS BETWEEN FS 559 THRU FS 559+80, IN THE CABIN. REMOVED/REPLACED SEAT TRACK IAW AMM 53-01-11.
- [SDR REXA2019061101009](https://openairdocs.org/sdr/REXA2019061101009.md): Doubler · corroded · Jun 11, 2019 · N927EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LWR SURFACE OF DOUBLER FOR REAR SERVICING POINT BETWEEN FS559.0+112 TO FS559.0+80 AND STRR21 AND STR 24 HAS CORROSION. REPAIRED LWD SURFACE OF DOUBLER FOR REAR SERVICING POINT BETWEEN FS559.0+112 TO FS559.0+80 AND STR 21 TO STR 24 IAW EA CRJ 253-09151.
- [SDR REXA2019061000997](https://openairdocs.org/sdr/REXA2019061000997.md): Attach Angle · cracked · Jun 10, 2019 · N927EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS 280.00 FLOOR SUPPORT BEAM ATTACH ANGLE RBL 9 OTBD CRACKED. REMOVED AND REPLACED OUTBD FS 280 RBL 9 FLOORBEAM ATTACHED ANGLE IAW SRM 51-42-21.
- [SDR REXA2019061000996](https://openairdocs.org/sdr/REXA2019061000996.md): Seat Track · corroded · Jun 10, 2019 · N927EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK ON TOP OF LBL 9 HAS CORROSION BETWEEN FC 559+80 AND FS 559+ 96, IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49.
- [SDR REXA2019061000993](https://openairdocs.org/sdr/REXA2019061000993.md): Seat Track · corroded · Jun 10, 2019 · N927EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK ON TOP OF RBL 27 HAS CORROSION BETWEEN FS 559+80 AND FS 559+96, IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49.
- [SDR REXA2019061000992](https://openairdocs.org/sdr/REXA2019061000992.md): Seat Track · corroded · Jun 10, 2019 · N927EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK ON TOP OF RBL 9 HAS CORROSION BETWEEN FS 559+80 AND FS 559+96 IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49.
- [SDR REXA2019061000991](https://openairdocs.org/sdr/REXA2019061000991.md): Seat Track · corroded · Jun 10, 2019 · N927EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK ON TOP OF LBL 27 HAS CORROSION BETWEEEN FS 559+80 AND FS 559+96, IN THE CARGO BAY. REMOVED AND REPLACED SEAT TRACK IAW AM 53-00-49.

Next page: https://openairdocs.org/aircraft/N927EV/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 = 'N927EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N927EV/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.