# Service difficulty reports: N135EV

A list on [N135EV](https://openairdocs.org/aircraft/N135EV.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 · 134 reports

- [SDR REXA2025011401094](https://openairdocs.org/sdr/REXA2025011401094.md): Bulkhead Web · corroded · Jan 13, 2026 · N135EV · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > CORROSION FOUND ON BS 280 RT BULKHEAD LOWER WEB. REPAIRED FS 280.00 R/H LOWER WEB IAW SRM 53-11-10-201-004-A01.
- [SDR REXA2025011401093](https://openairdocs.org/sdr/REXA2025011401093.md): Bulkhead Web · corroded · Jan 13, 2026 · N135EV · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > CORROSION FOUND ON BS 280 LT BULKHEAD LOWER WEB. INSTALLED BS 280 LT CAP ANGLE IAW SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, AND SRM 51-42-22-001-001-A01. FABRICATED, LOCATED AND DRILLED NEW REPAIR PARTS, LHS LOWER WEB, AND LT BUTTSTRAP, IAW SRM 53
- [SDR REXA2025011101087](https://openairdocs.org/sdr/REXA2025011101087.md): Floorbeam · cracked · Jan 3, 2026 · N135EV · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > THE LH LOWER CORROSION CAP ANGLE PN CC670-34096-2 ON THE RH FS 280 BULKHEAD IS CRACKED. REMOVED FS 280.00 BULKHEAD LH CAP ANGLE IAW CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01. LOCATED AND DRILLED NEW FS 280.00 LH CAP ANGLE P/N: CC670-34096-2S,
- [SDR REXA2026011500002](https://openairdocs.org/sdr/REXA2026011500002.md): Floorbeam · corroded · Dec 28, 2025 · N135EV · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > THE RT FS 280 FLOORBEAM HAS DEEP CORROSION AND REQUIRES REPLACEMENT. REMOVED BS 280 RT FLOORBEAM IAW SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-21-001-001-A01, INSTALLED A NEW RT BS 280 FLOORBEAM, IAW SRM 51-42-06-001-001-A01, SRM 51-42-13-
- [SDR REXA2026012000007](https://openairdocs.org/sdr/REXA2026012000007.md): Floorbeam · corroded · Dec 26, 2025 · N135EV · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > THE LH FS 280 FLOOR BEAM HAS DEEP CORROSION AND REQUIRES REPLACEMENT REMOVED FS280.00 LH CROSSBEAM IAW CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-21-001-001-A01 INSTALLED NEW LH FS 280 CROSSBEAM PN CC670-34094JP-1S IAW SRM 51-42-06-0
- [SDR REXA2026012000006](https://openairdocs.org/sdr/REXA2026012000006.md): Angle · corroded · Dec 26, 2025 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > BS 280 FWD J ANGLE IS CORRODED. REMOVED THE J ANGLE IAW SRM 51-42-06-001-001-A01, & 51-42-21-001-001-A01. LOCATED AND DRILLED NEW J-ANGLE AT FS280, P/N: CC670-34095-1S, IAW CRJ-900 SRM 51-40-11-001-001-A01. INSTALLED NEW J-ANGLE AT FS280, P/N: CC670-34095-1S
- [SDR REXA2026011500001](https://openairdocs.org/sdr/REXA2026011500001.md): Diaphragm · corroded · Dec 26, 2025 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LAVATORY STRUCTURAL LANDING BELOW FWD LAV SERVICE PORT IS CORRODED. LAVATORY DIAPHRAGM IS OUT OF LIMITS IAW SRM 53-21-23-101-005-A02, DUE TO MORE THAN 30 PERCENT OF THE LENGTH OF A MEMBER IS CORRODED. LOCATED AND DRILLED A NEW SERVICEABLE FWD LAVATORY DIA
- [SDR REXA2025011101085](https://openairdocs.org/sdr/REXA2025011101085.md): Floorbeam · corroded · Dec 26, 2025 · N135EV · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > F.S. 280 FWD J ANGLE IS CORRODED. REMOVED 280 J ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW J-ANGLE AT FS280, P/N: CC670-34095-1S, IAW CRJ-900 SRM 51-40-11-001-001-A01. INSTALLED NEW J-ANGLE AT FS280, P/N: CC6
- [SDR REXA2024123001619](https://openairdocs.org/sdr/REXA2024123001619.md): Door · cracked · Dec 29, 2024 · N135EV · Cndair CL6002D24 · Emergency Exits
  > LH AFT EE DOOR FWD LUG IS SUSPECTED TO BE CRACKED. REQUIRES EVAL COMPLIED WITH ENDEAVOR AIR EA CRJ952-17932 REV IR 12/10/2024
- [SDR REXA2024123001618](https://openairdocs.org/sdr/REXA2024123001618.md): Door · cracked · Dec 29, 2024 · N135EV · Cndair CL6002D24 · Emergency Exits
  > LH FWD EE DOOR FWD LUG IS SUSPECTED TO BE CRACKED. REQUIRES EVAL COMPLIED WITH ENDEAVOR AIR EA CRJ952-17934 REV IR 12/10/2024.
- [SDR REXA2024123001617](https://openairdocs.org/sdr/REXA2024123001617.md): Door · cracked · Dec 29, 2024 · N135EV · Cndair CL6002D24 · Emergency Exits
  > R/H AFT EMERGENCY EXIT DOOR AFT LUG CRACKED. COMPLIED WITH ENDEAVOR AIR EA CRJ952-17933 REV IR 12/10/2024.
- [SDR REXA2024121601593](https://openairdocs.org/sdr/REXA2024121601593.md): Floor Support · corroded · Dec 7, 2024 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON FLOOR SILL LEFT HAND SIDE AT FS 792 AND FS 801 ON THE OUTBOARD HOLES. COMPLIED WITH MHIRJ REO 690-53-41-506 REV-- DATED 2024-12--09
- [SDR REXA2024121001570](https://openairdocs.org/sdr/REXA2024121001570.md): None · none · Dec 4, 2024 · N135EV · Cndair CL6002D24 · Standard Practices/Structures
  > WHILE PERFORMING SERVICE BULLETIN 670BA-53-044 REVISION G, DATED JUL05/2022 FOUND FITTINGS AT STR12A LH AND RH SIDES PN CC670-33563-001SB AND CC670-33562-001SB CANNOT BE INSTALLED AS DESCRIBED IN SERVICE BULLETIN DUE TO AIRCRAFT EXISTING FASTENER PITCH COMPLIE
- [SDR REXA2023012600158](https://openairdocs.org/sdr/REXA2023012600158.md): Terminal Block · burned · Jan 20, 2023 · N135EV · Cndair CL6002D24 · Ice/Rain Protection System Wiring
  > AT 3500 MSL COCKPIT CREW NOTED METALLIC BURNING SMELL AND SMOKE FROM LOWER LEFT CORNER OF CAPTAINS WINDSHIELD NEAR VENT/POWER ELEMENT. CLEANED AND RESECURED LOOSE WIRES TO THE TERMINAL BLOCK REF AMM 56-11-01. PERFORMED OPS CHECK OF THE WINDOW TEMP CONTROLLER
- [SDR REXA2022100402177](https://openairdocs.org/sdr/REXA2022100402177.md): Lamp · inoperative · Sep 28, 2022 · N135EV · Cndair CL6002D24 · Emergency Lighting
  > R/H AFT EXTERIOR EMERG LIGHT INOP REMOVED AND REPLACED R/H AFT EXTERIOR EMERG LIGHT BULB IAW AMM 33-51-15. OPS CHECK GOOD. P/N: 8GH002473-08
- [SDR REXA2022060201044](https://openairdocs.org/sdr/REXA2022060201044.md): Fairing · cracked · May 27, 2022 · N135EV · Cndair CL6002D24 · Engine Cowling System
  > RH ENGINE UPPER COWL HINGE LINE FAIRING 443BT CRACKED PERFORMED REPAIR ON RH ENGINE UPPER COWL HINGE LINE FAIRING PER EA CRJ954-12492 REV D DATED 05/24/2022
- [SDR REXA2022060201045](https://openairdocs.org/sdr/REXA2022060201045.md): Hinge · corroded · May 25, 2022 · N135EV · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR STEP 832ET, UPPER HINGE HAS AREAS OF CORROSION CA REMOVED CORRODED UPPER HINGE AND REPLACED WITH NEW HINGE PER CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2022060201043](https://openairdocs.org/sdr/REXA2022060201043.md): Stringer · corroded · May 24, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 21R AT FS 364.00 TO FS 379.00 CORROSION PERFORMED REPAIR ON STGR 21R AT FS 364.00 TO FS 379.00 PER EA CRJ953-13542 REV IR DATED 05/05/2022
- [SDR REXA2022060201049](https://openairdocs.org/sdr/REXA2022060201049.md): Stringer · corroded · May 23, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 20R AT FS 394.00 TO 409.00 CORROSION PERFORMED REPAIR ON STGR 20R AT FS 394.00 TO 409.00 PER EA CRJ953-13497 REV IR DATED 05/03/2022
- [SDR REXA2022060201048](https://openairdocs.org/sdr/REXA2022060201048.md): Stringer · corroded · May 23, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 19R AT FS 364.00 TO FS 379.00 HAS SIGNS OF CORROSION ON UPPER SURFACE PERFORMED REPAIR ON STGR 19R AT FS 364.00 TO FS 379.00 PER EA CRJ953-13544 REV IR DATED 05/06/2022
- [SDR REXA2022060201047](https://openairdocs.org/sdr/REXA2022060201047.md): Stringer · corroded · May 23, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 21R AT FS 394.00 TO FS 409.00 CORROSION PERFORMED REPAIR ON STGR 21R AT FS 394.00 TO FS 409.00 PER EA CRJ953-13543 REV IR DATED 05/09/2022
- [SDR REXA2022060201046](https://openairdocs.org/sdr/REXA2022060201046.md): Stringer · corroded · May 23, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 20R AT FS 437.00 TO FS 453.00 CORROSION PERFORMED REPAIR ON STGR 20R FS 437.00 TO FS 453.00 PER EA CRJ953-13568
- [SDR REXA2022051900954](https://openairdocs.org/sdr/REXA2022051900954.md): Stringer · corroded · May 10, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 25R FS280.00 TO FS364.00 CORROSION PERFORMED REPAIR ON STGR 25R FROM FS 280.00 TO FS 364.00 PER EA CRJ953-12932 REV IR DATED 2/16/2022 AND CRJ953-12933 REV IR DATED 2/16/2022
- [SDR REXA2022051900955](https://openairdocs.org/sdr/REXA2022051900955.md): Splice · corroded · May 4, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 20R AT FS 477.00 CORRODED. REMOVED CORRODED JOINT SPLICE ON STGR 20R AT FS 477.00 AND REPLACED WITH NEW JOINT SPLICE ER CRJ900 SRM 51-21-06 AND 51-42-21
- [SDR REXA2022050900816](https://openairdocs.org/sdr/REXA2022050900816.md): Stringer · corroded · Apr 29, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "STGR 24R FS 280.00 TO FS 349.00 HAS SEVERAL PITS AROUND FASTENER TAILS. " PERFORMED REPAIR ON STGR 24R FROM FS 280.00 TO FS 364.00 PER EA CRJ953-13023 REV IR DATED 3/3/2022 AND EA CRJ953-12015 REV IR DATED 3/2/2022.
- [SDR REXA2022050900818](https://openairdocs.org/sdr/REXA2022050900818.md): Web · cracked · Apr 22, 2022 · N135EV · Cndair CL6002D24 · Passenger/Crew Doors
  > SUSPECTED CRACK ON PAX DOOR AFT WEB SKIN DRAG ANGLE PERFORMED REPAIR ON PAX DOOR AFT WEB SKIN DRAG ANGLE PER CRJ900 SRM 52-11-04-201-002-A01.
- [SDR REXA2022050900825](https://openairdocs.org/sdr/REXA2022050900825.md): Seal · torn · Apr 18, 2022 · N135EV · Cndair CL6002D24 · Emergency Exits
  > CREW ESCAPE HATCH HAS TORN SEAL REMOVED, REPLACED, AND LUBRICATED CREW ESCAPE HATCH IAW CRJ900 AMM 52-22-07, AMM 12-20-52, AMM 52-22-00
- [SDR REXA2022050900823](https://openairdocs.org/sdr/REXA2022050900823.md): Stringer · corroded · Apr 16, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > REPAIR REQUIRED ON STRINGER 21R FROM FS 333.00 TO FS 349.00 DUE TO CORROSION. PERFORMED REPAIR ON STRINGER 21R FROM FS 333.00 TO FS 349.00 PER EA CRJ953-13183 REV IR DATED: 4/9/2022
- [SDR REXA2022050900822](https://openairdocs.org/sdr/REXA2022050900822.md): Stringer · corroded · Apr 15, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 21R FROM FS 310.00 TO FS 333.00 CORRODED PERFORMED REPAIR ON STRINGER 21R FROM FS 310.00 TO FS 333.00 PER EA CRJ953-13182 REV IR DATED: 4/9/2022
- [SDR REXA2022050900821](https://openairdocs.org/sdr/REXA2022050900821.md): Beam · cracked · Apr 14, 2022 · N135EV · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT GAS SPRING SUPPORT BEAM CRACKED REMOVED CRACKED PAX DOOR GAS SPRING SUPPORT BEAM AND REPLACED WITH NEW BEAM. REF. CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2022050900817](https://openairdocs.org/sdr/REXA2022050900817.md): Plate · worn · Apr 12, 2022 · N135EV · Cndair CL6002D24 · Passenger/Crew Doors
  > EXCESSIVE WEAR ON PAX DOOR FWD AND AFT GUIDE PLATE BLENDED OUT LIGHT WEAR ON PAX DOOR FWD AND AFT GUIDE PLATES PER CRJ900 SRM 52-11-06-201-001-A01
- [SDR REXA2022050900820](https://openairdocs.org/sdr/REXA2022050900820.md): None · worn · Apr 8, 2022 · N135EV · Cndair CL6002D24 · Engine Cowling System
  > RH ENGINE LOWER CORE COWL RUB STRIP HAS HEAVY WEAR REMOVED WORN RH ENG. LOWER CORE COWL RUB STRIP AND REPLACED WITH NEW RUB STRIP PER EA CRJ954-13184 REV A DATED: 4/5/2022.
- [SDR REXA2022050900824](https://openairdocs.org/sdr/REXA2022050900824.md): Stringer · corroded · Apr 6, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 22R AT FS 333.00 CORRODED REMOVED AND REPLACED DAMAGED STRINGER 22R AT FS 333.00 PER CRJ900 SRM 51-42-21-001-001-A01.
- [SDR REXA2022050900819](https://openairdocs.org/sdr/REXA2022050900819.md): Stringer · corroded · Apr 6, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 26L BETWEEN FS 280.00 TO FS 364.00 CORRODED PERFORMED REPAIR ON STRINGER 26L BETWEEN FS 280.00 TO FS 364.00 PER EA CRJ953-12941 REV IR DATED 2/17/2022
- [SDR REXA2022050600815](https://openairdocs.org/sdr/REXA2022050600815.md): Channel · cracked · Apr 6, 2022 · N135EV · Cndair CL6002D24 · Cargo/Baggage Doors
  > AFT CARGO DOOR AFT TRACK LOWER U-CHANNEL SUPPORT BRACKET CRACKED REMOVED CRACKED U-CHANNEL BRACKET ON AFT CARGO DOOR AFT LOWER TRACK AND REPLACED WITH NEW BRACKET PER CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2022050500814](https://openairdocs.org/sdr/REXA2022050500814.md): Stringer · corroded · Mar 31, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 26R BETWEEN FS 280.00 TO FS 364.00 HAS CORROSION AROUND SEVERAL FASTENER TAILS. PERFORMED REPAIR ON STRINGER 26R BETWEEN FS 280.00 TO FS 364.00 PER ENGINEERING AUTHORIZATION CRJ953-12934 REV IR DATED 2/16/2022.
- [SDR REXA201808150698](https://openairdocs.org/sdr/REXA201808150698.md): Bulb · inoperative · Aug 10, 2018 · N135EV · Cndair CL6002D24 · Emergency Lighting
  > PAX DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-51-15. OPS TESTED GOOD IAW AMM 33-51-15-710-801.
- [SDR REXA201808150697](https://openairdocs.org/sdr/REXA201808150697.md): Light · worn · Aug 10, 2018 · N135EV · Cndair CL6002D24 · Emergency Lighting
  > SEVERAL EMERGENCY LIGHT STRIPS WERE WORN THROGHOUT THE CABIN. REPLACED IAW AMM 33-51-01-400-801, STEP A.
- [SDR REXA2018081520696](https://openairdocs.org/sdr/REXA2018081520696.md): Intercostal · cracked · Aug 2, 2018 · N135EV · Cndair CL6002D24 · Passenger/Crew Doors
  > AFTER REMOVAL OF PAX DOOR INNER SKIN FOUND AFT UPPER INTERCOSTAL DENTED AND CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-11, 51-42-06, AND 51-42-21.
- [SDR REXA2018081520695](https://openairdocs.org/sdr/REXA2018081520695.md): Intercostal · cracked · Aug 2, 2018 · N135EV · Cndair CL6002D24 · Passenger/Crew Doors
  > AFTER REMOVAL OF PAX DOOR INNER SKIN FOUND AFT LOWER INTERCOSTAL DENTED AND CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-11, 51-42-06, AND 51-42-21.
- [SDR REXA2018081502693](https://openairdocs.org/sdr/REXA2018081502693.md): Fitting · cracked · Aug 2, 2018 · N135EV · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR MACHINED LINTLE CRACKED AT BS 282. REPAIRED LINTLE IAW REO 670-53-21-493, REV D.
- [SDR REXA2018081530691](https://openairdocs.org/sdr/REXA2018081530691.md): Frame · corroded · Jul 30, 2018 · N135EV · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME AT BS 333, STRINGER 27 WAS FOUND CORRODED. RPAIRED THE FRAME IAW SRM 53-00-06.
- [SDR REXA2018081520690](https://openairdocs.org/sdr/REXA2018081520690.md): Intercostal · cracked · Jul 29, 2018 · N135EV · Cndair CL6002D24 · Passenger/Crew Doors
  > AFTER REMOVAL OF THE PAX DOOR INNER SKIN, FOUND FWD, UPPER INTERCOSTAL WAS DENTED AND CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06, AND 51-42-21.
- [SDR REXA2018081528688](https://openairdocs.org/sdr/REXA2018081528688.md): Floor Support · corroded · Jul 28, 2018 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFT CARGO, LBL 27 FLOOR SUPPORT WAS CORRODED, BS 1031 - 1015. REMOVED THE CORRODED SECTION OF THE FLOOR SUPPORT AND INSTALLED A REPAIR IAW REO 670-53-00-029.
- [SDR REXA2018081527687](https://openairdocs.org/sdr/REXA2018081527687.md): Hinge · cracked · Jul 27, 2018 · N135EV · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR TOP STEP 832ET INBD HINGE WAS CRACKED AND CORRODED. REMOVED & REPLACED THE DOOR STEP HINGE IAW AMM 53-11-04.
- [SDR REXA2018081526692](https://openairdocs.org/sdr/REXA2018081526692.md): Step · cracked · Jul 26, 2018 · N135EV · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR MID STEP WAS CRACKED, LT SIDE. REMOVED THE CRACK AND FOUND WITHIN LIMITS IAW SRM 52-11-04.
- [SDR REXA2018081560689](https://openairdocs.org/sdr/REXA2018081560689.md): Attach Bracket · cracked · Jul 26, 2018 · N135EV · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > NOSE HYDRAULIC COMPARTMENT, UPPER ACCUMULATOR, FWD ATACHMENT BRACKET CRACKED. REPLACED THE ATTACH BRACKET IAW SRM 51-42-21.
- [SDR REXA2018021400125](https://openairdocs.org/sdr/REXA2018021400125.md): Oxygen Mask · leaking · Feb 14, 2018 · N135EV · Cndair CL6002D24 · Crew Oxygen System
  > OBSERVER`S OXYGEN MASK LEAKING. R & R THE OBSERVER`S OXYGEN MASK IAW AMM 35-11-12, OPS CHECKED GOOD.
- [SDR REXA2018012900068](https://openairdocs.org/sdr/REXA2018012900068.md): Connector · defective · Jan 29, 2018 · N135EV · Cndair CL6002D24 · Pneumatic Indicating System
  > L BLEED DUCT WARNING CAME ON IN CRUISE FLIGHT, FOLLOWED BY RAPID DECENT TO 10000' FOLLOWED QRH CHECKLIST SUCCESSFULLY. AIRCRAFT LANDED UNEVENTFULLY. REPLACED ELBOW CONNECTIONS LT BLEED LOOP A, MT137P2, MT202P2, AND LOOP B MT203P1 IAW AMM 36-21-01 OPS TEST GOOD
- [SDR REXA2018010200008](https://openairdocs.org/sdr/REXA2018010200008.md): Bulb · inoperative · Jan 2, 2018 · N135EV · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY LIGHTS IN GALLEY RT SIDE FWD & AFT HAVE BULBS OUT. REPLACED THE BULBS, OP TESTED GOOD IAW AMM 33-51-00. P

Next page: https://openairdocs.org/aircraft/N135EV/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 = 'N135EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N135EV/reports

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