# Service difficulty reports: N266JB

A list on [N266JB](https://openairdocs.org/aircraft/N266JB.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 · 52 reports

- [SDR YENA2022060900587](https://openairdocs.org/sdr/YENA2022060900587.md): Floor Support · corroded · Jun 7, 2022 · N266JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENACE, CORR LATERAL FLOOR SUPPORT Y -1200 FR16; REF ALL WORK ACP ON TOMX W/O N266JB-1946 NR 00636 RPL FLOOR SUPPORT PER SRM 51-41-02.
- [SDR YENA2022060900586](https://openairdocs.org/sdr/YENA2022060900586.md): Spar · cracked · Jun 7, 2022 · N266JB · Emb ERJ190100IGW · Nacelle/Pylon, Frame/Spar/Rib
  > DURING HEAVY MAINTENACE, A CRACK WAS FOUND AFT BUSHING BORE RH PYLON I/B SPAR; MAJOR REPAIR - REF TOMX NR 1946-00564 - RH PYLON I/B SPAR WAS REPLACED PER EMB 190 SRM 51-43-03.
- [SDR YENA2022060900585](https://openairdocs.org/sdr/YENA2022060900585.md): Fastener · damaged · Jun 7, 2022 · N266JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENACE, LIGHTNING STRIKE FR 24 BTW STR 13L-14L CTR FUSELAGE; RE TOMX NR 1946-00023 - LIGHTNING STRIKE AT FASTENER FR 24 STR 13L-14L REPAIRED IAW EMB 190 SRM 53-00-00 REPAIR 53.
- [SDR YENA2022060900578](https://openairdocs.org/sdr/YENA2022060900578.md): Shear Tie · corroded · Jun 7, 2022 · N266JB · Emb ERJ190100IGW · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, CORROSION ON SHEAR CLIP AT FR 72 AND STGR 27-28 LH, AFT CARGO; ALL WORK ACCOMPLISHED ON TOMEX NR 00420, CORROSIÓN ON SHEAR CLIP AT FR 72 AND STGR 27-28 LH AFT CARGO WAS REMOVED AND EVALUATED, THEREFORE IT IS OUT LIMITS PER EMB 190 SR
- [SDR YENA2022060900579](https://openairdocs.org/sdr/YENA2022060900579.md): Shear Tie · corroded · Jun 7, 2022 · N266JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION ON SHEAR CLIP FR88 AND STGR 27-28 RH, AFT CARGO; ALL WORK ACCOMPLISHED ON TOMEX NRC 394, CORROSION ON SHEAR CLIP FR 88 AND STGR 27-28 RH WAS REMOVED AND EVALUATED, THEREFORE IT IS OUT LIMITS. THE SHEAR CLIP WAS REPLACED PER
- [SDR YENA2022060900580](https://openairdocs.org/sdr/YENA2022060900580.md): Floorbeam · corroded · Jun 7, 2022 · N266JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION ON FLOORBEAM AT PASSENGER CABIN FLOOR STRUCTURE FRAME 87 Y=-300; ALL WORK ACCOMPLISHED ON TOMEX NRC 00383, CORROSION ON FLOORBEAM AT PASSENGER CABIN FLOOR STRUCTURE FRAME 87 Y=-300 WAS REMOVED AND EVALUATED, THEREFORE IT IS
- [SDR YENA2022060900584](https://openairdocs.org/sdr/YENA2022060900584.md): Shear Tie · corroded · Jun 7, 2022 · N266JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION ON SHEAR CLIP AT FR 76 AND STGR 27-28 LH, AFT CARGO; WORK ACCOMPLISHED ON TOMEX NR # 00398, SHEAR CLIP AT FR 76 AND STGR 27-28 LH, AFT CARGO WAS REPLACED PER EMB 190 SRM 51-41-02, SRM 51-41-01, AND SRM 51-43-01. (CONSIDERED
- [SDR YENA2022060900583](https://openairdocs.org/sdr/YENA2022060900583.md): Shear Tie · corroded · Jun 7, 2022 · N266JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION ON SHEAR CLIP FR 87 AND STGR 27-28 RH, AFT CARGO; ALL WORK ACCOMPLISHED ON TOMEX NRC 00395, SHEAR CLIP FR 87 AND STGR 27-28 RH, AFT CARGO WAS REPLACED PER. EMB 190 SRM 51-41-02, SRM 51-41-01 AND SRM 51-43-01. (CONSIDERED AS
- [SDR YENA2022060900582](https://openairdocs.org/sdr/YENA2022060900582.md): Shear Tie · corroded · Jun 7, 2022 · N266JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION ON SHEAR CLIP AT FR 73 AND STGR 27-28 LH, AFT CARGO; ALL WORK ACCOMPLISHED ON TOMEX NRC 00410, SHEAR CLIP AT FR 73 AND STGR 27-28 LH, AFT CARGO WAS REPLACED PER. EMB 190 SRM 51-41-02, SRM 51-41-01 AND SRM 51-43-03 (CONSIDER
- [SDR YENA2022060900581](https://openairdocs.org/sdr/YENA2022060900581.md): Door Sill · corroded · Jun 7, 2022 · N266JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, ALL WORK ACCOMPLISHED ON TOMEX NR 00293, CORROSION IN LOWER SILL WHERE HOLD SLIDE FITTINGS IN FWD SERVICE DOOR CUTOUT FWD FUSELAGE STRUCTURE; ALL WORK ACCOMPLISHED ON TOMEX NR 293, CORROSION IN LOWER SILL WAS REMOVED AND EVALUATED, TH
- [SDR YENA2022060900577](https://openairdocs.org/sdr/YENA2022060900577.md): Seat · damaged · Jun 7, 2022 · N266JB · Emb ERJ190100IGW · Passenger Compartment Equipment
  > DURING HEAVY MAINTENANCE, E/F - SEATS - DIAPHRAGM FRONT TUBE HOLES - PERMANENT REPAIR - N266JB. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2022060900576](https://openairdocs.org/sdr/YENA2022060900576.md): Rib · cracked · Jun 7, 2022 · N266JB · Emb ERJ190100IGW · Wing Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, WINGS / LH WING / FIXED LEADING EDGE RIB 17 / CRACK - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2020120900580](https://openairdocs.org/sdr/YENA2020120900580.md): Rib · cracked · Nov 22, 2020 · N266JB · Emb ERJ190100IGW · Wing, Rib/Bulkhead
  > DURING HEAVY MAINTENANCE, CRACK RIB 22 LEADING EDGE INERNAL AREA ON LT WING, REF AEROMAN N/R 2020-360662. REMOVED AND REPLACED RIB 22 AND FASTENERS LOCATED ON LEADING EDGE LT WING, IAW E190 SRM 51-40-08 AND DRAWING 190-31005-409.
- [SDR YENA2020120900579](https://openairdocs.org/sdr/YENA2020120900579.md): Power Supply · failed · Nov 22, 2020 · N266JB · Emb ERJ190100IGW · Emergency Lighting
  > DURING HEAVY MAINTENANCE, INOPERABLE ELPU FWD LT IN PASSENGER CABIN, REF AEROMAN N/R 2020-360662. REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT, IAW E190 AMM 33-50-01-000-801-A. OPERATIONS CHECK GOOD, IAW E190 AMM 33-50-00-710-801-A.
- [SDR YENA2020120900578](https://openairdocs.org/sdr/YENA2020120900578.md): Power Supply · failed · Nov 22, 2020 · N266JB · Emb ERJ190100IGW · Emergency Lighting
  > DURING HEAVY MAINTENANCE, INOPERABLE AFT RT OUTBOARD ELPU IN PAX CABIN, REF AEROMAN N/R 2020- 360657. REMOVED AND REPLACED RT OUTBOARD ELPU, IAW E190 AMM 33-50-01-400-801-A. OPERATIONS CHECK GOOD, IAW E190 AMM 33-50-01-710-801-A.
- [SDR YENA201901160028](https://openairdocs.org/sdr/YENA201901160028.md): Power Unit · failed · Jan 16, 2019 · N266JB · Emb ERJ190100IGW · Emergency Lighting
  > FLT 2167, HPN-PBI. RT AFT EXTERIOR OVERWING EMERG. LIGHT INOP ( EXTERNAL EMERGENCY-OPS NOT CONDUCTED AT NIGHT); R & R EMERGENCY LIGHT POWER UNIT 243GLC PER AMM 33-50-01 OPS CHECKS OK. MDDR 375476 CLEARED, MX-4 UPDATED. PLACARD REMOVED.
- [SDR YENA201810200945](https://openairdocs.org/sdr/YENA201810200945.md): Skin · cracked · Oct 20, 2018 · N266JB · Emb ERJ190100IGW · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE CHECK AT SAL DATED 10/2018, CRACK WAS FOUND COMMON TO THE LT WING REAR LOWER SKIN PN 190-33065-009 AFT EDGE AT RIB 10. SEE REF /1/FOR DETAILS. CONTACTED FOR REPAIR DISPOSITION, AND PROVIDED THE REF /1/ ETD REPAIR, CONSISTING OF CUTTING
- [SDR YENA201710130844](https://openairdocs.org/sdr/YENA201710130844.md): Girt Bar · out of adjust · Oct 13, 2017 · N266JB · Emb ERJ190100IGW · Emergency Equipment
  > R1 DOOR WILL NOT DISARM. ADJUSTED GIRT BAR FLOOR FITTINGS IAW 52-41-00. DOOR OPS CHECKED OK, NO FURTHER DEFECTS NOTED.
- [SDR YENA201710130843](https://openairdocs.org/sdr/YENA201710130843.md): Stop Fitting · out of adjust · Oct 13, 2017 · N266JB · Emb ERJ190100IGW · Service Doors
  > R1 DOOR WILL NOT DISARM. ADJUSTED THEUPPER & AFT STOPS IAW AMM 52-41-00. OPS CHECKED GOOD.
- [SDR YENA20160921848](https://openairdocs.org/sdr/YENA20160921848.md): Beam · corroded · Sep 21, 2016 · N266JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > FWD CARGO LOWER BEAM HAS CORROSION UNDER NR 4 DOOR LATCH FITTING 10 INCHES AFT OF FRAME 26. REMOVED AND REPLACED THE BEAM IAW SRM 51-43-04.
- [SDR YENA20160921847](https://openairdocs.org/sdr/YENA20160921847.md): Seal Rest · corroded · Sep 21, 2016 · N266JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > CORROSION FWD CARGO DOOR CENTER SEAL REST AT FRAME 25 APROX. 12 INCHES AFT. REMOVED AND REPLACED FWD CARGO DOOR SEAL REST IAW SRM 51-41-01.
- [SDR YENA20160921846](https://openairdocs.org/sdr/YENA20160921846.md): Structure · corroded · Sep 21, 2016 · N266JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > FWD RIGHT STRUCTURE CORRODED 4.75 INCHES AFT OF FRAME 13 AND RBL 37. REMOVED CORROSION IAW SRM 51-12-01.
- [SDR YENA20160921845](https://openairdocs.org/sdr/YENA20160921845.md): Structure · corroded · Sep 21, 2016 · N266JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > FWD RT STRUCTURE CORRODED 5.25 INCHES AFT OF FRAME 12 AND RBL 36.25. REMOVED AND REPLACED IAW SRM 51-43-04, AND 51-41-02.
- [SDR YENA20160921844](https://openairdocs.org/sdr/YENA20160921844.md): Shear Tie · corroded · Sep 21, 2016 · N266JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > SHEAR TIE CORRODED AT FRAME 84 STRINGERS 27-28L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-01, 51-41-02, AND 51-21-01.
- [SDR YENA20160921843](https://openairdocs.org/sdr/YENA20160921843.md): Mount · corroded · Sep 21, 2016 · N266JB · Emb ERJ190100IGW · Fuselage Main, Attach Fittings
  > FWD LAVATORY MOUNT FITTING CORRODED 6.5 INCHES AFT OF FRAME 15 AND LBL 44. REMOVED AND REPLACED THE MOUNT FITTING IAW SRM 51-43-03.
- [SDR YENA20160921842](https://openairdocs.org/sdr/YENA20160921842.md): Skin · corroded · Sep 21, 2016 · N266JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > CORROSION AFT CARGO DOOR LOWER CUTOUT AT FRAME 77, 6' AFT. REMOVED CORROSION IAW SRM 51-10-03. FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.
- [SDR YENA20160921841](https://openairdocs.org/sdr/YENA20160921841.md): Skin · corroded · Sep 21, 2016 · N266JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > CORROSION AFT CARGO DOOR LOWER CUTOUT AT FRAME 77, 14' AFT. REMOVED CORROSION IAW SRM 51-10-03. FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.
- [SDR YENA20160921840](https://openairdocs.org/sdr/YENA20160921840.md): Skin · corroded · Sep 21, 2016 · N266JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > CORROSION AFT CARGO DOOR LOWER CUTOUT AT FRAME 77, 16' AFT. REMOVED CORROSION IAW SRM 51-10-03. FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.
- [SDR YENA20160921839](https://openairdocs.org/sdr/YENA20160921839.md): Skin · corroded · Sep 21, 2016 · N266JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > CORROSION AFT CARGO DOOR LOWER CUTOUT AT FRAME 78, 5' AFT. REMOVED CORROSION IAW SRM 51-10-03. FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.
- [SDR YENA20160921838](https://openairdocs.org/sdr/YENA20160921838.md): Skin · corroded · Sep 21, 2016 · N266JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > CORROSION AFT CARGO DOOR LOWER CUTOUT AT FRAME 78, 5' AFT. REMOVED CORROSION IAW SRM 51-10-03. FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.
- [SDR YENA20160921837](https://openairdocs.org/sdr/YENA20160921837.md): Finger Doubler · corroded · Sep 21, 2016 · N266JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > CORROSION FWD CARGO DOOR AFT FINGER DOUBLER AT FRAME 26, 1 INCH AFT. REMOVED AND REPLACED THE FINGER DOUBLER IAW SRM 51-10-03. FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.
- [SDR YENA20160921836](https://openairdocs.org/sdr/YENA20160921836.md): Finger Doubler · corroded · Sep 21, 2016 · N266JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > CORROSION FWD CARGO DOOR AFT FINGER DOUBLER AT FRAME 27, 1.5 INCHES AFT. REMOVED AND REPLACED THE FINGER DOUBLER. FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.
- [SDR YENA20160921835](https://openairdocs.org/sdr/YENA20160921835.md): Finger Doubler · corroded · Sep 21, 2016 · N266JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > CORROSION FWD CARGO DOOR AFT FINGER DOUBLER AT FRAME 24, 13.5 INCHES AFT. REMOVED AND REPLACED THE FINGER DOUBLER IAW SRM 51-10-03. FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.
- [SDR YENA20160921834](https://openairdocs.org/sdr/YENA20160921834.md): Finger Doubler · corroded · Sep 21, 2016 · N266JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > CORROSION FWD CARGO DOOR AFT FINGER DOUBLER AT FRAME 25, 15.5 INCHES AFT. REMOVED AND REPLACED THE FINGER DOUBLER IAW SRM 51-23-04, 51-23-05, AND 51-23-06.
- [SDR YENA20160921833](https://openairdocs.org/sdr/YENA20160921833.md): Finger Doubler · corroded · Sep 21, 2016 · N266JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > CORROSION ON AFT CARGO DOOR FWD FINGER DOUBLER FRAME 78. REMOVED THE CORROSION IAW SRM 51-10-03, AND FOUND OUT OF LIMITS. REPLACED THE FINGER DOUBLER IAW NR00103.
- [SDR YENA20160921832](https://openairdocs.org/sdr/YENA20160921832.md): Finger Doubler · corroded · Sep 21, 2016 · N266JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > CORROSION ON THE AFT CARGO DOOR FWD LOWER FINGER DOUBLER AT FRAME 77. REMOVED THE CORROSION IAW SRM 51-10-03. FOUND TO BE OUT OF LIMITS. REPLACED THE FINGER DOUBLER.
- [SDR YENA20160921831](https://openairdocs.org/sdr/YENA20160921831.md): Finger Doubler · corroded · Sep 21, 2016 · N266JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > CORROSION ON AFT CARGO DOOR FWD FINGER DOUBLER AT FRAME 77. REMOVED THE CORROSION, AND FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.
- [SDR YENA20160921830](https://openairdocs.org/sdr/YENA20160921830.md): Finger Doubler · corroded · Sep 21, 2016 · N266JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > CORROSION AFT CARGO DOOR FORWARD LOWER FINGER DOUBLER FRAME 77. REPLACED THE FINGER DOUBLER IAW SRM 51-43-03, 51-43-04, AND 51-23-06.
- [SDR YENA20160921829](https://openairdocs.org/sdr/YENA20160921829.md): Finger Doubler · corroded · Sep 21, 2016 · N266JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > AFT CARGO DOOR AFT LOWER FINGER DOUBLER FRAME 80 CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-10-03. DOUBLER REPLACED.
- [SDR YENA20160921828](https://openairdocs.org/sdr/YENA20160921828.md): Finger Doubler · corroded · Sep 21, 2016 · N266JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > CORROSION AFT CARGO DOOR AFT LOWER FINGER DOUBLER FRAME 79. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-75-16. REPLACED THE FINGER DOUBLER IAW NR 00105.
- [SDR YENA20160921827](https://openairdocs.org/sdr/YENA20160921827.md): Finger Doubler · corroded · Sep 21, 2016 · N266JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > CORROSION ON AFT CARGO DOOR AFT LOWER FINGER DOUBLER FRAME 79. REMOVED AND REPLACED THE FINGER DOUBLER IAW SRM 51-43-03, 51-43-04, AND 51-23-06.
- [SDR YENA20140720138](https://openairdocs.org/sdr/YENA20140720138.md): Warning Message · false activation · Jul 20, 2014 · N266JB · Emb ERJ190100IGW · Central Warning
  > ACFT DIVERTED DUE TO "AVNX MAU 1A FAIL" ON EICAS IN FLIGHT. ACCOMPLISHED EBIT, PBIT AND RETURN TO SERVICE TEST IAW AMM 27-00-00-070-801-A. NO FURTHER FAULTS NOTED. ACFT GOOD FOR SERVICE.
- [SDR YENA20140518095](https://openairdocs.org/sdr/YENA20140518095.md): Power Supply · failed · May 18, 2014 · N266JB · Emb ERJ190100IGW · Emergency Lighting
  > ON MAINTENANCE CHECK, FOUND R1 DOOR LOWER EXIT LIGHT INOPERATIVE. TROUBLESHOOTING FOUND POWER SUPPLY OUTPUT BAD. R & R RT FWD EMERGENCY LIGHT POWER SUPPLY, REF AMM 33-50-00. OPS CHECKS NORMAL.
- [SDR YENA20140209020](https://openairdocs.org/sdr/YENA20140209020.md): Processor · failed · Feb 9, 2014 · N266JB · Emb ERJ190100IGW · Central Computers
  > AIRCRAFT DIVERTED, AVNX MAU 3 FAIL, YD OFF. APPLIED T/S PROCEDURES, FOUND NIC PROC 6 FAILED. R & R NIC PROC 6 IAW AMM 31-41-04. NO FAULTS, OP'S CHECK OK.
- [SDR YENA20130530116](https://openairdocs.org/sdr/YENA20130530116.md): Slide · defective · May 30, 2013 · N266JB · Emb ERJ190100IGW · Escape Slide
  > CREW REPORTED L2 DOOR WILL NOT DISARM. R & R L2 DOOR VENT FLAP CAM IAW AMM 52-12-25 AND L2 DOOR SLIDE IAW AMM 25-65-01. OPS CHECK OK.
- [SDR YENA20130131025](https://openairdocs.org/sdr/YENA20130131025.md): Controller · failed · Jan 31, 2013 · N266JB · Emb ERJ190100IGW · Cabin Pressure Controller
  > FLT 1731 JFK-BDA, AIR TURNBACK TO JFK DUE TO BLEED 1 AND 2 FAILED ON TAKEOFF AT TO-1. RESET SUCCESSFUL REPEAT AT 11000FT. FAILED AGAIN BLEEDS 1 AND 2. REMOVED AND REPLACED ENGINE NR 1 PRSOV AS PER AMM 36-11-03. REMOVED AND REPLACED HP BLEED VALVE NR 2 AS P
- [SDR YENA20130131024](https://openairdocs.org/sdr/YENA20130131024.md): Bleed Valve · failed · Jan 31, 2013 · N266JB · Emb ERJ190100IGW · Pneumatic Distribution System
  > FLT NR 1731 JFK-BDA, AIR TURNBACK TO JFK DUE TO BLEED 1 AND 2 FAILED ON TAKEOFF AT TO-1. RESET SUCCESSFUL REPEAT AT 11000F. FAILED AGAIN BLEEDS 1 AND 2. REMOVED AND REPLACED ENGINE NR 1 PRSOV AS PER AMM 36-11-03. REMOVED AND REPLACED HP BLEED VALVE NR 2 AS
- [SDR YENA20130131023](https://openairdocs.org/sdr/YENA20130131023.md): Shutoff Valve · failed · Jan 31, 2013 · N266JB · Emb ERJ190100IGW · Pneumatic Distribution System
  > FLT 1731 JFK-BDA, AIR TURNBACK TO JFK DUE TO BLEED 1 AND 2 FAILED ON TAKEOFF AT TO-1. RESET SUCCESSFUL REPEAT AT 11000FT. FAILED AGAIN BLEEDS 1 AND 2. REMOVED AND REPLACED ENGINE NR 1 PRSOV AS PER AMM 36-11-03. REMOVED AND REPLACED HP BLEED VALVE NR 2 AS P
- [SDR YENA20120624534](https://openairdocs.org/sdr/YENA20120624534.md): Power Unit · failed · Jun 24, 2012 · N266JB · Emb ERJ190100IGW · Emergency Lighting
  > FLT 1018 JFK-BOS, ON GROUND CHECK FOUND R2 DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT FOR R2 DOOR IAW AMM 33-50-01-04. OPS CHECK GOOD.
- [SDR YENA20100905123](https://openairdocs.org/sdr/YENA20100905123.md): Bleed Air Sys · failed · Sep 5, 2010 · N266JB · Emb ERJ190100IGW · Pneumatic Distribution System
  > FLT 331 IAD-MCO, AIR RETURN TO IAD DUE TO SMOKE AND HAZE IN ENTIRE AIRCRAFT PRIOR TO ROTATION FOLLOWED BY BLEED 1 FAIL AT APPROX 1000 FEET. CREW DECLARED EMERGENCY AND A/C RETURN TO FIELD. PERFORMED VISUAL INSPECTION PER FIM 21-20-00-810-801-A AND NO DEFECTS

Next page: https://openairdocs.org/aircraft/N266JB/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 = 'N266JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N266JB/reports

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