# Service difficulty reports: N309JB

A list on [N309JB](https://openairdocs.org/aircraft/N309JB.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR EE4Y2026061224637](https://openairdocs.org/sdr/EE4Y2026061224637.md): Electrical Box · fire · Jun 12, 2026 · N309JB · Emb ERJ190100IGW · Electrical Power System
  > COOPESA REPORTS THAT A FIRE OUTBREAK OCCURRED INSIDE THE FORWARD FUSELAGE, SPECIFICALLY WITHIN THE FORWARD CARGO COMPARTMENT NEAR THE INTERNAL SIDE OF THE EXTERNAL AC POWER RECEPTACLE. THE COOPESA EMERGENCY RESPONSE TEAM ACCESSED THE AFFECTED AREA THROUGH THE
- [SDR EE4Y2026061224636](https://openairdocs.org/sdr/EE4Y2026061224636.md): Unknown · fire · Jun 12, 2026 · N309JB · Emb ERJ190100IGW · Standard Practices/Structures
  > COOPESA REPORTS THAT A FIRE OUTBREAK OCCURRED INSIDE THE FORWARD FUSELAGE, SPECIFICALLY WITHIN THE FORWARD CARGO COMPARTMENT NEAR THE INTERNAL SIDE OF THE EXTERNAL AC POWER RECEPTACLE. THE COOPESA EMERGENCY RESPONSE TEAM ACCESSED THE AFFECTED AREA BY THE FORWA
- [SDR EE4Y2026061224635](https://openairdocs.org/sdr/EE4Y2026061224635.md): Unknown · fire · Jun 12, 2026 · N309JB · Emb ERJ190100IGW · Standard Practices/Structures
  > A FIRE OUTBREAK OCCURRED INSIDE THE FORWARD FUSELAGE, SPECIFICALLY WITHIN THE FORWARD CARGO BAY NEAR THE INTERNAL SIDE OF THE EXTERNAL AC POWER RECEPTACLE. EMERGENCY RESPONSE TEAM ACCESSED THE AFFECTED AREA BY THE FWD CARGO BAY USING FIRE EXTINGUISHER. VISU
- [SDR EE4Y2026061124632](https://openairdocs.org/sdr/EE4Y2026061124632.md): Electrical Box · fire · Jun 11, 2026 · N309JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > COOPESA REPORTS THAT A FIRE OUTBREAK OCCURRED INSIDE THE FORWARD FUSELAGE, SPECIFICALLY WITHIN THE FORWARD CARGO COMPARTMENT NEAR THE INTERNAL SIDE OF THE EXTERNAL AC POWER RECEPTACLE. FROM THE MOMENT THE SPARK AND FIRE BEGAN TO THE INITIATION OF COOPESA’S EM
- [SDR EE4Y2026061124630](https://openairdocs.org/sdr/EE4Y2026061124630.md): Electrical Box · fire · Jun 11, 2026 · N309JB · Emb ERJ190100IGW · Electrical Power System
  > COOPESA REPORTS THAT A FIRE OUTBREAK OCCURRED INSIDE THE FORWARD FUSELAGE, SPECIFICALLY WITHIN THE FORWARD CARGO COMPARTMENT NEAR THE INTERNAL SIDE OF THE EXTERNAL AC POWER RECEPTACLE. THE COOPESA EMERGENCY RESPONSE TEAM ACCESSED THE AFFECTED AREA THROUGH THE
- [SDR EE4Y2026051324480](https://openairdocs.org/sdr/EE4Y2026051324480.md): Skin · corroded · May 13, 2026 · N309JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING THE STRUCTURAL INSPECTION, CORROSION SPOTS WERE FOUND ON THE EXTERNAL SKIN SURFACE BETWEEN FR16-17, AND BETWEEN STRINGERS 26R-27R, AROUND THE ANTENNA CUT-OUT AREA. THE CORROSION WAS REMOVED BY BLEND-OUT IN ACCORDANCE WITH SRM PART II 51-10-03 REQUIREMEN
- [SDR EE4Y2026051324479](https://openairdocs.org/sdr/EE4Y2026051324479.md): Skin · damaged · May 13, 2026 · N309JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING A STRUCTURAL INSPECTION, LIGHTNING STRIKE DAMAGE (LSD) WAS IDENTIFIED AT FR03 AND Y=25MM, SEE FIGURE 1. SINCE THE DAMAGE DEPTH EXCEEDED 50% OF THE SKIN THICKNESS, IT WAS REMOVED BY DRILLING THROUGH THE SKIN ONLY. AFTER REMOVING THE FRAME PRODUCTION FAST
- [SDR EE4Y2026051324478](https://openairdocs.org/sdr/EE4Y2026051324478.md): Skin · damaged · May 13, 2026 · N309JB · Emb ERJ190100IGW · Passenger/Crew Doors
  > DURING THE STRUCTURAL INSPECTION, AN EXISTING REPAIR WAS FOUND AT THE FORWARD AREA OF THE LH MLG DOOR SKIN. SINCE THE PREVIOUS OPERATOR DID NOT PROVIDE REPAIR RECORDS, THE REPAIR WAS REMOVED. AFTER REMOVAL, A SKIN CUTOUT WAS IDENTIFIED. THE SRM WAS CONSULTED
- [SDR EE4Y2026051324477](https://openairdocs.org/sdr/EE4Y2026051324477.md): Skin · damaged · May 13, 2026 · N309JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > CUSTOMER REPORTS A LIGHTNING STRIKE DAMAGE AFFECTING THE FORWARD FUSELAGE SKIN, LOCATED AT FR19 + 292 MM, STRG22R + 17 MM. A REPAIR CANNOT BE PERFORMED IN ACCORDANCE WITH ERJ190 SRM PART II, 531001, AD53 BECAUSE THE DISTANCE BETWEEN THE DAMAGE AND THE ADJACENT
- [SDR EE4Y2026051324476](https://openairdocs.org/sdr/EE4Y2026051324476.md): Skin · damaged · May 13, 2026 · N309JB · Emb ERJ190100IGW · Wing, Plate/Skin
  > THIS JOB WAS PERFORMED BY CUSTOMER REQUEST TO REDO EXISTING REPAIR LOCATED AT WING MAIN BOX - RH WING MAIN BOX LOWER SKIN AT RIB-JACKING FITTING. DUE TO THE REPAIR WAS FOUND WITH MISSING TRACEABILITY, IT WAS REMOVED AND A PERMANENT REPAIR IS PERFORMED AS PER E
- [SDR EE4Y2026051324474](https://openairdocs.org/sdr/EE4Y2026051324474.md): Skin · temp repair · May 13, 2026 · N309JB · Emb ERJ190100IGW · Wing, Plate/Skin
  > THIS JOB IS PERFORMED BY CUSTOMER REQUEST, TO REDO AN EXISTING REPAIR LOCATED AT WING MAIN BOX - CRACK FOUND L/H WING LOWER SKIN AFT EDGE BTW RIB 9-10. DUE TO THE REPAIR WAS FOUND WITH MISSING TRACEABILITY, IT WAS REMOVED AND A PERMANENT REPAIR IS PERFORMED AS
- [SDR EE4Y2026051324470](https://openairdocs.org/sdr/EE4Y2026051324470.md): Skin · damaged · May 13, 2026 · N309JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > AN EXISTING BLEND-OUT WAS IDENTIFIED AT FR78 + 290 MM, BETWEEN STRINGERS 27R-28R. THE BLEND-OUT WAS PERFORMED IN ACCORDANCE WITH SRM PART II 51-10-03, TYPE D. AFTER EVALUATION, IT WAS DETERMINED THAT THE BLEND-OUT EXCEEDS THE LIMITS SPECIFIED IN SRM PART II 53
- [SDR EE4Y2026051324469](https://openairdocs.org/sdr/EE4Y2026051324469.md): Crossbeam · damaged · May 13, 2026 · N309JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > THIS REPORT IS PERFORMED BY CUSTOMER REQUEST TO PERFORM EXISTING REPAIR LOCATED AT THE CENTER FUSELAGE II - CROSS BEAM AT FR57 WITH TOOL MARK. THIS CONDITION REPORTED WAS REPAIRED IAW ETD2017-190-026630 REV. A DTD APR 06 2017 AND DOCUMENTED UNDER COOPESA EO CO
- [SDR EE4Y2026042524380](https://openairdocs.org/sdr/EE4Y2026042524380.md): Structure · fire · Apr 25, 2026 · N309JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > DURING AIRCRAFT PREPARATION FOR MAINTENANCE, THERE WAS A FIRE OUTBREAK IN THE CARGO COMPARTMENT COMMON TO THE INTERNAL AREA OF THE EXTERNAL POWER RECEPTACLE. THIS CONDITION WAS REPORTED TO EMB. FOR ADDITIONAL DETAILS SEE JOB A1Q349 ITEM 997-6.5
- [SDR EE4Y2026042424376](https://openairdocs.org/sdr/EE4Y2026042424376.md): Skin · damaged · Apr 24, 2026 · N309JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING THE STRUCTURAL INSPECTION, EXISTING SKIN BLEND-OUTS AND LIGHTNING STRIKES DAMAGE WERE FOUND BETWEEN FR23-24, NEAR STRINGER 27R. THE BLEND-OUTS WERE REWORKED IN ACCORDANCE WITH SRM PART II 51-10-03 REQUIREMENTS. ADDITIONALLY, LIGHTNING STRIKES DAMAGE WER
- [SDR EE4Y2026042424374](https://openairdocs.org/sdr/EE4Y2026042424374.md): Skin · canning · Apr 24, 2026 · N309JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING A STRUCTURAL INSPECT, AN EXISTING REPAIR DOUBLER BETWEEN FR08 AND FR09, AND BETWEEN STRINGER 20L AND 21L WAS IDENTIFIED. ACCORDING TO PREVIOUS OPERATOR RECORDS, THIS REPAIR WAS INSTALLED IN ACCORDANCE WITH ETD2017-190-105910 GUIDELINES. THE RECORDS DID
- [SDR EE4Y2026042424373](https://openairdocs.org/sdr/EE4Y2026042424373.md): Skin · not reported · Apr 24, 2026 · N309JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING THE REMOVAL OF THE LIVE TV KA BAND CONNECTIVITY SYSTEMS STRUCTURAL PROVISIONS IN ACCORDANCE WITH SB 190-53-0125 (UNDER ETD2026-190-001029 EFFECTIVITY), THE FOLLOWING DISCREPANCIES WERE IDENTIFIED. THE SB 190-53-0125 DOES NOT INCLUDE INSTRUCTIONS TO INST
- [SDR EE4Y2026042424372](https://openairdocs.org/sdr/EE4Y2026042424372.md): Pinion · corroded · Apr 24, 2026 · N309JB · Emb ERJ190100IGW · Leading Edge Devices
  > DURING THE ACCOMPLISHMENT OF INSPECTION TASK CARD 57-40-006-0547, WE FOUND SLAT PINION #9 (LH AND RH, SLAT PINION #9 P/N: 190-03175-403) PRESENTING PITTING CORROSION. THE CONDITION IS LIMITED TO THE PINION TEETH, WITH NO MATERIAL LOSS OBSERVED. WE SEARCHED FOR
- [SDR EE4Y2026042424371](https://openairdocs.org/sdr/EE4Y2026042424371.md): Inlet · dented · Apr 24, 2026 · N309JB · Emb ERJ190100IGW · Engine Air Intake System
  > AZORRA AVIATION HOLDINGS, LLC REPORTS THAT DENTS WERE FOUND ON THE ENGINE #2 AIR INLET MODULE INNER BARREL LOWER SKIN, LOCATED BETWEEN THE 5.0 AND 7.0 O’CLOCK POSITIONS. THE DENTS WERE EVALUATED IN ACCORDANCE WITH SRM 71-61-01 AD53 AND DETERMINED TO BE OUT OF
- [SDR EE4Y2026042424370](https://openairdocs.org/sdr/EE4Y2026042424370.md): Inlet · dented · Apr 24, 2026 · N309JB · Emb ERJ190100IGW · Engine Air Intake System
  > AZORRA AVIATION HOLDINGS, LLC REPORTS THAT DENTS WERE FOUND ON THE ENGINE #1 AIR INLET MODULE INNER BARREL LOWER SKIN, LOCATED BETWEEN THE 5.0 AND 7.0 O’CLOCK POSITIONS. THE DENTS WERE EVALUATED IN ACCORDANCE WITH SRM 71-61-01 AD53 AND DETERMINED TO BE OUT OF
- [SDR EE4Y2026032624179](https://openairdocs.org/sdr/EE4Y2026032624179.md): Skin · damaged · Mar 26, 2026 · N309JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING A STRUCTURAL INSPECTION, LIGHTNING STRIKE DAMAGE (LSD) WAS IDENTIFIED AT FR03 AND Y=25MM, SEE FIGURE 1. SINCE THE DAMAGE DEPTH EXCEEDED 50% OF THE SKIN THICKNESS, IT WAS REMOVED BY DRILLING THROUGH THE SKIN ONLY. AFTER REMOVING THE FRAME PRODUCTION FAST
- [SDR EE4Y2026032624178](https://openairdocs.org/sdr/EE4Y2026032624178.md): Skin · damaged · Mar 26, 2026 · N309JB · Emb ERJ190100IGW · Landing Gear Doors
  > DURING THE STRUCTURAL INSPECTION, AN EXISTING REPAIR WAS FOUND AT THE FORWARD AREA OF THE LH MLG DOOR SKIN. SINCE THE PREVIOUS OPERATOR DID NOT PROVIDE REPAIR RECORDS, THE REPAIR WAS REMOVED. AFTER REMOVAL, A SKIN CUTOUT WAS IDENTIFIED. THE SRM WAS CONSULTED F
- [SDR EE4Y2026032624177](https://openairdocs.org/sdr/EE4Y2026032624177.md): Panel · corroded · Mar 26, 2026 · N309JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > CORROSION WAS DETECTED AT THE NLG WHEEL WELL RH PANEL, SPECIFICALLY IN THE REAR BELLCRANK REGION. THE SRM WAS CONSULTED FOR CORROSION REMOVAL AND EVALUATION, BUT NO APPLICABLE INSTRUCTIONS WERE FOUND. CONSEQUENTLY, THE CORROSION WAS REMOVED BY PERFORMING A SPO
- [SDR YENA2022032200298](https://openairdocs.org/sdr/YENA2022032200298.md): None · none · Mar 18, 2022 · N309JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE, CORROSION EXTERNAL SKIN FR88 TO FR89 BTW STRG 25R TO STRG 27R ON LOWER FUSELAGE; (RESOLVED ON W/O: 1151547 TASKCARD: NR-00008) REF AEROMAN NR 2022-124793 WO 2022 83/1 PERFORMED REPAIR LOC EXTERNAL SKIN FR88 TO FR89 BTW STRG 25R TO
- [SDR YENA2022032200297](https://openairdocs.org/sdr/YENA2022032200297.md): Slide · deployed · Mar 18, 2022 · N309JB · Emb ERJ190100IGW · Emergency Equipment
  > DURING HEAVY MAINTENANCE, DEPLOYED SLIDE NOT CONTROLLED ON DOOR 812 AFT GALLEY AREA; REF AEROMAN NR 2022- 124776 WO 2022 83/1 R & R SLIDE AT DOOR 812 AFT GALLY ARE IAW E190- AMM - 25-65-01-000-801-A
- [SDR YENA2021112300781](https://openairdocs.org/sdr/YENA2021112300781.md): Slide · deployed · Nov 22, 2021 · N309JB · Emb ERJ190100IGW · Service Doors
  > FLT 1433, MCO-SJU. L2 DOOR WAS OPENED TO ASSIST COOL AIRCRAFT. UPON CLOSING L2 DOOR FA2 NOTED THE DOOR WOULD NOT CLOSE DUE TO SLIDE OBSTRUCTION DOOR. ( SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA201712120999](https://openairdocs.org/sdr/YENA201712120999.md): Steering Sys · malfunctioned · Dec 12, 2017 · N309JB · Emb ERJ190100IGW · Landing Gear Steering System
  > FT # 234, JFK-BTV. C: UPON CLEARING THE RUNWAY STEER FAIL MESSAGE CAME ON RAN RESET STEER FAIL.MESSAGE STAYED ON. GROUND CREW TOWED WAS FROM AN ACTIVE TAXIWAY TO THE GATE; COMPILED WITH FTM 32-00-00-810-01A. FAULT CLEARED AFTER MAV RESET. FOUND TO BE TRANSITIO
- [SDR YENA201705080354](https://openairdocs.org/sdr/YENA201705080354.md): Warning Light · false activation · May 8, 2017 · N309JB · Emb ERJ190100IGW · Landing Gear Brake System
  > ON SHORT FINAL LT & RT BRAKE FAULT, DID A GO AROUND, ON SECOND APPROACH WHEN THE MMLG DOWN THE MESSAGE WENT AWAY. EMERGENCY DELCARED LANDED SAFELY WITH NORMAL BRAKING. PERFORMED BCM1 & BCM2 PRESSURE PULSE INIT TEST IAW FIM 32-41-00-810-825A. ALL TEST PASSED N
- [SDR YENA201611251019](https://openairdocs.org/sdr/YENA201611251019.md): Unknown · odor · Nov 25, 2016 · N309JB · Emb ERJ190100IGW · Air Distribution System
  > FLT 1913 MCO-CUN, AIR RETURN BACK TO MCO. UPON TAKEOFF, WHILE CLIMBING THROUGH 800 FEET A STRONG ELECTRICAL SMELL BEGAN COMING OUT OF CA VENT. STRONG FUMES; PERFORMED INSPECTION IAW FIM 21-20-00. NO FAULT FOUND. INSPECTED BORESCOPE PLUGS ON NR 1 ENGINE REF TAS
- [SDR YENA20160331270](https://openairdocs.org/sdr/YENA20160331270.md): Display · failed · Mar 31, 2016 · N309JB · Emb ERJ190100IGW · Central Display
  > ENROUTE GOT EICAS MESSAGE, RECIRCULATING SMOKE. SHORTLY AFTER, SMELLED AN ELECTRICAL ODOR. AFTER TURNING OFF RECIRCULATING FANS IAW QRH, ODOR AND CAUTION DISSIPATED, DIVERTED. ACCOMPLISHED FIM TASK 21-20-00, FOUND NR 4 DISPLAY UNIT BAD. R & R NR 4 DISPLAY
- [SDR YENA20141113248](https://openairdocs.org/sdr/YENA20141113248.md): Torque Tube · failed · Nov 13, 2014 · N309JB · Emb ERJ190100IGW · Leading Edge Devices
  > CREW DECLARED AN EMERGENCY DUE TO "SLAT FAIL" MESSAGE ON APPROACH. QRH PROCEDURE FOLLOWED, LANDED FLAP POSITION 2 SLAT 0. R & R SLAT TORQUE TUBE IAW AMM 27-81-03. PERFORMED SLAT RIGGING IAW AMM 27-80-00. OPS CHECK IAW AMM 27-80-00 FOUND NORMAL.
- [SDR YENA20141103239](https://openairdocs.org/sdr/YENA20141103239.md): Floorbeam · corroded · Nov 3, 2014 · N309JB · Emb ERJ190100IGW · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE CHECK, IT WAS NOTED FRAME 14 FLOORBEAM ON THE RBL 12 TO 35 FOUND EVIDENCE OF CORROSION. REMOVED CORROSION IAW SRM 51-10-03. REPAIRED IAW E14-669-01.
- [SDR YENA20140622120](https://openairdocs.org/sdr/YENA20140622120.md): Battery Pack · failed · Jun 22, 2014 · N309JB · Emb ERJ190100IGW · Emergency Lighting
  > EMERGENCY EXIT LIGHT BELOW LT OVERWING EXIT INOPERATIVE. R & R NR 4 EMERGENCY BATTERY PACK IAW AMM 33-30-01. OPS CHECK OF EMERGENCY EXIT LIGHTS GOOD.
- [SDR YENA20140330067](https://openairdocs.org/sdr/YENA20140330067.md): Anti-Ice System · failed · Mar 30, 2014 · N309JB · Emb ERJ190100IGW · Ice Detection
  > AFTER TAKEOFF, ANTI ICE 1 FAILED & ANTI ICE I ENG 2 FAILED, ACCOMPANIED BY A STRONG ODOR, QRH ACCOMPLISHED. ODOR DISSIPATED. F/A 1 SAID FAINT ODOR RETURNED. AT 500 FT ON APPROACH, BLEED 2 FAIL CAUTION AND DURING LANDING ICE DETECTOR 1 FAILED CAUTION ON EICA
- [SDR YENA20130718150](https://openairdocs.org/sdr/YENA20130718150.md): Position Sensor · failed · Jul 18, 2013 · N309JB · Emb ERJ190100IGW · Control Column Section
  > AIR RETURN DUE TO ELEVATOR HAS ABNORMAL FEELING/FRICTION WHILE IN FLIGHT (NO CAS MESSAGE PRESENT). TROUBLESHOT TO CONTROL COLUMN POSITION SENSOR. R & R CONTROL COLUMN POSITION SENSOR IAW AMM 27-33-01. OPS CHECK GOOD. ACFT OK TO CONTINUE.
- [SDR YENA20130619129](https://openairdocs.org/sdr/YENA20130619129.md): Pressure Switch · failed · Jun 19, 2013 · N309JB · Emb ERJ190100IGW · Engine Fuel Indicating System
  > CREW DECLARED AN EMERGENCY AND AIR RETURN TO DEPARTURE. AFTER TAKEOFF CREW RECEIVED A FUEL FEED 2 FAULT AND THEN A ENG 2 FUEL LOW PRESSURE CAS MESSAGE. QRH FOLLOWED. MESSAGES NOT CLEARED AND EJECTOR PUMP SHOWED OFF. AC PUMP 2 SHOWED GREEN BUT FUEL LINES WER
- [SDR YENA20130216044](https://openairdocs.org/sdr/YENA20130216044.md): Connector · loose · Feb 16, 2013 · N309JB · Emb ERJ190100IGW · Light System Wiring
  > FLT 6433 JFK-BNA, ON HEAVY MAINTENANCE CHECK FOUND AFT SERVICE DOOR UPPER EMERGENCY LIGHT INOP. TROUBLESHOT AND FOUND CONNECTOR GL8-L1 LOOSE ON AFT RIGHT SERVICE DOOR EMERGENCY EXIT. RE-SECURED TO LIGHT ASSEMBLY AND OPS CHECK GOOD IAW EMB E190 AMM 33-50-11 A
- [SDR YENA20120206436](https://openairdocs.org/sdr/YENA20120206436.md): Valve · failed · Feb 6, 2012 · N309JB · Emb ERJ190100IGW · Pneumatic Distribution System
  > FLT 450 SJU-SXM, AIR TURNBACK DUE TO JUST AFTER TAKEOFF, BLEED 2 STARTED FLUCTUATING FROM 2 TO 118 PSI WITH NR 1 ENGINE BLEED ON MEL. CREW PERFORMED QRH BLEED FAIL RESET, BLEED 2 CONTINUED TO FLUCTUATE. AFTER RESET FOR 3-5 MINUTES THEN STABILIZED AT 45 PSI D
- [SDR YENA20110502246](https://openairdocs.org/sdr/YENA20110502246.md): Power Unit · failed · May 2, 2011 · N309JB · Emb ERJ190100IGW · Emergency Lighting
  > FLT 6403 JFK-BNA ON GROUND FOR MAINTENANCE, FOUND UPPER EMERGENCY LIGHT ON PANEL 198NR INOP.REF EAMS NON-ROUTINE 1501 REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT 4 IAW EMB 190 AMM 33-50-01, SYSTEM OPS CHECK OK.
- [SDR YENA20110319217](https://openairdocs.org/sdr/YENA20110319217.md): Door · open · Mar 19, 2011 · N309JB · Emb ERJ190100IGW · Passenger/Crew Doors
  > FLT 1249 BOS-IAD, ON GROUND - THE FLIGHT CREW REPORTED L1 DOOR WOULD NOT DISARM. MX ENTERED A/C FROM R1 DOOR AND FOUND L1 DOOR PARTIAL OPEN WITH GIRT BAR ATTACHED TO FLOOR. RE-INSTALLED GIRT BAR TO DOOR. VISUAL INSP OF DOOR MECHANISM AND SLIDE NO DEFECTS NO
- [SDR YENA20100326042](https://openairdocs.org/sdr/YENA20100326042.md): Wire Harness · failed · Mar 26, 2010 · N309JB · Emb ERJ190100IGW · Flight Control System Wiring
  > FLT JB432 MCO-BOS INBOUND TO BOS CREW DECLARED AN EMERGENCY LANDING AFTER SELECTING FLAPS 2 RECEIVED "SLAT FAIL" AT POSITION 3, QRH PROCEDURES FOLLOWED. FLAPS OPERATED NORMALLY WHILE SLATS REMAINED AT POS 3 AIRCRAFT LANDED WITHOUT INCIDENT. BOS MX TROUBLESHO

## 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 = 'N309JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N309JB/reports

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