# Service difficulty reports: N284JB

A list on [N284JB](https://openairdocs.org/aircraft/N284JB.md).

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

- [SDR YENA2024121801568](https://openairdocs.org/sdr/YENA2024121801568.md): Seal · leaking · Dec 18, 2024 · N284JB · Emb ERJ190100IGW · Passenger/Crew Doors
  > FLT#2354, DCA-BOS. 'LOUD WIND SOUND FROM L1 DOOR FOR ENTIRE DURATION OF FLIGHT; REMOVED AND REPLACED L1 FWD PASS DOOR SEAL - REF AMM 52-11-21. OPS & LEAK CHECKS ON L/P# 4191373, ITEM 1.'
- [SDR YENA2024121601563](https://openairdocs.org/sdr/YENA2024121601563.md): Door Sill · damaged · Dec 13, 2024 · N284JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > FLT#216, BUS-BOS. 'FA & AO SAYS L1 DOOR MAKES AN UNUSUAL "POP" WHEN OPENING THE L1 DOOR; REPLACED L1 DOOR PROTECTIVE SILL PER AMM 53-10-22. OPS CHK OF L1 DOOR NORMAL. A/C OK TO CONT. SVC.'
- [SDR YENA2024091601271](https://openairdocs.org/sdr/YENA2024091601271.md): Controller · malfunctioned · Sep 13, 2024 · N284JB · Emb ERJ190100IGW · Pneumatic Indicating System
  > FLT#455, BOS-JFK. 'INFLIGHT (WHILE ALREADY OPERATING W/MEL 36-00-00A) XBLEED FAIL EICAS MESSAGE PRESENTED AND AMBER X WAS DISPLAYED ON ECS SYNOPTICS PAGE; FOLLOWING FIM TASK 36-10-00-810-801-A00 FOUND AMS CH2 TO ERRONEOUSLY SHOW XBLEED VALVE X'D OUT. RESET AMS
- [SDR YENA2024070800946](https://openairdocs.org/sdr/YENA2024070800946.md): Module · failed · Jul 3, 2024 · N284JB · Emb ERJ190100IGW · Aileron Control System
  > FLT#2186, PIT-BOS. (AIRCRAFT DECLARED AN EMERGENCY INTO BOS). 'AT FL 370 MO 78 SIGNIFICANT VIBRATION IN CONTROL YOKE. SUSPECT IN ROLL AXIS PSHMABAY APPROX 60HZ "SHAKER ANTICIPATED EICAS MESSAGE APPEARED. QRH CHECKLIST EXECUTED, ADDITIONAL INFO LIGHT ICING ENCO
- [SDR YENA2024031200410](https://openairdocs.org/sdr/YENA2024031200410.md): Light · inoperative · Mar 11, 2024 · N284JB · Emb ERJ190100IGW · Emergency Lighting
  > DURING HEAVY MAINTENANCE: LH EMERGENCY EXIT DOOR SIDEWALL PANEL LIGHT IS INOP; REF. EAMS W/O: H9427 NR00721 - R&R EMERGENCY LIGHT ASSEM. #4 PER EMB 190-33-50-01-400-801-A. OPS OK.
- [SDR YENA2023082500991](https://openairdocs.org/sdr/YENA2023082500991.md): Unknown · unknown · Aug 20, 2023 · N284JB · Emb ERJ190100IGW · Flight Compartment Lighting
  > FLT#655, SYR-MCO. 'COCKPIT EMER LIGHT NOT TURNING ON DURING EMER LIGHT TEST; CYCLED POWER OPERATIONAL CHECK NORMAL PER AMM 33-11-60.'
- [SDR YENA2023072200848](https://openairdocs.org/sdr/YENA2023072200848.md): Unknown · unknown · Jul 23, 2023 · N284JB · Emb ERJ190100IGW · Emergency Equipment
  > FLT#1954, DCA-BOS. 'UPON INSPECTION FOUND L2 DOOR SLIDE INTERFERE WITH L AFT FA SEAT; REMOVED AND REPLACED L2 DOOR SLIDE IAW AMM TASK CARD 25-65-01.
- [SDR YENA2023051900542](https://openairdocs.org/sdr/YENA2023051900542.md): Unknown · unknown · May 10, 2023 · N284JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > FLT#8448, CUN-BOS. 'GOUGE BELOW L1 DOOR NEEDS TO BE REPAIRED; DAMAGE REPAIRED PER EC# E23-355-02,' (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023040400313](https://openairdocs.org/sdr/YENA2023040400313.md): Power Supply · failed · Mar 31, 2023 · N284JB · Emb ERJ190100LR · Emergency Lighting
  > FLT#884, MCO-JFK. 'L1 DOOR EXIT SIGN INOP; REMOVED AND REPLACED FWD L/H ELPU IAW AMM 33-50-01. OPS TEST GOOD.'
- [SDR YENA2023033100308](https://openairdocs.org/sdr/YENA2023033100308.md): Power Supply · failed · Mar 31, 2023 · N284JB · Emb ERJ190100LR · Emergency Lighting
  > FLT#884, MCO-JFK. 'L1 DOOR EXIT SIGN INOP; REMOVED AND REPLACED FWD L/H ELPU IAW AMM 33-50-01. OPS TEST GOOD.'
- [SDR YENA2023030700216](https://openairdocs.org/sdr/YENA2023030700216.md): None · none · Mar 3, 2023 · N284JB · Emb ERJ190100LR · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION IN SEAT TRACK LOCATED Y= - 270.0 AND BETWEEN FR 84/85 AT CF III PASSENGER CABIN FLOOR STRUCTURE; ALL WORK ACCOMPLISHED ON TOMEX NRC 000110, SEAT TRACK LOCATED BETWEEN FR 84/85 AT CF III PASSENGER CABIN FLOOR STRUCTURE WAS R
- [SDR YENA2023030700215](https://openairdocs.org/sdr/YENA2023030700215.md): None · none · Mar 3, 2023 · N284JB · Emb ERJ190100LR · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION IN DOUBLER OF WASTE ACCESS DOOR CUTOUT LOCATED BETWEEN FR 88/89 AND STRG 27R/28R AT CF III AFT CARGO COMPARTMENT INTERNAL STRUCTURE; ALL WORK ACCOMPLISHED ON TOMEX NRC 00128. DOUBLER OF THE WASTE ACCESS DOOR CUTOUT LOCATED B
- [SDR YENA2023030700214](https://openairdocs.org/sdr/YENA2023030700214.md): None · none · Mar 3, 2023 · N284JB · Emb ERJ190100LR · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION IN SHEAR CLIP LOCATED IN FR 84 AND BETWEEN STRG 27R/28R AT CF III INTERNAL STRUCTURE AFT CARGO COMPARTMENT; ALL WORK ACCOMPLISHED ON TOMEX NRC 00095: CORROSION IN SHEAR CLIP LOCATED IN FR 84 AND BETWEEN STRG 27R/28R AT CF II
- [SDR YENA2023030700213](https://openairdocs.org/sdr/YENA2023030700213.md): None · none · Mar 3, 2023 · N284JB · Emb ERJ190100LR · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION IN THE SHEAR CLIP LOCATED IN FR 88 AND BETWEEN STRG 27R/28R AT CF III INTERNAL STRUCTURE AFT CARGO COMPARTMENT; ALL WORK ACCOMPLISHED ON TOMEX NRC 00097, SHEAR CLIP LOCATED IN FR 88 AND BETWEEN STRG 27R/28R AT CF III INTERN
- [SDR YENA2023030700212](https://openairdocs.org/sdr/YENA2023030700212.md): None · none · Mar 3, 2023 · N284JB · Emb ERJ190100LR · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION IN THE SHEAR CLIP LOCATED IN FR 86 AND BETWEEN STRG 27R/28R AT CF III INTERNAL STRUCTURE AFT CARGO COMPARTMENT; ALL WORK ACCOMPLISHED ON TOMEX NRC 00098, SHEAR CLIP LOCATED IN FR 86 AND BETWEEN STRG 27R/28R WAS REPLACED PER
- [SDR YENA2023030700211](https://openairdocs.org/sdr/YENA2023030700211.md): None · none · Mar 3, 2023 · N284JB · Emb ERJ190100LR · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION IN THE SHEAR CLIP LOCATED IN FR 87 AND BETWEEN STRG 27R/28R AT CF III INTERNAL STRUCTURE AFT CARGO COMPARTMENT; ALL WORK ACCOMPLISHED ON TOMEX NRC 00096, SHEAR CLIP LOCATED IN FR 87 AND BETWEEN STRG 27R/28R WAS REPLACED PER
- [SDR YENA2023030700210](https://openairdocs.org/sdr/YENA2023030700210.md): None · none · Mar 3, 2023 · N284JB · Emb ERJ190100LR · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: [CPCP FINDING]: CORROSION ON SHEAR CLIP LOCATED ON FR-76 BETWEEN STRG-23L/24L; ALL WORK ACCOMPLISHED ON TOMEX NRC 00078, SHEAR CLIP LOCATED ON FR-76 BETWEEN STRG-23L/24L WAS REPLACED PER EMB190 SRM 51-41-01 AND SRM 51-41-02. (CONSIDER
- [SDR YENA2023030700209](https://openairdocs.org/sdr/YENA2023030700209.md): None · none · Mar 3, 2023 · N284JB · Emb ERJ190100LR · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION IN THE SHEAR CLIP LOCATED IN FR 83 AND BETWEEN STRG 28R/27R AT CF III INTERNAL STRUCTURE AFT CARGO COMPARTMENT; ALL WORK ACCOMPLISHED ON TOMEX NRC 00094, SHEAR CLIP LOCATED IN FR 83 AND BETWEEN STRG 28R/27R WAS REPLACED PER
- [SDR YENA2023030700208](https://openairdocs.org/sdr/YENA2023030700208.md): None · none · Mar 3, 2023 · N284JB · Emb ERJ190100LR · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III / FR84 & Y-270 SEAT TRACK EXISTING REPAIR / CORROSION -PERMANENT REPAIR. (CONSIDERED AS A MAOR REPAIR)
- [SDR YENA2021010800023](https://openairdocs.org/sdr/YENA2021010800023.md): Not Reported · not reported · Jan 3, 2021 · N284JB · Emb ERJ190100IGW · Fuselage Structure (General)
  > DURING HMV, EC E20-834-01. THIS IS CLASSIFIED AS A MAJOR REPAIR.
- [SDR YENA2021010800022](https://openairdocs.org/sdr/YENA2021010800022.md): Rib · cracked · Jan 3, 2021 · N284JB · Emb ERJ190100IGW · Wing, Rib/Bulkhead
  > DURING HMV, CRACK RIB 27 LEADING EDGE INTERNAL AREA ON LT WING, REF AEROMAN NR W/O 2020-368/1 WCC 2020-393240. REMOVED AND REPLACED NEW RIB 27 AND FASTENERS ON LT WING, IAW E190 SRM 51-40-08 AND DRAWING 191-03201-421.
- [SDR YENA2021010800021](https://openairdocs.org/sdr/YENA2021010800021.md): Rib · cracked · Jan 3, 2021 · N284JB · Emb ERJ190100IGW · Wing, Rib/Bulkhead
  > DURING HMV, CRACK RIB 17 LEADING EDGE INTERNAL AREA ON RT WING, REF AEROMAN NR W/O 2020-368/1 WCC 2020-393251. REMOVED AND REPLACED NEW RIB 17 AND FASTENERS ON RT WING, IAW E190 SRM 51-40-08 AND DRAWING 191-03201-421. PERFORMED APPLIED PROMOTER ADHESIVE ON R
- [SDR YENA2021010800020](https://openairdocs.org/sdr/YENA2021010800020.md): Rib · cracked · Jan 3, 2021 · N284JB · Emb ERJ190100IGW · Wing, Rib/Bulkhead
  > DURING HMV, CRACK RIB 17 LEADING EDGE INTERNAL AREA ON RT WING. REMOVED AND REPLACED NEW RIB 17 AND FASTENERS ON RT WING, IAW E190 SRM 51-40-08 AND DRAWING 191-03201-421. PERFORMED APPLIED PROMOTER ADHESIVE ON RIVETS RIB 17 LOCATED INSIDE THE FUEL TANK ON RT
- [SDR YENA2021010800019](https://openairdocs.org/sdr/YENA2021010800019.md): Support Web · cracked · Jan 3, 2021 · N284JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HMV, CRACK INTERNAL STRUCTURES SUPPORT WEB LOCATED CENTER WING TO FUSELAGE FAIRING AREA ON LOWER FUSELAGE, REF AEROMAN N/R 2020-393373 WO 2020 368/1. PERFORMED PERMENANT REPAIR TO CENTER FUSELAGE II WF RT REAR WEB CRACK AND CORROSION, PER AEROMAN EA53-
- [SDR YENA2020021730173](https://openairdocs.org/sdr/YENA2020021730173.md): Battery · failed · Feb 13, 2020 · N284JB · Emb ERJ190100IGW · Emergency Lighting
  > FT # 1579, DCA-FLL. R/H EXTERIOR EMERG LIGHT BELOW EMERG EXIT WON'T COME ON; R & R BATT POWER UNIT AMM 33-50-01. OPS CHECK NORM. A/C OK TO CONT.
- [SDR YENA2019103010626](https://openairdocs.org/sdr/YENA2019103010626.md): Mount · cracked · Oct 1, 2019 · N284JB · Emb ERJ190100IGW · Engine Mount Section
  > FT # 2601, BUF-JFK. FOUND CRACK ON PYLON LOWER LINK LUG ENG #1 INBD SIDE; REF LOGPAGE # 2482048-1 W/O# 1019537 FOR WORK PERFORMED. REF AEROMAN NR 2019-341092 WO 2019 35211 ACCOMPLISHED THE REPLACEMENT OF THE LH PYLON INBOARD UPPER SPAR WING USING ALTERNATE TOO
- [SDR YENA2018120620811](https://openairdocs.org/sdr/YENA2018120620811.md): Life Raft · damaged · Dec 2, 2018 · N284JB · Emb ERJ190100IGW · Life Raft
  > FT # 395, HPN-MCO. INFLIGHT REPORTED AFT LIFE-RAFT BINDING IS UNRAVELING; REMOVED + REPLACED R/H AFT LIFE-RAFT IAW EMM 21-66-01
- [SDR YENA201701010001](https://openairdocs.org/sdr/YENA201701010001.md): Cable · failed · Jan 1, 2017 · N284JB · Emb ERJ190100IGW · Service Doors
  > FLT 79, DCA-FLL. FLIGHT CREW NOTIFIED MAINTENANCE THAT R1 SERVICE DOOR UNABLE TO DISARM. R & R R1 DOOR BALL FLEX CABLE IAW SB 190-52-0042 & EC E17-001-01.
- [SDR YENA20150611191](https://openairdocs.org/sdr/YENA20150611191.md): Shear Tie · corroded · Jun 11, 2015 · N284JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE, FOUND A CORRODED SHEAR TIE AT FRAME 78 BETWEEN STRINGERS 27 & 28L R & R THE SHEAR TIE AND TOP COATED RIVET HEADS. IAW SRM 51-40-01, 51-40-02, AND 51-23-06.
- [SDR YENA20150611190](https://openairdocs.org/sdr/YENA20150611190.md): Beam · corroded · Jun 11, 2015 · N284JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE FOUND CORROSION AFT CABIN PASSENGER DOOR LOWER BEAM FRAMES 85-87, STR 17L AROUND GIRT BAR. BLENDED AFFECTED AREA IAW SRM 51-10-08 PERFORMED HFEC PRIMED AND PAINTED AFFECTED AREA.
- [SDR YENA20150611189](https://openairdocs.org/sdr/YENA20150611189.md): Shear Tie · corroded · Jun 11, 2015 · N284JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE FOUND CORRODED SHEAR TIE AT FR 88 BETWEEN STR 27 & 28R. INSTALLED A NEW SHEAR TIE IAW SRM 51-41-01 AND 51-41-02 PRIMED TOPCOATED RIVETS HEADS IAW SRM 51-23-05 51-23-06.
- [SDR YENA20130807171](https://openairdocs.org/sdr/YENA20130807171.md): Unknown · odor · Aug 7, 2013 · N284JB · Emb ERJ190100IGW · Air Distribution System
  > AFTER TAKEOFF, A PUNGENT, STAGNANT, DIRTY, MUSKY ODOR UNLIKE BURNING OR SMOKE, FILLED THE ACFT COCKPIT AND CABIN. WENT AWAY WITHIN 10 MINUTES. NO EICAS OR OTHER DEFECTS NOTED. ACCOMPLISHED TC 21-20-00-810-803A. REPLACED BOTH RECIRCULATING FILTERS IAW 21-24-
- [SDR YENA20130604124](https://openairdocs.org/sdr/YENA20130604124.md): Light · inoperative · Jun 4, 2013 · N284JB · Emb ERJ190100IGW · Emergency Lighting
  > DURING HEAVY MX CHECK, DISCOVERED RT AFT EMERGENCY EXTERIOR EXIT LIGHT FOUND INOPERATIVE. REMOVED AND REPLACED RT AFT EMERGENCY EXIT LIGHT IAW AMM 33-50-25.
- [SDR YENA20130508098](https://openairdocs.org/sdr/YENA20130508098.md): Audio Panel · failed · May 8, 2013 · N284JB · Emb ERJ190100IGW · Audio Integrating System
  > FLT 1717 MCO-SDQ, #2 ACP (AUDIO CONTROL PANEL) FAILED IN FLIGHT (WENT BLACK) WITH COMM AUDIO 2 BREAKER POPPED. BREAKER POPPED 1 HOUR AFTER TAKEOFF WITH A NOTICEABLE BURNING SMELL. SMELL WENT AWAY AFTER BREAKER POPPED. REMOVED AND REPLACED NR 2 DAP (DIGITAL
- [SDR YENA20120922607](https://openairdocs.org/sdr/YENA20120922607.md): Controller · failed · Sep 22, 2012 · N284JB · Emb ERJ190100IGW · Windshield/Door Rain/Ice Removal
  > FLT 559 HPN-TPA, CREW DECLARED EMERGENCY DUE TO DESCENDING THRU 17000, CAPTAIN WINDSHIED SHATTERED. EICAS MESSAGE APPEARED "WINDSHIELD 1 HEATER FAIL". REMOVED AND REPLACED WINDSHIELD HEAT CONTROLLER IAW AMM 30-42-01. OPS TEST IAW AMM 30-42-00 TASK 30-42-00-
- [SDR YENA20120922606](https://openairdocs.org/sdr/YENA20120922606.md): Windshield · cracked · Sep 22, 2012 · N284JB · Emb ERJ190100IGW · Flight Compartment Windows
  > FLT 559 HPN-TPA, CREW DECLARED EMERGENCY DUE TO DESCENDING THRU 17000, CAPTAIN WINDSHIELD SHATTERED. EICAS MESSAGE APPERARED "WINDSHIELD 1 HEATER FAIL". REMOVED AND REPLACED CAPTAINS SIDE WINDSHIELD IAW AMM 56-11-00. OPS TEST OK.
- [SDR YENA20120620531](https://openairdocs.org/sdr/YENA20120620531.md): Acm · failed · Jun 20, 2012 · N284JB · Emb ERJ190100IGW · Cabin Cooling System
  > FLT 1109 JFK-RDU, CREW DECLARED EMERGENCY DUE TO SMELL IN COCKPIT DURING DESCENT. F/A'S CALLED TO REPORT SMOKE IN CABIN OVER EMERGENCY EXIT ROWS. DONNED O2 MASKS AND RAN QRH. AFTER LANDED AND STOPPED ON RUNWAY NO INTERNAL OR EXTERNAL INDICATION OF SMOKE/FIR
- [SDR YENA20110514253](https://openairdocs.org/sdr/YENA20110514253.md): Sensor · failed · May 14, 2011 · N284JB · Emb ERJ190100IGW · Leading Edge Slat Position Indicating System
  > FLT 581 HPN-PBI, AIRCRAFT DIVERTED TO JFK DUE TO WING LEAK MSG AND TO AVOID ICING CONDITION. HOWEVER, DURING APPROACH THE CREW DECLARED EMERGENCY DUE TO SLAT FAIL. QRH COMPLIED WITH, ALSO GOT THE FOLLOWING EICAS MESSAGE, SHAKER ANTICIPATED, AOA LIMIT FAIL, SP
- [SDR YENA20100329044](https://openairdocs.org/sdr/YENA20100329044.md): Transceiver · failed · Mar 29, 2010 · N284JB · Emb ERJ190200IGW · Weather Radar System
  > FLT 572 PBI-HPN, EN ROUTE TO WHITE PLAINS WX RADAR BEGAN TO MALFUNCTION F/O WAS CHANGING SCALE AND CA RADAR SLAVED THEN WENT AWAY, F/O TILT ANGLE KEPT FLUCTUATING TO 3 THEN JUST SAWED ADJUST TO ANY ANGLE LOCKED UP. RADAR WOULD PAINT AT 12 MILE RING BUT ONLY S
- [SDR YENA20100112006](https://openairdocs.org/sdr/YENA20100112006.md): Sensor · malfunctioned · Jan 12, 2010 · N284JB · Emb ERJ190100IGW · Leading Edge Slat Position Indicating System
  > FLT JB907 JFK-ORD ON APPROACH TO ORD CREW DECLARED AN EMERGENCY FOR A "SLAT FAIL" CAS MESSAGE WHEN SELECTING FLAPS SLATS FROM ZERO TO 1. CREW ACCOMPLISHED QRH PROCEDURES AND LANDED UNEVENTFULLY. MX RETRIEVED CMC CODE 27811014ACE AND COMPLIED WITH AMM FIM 27-
- [SDR YENA20091220176](https://openairdocs.org/sdr/YENA20091220176.md): Pump · failed · Dec 20, 2009 · N284JB · Emb ERJ190100IGW · Hydraulic Pump (Electric/Engine), Main
  > FLT 1244 CLT-BOS DURING CRUISE AT FL350 PILOT DECLARED EMERGENCY DUE TO EICAS MESSAGE "HYD 2 EDP FAIL" LOSE OF NR 2 HYDRAULIC SYSTEM. RETURNED BACK TO CLT AND LANDED AIRCRAFT UNEVENTFULLY AND TAXIED TO THE GATE. MX REMOVED AND REPLACED ENGINE DRIVEN HYD PUMP
- [SDR YENA20090713073](https://openairdocs.org/sdr/YENA20090713073.md): Fadec · malfunctioned · Jul 13, 2009 · N284JB · Emb ERJ190100IGW · Fuel Control/Turbine Engines
  > THE ENG 1 TLA EICAS MSG APPEARED IN FLIGHT. FOLLOWED QRH AND DIVERTED TO NEAREST SUITABLE AIRPORT. THE NUMBER 1 ENGINE FAILED WHILE TAXIING IN TO THE GATE. MSG PRESENT FAIL ICON ON NR 1 N1 GAUGE. ENGINE 1 FAIL MSG ACCOMPANIED ENG 1 NO DISPATCH ENG SHORT DI
- [SDR YENA20090531058](https://openairdocs.org/sdr/YENA20090531058.md): Unknown · odor · May 31, 2009 · N284JB · Emb ERJ190100IGW · Air Distribution System
  > F/A SMELLED FUMES IN AREA OF SEAT ROW 23 & 24 CLOSE TO FLOOR SMELL OF BURNING RUBBER. PERFORMED FIM 21-20-00-810-801-A. FOUND NO FAULTS. AS PRECAUTION LTV WILL BE DEACTIVATED REF LP 533524 DUE TO ENTRY INTO CENTER E-BAY BUY BACK REQUIRED. NOTE: FLIGHT WAS
- [SDR YENA200812190129](https://openairdocs.org/sdr/YENA200812190129.md): Sensor · failed · Dec 16, 2008 · N284JB · Emb ERJ190100IGW · Leading Edge Slat Position Indicating System
  > FLT NR 1304, IAD-JFK, SLAT FAIL WHEN MOVING FLAP HANDLE TO 1. AFTER FOLLOWING QRH SLAT INDICATION OF ZERO AND AMBER FLAPS 2 (FLAP HANDLE 2) GREEN. OTHER MSGS, SHAKE ANTICIPATED, AOA LIMIT FAIL, SPOILER FAULT, SLAT FAIL. FOUND SLAT SENSOR AT FAULT OB, R&R PREV
- [SDR YENA200812110127](https://openairdocs.org/sdr/YENA200812110127.md): Sensor · failed · Dec 11, 2008 · N284JB · Emb ERJ190100IGW · Leading Edge Slat Position Indicating System
  > FLT NR 1219, BOS-BUF, SLAT FAIL IN FLIGHT WHEN FLAPS SELECTED TO POSITION ON APPROACH. R&R LT OTBD SKEW SENSOR IAW 27-83-01. OPS CHECK OK.

## 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 = 'N284JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N284JB/reports

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