# Service difficulty reports: N570JB

A list on [N570JB](https://openairdocs.org/aircraft/N570JB.md).

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

- [SDR YENA2024110501437](https://openairdocs.org/sdr/YENA2024110501437.md): Crossbeam · cracked · Nov 3, 2024 · N570JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE H1, LOCATED ON CROSSBEAM SPLIC ING AREA FR16 LH SIDE ON PASSENGER CABIN. CRACK DEPTH = 0.106 INCHES, CRACK DIRECTION: 11 OCLOCK LOOKING FWD; (RESOLVED ON W/O: 1321566 TASKCARD: NR-00013) REF AE
- [SDR YENA2024110501436](https://openairdocs.org/sdr/YENA2024110501436.md): Crossbeam · cracked · Nov 3, 2024 · N570JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE H2, LOCATED ON CROSSBEAM SPLIC ING AREA FR16 LH SIDE ON PASSENGER CABIN. CRACK DEPTH = 0.113 INCHES, CRACK DIRECTION: 12 OCLOCK LOOKING FWD; (RESOLVED ON W/O: 1321566 TASKCARD: NR-00014) REF AE
- [SDR YENA2024110501435](https://openairdocs.org/sdr/YENA2024110501435.md): Crossbeam · cracked · Nov 3, 2024 · N570JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: DISCREPANCY DESCRIPTION: CRACK INDICATION FOUND ON FASTENER HOLE H2, LOCATED ON CROSSBEAM SPLIC ING AREA FR16 RH SIDE ON PASSENGER CABIN. CRACK DEPTH = 0.091 INCHES, CRACK DIRECTION: 11 OCLOCK LOOKING FWD; (RESOLVED ON W/O: 1321566 TA
- [SDR YENA2024110501434](https://openairdocs.org/sdr/YENA2024110501434.md): Door Frame · cracked · Nov 3, 2024 · N570JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR68 RH AT LOWER INB FASTENER HOLE OF DOOR S TOP FITTING Ñ1 AREA. CRACK DIRECTION 5 OCLOCK VIEW LOOKING AFT. CRACK D= 0.170 INCH; (RESOLVED ON W/O: 1321566 TASKCARD: NR-00021) REF AEROMAN NR 2024-521414 WO 20
- [SDR YENA2024110501433](https://openairdocs.org/sdr/YENA2024110501433.md): Window Frame · cracked · Nov 3, 2024 · N570JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / CENTER POST LOWER NODE / AREA LH/RH CRACKS - PERMANENT REPAIR; REFERENCES: /1/ DOSSIER REFERENCE 81461224 /2/ AEM EA 53-9039-24 (COVER, P1 THROUGH P5) /3/ R53113672 ISSUE C /4/ R531134
- [SDR YENA2024110501432](https://openairdocs.org/sdr/YENA2024110501432.md): Skin · damaged · Nov 3, 2024 · N570JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR35 FWD FACE TO PRESSURE BULKHEAD ATTACHMENT / STR 30LH / FASTENER HOLES / CRACKS - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-9040-24 REV. 0 (COVER + PARTS 1-4) /2/ AIRBUS RDAF 81463325/004/2024 ISS
- [SDR YENA2023110301343](https://openairdocs.org/sdr/YENA2023110301343.md): Unknown · unknown · Oct 31, 2023 · N570JB · Airbus A320232 · Airfoil Anti/De-ice System
  > FLT#520, ATL-JFK. ' WING ANTI-ICE FAULT MESSAGE ON DESCENT AFTER SELECTING IT ON; ACCOMPLISHED WAI OPS CHECK PER AMM 30-11-00-710. OPS CHECK OK. MSG CLEARED. OK TO CONT IN SVC AT THIS TIME.'
- [SDR YENA2023102501318](https://openairdocs.org/sdr/YENA2023102501318.md): Unknown · unknown · Oct 23, 2023 · N570JB · Airbus A320232 · Air Distribution System
  > FLT#537, JFK-STI. '(AIRCRAFT PERFORMED AN AIR TURN BACK) 'FUMES REPORTED BY FLIGHT ATTEDENANTS IN THE FORWARD GALLEY; ACCOMPLISHED INFO NOTICE 2017-T015J. REF TSM 05-50-00-810-831-A & 71-00-00-810-801-A. PERFORMED LEVEL A DECONTAMINATION PER AMM 21-00-00-615-8
- [SDR YENA2023060800595](https://openairdocs.org/sdr/YENA2023060800595.md): Unknown · unknown · Jun 8, 2023 · N570JB · Airbus A320232 · Auto Flight System
  > DURING HEAVY MAINTENANCE: RUDDER TRIM SWITCH CONTROL REQUIRES REPLACEMENT PER JETBLUE REQUEST; C/W PER STS WO#W003031 NRN W003031119. NO DEFECTS NOTED.
- [SDR YENA2023060800594](https://openairdocs.org/sdr/YENA2023060800594.md): Unknown · unknown · Jun 8, 2023 · N570JB · Airbus A320232 · Cabin Pressure Controller
  > DURING HEAVY MAINTENANCE: PRESSURIZATION WILL NOT EXCEED 4.4 GOT EXCESSIVE CAB. ALT OUT OF FL210.; REPAIRS ACCOMPLISHED UNDER STS WO# 003031.REF. LOG PAGE # 3719161, ITEM 1(THIS AIRCRAFT, AIRFRAME, AIRCRAFT ENGINE, PROPELLER, OR APPLIANCE IDENTIFIED ABOVE WAS
- [SDR YENA2023060800593](https://openairdocs.org/sdr/YENA2023060800593.md): Unknown · unknown · Jun 8, 2023 · N570JB · Airbus A320232 · Compressor Bleed Control
  > DURING HEAVY MAINTENANCE: ENG 1 COMPRESSOR VANE; REPAIRS ACCOMPLISHED UNDER STS WO# 003031.REF. LOG PAGE # 3719161, ITEM 1 (THIS AIRCRAFT, AIRFRAME, AIRCRAFT ENGINE, PROPELLER, OR APPLIANCE IDENTIFIED ABOVE WAS REPAIRED AND INSPECTED IN ACCORDANCE WITH WO# W00
- [SDR YENA2023020300135](https://openairdocs.org/sdr/YENA2023020300135.md): Duct · failed · Jan 31, 2023 · N570JB · Airbus A320232 · Air Distribution System
  > FLT#1979, DCA-FLL. 'WHILE CHECKING NRU BOWL PER TASK CARD A320-21-26-43-710-001. FOUND CORROSION AROUND SKIN AIR INLET VALVE; CORROSION FOUND TO BE ON INLET DUCT FLANGE ONLY NOT ON AIRCRAFT SKIN. REMOVED AND REPLACED SKIN AIR DUCT ASSY IAW AMM 21-26-00.'
- [SDR YENA2022122301290](https://openairdocs.org/sdr/YENA2022122301290.md): Unknown · odor · Dec 26, 2022 · N570JB · Airbus A320232 · Air Distribution System
  > FLT#1405, MCO-SDQ. DURING DECENT DIRTY SOCK SMELL IN ENTIRE CABIN; PERFORMED INFO NOTICE 2017-T015 PER TSM 05-50-00-810-085B. AIRCRAFT OF FOR SERVICE.
- [SDR YENA2022091900925](https://openairdocs.org/sdr/YENA2022091900925.md): None · none · Sep 18, 2022 · N570JB · Airbus A320232 · Air Conditioning System
  > FLT#1586, MCO-BUF. 'LEVEL 2 FUME EVENT PERSISTENT ODOR (MELTED CRAYON) DURING CLIMBOUT AND DESCENT ODOR DETECTED BY BOTH PILOTS AND ALL FA'S; MX-270 MISSING, RAN #1 AND 2 PACK ON APU NO DEFECTS OR CRAYON SMELL RAN #1 AND 2 ENG AND #1 AND 2 PACKS NO DEFECTS OR
- [SDR YENA2022080500748](https://openairdocs.org/sdr/YENA2022080500748.md): None · none · Aug 2, 2022 · N570JB · Airbus A320232 · Air Conditioning System
  > FLT#1568, PUJ-JFK. 'ON TAXI OUT, INFLIGHT CALLED UP REPORTING A PUNGENT ODOR. AGREED TO TAKE OFF TO SEE IF IT WOULD DISSIPATE. NO SMELL COMING FROM A/C OUTLETS. CALLED UP AGAIN ON CLIMB & CRUISE. ODOR WAS ONLY NOTICED IN GALLEY AND THE FIRST 4 ROWS. RAN
- [SDR YENA2022012800027](https://openairdocs.org/sdr/YENA2022012800027.md): Stowage Box · failed · Jan 24, 2022 · N570JB · Airbus A320232 · Crew Oxygen System
  > FLT #603, EWR-SDQ (DIVERTED TO FLL). LEAK IN CREW OXY SYSTEM PSI DROPPED FROM 1150 TO 750 OVER 2.5 HRS; FOUND LEAK AT CAPTS OXYGEN STOWAGE BOX, REMOVED AND REPLACED (10RN1) MASK STOWAGE BOX IAW AMM 35-12-41, NO LEAKS NOTED
- [SDR YENA2021060300349](https://openairdocs.org/sdr/YENA2021060300349.md): Power Supply · failed · May 30, 2021 · N570JB · Airbus A320232 · Doors
  > FLT 40, MDE-FLL. L2 & LEFT OWE DOORS SHOWING OPEN ON DOOR PAGE WHEN CLOSED; FOUND RELAY 12WN NOT SUPPLY HOT BATT BUS WHEN NOT ENERGIZED DRAIN EPSU BATTERY 12WL. REMOVED AND REPLACED EPSU 11WL IAW AMM33-51-38 & REMOVED REPLACED RELAY 12WN IAW ESPM 20-46-50 OPS
- [SDR YENA2021043000297](https://openairdocs.org/sdr/YENA2021043000297.md): Unknown · odor · Apr 26, 2021 · N570JB · Airbus A320232 · Air Distribution System
  > FLT # 1225, JFK-TPA. FL EXPERIENCED A TINGLY FEELING IN HER MOUTH. ODOR POSSIBLY BURNING ELECTRIC,DETECTED BY CREW MOSTLY (STRONGEST) IN AFT CABIN; ACCOMPLISHED LEVEL 1 ODOR PER INFO NOTED 2017-T015F SECTION C. A/C IS OK FOR SERVICE. ACCOMPLISHED DECONTAMIN
- [SDR YENA2021042300263](https://openairdocs.org/sdr/YENA2021042300263.md): Cabin Air Sys · odor · Apr 20, 2021 · N570JB · Airbus A320232 · Air Distribution System
  > FLT 928, MCO-SJU. DIRTY SOCK SMELL AFT CABIN APPROX PASSING 10000 FT ON DESCENT; COMPLIED WITH INFO NOTICE 2017-T015F SEC. B APU PLACED ON MEL 36-12-02A, MX4 UPDATED, PLACARD INSTALLED. MCC NOTIFIED. AICRAFT OK FOR SERVICE. APU BLEED/LOAD CONTROL VALVE SECURE
- [SDR YENA2021041500231](https://openairdocs.org/sdr/YENA2021041500231.md): Apu · oil consumption · Apr 11, 2021 · N570JB · Airbus A320232 · APU Oil System
  > FLT 1448, LAS-JFK. VERY STRONG STENCH OF THE DIRTY SOCK SMELL. F/A & CUSTOMER COMPLAINED OF THE SMELL. THIS OCCURRED BETWEEN 6000 DOWN TO 2000 FT THEN THE SMELL DISSIPATED; DURING INITIAL INSP OF APU AREAS, FOUND LIGHT WETNESS AT DRAIN TUBE. RAN APU FOR 5 MIN
- [SDR YENA2021041200223](https://openairdocs.org/sdr/YENA2021041200223.md): Ecs · odor · Apr 8, 2021 · N570JB · Airbus A320232 · Air Distribution System
  > FLT 2836, STI-JFK. DIRTY SOCKS ODOR IN AFT CABIN, LEVEL 2 AND SLIGHTLY DETECTABLE IN FWD CABIN. NONE ON FLIGHT DECK. OCCURED DURING DESCENT THROUGH 8,000 FEET; PER INFO NOTICE 2017-T015F THIS IS A LEVEL 1 ODOR. COMPLIED WITH INFORMATION NOTICE 2017-T015F SE
- [SDR YENA2021021200099](https://openairdocs.org/sdr/YENA2021021200099.md): Unknown · odor · Feb 8, 2021 · N570JB · Airbus A320232 · Air Distribution System
  > FLT # 563, ORD-FLL. REPORTED AN ODOR EVENT ON DESCENT. “F/A REPORTED FUME ODOR ON FINAL FOR APPROX. 1 MINUTE”. THE CREW GENERATED A CABIN ODOR REPORT, AND DESCRIBED THE ODOR TYPE AS NAIL POLISH. A REVIEW OF TRAX SHOWS NO 30 DAY HISTORY; COMPLIED WITH INFORMA
- [SDR YENA2020113000547](https://openairdocs.org/sdr/YENA2020113000547.md): Indication Sys · malfunctioned · Nov 26, 2020 · N570JB · Airbus A320232 · Fuel Storage
  > FLT 1697, PHL-MCO. EMREGENCY DECLARED. INFLIGHT FUEL 1000 LBS TRANSFERRED FROM RIGHT INNER TO RIGHT OUTER TANK, LEFT SIDE DID NOT. FUEL TANK TEMP ON RIGHT SIDE HIGHER THAN LEFT SIDE FUEL TEMP. T/S DEBRIEFED CREW-DEPARTED PHL WITH 500 LBS IN THE OUTER TANKS
- [SDR YENA201906010303](https://openairdocs.org/sdr/YENA201906010303.md): Epsu · no test · Jun 1, 2019 · N570JB · Airbus A320232 · Emergency Lighting
  > FT 391, L1 DOOR SLIDE FAILED EMERGENCY LIGHT TEST; R AND R L1 DOOR SLIDE ASSY IAW AMM 25-62-44. OPS CHK GOOD.
- [SDR YENA2019060610302](https://openairdocs.org/sdr/YENA2019060610302.md): Light · no test · Jun 1, 2019 · N570JB · Airbus A320232 · Emergency Equipment
  > FT # 391, L1 DOOR SLIDE FAILED EMERGENCY LIGHT TEST; R AND R L1 DOOR SLIDE ASSY IAW AMM 25-62-44. OPS CHK GOOD.
- [SDR YENA2018101070624](https://openairdocs.org/sdr/YENA2018101070624.md): Web · corroded · Aug 17, 2018 · N570JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CARGO DR ENTRY WEB BOX HAS. A FEW AREAS OF CORR NEAR THRESHOLD; REF NR 440498-24446: REM & RPL AFT CARGO DR ENTRY TORQUE BOX WEB IAW SRM 51-72-11.
- [SDR YENA2018101070623](https://openairdocs.org/sdr/YENA2018101070623.md): Floorbeam · corroded · Aug 17, 2018 · N570JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RT FLOORBEAM -Y1292 UPPER SURFACE AT FR 66; REPLACED FLOORBEAM. WORK ACCOMPLISHED ON NR 24381.
- [SDR YENA2018101070622](https://openairdocs.org/sdr/YENA2018101070622.md): Floorbeam · corroded · Aug 17, 2018 · N570JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RT FLOORBEAM AY -Y1292, FRAME 68 +10.00", STR 23R. HAS CORROSION THAT IS OUT OF LIMITS AFTER BLEND-OUT WAS PERFORMED; BLENDED CORROSION IAW SRM 51-74-00, FROM RT FLOORBEAM -Y1292, FR 68 +10.00". DAMAGE IS
- [SDR YENA2018101070621](https://openairdocs.org/sdr/YENA2018101070621.md): Support Angle · corroded · Aug 17, 2018 · N570JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LT AFT SHEAR WEB SUPPORT ANGLE, AT FR 69, + 18.00", STR 23L. HAS CORROSION THAT IS BEYOND ALLOWABLE LIMITS PER SRM 51-73-11, ON THE UPPER AND LOWER SURFACES; REMOVED AND REPLACED THE LT SHEAR WEB SUPPORT AN
- [SDR YENA2018101070620](https://openairdocs.org/sdr/YENA2018101070620.md): Floorbeam · corroded · Aug 17, 2018 · N570JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LT FLOORBEAM AT Y1292, FRAME 67 +12.00". HAS CORROSION THAT IS BEYOND LIMITS AFTER BLEND-OUT (REF. 53-00-14-283-002, FIG 001, SHT 1); REMOVED AND REPLACED LT FLOORBEAM (P/N: D5347217220400) AT Y1292, FRAME
- [SDR YENA2018101070619](https://openairdocs.org/sdr/YENA2018101070619.md): Floorbeam · corroded · Aug 17, 2018 · N570JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LT FLOORBEAM Y1292 AT FR 67 +15; REMOVED AND REPLACED LT FLOORBEAM Y1292 FR 68-69 STR 23L IAW SRM 51-42-11 & 51-72-11; REF NR 24397.
- [SDR YENA2018101070618](https://openairdocs.org/sdr/YENA2018101070618.md): Support Angle · corroded · Aug 17, 2018 · N570JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LT SUPPORT ANGLE AT FR 20 BEAM Y1732; REMOVED AND REPLACED LT SUPPORT ANGLE AT FR 20 BEAM Y1732 IAW SRM 52-42-11 7 51-72-11. WORK ACCOMPLISHED ON NR 24423.
- [SDR YENA2018101070617](https://openairdocs.org/sdr/YENA2018101070617.md): Door Sill · corroded · Aug 17, 2018 · N570JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON L2 DOOR SILL FR 66 STR 23L; REPLACED DOOR SILL. REF NR 24430.
- [SDR YENA2018101070616](https://openairdocs.org/sdr/YENA2018101070616.md): Support Angle · corroded · Aug 17, 2018 · N570JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RT AFT SHEAR WEB SUPPORT ANGLE, AT FR 69 +19.00", STR 23R. HAS UPPER AND LOWER SURFACE CORROSION; AFTER BLEND-OUT, DAMAGE WAS FOUND TO BE OUT OF LIMITS PER SRM 51-74-00. SUPPORT FRAME REMOVED AND REPLACED P
- [SDR YENA2018101070615](https://openairdocs.org/sdr/YENA2018101070615.md): Floorbeam · corroded · Aug 17, 2018 · N570JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LT CABIN FLOORBEAM Y1292 AT FR 66 +3.00"; BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-0014-283-002, FIG 001. REF. NR 24396. NOTE: FLOORBEAM AT Y1292, FR66 WAS REPLACED ON NR 24395.
- [SDR YENA2018101070614](https://openairdocs.org/sdr/YENA2018101070614.md): Door Sill · corroded · Aug 17, 2018 · N570JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON L2 DOOR SILL DRAIN. CORRODED AROUND FASTENER'S AT FR 67 +14.00"; REMOVED AND REPLACED L2 DOOR SILL IAW SRM 51-72-11-911-001. REF LCQ NR 24393.
- [SDR YENA2018101070613](https://openairdocs.org/sdr/YENA2018101070613.md): Seat Track · corroded · Aug 17, 2018 · N570JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RT SEAT TRACK AT FR 20 BEAM Y-1292; REMOVED AND REPLACED THE R2 DOOR SILL BEAM IAW SRM 51-72-11-911-001. REF LCQ NR 24377.
- [SDR YENA2018082017318](https://openairdocs.org/sdr/YENA2018082017318.md): Cable · no test · Aug 17, 2018 · N570JB · Airbus A320232 · Emergency Equipment
  > DURING HEAVY MAINTENANCE, THE LT OVERWING HATCH RESERVOIR CABLE FAILED AN OPS CHECK. REMOVED AND REPLACED THE FLEXIBLE CABLE IAW AMM 25-62-43-000-001-A, AND 25-62-43-400-001-A.
- [SDR YENA2018082017317](https://openairdocs.org/sdr/YENA2018082017317.md): Release Cable · failed · Aug 17, 2018 · N570JB · Airbus A320232 · Escape Slide
  > DURING HEAVY MAINTENANCE, THE RT OVERWING H RESERVOIR CABLE FAILED AN OPS CHECK; REMOVED AND REPLACED RT ESCAPE SLIDE RELEASE CABLE IAW AMM 25-62-43-020-053-A, AND 25-62-43-420-050-A.
- [SDR YENA201710190850](https://openairdocs.org/sdr/YENA201710190850.md): Battery Pack · failed · Oct 19, 2017 · N570JB · Airbus A320232 · Emergency Lighting
  > RT EPSU BATTERY 12WL FAILED AN EMERGENCY LIGHT TEST. R & R THE BATTERY PACK IAW AMM 33-51-38, OPS CHECKED GOOD.
- [SDR YENA20150420078](https://openairdocs.org/sdr/YENA20150420078.md): Structure · contaminated · Apr 20, 2015 · N570JB · Airbus A320232 · Rudder Structure
  > DURING HEAVY MAINTENANCE, DURING THE ACCOMPLISHMENT OF THE RUDDER SIDESHELL INSPECTION WATER INGRESSION FOUND AT HOIST POINT NR 3 IAW A320-55-1041-3. DURING PULSE INFARED INSPECTION, FOUND 1 AREA ON THE RT SIDE OF THE RUDDER SIDESHELL THAT IS OUT OF LIMITS IA
- [SDR YENA20130820181](https://openairdocs.org/sdr/YENA20130820181.md): Sill · corroded · Aug 20, 2013 · N570JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > ON HEAVY MX CHECK, FOUND CORROSION ON LOWER SILL AFT PAX CABIN FRAME 68, STRINGER 23L AND FRAME 66, STRINGER 23L. ACCOMPLISHED REPAIR IAW WITH EC A13-534-01.
- [SDR YENA20130819180](https://openairdocs.org/sdr/YENA20130819180.md): Sill · corroded · Aug 19, 2013 · N570JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY CHECK, FOUND CORROSION ON LOWER SILL AT FRAME 66 STRINGER 23R AFT PAX CABIN. ACCOMPLISHED REPAIR TO THE R2 DOOR LOWER SILL BEAM IAW EO AEM-HC53-324/23 AND EC A13-533-01.
- [SDR YENA20130713147](https://openairdocs.org/sdr/YENA20130713147.md): Battery · failed · Jul 13, 2013 · N570JB · Airbus A320232 · Emergency Lighting
  > DURING MX, DISCOVERED THE EPSU AT FIN NR 10 BATTERY FAILED CAPACITY TEST. R & R BATTERY AT EPSU FIN NR 10 IAW AMM 33-51-38. OPS CHECKED NORMAL.
- [SDR YENA20100512071](https://openairdocs.org/sdr/YENA20100512071.md): Lamp · failed · May 12, 2010 · N570JB · Airbus A320232 · Emergency Lighting
  > ON GROUND, DURING MAINT CHECK LT EXT EMERGENCY LIGHT AFT INOP. RELAMPED LT WING EXT EMERGENCY LIGHT OPS CK GOOD.
- [SDR YENA200811240117](https://openairdocs.org/sdr/YENA200811240117.md): Power Supply · failed · Nov 23, 2008 · N570JB · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILED FWD EPSU. REMOVED AND REPLACED EPSU, OPS CHECK NORMAL IAW AMM 33-51-38-04.
- [SDR YENA2008042](https://openairdocs.org/sdr/YENA2008042.md): Unknown · odor · May 3, 2008 · N570JB · Airbus A320232 · Air Distribution System
  > FLT 316, SAN-IAD, ON TAXI OUT, RETURNED TO GATE, BURNING SMELL COMING FROM REAR OF LAVATORY OF AIRCRAFT. T/S RT & LT AFT LAVS. NO C/B POPPED. WATER HEATERS OK. FLUSH TIMERS OK. NO SMOKE SMELL FROM LAVS. BACK GALLEY C/B PANELS. NO POPPED C/B. FLIGHT CRE
- [SDR YENA2008017](https://openairdocs.org/sdr/YENA2008017.md): Unknown · odor · Feb 11, 2008 · N570JB · Airbus A320232 · Air Distribution System
  > FLT 383, LGA-FLL, APPROXIMATELY 3 MINUTES PRIOR TO LANDING NR 1 F/A CALLED TO REPORT "BURNING SMELL" IN CABIN. NR 1 F/A TURNED OFF TV'S AND DID NOT SMELL IT AGAIN. BOTH PILOTS COULD SMELL THE SAME THING IN THE COCKPIT. ACCOMPLISHED AND PERFORMED CHECK AS PE
- [SDR YENA2007061](https://openairdocs.org/sdr/YENA2007061.md): Bottle · cracked · Jun 10, 2007 · N570JB · Airbus A320232 · Passenger/Crew Doors
  > L-1 ENTRY DOOR ASSIST BOTTLE LEAKING (CRACKED). REPLACED L-1 ENTRY DOOR ASSIST BOTTLE PER AMM 52-11-14, LEAK 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 = 'N570JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N570JB/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.