# Service difficulty reports: N569JB

A list on [N569JB](https://openairdocs.org/aircraft/N569JB.md).

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

- [SDR YENA2026082400703](https://openairdocs.org/sdr/YENA2026082400703.md): Check Valve · failed · Aug 21, 2026 · N569JB · Airbus A320232 · Hydraulic System, Main
  > FLT 2895, BOS-PUJ(AIRTURN BACK TO BOS). Y HYD RSVR OVERHEAT; FOLLOWED TSM 29-13-00-810-802-A & TSM 29-13-00-810-804-A. R&R'D CHECK VALVE FIN 3083GM IAW AMM 29-24-21. OPS CHECK GOOD. LEAK CHECK GOOD.
- [SDR YENA2025012900122](https://openairdocs.org/sdr/YENA2025012900122.md): Slide · abnormal · Jan 28, 2025 · N569JB · Airbus A320232 · Escape Slide
  > FLT#2694, NAS-FLL. 'WHILE WORKING MDDR # 571952 R1 ARM/DISARM INDICATION. NOTICED MINUMUM SLIDE ESCAPE UNRAVEL. SAFETY PIN WAS INSTALLED ON REGULATOR AND SLIDE WAS NOT DEPLOY. REMOVED R1 DOOR SLIDE ESCAPE SLIDE IN REF TO AMM 25-62-44; INSTALLED R1 ESCAPE SLIDE
- [SDR YENA2025012200098](https://openairdocs.org/sdr/YENA2025012200098.md): Indication Sys · failed · Jan 19, 2025 · N569JB · Airbus A320232 · Auto Flight System
  > FLT#62, PBI-LGA. (AIRCRAFT PERFORMED AN AIR TURN BACK TO PBI) ' AT FL 280 MAP NOT AVAILABLE AUTO THR OFF, NO FLIGHT DIRECT A/P OFF. RAN CK LIST ADV MX. RETURNED TO PBI; ACCOMPLISHED TSM 22-11-00-810 REMOVED AND REPLACED FMGC 1 SYS OPS CHECK NORM AMM 22-83-34.
- [SDR YENA2024071100962](https://openairdocs.org/sdr/YENA2024071100962.md): Stringer · corroded · Jul 3, 2024 · N569JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 43L BTW FRAME 57 AND FRAME 58 IN AFT CARGO COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1308674 TASKCARD: NR-00019) PERFORMED PERMANENT REPAIR ON STRINGER 43L BTW FRAME 57 AND FRAME 58 IN AFT CARGO COMPARTMENT IAW
- [SDR YENA2024071100961](https://openairdocs.org/sdr/YENA2024071100961.md): Support · corroded · Jul 3, 2024 · N569JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CORROSION LOWER SILL AT LEVEL OF FRAME 60 IN BULK CARGO COMPARTMENT ( CPCP FINDING); (RESOLVED ON W/O: 1308674 TASKCARD: NR-00020) PERFORMED PERMANENT REPAIR ON LOWER SILL AT LEVEL OF FRAME 60 IN BULK CARGO COMPARTMENT IAW A320 SRM 5
- [SDR YENA2024071100960](https://openairdocs.org/sdr/YENA2024071100960.md): Stop Fitting · cracked · Jul 3, 2024 · N569JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND DOOR STOP 7 FR20LH HOLE H1. CRACK DEPTH 0.063 I NCH AND DIRECTION 12 OCLOCK; (RESOLVED ON W/O: 1308674 TASKCARD: NR-00023) PERFORMED PERMANENT REPAIR ON DOOR STOP 7 FR20 LH ON HOLE H1 IAW A320 SRM 53-11-12-300-0
- [SDR YENA2024071100959](https://openairdocs.org/sdr/YENA2024071100959.md): Frame · cracked · Jul 3, 2024 · N569JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME LOC DOOR STOP 7 FR16RH HOLE H1. CRACK DEPTH 0.063 INCH AND DIRECTION 9 O'CLOCK; (RESOLVED ON W/O: 1308674 TASKCARD: NR-00025) REMOVED AND REPLACED INTERCOSTAL FITTING LOC. AT LEVEL OF DOOR STOP 7 FR16 R
- [SDR YENA2024071100958](https://openairdocs.org/sdr/YENA2024071100958.md): Intercostal · cracked · Jul 3, 2024 · N569JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON INTERCOSTAL LAYER LOC DOOR STOP 7 FR16RH HOL E H3. CRACK DEPTH 0.063 INCH AND DIRECTION 12 OCLOCK; (RESOLVED ON W/O: 1308674 TASKCARD: NR-00024) REMOVED AND REPLACED INTERCOSTAL FITTING LOC. AT LEVEL OF DOOR
- [SDR YENA2024071100957](https://openairdocs.org/sdr/YENA2024071100957.md): Skin · corroded · Jul 3, 2024 · N569JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION INTERNAL SKIN BTW FR 12 TO FR 14 LOWER AREA ON LH AVIONIC COMPARTMENT(CPCP FINDING); (RESOLVED ON W/O: 1308674 TASKCARD: NR-00047) REF AEROMAN N/R 2024-29895, PERFORMED REPAIR TO CORROSION AT THE FWD FUSELAGE LOWER SKIN AT N
- [SDR YENA2024071100956](https://openairdocs.org/sdr/YENA2024071100956.md): Fuel Tank · corroded · Jul 3, 2024 · N569JB · Airbus A320232 · Fuel Storage
  > DURING HEAVY MAINTENANCE: CORROSION ON UPPER SKIN BTW FR41/FR42 LH SIDE CENTER TANK AREA IN PASS ENGER CABIN; (RESOLVED ON W/O: 1308674 TASKCARD: NR-00050) REF AEROMAN N/R 2024-298788, REMOVED CORROSION MECHANICALLY LOCATED ON UPPER SKIN BTW FR41/FR42 LH SIDE
- [SDR YENA2024071100955](https://openairdocs.org/sdr/YENA2024071100955.md): Shear Web · cracked · Jul 3, 2024 · N569JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CRACKED SHEAR WEB LOCATED AT FR 71 BTW STR 27R AND 32R IN THE THS COMPARTMENT; REF AEROMAN WO# 2024-177/1 NR# 2024-298723 FOR ALL WORK ACCOMPLISHED REMOVED DAMAGED SHEAR WEB FABRICATED AND INSTALLED NEW WEB IAW A320 SRM 51-41-2, SRM 5
- [SDR YENA2024071100954](https://openairdocs.org/sdr/YENA2024071100954.md): Fitting · corroded · Jul 3, 2024 · N569JB · Airbus A320232 · Fuselage Main, Attach Fittings
  > DURING HEAVY MAINTENANCE: CORROSION ON FITTING BTW FR13- FR14 INTERNAL STRUCTURE LOWER AREA ON LH AVIONICS COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1308674 TASKCARD: NR-00051) REF AEROMAN NR 2024-298984 WO# 2024-177/1 REMOVED AND REPLACED FITTING AND FAST
- [SDR YENA2024071100953](https://openairdocs.org/sdr/YENA2024071100953.md): Skin · corroded · Jul 3, 2024 · N569JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: FUSELAGE/ FWD LOWER SKIN AT NLG/ FR12-13 LH LOWER STGR AT Y520/ CORROSION- TEMPORARY REPAIR (A24-745-01) (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2023041900412](https://openairdocs.org/sdr/YENA2023041900412.md): Unknown · unknown · Apr 18, 2023 · N569JB · Airbus A320232 · Air Conditioning System
  > FLT#87, ALB-FLL. 'DURING DESCENT ( 8000 MSL) COCKPIT ODOR ( FUME EVENT) WAS NOTED UNTIL LANDING. X BLEED & PACK 1 OFF UNTIL PARKING; PERFORMED INSPECTION OF APU COMP NO LEAK ( OIL / FUEL) FOUND AT THIS MOMENT. PERFORMED INFO NOTE 2017-T015J. ACCOMPLISHED
- [SDR YENA2022112101142](https://openairdocs.org/sdr/YENA2022112101142.md): Vent · corroded · Nov 10, 2022 · N569JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FOUND CORROSION ON LAV VENT EXTRACT; REF FLIGHT STARV W/O FS220088. N/R 00004, PERFORMED DOUBLER REPAIR IAW A320 SRM 53-41-00, SEE FS 220088 N/R 00004 FOR WORK ACCOMPLISHED. MAJOR REPAIR.
- [SDR YENA2022062900636](https://openairdocs.org/sdr/YENA2022062900636.md): None · none · Jun 28, 2022 · N569JB · Airbus A320232 · Fuselage Structure (General)
  > FLT#837, JFK-STI. (AIRCRAFT DECLARED AN EMERGENCY AND PERFORMED AN AIR TURN BACK TO JFK) ' DURING TAKEOFF ROLL AT ROTATION SPEED, AIRCRAFT JERKED HARD LEFT. AFTER LIFT-OFF A SIGNIFICANT VIBRATION WAS FELT. SUSPECTED BLOWN TIRE. DECIDED NOT TO RETRACT LANDING G
- [SDR YENA2020021940183](https://openairdocs.org/sdr/YENA2020021940183.md): Slide · no test · Feb 14, 2020 · N569JB · Airbus A320232 · Escape Slide
  > DURING HEAVY MAINTENANCE, REF AEROM 2020- 42075 WO 12/1 PERFORMED CREW DOOE CONTROLLED DEPLOYMENT 832 IAW AMM 25-62-00-710-001-A & REPLACED SLIDE 832 IAW AMM 25-62-44-400-007-A; SUPPLEMENTAL INFORMATION TO FOLLOW
- [SDR YENA2020021940182](https://openairdocs.org/sdr/YENA2020021940182.md): Skin · dented · Feb 14, 2020 · N569JB · Airbus A320232 · Leading Edge Devices
  > DURING HEAVY MAINTENANCE, ENT SLAT 1 LOWER SKIN RH WING; REF AEROMAN NR 2020-42151 WO 2020 12/1 PERFORMED REPAIR ON SLAT #1 LOWER SKIN RH WING IAW EA # 57-0116-20 PART 1.
- [SDR YENA202002184182](https://openairdocs.org/sdr/YENA202002184182.md): Slide · failed · Feb 14, 2020 · N569JB · Airbus A320232 · Escape Slide
  > DURING HEAVY MAINTENANCE, REF AEROM 2020- 42075 WO 12/1 PERFORMED CREW DOOE CONTROLLED DEPLOYMENT 832 IAW AMM 25-62-00-710-001-A & REPLACED SLIDE 832 IAW AMM 25-62-44-400-007-A; SUPPLEMENTAL INFORMATION TO FOLLOW
- [SDR YENA2020021840181](https://openairdocs.org/sdr/YENA2020021840181.md): Skin · dented · Feb 14, 2020 · N569JB · Airbus A320232 · Leading Edge Devices
  > DURING HEAVY MAINTENANCE, REF AEROMAN W/O 2020-12/1 WCC 2020-42059, WEIGHT VARIANT UPGRADE FOR ACFT N569JB - SRM REPAIR SURVEY - LEFT WING - SLAT #2 DENT DAMAGE - LEADING EDGE; REF AEROMAN W/O 2020-12/1 WCC 2020-42059, PERFOEMED PERMANENT REPAIR ON LEFT WING S
- [SDR YENA2020021840180](https://openairdocs.org/sdr/YENA2020021840180.md): Skin · corroded · Feb 14, 2020 · N569JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, REF AEROMAN W/O 2020-12/1 WCC 2020-42262, CORROSION ON TOP SKIN, LOWER SURFACE, TRAILING EDGE, REAR SPAR, RIB 16 PLUS 20 INCHES ON LH WINGL; REF AEROMAN W/O 2020-12/1, WCC 2020-42262, EVALUATED EXISTING REWORK LOCATED RIB 16 + 20, TOP
- [SDR YENA2020021840179](https://openairdocs.org/sdr/YENA2020021840179.md): Structure · broken · Feb 14, 2020 · N569JB · Airbus A320232 · Rudder Structure
  > DURING HEAVY MAINTENANCE, PER AEROMAN WORK ORDER 2020-12/1, WCC# 2020-42019, FOUND BROKEN RUDDER TIP (326AT) ON VERTICAL STABILIZER; PER AEROMAN WORK ORDER 2020-12/1, WCC# 2020-42019, PERFORMED PERMANENT REPAIR ON RUDDER TIP (326AT) ON VERTICAL STABILIZER IAW
- [SDR YENA201901100020](https://openairdocs.org/sdr/YENA201901100020.md): Battery Pack · failed · Jan 10, 2019 · N569JB · Airbus A320232 · Emergency Lighting
  > FLT 2066, RSW-BOS. FDW BATTERY PACK FAIL ( ESPU); R & R FWD (EPSU) EMERGENCY BAT LIGHT IAW AMM 35-51-00. OPS CHECK GOOD.
- [SDR YENA2018062210263](https://openairdocs.org/sdr/YENA2018062210263.md): Lens · missing · Jun 21, 2018 · N569JB · Airbus A320232 · Emergency Lighting
  > RIGHT OVERWING EXIT, TWO EMERGENCY EXIT SIGN COVERS WERE MISSING. REPLACED THE COVERS IAW AMM 33-51-15. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR YENA201805190919](https://openairdocs.org/sdr/YENA201805190919.md): Not Reported · cracked · May 19, 2018 · N569JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CRACKS WERE FOUND. REFER EC A18-414-01. FUSELAGE/ CENTER FUSELAGE/ ALI 521110-01/ FR16LT & FR20LT FASTENER HOLES/ MULTIPLE CRACKS- PERMANENT REPAIR; APPROVED THIS REPAIR PER REF /3/ RDAS AND IS CLASSIFIED AS MAJOR CATEGORY 'B'.
- [SDR YENA201805190477](https://openairdocs.org/sdr/YENA201805190477.md): Door Sill · corroded · May 19, 2018 · N569JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LT DADO PANEL SUPPORT FLOOR BEAM AT FR 66 3" FWD OF GIRT BAR FITTING HAS BIG AREA OF CORROSION. REMOVED CORROSION ON L2 DOOR SILL, FOUND TO BE OUT OF LIMITS IAW 53-00-14-283-002 FIG 101 PG 4, REQUIRED NEW L
- [SDR YENA201805190476](https://openairdocs.org/sdr/YENA201805190476.md): Door Sill · corroded · May 19, 2018 · N569JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RT AFT CABIN R2 DOOR I/B SILL 1 INCH AFT OF FRAME 66. REMOVED AND REPLACED R2 DOOR SILL PN D5348004320701 PO 1041397.7 IAW SRM 51-72-11-911-001.
- [SDR YENA201805190475](https://openairdocs.org/sdr/YENA201805190475.md): Door Sill · corroded · May 19, 2018 · N569JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RT AFT CABIN R2 DOOR I/B SILL 1 INCH AFT OF FRAME 66. REMOVED AND REPLACED R2 DOOR SILL PN D5348004320701 PO 1041397.7 IAW SRM 51-72-11-911-001.
- [SDR YENA201805190474](https://openairdocs.org/sdr/YENA201805190474.md): Floorbeam · corroded · May 19, 2018 · N569JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON MAIN CABIN AT FR68 FLOORBEAM Y-1292 (RT) ON UPPER SURFACE. REMOVED AND REPLACED MAIN CABIN AT FR68 FLOORBEAM Y-1292 (RT) PN D5347218920400 PO 1036857.5 IAW SRM 51-72-11 AND 51-42-11 PER 2.F AND 2.D.
- [SDR YENA201805190473](https://openairdocs.org/sdr/YENA201805190473.md): Floorbeam · corroded · May 19, 2018 · N569JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y465 5 INCHES AFT OF FRAME 66. REMOVED AND REPLACED FLOORBEAM Y464 F66 IAW SRM 51-72-11.
- [SDR YENA201805190472](https://openairdocs.org/sdr/YENA201805190472.md): Floorbeam · corroded · May 19, 2018 · N569JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RT AFT CABIN FLOORBEAM Y464 1 INCH FWD OF FRAME 66. REMOVED CORROSION ORIG MAT.140" REMAINING MAT.088" MAT LOSS.052" L 2.5" W 1.3". FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOORBEAM Y464 AT AFT C
- [SDR YENA201805190471](https://openairdocs.org/sdr/YENA201805190471.md): Floor Support · corroded · May 19, 2018 · N569JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RT FLOOR SUPPORT 1 INCH OF FRAME 20 IN FRONT OF R2 DOOR CUTOUT. REMOVED AND REPLACED WEB AND ANGLE PN D5311278520301 AND D5311278620101 IAW SRM 51-72-11 AND GMM 5-169.
- [SDR YENA201805190470](https://openairdocs.org/sdr/YENA201805190470.md): Shear Web · corroded · May 19, 2018 · N569JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RT AFT CABIN CORNER SHEAR WEB. REMOVED AND REPLACED RT AFT CABIN CORNER SHEAR WEB IAW SRM 51-72-11-911-001.
- [SDR YENA201805190469](https://openairdocs.org/sdr/YENA201805190469.md): Floorbeam · corroded · May 19, 2018 · N569JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LT AFT CABIN FLOORBEAM Y1292 FR66 +1" STR23L. REMOVED AND REPLACED FLOORBEAM Y1292 AT FR66 +1" STR23L IAW SRM 51-72-11.
- [SDR YENA201802260110](https://openairdocs.org/sdr/YENA201802260110.md): Bulb · broken · Feb 26, 2018 · N569JB · Airbus A320232 · Lighting System
  > DURING APPROACH, A STRONG ODOR IN THE COCKPIT AND CABIN, OF ELECTRICAL ODOR, LIKE A BALLAST IN A FLUORESCENT LIGHT BURNING OUT. TURNED OFF THE COMMERCIAL BUTTON ON OVHD ELEC PANEL AND THE AFT AVIONICS COMP. SWITCH. THE ODOR SUBSIDED BUT CHANGED TO THE ODOR
- [SDR YENA201705300440](https://openairdocs.org/sdr/YENA201705300440.md): Wire · damaged · May 30, 2017 · N569JB · Airbus A320232 · Light System Wiring
  > EMERGENCY LIGHTING FORWARD PARTION RED LIGHT INOPERATIVE. FOUND A DAMAGE WIRE AT FIN 361WL1. REPAIR THE WIRE IAW ESPM 20-53-51. OPS CHECKED GOOD.
- [SDR YENA20141230286](https://openairdocs.org/sdr/YENA20141230286.md): Warning Light · faulted · Dec 30, 2014 · N569JB · Airbus A320232 · Landing Gear Retraction/Extension System
  > AIRCRAFT DIVERTED DUE TO LGCIU 1 FAULT. LANDING GEAR GEAR AURAL, INDICATED ALL THREE UNLOCKED. PERFORMED INDICATION CHECK AND GEAR WAS UP AND LOCKED. WHEELS -SD- SHOWED AMBER XX ALL GEARS. R & R LGCIU (5GA1) IAW AMM 32-31-71 AS A PRECAUTION. LANDING GEAR
- [SDR YENA20141118250](https://openairdocs.org/sdr/YENA20141118250.md): Battery Pack · no test · Nov 18, 2014 · N569JB · Airbus A320232 · Emergency Lighting
  > DURING MAINTENANCE CHECK OF CABIN EMERGENCY LIGHTS, FOUND AFT BATTERY PACK SHOWING EXTERIOR LIGHT FAULT AND BATTERY FAULT. R & R BATTERY PACK IAW AMM CH 33-51-38. OPS CHECKED GOOD.
- [SDR YENA20111208393](https://openairdocs.org/sdr/YENA20111208393.md): Oxygen Mask · not seated · Dec 8, 2011 · N569JB · Airbus A320232 · Crew Oxygen System
  > FLT 824 SDQ-JFK, AIRCRAFT DIVERTED TO SJU DUE TO OXYGEN APPEARS TO BE LEAKING, DEPARTED WITH 550 PSI AFTER 30 MIN OF FLIGHT O2 WAS 360 PSI AND DECREASING. RESET ALL MASK BEFORE DEPARTURE. SERVICED CREW O2 BOTTLE IAW AMM 12-14-35 AND PERFORMED FIM TASK 35-10-
- [SDR YENA20101120155](https://openairdocs.org/sdr/YENA20101120155.md): Battery Pack · failed · Nov 20, 2010 · N569JB · Airbus A320232 · Emergency Lighting
  > FLT 6403 JFK-SAL, ON MAINTENANCE CHECK FOUND EPSU UNIT FAULT IN FWD AREA GALLEY. REPLACED BATTERY PACK IN FWD AREA GALLEY. TEST OK IAW AMM 33-51-38.
- [SDR YENA20100410055](https://openairdocs.org/sdr/YENA20100410055.md): Smoke Detector · failed · Apr 10, 2010 · N569JB · Airbus A320232 · Smoke Detection
  > FLT 762 CUN-JFK DIVERTED TO MCO, SMOKE LAV / CRG DET FAULT. REMOVED AND REPLACED FWD LAV SMOKE DET UNIT IAW MM 26-17-15. OPS CHECK ALL NORMAL.
- [SDR YENA2008081](https://openairdocs.org/sdr/YENA2008081.md): Bleed Valve · failed · Aug 21, 2008 · N569JB · Airbus A320232 · Compressor Bleed Valve
  > FLT 785, MCO-BON, DIVERTED TO FLL, ENG NR 2 BLEED FAULT. ACCOMPLISHED ECAM QRH, NO PRESSURIZATION IN CABIN. LOST BOTH (1&2) EMERGENCY DESCENT REQUIRED. REMOVED AND REPLACED NR 2 ENG PRESSURE REGULATING VALVE 4001HA PER AMM 36-11-52. OPS CHECK OK.
- [SDR YENA2008073](https://openairdocs.org/sdr/YENA2008073.md): Compressor · stalled · Aug 1, 2008 · N569JB · Airbus A320232 · Turbine Engine Compressor Section
  > FLT 1262, LGB-SMF, AIR RETURN TO LGB, ENG NR 1 COMPRESSOR STALL (ECAM) THRUST LEVERS AT CL DETENT LEVEL AT FL230 "BANG" AND YAW AND VIBRATION SAW ZERO EPR, THEN WENT BACK TO NORMAL. DID NOT SHUT DOWN IAW QRH 6-26. PERFORMED TSM 71-00-00-710-013-A, GVI, BLEED
- [SDR YENA200332](https://openairdocs.org/sdr/YENA200332.md): Bottle · discharged · Oct 29, 2003 · N569JB · Airbus A320232 · Escape Slide
  > L2 SLIDE RAFT BOTTLE PRESSURE LOW FOUND DURING WEEKLY CHECK. REMOVED AND REPLACED L2 SLIDE RAFT IAW 25-62-44.

## 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 = 'N569JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N569JB/reports

---
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