# Service difficulty reports: N562JB

A list on [N562JB](https://openairdocs.org/aircraft/N562JB.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 · 65 reports

- [SDR YENA2026022500238](https://openairdocs.org/sdr/YENA2026022500238.md): Apu · contaminated · Feb 25, 2026 · N562JB · Airbus A320232 · Airborne Auxiliary Power Unit (APU) System
  > FLT #1367 HPN-PBI. "AFT INFLIGHT SMELLED DIRTY SOCK SMELL AS SOON AS WE TOUCHED DOWN AND TAXIED TO THE GATE. THIS WAS AFTER APU STARTED CLEARING THE RUNWAY.;INSPECTED APU AREA FOUND SATURATED WITH TYPE 1 DE-ICE FLUID TO INCLUDE INTAKE & PLENUM. C/W INFO NOTICE
- [SDR YENA2025009000905](https://openairdocs.org/sdr/YENA2025009000905.md): Slide · unwanted deploy · Aug 30, 2025 · N562JB · Airbus A320232 · Escape Slide
  > FLT#1567, HPN-PBI. "ACCIDENTAL DEPLOYMENT OF R1 DOOR SLIDE; REMOVED AND REPLACED R1 DOOR SLIDE FUNCTIONAL TESTS GOOD IAW AMM 25-62-44 A/C OK FOR SERV"
- [SDR YENA2024121601559](https://openairdocs.org/sdr/YENA2024121601559.md): Computer · failed · Dec 14, 2024 · N562JB · Airbus A320232 · Elevator Control System
  > FLT#787, JFK-SXM. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) 'F CTL ELAC 1 PITCH FAULT IN FLIGHT. NECESSITATED A RETURN TO JFK FLT MX; REF TSM 27-93-00-810-859-A. REMOVED AND REPLACED ELAC 1 COMPUTER IAW AMM 27-93-34. REF L/P 4133099 (AS PRECAUTION R/R ELEC
- [SDR YENA2024120201516](https://openairdocs.org/sdr/YENA2024120201516.md): Autopilot Sys · abnormal · Dec 1, 2024 · N562JB · Airbus A320232 · Rudder Control System
  > FLT#2062,SJU-BOS. 'WHILE CLIMBING RECEIVED ECAM AUTO FLT RUD TRV LIMITER 1 ( RUDDER TRAVEL LIMITER SYSTEMS).' (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA2024041100512](https://openairdocs.org/sdr/YENA2024041100512.md): Unknown · odor · Apr 9, 2024 · N562JB · Airbus A320232 · Air Distribution System
  > FLT#130, RSW-JFK. 'GETTING ON OIL SMELLS IN THE CABIN WITH ENGINES RUNNING AND NO APU ( PACKS).' (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA2023122101619](https://openairdocs.org/sdr/YENA2023122101619.md): Unknown · unknown · Dec 20, 2023 · N562JB · Airbus A320232 · Air Distribution System
  > FLT#2107, JFK-FLL. 'F/A REPORTED DIRTY SOCK SMELL AT 6000 FT UNTIL LANDING (AT SAME TIME WE ENTER CLOUD DECK) ( APU SYSTEM); INSPECTED APU & NO LEAKS NOTED AFETR RECTIVATION & OPERATION OF BLEED SYSTEM AMM 21-00-00 & 36-10-00. PER INFO NOTICE 2017 T015 SUSPEC
- [SDR YENA2023121501589](https://openairdocs.org/sdr/YENA2023121501589.md): Unknown · unknown · Dec 14, 2023 · N562JB · Airbus A320232 · Hydraulic System, Main
  > FLT#1920, MSY-LGA. (AIRCRAFT DECLARED AN EMERGENCY INTO LGA), ' HYD B RESERVOIR LOW LEVEL IN FLIGHT INDICATOR SHOWED VERY LOW FLUID IN B SYSTEM; REMOVED AND REPLACED B HYD PRESS SW (10CE1) SEAL REF AMM 27-92-17. OPS CHECK OK. LEAK CHECK OK. AC OK FOR SVC.'
- [SDR YENA2023113001518](https://openairdocs.org/sdr/YENA2023113001518.md): Unknown · unknown · Nov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, Attach Fittings
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH INTERCOSTAL FITTING AT OPEN FASTENER H OLE H1, CRACK DIRECTION IS 5 OCLOCK, AT DOOR STOP FITTING 7 POSITION, AT FWD GALLEY AREA (1 EA); REF AEROMAN N/R 2023- 631069, PERFORMED REPAIR FR16LH AT LEVEL DOO
- [SDR YENA2023113001517](https://openairdocs.org/sdr/YENA2023113001517.md): Unknown · unknown · Nov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, Attach Fittings
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH INTERCOSTAL FITTING AT OPEN FASTENER H OLE H3, CRACK DIRECTION IS 5 OCLOCK, AT DOOR STOP FITTING 7 POSITION, AT FWD GALLEY AREA (1 EA); REF AEROMAN N/R 2023- 631070, PERFORMED REPAIR FR16LH AT LEVEL DOO
- [SDR YENA2023113001516](https://openairdocs.org/sdr/YENA2023113001516.md): Unknown · unknown · Nov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, Attach Fittings
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH INTERCOSTAL FITTING AT OPEN FASTENER H OLE H3, CRACK DIRECTION IS 10 OCLOCK, AT DOOR STOP FITTING 7 POSITION, AT FWD GALLEY AREA (1 EA); PERFORMED REPAIR FR16RH AT LEVEL DOOR STOP FITTING #7 HOLE 3. IAW
- [SDR YENA2023113001515](https://openairdocs.org/sdr/YENA2023113001515.md): Unknown · unknown · Nov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN INBOARD UPPER HOLE LOCATED AT DOOR STOP FITTING 7 RH SIDE, FRAME 66; CRACK LOCATION: 12 OCLOCK, CRACK DEPTH: 0.128 INCH APPROX; (RESOLVED ON W/O: 1269492 TASKCARD: NR-00012) FUR-A320-53-00976, REF A
- [SDR YENA2023113001514](https://openairdocs.org/sdr/YENA2023113001514.md): Unknown · unknown · Nov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN INBOARD UPPER HOLE LOCATED AT DOOR STOP FITTING 7 RH SIDE, FRAME 66; CRACK LOCATION: 12 OCLOCK, CRACK DEPTH: 0.128 INCH APPROX; REF AEROMAN N/R 20232-631118, PERFORMED REPAIR ON DOOR STOP FITTING #7 FR
- [SDR YENA2023113001513](https://openairdocs.org/sdr/YENA2023113001513.md): Unknown · unknown · Nov 27, 2023 · N562JB · Airbus A320232 · Elevator Structure
  > DURING HEAVY MAINTENANCE: WEAR ON BUSHING I/B ACTUATOR HING O/B LUG ON LH ELEVATOR; AFTER REMOVAL OF THE WORN BUSHING FOUND CORROSION ON THE LUG BORE FORUND TO BE OUT OF LIMITS. REMOVED AND REPLACED ELEVATOR ACTUATOR ATTACH FITTING O/B LH THIS IS A CAT "A" REP
- [SDR YENA2023113001512](https://openairdocs.org/sdr/YENA2023113001512.md): Unknown · unknown · Nov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT AREA LH SIDE CONTINUITY FITTING, CRACK LENGTH IS 0.180 INCH, IN COC KPIT (1 EA); ROTOTEST INSPECTION IN OPEN FASTENER 3 HOLES OF LH AND RH SIDES IAW NTM 51-10-0
- [SDR YENA2023113001511](https://openairdocs.org/sdr/YENA2023113001511.md): Unknown · unknown · Nov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT INTERNAL AREA, LH SIDE, FROM UPPER TENSION BOLT, CRACK LENGTH IS 0. 100 INCH, CRACK DIRECTION IS 2 OCLOCK, IN COCKPIT (1 EA); REMOVED AND REPLACED MIRROR FITTIN
- [SDR YENA2023113001510](https://openairdocs.org/sdr/YENA2023113001510.md): Unknown · unknown · Nov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: DISCREPANCY DESCRIPTION: CRACK INDICATION FOUND IN OPEN INBOARD LOWER HOLE LOCATED AT DOOR STOP FITTING 1 RH SIDE, FRAME 68; CRACK LOCATION: 06 OCLOCK, CRACK DEPTH: 0.145 INCH APPROX; (RESOLVED ON W/O: 1269492 TASKCARD: NR-00024) PE
- [SDR YENA2023113001509](https://openairdocs.org/sdr/YENA2023113001509.md): Unknown · unknown · Nov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN INBOARD LOWER HOLE LOCATED AT DOOR STOP FITTING 1 LH SIDE, FRAME 68; CRACK LOCATION: 06 AND 12 OCLOCK, CRACK DEPTH:0.187 INCH APPROX; (RESOLVED ON W/O: 1269492 TASKCARD: NR-00025) PERFORMED REPAIR ON F
- [SDR YENA2023113001508](https://openairdocs.org/sdr/YENA2023113001508.md): Unknown · unknown · Nov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: DISCREPANCY DESCRIPTION: CORROSION STRINGER 43L LOCATED BTW FRAME 62 AND FRAME 63 IN AFT CARGO COMPARTMENT (CPCP-RELATED MPD TASK 534107-01); (RESOLVED ON W/O: 1269492 TASKCARD: NR-00026) REMOVED AND REPLACED STRINGER 43L LOCATED BTW
- [SDR YENA2023113001507](https://openairdocs.org/sdr/YENA2023113001507.md): Unknown · unknown · Nov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 RH SIDE AT UPPER JOGGLE AREA, HOLE A, CRA CK DIRECTION IS 3 OCLOCK AT FWD GALLEY AREA (1EA); REF AEROMAN NR 2023-631084 WO 2023 358/1 ACCOMPLISHED REPAIR OF THE CRACK AT FR 20 RH UPPER JOGGLE AREA HOLE A I
- [SDR YENA2023113001506](https://openairdocs.org/sdr/YENA2023113001506.md): Unknown · unknown · Nov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 AT FWD GALLEY AREA (1 EA) (CRACK INDICAT ION ON FRAME 20 LH SIDE AT UPPER JOGGLE AREA, HOLE 6, CRACK DIRECTION IS 3 OCLOCK AT FWD GALLEY AREA (1 EA); REF AEROMAN NR 2023-631085 WO 2023 358/1 ACCOMPLISHED R
- [SDR YENA2023113001505](https://openairdocs.org/sdr/YENA2023113001505.md): Unknown · unknown · Nov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CORROSION FLOOR STRUCTURE ON UPPER SURFACE OF THE UPPER SKIN OF THE C ENTER WING BOX FR41 TO FR42 ON LH SIDE IN PASSENGER CABIN (CPCP RELATE D REFER MPD TASK 571157-01); REF AEROMAN NR 2023-631067 WO 2023 358/1 PERFORMED PERMANENT REP
- [SDR YENA2023113001504](https://openairdocs.org/sdr/YENA2023113001504.md): Unknown · unknown · Nov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / CENTER POST LOWER ATTACHMENT AREA AND CONTINUITY FITTING / CRACKS - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023113001503](https://openairdocs.org/sdr/YENA2023113001503.md): Unknown · unknown · Nov 27, 2023 · N562JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: WINGS / CENTER WING BOX / TOP SKIN PANEL / UPPER SURFACE / BETWEEN FR41-42 AT BEAM Y1292 TO Y1732 / CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2023012700077](https://openairdocs.org/sdr/YENA2023012700077.md): A/C Pack · odor · Jan 23, 2023 · N562JB · Airbus A320232 · Cabin Cooling System
  > FLT#953, JFK-PBI. 'AFT CABIN ODOR REPORTED BY INFLIGHT CREW. PACK 2 WAS ISOLATED, ODOR WENT AWAY; COMPLIED WITH INFO NOTICE 2017-T015J, SECTION B2. DECONTAMINATION LEVEL A ACCOMPLISHED PER TSM 05-50-00-810-831-A. IDENTIFIED PACK 2 AS A SOURCE OF ODOR. REF.
- [SDR YENA2022082600821](https://openairdocs.org/sdr/YENA2022082600821.md): Thermostat · failed · Aug 23, 2022 · N562JB · Airbus A320232 · Pneumatic System
  > FLT#8097, JFK-DEN. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) 'SHORTLY AFTER T/O, WE RECEIVED A AIR ENG 1 BLEED FAULT. LEVELS AT 8,000 RAN QRC ECAM & QRH PROCEDURES. NEEDED TO AVOID ICING CONDITIONS. WHICH WE WERE UNABLE TO THUS FORCING US TO RETURN TO JFK.
- [SDR YENA202206270621](https://openairdocs.org/sdr/YENA202206270621.md): None · none · Jun 26, 2022 · N562JB · Airbus A320232 · Air Conditioning System
  > FLT#109, BOS-JAX. 'STRONG DIRTY SOCK ODOR ON DESCENT AND ARRIVAL STARTED AT 11000 FEET. TURNED OFF PACK 1 AND IT AIDED SOME. FRESH OIL FROM THE BOTTOM OF THE TAIL SEEPING FROM SEVERAL AREAS OF APU. APU LOW OIL WRITE UP AND SERVICED 3 DAYS AGO ODOR REPORTING FO
- [SDR YENA2022010400007](https://openairdocs.org/sdr/YENA2022010400007.md): Unknown · odor · Dec 28, 2021 · N562JB · Airbus A320232 · Air Distribution System
  > FLT 275, BDL-SJU. "TRANSIENT ENVIRONMENTAL ODOR " DETECTED DURING APPROACH PHASE. MILD TO MODERATE ODOR LASTED 10 MINUTES OF FLIGHT LOCATED AFT OF CABIN. DETECTED BY 2 AFT FLIGHT ATT. DESCRIBED AS LEVEL II.; COMPLIED WITH INFO NOTICE 2017-T015I SECTION A(A),
- [SDR YENA2021031900177](https://openairdocs.org/sdr/YENA2021031900177.md): Fairing · out of adjust · Mar 16, 2021 · N562JB · Airbus A320232 · Nose/Tail Landing Gear
  > FLT 6302, EWR- JFK. NOSE GEAR DOOR DID NOT CLOSE AFTER T/O CYCLED GEAR AND STILL DID NOT CLOSE UNTILL FIFTEEN MINUTES BEFORE LANDING; ADJUSTED NLG LEG FAIRING IAW AMM 32-22-00; PERFORMED NORMAL EXTENSION AND RETRACTION OPERATIONAL TEST IAW AMM 32-31-00-720-00
- [SDR YENA2021022600134](https://openairdocs.org/sdr/YENA2021022600134.md): Control Unit · failed · Feb 25, 2021 · N562JB · Airbus A320232 · Landing Gear Steering System
  > FLT 2469, BOS-FLL. WHEEL N/W STRG FAULT IN FLIGHT; R & R BSCU IAW AMM 32-42-34. PERFORMED OPS CK OF STEERING AND NO FAULT NOTED AT THIS TIME
- [SDR YENA2021022600133](https://openairdocs.org/sdr/YENA2021022600133.md): Control Unit · failed · Feb 25, 2021 · N562JB · Airbus A320232 · Landing Gear Steering System
  > FLT 2469, BOS-FLL. WHEEL N/W STRG FAULT IN FLIGHT; R & R BSCU IAW AMM 32-42-34. PERFORMED OPS CK OF STEERING AND NO FAULT NOTED AT THIS TIME
- [SDR YENA2021022600132](https://openairdocs.org/sdr/YENA2021022600132.md): Control Unit · failed · Feb 25, 2021 · N562JB · Airbus A320232 · Landing Gear Steering System
  > FLT 2469,BOS-FLL. WHEEL N/W STRG FAULT IN FLIGHT; R & R BSCU IAW AMM 32-42-34. PERFORMED OPS CK OF STEERING AND NO FAULT NOTED AT THIS TIME
- [SDR YENA2021020500091](https://openairdocs.org/sdr/YENA2021020500091.md): Keelbeam · cracked · Jan 31, 2021 · N562JB · Airbus A320232 · Fuselage Main, Keel
  > DURING HEAVY MAINTENANCE, CRACK INDICATION ON WEB OF TI ANGLE RT HAND AT FR41-42 LOWER HOLE POSITION; (REF AEROMAN NR 2021-12/1-2021-30271 -) ACCOMPLISHED REPAIR OF THE CRACK DAMAGE, FR 41-42 ON THE KEEL BEAM RT HANDS IAW AEROMAN EA 53-0019-21 AND AIRBUS RDAS
- [SDR YENA2020120800568](https://openairdocs.org/sdr/YENA2020120800568.md): Pump · failed · Dec 1, 2020 · N562JB · Airbus A320232 · Engine Fuel Pump
  > FLT 1421, PHL-SJU. RETURNED TO FIELD. FUEL FLOW FLUCTUATION. R & R NR 2 ENGINE FUEL PUMP, REF AMM 73-12-41. OPERATIONS AND LEAK CHECK GOOD.
- [SDR YENA2020120800567](https://openairdocs.org/sdr/YENA2020120800567.md): Transmitter · failed · Dec 1, 2020 · N562JB · Airbus A320232 · Engine Fuel Indicating System
  > FLT 1421, PHL-SJU. RETURNED TO FIELD. FUEL FLOW FLUCTUATION. R & R NR 2 ENGINE FUEL FLOW TRANSMITTER, REF AMM 73-31-17. OPERATIONS CHECK OK.
- [SDR YENA2020120700566](https://openairdocs.org/sdr/YENA2020120700566.md): Fmu · failed · Dec 1, 2020 · N562JB · Airbus A320232 · Fuel Controlling System
  > FLT 1421, PHL-SJU. RETURNED TO FIELD. ON CLIMBOUT FUEL FLOW INDICATION INDICATED A FLUCTUATION OF BETWEEN 1800-8000 LB/HR ON ENGINE NR 2. PREVIOUSLY WRITTEN UP. R & R NR 2 ENGINE FMU, REF AMM 73-22-52. OPERATIONS CHECK OK. PERFORM HIGH POWER ASSURANCE R
- [SDR YENA2020012950066](https://openairdocs.org/sdr/YENA2020012950066.md): Battery · no test · Jan 25, 2020 · N562JB · Airbus A320232 · Emergency Lighting
  > EMER LT BAT CAPACITY TEST FAIL; PER T/C A320-33-51-00-710-003 R & R EMER LT BAT AS REQ MM 33-51-00.
- [SDR YENA2020012925065](https://openairdocs.org/sdr/YENA2020012925065.md): Battery · no test · Jan 25, 2020 · N562JB · Airbus A320232 · Emergency Lighting
  > EMER LT BAT CAPACITY TEST FAIL; PER T/C A320-33-51-00-710-003 R & R EMER LT BAT AS REQ MM 33-51-00.
- [SDR YENA202001285064](https://openairdocs.org/sdr/YENA202001285064.md): Battery · no test · Jan 25, 2020 · N562JB · Airbus A320232 · Emergency Lighting
  > EMER LT BAT CAPACITY TEST FAIL; PER T/C A320-33-51-00-710-003 R & R EMER LT BAT AS REQ MM 33-51-00.
- [SDR YENA201710010810](https://openairdocs.org/sdr/YENA201710010810.md): Door Sill · corroded · Oct 1, 2017 · N562JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE R2 DOOR SILL UPPER SURFACE AFT INBD CORNER FRAME 68, STRINGER 23. REPLACED THE DOOR SILL IAW SRM 51-42-11.
- [SDR YENA201710010809](https://openairdocs.org/sdr/YENA201710010809.md): Door Sill · corroded · Oct 1, 2017 · N562JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON L2 DOOR SILL AFT OF THE INBD CORNER UPPER SURFACE AT FRAME 68, STRINGER 23L. REPLACED THE DOOR SILL IAW SRM 53-41-14-283-002.
- [SDR YENA201710010808](https://openairdocs.org/sdr/YENA201710010808.md): Floor Support · corroded · Oct 1, 2017 · N562JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN FLOOR SUPPORT-Y1292, FRAME 20 STRINGER 23R. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11.
- [SDR YENA201710010803](https://openairdocs.org/sdr/YENA201710010803.md): Floor Support · corroded · Oct 1, 2017 · N562JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN FLOOR SUPPORT Y503 FRAME 20, STRINGER 23R. REPLACED THE FLOOR SUPPORT IAW SRM 53-11-14.
- [SDR YENA201710010807](https://openairdocs.org/sdr/YENA201710010807.md): Floorbeam · corroded · Oct 1, 2017 · N562JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOORBEAM Y464, FRAME 66 +10. REPLACED THE FLOORBEAM IAW SRM 51-72-11.
- [SDR YENA20171001806](https://openairdocs.org/sdr/YENA20171001806.md): Floorbeam · corroded · Oct 1, 2017 · N562JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN FLOORBEAM Y1292 FR 16. REPLACED THE FLOORBEAM IAW SRM 51-72-11.
- [SDR YENA20171001805](https://openairdocs.org/sdr/YENA20171001805.md): Floorbeam · corroded · Oct 1, 2017 · N562JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN FLOORBEAM -Y1732 FR 20. REPLACED THE FLOORBEAM IAW SRM 51-72-11.
- [SDR YENA20171001804](https://openairdocs.org/sdr/YENA20171001804.md): Floorbeam · corroded · Oct 1, 2017 · N562JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT FLOORBEAM -Y1292 FRAME 68. REPLACED THE FLOORBEAM IAW IAW SRM 51-42-11.
- [SDR YENA20171001803](https://openairdocs.org/sdr/YENA20171001803.md): Dummy Rail · corroded · Oct 1, 2017 · N562JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION WAS DISCOVERED ON FWD CABIN DUMMY RAIL, Y503, FRAME 20. REPLACED THE DUMMY RAIL IAW SRM 53-11-14.
- [SDR YENA201708180665](https://openairdocs.org/sdr/YENA201708180665.md): Lens · broken · Aug 18, 2017 · N562JB · Airbus A320232 · Emergency Lighting
  > EMERGENCY EXIT LIGHT LENS AT SEAT 11C IS BROKEN. REPLACED THE LENS, OK FOR SERVICE.
- [SDR YENA201705070355](https://openairdocs.org/sdr/YENA201705070355.md): Control Panel · failed · May 7, 2017 · N562JB · Airbus A320232 · Communications System
  > SMOKE PUSHBUTTON INDICATING RED SMOKE ON THE AFT AVIONICS RACK. NO AURAL WARNING. QRA COMPLETE. R & R SDCP IAW AMM 23-39-00 SECT 4000, STEP 25 AND PERFORMED ELECTRICAL ODOR SYSTEM INTEGRITY CHECK IAW AMM 23-39-00, SECT 5000, STEP 10. NO ODOR OR FAULT NOTE
- [SDR YENA20160130086](https://openairdocs.org/sdr/YENA20160130086.md): Floor Support · corroded · Jan 30, 2016 · N562JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN, AFT WET AREA, FLOOR SUPPORT 1292, FRAME 66. R & R THE FLOOR SUPPORT BETWEEN FRAMES 66 - 64 IAW SRM 53-72-11, 51-42-11 PARA 2D, 51-21-11, 51-23-12 & GMM 5-169.

Next page: https://openairdocs.org/aircraft/N562JB/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 = 'N562JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N562JB/reports

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