# Service difficulty reports: N585JB

A list on [N585JB](https://openairdocs.org/aircraft/N585JB.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 · 80 reports

- [SDR YENA2026040300369](https://openairdocs.org/sdr/YENA2026040300369.md): Unknown · odor · Apr 2, 2026 · N585JB · Airbus A320232 · Air Distribution System
  > FLT 721 BOS-PBI. SOCK ODOR ON LANDING BELOW 10000 JUMP SEATER PICKED UP ON IT. C/W INFO NOTICE 2017-T015 DETERMINER TO BE TYPE 10 AMBIENT PER TSM 05-50-00 NO APU FINDINGS OR LEAKS NOTED ACCOMPLISHED DECONTAMINATIOPN PER MM 21-00-00 AIRCRAFT OK FOR SVC.
- [SDR YENA2025120201167](https://openairdocs.org/sdr/YENA2025120201167.md): Door Actuator · cracked · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE A FR16 LH DOUBLE JOGGLE AREA, CRACK DIRECTION 3 OCLOCK AND CRACK DEPTH 0.077 INCH. CONFIRM INDICATION OF CRACK USING BOROSCOPE AS PER NTM 51-90-00. PERFORMED PERMANENT REPAIR ON PRIMARY STRUCTURE A
- [SDR YENA2025120201166](https://openairdocs.org/sdr/YENA2025120201166.md): Door Frame · cracked · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 AT FWD GALLEY AREA (1 EA) (CRACK INDICATION FOUND IN OPEN HOLE 7 FR16 LH DOUBLE JOGGLE AREA, CRACK DIRECTION 3 OCLOCK AND CRACK DEPTH 0.107 INCH. CONFIRM INDICATION OF CRACK USING BOROSCOPE AS PER NTM 51-9
- [SDR YENA2025120201165](https://openairdocs.org/sdr/YENA2025120201165.md): Door Frame · cracked · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 AT FWD GALLEY AREA (1 EA) (CRACK INDICATION FOUND IN OPEN HOLE D FR16 LH DOUBLE JOGGLE AREA, CRACK DIRECTION 9 OCLOCK AND CRACK DEPTH 0.101 INCH. CONFIRM INDICATION OF CRACK USING BOROSCOPE AS PER NTM 51-9
- [SDR YENA2025120201164](https://openairdocs.org/sdr/YENA2025120201164.md): Door Frame · cracked · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 AT FWD GALLEY AREA (1 EA) (CRACK INDICATION FOUND IN OPEN HOLE B FR16 RH DOUBLE JOGGLE AREA, CRACK DIRECTION 3 OCLOCK AND CRACK DEPTH 0.081 INCH. CONFIRM INDICATION OF CRACK USING BOROSCOPE AS PER NTM 51-9
- [SDR YENA2025120201163](https://openairdocs.org/sdr/YENA2025120201163.md): Door Frame · cracked · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 AT FWD GALLEY AREA (1 EA) (CRACK INDICATION FOUND IN OPEN HOLE C FR16 RH DOUBLE JOGGLE AREA, CRACK DIRECTION 9 OCLOCK AND CRACK DEPTH 0.102 INCH. CONFIRM INDICATION OF CRACK USING BOROSCOPE AS PER NTM 51-9
- [SDR YENA2025120201162](https://openairdocs.org/sdr/YENA2025120201162.md): Door Frame · cracked · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 AT FWD GALLEY AREA (1 EA) (CRACK INDICATION FOUND IN OPEN HOLE A FR16 RH DOUBLE JOGGLE AREA, CRACK DIRECTION 9 OCLOCK AND CRACK DEPTH 0.086 INCH. CONFIRM INDICATION OF CRACK USING BOROSCOPE AS PER NTM 51-9
- [SDR YENA2025120201161](https://openairdocs.org/sdr/YENA2025120201161.md): Door Frame · cracked · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 AT FWD GALLEY AREA (1 EA) (CRACK INDICATION FOUND IN OPEN HOLE A FR16 RH DOUBLE JOGGLE AREA, CRACK DIRECTION 9 OCLOCK AND CRACK DEPTH 0.086 INCH. CONFIRM INDICATION OF CRACK USING BOROSCOPE AS PER NTM 51-9
- [SDR YENA2025120201160](https://openairdocs.org/sdr/YENA2025120201160.md): Door Frame · cracked · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 AT FWD GALLEY AREA (1 E/A) (CRACK INDICATION FOUND OPEN HOLE B FR16 LH DOUBLE JOGGLE AREA) PERFORMED PERMANENT REPAIR ON PRIMARY STRUCTURE AT HOLE B FR16 LH DOUBLE JOGGLE AREA IAW SRM 53-11-12-300-012.
- [SDR YENA2025120201159](https://openairdocs.org/sdr/YENA2025120201159.md): Support · corroded · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOC. STR23L AND FR68 AT AFT GALLEY AREA. PERFORMED PERMANENT REPAIR ON LOWER SILL LOC. STR23L AND FR68 AT AFT GALLEY AREA IAW SRM A320 53-41-14-300-001 THIS REPAIR IS CATEGORY A AND FURTHER INSPECTION.;
- [SDR YENA2025120201158](https://openairdocs.org/sdr/YENA2025120201158.md): Skin · no discrepancy · Nov 30, 2025 · N585JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE OF TOP SKIN LOC. REAR SPAR BTW RIB18 AND RIB19 ON LH WING; EVALUATED REWORK AREA ON UPPER SURFACE OF TOP SKIN REAR SPAR BTW RIB18 AND RIB19 ON LH WING AND FOUND WITHIN LIMITS IAW SRM 57-21-11-283-007.
- [SDR YENA2025120201157](https://openairdocs.org/sdr/YENA2025120201157.md): Door Frame · cracked · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 16 LT SIDE DOOR STOP 7 LOWER OUTBOARD HOLE AT 12 OCLOCK, CRACK LENGTH 0.078 INCH APROX; PERFORMED PERMANENT REPAIR OUTBOARD HOLE ON FR 16 LH SIDE DOOR STOP 7 LOWER IAW SRM 53-11-12-300-010 AND DWG D531354
- [SDR YENA2025120201156](https://openairdocs.org/sdr/YENA2025120201156.md): Window Frame · cracked · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON WINDSHIELD IN COCKPIT (1 EA) (CRACK INDICATION FOU ND CONTINUITY FITTING WINDSHIELD RH SIDE.. CRACK DIRECTION VERTICAL. CRACK LENGTH 0.200 INCH.); PERFORMED REPAIR TO CRACKS AFFECTING THE WINDSHIELD FRAMING CENTER
- [SDR YENA2025120201155](https://openairdocs.org/sdr/YENA2025120201155.md): Window Frame · cracked · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CENTER POST, LOWER ATTACHMENT ARE A, INBOARD LOWER RADIUS LH SIDE, CRACK LONGITUDINAL DIRECTION, LENGTH= 0.120 INCHES APPROX; PERFORMED REPAIR TO CRACKS AFFECTING THE WINDSHIELD FRAMING CENTER POST
- [SDR YENA2025120201154](https://openairdocs.org/sdr/YENA2025120201154.md): Skin · dented · Nov 30, 2025 · N585JB · Airbus A320232 · Horizontal Stabilizer, Plate/Skin
  > DURING HEAVY MAINTENANCE: SEVERAL DENTS ON ACCESS PANEL 341BB LEADING EDGE ON RH HORIZONTAL STABILIZER; EVALUATED DENTS ON ACCESS PANEL 341BB LEADING EDGE ON RH HORIZONTAL STABILIZER AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS AS PER A320 SRM 55-12-11-283-003 PA
- [SDR YENA2025120201153](https://openairdocs.org/sdr/YENA2025120201153.md): Shear Plate · cracked · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CRACK SHEAR PLATE STR 23R FR 69-FR 70; R & R SHEAR PLATE STR 23R FR 69-FR 70 IAW A320 SRM 51-72-11, SRM 51-42-11 & DWG D53474180.
- [SDR YENA2025120201152](https://openairdocs.org/sdr/YENA2025120201152.md): Shear Plate · cracked · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CRACK SHEAR PLATE STR 23L FR69-FR70; R& R SHEAR PLATE STR 23L FR 69-FR 70 IAW A320 SRM 51-72-11, 51-42-11 & DWG D53474180.
- [SDR YENA2025120201151](https://openairdocs.org/sdr/YENA2025120201151.md): Fitting · cracked · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: NOSE FWD FUSELAGE RACK 10VU LUGS SEVERAL FINDINGS WITH CRACKED OR BROKEN FITTINGS.
- [SDR YENA2025120201150](https://openairdocs.org/sdr/YENA2025120201150.md): Floorbeam · cracked · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE: CENTER BOX FR36 FLOORBEAM CRACKED.
- [SDR YENA2025120201149](https://openairdocs.org/sdr/YENA2025120201149.md): Window Post · cracked · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: NOSE FWD FUSELAGE WINDSHIELD FRAME, CENTER POST LOWER NODE AREA CONTINUITY FITTING RT & LT SIDE CRACKED.
- [SDR YENA2025120201148](https://openairdocs.org/sdr/YENA2025120201148.md): Pressure Panel · cracked · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CENTER FUSELAGE, FR 36 LT SIDE PRESSURE PANEL, HOLES #6, 7, 15 & 20 / CRACKED.
- [SDR YENA2025120201147](https://openairdocs.org/sdr/YENA2025120201147.md): Pressure Blkhd · cracked · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage Main, Bulkhead
  > DURING HEAVY MAINTENANCE: FUSELAGE CENTER FUSELAGE, FR35 & STGR 30L PRESSURE BULKHEAD ATTACHMENT HOLES CRACKED
- [SDR YENA2025120201146](https://openairdocs.org/sdr/YENA2025120201146.md): Stringer · corroded · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 43L LOC, BTW FR. 56 TO FR. 57 ON FLOOR SURFACE IN AFT CARGO COMPARTMENT REMOVED AND REPLACED STRINGER LOC.BTW FR54 TO FR60 STRG 43L ON AFT CARGO COMPARTMENT I.A.W A320 SRM 51-42-11, A320 SRM 51-72-11 AND DWG E534703
- [SDR YENA2025120201145](https://openairdocs.org/sdr/YENA2025120201145.md): Stringer · corroded · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 42L LOC. BTW FR. 54 TO FR. 58 ON FLOOR SURFACE I N AFT CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR STRINGER 42L LOC. BTW FR. 54 TO FR. 58 ON FLOOR SURFACE IN AFT CARGO COMPARTMENT I.A.W. A320 SRM 53-00-13-300-00
- [SDR YENA2025120201144](https://openairdocs.org/sdr/YENA2025120201144.md): Dummy Rail · corroded · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE: CORROSION RAIL DUMMY Y503.2 LOC. BTW FR12 AND FR16 FWD GALLEY AREA, REPLACED RAIL DUMMY Y503.2 LOC. BTW FR12 AND FR16 FWD GALLEY AREA IAW A320 SRM 51-42-11, SRM 51-72-11-911-001 AND DWG D53112826, D53112056
- [SDR YENA2025120201143](https://openairdocs.org/sdr/YENA2025120201143.md): Seat Track · corroded · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE: CORROSION FLOOR BEAM -Y464 LOC. BTW FR64 ANF FR68 AT AFT GALLEY AREA. REPLACED FLOOR BEAM -Y464 LOC. BTW FR64 AND FR68 AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DWG D53472816.
- [SDR YENA2025120201142](https://openairdocs.org/sdr/YENA2025120201142.md): Seat Track · corroded · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE: CORROSION FLOOR BEAM +Y765 LOC. BTW FR12 AND FR24 AT FWD GALLEY AREA. REPLACED FLOOR BEAM Y765, LOC. BTW FR 12 TO FR24 FWD GALLEY AREA IAW A320 SRM 51-72-11 AND DWG D53112812 DWG D53110097 DWG D53110984 DWG D53110920,
- [SDR YENA2025120201141](https://openairdocs.org/sdr/YENA2025120201141.md): Seat Track · corroded · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE: CORROSION FLOOR BEAM -Y765 LOC. BTW FR12 AND FR24 AT FWD GALLEY AREA. REPLACED FLOOR BEAM -Y765 LOC. BTW FR12 AND FR24 AT FWD GALLEY AREA IAW A320 SRM 51-72-11, DWG D53112812, DWG D533110984 DWG D53110876,
- [SDR YENA2025120201140](https://openairdocs.org/sdr/YENA2025120201140.md): Seat Track · corroded · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE: CORROSION FLOOR BEAM +Y1292 LOC. BTW FR12 AND FR24 AT FWD GALLEY AREA. REPLACED FLOOR BEAM Y1292 LOC. BTW FR12 TO FR24 FWD GALLEY AREA IAW A320 SRM 51-72-11 AND DWG D53112812 DWG D53110097 DWG D53110984 DWG D53110920,
- [SDR YENA2025120201139](https://openairdocs.org/sdr/YENA2025120201139.md): Seat Track · corroded · Nov 30, 2025 · N585JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE: CORROSION FLOOR BEAM -Y1292 LOC. BTW FR12 AND FR24 AT FWD GALLEY AREA. REPLACED FLOOR BEAM -Y1292 LOC. BTW FR12 AND FR24 AT FWD GALLEY AREA I.A.W SRM 51-72-11 AND DWG D53112812, D53112639, D53110876,
- [SDR YENA2023121501579](https://openairdocs.org/sdr/YENA2023121501579.md): Transceiver · failed · Dec 11, 2023 · N585JB · Airbus A320232 · Communications System
  > FLT#2851, FLL-UIO. 'LOST COM 1 OCCURRED RIGHT AFTER TAKE OFF; FOLLOWED TSM 23-12-00-810-813-A, VERFIED WITH CREW, VHF 1 ONLY UNABLE TO TRANSMITT. OK TO RX. VHF 1 OK ON GROUND AT ALL TIMES. PFR AND BITE TEST SHOWED 1RC1 AT FAULT. REMOVED AND REPLACED VHF 1 TRAN
- [SDR YENA2022012400024](https://openairdocs.org/sdr/YENA2022012400024.md): Adiru · failed · Jan 23, 2022 · N585JB · Airbus A320232 · Flight Environment Data
  > FLT #1 139, JFK-BQN(AIR TURNBACK TO JFK). ON CLIMB OUT ADR 1 FAULT ECAM, HOWEVER NO ATT/HDG DISPLAY ON PFD 1 + NO 1. RAN ADR 1 QRH + 1R1 QRH IR 1 RECOVERED IN ATT ONLY MODE. PRECAUTIONARY RETURN TO JFK.; R + R ADR 1 FIN 1FP1 AMM 32-12-34. OPS CK NORM. NO F
- [SDR YENA2021102700725](https://openairdocs.org/sdr/YENA2021102700725.md): Unknown · odor · Oct 26, 2021 · N585JB · Airbus A320232 · Air Distribution System
  > FLT 371, LGA-FLL. DIRTY SOCK SMELL THROUGHOUT AIRCRAFT FROM FL190-10,000 FT, SMELL CLEARED UP THEREAFTER; COMPLIED WITH INFORMATION NOTICE 2017-TO15 SECTION A(A), ISOLATED FAULT TO TYPE 10(A), 1, C PER TSM 05-50-00-810-085-B/TSM 05-50-00-810-085-D AIRCRAFT IS
- [SDR YENA2021070700431](https://openairdocs.org/sdr/YENA2021070700431.md): Apu · contaminated · Jul 2, 2021 · N585JB · Airbus A320232 · Airborne Auxiliary Power Unit (APU) System
  > FLT 851, JFK-CUN. BELOW 10FT FA NOTICE ODOR BECAME STRONGER APPROACH TO LAND FA SAID SICK ( PACKS); ACCOMPLISHED ECS DECONTAMINATION IAW AMM 21-00-00-615-803. SOURCE OF ODOR COMING FROM APU. MDDR CLARED MX-4 UPDATED PLACARD REMOVED.
- [SDR YENA2021060400351](https://openairdocs.org/sdr/YENA2021060400351.md): Priority Valve · leaking · Jun 3, 2021 · N585JB · Airbus A320232 · Hydraulic System, Main
  > FLT# 1051, HPN-JFK. YELLOW HYDRAULIC SYSTEM LOSING QUANTITY IN FLIGHT; FOUND LEAKING YELLOW SYS PRIORITY VALVE OF YELLOW SYS REF AMM 29-13-33. OPS CHK AND LEAK CHK OPS GOD.
- [SDR YENA2021060700360](https://openairdocs.org/sdr/YENA2021060700360.md): Unknown · odor · May 16, 2021 · N585JB · Airbus A320232 · Air Distribution System
  > FLT 2118, NAS-EWR. FA REPORTS ODOR FROM BACK 1/2 OF AIRCRAFT IN DESCENT; REF INFO NOTICE 2017-T015F PERFORMED STEPS TO TRY TO REPRODUCE ODOR ON GROUND, NO ODOR NOTED. INSPECTED AFT HALF OF CABIN AND DID NOT NOTE ANY BAD ODORS. A/C OK FOR SVC
- [SDR YENA2021043000299](https://openairdocs.org/sdr/YENA2021043000299.md): Unknown · odor · Apr 27, 2021 · N585JB · Airbus A320232 · Air Distribution System
  > FLT # 473, BOS-AUA. STRONG FUMES AFT ON CLIMBOUT WHICH DISAPPEARED @ CRUISE IN DESCENT FUMES STRONG OBSERVED COCKPIT AND CABIN FOLLOWED ALL FROM V1 SUPP PROCEDURES COCKPIT CABIN ODOR RECOGNITION & ISOLATION QRH PROCEDURES; INFO NOTICE 2017-T015F LVL ODOR COMP
- [SDR YENA2020010210004](https://openairdocs.org/sdr/YENA2020010210004.md): Epsu · failed · Jan 1, 2020 · N585JB · Airbus A320232 · Emergency Lighting
  > FT # 433, DCA-PBI. EMERGENCY LIGHTS AT 51WL AND 43WL INOP; R & R EPSU AT 11WL IAW AMM 33-51-38 REPLACED EMERGENCY LIGHT ASSY AT 43WL IAW AMM 33-51-17. REPLACED BATTERY TO EPSU AT 11WL IAW AMM 33-51-38 ALL OPS CHECKS OKAY.
- [SDR YENA2020010210003](https://openairdocs.org/sdr/YENA2020010210003.md): Battery · discharged · Jan 1, 2020 · N585JB · Airbus A320232 · Emergency Lighting
  > FT # 433, DCA-PBI. EMERGENCY LIGHTS AT 51WL AND 43WL INOP; R & R EPSU AT 11WL IAW AMM 33-51-38 REPLACED EMERGENCY LIGHT ASSY AT 43WL IAW AMM 33-51-17. REPLACED BATTERY TO EPSU AT 11WL IAW AMM 33-51-38 ALL OPS CHECKS OKAY.
- [SDR YENA2020010210002](https://openairdocs.org/sdr/YENA2020010210002.md): Battery · discharged · Jan 1, 2020 · N585JB · Airbus A320232 · Emergency Lighting
  > FT # 433, DCA-PBI. EMERGENCY LIGHTS AT 53WL AND 42WL INOP; R & R EPSU AT (12WL) AND BATTERY A 12WL IAW AMM 33-51-38 OPS CHECK OKAY.
- [SDR YENA2020010210001](https://openairdocs.org/sdr/YENA2020010210001.md): Epsu · failed · Jan 1, 2020 · N585JB · Airbus A320232 · Emergency Lighting
  > FT # 433, DCA-PBI. EMERGENCY LIGHTS AT 53WL AND 42WL INOP; R & R EPSU AT (12WL) AND BATTERY A 12WL IAW AMM 33-51-38 OPS CHECK OKAY.
- [SDR YENA2019121610700](https://openairdocs.org/sdr/YENA2019121610700.md): Power Supply · failed · Dec 11, 2019 · N585JB · Airbus A320232 · Emergency Lighting
  > FT # 8, LAS-FLL. WITH AIRCRAFT POWER OFF R/H OVERWING EXIT HATCH "SLIDE ARMED" LIGHT REMAINS ILLUMINATED WITH POWER ON. R/H OVERWING "EXIT SALIDA" SIGN DOES NOT COME ON WITH EMERGENCY LIGHTS SELECTED ON; REPLACED R/H OVERWING PSU & BATTERY PER M/M 33-51-38. OP
- [SDR YENA2019121610699](https://openairdocs.org/sdr/YENA2019121610699.md): Battery Pack · failed · Dec 11, 2019 · N585JB · Airbus A320232 · Emergency Lighting
  > FT # 8, LAS-FLL. WITH AIRCRAFT POWER OFF R/H OVERWING EXIT HATCH " SLIDE ARMED" LIGHT REMAINS ILLUMINATED WITH POWER ON. R/H OVERWING "EXIT SALIDA" SIGN DOES NOT COME ON WITH EMERGENCY LIGHTS SELECTED ON; REPLACED R/H OVERWING PSU & BATTERY PER M/M 33-51-38. O
- [SDR YENA2019112510677](https://openairdocs.org/sdr/YENA2019112510677.md): Stringer · corroded · Nov 21, 2019 · N585JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE, (NR 2019-313245) CORROSION STRINGER 43R COUPLING LOC BTW FR27 TO FR28 TO IN FWRD CARGO COMPARTMENT; REMOVED & REPLACED COUPLING LOC BTW FR27 - FR28 AND STR 43R IN FWD CARGO COMPARTMENT IAW A320-SRM 51-72-11 AND DRWG # D53231776. TOOL
- [SDR YENA2019112510676](https://openairdocs.org/sdr/YENA2019112510676.md): Dummy Rail · corroded · Nov 21, 2019 · N585JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE, (NR 2019-313319) CORROSION DUMMY RAIL Y 503.2 FR 16 AT FWD GALLEY AREA; REMOVED AND REPLACED RAIL DUMMY Y503.2 BTW FR 12 - FR16 AT LEVEL STR 23L FWD GALLEY AREA IAW A320-51-72-11 AND DRAWING D53112825 AND DRAWING 53112826 TOOL USED CA
- [SDR YENA201911251675](https://openairdocs.org/sdr/YENA201911251675.md): Web · corroded · Nov 21, 2019 · N585JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, (NR 2019-313314) CORROSION FR69 TO FR70 WEB LEVEL AT AFT GALLEY AREA; REMOVED & REPLACED WEB LOC AT LEVEL STR 23R AND BTW FR69 - FR70 IAW A320 SRM 51-72-11 AND DRAWING #D53474180 TOOL USED: CALIPER P/N 500-197-30 S/N A18229578 DUE
- [SDR YENA201911251674](https://openairdocs.org/sdr/YENA201911251674.md): Floor Support · corroded · Nov 21, 2019 · N585JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, (NR 2019-313313) CORROSION FLOOR BEAM -Y1225 LOC BTW FR66 - FR68 AT AFT GALLEY AREA; REMOVED AND REPLACED FLOOR BEAM -Y1225 BTW FR66 - 68 AND STR 23R AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DRAWING # D53472780 TOOL USED CALIPER
- [SDR YENA201911251673](https://openairdocs.org/sdr/YENA201911251673.md): Floor Support · corroded · Nov 21, 2019 · N585JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, (NR 2019-313315) CORROSION FLOOR BEAM + Y1225 LOC BTW FR66 - FR68 AND STR 23L AT AFT GALLEY AREA; REMOVED AND REPLACED FLOOR BEAM +Y1225 LOC BTW FR66 TO FR68 AND STR 23L AT AFT GALLETY AREA IAW A320 SRM 51-72-11 AND DRAWING # D5347278
- [SDR YENA201911251672](https://openairdocs.org/sdr/YENA201911251672.md): Structure · corroded · Nov 21, 2019 · N585JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE, (NR 2019-313370) CORROSION LOWER SILL BTW FR66 - FR68 AT LEVEL STR23L AT AFT GALLEY AREA; REMOVED AND REPLACED LOWER SILL LOCATED BTW FR66 - FR68 AT LEVEL STR 23L AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DRAWING D53480505. TOOL U
- [SDR YENA201911251671](https://openairdocs.org/sdr/YENA201911251671.md): Structure · corroded · Nov 21, 2019 · N585JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE, (REF NR 2019-313369) CORROSION LOWER SILL LOC BTW FR66 TO 68 AT LEVEL STR23 AT AFT GALLEY AREA; REMOVED AND REPLACED LOWER SILL BTW FR66 TO FR68 AT LEVEL STR 23R AT AFT GALLEY AREA IAW SRM A 320-51-72-11 AND A320 51-72-11 AND DRAWING

Next page: https://openairdocs.org/aircraft/N585JB/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 = 'N585JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N585JB/reports

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