# Service difficulty reports: N613JB

A list on [N613JB](https://openairdocs.org/aircraft/N613JB.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 · 96 reports

- [SDR YENA2026080300642](https://openairdocs.org/sdr/YENA2026080300642.md): Apu · odor · Jul 31, 2026 · N613JB · Airbus A320232 · Airborne Auxiliary Power Unit (APU) System
  > FLT 1098, MCO-BOS (AIRTURN BACK). DIRTY SOCK ODOR IN CABIN AND FLIGHT DECK, APU BLEED HAD BEEN ON FOR APPROX 10 MINS, ODOR BEGAN APPROX 5 MIN AFTER RAIN STARTED, ( APU BLEED AIR SUPPLY SYSTEM) FUME EVENT COCKPIT & AFT CABIN TRIED ISOLATION CHECKLIST BUT COU
- [SDR YENA20260210001](https://openairdocs.org/sdr/YENA20260210001.md): Skin · corroded · Feb 8, 2026 · N613JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: RT WING TOP SKIN PANEL CORRODED /1/ - AIRBUS DOSSIER 81709907 /2/ - AIRBUS RDAF REF. & ISSUE.: 81709907/003/2025 ISSUE A /3/ - AIRBUS RI R572-44701 ISSUE B /4/ - AIRBUS RI R572-58616 ISSUE N /5/ - AIRBUS RI R572-58926 ISSUE E /6/ - A
- [SDR YENA2026021100194](https://openairdocs.org/sdr/YENA2026021100194.md): Skin · dented · Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN LOCATED FR5 TO FR6 AND 14 INCHES BELOW LH SIDE STRI NGER AT LOWER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00006) REF AE WO # 2025-414/1 NR # 2025-717347 EVALUATED DENT EXTERNAL SKIN LOCATED FR5 TO FR6 AND 1
- [SDR YENA2026021100193](https://openairdocs.org/sdr/YENA2026021100193.md): Skin · dented · Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN LOCATED FR30 TO FR31 BTW STR39L TO STR40L AT LOWER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00007) REF AE WO # 2025-414/1 NR # 2025-717348 EVALUATED DENT EXTERNAL SKIN LOCATED FR30 TO FR31 BTW STR39L TO STR4
- [SDR YENA2026021100192](https://openairdocs.org/sdr/YENA2026021100192.md): Skin · dented · Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN LOCATED FR70 TO FR71 BTW STR31R TO STR32R AT LOWER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00008) REF AE WO # 2025-414/1 NR # 2025-717299 PERFORMED DETAIL VISUAL INSPECTION ON AREA AND NOT FOUND DENT ONLY
- [SDR YENA2026021100191](https://openairdocs.org/sdr/YENA2026021100191.md): Skin · dented · Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN DOOR 812 AT LOWER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00009) REF AEROMAN WO # 2025=414/1 NR # 2025-717302 EVALUATED DENT ON EXTERNAL SKIN DOOR 812 AT LOWER FUSELAGE AND FOUND WITHIN LIMITS I.A.W A320 SR
- [SDR YENA2026021100190](https://openairdocs.org/sdr/YENA2026021100190.md): Skin · bulged · Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: BULGE EXTERNAL SKIN LOCATED FR24 TO FR25 BTW STR19L TO STR20L ON UPPER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00010) REF AEROMAN WO # 2025-414/1 NR # 2025-717282 EVALUATED BULGE EXTERNAL SKIN LOCATED FR24 TO FR25 BTW STR19L
- [SDR YENA2026021100189](https://openairdocs.org/sdr/YENA2026021100189.md): Skin · dented · Feb 8, 2026 · N613JB · Airbus A320232 · Service Doors
  > DURING HEAVY MAINTENANCE: DENT SKIN LOCATED LOWER AREA DOOR R2 AT LOWER FUSELAGE; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00011) REF AEROMAN WO # 2025-414/1 NR# 2025-717349 EVALUATED DENTS LOCATED LOWER SKIN AREA DOOR R2 AT LOWER FUSELAGE AND FOUND WITHIN LIMIT
- [SDR YENA2026021100188](https://openairdocs.org/sdr/YENA2026021100188.md): Frame · cracked · Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK NDICATION FOUND ON FRAME 16 RH SIDE IN UPPER DOUBLE JOGGLE AREA AT OPEN FASTENER HOLE 8, CRACK DIRECTION AT 3 OCLOCK LOOKING INBOARD, D=0.120INCH, CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00; (RESOLVED ON W/O:
- [SDR YENA2026021100187](https://openairdocs.org/sdr/YENA2026021100187.md): Frame · cracked · Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16 RH SIDE IN UPPER DOUBLE JOGGLE AREA AT OPEN FASTENER HOLE A, CRACK DIRECTION AT 3 OCLOCK LOOKING INBOARD, D=0.110 INCH, CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00; (RESOLVED ON W/
- [SDR YENA2026021100186](https://openairdocs.org/sdr/YENA2026021100186.md): Frame · cracked · Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 20 RH SIDE IN UPPER DOUBLE JOGGLE AREA AT OPEN FASTENER HOLE 6, CRACK DIRECTION AT 11 O CLOCK LOOKING INBOARD, D=0.125 INCH, CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00; (RESOLVED ON
- [SDR YENA2026021100185](https://openairdocs.org/sdr/YENA2026021100185.md): Door Frame · cracked · Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 LH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 6 OCLOCK, CRACK DEPTH IS 0.105 INCH, AT AFT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1425349 TASKCARD: NR-00038
- [SDR YENA2026021100184](https://openairdocs.org/sdr/YENA2026021100184.md): Door Frame · cracked · Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 5 POSITION, CRACK DIRECTION IS 7 OCLOCK, CRACK DEPTH IS 0.090 INCH, AT AFT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1425349 TASKCARD: NR-00039
- [SDR YENA2026021100183](https://openairdocs.org/sdr/YENA2026021100183.md): Skin · deformed · Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: DEFORMATION LOC. FR70 TO FR76 BTW STR31R TO 31L JACKING POINT AREA REAR FUSELAGE; REF AEROMAN N/R 2025-717439, PERFORMED PERMANENT REPAIR LOC. FR70 TO FR76 BTW STR31R TO 31L JACKING POINT AREA REAR FUSELAGE, THIS REPAIR IS CATEGORY A,
- [SDR YENA2026021100182](https://openairdocs.org/sdr/YENA2026021100182.md): Door Frame · cracked · Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE UPPER INBO ARD AT DOOR STOP FITTING 3 POSITION, CRACK DIRECTIONS ARE 1 AND 6 OCLOCK, CRACK DEPTH IS 0.095 INCH, AT AFT GALLEY AREA (2 EA); (RESOLVED ON W/O: 1425349 TASKCARD:
- [SDR YENA2026021100181](https://openairdocs.org/sdr/YENA2026021100181.md): Door Frame · cracked · Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE UPPER INBO ARD AT DOOR STOP FITTING 3 POSITION, CRACK DIRECTIONS ARE 1 AND 6 OCLOCK, CRACK DEPTH IS 0.095 INCH, AREA 2 FOR PURPOSE OF TRACKING; (RESOLVED ON W/O: 1425349 TASKC
- [SDR YENA2026021100180](https://openairdocs.org/sdr/YENA2026021100180.md): Door Frame · cracked · Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE UPPER INBO ARD AT DOOR STOP FITTING 3 POSITION, CRACK DIRECTIONS ARE 1 AND 6 OCLOCK, CRACK DEPTH IS 0.095 INCH, AREA 3 FOR PURPOSE OF TRACKING; (RESOLVED ON W/O: 1425349 TASKC
- [SDR YENA2026021100179](https://openairdocs.org/sdr/YENA2026021100179.md): Frame · cracked · Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE AT AFT WEB FACE AND STGR 8 HORIZONTAL FLANGE RADIUS, CRACK LENGTH IS 0.095 INCH, AT AFT GALLEY AREA ( 1 EA); (RESOLVED ON W/O: 1425349 TASKCARD: NR-00045) REF AE WO # 2025-414/1 NR # 2025-717399 PE
- [SDR YENA2026021100178](https://openairdocs.org/sdr/YENA2026021100178.md): Frame · cracked · Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE AT AFT WEB FACE AND STGR 8 HORIZONTAL FLANGE RADIUS, CRACK LENGTH IS 0.095 INCH, TRANSVERSAL FLANGE ARE A FOR PURPOSE OF TRACKING; (RESOLVED ON W/O: 1425349 TASKCARD: NR-00046) REF AE WO # 2025-414
- [SDR YENA2026021100177](https://openairdocs.org/sdr/YENA2026021100177.md): Door Frame · cracked · Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTIONS ARE 12 AND 6 OCLOCK, CRACK DEPTH IS 0.115 INCH, AT AFT GALLEY AREA (2 EA); REF AEROMAN N/R 2025-717397, ACCOMP
- [SDR YENA2026021100176](https://openairdocs.org/sdr/YENA2026021100176.md): Window Frame · cracked · Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK FOUND ON UPPER RADIUS OF WINDSHIELD CENTER POST LOWER ATTACHMENT AREA RH SIDE. CRACK L= 0.109 INCH. CRACK DIRECTION 11 O CLOCK; REF AEROMAN N/R 2025-717306, ACCOMPLISHED THE PERMANENT REPAIR OF THE CRACKS ON THE WINDSHIELD FRAMI
- [SDR YENA2026021100175](https://openairdocs.org/sdr/YENA2026021100175.md): Window Frame · cracked · Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE TRAILING EDGE LOWER AREA OF SKINAT LEVEL RIB 15 ON RH WING; REF AE WO # 2025-414/1 NR # 2025-716959 ACCOMPLISHED PERMANENT REPAIR ON RH WING/TOP SKIN PANEL 2 / TEOH LWR SURFACE / RIB 15 I.A.W EA 57-0135-25(COVE
- [SDR YENA2026021100174](https://openairdocs.org/sdr/YENA2026021100174.md): Skin · corroded · Feb 8, 2026 · N613JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE TRAILING EDGE LOWER AREA OF SKINAT LEVEL RIB 15 ON RH WING; REF AE WO # 2025-414/1 NR # 2025-716959 ACCOMPLISHED PERMANENT REPAIR ON RH WING/TOP SKIN PANEL 2 / TEOH LWR SURFACE / RIB 15 I.A.W EA 57-0135-25(COVE
- [SDR YENA2026021100173](https://openairdocs.org/sdr/YENA2026021100173.md): Skin · corroded · Feb 8, 2026 · N613JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE AT LEVEL RIB 8 TO RIB 9 TRAILING EDGE ON RH WNG; REF AEROMAN WO 2025-414/1 NR # 2025-716950 ACCOMPLISHED REPAIR OF CORROSION DAMAGE AT RH WING/TOP SKIN PANEL 2 / TEOH LWR SURFACE / RIB7-RIB9 I.A.W EA 57-0135-2
- [SDR YENA2026021100172](https://openairdocs.org/sdr/YENA2026021100172.md): Skin · corroded · Feb 8, 2026 · N613JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE UPPER SKIN LOWER AREA BTW RIB8 TO RIB 9 ON RH WING; REF AEROMAN WO # 2025-414/1 NR # 2025-717170 PERFORMED PERMANENT REPAIR ON TRAILING EDGE UPPER SKIN LOWER AREA ON RIB 8 RH WING IAW EA # 57-0135-25 (COVER AND
- [SDR YENA2026021100171](https://openairdocs.org/sdr/YENA2026021100171.md): Skin · corroded · Feb 8, 2026 · N613JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION TE UPPER SKIN LOWER AREA SURFACE AT LEVEL RIB 7 ON RT WING; REF AEROMAN WO #2025-414/1 NR # 2025-717174, PERFORMED PERMANENT REPAIR ON TE UPPER SKIN LOWER AREA SURFACE AT LEVEL RIB 7 ON RT WING IAW EA 57-0135 -25 (COVER PART
- [SDR YENA2026021100170](https://openairdocs.org/sdr/YENA2026021100170.md): Door Frame · cracked · Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE/ REAR FUSELAGE/ FR68 RH DOOR STOP FITTING #1/ CRACK/ PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-0101-25 (COVER, PART 1+2) /2/ AIRBUS DOSSIER 81714674 /3/ AIRBUS RDAF 81714674/003/2025#A /4/ A320 SRM 53-41-12-300-011. DES
- [SDR YENA2026021100169](https://openairdocs.org/sdr/YENA2026021100169.md): Skin · corroded · Feb 8, 2026 · N613JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: RT WING TOP SKIN PANEL CORRODED /1/ - AIRBUS DOSSIER 81709907 /2/ - AIRBUS RDAF REF. & ISSUE.: 81709907/003/2025 ISSUE A /3/ - AIRBUS RI R572-44701 ISSUE B /4/ - AIRBUS RI R572-58616 ISSUE N /5/ - AIRBUS RI R572-58926 ISSUE E /6/ - A
- [SDR YENA2026021100168](https://openairdocs.org/sdr/YENA2026021100168.md): Window Frame · cracked · Feb 8, 2026 · N613JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE, WINDSHIELD FRAME CENTER POST, LOWER NODE AREA CRACKED. REFERENCE: EA 53-0097-25, SB A320-53-1331, RDAF 81709993/003/2025 A, MESSAGE 81709993/010, REPAIR INSTRUCTION R53113430, ISSUE G, REPAIR INSTRUCTION R53112919 ISSUE K, REP
- [SDR YENA2025032400301](https://openairdocs.org/sdr/YENA2025032400301.md): Thermostat · failed · Mar 21, 2025 · N613JB · Airbus A320232 · Engine Indicating System
  > FLT#2121, FLL-LAX. (AIRCRAFT DECLARED AN EMERGENCY).' ON CLIMB OUT 2 TIMES AIR ENG 1 BLEED ABNORMAL MSG CLEARED ITSELF 3RD TIME WE COMPLIED WITH QRH TAKEOFF WAS A TOGA BLEEDS OFF AND PSI WAS 22 / 215 C. ENG ONE #1. WHEN WE STARTED GETTING THE BLEED ABNORMAL M
- [SDR YENA2025032400300](https://openairdocs.org/sdr/YENA2025032400300.md): Hydraulic System · low · Mar 21, 2025 · N613JB · Airbus A320232 · Hydraulic System, Main
  > FLT#2121, FLL-LAX. (AIRCRAFT DECLARED AN EMERGENCY).' APPROX 3 HOURS INTO FLIGHT PERFORMING SYSTEMS CHECKS. THE HYD STATUS PAGE SHOWED AMBER LINE FROM GREEN SYSTEM RESERVOIR TO GREEN ENG PUMP AND RESERVOIR INDICATOR WAS AMBER 3000 GREEN; ACCOMPLISHED VISUAL I
- [SDR YENA2025031900274](https://openairdocs.org/sdr/YENA2025031900274.md): Pump · faulted · Mar 18, 2025 · N613JB · Airbus A320232 · Hydraulic Pump (Electric/Engine), Main
  > FLT#2096, CUN-FLL. (AIRCRAFT DECLARED AN EMERGENCY INTO FLL) 'HYD G RSVR LO LVL ECAM MSG. EMG 1 PUMP AND PTU OFF ACCORDING TO ECAM.' (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA2025021000140](https://openairdocs.org/sdr/YENA2025021000140.md): Unknown · odor · Feb 6, 2025 · N613JB · Airbus A320232 · Air Distribution System
  > FLT#667, HPN-PBI. 'OBVIOUS OIL FUMES ODOR IN FLT DECK AND FRONT OF A/C TURNED PACK 1 OFF. STILL BAD SEVERAL MINUTES LATER. OPEN
- [SDR YENA2025012200094](https://openairdocs.org/sdr/YENA2025012200094.md): Bleed Air Sys · odor · Jan 20, 2025 · N613JB · Airbus A320232 · APU Bleed Air System
  > FLT#743, JFK-AUA. 'DIRTY SOCK SMELL REPORTED BY FLIGHT ATTENDANT FROM MID TO AFT CABIN ( APU BLEED AIR SUPPLY SYSTEM); REF LP # 4219340, ITEM 2 OR WO # 1387703 TSI. THIS CLEARS THIS MDDR. MDDR CLEARED. MX-4 UPDATED. PLACARD RMVD. MCC NOTIFIED.'
- [SDR YENA2024101801371](https://openairdocs.org/sdr/YENA2024101801371.md): Filter · odor · Oct 14, 2024 · N613JB · Airbus A320232 · Air Distribution System
  > FLT#791, BOS-TPA.' ODOR SMELL IN CABIN AT ROW 3 & 4. APU BLEED ON; COMPLIED WITH INFO NOTICE 2017-T015 SECTION A. ISOLATED FAULT TO TYPE 10 AMBIENT AIR ODOR PER TSM 05-50-00-810-085-B/ TSM 05-50-00-810-085-D. A/C IS OK FOR SERVICE. REMOVED & REPLACED RECIRC.
- [SDR YENA2024020800250](https://openairdocs.org/sdr/YENA2024020800250.md): Engine · stalled · Feb 8, 2024 · N613JB · Airbus A320232 · Engine (Turbine/Turboprop)
  > FLT#1510, PAP-FLL. (AIRCRAFT DECLARED AN EMERGENCY AND DIVERTED TO SDQ). 'ENG 2 FAIL/STALL ON CLIMB OUT.' (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA2023082100962](https://openairdocs.org/sdr/YENA2023082100962.md): Safety Valve · failed · Aug 19, 2023 · N613JB · Airbus A320232 · Hydraulic Power System
  > FLT#2276, MCO-PVD. (AIRCRAFT PERFORMED AN AIR TURN BACK) ' GREEN HYDRAULIC FAILURE CLIMBING THRU 4,000 MANUAL GEAR EXTENSION NORMAL LANDING; FOUND L/G SAFETY VALVE DETACHED FROM MANIFOLD AND LEAKING. REF L/P 3755398, ITEMS 1 (INSTALLED NEW L/G SAFETY VALVE (49
- [SDR YENA2023011200034](https://openairdocs.org/sdr/YENA2023011200034.md): Door · cracked · Jan 10, 2023 · N613JB · Airbus A320232 · Emergency Exits
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 833 (FWD LH SIDE), SEGMENT 1, IN PASSENGER CABIN; REF WO 2022 287/1 NR 2002-679963. PERFORMED MODIFICATION ON EMERGENCY EXIT DOOR 833 IAW EC A320-52-1144 TASK CARD A320-52-1144-01 DOORS / EMERG
- [SDR YENA2023011200033](https://openairdocs.org/sdr/YENA2023011200033.md): Door · cracked · Jan 10, 2023 · N613JB · Airbus A320232 · Emergency Exits
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 843 (FWD RH SIDE), SEGMENT 1, IN PASSENGER CABIN; REF WO 2022 287/1 NR 2022 - 679964. PERFORMED MODIFICATION ON EMERGENCY EXIT DOOR 843 IAW EC A320-52 1144 TASK CARD A320-52-1144-02 DOORS / EMER
- [SDR YENA2023011200032](https://openairdocs.org/sdr/YENA2023011200032.md): Door · cracked · Jan 10, 2023 · N613JB · Airbus A320232 · Emergency Exits
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 834 (AFT LH SIDE), SEGMENT 1, IN PASSENGER CABIN; REF WO 2022-287/1 NR2022-679965. PERFORMED MODIFICATION ON EMERGENCY EXIT DOOR 834 IAW EC A320-52-1144 TASK CARD A320-52-1144-03 DOORS / EMERG
- [SDR YENA2023011200031](https://openairdocs.org/sdr/YENA2023011200031.md): Door · cracked · Jan 10, 2023 · N613JB · Airbus A320232 · Emergency Exits
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 844 (AFT RH SIDE), SEGMENT 1, IN PASSENGER CABIN; REF WO 2022-287/1 NR2022-679966 PERFORMED MODIFICATION ON EMERGENCY EXIT DOOR 844 IAW EC A320-52-1144 TASK CARD A320-52-1144-04 DOORS / EMERGENC
- [SDR YENA2022080300743](https://openairdocs.org/sdr/YENA2022080300743.md): Drive Unit · failed · Aug 1, 2022 · N613JB · Airbus A320232 · Inertial Guidance System
  > FLT#2603, EWR- TPA. (AIRCRAFT PERFORMED AN AIR TURN BACK TO EWR) WEATHER RADAR FAILURE ON CLIMB OUT; REMOVED AND REPLACED WX RADAR TRANSCEIVER IAW AMM 34-41-33. DUE TO BITE TEST FAILURE. REF LOG PAGE 3476359, ITEM 1 (REMOVED AND REPLACED WX RADAR ANTENNA & DRI
- [SDR YENA2022080300742](https://openairdocs.org/sdr/YENA2022080300742.md): Transceiver · failed · Aug 1, 2022 · N613JB · Airbus A320232 · Inertial Guidance System
  > FLT#2603, EWR- TPA. (AIRCRAFT PERFORMED AN AIR TURN BACK TO EWR) WEATHER RADAR FAILURE ON CLIMB OUT; REMOVED AND REPLACED WX RADAR TRANSCEIVER IAW AMM 34-41-33. DUE TO BITE TEST FAILURE. REF LOG PAGE 3476359, ITEM 1 (REMOVED AND REPLACED WX RADAR ANTENNA & DRI
- [SDR YENA2022071800673](https://openairdocs.org/sdr/YENA2022071800673.md): Bleed Air Sys · odor · Jul 16, 2022 · N613JB · Airbus A320232 · APU Bleed Air System
  > FLT#153, DEN-LGA. ' FOUL ODOR WITH APU BLEED AND PACKS ON, DISSIPATED DURING CLIMB AFTER 5-7 MINS, CABIN ODOR FORM COMPLETED( APU BLEED AIR SUPPLY SYSTEM).' (SUPPLEMENTAL TO FOLLOW)
- [SDR YENA2022071800672](https://openairdocs.org/sdr/YENA2022071800672.md): Ecs · odor · Jul 16, 2022 · N613JB · Airbus A320232 · Air Conditioning System
  > FLT#571, LGA-FLL. ' DIRTY SOCK SMELL IN DESCENT THE SMELL DISSIPATED WITH PACK 1 OFF; PREFORMED LEVEL A DECONTAMINATION OF THE ENVIRONMENTAL CONTROL SYSTEM IAW AMM 21-00-00-615-802-A, USING ENG BLEED. NO ODOR PRESENT UPON COMPLETION.'
- [SDR YENA2022022800102](https://openairdocs.org/sdr/YENA2022022800102.md): Bleed Valve · failed · Feb 25, 2022 · N613JB · Airbus A320232 · Engine Pressure Ratio (EPR)
  > FLT # 1691, JFK-LIR(DIVERTED TO MCO). ENGINE 1 STALL AT CRUISE 34000, LOUD SHAKE NO ECAM PRESENT DIVERT TO MCO; PER TSM 71-00-00-810-808-A, ACCOMPLISHED HPC BORESCOPE OF #1 ENG HPC STG'S 3,6 AND 7 IAW AMM 72-00-00-200-016-B01 AND BORESCOPE INSPECTION OF HPC
- [SDR YENA2021100400641](https://openairdocs.org/sdr/YENA2021100400641.md): Battery · no test · Oct 2, 2021 · N613JB · Airbus A320232 · Emergency Lighting
  > FLT 576, MSY-JFK. BATTERY CAPACITANCE TEST REQ; R/R EPSU BATTERY IAW AMM 33-51-00 + T/C A320 - 33-51-00-710.
- [SDR YENA2021100400640](https://openairdocs.org/sdr/YENA2021100400640.md): Battery · no test · Oct 2, 2021 · N613JB · Airbus A320232 · Emergency Lighting
  > FLT 576, MSY-JFK. BATTERY CAPACITANCE TEST REQ; R/R EPSU BATTERY IAW AMM 33-51-00 + T/C A320 - 33-51-00-710.
- [SDR YENA2021100400639](https://openairdocs.org/sdr/YENA2021100400639.md): Battery · no test · Oct 2, 2021 · N613JB · Airbus A320232 · Emergency Lighting
  > FLT 576, MSY-JFK. BATTERY CAPACITY TEST REQ; R/R EPSU BATTERY IAW AMM 33-51-00 + TC A320 - 33-51-00-710.
- [SDR YENA2021100400638](https://openairdocs.org/sdr/YENA2021100400638.md): Battery · no test · Oct 2, 2021 · N613JB · Airbus A320232 · Emergency Lighting
  > FLT 576, MSY-JFK. BATTERY CAPACITY TEST REQ; R/R EPSU BATTERY IAW AMM 33-51-00 + TC A320 - 33-51-00-710.

Next page: https://openairdocs.org/aircraft/N613JB/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 = 'N613JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N613JB/reports

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