# Service difficulty reports: N608JB

A list on [N608JB](https://openairdocs.org/aircraft/N608JB.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 · 61 reports

- [SDR YENA2026032500339](https://openairdocs.org/sdr/YENA2026032500339.md): Unknown · odor · Mar 23, 2026 · N608JB · Airbus A320232 · Air Distribution System
  > FLT # 525 PVD-SJU." INFLIGHT REPORTED FUMES EVENT ON DESCENT THROUGH 10,000'.; ACCOMPLISHED INFO NOTICE 2017-T015M, STEPS 1 AND 2 IDENTIFIED AS TYPE 9 ELECTRICAL. C/W TYPE 9 INSPECTION IAW AMM SUBTASK 05-50-00-810-085 NO TRIPPED C/B AND ELECTRICAL SMELL NOTED.
- [SDR YENA2025092200954](https://openairdocs.org/sdr/YENA2025092200954.md): Unknown · odor · Sep 21, 2025 · N608JB · Airbus A320232 · Air Distribution System
  > FLT#1405, MCO-SDQ. "DESCENTING THROUGH 14000FT STRONG SMELL ( ELECTRICAL/ OIL SMELL) ISOLATED SOURCE TO PACK 1 ON THE GROUND..
- [SDR YENA2025009000901](https://openairdocs.org/sdr/YENA2025009000901.md): Line · leaking · Aug 30, 2025 · N608JB · Airbus A320232 · APU Oil System
  > FLT#1952, MCO-BOS. "FUMES EVENT ON ARRIVAL AT 10,000 FT MUSTY DIRTY SCCK SMELL IN FLIGHT DECK AND FWD CABIN SMELL WENT AWAY WHEN #1 PACK TURNED OFF VIA PROCEDURE; INSPECTED A/C FOR OIL LEAK SIGNS. FOUND APU COOLING FAN TRANSFER TUBE LEAKING. R/R APU TRANSFER T
- [SDR YENA2025082800881](https://openairdocs.org/sdr/YENA2025082800881.md): Unknown · odor · Aug 27, 2025 · N608JB · Airbus A320232 · Air Distribution System
  > FLT#699, LGA-MCO. #3&4 INFLIHT CREW REPORTS A VERY STRONG CHEMICAL SMELL IN AFT GALLEY PRODUCING A METALLIC TASTE IN THE MOUTH, SORE THROAT AND HEADACHE OCCURED ON DESCENT FROM 4500 THROUGH ENGINE SHUTDOWN AT GATE. #3 SEEKING MEDICAL ATTN. ACCOMPLISHED TASK
- [SDR YENA2025081300834](https://openairdocs.org/sdr/YENA2025081300834.md): Filter · odor · Aug 12, 2025 · N608JB · Airbus A320232 · Air Distribution System
  > FLT#562, SJU-BOS. LEVEL 2 ODOR EVENT. DISSIPATED WITH PACK 1 TURNED OFF VIA ODOR CHECKLIST. DIRTY SOCK/ BURNT CRAYON; REMOVED AND REPLACED LH OZONE FILTER IAW AMM 21-51-41, AND RECIRCULATING FILTERS IAW AMM 21-21-41. INSPECTED APU COMPARTMENT NO LEAK NOTED. C
- [SDR YENA2025081200829](https://openairdocs.org/sdr/YENA2025081200829.md): Fitting · not reported · Aug 9, 2025 · N608JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: REPLACE THE CONTINUITY FITTINGS IAW EA #53-0053-25 PART# 3 AND 4; REF AEROMAN WO# 2025-190/1 WCC# 2025-416752 FOR WORK PERFORMED. REMOVED AND REPLACED CONTINUITY FITTINGS I.A.W. EA# 53-0035-25,(COVER PLUS REV 0), PART #3 AND PART #
- [SDR YENA2025081200828](https://openairdocs.org/sdr/YENA2025081200828.md): Window Frame · cracked · Aug 9, 2025 · N608JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CENTER LOWER POST ON UPPER TENSION BOLT AREA ON LH SIDE CRACK LENGTH = 0.250 INCH APPROX; AEROMAN WO#2025-190/1 WCC# 2025-416536 FOR WORK PERFORMED; PERFORMED PERMANENT REPAIR ON FUSELAGE WINDSHIEL
- [SDR YENA2025081200827](https://openairdocs.org/sdr/YENA2025081200827.md): Window Frame · cracked · Aug 9, 2025 · N608JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: WINDSHIELD FRAME CENTER POST LOWER NODE AREA CRACKED. POST REPAIR INSPECTIONS OF THE MIRROR FITTINGS (TBD) AEROMAN EA 53-0371-22 REV. 0. AIRBUS RDAF 81098121/004/2022#A. AIRBUS DOSSIER 81098121. AIRBUS TD/81039011/009/2022#A.
- [SDR YENA2025030700245](https://openairdocs.org/sdr/YENA2025030700245.md): Unknown · odor · Mar 6, 2025 · N608JB · Airbus A320232 · Air Distribution System
  > FLT#613, HPN-FLL. DURING DESCENT ODOR OBSERVED IN FLIGHT DECK AND CABIN DIRTY SOCK/ HOT PLASTIC MX-270 FILLED OUT; COMPLIED WITH INFO. NOTICE 2017-T015, SECTION B2, PERFORMED DECONTAMINATION LEVEL A, PACK BURN IAW AMM 21-00-00-615-802A, NO ODOR NOTED AFTER
- [SDR YENA2025012900116](https://openairdocs.org/sdr/YENA2025012900116.md): Unknown · odor · Jan 26, 2025 · N608JB · Airbus A320232 · Air Distribution System
  > FLT#1145, RIC-FLL. 'FA REPORTS BURNING SMELL DURING LAST 10 MINUTES OF FLIGHT IN AFT GALLEY; VISUAL CHECK OF AFT GALLEY AND BOTH LAV'S, NO EVIDENCE OF BURNING. NO SMELL NOTED AT THIS TIME IAW TSM 05-50-00.'
- [SDR YENA2025012200093](https://openairdocs.org/sdr/YENA2025012200093.md): Actuator · faulted · Jan 20, 2025 · N608JB · Airbus A320232 · Nose/Tail Landing Gear
  > FLT#704, RSW-BDL. (AIRCRAFT DIVERTED TO MCO). 'NOSE GEAR DID NOT RETRACT PROPERLY AFTER TAKEOFF. NOSE GEAR UNLOCKED ECAM PERFORMED GEAR EXTENDED NORMAL LANDING; INSTALLED NLG UNLOCKING ACTUATOR PER A320 AMM 32-31-23 OPS CHECK AND FUNCTIONAL CHECK OF FREE FALL
- [SDR YENA2025010300004](https://openairdocs.org/sdr/YENA2025010300004.md): Unknown · odor · Dec 30, 2024 · N608JB · Airbus A320232 · Air Distribution System
  > FLT#1098, MCO-LGA. 'FA'S REPORT CLIMBING OUT OF MCO DIRTY SOCK SMELL. THE SMELL DISSIPATED + RETURN HEAVY AGAIN ON DESCENT INTO LGA. THE SMELL WAS NOTICED FROM EXIT ROW BACK. WEATHER CONDITIONS IN MCO WAS HEAVY RAIN; ACCOMPLISHED INFO NOTICE 2017-T015K SECTION
- [SDR YENA2024052900795](https://openairdocs.org/sdr/YENA2024052900795.md): Compressor · stalled · May 27, 2024 · N608JB · Airbus A320232 · Turbine Engine Compressor Section
  > FLT#1537, JFK-STI. (AIRCRAFT DIVERTED TO BOS AND DECLARED AN EMERGENCY) ' ON CLIMB THROUGH 14000 FT ABOUT 6 LARGE THUMPS NOISES, VIBRATION, YAWING FOLLOWED BY COMPRESSOR VANE FAULT ENG 2 EGT OVERTEMP AND N2 AMBER XX.' OPEN
- [SDR YENA2023061600668](https://openairdocs.org/sdr/YENA2023061600668.md): Unknown · unknown · Jun 14, 2023 · N608JB · Airbus A320232 · Standard Practices/Structures
  > FLT#1936, STI-JFK. 'IN DESCENT AND APPROACH BELOW 10000, WE NOTICED A MUSTY SMELL LIKE CRAYONS. IN THE FLIGHT DECK. ODOR WAS ONLY APPARENT IN THE FLIGHT DECK. PER FCOM VOL1, WE SHUT THE CROSSBREED VALVE AND TURNED PACL 1 OFF. THE ODOR DISSIPATED QUICKLY. THE S
- [SDR YENA2023011700042](https://openairdocs.org/sdr/YENA2023011700042.md): Unknown · fumes · Jan 16, 2023 · N608JB · Airbus A320232 · Air Distribution System
  > FLT#22, MBJ-MCO.' HAD A LEVEL 2 FUMES IN CLIMB OUT. TURNED OFF PACK 2 AND THE FUMES SEEMED TO DISSIPATE; INTEROGATED PILOT SURVEY. ALL POINTS TOWARDS DEICE FLUID CONTAMINATION INSPECTED #2 PACK AREA FOUND NO EVIDENCE OF GLYCOL. FOUND DEICE RESIDUE ON RH SIDE O
- [SDR YENA2022090600876](https://openairdocs.org/sdr/YENA2022090600876.md): None · none · Sep 1, 2022 · N608JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA CONTINUITY FITTING, LH SIDE, CRACK LENGTH IS 0.200 INCHES APPROX IN COCKPIT (1 EA); REF AEROMAN N/R 2022-408601 WO 2022-178/1 REMOVED AND REPLACED CONTINUIT
- [SDR YENA2022090600875](https://openairdocs.org/sdr/YENA2022090600875.md): None · none · Sep 1, 2022 · N608JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA CONTINUITY FITTING, RH SIDE, CRACK LENGTH IS 0.200 INCHES APPROX IN COCKPIT (1 EA); REF AEROMAN N/R 2022-408602 WO 2022-178/1 REMOVED AND REPLACED CONTINUI
- [SDR YENA2022090600874](https://openairdocs.org/sdr/YENA2022090600874.md): None · none · Sep 1, 2022 · N608JB · Airbus A320232 · Doors
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FRAME SEGMENT 1 AT OVERWING EMERGENCY EXIT DOOR (AFT LH EEH DOOR 834) CRACK L=0.250 INCH APPROX; ACCOMPLISHED EC# A320-52-1144 ON EMERGENCY EXIT DOOR 834 FOR REPLACEMENT OF FRAME REINFORCE DOOR STRUCTURE REF AEROMAN N
- [SDR YENA2022090600873](https://openairdocs.org/sdr/YENA2022090600873.md): None · none · Sep 1, 2022 · N608JB · Airbus A320232 · Doors
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FRAME SEGMENT 1 AT THE OVERWING EMERGENCY EXIT DOOR (FWD LH EEH DOOR 833) CRACK L=0.196 INCH APPROX; REF AEROMAN N/R 2022-408533 WO 2022-178/1 ACCOMPLISHED EC# A320-52-1144 ON EMERGENCY EXIT DOOR 833 FOR REPLACEMENT O
- [SDR YENA2022090600872](https://openairdocs.org/sdr/YENA2022090600872.md): None · none · Sep 1, 2022 · N608JB · Airbus A320232 · Doors
  > DURING HEAVY MAINTENANCE: CRACK INDICATIONS WERE FRAME SEGMENTS 1 AT THE OVERWING EMERGENCY EXIT DOOR (FWD RH EEH DOOR 843) CRACK L=0.194 INCH APPROX; REF AEROMAN N/R 2022-408535 WO 2022-178/1 ACCOMPLISHED EC# A320-52-1144 ON EMERGENCY EXIT DOOR 843 FOR REPLAC
- [SDR YENA2022090600871](https://openairdocs.org/sdr/YENA2022090600871.md): None · none · Sep 1, 2022 · N608JB · Airbus A320232 · Doors
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FRAME SEGMENT 1 AT OVERWING EMERGENCY EXIT DOOR (AFT RH EEH DOOR 844) CRACK L=0. 197 INCH APPROX; REF AEROMAN N/R 2022-408536 WO 2022-178/1 ACCOMPLISHED EC# A320-52-1144 ON EMERGENCY EXIT DOOR 844 FOR REPLACEMENT OF
- [SDR YENA2022062900638](https://openairdocs.org/sdr/YENA2022062900638.md): None · none · Jun 27, 2022 · N608JB · Airbus A320232 · Air Conditioning System
  > FLT#173, FLL-PUJ. (AIRCRAFT PERFORMED AN AIR TURN BACK TO FLL) 'AT 8500 FEET AVIONICS DOOR SHOWED UNSAFELY. WE JUST HAD WORK ACCOMPLISHED ON AVIONICS. OUT OF ABUNDANCE OF CAUTION, WE RETURNED TO FLL ( ECAM DOOR PAGE INDICATIONS 4) AVIONICS COMPARTMENT ACCESS D
- [SDR YENA2021110300742](https://openairdocs.org/sdr/YENA2021110300742.md): Battery · no test · Nov 3, 2021 · N608JB · Airbus A320232 · Emergency Lighting
  > FLT 2424, MCO-DCA. BATTERY ENERGENCY LIGHT 12WL FAILED CAPACITY TEST; REMOVED AND REPLACED EMERGENCY LT BATTERY AT RH CENTER CABIN IAW AMM 33-51-38, OPS CHECK NORMAL
- [SDR YENA2021070200416](https://openairdocs.org/sdr/YENA2021070200416.md): Battery · inoperative · Jun 29, 2021 · N608JB · Airbus A320232 · Emergency Equipment
  > FLT 959, BDL-FLL. FO'S EMERGENCY FLASHLIGHT NOT CHARGING; REPLACED FO'S EMERGENCY FLASHLIGHT BATTERY AS REQUIRED, OPS NORMAL.
- [SDR YENA2020020430141](https://openairdocs.org/sdr/YENA2020020430141.md): Slide · no test · Jan 31, 2020 · N608JB · Airbus A320232 · Escape Slide
  > DURING HEAVY MAINTENANCE, PER AEROMAN W/O 2019-341/1 WCC 2019-398297, THE SLIDE RAFT ON DOOR 841 DID NOT PASS OPERATIONAL TEST DURING INSTALLATION PROCEDURE. R1 SLIDE MUST BE REPLACED; PER AEROMAN W/O 2019-341/1, WCC 2019-398297, REMOVED AND REPLACED ESCAPE SL
- [SDR YENA2020020430139](https://openairdocs.org/sdr/YENA2020020430139.md): Skin · corroded · Jan 31, 2020 · N608JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, WV UPGRADE RH WING CORROSION TOP SKIN LOWER SURFACE TE RIB 13 EC A 17-790-19; (REF AEROMAN NR 2019-398193 WO 2019 341/1 JB EC A20-100-01) FOR DETAILED INFORMATION ON WORK PERFORMED. THIS REPAIR IS MAJOR AND CAT B.
- [SDR YENA2020020430138](https://openairdocs.org/sdr/YENA2020020430138.md): Slide · mismanufactured · Jan 31, 2020 · N608JB · Airbus A320232 · Escape Slide
  > DURING HEAVY MAINTENANCE, IMPROPERLY PACKED SLIDE DOOR 831; (REF AEROMAN NR 2019 398007 WO 2019 341/1) R & R SERVICEABLE ESCAPE SLIDE DOOR 831 IAW AMM 25-62-44-900-007-A
- [SDR YENA2020020430137](https://openairdocs.org/sdr/YENA2020020430137.md): Dampener · corroded · Jan 31, 2020 · N608JB · Airbus A320232 · Passenger/Crew Doors
  > DURING HEAVY MAINTENANCE, CORROSION CREW DOOR 831 DOOR DAMPNER; (REF AEROMAN NR 2019-398006 WO 2019 341/1) R & R DOOR DAMPNER & EMERGENCY OPERATION CYLINDER DOOR 831 IAW 52-11-14-400-001B OPS OK
- [SDR YENA2020020430136](https://openairdocs.org/sdr/YENA2020020430136.md): Floor Support · corroded · Jan 31, 2020 · N608JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION FLOOR BEAM +N Y 1162 FR 68-FR69 LH SIDE AFT GALLEY; (REF AEROMAN NR 2019-398173 WO 2019 341/1) R & R FLOOR BEAM Y 1162.5 BETWEEN FR 68-69 LH GALLEY IAW SRM A320 51-72-11
- [SDR YENA2020020430135](https://openairdocs.org/sdr/YENA2020020430135.md): Floor Support · corroded · Jan 31, 2020 · N608JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION FLOOR BEAM -Y1292 FR 66-68 RH SIDE AFT GALLEY; (REF AEROMAN NR 2019-398171 WO 2019 341/1) R & R FLOOR BEAM -Y1292 FR66-68 RH SIDE AFT GALLEY IAW SRM 51-72-11
- [SDR YENA2020020430134](https://openairdocs.org/sdr/YENA2020020430134.md): Floor Support · corroded · Jan 31, 2020 · N608JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION FLOOR BEAM - Y 1292 LOCATED FR 66-FR68 RH SIDE AT AFT GALLEY AREA; REF AEROMAN NR 2019 398171 WO 2019 341/1 R& R FLOOR BEAM -Y1292 LOCATED FR 66-FR 68 & FASTENERS RH SIDE AT AFT GALLEY AREA IAW SRM A320-51-72-11
- [SDR YENA2020020430133](https://openairdocs.org/sdr/YENA2020020430133.md): Floor Support · corroded · Jan 31, 2020 · N608JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION FLOOR BEAM -Y1292 FR 66-68 RH SIDE AFT GALLEY; REF AEROMAN NR 2019-398171 WO 2019 341/1 R & R FLOOR BEAM -Y1292 FR66-68 RH SIDE AFT GALLEY IAW SRM 51-72-11
- [SDR YENA2020020430132](https://openairdocs.org/sdr/YENA2020020430132.md): Floor Support · corroded · Jan 31, 2020 · N608JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION FLOOR BEAM -Y1162.5 LOCATED FR 68-FR69 RH SIDE AT AFT GALLEY AREA; REF AEROMAN NR 2019 398172 WO 2019 341/1 R & R FLOOR BEAM -Y1162.5 LOCATED FR68-FR69 RH SIDE AT AFT GALLEY AREA IAW SRM 51-72-11
- [SDR YENA2020020431131](https://openairdocs.org/sdr/YENA2020020431131.md): Floor Support · corroded · Jan 31, 2020 · N608JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION FLOOR BEAM + Y1162.5 LOCATED FR 68-69 LH SIDE AFT GALLEY; (REF AEROMAN NR 2019 398173 WO 2019 341/1) R & R NEW FLOOR BEAM Y1162.5 SPLICE 4 EA & FASTNERS LOC BTW FR 68 FR 69 LH GALLEY ARREA IAW SRM A320-51-72-11
- [SDR YENA2018102940706](https://openairdocs.org/sdr/YENA2018102940706.md): Light · malfunctioned · Oct 24, 2018 · N608JB · Airbus A320232 · Emergency Lighting
  > FLT 993, BOS-DEN. UPON PREFLIGHT EXIT ROW LIGHT 10DEF REMAINS ON - END; RESET AND OPS CHECK OF EMER LIGHT SYS OK IAW AMM 33-50-00.
- [SDR YENA201804230189](https://openairdocs.org/sdr/YENA201804230189.md): Slide · not reported · Apr 23, 2018 · N608JB · Airbus A320232 · Escape Slide
  > DURING HEAVY MAINTENANCE, L1 DOOR SLIDE PRESSURE; REMOVED AND REPLACED L1 DOOR SLIDE IAW A320-AMM 25-62-44-000-012-A & 25-62-44-400-007-A.
- [SDR YENA2018042500188](https://openairdocs.org/sdr/YENA2018042500188.md): Epsu · no test · Apr 23, 2018 · N608JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, THE LEFT EPSU FAILED SELF TEST. REMOVED AND REPLACED EPSU IAW AMM 33-51-36-000-001, & 33-51-36-420-050-A. OPS CHECKED GOOD IAW AMM 33-51-38-740-050-B.
- [SDR YENA201710220854](https://openairdocs.org/sdr/YENA201710220854.md): Landing Gear · malfunctioned · Oct 22, 2017 · N608JB · Airbus A320232 · Landing Gear Retraction/Extension System
  > LANDING GEAR LGCIU 2 FAULT ECAM DURING DESCENT. FOLLOWED QRH FOR BOTH LGCIU’S AT FAULT AND PERFORMED THE LG GRAVITY EXTENSION. UNDER THIS CONDITION THE AIRCRAFT HAD NO NOSE WHEEL STEERING AND WAS TOWED OFF THE TAXI WAY AFTER LANDING. THE CABIN WAS NOT PREPPED
- [SDR YENA201709020734](https://openairdocs.org/sdr/YENA201709020734.md): Unknown · odor · Sep 2, 2017 · N608JB · Airbus A320232 · Air Distribution System
  > DURING FINAL APPROACH, CAPTAIN AND FIRST OFFICER EXPERIENCED A SLIGHT BURNING ODOR FROM APPARENT AIR CONTAMINATION; RAN ENVIRONMENTAL SYSTEM ISOLATED PACKS NO ODOR PRESENT. COMPLIED WITH INFORMATION NOTICE 2017-T015B SECTION A. AIRCRAFT IS OK FOR SERVICE.
- [SDR YENA20160815745](https://openairdocs.org/sdr/YENA20160815745.md): Floorbeam · corroded · Aug 15, 2016 · N608JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING ROUTINE MAINTENANCE, CORROSION WAS FOUND ON FLOORBEAM -Y1732 AT FRAME 66. REMOVED AND REPLACED THE FLOORBEAM.
- [SDR YENA20160815744](https://openairdocs.org/sdr/YENA20160815744.md): Door Sill · corroded · Aug 15, 2016 · N608JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS FOUND ON L2 DOOR MID SHAPE SILL AT FRAME 67. REMOVED AND REPLACED THE SILL.
- [SDR YENA20160815743](https://openairdocs.org/sdr/YENA20160815743.md): Floorbeam · corroded · Aug 15, 2016 · N608JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING ROUTINE MAINTENANCE, CORROSION WAS FOUND ON FLOORBEAM Y 1292 AT FRAME 68. REMOVED AND REPLACED THE FLOORBEAM.
- [SDR YENA20160815742](https://openairdocs.org/sdr/YENA20160815742.md): Floorbeam · corroded · Aug 15, 2016 · N608JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING ROUTINE MAINTENANCE, CORROSION WAS FOUND ON THE FLOORBEAM - Y765, DIRECTLY ABOVE FRAME 68. REMOVED AND REPLACED FLOORBEAM.
- [SDR YENA20160815741](https://openairdocs.org/sdr/YENA20160815741.md): Door Sill · corroded · Aug 15, 2016 · N608JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS FOUND ON L2 PAX DOOR CUT OUT DOOR SILL GIRT BAR FITTING, FRAME 68. REMOVED AND REPLACED SILL.
- [SDR YENA20160815740](https://openairdocs.org/sdr/YENA20160815740.md): Floorbeam · corroded · Aug 15, 2016 · N608JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING ROUTINE MAINTENANCE, CORROSION WAS FOUND ON THE FLOORBEAM Y1292 AT FRAME 67. REMOVED AND REPLACED THE FLOORBEAM.
- [SDR YENA20160815739](https://openairdocs.org/sdr/YENA20160815739.md): Floorbeam · corroded · Aug 15, 2016 · N608JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING ROUTINE MAINTENANCE, CORROSION WAS FOUND ON THE FLOORBEAM FRAME 20, Y1292. REMOVED AND REPLACED THE FLOORBEAM.
- [SDR YENA20160815738](https://openairdocs.org/sdr/YENA20160815738.md): Dummy Rail · corroded · Aug 15, 2016 · N608JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE MAINTENANCE, CORROSION WAS FOUND ON DUMMY RAIL AT NUT PLATE FRAME 16 -Y254. REMOVED AND REPLACED THE DUMMY RAIL.
- [SDR YENA20160815737](https://openairdocs.org/sdr/YENA20160815737.md): Floorbeam · corroded · Aug 15, 2016 · N608JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING ROUTINE MAINTENANCE, CORROSION WAS FOUND ON FLOORBEAM -Y765 AT FRAME 66. REMOVED AND REPLACED FLOORBEAM.
- [SDR YENA20160815736](https://openairdocs.org/sdr/YENA20160815736.md): Floor Support · corroded · Aug 15, 2016 · N608JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS FOUND ON FLOOR SUPPORT -Y1292, 5 INCHES AFT OF FRAME 68. REMOVED AND REPLACED THE FLOOR SUPPORT.
- [SDR YENA20160815735](https://openairdocs.org/sdr/YENA20160815735.md): Floor Support · corroded · Aug 15, 2016 · N608JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS FOUND ON FLOOR SUPPORT -Y1292, 10 INCHES AFT OF FRAME 66. REMOVED AND REPLACED THE FLOOR SUPPORT.

Next page: https://openairdocs.org/aircraft/N608JB/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 = 'N608JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N608JB/reports

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