# Service difficulty reports: N605JB

A list on [N605JB](https://openairdocs.org/aircraft/N605JB.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 · 60 reports

- [SDR YENA2026050700450](https://openairdocs.org/sdr/YENA2026050700450.md): Transponder · failed · May 6, 2026 · N605JB · Airbus A320232 · Dependent Position Determining System
  > FLT# 754, SJU-FLL. (AIRCRAFT RTF TO SJU, AN EMERGENCY WAS DECLARED) "AFTER TAKEOFF WE RECIEVED AN ECAM FOR TRANSPONDER 2 + THE FO'S MAP DISAPPEARD THEN WE SMELL A VERY STRONG ELECTRICAL BURNING SMELL; FOUND ATC TRANSPONDER COMPUTER WITHIN BURNT SMELL REMREP #2
- [SDR YENA2026012900086](https://openairdocs.org/sdr/YENA2026012900086.md): Unknown · odor · Jan 28, 2026 · N605JB · Airbus A320232 · Air Distribution System
  > FLT 866, FLL-BUF. RECEIVED REPORT FROM NR 1 FA SHE SMELLED BURNT PLASTIC IN FWD GALLEY AND A CHEMICAL SMELL FROM THE AFT GALLEY. THE #1 REPORTED IT TO THE PREVIOUS PILOTS. NO ENTRY IN THE LOG BOOK WAS MADE FROM THE PREVIOUS CREW.; ACCOMPLISHED TSM: 05-50-00-8
- [SDR YENA2025110301080](https://openairdocs.org/sdr/YENA2025110301080.md): Computer · failed · Oct 30, 2025 · N605JB · Airbus A320232 · Flight Control System
  > FLT#1230, CUN-EWR. (AIRCRAFT DIVERTED TO TPA) "F/CTL ELAC 2 PITCH FAULT AIRCRAFT PITCHED DOWN UNCOMMANDED IN CRUISE FLIGHT. AUTOPILOT STAYED ON; PERFORMED INTEROGGATION OF FCDC SYS #2 IAW TSM 27-00-00-810-801-A. ACCORDING TO DFDR REPORTS, TECH SUPPORT IDENTIFI
- [SDR YENA2025021100150](https://openairdocs.org/sdr/YENA2025021100150.md): Plate · worn · Feb 8, 2025 · N605JB · Airbus A320232 · Nacelle/Pylon Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: WEAR RIB 8 REINFORCING PLATE ON LH PYLON; REF AEROMAN WO 2025 25/1 NR 2025-76346 REPLACEMENT PYLON MOUNTING PLATE LOC SKIN LH WING IAW A320 SRM 57-21-11-300-005 AND A320 SRM 51-72-11-911-001 THIS REPAIR IS CATEGORY (A) NOT REQUIRED MO
- [SDR YENA2025021100149](https://openairdocs.org/sdr/YENA2025021100149.md): Structure · cracked · Feb 8, 2025 · N605JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN HOLE 1 LOC FR16RH DOUBLE JOGGLE AREA. C RACK DIRECTION 2 OCLOCK AND CRACK LENGTH 0.100 INCH; (RESOLVED ON W/O: 1353223 TASKCARD: NR-00006) REF AEROMAN WO 2025 25/1 NR 2025-76442 PERFORMED PERMANENT REPAI
- [SDR YENA2024011700061](https://openairdocs.org/sdr/YENA2024011700061.md): Outflow Valve · failed · Jan 15, 2024 · N605JB · Airbus A320232 · Pressure Regulator/Outflow Valve
  > FLT#1194, FLL-PVD. (AIRCRAFT PERFORMED ANA IR TURN BACK TO FLL) 'CAB PR SYS 1&2 FAULT DURING CLIMB OUT (5,000 FT); REMOVED AND REPLACED OUTFLOW VALVE ASSY IAW AMM 21-31-51. OPS CHECK OK.'
- [SDR YENA2023070300754](https://openairdocs.org/sdr/YENA2023070300754.md): Controller · failed · Jun 30, 2023 · N605JB · Airbus A320232 · Cabin Pressure Controller
  > FLT#113, MCO-CUN. (AIRCRAFT DIVERTED TO FLL) '(CPC2) CRUISING AT FL340. ECAM CAB ALT HI RED WARNING. ALL CAB PRESS INDICATIONS ARE NORMAL. CAB PRESS SYS 2 FAULT ALSO DISPLAYED. SYS 1 WAS OPERATIONAL. ( AUTOMATIC CABIN PRESSURE CONTROL SYSTEM-CPC2); REMOVED AN
- [SDR YENA2022100300981](https://openairdocs.org/sdr/YENA2022100300981.md): None · none · Oct 1, 2022 · N605JB · Airbus A320232 · Fuselage Structure (General)
  > FLT#170, FLL-BOS. 'LEVEL 1 ODOR EVENT. FCOM ODER ISOLATION PROCEDURE COMPLIED WITH. PACK 1 SUSPECTED. ODOR NOT DETECTABLE AFTER 3-5 MIN AIRCRAFT ENVIRONMENTAL SYSTEM ODER; PERFORMED LEVEL A DECONTAMINATION AND REPLACED BOTHH RECIRCULATION FILTER OER E 30905. R
- [SDR YENA2022050900458](https://openairdocs.org/sdr/YENA2022050900458.md): None · none · May 7, 2022 · N605JB · Airbus A320232 · Fuselage Structure (General)
  > FLT#867, EWR-PLS. 'STRONG DIRTY SOCK SMELL ON APPROACH FROM 15,000 FT UNTIL LANDING IN COCKPIT AND ENTIRE CABIN; COMPLIED WITH INFORMATION NOTICE 2017-T01 SECTION A (A), ISOLATED FAULT TO TYPE 10 (A) 1, PER TSM 05-5--00-810-085-B/TSM 05-50-00-810-085-D AIRCRA
- [SDR YENA2022042900424](https://openairdocs.org/sdr/YENA2022042900424.md): None · none · Apr 27, 2022 · N605JB · Airbus A320232 · Oxygen System
  > FLT#2519, LGA-MSY. 'FA/S IN REAR OF AIRPLANE REPORTED STRONG MUSTY ODOR AT AROUND 10000' ON DESCENT ACCOMPANIED BY HEADACHE. FO ALSO REPORTED THE SMELL BUT NOT AS STRONG ( PACKS); RAN BOTH ENGINES WITH RESPECTIVE PACKS AND BLEEDS. 2 FULL CYCLES HOT AND COLD,
- [SDR YENA2022041800376](https://openairdocs.org/sdr/YENA2022041800376.md): None · none · Apr 14, 2022 · N605JB · Airbus A320232 · Air Conditioning System
  > FLT#6100, FLL-EWR. (AIRCRAFT DIVERTED TO JFK) 'AT 13000 IN DESCENT SEVERE FUME SMELL STARTED EMANATING FROM THE CABIN ON FERRY FLIGHT. DH CAPT FOUND IT STRONGEST AROUND 4 AND 5 ROWS PILOTS AND DH PILOT WENT ON O2 UNTIL POST SHUT DOWN AT GATE; REF LOG PAGE 3354
- [SDR YENA2022041500375](https://openairdocs.org/sdr/YENA2022041500375.md): A/C Pack · failed · Apr 13, 2022 · N605JB · Airbus A320232 · Cabin Cooling System
  > FLT#867, EWR-PLS. '“RAN COCKPIT/CABIN ODOR REPORTING AND ISOLATION PROCEDURE. DETERMINED NASTY AND NAUSEATING ODOR FROM PACK 1. MORE NOTICEABLE IN ROWS 1-10 MY EYES STARTED BURNING AFTER 10 MINUTES STANDING NEXT TO ROW 4”. ( PACKS); ACCOMPLISHED INFO NOTICE 2
- [SDR YENA2022041100347](https://openairdocs.org/sdr/YENA2022041100347.md): Packboard · odor · Apr 8, 2022 · N605JB · Airbus A320232 · Cabin Cooling System
  > FLT#492, LAX-BUF. 'MILD MUSTY SMELL OBSERVED IN CRUISE. PER FCOM ISOLATED PACK 2 OFF AND THE ODOR SEEMED TO DISSIPATE.'(SUPPLEMENTAL TO FOLLOW)
- [SDR YENA2022031500227](https://openairdocs.org/sdr/YENA2022031500227.md): Stringer · corroded · Feb 19, 2022 · N605JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE, PER AEROMAN N/R 2022-19278 - CORROSION STRINGER 42R BETWEEN FR31 TO FR34 IN FWD CARGO COMPARTMENT; PER AEROMAN N/R 2022-19278 - PERFORMED PERMANENT REPAIR SECTION STRINGER LOC ON FR 31 TO FR 34 AND STRINGER 42R IAW SRM A320 53-00-13-3
- [SDR YENA2022031500226](https://openairdocs.org/sdr/YENA2022031500226.md): Stringer · corroded · Feb 19, 2022 · N605JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE, REF. AEROMAN N/R 2022-19279 - CORROSION STRINGER 39L BETWEEN FR31/FR32 IN FWD CARGO COMPARTMENT; PER AEROMAN N/R 2022-19279 - PERFORMED PERMANENT REPAIR ON SECTION STRINGER LOC. ON FR31 TO FR 33 AND STR 39L IN FWD CARGO COMPARTMENT IA
- [SDR YENA2022031500225](https://openairdocs.org/sdr/YENA2022031500225.md): Stringer · corroded · Feb 19, 2022 · N605JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE, REF. AEROMAN N/R 2022-19281 - CORROSION STRINGER 43L BETWEEN FR32/FR34 IN FWD CARGO COMPARTMENT; PER AEROMAN N/R 2022-19281 - PERFORMED PERMANENT REPAIR SECTION STRINGER 43L BTW FR31 TO FR35 IN FWD CARGO COMPARTMENT IAW SRM A320-51-4
- [SDR YENA2022031500224](https://openairdocs.org/sdr/YENA2022031500224.md): Stringer · corroded · Feb 19, 2022 · N605JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE, REF. AEROMAN N/R 2022-19283 - CORROSION STRINGER 43R BETWEEN FR32/FR34 IN FWD CARGO COMPARTMENT; PER AEROMAN N/R 2022-19283 - PERFORMED PERMANENT REPAIR ON SECTION STRINGER LOC. ON FR32 TO FR 34 AND STR 43R IN FWD CARGO COMPARTMENT IA
- [SDR YENA2022031500223](https://openairdocs.org/sdr/YENA2022031500223.md): Stringer · corroded · Feb 19, 2022 · N605JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE, REF. AEROMAN N/R 2022-19151 - CORROSION STRINGER 44 BETWEEN FRAME 24A TO FRAME 28 IN FWD CARGO COMPA RTMENT; PER AEROMAN N/R 2022-19151 - REMOVED AND REPLACED STRINGER 44 PRODUCTION SECTION LOC BTW FR24A TO FR28 IN FWD CARGO COMPARTME
- [SDR YENA2022031500222](https://openairdocs.org/sdr/YENA2022031500222.md): Stringer · corroded · Feb 19, 2022 · N605JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE, REF. AEROMAN N/R 2022-19280 - CORROSION STRINGER 40L BETWEEN FR31/FR32 IN FWD CARGO COMPARTMENT; PER AEROMAN N/R 2022-19280 - PERFORMED PERMANENT REPAIR ON SECTION STRINGER LOC. FR 31 TO FR 33 AND STRINGER 40L IN FWD CARGO COMPARTMENT
- [SDR YENA2022031500221](https://openairdocs.org/sdr/YENA2022031500221.md): Frame · cracked · Feb 19, 2022 · N605JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, REF AEROMAN N/R 2022-19125 - CRACK INDICATIONS WERE FOUND IN FRAME SEGMENT 1 AT FWD RH SIDE OVERWIN G EMERGENCY EXIT HATCH (EEH DOOR 843). AFT FRAME SEGMENT L= 2.20 INCHES. FWD FRAME SEGMENT L= 2.00 INCHES; PER AEROMAN N/R 2022-19125
- [SDR YENA2022031500220](https://openairdocs.org/sdr/YENA2022031500220.md): Frame · cracked · Feb 19, 2022 · N605JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, REF AEROMAN N/R 2022-19128 - CRACK INDICATIONS WERE FOUND IN FRAME SEGMENT 1 AT AFT RH SIDE OVERWIN G EMERGENCY EXIT HATCH (EEH DOOR 844). AFT FRAME SEGMENT L= 1.20 INCHES. FWD FRAME SEGMENT L= 1.70 INCHES; PER AEROMAN N/R 2022-19128
- [SDR YENA2022031500219](https://openairdocs.org/sdr/YENA2022031500219.md): Frame · cracked · Feb 19, 2022 · N605JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, REF AEROMAN N/R 2022-19130 - CRACK INDICATIONS WERE FOUND IN FRAME SEGMENT 1 AT AFT LH SIDE OVERWIN G EMERGENCY EXIT HATCH (EEH DOOR 834). FWD FRAME SEGMENT L= 0.80 INCHES; PER AEROMAN N/R 2022-19130 - REMOVED AND REPLACED FRAME SEGME
- [SDR YENA2022031500218](https://openairdocs.org/sdr/YENA2022031500218.md): Frame · cracked · Feb 19, 2022 · N605JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, REF AEROMAN N/R 2022-19132 - CRACK INDICATIONS WERE FOUND IN FRAME SEGMENT 1 AT FWD LH SIDE OVERWING EMERGENCY EXIT HATCH (EEH DOOR 833). AFT FRAME SEGMENT L= 1.40 INCHES. FWD FRAME SEGMENT L= 1.20 INCHES; PER AEROMAN N/R 2022-19132 -
- [SDR YENA2022031500217](https://openairdocs.org/sdr/YENA2022031500217.md): Stringer · corroded · Feb 19, 2022 · N605JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION STRINGER 41R BETWEEN FR32/FR34 IN FWD CARGO COMPARTMENT; REF: ARM W/O 2022 2/1 N/R 2022-19284 REPLACED SECTION STRINGER 41R AND FASTENERS LOC ON FR32 TO FR34 IAW SRM A320 51-72-11, 51-42-11 AND DRAWINGS # E533231472, D532314
- [SDR YENA2022031500216](https://openairdocs.org/sdr/YENA2022031500216.md): Fitting · corroded · Feb 19, 2022 · N605JB · Airbus A320232 · Wing Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION ON FITTING MLG ACTUATOR L/H SIDE; (RESOLVED ON W/O: 1142568 TASKCARD: NR-00039) REF: ARM W/O 2022 2/1 N/R 2022-19333 REPAIRED IAW A320 SRM 57-26-13-300-007 TABLE 001. THIS IS CAT C WITH REPAIR LIFE LIMIT 40000FC FROM FIR
- [SDR YENA2022031500215](https://openairdocs.org/sdr/YENA2022031500215.md): Fitting · corroded · Feb 19, 2022 · N605JB · Airbus A320232 · Wing Main, Frame Structure
  > DURING HEAVY MAINTENANCE, CORROSION ON FITTING MLG ACTUATOR RH SIDE; (RESOLVED ON W/O: 1142568 TASKCARD: NR-00040) REF: ARM W/O 2022 2/1 N/R 2022-19333 REPAIRED FITTING IAW A320 SRM 57-26-13-300-008 TABLE 001. THIS REPAIR IS CAT C WIFE LIMIT 35000FC FROM R
- [SDR YENA2022031500214](https://openairdocs.org/sdr/YENA2022031500214.md): Stringer · corroded · Feb 19, 2022 · N605JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION STRINGER 44 BETWEEN FR33/FR34 IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1142568 TASKCARD: NR-00041) REF: ARM W/O 2022 2/1 N/R 2022-19282 REPAIRED IAW A320 SRM 53-00-13-300-001 PROCEDURE 2. A AND DRAWING D53231375. THIS RE
- [SDR YENA2021122700870](https://openairdocs.org/sdr/YENA2021122700870.md): Battery · failed insp · Dec 21, 2021 · N605JB · Airbus A320232 · Emergency Lighting
  > FLT 119, ALB-MCO. LEFT EMER. BAT FAILED CAP. CK; REPLACED LEFT EMER BAT IAW AMM 33-51-00
- [SDR YENA2021071500463](https://openairdocs.org/sdr/YENA2021071500463.md): Battery · no test · Jul 11, 2021 · N605JB · Airbus A320232 · Emergency Lighting
  > FLT 274, AUA-BOS. FWD L/H EMERGENCY LIGHT BATTERY/EPSU FAILLED CAPACITY TEST; R & R BATTERY IAW AMM 33-51-00.
- [SDR YENA2021012200075](https://openairdocs.org/sdr/YENA2021012200075.md): Battery · no test · Jan 20, 2021 · N605JB · Airbus A320232 · Emergency Lighting
  > FLT 1380, FLL-DCA. EPSU 11WL FAILED BAT CAP TEST. R & R EPSU BAT AT 11WL, IAW 320 MM 33-51-38. OPERATIONS CHECK GOOD.
- [SDR YENA2021012200074](https://openairdocs.org/sdr/YENA2021012200074.md): Battery · no test · Jan 20, 2021 · N605JB · Airbus A320232 · Emergency Lighting
  > FLT 1380, FLL-DCA. EPSU 10WL FAILED BAT CAP TEST. R & R EPSU BAT AT 10WL, IAW 320 MM 33-51-38. OPERATIONS CHECK GOOD.
- [SDR YENA2021012200073](https://openairdocs.org/sdr/YENA2021012200073.md): Battery · no test · Jan 20, 2021 · N605JB · Airbus A320232 · Emergency Lighting
  > FLT 1380, FLL-DCA. EPSU 13WL FAILED BAT CAP TEST. R & R EPSU BAT AT 13WL, IAW 320 MM 33-51-38. OPERATIONS CHECK GOOD.
- [SDR YENA2020122100616](https://openairdocs.org/sdr/YENA2020122100616.md): Fitting · dirty · Dec 17, 2020 · N605JB · Airbus A320232 · Emergency Equipment
  > FLT 1305, EWR-FLL. L1 DOOR ARMING LEVER DIFFICULT TO ENGAGE AND BEGAN MOVING DURING TAKEOFF ROLL. FOUND FWD FLOOR FITTING SPRING PAWL NOT ENGAGING WITH GIRT BAR DUE TO DEBRIS IN FITTING. CLEANED FITTING & REMOVED DEBRIS. REMOVED GIRT BAR FROM ARMING MECHAN
- [SDR YENA201902085057](https://openairdocs.org/sdr/YENA201902085057.md): Lens · missing · Feb 5, 2019 · N605JB · Airbus A320232 · Emergency Lighting
  > FT # 65, ROW 11 DEF RED EMERG. LIGHT LENS MISSING OUTBOARD SEAT; REPLACED RED EMERG. LIGHT LENS AS REQ'D. OPS CHECKS GOOD.
- [SDR YENA201706280542](https://openairdocs.org/sdr/YENA201706280542.md): Battery Pack · failed · Jun 28, 2017 · N605JB · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT FAILED TO TEST. R & R THE BATTERY PACK IAW AMM 33-51-11. EMERGENCY LIGHT TESTED OK.
- [SDR YENA201706280533](https://openairdocs.org/sdr/YENA201706280533.md): Battery Pack · no test · Jun 28, 2017 · N605JB · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT FAILED TO TEST. R & R THE BATTERY PACK IAW AMM 33-51-11. EMERGENCY LIGHTS TESTED OK.
- [SDR YENA201706070476](https://openairdocs.org/sdr/YENA201706070476.md): Unknown · odor · Jun 7, 2017 · N605JB · Airbus A320232 · Air Distribution System
  > DURING DECENT PASSING 14000 FT, F/A CALLED COCKPIT TO NOTIFY US THAT A STRONG BURNING ODOR IS COMING FROM REAR OF THE ACFT AT ROWS 22 TO REAR GALLEY. NOTHING VISIBLE. DECLARED AN EMERGENCY. TURNED OFF LIVE TV, ODOR DISIPATED AROUND 6000 FEET ON APPROACH.
- [SDR YENA20161029959](https://openairdocs.org/sdr/YENA20161029959.md): Fan · failed · Oct 29, 2016 · N605JB · Airbus A320232 · Air Distribution Fan
  > FLT 1165, PILOT FELT VIBRATION IN COCKPIT FOLLOWED BY ELECTRICAL ODOR AND SMOKE COMING FROM PEDESTAL VENT. EXTRACT FAULT ECAM THEN CAME ON. FOLLOWED ECAM AND QRH FOR AVIONICS SMOKE SMOKE SOURCE. ISOLATED TO VENT EXTRACT FAN. MAINTENANCE PERFORMED TSM 24-00
- [SDR YENA20161017926](https://openairdocs.org/sdr/YENA20161017926.md): Selector Valve · leaking · Oct 17, 2016 · N605JB · Airbus A320232 · Landing Gear Retraction/Extension System
  > PILOT REPORTED LANDING GEAR LGCIU NR 1 FAULT AFTER TAKEOFF. CREW RETURNED TO DEPARTURE FOR TROUBLESHOOTING. DURING TROUBLESHOOTING, FOUND LANDING GEAR SELECTOR VALVE ASSEMBLY LEAKING HYDRAULIC FLUID. R & R LANDING GEAR SELECTOR VALVE IAW AMM 32-31-12.
- [SDR YENA20160315241](https://openairdocs.org/sdr/YENA20160315241.md): Floorbeam · corroded · Mar 15, 2016 · N605JB · Airbus A320232 · Fuselage Main, Floor Beam
  > CORROSION ON CABIN FLOORBEAM T-CAP, Y-1292 RT AT CROSSBEAM 20; R & R FLOORBEAM - Y1292 AT FRAME, CROSSBEAM 20 IAW SRM 51-42-11. REF SERVICE ORDER 440295, NR 20400 FOR ADDITIONAL INFORMATION.
- [SDR YENA20160315240](https://openairdocs.org/sdr/YENA20160315240.md): Shear Web · corroded · Mar 15, 2016 · N605JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > SUP: UNDER RT OTBD. CABIN SHEAR WEB CORRODED BETWEEN CROSSBEAMS 69 & 70; R & R SUPPORT UNDER RT OTBD. CABIN SHEAR WEB AT CROSSBEAM 69 & 70 IAW SRM 51-42-11.
- [SDR YENA20160315239](https://openairdocs.org/sdr/YENA20160315239.md): Floorbeam · corroded · Mar 15, 2016 · N605JB · Airbus A320232 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM T-CAP Y1732 LT AT CROSSBEAM 66; REMOVED CORROSION ON FLOORBEAM T-CAP LT, PERFORMED UT INSPECTION. MATERIAL MEASUREMENT FROM.155 TO.088 FAB 1 EA FITTING + ANGLE, DRILLED 2 EA FITTING /ANGLE IAW SRM 53-41-14, FIG 201,TREATED + PRIME F
- [SDR YENA20160315238](https://openairdocs.org/sdr/YENA20160315238.md): Floorbeam · corroded · Mar 15, 2016 · N605JB · Airbus A320232 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM T-CAP 1732, RT AT CROSSBEAM 66; REMOVED CORROSION AND INSTALLED REPAIR AT FRAME 66 T-CAP 1732, RT IAW SRM 53-41-14.
- [SDR YENA20160315237](https://openairdocs.org/sdr/YENA20160315237.md): Stringer · corroded · Mar 15, 2016 · N605JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPARTMENT STR 44 HAS CORROSION AROUND FASTENERS AT 8" AFT OF FR 31; REMOVED CORROSION AND CHECK LIMITS IAW SRM 51-74-00, PAGE 5, 53-21-13, FIG 102, FOUND TO BE OUT LIMITS IAW SRM 51-74-00 PAR 5, 53-21-13, FIG 102 INSTALLED REPAIR AT STR 44 IAW SRM
- [SDR YENA20160315236](https://openairdocs.org/sdr/YENA20160315236.md): Stringer Splice · corroded · Mar 15, 2016 · N605JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO STRINGER SPLICE 43L HAS CORROSION BETWEEN FR 30-FR 31; REMOVED STR SPLICE AT 43L BETWEEN FR 30-FR 31 CUTOUT CORRODED STR RECEIVED NEW SPLICE AND REPAIR STRINGER, TREATED, PRIMED, TOP COATED, AND INSTALLED REPAIR SPLICE, REPAIR STRINGER, AND REPLACEME
- [SDR YENA20160315235](https://openairdocs.org/sdr/YENA20160315235.md): Stringer · corroded · Mar 15, 2016 · N605JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPARTMENT STR 41L HAS CORROSION AROUND THE FASTENERS AT 3" FWD OF FR32; REMOVED DAMAGE IN FWD CARGO COMPARTMENT STR 41L R32 FABRICATED NEW STR AND 2 SPLICE PLATE AND INSTALLED IAW SRM 53-00-13, PB 201, FIG 201. REMOVED DOPT DS D 83T TREATED, PRIME
- [SDR YENA20160315234](https://openairdocs.org/sdr/YENA20160315234.md): Stringer · corroded · Mar 15, 2016 · N605JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPARTMENT STR 41R HAS CORROSION AROUND FASTENERS; STR 41R AT FRAME 28-30 FOUND STR AND SPLICE IAW SRM 53-21-13, PG 101, REMOVED STR AND SPLICE IAW SRM 51-42-11, FWD NEW STRINGER AND SPLICE IAW SRM 53-21-13 LOCATED DRILLED AND DEBURRED REPAIR STRING
- [SDR YENA20160315233](https://openairdocs.org/sdr/YENA20160315233.md): Stringer · corroded · Mar 15, 2016 · N605JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPARTMENT STRINGER 41R HAS CORROSION AROUND THE FASTENERS FR 29 - FR 30; REPAIR STRINGER AT 41R & FRAME 28-30 IAW SRM 53-21-13 INSTALLED FLOORBOARD PANELS & THRESHOLD IAW AMM 25-554-12.
- [SDR YENA20151121580](https://openairdocs.org/sdr/YENA20151121580.md): Contactor · inoperative · Nov 21, 2015 · N605JB · Airbus A320232 · Electrical Power System
  > EMERGENCY GENERATOR TEST FAILED. R & R RELAYS 12XE AND 16XE, NO HELP, REF SWPM 20-46-50. R & R 3XC 3 POLE CONTACTOR IAW AMM 24-25-55. NO HELP. CONTINUED ON DEFECT 1730594-2.
- [SDR YENA20151121577](https://openairdocs.org/sdr/YENA20151121577.md): Generator · inoperative · Nov 21, 2015 · N605JB · Airbus A320232 · Electrical Power System
  > EMERGENCY GENERATOR TEST FAIL. R & R CONSTANT SPEED MOTOR GENERATOR, EMERGENCY GEN 8XE, IAW AMM 24-24-51. LEAK AND OPS CHECK GOOD.

Next page: https://openairdocs.org/aircraft/N605JB/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 = 'N605JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N605JB/reports

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