# Service difficulty reports: N627JB

A list on [N627JB](https://openairdocs.org/aircraft/N627JB.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 · 66 reports

- [SDR YENA2025121701226](https://openairdocs.org/sdr/YENA2025121701226.md): Control Rod · faulted · Dec 15, 2025 · N627JB · Airbus A320232 · Landing Gear Doors
  > FLT 967, HPN-PBI. AN EMERGENCY WAS DECLARED AND AIRCRAFT DIVERTED TO JFK, AFTER T/O LAND GR. (NOSE) DOORS NOT CLOSED. RECYCLED. COMPLIED W/ QRH - PROBLEM PERSISTED; REF LP #'S 4145594 (REF TSM 32-31-00-810-859-A REMOVED AND REPLACED LT & RT NLG DOOR CONTROL RO
- [SDR YENA2025082100859](https://openairdocs.org/sdr/YENA2025082100859.md): Frame · damaged · Aug 19, 2025 · N627JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, PARTIAL REPLACEMENT OF FRAME 16 IAW TC A23-042-02. PERFORMED PERMANENT REPAIR WITH PARTIAL REPLACEMENT TO FRAME 16, S8R - 13R IAW SRM 51-42-11, DWG R531-13279-002, ISSUE E, AND EC A23-042-02.
- [SDR YENA2025082100858](https://openairdocs.org/sdr/YENA2025082100858.md): Frame · deformed · Aug 19, 2025 · N627JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: DEFORMATION ON FRAME 74 BTW STR 20R TO STR 20L AREA REAR FUSELAGE; REMOVED AND REPLACED FRAME 74 LOC. BTW STR20R TO STR 20L AREA REAR FUSELAGE I.A.W A320 SRM 51-42-11, A320 SRM 51-72-11 AND DRAWING D53572510.
- [SDR YENA2025082100857](https://openairdocs.org/sdr/YENA2025082100857.md): Bushing · loose · Aug 19, 2025 · N627JB · Airbus A320232 · Wing Main, Frame Structure
  > DURING HEAVY MAINTENANCE: SECONDARY FINDINGS LOOSE REPAIR BUSHING (1 EA), LOCATED BETWEEN RIB 16 TO RIB 17 FUEL TAN K AREA LH WING.; (RESOLVED ON W/O: 1391229 TASKCARD: NR-00039) PERFORMED BUSHING HOLE REPAIR AND REPLACED BRIDGING PLATE LOCATED BTW RIB16 TO R
- [SDR YENA2025082100856](https://openairdocs.org/sdr/YENA2025082100856.md): Frame · deformed · Aug 19, 2025 · N627JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: DEFORMATION ON FRAME 73 BTW STR20R TO STR 20L AREA REAR FUSELAGE; (RESOLVED ON W/O: 1391229 TASKCARD: NR-00040) REMOVED AND REPLACED DAMAGED FRAME 73 AND DAMAGED SHEAR WEBS/CLIPS LOCATED BTW STGR 20R TO STGR 20L AREA REAR FUSELAGE I
- [SDR YENA2025082100855](https://openairdocs.org/sdr/YENA2025082100855.md): Skin · deformed · Aug 19, 2025 · N627JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: DEFORMATION SKIN LOCATED BETWEEN FR 72 TO FR 75 AND STR 31L TO STR 31R JACKING POINT AREA REAR FUSELAGE; (RESOLVED ON W/O: 1391229 TASKCARD: NR-00041) PERFORMED PERMANENT REPAIR ON THE AFT FUSELAGE BOTTOM SKIN BETWEEN FR 72 TO FR 75
- [SDR YENA2025082100854](https://openairdocs.org/sdr/YENA2025082100854.md): Structure · damaged · Aug 19, 2025 · N627JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE / AFT FUSELAGE / FR72-75 AND STGR31L-31R / DEFORMATION (TAIL JACK DAMAGE) -PERMANENT REPAIR; REFERENCES: /A/ AEM EA 53-0047-25 (COVER & PART 1+2) /B/ AIRBUS DOSSIER 81633073 /C/ SRM 53-51-29-300-002 /D/ SRM 51-72-11 /E/ AIRBU
- [SDR YENA2025011300042](https://openairdocs.org/sdr/YENA2025011300042.md): Warning Message · false activation · Jan 10, 2025 · N627JB · Airbus A320232 · Central Warning
  > FLT#8358, SJO-EWR. (AIRCRAFT DIVERTED TO MCO). 'ENG 1 EPR MODE FAULT ECAM AUTO THRUST INOP SPLIT FROM L N1 & R N1, IN CRUISE 12-15% ENG 1 N1 69% ENG 2 N2 82% IN CRUISE WITH THRUST LEVERS MATCHED; PERFORMED TWM 73-22-00-810-817B DURING WIRINGS CHECKS FOUND AN O
- [SDR YENA2024072901056](https://openairdocs.org/sdr/YENA2024072901056.md): Slide Raft · unlaced · Jul 23, 2024 · N627JB · Airbus A320232 · Escape Slide
  > FLT#1890, SJU-EWR. 'DURING MX R1 DOOR SLIDE UNRAVELLED; REMOVED AND REPLACED R1 DOOR SLIDE PACK ASSY IAW AMM 25-62-44. OPS CHECK GOOD.'
- [SDR YENA2024022000288](https://openairdocs.org/sdr/YENA2024022000288.md): Unknown · odor · Feb 20, 2024 · N627JB · Airbus A320232 · Air Distribution System
  > FLT#1924, STI-BOS. 'FA'S REPORT THAT CABIN WAS FILLED WITH "DIRTY SOCK" ODOR DURING DESCENT; AIRCRAFT INSPECTED IAW TSM 05-50-00-810-085, ODOR IDENTIFIED AS TYPE 10, ( A),1C - AMBIENT AIR. IAW INFO NOTICE 2017-T015J, BOTH PACKS OPERATED WITH APU, NO
- [SDR YENA2023013100105](https://openairdocs.org/sdr/YENA2023013100105.md): None · none · Jan 27, 2023 · N627JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 16LH DOOR STOP 7 UPPER HOLE INBD POS CRACK DIRECTION IS 2 O'CLOCK L; 0.064" APPROX. (WO# 2022-456/1 WCC 2022-703036 AEROMAN); REF AEROMAN WO 2022-456/1 WCC 2022-703036 REMOVED AND REPLACED INTERCOSTAL FI
- [SDR YENA2023013100104](https://openairdocs.org/sdr/YENA2023013100104.md): None · none · Jan 27, 2023 · N627JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 16LH DOOR STOP 7 LWR HOLE INBD POSITION, CRACK DIRECTION IS 1 O'CLOCK, L: 0.064" APPROX (WO 2022-456/1 WCC 2022-703035 AEROMAN); REF AEROMAN WO# 2022-456/1 WCC# 2022-703035 REMOVED AND REPLACED INTERCOSTA
- [SDR YENA2023013100103](https://openairdocs.org/sdr/YENA2023013100103.md): None · none · Jan 27, 2023 · N627JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR16RH, DOOR STOP 7 LWR HOLE INBD POSITION, CRACK DIRECTION IS 8 O'CLOCK, L= 0.150" APPROX (AEROMAN WO2022-456/1 WCC 2022-703037; REF AEROMAN WO 2022-456-1 WCC 2022-703037 FOR WORK PERFORMED REMOVED AND REPL
- [SDR YENA2023013100102](https://openairdocs.org/sdr/YENA2023013100102.md): None · none · Jan 27, 2023 · N627JB · Airbus A320232 · Doors
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 16R, DOOR STOP 7 UPPER HOLE INBD POSITION, CRACK DIRECTION IS 5 O'CLOCK L; 0.089" APPROX. (AEROMAN WO# 2022-456/1 WCC 2022-703038); REF AEROMAN WO# 2022-456/1 WCC 2022-703038 FOR WORK PERFORMED: REMOVED AN
- [SDR YENA2023013100101](https://openairdocs.org/sdr/YENA2023013100101.md): None · none · Jan 27, 2023 · N627JB · Airbus A320232 · Doors
  > DURING HEAVY MAINTENANCE: CRACK INDICATIONS WERE FOUND ON BOTH INNER FRAME SEGMENTS OF FWD LH SIDE OVERWING EMERGENCY EXIT HATCH / EEH DOOR 833) CRACK LENGTH 0.20 APPROX. (AEROMAN WO2022-456-1 WCC# 2022-703077); REF AEROMAN WO 2022-456/1 WCC# 2022-703077 FOR W
- [SDR YENA2023013100100](https://openairdocs.org/sdr/YENA2023013100100.md): None · none · Jan 27, 2023 · N627JB · Airbus A320232 · Doors
  > DURING HEAVY MAINTENANCE: CRACK INDICATIONS WERE FOUND ON BOTH INNER FRAME SEGMENTS OF FWD RH SIDE OVERWING EMERGENCY EXIT HATCH (EEH DOOR 844) WITH CRACK LENGTH 0.20 APPROX (AEROMAN WO2022-456/1 WCC# 2022-703079); REF AEROMAN WO 2022-456/1 WCC 2022-703079 FOR
- [SDR YENA2023013100099](https://openairdocs.org/sdr/YENA2023013100099.md): None · none · Jan 27, 2023 · N627JB · Airbus A320232 · Doors
  > DURING HEAVY MAINTENANCE: CRACK INDICATIONS WERE FOUND ON BOTH INNER FRAME SEGMENTS OF FWD RH SIDE OVERWING EMERGENCY EXIT HATCH (EEH DOOR 843) CRACK LENGTH 0.20" APPROX (AEROMAN WO 2022-456/1 WCC 2022-703078); REF AEROMAN WO# 2022-456/1 WCC# 2022-703078 FOR W
- [SDR YENA2023013100098](https://openairdocs.org/sdr/YENA2023013100098.md): None · none · Jan 27, 2023 · N627JB · Airbus A320232 · Doors
  > DURING HEAVY MAINTENANCE: CRACK INDICATIONS WERE FOUND ON BOTH INNER FRAME SEGMENTS OF AFT LH SIDE OVERWING EMERG EXIT HATCH (EEH DOOR 834) CRACK LENGTH 0.20" APPROX (WO 2022-456/1 WCC 2022-703081 AEROMAN); REF AEROMAN WO 2022-456/1 WCC 2022-703081 FOR WORK P
- [SDR YENA2023013100097](https://openairdocs.org/sdr/YENA2023013100097.md): None · none · Jan 27, 2023 · N627JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STR 40R-STR41R AT FR 32 IN FWD CARGO COMPARTMENT (CPCP RELATED MPD TASK 532180-01); REMOVED AND REPLACED SHEAR TIE LOC. BTW STR 40R-41R AT FR 32 IN FWD CARGO COMPARTMENT IAW SRM A320-51-42-11 AND SRM 51-72
- [SDR YENA2023013100096](https://openairdocs.org/sdr/YENA2023013100096.md): None · none · Jan 27, 2023 · N627JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STR 42R-43R AT FR 33 IN FWD CARGO COMPARTMENT. (CPCP-RELATED MPD TASK 532180-01); REMOVED AND REPLACED SHEAR TIE LOC. BTW STR 42R-43R AT FR 33 IN FWD CARGO COMPARTMENT IAW SRM A320-51-42-11 AND SRM 51-72-1
- [SDR YENA2023013100095](https://openairdocs.org/sdr/YENA2023013100095.md): None · none · Jan 27, 2023 · N627JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC.BTW STR 42L-43L AT FR 32 IN FWD CARGO COMPARTMENT (CPCP-RELATED MPD TASK 532180-01); REMOVED AND REPLACED SHEAR TIE LOC. BTW STR 42L-43L AT FR 32 IN FWD CARGO COMPARTMENT IAW SRM A320-51-42-11 AND SRM A320-51-7
- [SDR YENA2023013100094](https://openairdocs.org/sdr/YENA2023013100094.md): None · none · Jan 27, 2023 · N627JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STR 40R-41R AT FR 34 IN FWD CARGO COMPARTMENT (CPCP RELATED MPD TASK 532180-01); REMOVED AND REPLACED SHEAR TIE LOC. BTW STR 40R-41R AT FR 34 IN FWD CARGO COMPARTMENT IAW SRM A320-51-42-11 AND SRM 51-72-11
- [SDR YENA2023013100093](https://openairdocs.org/sdr/YENA2023013100093.md): None · none · Jan 27, 2023 · N627JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 41R-BTW FR 31-32 IN FWD CARGO COMPARTMENT (CPCP-RELATED MPD TASK 532180-01); REMOVED AND REPLACED STRINGER 41R LOC. BTW FR 30-35 IN FWD CARGO COMPARTMENT IAW SRM A320-51-42-11 AND SRM 51-72-11, DRAWING D53231945; D5
- [SDR YENA2023013100092](https://openairdocs.org/sdr/YENA2023013100092.md): None · none · Jan 27, 2023 · N627JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STR 40R-41R AT FR 34 IN FWD CARGO COMPARTMENT (CPCP RELATED MPD TASK 532180-01); REMOVED AND REPLACED SHEAR TIE LOC. BTW STR 40R-41R AT FR 34 IN FWD CARGO COMPARTMENT IAW SRM A320-51-42-11 AND A320-53-72-1
- [SDR YENA2023013100091](https://openairdocs.org/sdr/YENA2023013100091.md): None · none · Jan 27, 2023 · N627JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STR 42L-43L AT FR 33 IN FWD CARGO COMPARTMENT (CPCP-RELATED MPD TASK 532180-01); REMOVED AND REPLACED CORROSION SHEAR TIE LOC. BTW STR 42L-43L AT FR 33 IN FWD CARGO COMPARTMENT IAW SRM A320-51-42-11 AND SR
- [SDR YENA2023013100090](https://openairdocs.org/sdr/YENA2023013100090.md): Shear Tie · corroded · Jan 27, 2023 · N627JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STR 40R-STR 41R AT FR 33 IN FWD CARGO COMPARTMENT; REMOVED AND REPLACED SHEAR TIE LOC.BTW STR40R-STR 41R AT FR 33 IN FWD CARGO COMPARTMENT IAW SRM A320-51-42-11 AND SRM A320-51-72-11, DWG D53231586. REF. A
- [SDR YENA2023013100089](https://openairdocs.org/sdr/YENA2023013100089.md): Shear Tie · corroded · Jan 27, 2023 · N627JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STR 41R-42R AT FR 34 IN FWD CARGO COMPARTMENT (CPCP RELATED MPD TASK 532180-01); REMOVED AND REPLACED SHEAR TIE LOC.BTW STR 41R-STR 42R AT FR 34 IN FWD CARGO COMPARTMENT IAW SRM A320-51-42-11 AND SRM A320-
- [SDR YENA2023013100088](https://openairdocs.org/sdr/YENA2023013100088.md): Shear Tie · corroded · Jan 27, 2023 · N627JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STR 41R-42R AT FR 33 IN FWD CARGO COMPARTMENT (CPCP RELATED MPD TASK 532180-01); REMOVED AND REPLACED SHEAR TIE LOC. BTW STR41R-STR42R AT FR 33 IN FWD CARGO COMPARTMENT (CPCP RELATED MPD TASK 532180-01) RE
- [SDR YENA2023013100087](https://openairdocs.org/sdr/YENA2023013100087.md): Shear Tie · corroded · Jan 27, 2023 · N627JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STR 43R-STR 44R AT FR33 IN FWD CARGO COMPARTMENT (CPCP RELATED MPD TASK 532180-01). REF. AEROMAN NR 2022-703114 FOR DETAILS. ( JETBLUE NR 000024); REMOVED AND REPLACED SHEAR TIE LOC. BTW STR 43R-STR44R AT
- [SDR YENA2023013100086](https://openairdocs.org/sdr/YENA2023013100086.md): Shear Tie · corroded · Jan 27, 2023 · N627JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STR 41R-42R AT FR 32 IN FWD CARGO COMPARTMENT (CPCP RELATED MPD TASK 532180-0); REMOVED AND REPLACED SHEAR TIE LOC. BTW STR 41R-42R AT FR 32 IN FWD CARGO COMPARTMENT IAW SRM A320-51-42-11 AND SRM 51-72-11,
- [SDR YENA2023013100085](https://openairdocs.org/sdr/YENA2023013100085.md): Shear Tie · corroded · Jan 27, 2023 · N627JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STR 41L-42L AT FR 32 IN FWD CARGO COMPARTMENT (CPCPO RELATED MPD TASK 532180-01); REMOVED AND REPLACED SHEAR TIE LOC. BTW STR 41L-42L AT FR 32 IN FWD CARGO COMPARTMENT IAW SRM A320-51-42-11 AND SRM A320-51
- [SDR YENA2022080100730](https://openairdocs.org/sdr/YENA2022080100730.md): A/C Pack · odor · Jul 30, 2022 · N627JB · Airbus A320232 · Air Distribution Fan
  > FLT#852, CUN-JFK. 'FUME EVENT ON TAKE-OFF AND INITIAL CLIMB; RAN ENG#1 AND #2 IAW AMM 72-00-00. COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION(B) 2, AND ACCOMPLISHED TSM 05-50-00-810-831-A #4 FAULT ISOLATION, SUBTASK 05-50-00-810-085-B + TASK AMM 21-00-00
- [SDR YENA2022012000037](https://openairdocs.org/sdr/YENA2022012000037.md): Thermostat · failed · Jan 17, 2022 · N627JB · Airbus A320232 · Pneumatic Distribution System
  > FLT # 393, BOS-DEN(AIR TURNBACK TO BOS). CLIMBING OUT OF 5000 AIR BLEED 1 FAULT, ECAM ACTION COMPLETED, QRH FOLLOWED. PACK 1 AND 2 SHOWING AMBER XX AND PRESSURIZATION NOT WORKING PROPERLY. WE HELD ALTITUDE AT 10,000 FEET AND ATTEMPTED TO RESET PACKS WITH NO RE
- [SDR YENA2021072300475](https://openairdocs.org/sdr/YENA2021072300475.md): Gps · faulted · Jul 22, 2021 · N627JB · Airbus A320232 · Global Positioning System
  > FLT # 1557, FLL-CUN. GPS PRIMARY LOST, NAV ACCUR LOW, EST 30 MILES OFF; PERFORMED RE-ALIGMENT OF ADIRUS IAW AMM 34-10-00. PERFORMED RESET AND TEST OF FCU 1 AND 2, ALSO FMGC 1 AND 2 IAW AMM 22-96-00 AND 22-91-00. TEST OK. PERFORMED RESET AND TEST OF GPS 1 AN
- [SDR YENA2021072300474](https://openairdocs.org/sdr/YENA2021072300474.md): Unknown · odor · Jul 19, 2021 · N627JB · Airbus A320232 · Air Distribution System
  > FLT # 1909, PAP-FLL. INTERMITTENT ODOR LIKE A BURNT WIRE/HOT METAL IN THE FLIGHT DECK. NOT REAL STRONG. COMING THRU AIR VENT. ONLY IN FLIGHT DECK AND VERY TRANSIENT; FOUND FAULT ELECTRICAL ODOR IN COCKPIT AREA WHILE TROUBLESHOOTING WITH PACK 1 ON/OFF AND CABI
- [SDR YENA2019110730636](https://openairdocs.org/sdr/YENA2019110730636.md): Bolt · loose · Nov 3, 2019 · N627JB · Airbus A320232 · Escape Slide
  > FT # 1931, BOS-IAH. L1 DR SLIDE "MISSING" APPEARS TO HAVE A LOOSE BOLT ON UPPER LEFT CORNER AND SLIDE APPEARS LOOSE ( PASS/OVERWING DOORSLIDE/RAFTS); REMOVED AND REPLACED LEFT BOLT ASSY ON L1 DOOR SLIDE IAW AMM 25-62-44-400-007-A. PLACARD REMOVED MX-4 UPDATED
- [SDR YENA2019082620478](https://openairdocs.org/sdr/YENA2019082620478.md): Unknown · odor · Aug 22, 2019 · N627JB · Airbus A320232 · Air Distribution System
  > FLT 174, SMELL OCCURRED BRIEFLY IN AFT GALLEY WHEN IDLE PASSING 13K AND IN FRONT GALLEY PASSING 6K LIGHTS OFF AT THE TIME NO SMELL DURING LANDING OR TAXI TO GATE. ELEC ODOR IN FWD AND AFT GALLEY INSPECTED COFFEE MAKERS REMOVED OVHD CEILING LIGHTS PANEL, SELE
- [SDR YENA2019082620475](https://openairdocs.org/sdr/YENA2019082620475.md): Unknown · odor · Aug 22, 2019 · N627JB · Airbus A320232 · Air Distribution System
  > FLT 174, MILD ELEC SMELL FLUID GALLEY SMELL SUBSEQUENTLY REPORTED ALSO IN AFT GALLEY SEEMED TO DISSIPATE WITH ALL GALLEY LIGHTING TURNED OFF AS REPORTED BY FAS, PERFORMED CHAP 5 INSPECTION IAW CABIN ODOR REPORT, FOUND TYPE 9 AS POSSIBLE SOURCE IE, COFFEE M
- [SDR YENA201907080397](https://openairdocs.org/sdr/YENA201907080397.md): Battery · discharged · Jul 8, 2019 · N627JB · Airbus A320232 · Emergency Lighting
  > FLT 391, BOS-TPA. EMERGENCY LIGHT TEST FAILED EPSU BATTERIES AT FIN# 11WL AND 13WL; REMOVED & REPLACED EMERGENCY LIGHT BATTERIES AT FIN 11WL AND 13WL PER AMM 33-51-38.
- [SDR YENA201907080396](https://openairdocs.org/sdr/YENA201907080396.md): Battery · discharged · Jul 8, 2019 · N627JB · Airbus A320232 · Emergency Lighting
  > FLT 391, BOS-TPA. EMERGENCY LIGHT TEST FAILED EPSU BATTERIES AT FIN# 11WL AND 13WL; REMOVED & REPLACED EMERGENCY LIGHT BATTERIES AT FIN 11WL AND 13WL PER AMM 33-51-38.
- [SDR YENA201904070243](https://openairdocs.org/sdr/YENA201904070243.md): Bracket · cracked · Apr 7, 2019 · N627JB · Airbus A320232 · Fuselage Main, Attach Fittings
  > FLT 2451, PLS-BOS. ON 4/7/2019 AT BOS, WAS REPORTED WITH CRACK DAMAGE TO THE LT MLG DOOR ACTUATOR BRACKET. CONTACTED FOR BRACKET REPLACEMENT INSTRUCTIONS AND PROVIDED REF /1/ RI. BOS MAINTENANCE COULD NOT PERFORM THE REPAIR DUE TO TOOLING ISSUES, AC WAS CDL AN
- [SDR YENA201812080844](https://openairdocs.org/sdr/YENA201812080844.md): Floorbeam · corroded · Dec 8, 2018 · N627JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y1292, FR 67-68, STR 23L. MEAS 3.5'L X 1.20"W X.045"D. P/N: D 5347217220. REMOVED AND REPLACED AFT CABIN FLOORBEAM Y1292, FR 67-68, STR 23L, IAW SRM 51-72-11.
- [SDR YENA201812080843](https://openairdocs.org/sdr/YENA201812080843.md): Floorbeam · corroded · Dec 8, 2018 · N627JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y-1292, FR 68-69, STR 23. MEAS 1.5'L X.90"W X.097"D. P/N: D 53472189204; REMOVED AND REPLACED THE AFT CABIN FLOORBEAM Y-1292, FR 68-69, STR 23R, IAW SRM: 51-72-11.
- [SDR YENA201807020273](https://openairdocs.org/sdr/YENA201807020273.md): Light · inoperative · Jun 27, 2018 · N627JB · Airbus A320232 · Emergency Lighting
  > FLT 1905, EWR-FLL. EMERGENCY LIGHTING ON SEAT 1C & 19C INOP (FLOOR PROX EMERG ESCAPE PATH MARK SYS - INCANDESCENT LIGHTING SYS - NOT APPLICABLE TO (N703 AND UP). REPLACED ESCAPE LIGHT ROW 1L AND 19R HARNESS REF ESPM 20-70-00. OPS CHECK GOOD.
- [SDR YENA201709060743](https://openairdocs.org/sdr/YENA201709060743.md): Unknown · odor · Sep 6, 2017 · N627JB · Airbus A320232 · Air Distribution System
  > ODOR IN THE FLIGHT DECK AFTER INITIAL THRUST REDUCTION AFTER TAKEOFF. CABIN CREW DID NOT NOTICE ANY ODOR. STRONG ODOR THROUGHOUT AIRCRAFT DURING DECENT. PERFORMED AN INSPECTION OF THE NR 1 AND 2 ENGINES FOR EXTERNAL OIL LEAKS AND CORRECT SERVICING. ALL CHEC
- [SDR YENA201708090653](https://openairdocs.org/sdr/YENA201708090653.md): Unknown · odor · Aug 9, 2017 · N627JB · Airbus A320232 · Air Distribution System
  > RETURNED TO AIRFIELD DUE TO A DIRTY SOCK ODOR AFTER TAKE OFF, WENT AWAY AFTER 1000FT, ODOR CONTINUED IN THE AFT GALLEY. ON DESCENT, THE ODOR WAS VERY STRONG IN THE COCKPIT; COMPLIED WITH INFO NOTICE 2017-T015 A SECTION B TABLE 1. NO DIRTY SOCKS ODOR NOTED. A
- [SDR YENA201708030639](https://openairdocs.org/sdr/YENA201708030639.md): Condenser · odor · Aug 3, 2017 · N627JB · Airbus A320232 · Cabin Cooling System
  > NR 1 A/C PACK HAD A DIRTY SOCK ODOR IN CABIN. REPORTED STRONGEST BY FA 3 IN REAR OF CABIN, SOME ODOR IN COCKPIT AS WELL, DURING CLIMBOUT. SUBSIDED DURING CRUISE. APU OFF, A/C PACK FLOW HIGH, NR 1 ENGINE 1:15 DURING TAXI PRIOR TO TAKE OFF, TURNING THE NR
- [SDR YENA201707240615](https://openairdocs.org/sdr/YENA201707240615.md): Oil System · overserviced · Jul 24, 2017 · N627JB · Airbus A320232 · APU Oil System
  > OUT OF 2,000 FEET DURING DECENT AT 250 KNOTS, A DIRTY SOCKS ODOR OVERTAKE THE ENTIRE FLIGHT DECK FLIGHT ATTENDENTS COULD SMELL IT IN THE AFT GALLEY AS WELL; COMPLIED WITH INFORMATION NOTICE 2017-T015A, SECTION B, TABLE 1 AIRCRAFT IS OK FOR SERVICE. WHILE CHECK
- [SDR YENA201707190593](https://openairdocs.org/sdr/YENA201707190593.md): Unknown · odor · Jul 19, 2017 · N627JB · Airbus A320232 · Air Distribution System
  > FUMES IN COCKPIT DURING APPROACH, PASSING 4500 FT. NOT DETECTED IN CABIN. APU NOT RUNNIG, SMELLED LIKE DIRTY SOCKS. PERFORMED A NR 1 & 2 ENGINES IDK RUN IAW AMM 71-00-00. COMPLIED WITH INFORMATION NOTICE 2017-T015 A SECTION B TABLE 1. PERFORMED PACK DECONA
- [SDR YENA201702080085](https://openairdocs.org/sdr/YENA201702080085.md): Skin · corroded · Feb 8, 2017 · N627JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON THE FORWARD FUSELAGE SKIN AT FRAME 14 & STRINGER 36L. REPAIRED IAW EC A17-099-01.

Next page: https://openairdocs.org/aircraft/N627JB/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 = 'N627JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N627JB/reports

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