# Service difficulty reports: N645JB A list on [N645JB](https://openairdocs.org/aircraft/N645JB.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 · 52 reports - [SDR YENA2025061100583](https://openairdocs.org/sdr/YENA2025061100583.md): Lgciu · failed · Jun 10, 2025 · N645JB · Airbus A320232 · Central Display > FLT#690, FLL-BOS. (AIRCRAFT PERFORMED AN AIR TURN BACK TO FLL).'EIS DMC #3 INOP; REMOVED AND REPLACED #1LGCIU IAW AMM 32-31-71. OPS CHECK GOOD SEE ITEM#2 FOR DMC #1 RESOLUTION.' - [SDR YENA2024092601305](https://openairdocs.org/sdr/YENA2024092601305.md): Idg · failed · Sep 23, 2024 · N645JB · Airbus A320232 · AC Generator-Alternator > FLT#2201, JFK - FLL (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) 'DURING CLIMB PHASE AT 30500 FT LOST GEN# 01 AND FAC #01; REMOVED AND REPLACED NO 1 IDG IAW AMM 24-21-51-410-010. ALL OPS CHECK OK & LEAK CHECK OK AT THIS TIME. A/C OK FOR CONT SVC.' - [SDR YENA2024012400096](https://openairdocs.org/sdr/YENA2024012400096.md): Shear Tie · corroded · Jan 17, 2024 · N645JB · Airbus A320232 · Fuselage Internal Mounting Structure > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED BTW STRINGER 43L AND STRINGER 44 AT LEVEL OF FRAME 33 IN FWD CARGO COMPARTMENT(CPCP RELATED MPD TASK 532180-01); (RESOLVED ON W/O: 1243677 TASKCARD: NR-00016) REF AEROMAN WO 2023 464/1 NR 2023-731912 REMOVE - [SDR YENA2024012400095](https://openairdocs.org/sdr/YENA2024012400095.md): Shear Tie · corroded · Jan 17, 2024 · N645JB · Airbus A320232 · Fuselage Internal Mounting Structure > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED BTW STRINGER 43R AND STRINGER 44 AT LEVEL OF FRAME 29 IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1243677 TASKCARD: NR-00018) REF AEROMAN WO 2023 464/1 NR 2023-731899 REMOVED AND REPLACED SHEAR TIE AND SUP - [SDR YENA2024012400094](https://openairdocs.org/sdr/YENA2024012400094.md): Door Frame · cracked · Jan 17, 2024 · N645JB · Airbus A320232 · Fuselage Main, Structure > DURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR (AFT RH EEH DOOR 844) CRACK L=0.129 INCH APPROX; REF AEROMAN WO 2023 464/1 NR 2023-732064 REMOVED AND REPLACED FRAME SEGMENTS ON EMERGENCY EXIT DOOR DOOR - [SDR YENA2024012400093](https://openairdocs.org/sdr/YENA2024012400093.md): Door Frame · cracked · Jan 17, 2024 · N645JB · Airbus A320232 · Fuselage Main, Structure > DURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR (AFT LH EEH DOOR 834) CRACK L=0.125 INCH APPROX; REF AEROMAN WO 2023 464/1 NR 732065 REMOVED AND REPLACED FRAME SEGMENTS ON EMERGENCY EXIT DOOR DOOR 834 F - [SDR YENA2024012400092](https://openairdocs.org/sdr/YENA2024012400092.md): Door Frame · cracked · Jan 17, 2024 · N645JB · Airbus A320232 · Fuselage Main, Structure > DURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR (FWD LH EEH DOOR 833) CRACK L=0.127 INCH APPROX; REF AEROMAN WO 464/1 NR 2023-732066 REMOVED AND REPLACED FRAME SEGMENTS ON EMERGENCY EXIT DOOR DOOR 833 F - [SDR YENA2024012400091](https://openairdocs.org/sdr/YENA2024012400091.md): Door Frame · cracked · Jan 17, 2024 · N645JB · Airbus A320232 · Fuselage Main, Structure > DURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR (FWD RH EEH DOOR 843) CRACK L=0.130 INCH APPROX; REF AEROMAN WO 2023 464/1 NR 2023-732067 REMOVED AND REPLACED FRAME SEGMENTS ON EMERGENCY EXIT DOOR DOOR - [SDR YENA2024012400090](https://openairdocs.org/sdr/YENA2024012400090.md): Door Frame · cracked · Jan 17, 2024 · N645JB · Airbus A320232 · Fuselage Main, Structure > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE H1 (UPPER INBOARD POS) LOCATED ON DOORSTOP FITTING 7 FRAME 16 RH; CRACK DIRECTION: 06 OCLOCK, D1-D2=0. 099 INCH; (RESOLVED ON W/O: 1243677 TASKCARD: NR-00027) REF AEROMAN WO 2023 464/1 NR 2023-73194 - [SDR YENA2024012400089](https://openairdocs.org/sdr/YENA2024012400089.md): Stop Fitting · damaged · Jan 17, 2024 · N645JB · Airbus A320232 · Fuselage Main, Structure > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUNDS (2EA) IN OPEN HOLE (1EA) H3 (LOWER INBOARD POS) LOCATED ON DOORSTOP FITTING 7 FRAME 16 RH CRACK DIRECTION: 11 AND 12 OCLOCK, D1-D2= 0.166 INCH; D1-D2=0.105 INCH; REF AEROMAN WO 2023 464/1 NR 731941 PERFORMED P - [SDR YENA2024012400088](https://openairdocs.org/sdr/YENA2024012400088.md): Slat Track · cracked · Jan 17, 2024 · N645JB · Airbus A320232 · Wing, Attach Fittings > DURING HEAVY MAINTENANCE: CRACK ON SLAT FWD STOP BOLT SLAT TRACK POSITION ON R/H WING / REF AEROMAN WO 2023 464/1 NR 2023-732209 * PERFROMED PERMANANT REPAIR LOC SLAT TRACK RIB 7 LOWER LUG ON RH WING. THIS REPAIR IS CAT A., NO FURTHER ACTIONS REQUIRED IAW A320 - [SDR YENA2024012400087](https://openairdocs.org/sdr/YENA2024012400087.md): Skin · dented · Jan 17, 2024 · N645JB · Airbus A320232 · Fuselage Main, Plate/Skin > DURING HEAVY MAINTENANCE: DENTS ON EXTRENAL SKIN LOCATED EXISTING REPAIR BTE 23 - FR24 & R40R - STR 43R AT LOWER FUSLELAGE / (RESOLVED ON W/O: 1243677 TASKCARD: NR-00043) REF AEROMAN WO 2023- 464/1 NR 2023-731807 PERFORMED PERMANENT REPAIR LOCATED ON EXTERNAL - [SDR YENA2023090501039](https://openairdocs.org/sdr/YENA2023090501039.md): Unknown · unknown · Sep 2, 2023 · N645JB · Airbus A320232 · Air Conditioning System > FLT#2110, SDQ-JFK. 'BELOW 4000 ODOR FUME EVENT ON APPROACH MUSTY DRY COCKPIT; COMPLIED WITH INFORMATION NOTICE 2017 T015 SECTION A ISOLATED FAULT TO TYPE 10 1 C PER TSM 05-00-810-085 B TSM 05-50-00-810-085D. A/C OK FOR SVC.' - [SDR YENA2021083100551](https://openairdocs.org/sdr/YENA2021083100551.md): Valve · failed · Aug 27, 2021 · N645JB · Airbus A320232 · Pneumatic Distribution System > FLT 119, MCO-ALB. DIVERTED TO JFK. AIR ENG 1 AND 2 BLEED FAULT ECAM DURING CLIMB; R & R VALVE (6HV) IAW AMM 36-12-52. OPS CHK OK. A/C OK FOR CONT. SVC. - [SDR YENA2021020500090](https://openairdocs.org/sdr/YENA2021020500090.md): Slide · no test · Feb 3, 2021 · N645JB · Airbus A320232 · Escape Slide > DURING HMV, DURING OPERATIONAL OF THE SLIDE RAFT, THE SLIDE RAFT TOUCH THE FUSELAGE ON DOOR 832 IAW AMM 25-6244-400-A PROCEDURE4B.12.B; REF AEROMAN N/R 2021- 12176. R & R FOR SERVICEABLE ESCAPE SLIDE IAW AMM 25-62-44-000-007-A, AMM 25-26-44-400-007-A. PN OFF - [SDR YENA2021020500089](https://openairdocs.org/sdr/YENA2021020500089.md): Slide · no test · Feb 3, 2021 · N645JB · Airbus A320232 · Escape Slide > DURING HMV, DURING OPERATIONAL OF THE SLIDE RAFT, THE SLIDE RAFT TOUCH THE FUSELAGE ON DOOR 831 AS PER AMM 25-62-44-400-A PROCEDURE 4.B.12(B); REF AEROMAN N/R 2021-12173, R & R FOR SERVICEABLE ESCAPE SLIDE OF DOOR 831 IAW AMM 25-62-44-000-012-A, AMM 25-62-44- - [SDR YENA2020022400193](https://openairdocs.org/sdr/YENA2020022400193.md): Unknown · vibration · Feb 20, 2020 · N645JB · Airbus A320232 · Standard Practices/Structures > FT # 1460, FLL-BDL. DIVERTED TO MCO. ON CLIMB OUT ACCELERATING TO 335 KNT A/C PERFORMED MODERATED VIBRATION CLIMB TROUGH FL 240. VIBRATION WAS IN AFT OF A/C. LEVELED OFF FL 260 SLOWING DOWN TO 250 KTS, VIBRATING REDUCED BUT WAS STILL NOTICEABLE. SPED UP TO 33 - [SDR YENA201909260554](https://openairdocs.org/sdr/YENA201909260554.md): Battery · discharged · Sep 26, 2019 · N645JB · Airbus A320232 · Emergency Lighting > FT # 1914, CUN-MCO. WHILE WORKING EMERGENCY LIGHT TEST ON WKLY FOUND ALL FWD EMERGENCY LIGHTS INOP; FOUND 10WL ESPU BATTERY DEAD. R & R BATTERY AND OPS TEST NORMAL IAW AMM 33-51-38. - [SDR YENA201909260553](https://openairdocs.org/sdr/YENA201909260553.md): Battery · discharged · Sep 26, 2019 · N645JB · Airbus A320232 · Emergency Lighting > FT # 1914, CUN-MCO. WHILE WORKING EMERGENCY LIGHT TEST ON WKLY FOUND EMERGENCY EXIT ROW LIGHTS BLINKING AND SOME OFF; FOUND 11WL ESPU BATTERY DEAD. R&R BATTERY AND OPS TEST NORMAL IAW AMM 33-51-38. - [SDR YENA201803080903](https://openairdocs.org/sdr/YENA201803080903.md): Skin Panel · debonded · Mar 8, 2018 · N645JB · Airbus A320232 · Rudder, Plate/Skin > AT C6 CHECK LCQ DATED 02/18, DURING RUDDER INSPECTION PER TC A320-55-40-00-210-001, DISBOND DAMAGE WAS FOUND ON THE RUDDER P/N D5547100400000 S/N TS4250 LT SIDE SIDE SHELL SKIN PANEL AT THE LOWER FORWARD NR 2 HOIST POINT. SEE REF /2/ FOR EXACT LOCATION AND DAM - [SDR YENA201803080410](https://openairdocs.org/sdr/YENA201803080410.md): Door Sill · corroded · Mar 8, 2018 · N645JB · Airbus A320232 · Fuselage Miscellaneous Structure > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN R2 DOOR SILL PLATE AT FR66 AROUND FASTENER HOLE. REMOVED AND REPLACED R2 SILL ON NR 440462-38634. - [SDR YENA201803080409](https://openairdocs.org/sdr/YENA201803080409.md): Door Sill · corroded · Mar 8, 2018 · N645JB · Airbus A320232 · Fuselage Miscellaneous Structure > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN R2 SILL PLATE HAS CORROSION AT FR 66 +18 STR23R Y-1732; REMOVED AND REPLACED R2 SILL ON NR 440462-38634. - [SDR YENA201803080408](https://openairdocs.org/sdr/YENA201803080408.md): Door Sill · corroded · Mar 8, 2018 · N645JB · Airbus A320232 · Fuselage Miscellaneous Structure > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN R2 SILL PLATE HAS CORROSION AT FR 66 +6 STR23R Y-1732; REMOVED AND REPLACED R2 SILL ON NR 440462-38634. - [SDR YENA201803080407](https://openairdocs.org/sdr/YENA201803080407.md): Door Sill · corroded · Mar 8, 2018 · N645JB · Airbus A320232 · Fuselage Miscellaneous Structure > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN R2 SILL PLATE HAS CORROSION AT FR 68, -Y1732 STR23. REMOVED AND REPLACED AFT CABIN R2 SILL PLATE IAW SRM 51-72-11 & 51-42-11. - [SDR YENA201803080406](https://openairdocs.org/sdr/YENA201803080406.md): Floorbeam · corroded · Mar 8, 2018 · N645JB · Airbus A320232 · Fuselage Main, Floor Beam > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON MAIN CABIN FWD WET AREA FLOORBEAM Y-1732 AT FR 20. REMOVED AND REPLACED MAIN CABIN FWD WET AREA FLOORBEAM Y-1732 AT FR 20 IAW SRM 51-72-11. - [SDR YENA201803080405](https://openairdocs.org/sdr/YENA201803080405.md): Tee Fitting · corroded · Mar 8, 2018 · N645JB · Airbus A320232 · Emergency Exits > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RT AFT EMERGENCY EXIT BOTTOM INNER SECTION. REMOVED AND REPLACED LOWER AFT TEE SECTION IAW SRM 51-72-11 & 51-42-11 AT RT AFT EMERGENCY EXIT DOOR. - [SDR YENA201803080404](https://openairdocs.org/sdr/YENA201803080404.md): Tee Fitting · corroded · Mar 8, 2018 · N645JB · Airbus A320232 · Fuselage Miscellaneous Structure > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON L/H AFT EMERGENCY BOTTOM INNER SECTION. REMOVED AND REPLACED LOWER FORWARD T SECTION IAW SRM 51-72-11 & 51-42-11 AT LT EMERGENCY EXIT DOOR. - [SDR YENA201803080403](https://openairdocs.org/sdr/YENA201803080403.md): Door Sill · corroded · Mar 8, 2018 · N645JB · Airbus A320232 · Fuselage Miscellaneous Structure > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CARGO SILL PLATE HAS CORROSION BETWEEN FR24 AND FR28. REMOVED AND REPLACED FWD CARGO SILL PLATE IAW SRM 51-72-11. - [SDR YENA201803080402](https://openairdocs.org/sdr/YENA201803080402.md): Floorbeam · corroded · Mar 8, 2018 · N645JB · Airbus A320232 · Fuselage Main, Floor Beam > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON MAIN CABIN FWD WET AREA FLOORBEAM Y-1732 FR 20. REMOVED CORROSION, FOUND TO BE BEYOND LIMITS. REMOVED AND REPLACED WEB. - [SDR YENA201803080401](https://openairdocs.org/sdr/YENA201803080401.md): Floorbeam · corroded · Mar 8, 2018 · N645JB · Airbus A320232 · Fuselage Main, Floor Beam > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y-1292 BETWEEN FRV68-69. REMOVED AND REPLACED FLOORBEAM. - [SDR YENA201803080400](https://openairdocs.org/sdr/YENA201803080400.md): Floorbeam · corroded · Mar 8, 2018 · N645JB · Airbus A320232 · Fuselage Main, Floor Beam > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y-1292 FR 66 TO FR 64. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. - [SDR YENA201803080399](https://openairdocs.org/sdr/YENA201803080399.md): Dummy Rail · corroded · Mar 8, 2018 · N645JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON MAIN CABIN FWD. WET AREA DUMMY RAIL Y-81 HAS CORROSION AT FR 16. REMOVED CORROSION, FOUND TO BE BEYOND SRM LIMITS. REMOVED AND REPLACED DUMMY RAIL. - [SDR YENA2018100280398](https://openairdocs.org/sdr/YENA2018100280398.md): Dummy Rail · corroded · Mar 8, 2018 · N645JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON DUMMY RAIL AT Y580 AT FR 16; REMOVED AND REPLACED DUMMY RAIL IAW SRM 51-72-11& 51-42-11. REF NR 440462-38625. - [SDR YENA2018100280397](https://openairdocs.org/sdr/YENA2018100280397.md): Floorbeam · corroded · Mar 8, 2018 · N645JB · Airbus A320232 · Fuselage Main, Floor Beam > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM Y254 HAS CORROSION AT 16+6; REMOVED AND REPLACED FLOORBEAM. REF. LCQ NR 440462-38626. - [SDR YENA2018100280396](https://openairdocs.org/sdr/YENA2018100280396.md): Shear Web · corroded · Mar 8, 2018 · N645JB · Airbus A320232 · Fuselage Miscellaneous Structure > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FR69-FR70 RT SHEAR WEB; REMOVED AND REPLACED SHEAR WEB IAW SRM 51-73-11 SHEET 1. WORK ACCOMPLISHED ON NR 440462/38631. - [SDR YENA201803080129](https://openairdocs.org/sdr/YENA201803080129.md): Skin · debonded · Mar 8, 2018 · N645JB · Airbus A320232 · Rudder, Plate/Skin > DURING HEAVY MAINTENANCE, THE LT SIDE OF RUDDER WAS FOUND DISBONDED AT LOWER FORWARD NR 2 HOISTING POINT FROM 2 O'CLOCK TO 6 O'CLOCK POSITION EXTENDING AFT. REPAIRED IAW TD 80422 4941-005-2018A, AND EC A18-145-01. - [SDR YENA201803080128](https://openairdocs.org/sdr/YENA201803080128.md): Skin · damaged · Mar 8, 2018 · N645JB · Airbus A320232 · Fuselage Main, Plate/Skin > DURING HEAVY MAINTENANCE, FUSELAGE SKIN HAD A DENT WITH 2 GOUGES AT FRAME 23 + 10, STRINGERS 42-43R. REPAIRED IAW SRM 53-00-11-300-029, PARA 2(A)(3), & 53-00-11-300-029 PARA 2(A)(7-17). - [SDR YENA201710070830](https://openairdocs.org/sdr/YENA201710070830.md): Lens · missing · Oct 7, 2017 · N645JB · Airbus A320232 · Emergency Lighting > SEAT 9D EMERGENCY LIGHT LENS MISSING. REPLACED THE LENS IAW AMM 33-50-00. - [SDR YENA201710020812](https://openairdocs.org/sdr/YENA201710020812.md): Battery Pack · no test · Oct 2, 2017 · N645JB · Airbus A320232 · Emergency Lighting > EMERGENCY LIGHTS FAILED TO TEST. R & R THE BATTERY PACK AT FIN 13WL IAW AMM 33-51-38. - [SDR YENA201706290543](https://openairdocs.org/sdr/YENA201706290543.md): Coffeemaker · odor · Jun 29, 2017 · N645JB · Airbus A320232 · Buffet/Galleys > DIVERTED DUE TO AN ELECTRICAL ODOR REPORTED AROUND THE FORWARD COFFEE POTS AND GALLEY AREA. FOLLOWED FLOW CHART FOR SMOKE EVENT. FOLLOWED TSM 24-00-00-810-823-A. CAUSE OF SMOKE FROM FWD COFFEEMAKER. - [SDR YENA20160919819](https://openairdocs.org/sdr/YENA20160919819.md): Seat Track · corroded · Sep 19, 2016 · N645JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK FRAME 16 Y 254, CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11 - [SDR YENA20160919818](https://openairdocs.org/sdr/YENA20160919818.md): Seat Track · corroded · Sep 19, 2016 · N645JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK Y1292 FRAME 16 CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11. - [SDR YENA20160919817](https://openairdocs.org/sdr/YENA20160919817.md): Web · corroded · Sep 19, 2016 · N645JB · Airbus A320232 · Fuselage Miscellaneous Structure > LEFT OUTBOARD WEB FRAME 12 STRINGER 23 CORRODED. REPLACED WEB IAW SRM 51-72-11 - [SDR YENA20160919816](https://openairdocs.org/sdr/YENA20160919816.md): Dummy Rail · corroded · Sep 19, 2016 · N645JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings > DUMMY TRACK Y503 FRAMES 12-16 CORRODED. REMOVED AND REPLACED THE DUMMY TRACK IAW SRM 51-42-11 AND SRM 51-72-11. - [SDR YENA20160322253](https://openairdocs.org/sdr/YENA20160322253.md): Switch · malfunctioned · Mar 22, 2016 · N645JB · Airbus A320232 · Emergency Lighting > RETURNED TO GATE. EMERGENCY LIGHTS WILL NOT EXTINGUISH. ACCOMPLISHED TROUBLESHOOTING IAW 33-51-00-810-881-A, R & R EMERGENCY EXIT LIGHT SWITCH FIN 33LP AND EMERGENCY EXIT LIGHT RELAY 8WL IAW ESPM 20-45-00, ALL OPS CHECK NORMAL IAW 33-51-00. - [SDR YENA20150919430](https://openairdocs.org/sdr/YENA20150919430.md): Battery · no test · Sep 22, 2015 · N645JB · Airbus A320232 · Emergency Lighting > DURING MAINTENANCE, AFT EMERGENCY BATTERY FAILED CAPACITY CHECK. R & R AFT LT EMERGENCY BATTERY PACK IAW AMM 33-51-38. OPS CHECK GOOD. - [SDR YENA20141028234](https://openairdocs.org/sdr/YENA20141028234.md): Control Valve · failed · Oct 28, 2014 · N645JB · Airbus A320232 · Cabin Cooling System > AIR RETURN DUE TO CABIN TEMP FULL HOT. UNABLE TO CONTROL NR 1 PACK VALVE. INDICATED FULL OPEN AND HOT NO ECAM PRESENT. R & R 1 FLOW CONTROL VALVE, PERFORMED OPS CK + BITE TEST NO FAULTS NOTED AMM 21-51-51. - [SDR YENA20121124652](https://openairdocs.org/sdr/YENA20121124652.md): Epsu · failed · Nov 24, 2012 · N645JB · Airbus A320232 · Emergency Lighting > FLT 55 BTV-JFK, CREW REPORTED EMERGENCY LIGHT ON SIDE OF SEAT 8D BROKEN. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 12WL AS PER MM 33-51-38. OPS CHECK NORMAL. - [SDR YENA20121106635](https://openairdocs.org/sdr/YENA20121106635.md): Terminal · defective · Nov 6, 2012 · N645JB · Airbus A320232 · Emergency Lighting > FLT 153 JFK-MCO, ON GROUND MAINTENANCE CHECK FOUND ROW 11D EMERGENCY EXIT LIGHT IS INOP. REPLACED EMERGENCY LIGHT MODULE TERMINAL. SYSTEM OPS CHECK NORMAL. - [SDR YENA20120413478](https://openairdocs.org/sdr/YENA20120413478.md): Light · inoperative · Apr 13, 2012 · N645JB · Airbus A320232 · Emergency Lighting > FLT 152 MCO-JFK, ON GROUND CHECK FOUND EMERGENCY LIGHT AT 11D INOP. RELAMPED OPS CHECK. Next page: https://openairdocs.org/aircraft/N645JB/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 = 'N645JB' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N645JB/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.