# Service difficulty reports: N644JB

A list on [N644JB](https://openairdocs.org/aircraft/N644JB.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 · 51 reports

- [SDR YENA2026081700688](https://openairdocs.org/sdr/YENA2026081700688.md): Unknown · fumes · Aug 15, 2026 · N644JB · Airbus A320232 · Air Distribution System
  > FLT 2584, MCO- JFK. FUMES AT ENG START, TAXI, & T/O, APPLIED FUMES PROCEDURES TO DISIPATE WITH PACK 2 OFF.
- [SDR YENA2026080300647](https://openairdocs.org/sdr/YENA2026080300647.md): A/C Pack · odor · Aug 2, 2026 · N644JB · Airbus A320232 · Cabin Cooling System
  > FLT 545, ISP-PBI. LEVEL 2 FUMES EVENT ON DESCENT START AS A MILD DIRTY SOCK SMELL THEN AS A ALT GOT LOWER AND PACKS WHERE ON HP VALVES IN SWITCH TO A STRONG DIRTY SOCK SMELL BOTH PACKS TRIED TOO ISOLATE WHICH PACK BUT SEEMS TO BE BOTH PACKS O2 MASK WERE USED
- [SDR YENA2026070700518](https://openairdocs.org/sdr/YENA2026070700518.md): Unknown · odor · Jul 2, 2026 · N644JB · Airbus A320232 · Air Distribution System
  > FLT # 438, MCO-BDL. ON DESCENT FROM 6,000 FT TO 2500 FT STRONG DIRTY SOCK SMELL IN THE FLIGHT DECK. WE DID DESCENDED THROUGH SOME CLOUDS AND THAT IT WAS VERY HOT IN BDL 98F. FLIGHT ATTENDANTS REPORTED NOT SMELLING IT; C/W INFORMATION NOTICE 2017-T015 STEP 1
- [SDR YENA2026030200246](https://openairdocs.org/sdr/YENA2026030200246.md): Unknown · odor · Mar 1, 2026 · N644JB · Airbus A320232 · Air Distribution System
  > FLT #405 EWR-FLL. "ON DESCENT @ APPROX 10,000 FT ENGINES AT IDLE, APU OFF MAGIC MARKER ODOR IN FLIGHT DECK, DIMINISHED WITH PACK 1 OFF PER PROCEDURE RETURNED W/ PACK ON.;COMPLIED WITH INFORMATION NOTICE 2017-T015, STEP 1, ISOLATED FAULT TO TYPE 10 MISCELLANEO
- [SDR YENA2025070700682](https://openairdocs.org/sdr/YENA2025070700682.md): Motor · failed · Jul 5, 2025 · N644JB · Airbus A320232 · Trailing Edge Flap Actuator
  > FLT#302, FLL-JFK. (AN EMERGENCY WAS DECLARED) "FLAPS FAULT-ON CLIMB OUT F/CTL FLAP SYS 1 FAULT ON APPROACH F/CTL FLAPS FAULT SLATS EXTENDED TO POSITION 2 FLAPS DID NOT EXTEND AND STAYED AT ZERO. LANDED IN THAT CONFIGURATION @ 157 KTS. BRAKES STAYED BELOW 300 D
- [SDR YENA2024120201521](https://openairdocs.org/sdr/YENA2024120201521.md): Battery · failed · Dec 1, 2024 · N644JB · Airbus A320232 · Emergency Lighting
  > FLT#2752, SJU-TPA. 'EPSU BATTERY 12WL FAILED TEST; REMOVED AND REPLACED EPSU BATTERY AT 12WL IAW AMM 33-51-38.'
- [SDR YENA2024120201520](https://openairdocs.org/sdr/YENA2024120201520.md): Battery · inoperative · Dec 1, 2024 · N644JB · Airbus A320232 · Emergency Lighting
  > FLT#2752, SJU-TPA. 'EPSU BATTERY 11WL FAILED TEST; REMOVED AND REPLACED EPSU BATTERY AT 11WL IAW AMM 33-51-38.'
- [SDR YENA2024052100768](https://openairdocs.org/sdr/YENA2024052100768.md): Computer · unknown · May 17, 2024 · N644JB · Airbus A320232 · Door Warning System
  > FLT#1133, MCO-SJU. 'REPEAT WRITE-UP! RIGHT OVERWING EXIT SHOWS NOT ARMED IN FLIGHT, SHOWED ARMED ON THE GROUND; REMOVED AND REPLACED #2 SDAC IAW AMM 31-55-34. OPS CHECK NORMAL. PERFORMED PRESS. CHECK REF. AMM 05-53-00. NO FAULTS NOTED. A/C OK TO CONT. SVC.
- [SDR YENA2023122101626](https://openairdocs.org/sdr/YENA2023122101626.md): Unknown · unknown · Dec 19, 2023 · N644JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENACE: CRACK INDICATION FOUND IN OPEN INBOARD LOWER HOLE FROM DOOR STOP FITTIING #7, RH FRAME 16; CRACK DIRECTION: 6 O'CLOCK; D1-D2= 0.125 INCH; REF AEROMAN WO 2023 360/1 N/R 2023-692459, PERFORMED REPAIR ON FRAME 16 RH LOCATED INBOARD LOWER
- [SDR YENA2023122101625](https://openairdocs.org/sdr/YENA2023122101625.md): Unknown · unknown · Dec 19, 2023 · N644JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENACE: CRACK INDICATION FOUND IN OPEN UPPER HOLE FROM DOOR STOP FITTING #7; R H FRAME 16; CRACK DIRECTION: 6 CLOCK; D1-D2= 0.095 INCH; REF AERMAN WO 2023 360/1 N/R 2023-692458, PERFORMED REPAIR ON FRAME 16 RH LOCATED UPPER HOLE FROM DOOR STOP
- [SDR YENA2023122101624](https://openairdocs.org/sdr/YENA2023122101624.md): Unknown · unknown · Dec 19, 2023 · N644JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENACE: CORROSION ANGLE WEB FLOOR STRUCTURE BTW FR69/FR70 AT LEVEL STR23R AFT GALLEY AREA (1 EA) (CPCP RELATED REFER TO MPD TASK 534195-01); REF AEROMAN N/R 2023-692365 WO 2023 360/1, REMOVED AND REPLACED WEB LOC ON FLOOR STRUCTURE BETWEEN FR6
- [SDR YENA2023122101623](https://openairdocs.org/sdr/YENA2023122101623.md): Unknown · unknown · Dec 19, 2023 · N644JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENACE: CORROSION ANGLE WEB FLOOR STRUCTURE BTW FR69/FR70 AT LEVEL STR23L AFT GALLEY AREA (1 EA) (CPCP RELATED REFER TO MPD TASK 534195-01); REF AEROMAN NR 2023-692366 WO 2023 360/1, REMOVED AND REPLACED WEB LOC ON FLOOR STRUCTURE BETWEEN FR69
- [SDR YENA2022042700416](https://openairdocs.org/sdr/YENA2022042700416.md): Frame · cracked · Apr 22, 2022 · N644JB · Airbus A320232 · Emergency Exits
  > DURING HEAVY MAINTENANCE, CRACK INDICATIONS WERE FOUND IN FRAME SEGMENT 1 (I/B AND O/B POSITIONS) AT THE OVERWING EMERGENCY EXIT HATCH (AFT LH EER DOOR 834) L= 0.157 INCH APPROX; REF: ARM W/O 2022 3/1 N/R 2022-163379 EMP# 8610118 CHECKED BY 8603209 PERFORMED R
- [SDR YENA2022042700415](https://openairdocs.org/sdr/YENA2022042700415.md): Frame · cracked · Apr 22, 2022 · N644JB · Airbus A320232 · Emergency Exits
  > DURING HEAVY MAINTENANCE, CRACK INDICATIONS WERE FOUND IN FRAME SEGMENT 1 (I/B AND O/B POSITIONS) AT THE OVERWING EMERGENCY EXIT HATCH (FWD LH EEH DOOR 833) L= 0.152 INCH APPROX; REF: ARM W/O 2022 3/1 N/R 2022-163378 EMP# 8610118 CHECKED BY 8603209 REFORMED RE
- [SDR YENA2022042700414](https://openairdocs.org/sdr/YENA2022042700414.md): Frame · cracked · Apr 22, 2022 · N644JB · Airbus A320232 · Emergency Exits
  > DURING HEAVY MAINTENANCE, CRACK INDICATIONS WERE FOUND IN FRAME SEGMENT 1 (I/B AND O/B POSITIONS) AT THE OVERWING EMERGENCY EXIT HATCH (FWD RH EEH DOOR 843) L= 0.236 INCH APPROX; REF: ARM W/O 2022 3/1 N/R 2022-163377 EMP#86101118 CHECKED BY 8603209 PERFORMED R
- [SDR YENA2022042700413](https://openairdocs.org/sdr/YENA2022042700413.md): Frame · cracked · Apr 22, 2022 · N644JB · Airbus A320232 · Emergency Exits
  > DURING HEAVY MAINTENANCE, CRACK INDICATIONS WERE FOUND IN FRAME SEGMENT 1 (I/B AND O/B POSITIONS) AT THE OVERWING EMERGENCY EXIT HATCH (AFT RH EEH DOOR 844) L= 0.232 INCH APPROX; REF: ARM W/O 2022 3/1 N/R 2022-163377 EMP# 8610118 CHECKED BY 8603209 PERFORMED R
- [SDR YENA2022042700412](https://openairdocs.org/sdr/YENA2022042700412.md): Shear Tie · corroded · Apr 22, 2022 · N644JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOC BTW STR 43R AND STR 44 AT LEVEL OF FRAME 33 IN FWD CARGO COMPARTMENT; REF: ARM W/0 2022 3/1 N/R 2022-163466 EMP# 901069 CHECKED BY 8601415 REMOVED AND REPLACED CLEAT IAW A320 SRM 51-72-11 AND DWG D53232542000 A
- [SDR YENA2022042700411](https://openairdocs.org/sdr/YENA2022042700411.md): Shear Tie · corroded · Apr 22, 2022 · N644JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOC. BTW STR 43R AND STR 44 AT LEVEL OF FRAME 32 IN FWD CARGO COMPARTMENT; REF: ARM W/O 2022-3/1 2022-163468 REMOVED AND REPLACED CLEAT IAW A320 SRM 51-72-11 AND DWG D53232542000 AND E53231060.
- [SDR YENA2022042700410](https://openairdocs.org/sdr/YENA2022042700410.md): Shear Tie · corroded · Apr 22, 2022 · N644JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOC. BTW STR 43R AND STR44 LEVEL OF FRAME 33 IN FWD CARGO COMPARTMENT; REF: ARM W/O 2022 3/1 R/R 2022-163466 REMOVED AND REPLACED CLEAT IAW A320 SRM 51-72-11 AND DWG D53232542000 AND E53231062.
- [SDR YENA2022042700409](https://openairdocs.org/sdr/YENA2022042700409.md): Shear Tie · corroded · Apr 22, 2022 · N644JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOC BTW STR 43L AND STR 44 AT LEVEL OF FRAME 31 IN FWD CARGO COMPARTMENT; REF: ARM W/O 2022 3/1 N/R 2022-163473 REMOVED AND REPLACED CLEAT IAW A320 SRM 51-72-11 AND DWG D53232542000 AND E53231058.
- [SDR YENA2022042700408](https://openairdocs.org/sdr/YENA2022042700408.md): Shear Tie · corroded · Apr 22, 2022 · N644JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOC BTW STR 42R AND STR 43R AT LEVEL OF FRAME 29 IN FWD CARGO COMPARTMENT; REF: ARM W/O 2022 3/1 NR 2022-0163472 REMOVED AND REPLACED CLEAT IAW A320 SRM 51-72-11, SRM 51-42-11, DWG D53232542000 AND DWG D53230319000
- [SDR YENA2022042700407](https://openairdocs.org/sdr/YENA2022042700407.md): Shear Tie · corroded · Apr 22, 2022 · N644JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOC. BTW STR 43L AND STR 44 AT LEVEL OF FRAME 32 IN FWD CARGO COMPARTMENT; REF: ARM 2022 3/1 N/R 2022-163469 REMOVED AND REPLACED CLEAT IAW A320 SRM 51-72-11 AND DWG D53232542000 AND E53231060.
- [SDR YENA2022042700406](https://openairdocs.org/sdr/YENA2022042700406.md): Shear Tie · corroded · Apr 22, 2022 · N644JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOC BTW STR 43R AND STR 44 AT LEVEL OF FRAME 32 IN FWD CARGO COMPARTMENT; REF: ARM W/O 2022 3/2 N/R 2022-163468 REMOVED AND REPLACED CLEAT IAW A320 SRM 51-72-11 AND DWG D53232542000 AND E53231060.
- [SDR YENA2022042700405](https://openairdocs.org/sdr/YENA2022042700405.md): Frame · none · Apr 22, 2022 · N644JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, REF JB A5109057-04-JB. AGING AIRCRAFT PROGRAM. EXITING REPAIR EVALUATION LOC FR27 TO FR28 BTW STR 38R TO 42R AT LOWER FUSELAGE; REF AEROMAN WO 2022 3/1, NR 2022-163236. PERFORMED PERM REPAIR IAW JB EC A22-258-01.
- [SDR YENA2022042700404](https://openairdocs.org/sdr/YENA2022042700404.md): Doubler · damaged · Apr 22, 2022 · N644JB · Airbus A320232 · Fuselage Floor Panel
  > DURING HEAVY MAINTENANCE, ( A22-258-01) FUSELAGE / FWD FUSELAGE / FR 27-28 & STR 38R-42R / EXISTING DOUBLER REPAIR – PERMANENT APPROVAL FOR WV 17. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2021121300835](https://openairdocs.org/sdr/YENA2021121300835.md): Receiver · failed · Dec 11, 2021 · N644JB · Airbus A320232 · Flight Management Computing Hardware System
  > FLT 1239, LAS-CUN(DIVERTED TO TPA). GPS PRIMARY LOST IN FLIGHT; T/S PER TSM 34-52-00-810-847-A. MMR 1& 2 TEST GOOD. ATC 1 & 3 TEST GOOD. GPS VISIBILITY GOOD. R&R MMR1 AS PRECAUTION IAW AMM 34-36-31. BITE TEST GOOD. NO FAULTS NOTED @ THIS TIME
- [SDR YENA2020102600499](https://openairdocs.org/sdr/YENA2020102600499.md): Battery · failed · Oct 20, 2020 · N644JB · Airbus A320232 · Emergency Lighting
  > FLT 1382, IAH-JFK. PER TASK CARD A320-33-51-00-710-003 PERFORMED TEST ESPU BATTER FIN 13WL AFT FAIL. R & R ESPU BATTERY AT FIN 13WL AFT, IAW AMM 33-51-38.
- [SDR YENA2020102600498](https://openairdocs.org/sdr/YENA2020102600498.md): Battery · failed · Oct 20, 2020 · N644JB · Airbus A320232 · Emergency Lighting
  > FLT 1382, IAH-JFK. PER TASK CARD A320-33-51-00-710-003 PERFORMED TEST ESPU BATTERY FIN 10WL FWD FAIL. R & R ESPU BATTERY AT FIN 10WL FWD, IAW AMM 33-51-38. OPERATIONS CHECK GOOD.
- [SDR YENA201907270425](https://openairdocs.org/sdr/YENA201907270425.md): Shear Plate · cracked · Jul 27, 2019 · N644JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, REPORTED THAT DURING THE ACCOMPLISHMENT OF THE REF /3/ SB FOR INSPECTION OF THE TI- ANGLES BETWEEN THE BELLY FAIRING & KEEL BEAM SIDE PANEL (AS REQUIRED BY THE REF /4/ AD)– THAT ON THE RT SIDE THE TI-ANGLE AT FR 41-42 AND SHEAR PLATE
- [SDR YENA201905080268](https://openairdocs.org/sdr/YENA201905080268.md): Unknown · malfunctioned · May 8, 2019 · N644JB · Airbus A320232 · Fuel Transfer Valve
  > FLT 170, FLL-BOS. DIVERTED TO JFK. OUTER TANK TO INNER TANK TRANSFER VALVE INOP ( INTER CELL TRANSFER VALVES-LH WING-BOTH LATCH CLOSED); PERFORMED OPERATIONAL TEST OF INDIVIDUAL TRANSFER VALVES IAW AMM 28-15-00-710-002A WITH NO FAULTS NOTED. ALL INTERCELL TRA
- [SDR YENA2018101240681](https://openairdocs.org/sdr/YENA2018101240681.md): Battery · failed · Oct 4, 2018 · N644JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, EPSU BATRERY PACKS 10WL, 11WL, 12WL, 13WL FAILED OPERATIONAL CHECK; REF IAC N/R 13147-5802, R&R EPSU BATTERIES IAW AMM TASK 33-51-38-000-002, 33-51-38-400-002 OPS CHECK GOOD. 10WL: P/N OFF & ON 3214-31, S/N OFF 781924, S/N ON 811574
- [SDR YENA2018101240680](https://openairdocs.org/sdr/YENA2018101240680.md): Battery · failed · Oct 4, 2018 · N644JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, EPSU BATRERY PACKS 10WL, 11WL, 12WL, 13WL FAILED OPERATIONAL CHECK; REF IAC N/R 13147-5802, R&R EPSU BATTERIES IAW AMM TASK 33-51-38-000-002, 33-51-38-400-002 OPS CHECK GOOD. 10WL: P/N OFF & ON 3214-31, S/N OFF 781924, S/N ON 811574 1
- [SDR YENA2018101240679](https://openairdocs.org/sdr/YENA2018101240679.md): Battery · failed · Oct 4, 2018 · N644JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, EPSU BATRERY PACKS 10WL, 11WL, 12WL, 13WL FAILED OPERATIONAL CHECK; REF IAC N/R 13147-5802, R&R EPSU BATTERIES IAW AMM TASK 33-51-38-000-002, 33-51-38-400-002 OPS CHECK GOOD. 10WL: P/N OFF & ON 3214-31, S/N OFF 781924, S/N ON 811574
- [SDR YENA2018101240678](https://openairdocs.org/sdr/YENA2018101240678.md): Battery · failed · Oct 4, 2018 · N644JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, EPSU BATRERY PACKS 10WL, 11WL, 12WL, 13WL FAILED OPERATIONAL CHECK; REF IAC N/R 13147-5802, R&R EPSU BATTERIES IAW AMM TASK 33-51-38-000-002, 33-51-38-400-002 OPS CHECK GOOD. 10WL: P/N OFF & ON 3214-31, S/N OFF 781924, S/N ON 811574
- [SDR YENA201711210958](https://openairdocs.org/sdr/YENA201711210958.md): Door Sill · corroded · Nov 21, 2017 · N644JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BULK CARGO DOOR LOWER SILL FRAME 61 + 19. REPAIRED THE DOOR SILL IAW EC A17-1084-01.
- [SDR YENA201711210957](https://openairdocs.org/sdr/YENA201711210957.md): Door Sill · corroded · Nov 21, 2017 · N644JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BULK CARGO DOOR LOWER SILL FR 61 + 9"; REPAIRED SILL IAW EC A17-1084-01.
- [SDR YENA201711210956](https://openairdocs.org/sdr/YENA201711210956.md): Door Sill · corroded · Nov 21, 2017 · N644JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BULK CARGO DOOR SILL FRAME 61 TO 62. REPAIRED THE DOOR SILL IAW EC A17-1084-01.
- [SDR YENA201711210955](https://openairdocs.org/sdr/YENA201711210955.md): Seat Track · corroded · Nov 21, 2017 · N644JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED THE SEAT TRACK, FR 44 + 12, -Y765. REPLACED THE SEAT TRACK IAW SRM 51-72-11.
- [SDR YENA201711210954](https://openairdocs.org/sdr/YENA201711210954.md): Dummy Rail · corroded · Nov 21, 2017 · N644JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE DUMMY RAIL Y503.2, FRAME 16 IN THE FWD GALLEY AREA. REPLACED THE DUMMY RAIL.
- [SDR YENA20160927875](https://openairdocs.org/sdr/YENA20160927875.md): Connector · disconnected · Sep 27, 2016 · N644JB · Airbus A320232 · Light System Wiring
  > FLT 365 SMF-LGB. DURING A MAINTENANCE INSPECTION, THE OVERHEAD EMERGENCY LIGHT WAS DISCOVERED TO BE INOPERATIVE AT ROW 18. LIGHT ASSEMBLY WAS FOUND TO BE DISCONNECTED. REINSTALLED CONNECTOR, OPS CHECK PASSED. SUPPLEMENTAL INFORMATION TO FOLLOW.
- [SDR YENA20160208106](https://openairdocs.org/sdr/YENA20160208106.md): Battery · no test · Feb 8, 2016 · N644JB · Airbus A320232 · Emergency Lighting
  > FORWARD LT EMERGENCY LIGHT BATTERY FAILED CAP TEST. REPLACED BATTERY FIN 10WL IAW AMM 33-50-00, GROUND CHECKS OK.
- [SDR YENA20151026521](https://openairdocs.org/sdr/YENA20151026521.md): Battery Pack · failed · Oct 26, 2015 · N644JB · Airbus A320232 · Emergency Lighting
  > DURING WEEKLY CHECK, EMERGENCY LIGHTS ON RT OVERWING EXIT FAILED. REMOVED RT SIDE OVERWING BATTERY ON THE EPSU AND PERFORMED OPS TEST IAW 33-51-38.
- [SDR YENA20150325060](https://openairdocs.org/sdr/YENA20150325060.md): Wire Harness · damaged · Mar 25, 2015 · N644JB · Airbus A320232 · Light System Wiring
  > ON MAINTENANCE CHECK FOUND ROW 1 ABC EMERGENCY LIGHT INOPERATIVE. R & R HARNESS TO LIGHT ASSY IAW AMM 33-51-19. OPS CHECK GOOD.
- [SDR YENA20140930209](https://openairdocs.org/sdr/YENA20140930209.md): Computer · failed · Sep 30, 2014 · N644JB · Airbus A320232 · Trailing Edge Flap Control System
  > FLIGHT CONTROL FLAPS LOCKED WING TIP BRAKE ON DESCENT. R & R APU AND PERFORMED CHECKS IAW AMM 27-51-00, OPS CHECKED NORMAL.
- [SDR YENA20140910186](https://openairdocs.org/sdr/YENA20140910186.md): Flap System · malfunctioned · Sep 10, 2014 · N644JB · Airbus A320232 · Trailing Edge Flap Control System
  > DURING FINAL APPROACH, SELECTED FLAPS 2 AND RECEIVED A F/CTRL FLAPS LOCKED WING TIP BRAKE ON ECAM. ACCOMPLISHED FLAPS/SLATS SYS RESET IAW AMM 27-50-00. NO FAULTS NOTED ON FLAP/SLATS, OPS CHECK NORMAL.
- [SDR YENA20140724191](https://openairdocs.org/sdr/YENA20140724191.md): Slide · misrepaired · Jul 24, 2014 · N644JB · Airbus A320232 · Escape Slide
  > DISCREPANCY ON THE OVERWING SLIDE. DURING THE SCHEDULED RESTORATION OF OVERWING SLIDE, IT WAS FOUND THAT A VACUUM ADAPTER TOOL WAS STILL ATTACHED TO THE SLIDE ASPIRATOR. TOOL SHOULD HAVE BEEN REMOVED DURING THE FOLDING/PACKING PROCESS.
- [SDR YENA20120216440](https://openairdocs.org/sdr/YENA20120216440.md): Release Cable · failed · Feb 16, 2012 · N644JB · Airbus A320232 · Escape Slide
  > ON HEAVY MAINTENANCE CHECK FOUND LT EMERGENCY EXIT SLIDE RELEASE CABLE FAILED OPS CHECK. REPLACED CABLE AS PER TASK CARD A320-53-1227-01.
- [SDR YENA20120216439](https://openairdocs.org/sdr/YENA20120216439.md): Release Cable · failed · Feb 16, 2012 · N644JB · Airbus A320232 · Escape Slide
  > ON HEAVY MAINTENANCE CHECK FOUND RT EMERGENCY EXIT SLIDE RELEASE CABLE FAILED OPS CHECK. REPLACED CABLE AS PER TASK CARD A320-1227-02.
- [SDR YENA20120116413](https://openairdocs.org/sdr/YENA20120116413.md): Pressure Switch · leaking · Jan 16, 2012 · N644JB · Airbus A320232 · Hydraulic System, Main
  > FLT 830 SDQ-JFK, CREW DECLARED EMERGENCY AND AIRCRAFT DIVERTED TO SJU DUE TO AT CRUISE OF 34000, RECEIVED A GREEN HYD RESERVOIR LEVEL LOW ECAM INDICATING A LOSS OF GREEN HYD FLUID. THE TECHNICIAN REMOVED AND REPLACED NR 1 ENGINE HYD PRESSURE SWITCH IAW AMM 29
- [SDR YENA2007034](https://openairdocs.org/sdr/YENA2007034.md): Control Handle · damaged · May 14, 2007 · N644JB · Airbus A320232 · Landing Gear Selector
  > FLT 61, AFTER TAKEOFF SYR TO JFK, GEAR FAILED TO RETRACT. GEAR HANDLE WOULD NOT MOVE. GEAR HANDLE PANEL DISPLACED OUT APPRROX.5 INCH. ACCOMPLISHED TSM 32-31-00-30-885. LANDING GEAR RETRACTION/EXTENSION DONE 4 TIMES. NO FAULT NOTED. NO FAULT FOUND ON PFR

Next page: https://openairdocs.org/aircraft/N644JB/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 = 'N644JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N644JB/reports

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