# Service difficulty reports: N768JB

A list on [N768JB](https://openairdocs.org/aircraft/N768JB.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 · 53 reports

- [SDR YENA2026041700408](https://openairdocs.org/sdr/YENA2026041700408.md): Pbe · failed insp · Apr 16, 2026 · N768JB · Airbus A320232 · Emergency Equipment
  > FLT#399, LGA-MCO. "PER EC 353000-05-1 AFT FA PBE FAILED INSPECTION; REMOVED AND REPLACED AFT FA PBE AS REQUIRED.
- [SDR YENA2025070800707](https://openairdocs.org/sdr/YENA2025070800707.md): Door Frame · cracked · Jul 5, 2025 · N768JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE H1 AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTIONS ARE 6 AND 12 OCLOCK, CRACK D EPTH IS 0.115 INCH APPROX, AT FWD GALLEY AREA (2 EA); REF AEROMAN NR 2025-315768 WO 2025 177/
- [SDR YENA2025070800706](https://openairdocs.org/sdr/YENA2025070800706.md): Door Frame · cracked · Jul 5, 2025 · N768JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE H3 AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION IS 3OCLOCK, CRACK DEPTH IS 0.120 INCH APPROX, AT FWD GALLEY AREA (1 EA); REF AEROMAN NR 2025-315769 WO 2025 177/1 PERFORME
- [SDR YENA2025070800705](https://openairdocs.org/sdr/YENA2025070800705.md): Door Frame · cracked · Jul 5, 2025 · N768JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE IN OPEN FASTENER HOLE H1 AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION IS 7 OCLOCK, CRACK DEPTH IS 0.080 INCH APPROX, AT FWD GALLEY AREA (1 EA); REF AEROMAN NR 2025-315766 WO 2025 177/1 REMOVED
- [SDR YENA2025070800704](https://openairdocs.org/sdr/YENA2025070800704.md): Door Frame · cracked · Jul 5, 2025 · N768JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE IN OPEN FASTENER HOLE H3 AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTIONS ARE 6 AND 9 OCLOCK, CRACK DEPTH IS 0.085 INCH APPROX, AT FWD GALLEY AREA (2 EA); REF AEROMAN NR 2025-315767 WO 177/1 REMOV
- [SDR YENA2025070800703](https://openairdocs.org/sdr/YENA2025070800703.md): Door Frame · cracked · Jul 5, 2025 · N768JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE H2 AT CROS SBEAM SPLICING AREA, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.11 2 INCH, AT FWD GALLEY AREA (1 EA); PERFORMED PERMANENT REPAIR ON FRAME 16 LH SIDE HOLE H2 AT
- [SDR YENA2025070800702](https://openairdocs.org/sdr/YENA2025070800702.md): Dummy Rail · corroded · Jul 5, 2025 · N768JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE: CORROSION RAIL DUMMY Y503.2 LOC. BTW FR12/FR16 FWD GALLEY AREA (1 EA) (CPCP FINDING); (RESOLVED ON W/O: 1381843 TASKCARD: NR-00038) REF AEROMAN NR 2025-315823 WO 2025 177/1 REMOVED AND REPLACED RAIL DUMMY Y503.2 LOC. BTW FR12/FR16 FWD
- [SDR YENA2025070800701](https://openairdocs.org/sdr/YENA2025070800701.md): Floor Support · corroded · Jul 5, 2025 · N768JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CORROSION FLOOR SUPPORT -Y1292 LOC. BTW FR12/FR24 FWD GALLEY AREA (1 EA) (CPCP FINDING); (RESOLVED ON W/O: 1381843 TASKCARD: NR-00039) REF AEROMAN NR 2025-315824 WO 2025 177/1 REMOVED AND REPLACED FLOOR BEAM -Y1292 AND FASTENERS LOCAT
- [SDR YENA2025070800700](https://openairdocs.org/sdr/YENA2025070800700.md): Frame · cracked · Jul 5, 2025 · N768JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOARD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 1 OCLOCK, CRAC K DEPTH IS 0.110 INCH, AT AFT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1381843 TASKCARD: NR-00040
- [SDR YENA2025070800699](https://openairdocs.org/sdr/YENA2025070800699.md): Floor Support · corroded · Jul 5, 2025 · N768JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CORROSION FLOOR BEAM +Y1292 LOC. BTW FR12/FR24 FWD GALLEY AREA (CPCP FINDING); (RESOLVED ON W/O: 1381843 TASKCARD: NR-00044) REF AEROMAN NR 2025-315816 WO 2025 177/1 INSTALLED NEW FLOOR BEAM Y1292, SPLICE (1E/A) AND FASTENERS LOC. BTW
- [SDR YENA2025070800698](https://openairdocs.org/sdr/YENA2025070800698.md): Floor Support · corroded · Jul 5, 2025 · N768JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CORROSION FLOOR BEAM +Y765 LOC. BTW FR12/FR24 AT FWD GALLEY AREA (1 E A) (CPCP FINDING; (RESOLVED ON W/O: 1381843 TASKCARD: NR-00045) REF AEROMAN NR 2025-315817 WO 2025 177/1 REMOVED AND REPLACED FLOOR BEAM Y765 AND SPLICE (1E/A) LOC
- [SDR YENA2025070800697](https://openairdocs.org/sdr/YENA2025070800697.md): Stringer · corroded · Jul 5, 2025 · N768JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 26R LOCATED FR64 TO FR 65 IN AFT CARGO COMPARTMENT; REF AEROMAN NR 2025-315986 WO 2025 177/1 REMOVED AND REPLACED STRINGER 26R LOC. BTW FR64 TO FR67 IN AFT CARGO COMPARTMENT I.A.W A320 SRM 51-42-11, A320 SRM 51-72-1
- [SDR YENA2025070800696](https://openairdocs.org/sdr/YENA2025070800696.md): Hinge Fitting · corroded · Jul 5, 2025 · N768JB · Airbus A320232 · Vertical Stabilizer
  > DURING HEAVY MAINTENANCE: CORROSION FOUND ON BORE HINGE FITTING 1 OF VERTICAL STABILIZER; REF AEROMAN NR 2025-315970 WO 2025 177/1 REMOVED AND REPLACED HINGE FITTING #1 AND FASTENERS LOCATED VERTICAL STABILIZER IAW A320 SRM 55-3.
- [SDR YENA2025070800695](https://openairdocs.org/sdr/YENA2025070800695.md): Hinge Fitting · corroded · Jul 5, 2025 · N768JB · Airbus A320232 · Vertical Stabilizer
  > DURING HEAVY MAINTENANCE: CORROSION FOUND ON BORE HINGE FITTING 3 OF VERTICAL STABILIZER; REF AEROMAN NR 2025-315971 WO 2025 177/1 REMOVED AND REPLACED HINGE FITTING #3 AND FASTENERS LOCATED VERTICAL STABILIZER IAW A320 SRM 55-36.
- [SDR YENA2025070800694](https://openairdocs.org/sdr/YENA2025070800694.md): Hinge Fitting · corroded · Jul 5, 2025 · N768JB · Airbus A320232 · Vertical Stabilizer
  > DURING HEAVY MAINTENANCE: CORROSION FOUND ON BORE HINGE FITTING 4 OF VERTICAL STABILIZER; REF AEROMAN NR 2025-315972 WO 2025-177/1 REMOVED AND REPLACED HINGE FITTING #4 AND FASTENERS LOCATED VERTICAL STABILIZER IAW A320 SRM 55-3.
- [SDR YENA2025070800693](https://openairdocs.org/sdr/YENA2025070800693.md): Hinge Fitting · corroded · Jul 5, 2025 · N768JB · Airbus A320232 · Vertical Stabilizer
  > DURING HEAVY MAINTENANCE: CORROSION FOUND ON BORE HINGE FITTING 5 OF VERTICAL STABILIZER; REF AEROMAN NR 2025-315973 WO 2025 177/1 REMOVED AND REPLACED HINGE FITTING #5 AND FASTENERS LOCATED VERTICAL STABILIZER IAW A320 SRM 55.
- [SDR YENA2025070800692](https://openairdocs.org/sdr/YENA2025070800692.md): Hinge Fitting · corroded · Jul 5, 2025 · N768JB · Airbus A320232 · Vertical Stabilizer
  > DURING HEAVY MAINTENANCE: CORROSION FOUND ON BORE HINGE FITTING 7 OF VERTICAL STABILIZER; REF AEROMAN NR 2025-315974 WO 2025 177/1 REMOVED AND REPLACED HINGE FITTING #7 AND FASTENERS LOCATED VERTICAL STABILIZER IAW A320 SRM 55-36-4.
- [SDR YENA2025070800691](https://openairdocs.org/sdr/YENA2025070800691.md): Door Frame · cracked · Jul 5, 2025 · N768JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 833FRAME SEGMENTS(1), LONGEST CRACK LENGTH IS AT AFT FRAME SEGMENT, L=0.63INCH,IN PASSENGER CABIN (8); (RESOLVED ON W/O: 1381843 TASKCARD: NR-00047) REF AEROMAN WO 2025-177/1 NR 2025-315758. ACC
- [SDR YENA2025070800690](https://openairdocs.org/sdr/YENA2025070800690.md): Door Frame · cracked · Jul 5, 2025 · N768JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 834 FRAME SEGMENTS(1), LONGEST CRACK LENGTH IS AT FRAME SEGMENT, L=0.22INCH, IN PASSENGER CABIN (8EA); (RESOLVED ON W/O: 1381843 TASKCARD: NR-00048) REF AEROMAN WO 2025-177/1 NR 2025-315757. ACC
- [SDR YENA2025070800689](https://openairdocs.org/sdr/YENA2025070800689.md): Door Frame · cracked · Jul 5, 2025 · N768JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 843 FRAME SEGMENTS(1), LONGEST CRACK LENGTH IS AT AFT FRAME SEGMENT, L=1.33INCH,IN PASSENGER CABIN (11EA); (RESOLVED ON W/O: 1381843 TASKCARD: NR-00049) REF AEROMAN WO 2025-177/1 NR 2025-315759.
- [SDR YENA2025070800688](https://openairdocs.org/sdr/YENA2025070800688.md): Door Frame · cracked · Jul 5, 2025 · N768JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 844 FRAME SEGMENTS (1), LONGE ST CRACK LENGTH IS AT FWD FRAME SEGMENT, L=1.43 INCH, IN PASSENGER CAB IN (20 EA); ACCOMPLISHED THE REINFORCEMENT OF THE STRUCTURE ON EMERGENCY EXIT DOOR 844 IAW
- [SDR YENA2025070800687](https://openairdocs.org/sdr/YENA2025070800687.md): Skin · corroded · Jul 5, 2025 · N768JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION LEADING EDGE UPPER SURFACE LOC. BTW RIB1 TO RIB 2 ON LH WING; ACCOMPLISHED REPAIR OF CORROSION DAMAGE ON THE LH WING TOP SKIN PANEL UPPER SURFACE AT LEVEL OF RIB 1-2 AND STRG 4 IAW AEROMAN EA 57-0048-25 REV 0 (COVER PLUS P-1
- [SDR YENA2025070800686](https://openairdocs.org/sdr/YENA2025070800686.md): Skin · corroded · Jul 5, 2025 · N768JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE ON TOP SKIN LOWER SURFACE OVERHANG AT LEVEL R IB 6 TO RIB 7 ON RH WING (CPCP FINDING). REPAIR OF CORROSION ON THE RH WING TOP SKIN PANEL 2, LOWER SURFACE TEOH FALSE REAR SPAR BETWEEN WX3494.5 - WX4010.2 IN
- [SDR YENA2024073001063](https://openairdocs.org/sdr/YENA2024073001063.md): Unknown · fumes · Jul 29, 2024 · N768JB · Airbus A320232 · Air Distribution System
  > FLT#2072, BQN-FLL. 'DURING DESCENT INTO FLL RIGHT AROUND (9000 FT.) EXPERIENCED (TOXIC FUME) MAGIC MARKER SMELL IN THE COCKPIT; COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION A, ISOLATED FAULT TO TYPE 10, AS PER TSM 05-50-00-810-085-B. DEBRIEFED CREW NO
- [SDR YENA2024062700916](https://openairdocs.org/sdr/YENA2024062700916.md): Wire · damaged · Jun 26, 2024 · N768JB · Airbus A320232 · Light System Wiring
  > FLT#745, JFK-PSE. ' DOOR 2L EXIT LIGHTS INOP; PERFORMED SPLICE REPAIR APPROX 12 INCHES FROM 45WL 2 EXIT DOOR SIGN WIRE -A IAW AMM ESPM 20-53-21-02 AND REPLACED TERMINAL WIRE 1 IAW ESPM 20-56-22. OPS CHECK OF 2L EXIT DOOR EMERGENCY LIGHT OK 33-51-00. MDDR CLEAR
- [SDR YENA2023110601353](https://openairdocs.org/sdr/YENA2023110601353.md): Valve · failed · Nov 3, 2023 · N768JB · Airbus A320232 · Hydraulic System, Main
  > FLT#2786, RDU-JFK. (AIRCRAFT DECLARED AN EMERGENCY INTO JFK) ' HYD Y RSVR OVHT IN FLIGHT; REMOVED AND REPLACED YELLOW ELECTRIC PUMP CHECK VALVE (3083GM) IAW TSM 29-13-00. OPS CHECK WAS SUCCESSFUL. A/C OK FOR CONT SVC.'
- [SDR YENA2023090601047](https://openairdocs.org/sdr/YENA2023090601047.md): Unknown · unknown · Sep 5, 2023 · N768JB · Airbus A320232 · Powerplant System
  > FLT#2102, FLL-JFK. 'ENG #2 INLET STRUCK BY GO; REMOVED AND REPLACED NO. 2 ENG AIR INTAKE COWL IAW AMM 71-11-11. LEAK CHECK AND ALL OPS TEST REQD C/W, ALL GOOD.'
- [SDR YENA2023011700045](https://openairdocs.org/sdr/YENA2023011700045.md): Battery Pack · failed · Jan 13, 2023 · N768JB · Airbus A320232 · Emergency Lighting
  > FLT#2202, FLL-JFK. ' REF LP 3457586-2 EMERGENCY LIGHT SYSTEM FAILED (10WL); FOUND R1 ESCAPE SLIDE AT FAULT. REM/INS NEW SLIDE RAFT ASSY REF AMM 25-62-44. ALL TESTS ARE OK, TSH ACCOMPLISHED PER ASM 33-51-01 & AWL 33-51-01. (FAULT "EPSU (10WL) FWD L/DEU-B (300RH
- [SDR YENA2022092300951](https://openairdocs.org/sdr/YENA2022092300951.md): Unknown · odor · Sep 22, 2022 · N768JB · Airbus A320232 · Air Distribution System
  > FLT 76, BDL-LAX. INFLIGHT REPORTED THAT THEY SMELLED THE DIRTY SOCK SMELL DURING DESCENT AROUND 2K FT. INTENSITY WAS STRONG ONLY IN REAR OF ACFT THERE WAS A FAINT ODOR IN COCKPIT ON THE FINAL APPROACH. ACCOMPLISHED STAGE 1 ECS DECONTAMINATION LEVEL C IAW AMM 2
- [SDR YENA2022011900021](https://openairdocs.org/sdr/YENA2022011900021.md): Selector Valve · leaking · Jan 10, 2022 · N768JB · Airbus A320232 · Hydraulic System, Main
  > FLT # 613, *FUME EVENT* TRANSIENT FUMES 11000-9000 DESCENDING TO FLL, REAR FA'S REPORT CONTINUING BEYOND, FAS LIGHT HEADED ON GROUND; FOUND AFT CARGO DOOR SELECTOR VALVE LEAKING HYD FLUID INTO APU INLET. SECURED LINES ON VALVE IAW AMM 52-36-15. COMPLIED WITH
- [SDR YENA2020030920218](https://openairdocs.org/sdr/YENA2020030920218.md): Battery · discharged · Mar 2, 2020 · N768JB · Airbus A320232 · Emergency Lighting
  > FT # 391, BOS-TPA. EMERG LIGHT BATTERIES 12WL AND 13 WL FAILED LIGHT TEST; REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES FIN 12WL AND 13WL IAW AMM33-51-38
- [SDR YENA2020030920217](https://openairdocs.org/sdr/YENA2020030920217.md): Battery · discharged · Mar 2, 2020 · N768JB · Airbus A320232 · Emergency Lighting
  > FT # 391, BOS-TPA. EMERG LIGHT BATTERIES 12WL AND 13 WL FAILED LIGHT TEST; REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES FIN 12WL AND 13WL IAW AMM33-51-38
- [SDR YENA2019103160627](https://openairdocs.org/sdr/YENA2019103160627.md): Probe · failed · Oct 26, 2019 · N768JB · Airbus A320232 · Fuel Indicating System
  > FLT 313, DIVERTED. FUEL AUTO FEED FAULT ECAM BROUGHT US TO FUEL PAGE. R INNER WING TANK SHOWED 4000 LESS THANK R TANK. TOTAL FUEL WAS 3000 LESS THAN FLIGHT PLAN. ARRIVAL FOB WAS TRENDING DOWN AT SAME TIME (ABOUT 500 IN 5 MINUTES) 20 MIN LATER WING FUEL CORR
- [SDR YENA2019102510613](https://openairdocs.org/sdr/YENA2019102510613.md): Circuit Card · malfunctioned · Oct 21, 2019 · N768JB · Airbus A320232 · Fuel Quantity Indicator
  > FT # 319, FLL-SLC. RETURNED TO FIELD. IN FLIGHT RECEIVED FUEL ADV. LT TANK WAS 3500 MORE THAN RT TANK AND LT TANK WAS FLASHING. OUR FOB AND EFOB ALL DROPPED 3500 LBS. ATTEMPTED TO BALANCE THE FUEL IN THE TANKS. RESET CB'S FROM THE COMPUTER RESET TABLE 4-59 - N
- [SDR YENA201908280495](https://openairdocs.org/sdr/YENA201908280495.md): Cleat · corroded · Aug 28, 2019 · N768JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, FWD CARGO COMP FR 34 STR 42L-43L CLEAT HAD CORROSION; REMOVED AND REPLACED CLEAT IAW SRM 51-72-11 REFERENCE NR 440577-20713 FOR WORK ACCOMPLISHED.
- [SDR YENA201908280494](https://openairdocs.org/sdr/YENA201908280494.md): Floorbeam · corroded · Aug 28, 2019 · N768JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, FWD CABIN, LT FLOOR SUPPORT, FR 20 BEAM Y1292 HAS CORROSION AND SCRIBE LINE; REFERENCE NR 440577-20520 REMOVED CORROSION ON FLOORBEAM Y1292 FR 20 REMOVED.040" IN AN AREA L'2.0" X W2.0" FOUND TO BE OUT OF LIMITS PER SRM. REMOVED AND R
- [SDR YENA201908280493](https://openairdocs.org/sdr/YENA201908280493.md): Door Sill · corroded · Aug 28, 2019 · N768JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, BULK CARGO DOOR SILL HAS CORROSION AT FASTENER HOLES; REF N/R 440577-20567. R & R BULK CARGO DOOR SILL IAW SRM 51-42-16 PG 2 & 3, 53-41-49-300-002.
- [SDR YENA201908280492](https://openairdocs.org/sdr/YENA201908280492.md): Seat Track · out of limits · Aug 28, 2019 · N768JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE, SEAT TRACK Y-765 AT FR 43+14 IS OUT OF LIMITS REQUIRES REPLACEMENT; REF N/R 440577-20613 - R & R SEAT TRACK Y-765 AT FR 43+14.
- [SDR YENA201908280491](https://openairdocs.org/sdr/YENA201908280491.md): Skin · corroded · Aug 28, 2019 · N768JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, AFT FUSELAGE SKIN AROUND WASTE VENT FRAME 69-70 STRINGER 31-32R HAS CORROSION. NO MX-220 IS REQUIRED; REF NON-ROUTINE 20060, SERVICE ORDER 440577, REMOVED CORROSION AND INSTALLED REPAIR DOUBLER IAW SRM 53-41-11-300-004 CAT A REPAIR. N
- [SDR YENA201908280490](https://openairdocs.org/sdr/YENA201908280490.md): Stringer · corroded · Aug 28, 2019 · N768JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE, CORROSION IN AFT CARGO BETWEEN FR 67 - FR 69 STRINGER 38R; REF NON-ROUTINE 20813 SERVICE ORDER 440577, R & R STRINGER 38R BETWEEN FR 67069 IAW SRM 51-72-11 & SRM 53-41-13-300-004.
- [SDR YENA201908280489](https://openairdocs.org/sdr/YENA201908280489.md): Door Sill · corroded · Aug 28, 2019 · N768JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, BULK CARGO DOOR SILL HAS CORROSION AT FASTENER HOLES; REF NON-ROUTINE 20567 SERVICE ORDER 440577. R & R FASTENERS AND BULK DOOR SILL. FOUND TO BE OUT OF LIMITS. RECEIVED NEW BULK DOOR SILL AND INSTALLED IAW SRM 51-42-11 PAGE 2 & 3.
- [SDR YENA201908280488](https://openairdocs.org/sdr/YENA201908280488.md): Seat Track · out of limits · Aug 28, 2019 · N768JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE, SEAT TRACK Y-765 AT FR 47+17 TO FR 52+14 IS OUT OF LIMITS. REQUIRES REPAIR; REF NON-ROUTINE 20614 SERVICE ORDER 440577, R & R SEAT TRACK Y765 AT FR 47 - FR 53 IAW SRM 53-41-15.
- [SDR YENA201902210096](https://openairdocs.org/sdr/YENA201902210096.md): Actuator · tripped · Feb 21, 2019 · N768JB · Airbus A320232 · Leading Edge Slat Actuator
  > FLT 81, JFK-RNO. SLATS JAMMED AT ON APPROACH RECYCLE DID NOT WORK. DECLARED EMERGENCY FOLLOWED QRH AND LANDED. PERFORMED TSM 27-81-00-810-810-A FOUND NR 4 ACTUATOR TRIPPED ON THE LEFT HAND SIDE. RESET ACTUATOR AND LUBED SLAT SYSTEM AND PERFORMED OPS CHECK PER
- [SDR YENA2018080610304](https://openairdocs.org/sdr/YENA2018080610304.md): Battery · failed · Aug 1, 2018 · N768JB · Airbus A320232 · Emergency Lighting
  > EPSU EMERGENCY BATTERY 11WL FAILED A SYSTEM TEST. R & R THE BATTERY 11WL IAW AMM 33-51-38, EMERGENCY LIGHT TESTED GOOD.
- [SDR YENA201801230043](https://openairdocs.org/sdr/YENA201801230043.md): Unknown · odor · Jan 23, 2018 · N768JB · Airbus A320232 · Air Distribution System
  > F/AS REPORTED AN ODOR DURING DECENT. COMPLIED WITH INFORMATION NOTICE 2017-T015B, SECTION A. AIRCRAFT IS OK FOR SERVICE.
- [SDR YENA201711030884](https://openairdocs.org/sdr/YENA201711030884.md): Switch · inoperative · Nov 3, 2017 · N768JB · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT SWITCH WILL NOT TURN LIGHTS OFF. R & R THE LIGHT SWITCH IAW ESPM 20-45-51. OPS OK IAW AMM 33-51-00.
- [SDR YENA20160317245](https://openairdocs.org/sdr/YENA20160317245.md): Girt Bar · corroded · Mar 17, 2016 · N768JB · Airbus A320232 · Emergency Equipment
  > R1 DOOR FWD GIRT BAR FITTING SHOWS SIGNS OF CORROSION AROUND STUD HOLES; REPAIRED IAW SRM 53-11-14. ACCOMPLISHED INSPECTION.
- [SDR YENA20160317244](https://openairdocs.org/sdr/YENA20160317244.md): Girt Bar · corroded · Mar 17, 2016 · N768JB · Airbus A320232 · Emergency Equipment
  > L1 DOOR FWD GIRT BAR FITTING SHOWS SIGNS OF CORROSION AROUND STUD HOLES; REPAIRED IAW SRM 53-11-14. ACCOMPLISHED INSPECTION.
- [SDR YENA20160317243](https://openairdocs.org/sdr/YENA20160317243.md): Girt Bar · corroded · Mar 17, 2016 · N768JB · Airbus A320232 · Emergency Equipment
  > L1 DOOR AFT GIRT BAR SHOWS SIGNS OF CORROSION AROUND STUD HOLES; REPAIRED IAW SRM 53-11-14. ACCOMPLISHED INSPECTION.
- [SDR YENA20150922429](https://openairdocs.org/sdr/YENA20150922429.md): Power Supply · no test · Sep 22, 2015 · N768JB · Airbus A320232 · Emergency Lighting
  > DURING MAINTENANCE THE LT OVERWING EXIT EMERGENCY LIGHT WOULD NOT TURN ON IN MANUAL. R & R FIN 11 POWER SUPPLY BATTERY IAW AMM 33-51-38. OPS CHECK GOOD.

Next page: https://openairdocs.org/aircraft/N768JB/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 = 'N768JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N768JB/reports

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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.