N768JB

Service difficulty reports · 53

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR YENA2026041700408Pbe · failed inspFLT#399, LGA-MCO. "PER EC 353000-05-1 AFT FA PBE FAILED INSPECTION; REMOVED AND REPLACED AFT FA PBE AS REQUIRED.Apr 16, 2026 · N768JB · Airbus A320232 · Emergency EquipmentSDR YENA2025070800707Door Frame · crackedDURING 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/Jul 5, 2025 · N768JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025070800706Door Frame · crackedDURING 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 PERFORMEJul 5, 2025 · N768JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025070800705Door Frame · crackedDURING 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 Jul 5, 2025 · N768JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025070800704Door Frame · crackedDURING 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 REMOVJul 5, 2025 · N768JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025070800703Door Frame · crackedDURING 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 Jul 5, 2025 · N768JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025070800702Dummy Rail · corrodedDURING 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 FWDJul 5, 2025 · N768JB · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR YENA2025070800701Floor Support · corrodedDURING 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 LOCATJul 5, 2025 · N768JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2025070800700Frame · crackedDURING 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-00040Jul 5, 2025 · N768JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2025070800699Floor Support · corrodedDURING 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. BTWJul 5, 2025 · N768JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2025070800698Floor Support · corrodedDURING 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) LOCJul 5, 2025 · N768JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2025070800697Stringer · corrodedDURING 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 51-72-1Jul 5, 2025 · N768JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2025070800696Hinge Fitting · corrodedDURING 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.Jul 5, 2025 · N768JB · Airbus A320232 · Vertical StabilizerSDR YENA2025070800695Hinge Fitting · corrodedDURING 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.Jul 5, 2025 · N768JB · Airbus A320232 · Vertical StabilizerSDR YENA2025070800694Hinge Fitting · corrodedDURING 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.Jul 5, 2025 · N768JB · Airbus A320232 · Vertical StabilizerSDR YENA2025070800693Hinge Fitting · corrodedDURING 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.Jul 5, 2025 · N768JB · Airbus A320232 · Vertical StabilizerSDR YENA2025070800692Hinge Fitting · corrodedDURING 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.Jul 5, 2025 · N768JB · Airbus A320232 · Vertical StabilizerSDR YENA2025070800691Door Frame · crackedDURING 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. ACCJul 5, 2025 · N768JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025070800690Door Frame · crackedDURING 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. ACCJul 5, 2025 · N768JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025070800689Door Frame · crackedDURING 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.Jul 5, 2025 · N768JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025070800688Door Frame · crackedDURING 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 Jul 5, 2025 · N768JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025070800687Skin · corrodedDURING 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-1Jul 5, 2025 · N768JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2025070800686Skin · corrodedDURING 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 Jul 5, 2025 · N768JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2024073001063Unknown · fumesFLT#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 NOJul 29, 2024 · N768JB · Airbus A320232 · Air Distribution SystemSDR YENA2024062700916Wire · damagedFLT#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 CLEARJun 26, 2024 · N768JB · Airbus A320232 · Light System WiringSDR YENA2023110601353Valve · failedFLT#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.'Nov 3, 2023 · N768JB · Airbus A320232 · Hydraulic System, MainSDR YENA2023090601047Unknown · unknownFLT#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.'Sep 5, 2023 · N768JB · Airbus A320232 · Powerplant SystemSDR YENA2023011700045Battery Pack · failedFLT#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 (300RHJan 13, 2023 · N768JB · Airbus A320232 · Emergency LightingSDR YENA2022092300951Unknown · odorFLT 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 2Sep 22, 2022 · N768JB · Airbus A320232 · Air Distribution SystemSDR YENA2022011900021Selector Valve · leakingFLT # 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 Jan 10, 2022 · N768JB · Airbus A320232 · Hydraulic System, MainSDR YENA2020030920218Battery · dischargedFT # 391, BOS-TPA. EMERG LIGHT BATTERIES 12WL AND 13 WL FAILED LIGHT TEST; REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES FIN 12WL AND 13WL IAW AMM33-51-38Mar 2, 2020 · N768JB · Airbus A320232 · Emergency LightingSDR YENA2020030920217Battery · dischargedFT # 391, BOS-TPA. EMERG LIGHT BATTERIES 12WL AND 13 WL FAILED LIGHT TEST; REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES FIN 12WL AND 13WL IAW AMM33-51-38Mar 2, 2020 · N768JB · Airbus A320232 · Emergency LightingSDR YENA2019103160627Probe · failedFLT 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 CORROct 26, 2019 · N768JB · Airbus A320232 · Fuel Indicating SystemSDR YENA2019102510613Circuit Card · malfunctionedFT # 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 - NOct 21, 2019 · N768JB · Airbus A320232 · Fuel Quantity IndicatorSDR YENA201908280495Cleat · corrodedDURING 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.Aug 28, 2019 · N768JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201908280494Floorbeam · corrodedDURING 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 RAug 28, 2019 · N768JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA201908280493Door Sill · corrodedDURING 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.Aug 28, 2019 · N768JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201908280492Seat Track · out of limitsDURING 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.Aug 28, 2019 · N768JB · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR YENA201908280491Skin · corrodedDURING 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. NAug 28, 2019 · N768JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA201908280490Stringer · corrodedDURING 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.Aug 28, 2019 · N768JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA201908280489Door Sill · corrodedDURING 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.Aug 28, 2019 · N768JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201908280488Seat Track · out of limitsDURING 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.Aug 28, 2019 · N768JB · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR YENA201902210096Actuator · trippedFLT 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 Feb 21, 2019 · N768JB · Airbus A320232 · Leading Edge Slat ActuatorSDR YENA2018080610304Battery · failedEPSU EMERGENCY BATTERY 11WL FAILED A SYSTEM TEST. R & R THE BATTERY 11WL IAW AMM 33-51-38, EMERGENCY LIGHT TESTED GOOD.Aug 1, 2018 · N768JB · Airbus A320232 · Emergency LightingSDR YENA201801230043Unknown · odorF/AS REPORTED AN ODOR DURING DECENT. COMPLIED WITH INFORMATION NOTICE 2017-T015B, SECTION A. AIRCRAFT IS OK FOR SERVICE.Jan 23, 2018 · N768JB · Airbus A320232 · Air Distribution SystemSDR YENA201711030884Switch · inoperativeEMERGENCY LIGHT SWITCH WILL NOT TURN LIGHTS OFF. R & R THE LIGHT SWITCH IAW ESPM 20-45-51. OPS OK IAW AMM 33-51-00.Nov 3, 2017 · N768JB · Airbus A320232 · Emergency LightingSDR YENA20160317245Girt Bar · corrodedR1 DOOR FWD GIRT BAR FITTING SHOWS SIGNS OF CORROSION AROUND STUD HOLES; REPAIRED IAW SRM 53-11-14. ACCOMPLISHED INSPECTION.Mar 17, 2016 · N768JB · Airbus A320232 · Emergency EquipmentSDR YENA20160317244Girt Bar · corrodedL1 DOOR FWD GIRT BAR FITTING SHOWS SIGNS OF CORROSION AROUND STUD HOLES; REPAIRED IAW SRM 53-11-14. ACCOMPLISHED INSPECTION.Mar 17, 2016 · N768JB · Airbus A320232 · Emergency EquipmentSDR YENA20160317243Girt Bar · corrodedL1 DOOR AFT GIRT BAR SHOWS SIGNS OF CORROSION AROUND STUD HOLES; REPAIRED IAW SRM 53-11-14. ACCOMPLISHED INSPECTION .Mar 17, 2016 · N768JB · Airbus A320232 · Emergency EquipmentSDR YENA20150922429Power Supply · no testDURING 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.Sep 22, 2015 · N768JB · Airbus A320232 · Emergency Lighting
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