N612JB

Service difficulty reports · 65

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 = 'N612JB' 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 YENA2026101900988Warning Message · illuminatedFLT#773, BOS-AUA-RTF. ON GEAR RETRACTION WE GOT ECAM L/G DOORS NOT CLOSED. ECAM TOLD US TO CYCLE THE GEAR BELOW 220 KTS, WE STILL HAD 1 FLAP AND APP 190 KTS, CYCLED ONCE MSG STILL THERE. DROPPED THE GEAR TO MAKE SURE IT STILL CAME DOWN. LEFT IT DOWN AND RETURNOct 17, 2026 · N612JB · Airbus A320232 · Landing Gear Retraction/Extension SystemSDR YENA2026041000390Switch · intermittentFLT#1389, GCM-GCM. "CREW REPORTS EMERGENCY LIGHTS INOP. LIGHTS COME ON AND WILL NOT TURN OFF AFTER ENGINE START ( INTERIOR AND EXTERIOR EMERGENCY LIGHTING SYSTEMS (WITHOUT PASSENGERS) ); REF TSM 33-51-00-810-881-A ACCOMPLISHED WIRING CHECK FOR GND WIRE FROM 24Apr 8, 2026 · N612JB · Airbus A320232 · Emergency LightingSDR YENA2025122301248Reservoir · leakingFLT #2930 SJU - RDU (AN EMERGENCY WAS DECLARED ) "OW ALMOST 0 GREEN RESERV. ECAM HYD G ENG 1 PUMP LO PR G SYS LO PR ECAM AND QRH ACTIONS COMPLETED.; FOUND RH MLG DORO ACTUATION CYLINDER FLEX OPENEING HOSE BURST. REPLACED OPENING FLEX HOSE AND CLOSING FLEX HOSEDec 21, 2025 · N612JB · Airbus A320232 · Hydraulic System, MainSDR YENA2025122301238Hydraulic System · warning messageFLT # 2930 SJU- RDU ( AN EMERGENCY WAS DECLEARED ) "LOW ALMOST 0 GREEN RESERV. ECAM HYD G ENG 1 PUMP LO PR G SYS LO PR ECAM AND QRH ACTIONS COMPLETED. FOUND RH MLG DORO ACTUATION CYLINDER FLEX OPENEING HOSE BURST. REPLACED OPENING FLEX HOSE AND CLOSING FLEX HODec 21, 2025 · N612JB · Airbus A320232 · Hydraulic System, MainSDR YENA2025082800890Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON EMERGENCY EXIT DOOR (844) FRAME SEGMENT (1) (1EA), CRACK LENGTH: 0.100 INCH; ACCOMPLISHED DOORS / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH (AFT RH EEH) FRAME / REINFORCE DOOR STRUCTURE - MODIFICATION IAAug 28, 2025 · N612JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025082800889Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON EMERGENCY EXIT DOOR (834) FRAME SEGMENT (1) (2EA), CRACK LENGTH: 3.100 INCH; ACCOMPLISHED DOORS / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH (AFT LH EEH) FRAME / REINFORCE DOOR STRUCTURE - MODIFICATION IAAug 28, 2025 · N612JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025082800888Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON EMERGENCY EXIT DOOR (833) FRAME SEGMENT (1) (2EA), CRACK LENGTH: 2.500 INCH; ACCOMPLISHED DOORS / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH (FWD LH EEH) FRAME / REINFORCE DOOR STRUCTURE - MODIFICATION IAAug 28, 2025 · N612JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025082800887Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON EMERGENCY EXIT DOOR (843) FRAME SEGMENT (1) (2EA), CRACK LENGTH: 3.50 INCH; ACCOMPLISHED DOORS / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH (FWD RH EEH) FRAME / REINFORCE DOOR STRUCTURE - MODIFICATION IAAug 28, 2025 · N612JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025082800885Skin · damagedDURING HEAVY MAINTENANCE: LIGHTNING STRIKE EXTERNAL SKIN LOC. BTW FRAME 26 AND FRAME 27 AND BTW STRINGER 41L AND 42L AT LOWER FUSELAGE; WORK ACCOMPLISHED ON AEROMAN W/O:2025 194/1 NR: 2025 - 471516 REPAIR LOCATED BTW FRAME 26 AND FRAME 27 AND BTW STRINGER 41L Aug 28, 2025 · N612JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2025082800886Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 LH SIDE IN OPEN FASTENER HOLE ( INBOARD LOWER HOLE ) AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 5 O CLOCK; PERFORMED PERMANENT REPAIR LOCATED ON FRAME 68, L/H SIDE AT LEVEL OF DOOR STOP #1 I.A.W. Aug 28, 2025 · N612JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025082800884Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE ( INBOARD LOWER HOLE ) AT DOOR STOP FITTING 4 POSITION,CRACK DIRECTION IS 2 O CLOCK AND 7 O CLOCK; (RESOLVED ON W/O: 1402836 TASKCARD: NR-00034) REF AEROMAN WO # 2025-194/1 NAug 28, 2025 · N612JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025082800883Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE ( INBOARD LOWER HOLE ) AT DOOR STOP FITTING 1 POSITION,CRACK DIRECTION IS 12 O C LOCK AND 6 O CLOCK;(RESOLVED ON W/O: 1402836 TASKCARD: NR-00035) REF AEROMAN WO # 2025-194/1 NAug 28, 2025 · N612JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2024100801335Unknown · odorFLT#605, MCO-SDQ. 'ON DESCT <10,000' HAD STRONG ODOR- TURNED OFF PACK 1 AS PER FCOM - SMELL; COMPLIED WITH INFO NOTICE 2017-T015, SECTION B2 IDENTIFIED ODOR TYPE 5 AND TYPE 2, DECONTAMINATION LEVEL A WAS ACCOMPLISHED PER TSM 05-50-00-810-831-A. A/C FOR CONTINUOct 5, 2024 · N612JB · Airbus A320232 · Air Distribution SystemSDR YENA2023082800997Selector · failedFLT#2005, BOS-MCO. 'L/G DOORS NOT CLOSED UPON CYCLING L/G DOWN; REMOVED AND REPLACED LANDING GEAR DOORS SELECTOR VALVE (41GA)IAW AMM CH 32-31-34. PERFORMED FUNCTIONAL TEST OF THE NORMAL EXTENSION & RETRACTION OF THE L/G. TEST OK. REF AMM 32-31-00.'Aug 25, 2023 · N612JB · Airbus A320232 · Landing Gear Door Retract SectionSDR YENA2023062200727Unknown · unknownFLT#1348, SJU-DCA. 'FOUND R2 DOOR EMERGENCY EXIT SIGN ONE LAMP INOP; RELAMP R2 DOOR CABIN-WALL MOUNTED EMERGENCY -EXIT-MARKERS IN REFERENCE A320 AMM 33-51-13. THE OPS CHECK IS GOOD. A/C IS OK TO CONTINUE.Jun 22, 2023 · N612JB · Airbus A320232 · Emergency LightingSDR YENA2022122801295Unknown · odorFLT#98, DEN-JFK. 'DIRTY SOCK SMELL IN DESCENT ALL THE WAY TO LANDING STARTED AT 15000'; PERFORMED LEVEL A DECONTAMINATION OF ECS IAW AMM 21-00-00-615-802A. APU MEL FOR REPLACEMENT ON LOG PAGE 3565062, ITEM 2 (PLACED APU ON DEFERRAL IAW MEL 4-10-01A CAT C.Dec 23, 2022 · N612JB · Airbus A320232 · Air Distribution SystemSDR YENA2022121201245A/C Pack · odorFLT#1295, JFK-AUS. 'STRONG DIRTY SOCK SMELL REPORTED BY INFLIGHT BELOW 4 K ON APPROACH FLYING THROUGH MULTIPLE LAYERS OF CLOUDS AT THE TIME SMELL DISSIPATED UPON LANDING NO ODOR DETECTED ON GROUND; C/W INFORMATION NOTED 2017 - T015 SECTION B 1 PER TSM 05 - 50 Dec 10, 2022 · N612JB · Airbus A320232 · Cabin Cooling SystemSDR YENA2022112101139Unknown · odorFLT#757, DURING DESCENT THRU FL10.0 STRONG DIRTY SOCK ODOR FUMES EVENT STRONG IN THE MID CABIN. ECS DECONTAMINATION ACCOMPLISHED. OZONE FILTERS WERE REPLACED PER LP 3433706 (ACCOMP LEAK CHECK OF #2 OZONE FILTER. NO LEAKS NOTED REF AMM 21-51-410 AND LP 34337Nov 19, 2022 · N612JB · Airbus A320232 · Air Distribution SystemSDR YENA2022111701130Cooling Fan · contaminatedFLT # 613, HPN-FLL(DIVERTED TO JFK). FUME EVENT IN CABIN AND COCKPIT DURING CLIMBOUT STAYED AT 12000 DIVERT TO JFK NO OVERWEIGHT LANDING LEVEL 2 TO 3 EVENT STRONG ODOR WITH IRRITATION TO EYES , LUNGS ETC ; #1 ENGINE BOROSCOPED WITH NO EVIDENCE OF OIL ON LOGPAGNov 16, 2022 · N612JB · Airbus A320232 · Airborne Auxiliary Power Unit (APU) SystemSDR YENA2022110401087None · noneFLT#2102, FLL-JFK. 'IN-FLIGHT CREW ON INBOUND FLIGHT REPORTED DIRTY SOCK SMELL ON CLIMB AND DESCENT; COMPLIED WITH INFO NOTICE 2017-T015J PERFORMED ENGINE 1 & 2 IDLE RUNS. ISOLATED BLEED SOURCES AND OPERATED LH & RH PACKS INDIVIDUALLY. NO ODOR DETECTED.'Nov 3, 2022 · N612JB · Airbus A320232 · Air Conditioning SystemSDR YENA2022100400983None · noneDURING HEAVY MAINTENANCE: CORROSION LOWER SILL AT LEVEL FR68 AND STR 23L AFT GALLEY AREA (CPCP RELATED MPD TASK 534195-01): PERFORMED REPAIR AT LOWER SILL AND STR23L AFT GALLEY AREA IAW A320 SRM 53-41-14-300-001. THIS REPAIR IS CATEGORY A AND NO FURTHER INSPEOct 2, 2022 · N612JB · Airbus A320232 · Fuselage Structure (General)SDR YENA2022041100352Cabin Air Sys · odorFLT#350, GND-JFK. 'FAINT ODOR ENROUTE AT CRUISE ALTITUDE A PLASTIC OR ELECTRIC BURN SMELL LASTED APPROX 2 MIN AND QUICKLY DISSIPATED NO ASSOCIATED ISSUES NOTED COCKPIT ONLY CONFIRMED WITH FA'S; AFTER CREW DEBRIEF, CREW NOTED SMELL LASTED 30 SEC AND THEN DISSIPApr 10, 2022 · N612JB · Airbus A320232 · Cabin Cooling SystemSDR YENA2022030100106None · noneFLT # 1505, EWR-FLL. FUME EVENT DESC 8000' UNTIL TOUCHDOWN BOTH COCKPIT & CABIN ; COMPLETED WITH INFORMATION NOTICE 2017-T015, SECTION A (A), ISOLATED FAULT TO TYPE 10, (A), 1, C PER TSM 05-50-00-810085-B/TSM 05-50-00-810-085-D. AIRCRAFT IS OK FOR SERVICE.Feb 28, 2022 · N612JB · Airbus A320232 · Air Conditioning SystemSDR YENA2022021800078Module · failedFLT # 2029, JFK-RSW. SEC 2 FAULT. ( SPOILER ELEVATOR COMPUTERS - SEC2 (A320 W/O SHARKLETS AND A321'S) ) ; SEC 2 PLACED ON MEL 27-94-01D CAT C. “PULLED AND COLLARED C/B 121VU-Q18 IAW AMM TASK 27-94-00-040-002 A”. PERFORMED CFDS FAULT TEST IAW AMM TASK 27-94-00-Feb 15, 2022 · N612JB · Airbus A320232 · Flight Control SystemSDR YENA2022021800077Module · failedFLT # 2029, JFK-RSW. SEC 2 FAULT. ( SPOILER ELEVATOR COMPUTERS - SEC2 (A320 W/O SHARKLETS AND A321'S) ) ; SEC 2 PLACED ON MEL 27-94-01D CAT C. “PULLED AND COLLARED C/B 121VU-Q18 IAW AMM TASK 27-94-00-040-002 A”. PERFORMED CFDS FAULT TEST IAW AMM TASK 27-94-00-Feb 15, 2022 · N612JB · Airbus A320232 · Flight Control SystemSDR YENA2022021800076Computer · failedFLT # 2029, JFK-RSW. SEC 2 FAULT. ( SPOILER ELEVATOR COMPUTERS - SEC2 (A320 W/O SHARKLETS AND A321'S) ) ; SEC 2 PLACED ON MEL 27-94-01D CAT C. “PULLED AND COLLARED C/B 121VU-Q18 IAW AMM TASK 27-94-00-040-002 A”. PERFORMED CFDS FAULT TEST IAW AMM TASK 27-94-00-Feb 15, 2022 · N612JB · Airbus A320232 · Flight Control SystemSDR YENA2021070900453Selector Valve · failedFLT 193, L/G LGCIU 2 FAULT AT GEAR RETRACTION DEPARTING EWR FOR STI DIVERTED TO JFK ;REF L/P 3112277 ITEM # & #2 L/G SELECTOR VALVE 40GA REPLACED IAW AMM 32-31-12 NORMAL EXTENSION AND RETRACTION TEST ACCOMPLISHED NO FAULTS NOTED. PFR AND PREVIOUS LEG GIVE L/GJul 5, 2021 · N612JB · Airbus A320232 · Landing Gear Retraction/Extension SystemSDR YENA2019102940625Lamp · burned outFT # 1348, SJU-DCA. FWD BULKHEAD AT 1ABC RED EMER LIGHT ASSY BURNT OUT; RELAMPED PER AMM 33-51-18. OP CHK GOOD. OK FOR SVC.Oct 24, 2019 · N612JB · Airbus A320232 · Emergency LightingSDR YENA201901270043Unknown · odorFLT 1151, TPA-SJU. STRONG FUMES DURING DESCENT CABIN NOTICED STRONG FUMES IN AFT AND FRONT OF CABIN ( PACKS - SINGLE (SPEEDBRAKES OK) (N503-N665) ); PERFORMED OPERATIONAL CHECKS OF PACK 2 WITH ALL BLEED AIR SOURCES, REF AMM 71-00-00-810-801A. OPERATION IS NORMJan 27, 2019 · N612JB · Airbus A320232 · Air Distribution SystemSDR YENA2018080610303Coffeemaker · failedFAINT ELECTRICAL ODOR IN THE FWD GALLEY DURING CRUISE. PULLED BOTH COFFEE CIRCUIT BREAKERS, THE ODOR WENT AWAY. REMOVED THE NR 1 AND 2 FWD GALLEY COFFEEMAKERS IAW AMM 25-35-15. POWERED UP THE COFFEEMAKERS. REMAINED ON FOR 1 HOUR. NO FAULTS OR ODORS NOTAug 1, 2018 · N612JB · Airbus A320232 · Buffet/GalleysSDR YENA2018080610302Coffeemaker · failedFAINT ELECTRICAL ODOR IN THE FWD GALLEY DURING CRUISE. PULLED BOTH COFFEE CIRCUIT BREAKERS, THE ODOR WENT AWAY. REMOVED THE NR 1 AND 2 FWD GALLEY COFFEEMAKERS IAW AMM 25-35-15. POWERED UP THE COFFEEMAKERS. REMAINED ON FOR 1 HOUR. NO FAULTS OR ODORS NOTAug 1, 2018 · N612JB · Airbus A320232 · Buffet/GalleysSDR YENA2018072730294Power Unit · odorFLT 797, BOS-ATL. 21B POWER BOX HOT AND SMELLS OF ELEC ODOR ( LIVE TV SYS - ENTIRE SYSTEM ); ACCOMPLISHED ELECTRICAL ODOR SYSTEM INTEGRITY CHECK PER LTV-535, 44-20-000-210-803. RESULT SATISFACTORY.Jul 23, 2018 · N612JB · Airbus A320232 · Entertainment SystemSDR YENA2018061840256Fan · failedSTRONG BURNING ELECTRICAL ODOR REPORTED NEAR ROWS 1, 2, & 3. ODOR STOPPED AND DISSIPATED QUICKLY. PERFORMED A CABIN ODOR INSPECTION IAW AMM 05-50-810-831-A. FOUND THE AVIONICS BLOWER FAN TO BE SOURCE OF THE ODOR. R & R THE BLOWER FAN. RESET THE CIRCUIT BRJun 14, 2018 · N612JB · Airbus A320232 · Air Distribution FanSDR YENA201803060126Battery Pack · no testFWD LEFT EPSU BATTERY 10WL FAILED AN EMERGENCY LIGHT SYS TEST. R & R THE BATTERY PACK IAW AMM 33-51-38, SYSTEM TESTED OK.Mar 6, 2018 · N612JB · Airbus A320232 · Emergency LightingSDR YENA201710220855Engine · overservicedON FINAL, AT 2000 FT, THE FA REPORTED A DIRTY SOCK ODOR IN THE FRONT AND AFT CABIN. ODOR DISSIPATED AFTER LANDING. THERE WAS NO ODOR IN THE FLIGHT DECK. ACCOMPLISHED INFO NOTICE 2017-T015B SECTION B, FOUND THE NR 2 ENGINE OVERSERVICED. SERVICED THE ENGINEOct 22, 2017 · N612JB · Airbus A320232 · Turbine Engine Oil SystemSDR YENA201708010638Unknown · odorDIRTY SOCK ODOR NOTICED DURING DESCENT & APPROCH. NORMAL BLEED OPERATION. CRUISE, AND DESCENT ODOR MORE TOWARD AFT OF CABIN. OPERATED PACKS ON THE GROUND WITH NO FURTHER ISSUE NOTED. COMPLIED WITH INFORMATION NOTICE 2017-T015A SECTION A. AIRCRAFT OK FORAug 1, 2017 · N612JB · Airbus A320232 · Air Distribution SystemSDR YENA20160830788Beam · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON DOG LEG BEAM BETWEEN Y1162-Y1292, FRAME 66-FRAME 67. DOG LEG BEAM BETWEEN Y1162-Y1292, FRAME 66-67 WAS REPLACED IAW SRM 51-72-11 AND SRM 51-42-11, REV 114.Aug 30, 2016 · N612JB · Airbus A320232 · Fuselage Main, StructureSDR YENA20160830787Support · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON SHEAR PLATE SUPPORT FRAME 69-70 RT. R & R SHEER PLATE SUPPORT BETWEEN FRAME 69-70 RT IAW SRM 51-72-11 AND 51-42-11.Aug 30, 2016 · N612JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA20160830786Shear Plate · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON SHEAR PLATE FRAME 69-70 RT. R & R SHEER PLATE IAW SRM 51-72-11 AND 51-42-11.Aug 30, 2016 · N612JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA20160830785Shear Plate · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON SHEAR PLATE, CORRODED FRAME 69-70 LT. R & R SHEAR PLATE IAW SRM 51-72-11 AND 51-42-11 .Aug 30, 2016 · N612JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA20160830784Floorbeam · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM AT FRAME 68-69 -Y1162. R & R DOG LEG Y1162, FRAME 68-69 IAW SRM 51-72-11 AND SRM 51-42-11, REV 114, PN D5347218820400.Aug 30, 2016 · N612JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA20160830783Floorbeam · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM AT FRAME 68-69 -Y1162. R & R FLOORBEAM FRAME 68-69 -Y1162 IAW SRM 51-72-11 REV 114, SRM 51-42-11, REV 114, PN D5347218920400.Aug 30, 2016 · N612JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA20160830782Floorbeam · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM AT FRAME 65-67 -Y919. R & R FLOORBEAM 65-67-Y919 IAW SRM 51-72-11, REV 114 SRM 51-42-11, REV 114 & AIPC 53-41-04-21D, PN D5347209800600.Aug 30, 2016 · N612JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA20160830781Seat Track · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON SEAT TRACK AT FRAME 64-66 -Y1292. R & R SEAT TRACK FRAME 64-68 - Y1292 IAW SRM 51-72-11, REV 114-0, SRM 51-42-11, REV 114, PN D5347219021100.Aug 30, 2016 · N612JB · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR YENA20160830780Floorbeam · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM AT FRAME 66-68 -Y1162 THROUGH -Y1292. R & R FLOORBEAM FRAME 66-FRAME 68 BETWEEN -Y1162 THROUGH -Y1292 IAW SRM 51-72-11, REV 114, SRM 51-42-11, REV 114, PN D5347217220500.Aug 30, 2016 · N612JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA20160830779Seat Track · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON SEAT TRACK AT FRAME 12-24-Y1292. R & R SEAT TRACK FRAME 12-24-Y1292 IAW SRM 51-72-11 REV 114 & SRM 51-42-11, REV 114.Aug 30, 2016 · N612JB · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR YENA20160830778Seat Track · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON SEAT TRACK AT FRAME 64-67-Y765. R & R SEAT TRACK FRAME 64-67-Y765 IAW SRM 51-72-11, REV 114 & SRM 51-42-11, REV 114.Aug 30, 2016 · N612JB · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR YENA20160830777Floorbeam · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM AT FRAME 64-67-Y465. R & R FLOORBEAM, FRAME 64-67-Y465 IAW SRM 51-72-11 REV 114 & SRM 51-42-11, REV 114.Aug 30, 2016 · N612JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA20160830776Floorbeam · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM AT FRAME 12-16, Y503.2. R & R FLOORBEAM FRAME 12-24, Y1292 IAW SRM 51-72-11 REV 114 & SRM 51-42-11, REV 114, PN D53112600200.Aug 30, 2016 · N612JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA20160830775Floorbeam · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM AT FRAME 67-70 -Y765. R & R FLOORBEAM, FRAME 67-70, Y765. REPLACED IAW SRM 51-72-11, REV 114 AND SRM 51-42-11, REV 144, PN D5347219320000.Aug 30, 2016 · N612JB · Airbus A320232 · Fuselage Main, Floor Beam
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