# Service difficulty reports: N547JB

A list on [N547JB](https://openairdocs.org/aircraft/N547JB.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 · 72 reports

- [SDR YENA2026072000606](https://openairdocs.org/sdr/YENA2026072000606.md): Unknown · odor · Jul 18, 2026 · N547JB · Airbus A320232 · Air Distribution System
  > FLT 1468, PBI-HPN. DURING FLIGHT, ONE FLIGHT ATTENDANT REPORTED A DIRTY SOCK ODOR IN AFT GALLEY. LATER, ONE OTHER FLIGHT ATTENDANT SAID SO AS WELL.. INSPECTED & CLEANED AFT GALLEY FLOOR. ALSO REPLACED AFT LAV SINK DRAIN FILTERS AS REQ. NO FOUL ODOR DETECTED A
- [SDR YENA2025072800777](https://openairdocs.org/sdr/YENA2025072800777.md): Condenser · faulted · Jul 27, 2025 · N547JB · Airbus A320232 · Air Distribution System
  > FLT#1058, AUA-JFK. STRONG CHEMICAL ODOR EXPERIENCED BY INFLIGHT CREW UPON ARRIVAL AND INTENSIFIED AFTER LANDING. ( PACKS); REF LOG PAGE # 4318901 ITEM # 2 (REMOVED AND REPLACED PACK # 1 CONDENSER IAW AMM 21-52-32 REF L/P 4318902 ITEM # 1 FOR OPS CHK/LEAK CHK)
- [SDR YENA2025072500768](https://openairdocs.org/sdr/YENA2025072500768.md): Apu · odor · Jul 25, 2025 · N547JB · Airbus A320232 · Airborne Auxiliary Power Unit (APU) System
  > FLT#66, ABQ-JFK. "FUMES EVENT DURING APPROACH AND AT SHUT DOWN. ( APU SYSTEM)" (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA2025071400726](https://openairdocs.org/sdr/YENA2025071400726.md): Unknown · odor · Jul 11, 2025 · N547JB · Airbus A320232 · Air Distribution System
  > FLT#205, EWR-FLL. INFLIGHT REPORTED SLIGHT ODOR OF FUEL DURING TRANSITION FROM CRUISE TO DECENT; COMPLIED WITH INFO NOTICE 2017-T015, SECTION A ISOLATED FUALT TO TYPE 10-SUSPECT CUSTOMER WAS USING VIC'S IN ROW 3-4-PER TSM 05-50-00-810-085-B/TSM 05-50-00-810-08
- [SDR YENA2025070700683](https://openairdocs.org/sdr/YENA2025070700683.md): Unknown · odor · Jul 4, 2025 · N547JB · Airbus A320232 · Air Distribution System
  > FLT#1520, ATL-JFK,"DIRTY SOX ODOR ON DESCENT THROUGH 10.000 DISSIPATED WHEN PACK 2 SELECTED OFF; REF INFO NOTICE 2017-T015L AND TSM 05-50-00-810-831-A. NO PHYSICAL EVIDENCE OF OIL FOUND IN APU. ACCOMPLISHED BLEED ISOLATION PROCEDURE OF ENG #1, ENG #2, APU PACK
- [SDR YENA2025063000663](https://openairdocs.org/sdr/YENA2025063000663.md): Apu · odor · Jun 28, 2025 · N547JB · Airbus A320232 · Airborne Auxiliary Power Unit (APU) System
  > FLT#1075, MCO-PVD. "DURING DESCENT PILOTS AND FA'S EXPERIENCED A FUME EVENT. PILOTS NOTICED AN OIL SMELL AND FWD FA'S NOTICED BURNING RUBBER. A/C HAS FUME HISTORY. ( PACKS); REF LP#4197860 ITEM #2, APU ODOR IDETIFIED & CORRECTED. NO SMELL PRESENT AFTER DECON/
- [SDR YENA2025063000662](https://openairdocs.org/sdr/YENA2025063000662.md): Oil System · leaking · Jun 28, 2025 · N547JB · Airbus A320232 · APU Oil System
  > FLT#1434, SJU-MCO. "INFLIGHT CREW COMPLAINING OF A STRONG ODOR IN THE AFT OF THE AIRCRAFT FLIGHT ODOR SURVEY COMPLETED; COMPLIED WITH INFORMATION NOTICE 2017-T015 OIL B2 TYPE 1 APU OIL LEAK DECONTAMINATION LEVEL A WAS ACCOMPLISHED PER TSM 05-50-00-510-085-B."
- [SDR YENA2024052300779](https://openairdocs.org/sdr/YENA2024052300779.md): Slide Raft · unwanted deploy · May 22, 2024 · N547JB · Airbus A320232 · Escape Slide
  > FLT#2814, LGA-ATL. 'R1 SLIDE DEPLOYED AT THE GATE UPON ARRIVAL AND DISARM ( PASSENGER OR OVER WING DOOR SLIDE/SLIDE RAFTS (WITHOUT PASSENGERS)); REFERENCE LP 3942333, ITEM #1 (REMOVED AND REPLACED R1 DOOR ESCAPE SLIDE IAW AMM 25-62-44-400-803 - A OPS CHECK R1
- [SDR YENA2024032600465](https://openairdocs.org/sdr/YENA2024032600465.md): Girt Bar · misinstalled · Mar 23, 2024 · N547JB · Airbus A320232 · Emergency Equipment
  > DURING HEAVY MAINTENANCE: L1 DOOR WOULD NOT INDICATED ARMED ON THE GROUND AFTER LANDING WITH HANDLE IN ARMED POSITION; REMOVED AND INSTALLED ESCAPE SLIDE RAFT LH L1 DOOR IAW AMM 25-62-44-400-007-A INSTALLED PROPERLY FGIRT BAR IN THE GIRT BAR ASSEMBLY AND PERFO
- [SDR YENA2024032600464](https://openairdocs.org/sdr/YENA2024032600464.md): Stringer · corroded · Mar 23, 2024 · N547JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 33L BTW FR 58 TO FR 59 AFT CARGO COMPARTMENT; (RESOLVED ON W/O: 1282303 TASKCARD: NR-00033) REF WO 2024-39/1, NR 2024-108494.PERFORMED REPAIR AT STRINGER 33L BTW FR 58 TO FR 59 AFT CARGO COMPARTMENT I.A.W. A320 SRM
- [SDR YENA2024032600463](https://openairdocs.org/sdr/YENA2024032600463.md): Frame · cracked · Mar 23, 2024 · N547JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: REF WO 2024-39/1, NR 2024-108496.CRACK INDICATION FOUND ON FRAME 16LH UPPER DOUBLE JOGGLE AREA HOLE C, CRACK DIRECTION 10 OCLOCK AND CRACK DEPTH = 0.071 INCH.; (RESOLVED ON W/O: 1282303 TASKCARD: NR-00040) REF2024-39/1, NR 2024-108496
- [SDR YENA2024032600462](https://openairdocs.org/sdr/YENA2024032600462.md): Frame · cracked · Mar 23, 2024 · N547JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16LH UPPER DOUBLE JOGGLE AREA HOLE 7, CRACK DIRECTION 2 OCLOCK AND CRACK DEPTH = 0.122 INCH.; (RESOLVED ON W/O: 1282303 TASKCARD: NR-00039) REF WO 2024-39/1,NR 2024-108497.PERFORMED REPAIR ON HOLE 7 LOC
- [SDR YENA2024032600461](https://openairdocs.org/sdr/YENA2024032600461.md): Frame · cracked · Mar 23, 2024 · N547JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16RH UPPER DOUBLE JOGGLE AREA HOLE #6, CRACK DIRECTION 1 O'CLOCK AND CRACK DEPTH = 0.119 INCH.; (RESOLVED ON W/O: 1282303 TASKCARD: NR-00041) REF AEROMAN W.O. 2024-39/1 NR 108500 & JB EC A24-300-01 * A
- [SDR YENA2024032600460](https://openairdocs.org/sdr/YENA2024032600460.md): Frame · cracked · Mar 23, 2024 · N547JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16RH UPPER DOUBLE JOGGLE AREA HOLE C, CRACK DIRECTION 7 OCLOCK AND CRACK DEPTH= 0.105 INCH.; (RESOLVED ON W/O: 1282303 TASKCARD: NR-00042) REF AEROMAN WO 2024 39/1 NR 2024-108498; ACCOMPLISHED REPAIR OF
- [SDR YENA2024032600459](https://openairdocs.org/sdr/YENA2024032600459.md): Frame · cracked · Mar 23, 2024 · N547JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16 RH UPPER DOUBLE JOGGLE AREA HOLE A, CRACK DIRECTION 9 O'CLOCK AND CRACK DEPTH = 0.108 INCH.; (RESOLVED ON W/O: 1282303 TASKCARD: NR-00043) REF AEROMAN W.O.2024CNR 108499 & JB EC A24-300-01 * ACCOMPLI
- [SDR YENA2024032600458](https://openairdocs.org/sdr/YENA2024032600458.md): Support · corroded · Mar 23, 2024 · N547JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOC, AT LEVEL FR,68 STRG 23L AT AFT GALLEY AREA ( REFER TO MPD TASK 534195-01); REF WO 2024-39/1, NR 2024108558.PERFORMED PERMANENT REPAIR ON FR 68, STR 23L AT LOWER SILL L/H I.A.W. A320 SRM 51-41-14-300-001, REPA
- [SDR YENA2024032600457](https://openairdocs.org/sdr/YENA2024032600457.md): Stringer · corroded · Mar 23, 2024 · N547JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 43L BTW FR 57 TO FR 58 AFT CARGO COMPARTMENT (CPCP RELATED REFER TO MPD TASK 534107-01); REF WO 2024-39/1,NR 2024-108480.PERFORMED REPAIR AT STRINGER 43L BTW FR 57 TO FR 58 AFT CARGO COMPARTMENT I.A.W. A320 SRM 53-0
- [SDR YENA2024032600456](https://openairdocs.org/sdr/YENA2024032600456.md): Support · corroded · Mar 23, 2024 · N547JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOC, AT LEVEL FR,68 STRG 23R AT AFT GALLEY AREA ( REFER TO THE MPD TASK 534195-01); REF WO 2024--39/1, NR 2024-108556,PERFORMED PERMANENT REPAIR ON FR 68, STR 23R AT LOWER SILL R/H I.A.W. A320 SRM 51-41-14-300-001
- [SDR YENA2024032600455](https://openairdocs.org/sdr/YENA2024032600455.md): Support · corroded · Mar 23, 2024 · N547JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOC, AT LEVEL FR,68 STRG 23R AT AFT GALLEY AREA ( REFER TO THE MPD TASK 534195-01); REF WO 2024--39/1, NR 2024-108556,PERFORMED PERMANENT REPAIR ON FR 68, STR 23R AT LOWER SILL R/H I.A.W. A320 SRM 51-41-14-300-001
- [SDR YENA2023040400314](https://openairdocs.org/sdr/YENA2023040400314.md): Unknown · unknown · Apr 2, 2023 · N547JB · Airbus A320232 · Air Conditioning System
  > FLT#491, BUF-LAX. 'DIRTY SOCK SMELL NOTED BY INFLIGHT DURING APPROACH; PERFORMED T/S PER TSM 05-50-00-810-831 LEVEL A DECONTAMINATION OF THE ENVIRONMENTAL CONTROL SYSTEM. NO ODOR NOTED AT THIS TIME.'
- [SDR YENA2023032700288](https://openairdocs.org/sdr/YENA2023032700288.md): Computer · failed · Mar 25, 2023 · N547JB · Airbus A320232 · Fuel Indicating System
  > FLT#751, JFK-CUN. (AIRCRAFT PERFORMED AN AIR TURNBACK TO JFK) ' FOB INOP WITH XX AND NO FUEL IND ON BOH LEFT WING TANKS; SUMPED FUEL AS PRECAUTIONARY REF AMM 12-32-28 AND REMOVED AND REPLACED FQIC IAW AMM 28-42-34. OPS CHECK NORMA.L A/C OK FOR SERVICE.'
- [SDR YENA2022122301286](https://openairdocs.org/sdr/YENA2022122301286.md): A/C Pack · malfunctioned · Dec 20, 2022 · N547JB · Airbus A320232 · Cabin Cooling System
  > FLT#1691, JFK-LIR. ' ( PACKS)ON DESCENT, NOTICED THE CABIN TEMP INCREASE TO 76-78DEG TURNED TEMP VALVE KNOBS TO A COOLER SETTING. BUT NO RESPONSE TURNED THE HOT AIR VALVE OFF AND TEMP COOLED SMELT HOT SMELT HOT IN IN COCKPIT BEFORE THE CABIN COOLED OFF. TURNE
- [SDR YENA2020012320046](https://openairdocs.org/sdr/YENA2020012320046.md): Skin · corroded · Jan 22, 2020 · N547JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION TRAILIG EDGE UPPER SKIN RIB 17 LH WING. ACCOMPLISHED REPAIR OF CORROSSION ON LH WING RIB 17 IAW EA 57-5094-19 REV 0 RDAS 70562381/121/2020. THIS REPAIR IS CLASSIFIED AS MAJOR.
- [SDR YENA2020012320045](https://openairdocs.org/sdr/YENA2020012320045.md): Skin · corroded · Jan 22, 2020 · N547JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION TRAILING EDGE ON UPPER SKIN LOWER SURFACE RIB 18 LH WING; REF AEROMAN NR 2019-407615 WO 2019 335/1 ACCOMPLISHED REPAIR OF CORROSSION ON LH WING RIB 18 IAW AEROMAN EA 57-5094-19 REV O & AIRBUS RDAS 70562381/121 2020. THIS REP
- [SDR YENA2020012320044](https://openairdocs.org/sdr/YENA2020012320044.md): Skin · dented · Jan 22, 2020 · N547JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, DENT EXTERNAL SKIN LOC FR24 MORE 4 IN BTW STR 42-43 LOWER FUSELAGE; (REF AEROMAN NR 2019 407515 WO 2019 335/1) ACCOMPLISHED REPAIR AT THE DENT & DAMAGE FR 24-24A STR 42L-43L IAW AEROMAN EA 53-0025-20 REV O RDAS 807336681003/2020. THIS
- [SDR YENA2019102400612](https://openairdocs.org/sdr/YENA2019102400612.md): Battery Pack · no test · Oct 20, 2019 · N547JB · Airbus A320232 · Emergency Lighting
  > FT # 225, JFK-TPA. EMERG LIGHT BATTERIES 11WL AND 13WL FAILED TEST; REMOVED AND REPLACED EMER LIGHT BATTERIES 11WL AND 13WL IAW AMM 33-51-38.
- [SDR YENA2019102400611](https://openairdocs.org/sdr/YENA2019102400611.md): Battery · no test · Oct 20, 2019 · N547JB · Airbus A320232 · Emergency Lighting
  > FT # 225, JFK-TPA. EMERG LIGHT BATTERIES 11WL AND 13WL FAILED TEST; REMOVED AND REPLACED EMER LIGHT BATTERIES 11WL AND 13WL IAW AMM 33-51-38.
- [SDR YENA2019040530176](https://openairdocs.org/sdr/YENA2019040530176.md): Battery Pack · no test · Apr 3, 2019 · N547JB · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILED AT 10WL. REMOVED & REPLACED FWD EMERGENCY LIGHT BATTERY FIN 10WL IAW AMM 33-51-38.
- [SDR YENA2018080850306](https://openairdocs.org/sdr/YENA2018080850306.md): Unknown · odor · Aug 5, 2018 · N547JB · Airbus A320232 · Air Distribution System
  > F/A COMPLAINED OF ODORS IN AFT GALLEY. TRANSIENT IRRITATION AND HEADACHE OCCURRED, PETROLEUM LIKE ODOR. PERFORMED TSM 05-50-00-810-831-A. RAN PACKS AND FOUND NO CAUSE OF ODOR. INSPECTED CABIN WITH NO ODOR NOTED. PERFORMED EXTERNAL VISUAL AND CARGO BIN INSP
- [SDR YENA201805120917](https://openairdocs.org/sdr/YENA201805120917.md): Frame · cracked · May 12, 2018 · N547JB · Airbus A320232 · Fuselage Main, Frame
  > DURING C-9 MTC VISIT DATED 05/18, DURING ACCOMPLISHMENT OF THE REF.(4) SPECIAL DETAILED INSPECTION OF THE FR 16 & 20 LT & RT CROSSBEAM SPLICING, A CRACK WAS FOUND ON FASTENER HOLE B ON THE LT SIDE FRAME 16 AT THE CROSSBEAM SPLICING JOINT. SEE REF.(1) FOR DETAI
- [SDR YENA201805120440](https://openairdocs.org/sdr/YENA201805120440.md): Door Sill · corroded · May 12, 2018 · N547JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON R2 PAX DOOR SILL FR66-68 STR 23R SHAPE SILL HAS 3 EA. REMOVED CORROSION VERIFIED BEYOND LIMITS R2 SHAPE (LOWER CORNER) SILL FR67 +18" IAW SRM 53-41-79-283-001. REMOVED AND REPLACED IAW SRM 53-41-79 FIG002.
- [SDR YENA201805120439](https://openairdocs.org/sdr/YENA201805120439.md): Shear Plate · corroded · May 12, 2018 · N547JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RT AFT SHEAR PLATE WEB FRAME ON LOWER SURFACE FR 69+10" STR 23R. REMOVED AND REPLACED RT AFT SHEAR PLATE WEB FRAME HAS CORROSION ON LOWER SURFACE FR 69+10" STR 23R.
- [SDR YENA201805120438](https://openairdocs.org/sdr/YENA201805120438.md): Floorbeam · corroded · May 12, 2018 · N547JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON MAIN CABIN FLOORBEAM -Y1292 FR20 STR23. REMOVED AND REPLACED MAIN CABIN FLOORBEAM -Y1292 FR20 STR23 IAW SRM 53-11-14-283-004.
- [SDR YENA201805120437](https://openairdocs.org/sdr/YENA201805120437.md): Shear Plate · corroded · May 12, 2018 · N547JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LT AFT SHEAR PLATE WEB FRAME HAS CORROSION ON LOWER SURFACE FR69+10' STR23L. REMOVED AND REPLACED LT AFT SHEAR PLATE WEB FRAME HAS CORROSION ON LOWER SURFACE FR69+10' STR23L IAW SRM 53-41-14 FIG 002.
- [SDR YENA2018051620201](https://openairdocs.org/sdr/YENA2018051620201.md): Skin · corroded · May 12, 2018 · N547JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE LT WING UPPER SKIN. PERFORMED REWORK REPAIR ON AREA OF CORROSION 4A WING TOP SURFACE RIB 1+18" STR 6 IAW RAS 6213321 TD/80452321/005/2018#A,REWORK ARE REQ REINSP AT 40,500 FC OR 81,100 FH WHICHEVER OC
- [SDR YENA201710170846](https://openairdocs.org/sdr/YENA201710170846.md): Safety Valve · failed · Oct 17, 2017 · N547JB · Airbus A320232 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, AN ECAM MESSAGE FOR THE LANDING GEAR NOT UPLOCKED. LANDED. AFTER LANDING, LOST NOSE WHEEL STEERING; FOUND GREEN SYS SAFETY VALVE STUCK OPEN. R & R THE SAFETY VALVE IAW AMM 32-31-17-400-001. TESTED THE LANDING GEAR IAW AMM 32-31-00-720-002.
- [SDR YENA201708100655](https://openairdocs.org/sdr/YENA201708100655.md): Unknown · odor · Aug 10, 2017 · N547JB · Airbus A320232 · Air Distribution System
  > RECEIVED A CALL FROM AFT GALLEY DURING CLIMB ABOVE FL230 THAT A DIRTY SOCK ODOR WAS PRESENT IN THE REAR GALLEY. 15 MINUTES LATER, LEARNED OF PHYSICAL SYMPTOMS PRESENT OF THE NR 2 AND 3 FLIGHT ATTENDANTS. THROAT IRRITATION AND NAUSEUSNESS. CONFERED WITH MX C
- [SDR YENA201704020235](https://openairdocs.org/sdr/YENA201704020235.md): Skin · corroded · Apr 2, 2017 · N547JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY CHECK, CORROSION WAS DISCOVERED ON UPPER SKIN OF THE RIGHT WING RIB 12 & 16.5, STRINGER 11. THE SKIN WAS BLENDED IAW SRM 51-74-00, AND EC A17-284-01. MAJOR REPAIR.
- [SDR YENA201704020234](https://openairdocs.org/sdr/YENA201704020234.md): Battery Pack · no test · Apr 2, 2017 · N547JB · Airbus A320232 · Emergency Lighting
  > DURING A HEAVY CHECK, AFT CABIN EMERGENCY LIGHTS FAILED TO ILLUMINATE WITH THE SWITCH IN ARM AND THE 1WEL AND 2WL CIRCUIT BREAKERS PULLED. R & R THE BATTERY PACK 13WL IAW AMM 33-51-38-000-002-A, AND 33-51-38-400-002-A. OPS CHECKED GOOD IAW AMM 33-51-00-710-0
- [SDR YENA201704020233](https://openairdocs.org/sdr/YENA201704020233.md): Skin · dented · Apr 2, 2017 · N547JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY CHECK, A DENT WAS DISCOVERED ON FUSELAGE SKIN AT FRAME 69+15, STRINGER 20R. CUTOUT THE DAMAGED AREA AND FABRICATED A REPAIR DOUBLER AND INSTALLED IAW SRM 53-41-11-300-018.
- [SDR YENA201701120027](https://openairdocs.org/sdr/YENA201701120027.md): Battery · discharged · Jan 12, 2017 · N547JB · Airbus A320232 · Emergency Lighting
  > FLT 6445, JFK-SAL. EMERGENCY BATTERY WAS FOUND TO BE DISCHARGED AFT L POSITION (13WL). R & R BATTERY AND PERFORMED TEST IAW AMM 33-51-38-400-002-A. TEST PASSED.
- [SDR YENA20160731674](https://openairdocs.org/sdr/YENA20160731674.md): Control Servo · failed · Jul 31, 2016 · N547JB · Airbus A320232 · Landing Gear Steering System
  > FLT 1704, DURING CRUISE, FLIGHT CREW RECIEVED SEVERAL NOSE WHEEL STEERING FAULT ON ECAM. EMERGENCY DECLARED. ACFT LANDED UNEVENTFULLY. R & R NW STEERING SERVO CONTROL (6GC). PERFORMED LEAK & OPS CHECK. LEAK & OPS CHECK PASSED.
- [SDR YENA20150616213](https://openairdocs.org/sdr/YENA20150616213.md): Beam · corroded · Jun 16, 2015 · N547JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE, FOUND AFT CABIN BEAM AT Y1292, FRAME 67 CORRODED. R & R BEAM IAW SRM 51-42-11 AND 53-00-14. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.
- [SDR YENA20150616198](https://openairdocs.org/sdr/YENA20150616198.md): Beam · corroded · Jun 16, 2015 · N547JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE, FOUND AFT CABIN BEAM AT -Y1292, FRAME 67 CORRODED. R & R BEAM IAW SRM 51-42-11 AND 53-00-14.
- [SDR YENA20150616212](https://openairdocs.org/sdr/YENA20150616212.md): Fitting · corroded · Jun 16, 2015 · N547JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE, FOUND CORNER FITTING AT FRAME 68 CORRODED. REPLACED CORNER FITTING IAW SRM REF 51-42-11.
- [SDR YENA20150616211](https://openairdocs.org/sdr/YENA20150616211.md): Door Sill · corroded · Jun 16, 2015 · N547JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, FOUND L2 DOOR SILL CORRODED AT FRAME 68, STRINGERS 23L. REPAIRED L2 DOOR SILL AT FRAME 68 IAW SRM REF 53-41-14.
- [SDR YENA20150616210](https://openairdocs.org/sdr/YENA20150616210.md): Attach Fitting · corroded · Jun 16, 2015 · N547JB · Airbus A320232 · Fuselage Main, Attach Fittings
  > DURING HEAVY MAINTENANCE, FOUND L2 DOOR SILL AT FRAME 66 GIRT BAR ATTACH FITTING AT THE AFT OTBD FASTENER HOLE CORRODED. REAMED CORRODED HOLE AND REPAIRED IAW SRM REF 53-41-14, FIG 201. THIS ITEM HAS BEEN CLASSIFIED AS A LEVEL 2 CORROSION.
- [SDR YENA20150616209](https://openairdocs.org/sdr/YENA20150616209.md): Door Sill · corroded · Jun 16, 2015 · N547JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, FOUND L2 DOOR SILL CORRODED AT FRAME 66. REPAIRED L2 DOOR SILL AT FR 66 IAW SRM.
- [SDR YENA20150616208](https://openairdocs.org/sdr/YENA20150616208.md): Floorbeam · corroded · Jun 16, 2015 · N547JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, FOUND AFT CABIN LT FLOORBEAM AT FRAME 68, Y512 CORRODED. REPLACED BEAM IAW SRM REF 51-42-11.
- [SDR YENA20150616207](https://openairdocs.org/sdr/YENA20150616207.md): Structure · corroded · Jun 16, 2015 · N547JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE FOUND AFT CABIN RT BEAM AT FRAME 68; -Y765 CORRODED. REPLACED BEAM IAW SRM 51-72-11.

Next page: https://openairdocs.org/aircraft/N547JB/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 = 'N547JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N547JB/reports

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