# Service difficulty reports: N706JB

A list on [N706JB](https://openairdocs.org/aircraft/N706JB.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 · 54 reports

- [SDR YENA2026062900499](https://openairdocs.org/sdr/YENA2026062900499.md): Unknown · odor · Jun 25, 2026 · N706JB · Airbus A320232 · Air Distribution System
  > FLT 65, JFK-ABQ(DIVERTED TO ICT). PAX AND FA'S REPORTED STRONG ODOR OF GASOLINE IN THE AFT CABINN AND AFT GALLEY AFTER LANDING CUSTOMERS SAID IT WAS MORE OF A ROTTEN EGG ODOR THAN GASOLINE ( PACKS); PERFORMED LEVEL C DECONTAMINIATION APG 1 IAW AMM 05-50-00-80
- [SDR YENA2026060800465](https://openairdocs.org/sdr/YENA2026060800465.md): Unknown · fumes · Jun 5, 2026 · N706JB · Airbus A320232 · Air Distribution System
  > FLT 141, BDI--PBI. LEVEL 3 FUME ON DECENT. APPLIED ODOR/ FUME ISOL/ PROCEDURE PACK 1 / FLIGHT DECK; COMPLIED WITH INFORMATION NOTICE 2017-T015, STEPS 1 AND 2. IDENTIFIED ODOR TYPE 1 (APU) DEACTIVATED DECONTAMINATION LEVEL 1 WAS ACCOMPLISHED PER TSM 05-50-00-8
- [SDR YENA2026052600482](https://openairdocs.org/sdr/YENA2026052600482.md): Battery Pack · failed · May 25, 2026 · N706JB · Airbus A320232 · Emergency Lighting
  > DURING MAINTENANCE: "EMERG BATT 10WL FAILED TEST; REMOVED NAD REPLACED 10WL EMERG BATT IAW AMM 33-51-00 OPS CHK GOOD. A/C OK CONT SVC."
- [SDR YENA2025051900502](https://openairdocs.org/sdr/YENA2025051900502.md): Unknown · odor · May 15, 2025 · N706JB · Airbus A320232 · Air Distribution System
  > FLT#1962, PBI-LGA. '2 AFT F/A'S REPORTED FUME EVENT AT GATE ARRIVAL. IT BEGAN AT TOP OF DESCENT AND DISSIPATED DURING THE DESCENT. NO APU WAS OPERATING; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION A, ISOLATED FAULT TO TYPE 10, AMBIENT AIR HIGH HUMIDITY
- [SDR YENA2025051900501](https://openairdocs.org/sdr/YENA2025051900501.md): Unknown · odor · May 15, 2025 · N706JB · Airbus A320232 · Air Distribution System
  > FLT#1461, LGA-PBI. 'FLIGHT ATTENDANT REPORTED SMELL A FLUID BURNING SMELL AT 1800F DECENT TO APPROXIMATELY 1000 FT SMELL CAME BACK JUST BEFORE LANDING FA SMELL 8 OF 10 REPORTS; PER INFO NOTICE 2017-T015L PERFORMED TSM 05-50-00-810-831-A ODOR VERIFIED TO BE MIS
- [SDR YENA2024112501496](https://openairdocs.org/sdr/YENA2024112501496.md): Valve · malfunctioned · Nov 23, 2024 · N706JB · Airbus A320232 · Cabin Temperature Control System
  > FLT#977, BOS-LAS. (AIRCRAFT DIVERTED TO ORD) 'AFT CABIN INDICATED 54* IN FLIGHT; PERFORMED OPERATIONAL TEST OF THE PACK TEMP CONTROL SYSTEM IAW AMM 21-61-00-710-001. TEST REVEALED TRIM AIR VALVE 12HK AND 13HK FAILED. WHEN TWO TRIM AIR VALVES FAIL THE HOT AIR V
- [SDR YENA2024082901186](https://openairdocs.org/sdr/YENA2024082901186.md): Door Frame · cracked · Aug 28, 2024 · N706JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR ( AFT RH EEH DOOR 844) CRACK L=0.135 INCH APPROX; REF AEROMAN W.O. 2024 150/1 N.R. 2024- 404155 * WORKED UNDER DOCUMENT CONTROL CARD #2024-460556 AND EC#
- [SDR YENA2024082901185](https://openairdocs.org/sdr/YENA2024082901185.md): Door Frame · cracked · Aug 28, 2024 · N706JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION WERE FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR (FWD LH EEH DOOR 833) CRACK L=0.130 INCH APRPROX; REF AEROMAN W.O. 2024 150/1 N.R. 2024- 404156 * WORKED UNDER DOCUMENT CONTROL CARD #2024-460553 AND EC#
- [SDR YENA2024082901184](https://openairdocs.org/sdr/YENA2024082901184.md): Door Frame · cracked · Aug 28, 2024 · N706JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION WAS FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR ( FWD RH EEH DOOR 843) CRACK L=0.200 INCH APPROX; REF AEROMAN W.O. 2024 150/1 N.R. 2024- 404156 * WORKED UNDER DOCUMENT CONTROL CARD #2024-460554 AND EC#
- [SDR YENA2024082901183](https://openairdocs.org/sdr/YENA2024082901183.md): Door Frame · cracked · Aug 28, 2024 · N706JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION WASA FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR (AFT LH EEH DOOR 834) CRACK L=0.220 INCH APPROX; REF AEROMAN W.O. 2024 150/1 N.R. 2024- 404156 * WORKED UNDER DOCUMENT CONTROL CARD #2024-460555 AND EC#
- [SDR YENA2024082901182](https://openairdocs.org/sdr/YENA2024082901182.md): Fitting · cracked · Aug 28, 2024 · N706JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON INTERCOSTAL FITTING I/B LOWER HOLE COMMON TO DOOR STOP FITTING Ñ7 AT FR16 RH. CRACK DIRECTION AT 9 O CLOCK VIEW LO OKING FORWARD; (RESOLVED ON W/O: 1313885 TASKCARD: NR-00050) REMOVED AND REPLACED INTERCOSTAL
- [SDR YENA2024082901181](https://openairdocs.org/sdr/YENA2024082901181.md): Skin · dented · Aug 28, 2024 · N706JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: DENT ON EXTERNAL SKIN BTW FR 28 AND FR 29 STRG 37L-38L; (RESOLVED ON W/O: 1313885 TASKCARD: NR-00052) PERFORMED PERMANENT REPAIR LOC. ON EXTERNAL SKIN BTW FR 28 AND FR 29 STRG 37L-38L IAW A320 SRM 53-21-11-300-093, THIS REPAIR IS CLAS
- [SDR YENA2024082901180](https://openairdocs.org/sdr/YENA2024082901180.md): Skin · dented · Aug 28, 2024 · N706JB · Airbus A320232 · Passenger/Crew Doors
  > DURING HEAVY MAINTENANCE: DENT ON PASSENGER (R1) CREW DOOR 841 LOWER AFT CORNER AT FWD GALLEY AREA; (RESOLVED ON W/O: 1313885 TASKCARD: NR-00055) 52PERFORMED REPAIR ON PASSENGER CREW DOOR 841 LOWER AFT CORNER AT FWD GALLERY AREA IAW A320 SRM 52-10-00-300-003 I
- [SDR YENA2024082901179](https://openairdocs.org/sdr/YENA2024082901179.md): Skin · damaged · Aug 28, 2024 · N706JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, TAIL CONE, FR 80-84 BOTH RT & LT SIDES, APU AIR INTAKE DUCT, THIS PERMANENT REPAIR HAS BEEN APPROVED VIA REF /3/RDAF AND IS CLASSIFIED AS MAJOR.(E/C: A24-1107-01)
- [SDR YENA2024062400895](https://openairdocs.org/sdr/YENA2024062400895.md): Ecs · odor · Jun 23, 2024 · N706JB · Airbus BD5001A11 · Air Distribution System
  > FLT#1077, MCO-PUJ. DUE TO ODOR EVENT AND GROUND TIME ODOR IN ALL PHASE OF FLIGHT; INSPECTED A/C AND FOUND ODOR TO BE LEVEL B IAW AMM 49-00-00-200-811-A. PERFORMED ECS DECON WITH ENGINES IAW AMM 21-00-00-615-803-A. FOUND FUEL, HYDRAULIC LEAKS AND APU COOLING FA
- [SDR YENA2024051500746](https://openairdocs.org/sdr/YENA2024051500746.md): Unknown · odor · May 13, 2024 · N706JB · Airbus A320232 · Air Distribution System
  > FLT#987, ORH-MCO. 'DIRTY SOCKS SMELLED BY ALL 4 FLIGHT ATTENDANTS AND FLIGHT DECK APU WAS ON, BLEEDS ON APU SMELL EQUAL THROUGHOUT THE CABIN; COMPLITED WITH INFORMATIONAL NOTICE 2017-T015, SECTION B1. DECONTAMINATION LEVEL B WAS ACCOMPLISHED PER TSM 05-50-00-7
- [SDR YENA2024050200699](https://openairdocs.org/sdr/YENA2024050200699.md): Unknown · odor · May 1, 2024 · N706JB · Airbus A320232 · Air Distribution System
  > FLT#1141, BDL-PBI. 'DIRTY SOCK/TAL SMELL DESCENDING THRU 9000' DISSIPATED SLIGHTLY WHEN PACK 1 SELECTED OFF.CABIN ODOR REPORTING FORM COMPLETE; ACCOMPLISHED TASKS IAW INFO NOTICE 2017-T015J,ACCOMPLISHED TSM 05-50-00-810-831-A. DETERMINED THAT ODOR EVENT IS A
- [SDR YENA2023121501588](https://openairdocs.org/sdr/YENA2023121501588.md): Unknown · unknown · Dec 12, 2023 · N706JB · Airbus A320232 · Air Distribution System
  > FLT#737, BDL-MCO. 'ON SHORT FINAL WE SMELLED THE "DIRTY SOCK SMELL" ON THE FLIGHT DECK. DURING DEPLANING THE FLIGHT ATTENDANTS COMPLAINED OF THE SAME SMELL OCCURRING RIGHT BEFORE LANDING; COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION B2. DECONTAMINATION L
- [SDR YENA2023090501033](https://openairdocs.org/sdr/YENA2023090501033.md): Filter · failed · Sep 1, 2023 · N706JB · Airbus A320232 · Air Distribution System
  > FLT#626, FLL-RDU. 'ODOR/ FUME EVENT: LEVEL 2 AFT FLIGHT ATTENDANTS REPORTED SMELLING DIRTY SOCKS " SMELL SHORTLY AFTER THE 10000 CHIME ON DESCENT INTO RDU. CLEAR SKIES, NO CLOUDS, FIRST OFFICER REPORTED ODOR SMELL AROUND 3000FT ODOR DISSIPATED ON LANDING. ( PA
- [SDR YENA2022120501203](https://openairdocs.org/sdr/YENA2022120501203.md): Unknown · odor · Dec 4, 2022 · N706JB · Airbus A320232 · Air Distribution System
  > FLT#1433, MCO-SJU. 'DURING CRUISE AND DESCENT, THE INFLIGHT CREW DETECTED A CHEMICAL-TYPE ODOR IN THE FLIGHT ATTENDANT REPORTED A SCRATCHY SORE THROAT AND ONE FELT NAUSEATED. NO ODORS WERE DETECTED ON THE FLIGHT DECK; EXECUTED T/S AS PER INFO NOTICE 2017-7015
- [SDR YENA2022110301086](https://openairdocs.org/sdr/YENA2022110301086.md): Clamp · broken · Oct 25, 2022 · N706JB · Airbus A320232 · Waste Disposal System
  > FLT#113, MCO - CUN. '(AIRCRAFT PREFORMED AN AIR TURN BACK TO MCO).' "PREVIOUS WRITE-UP" ON CLIMB OUT, CRUISE, AND DESCENT CONSTANT VIBRATION IN COCKPIT / CABIN FILLED OUT ACFT VIB FORM MCC REQUESTED RTB ALL PARAMETER, ON VIB FORM; REF LP # 3482684, ITEM 2 (RIG
- [SDR YENA2022090200861](https://openairdocs.org/sdr/YENA2022090200861.md): None · none · Aug 29, 2022 · N706JB · Airbus A300* · Engine Cowling System
  > FLT#2457, LGA-DEN. (AIRCRAFT DIVERTED TO JFK) 'ENG 1 VIBRATION IN CLIMB ABOVE 10,000 THROUGH FL200 HIGH VIB NOTED 1.7 FLUCTUATE BETWEEN0.1-1.6 ON DECENT. VIBRATION FELT BY PAX AND FA DURING CLIMB; SYSTEM CHECKED AND PERFORMED FAN TRIM BALANCE WITH EVMU ONE-SH
- [SDR YENA2022060600554](https://openairdocs.org/sdr/YENA2022060600554.md): Actuator · failed · Jun 6, 2022 · N706JB · Airbus A320232 · Compressor Bleed Control
  > FLT#942, LAX-RNO. (AIRCRAFT PERFORMED AN AIR TURN BACK TO LAX) 'ENG 2 COMPRESSOR VANE ECAM; CLM REPORTS B25TK FOR ENGINE 2 REF TSM 75-30-00-810-850. BLEED 2.5ACT FAIL ON BOTH FADEC CHANNELS. REMOVED AND REPLACED 2.5 BLEED MASTER ACTUATOR PER AMM 75-31-42 PB 40
- [SDR YENA2022042200391](https://openairdocs.org/sdr/YENA2022042200391.md): None · none · Apr 19, 2022 · N706JB · Airbus A320232 · Fire Protection System
  > FLT#1475, BDL-SJU. 'SMOKE FWD AND AFT CARGO SMOKE ECAM MESSAGES; PERFORMED T/S PER TSM 26-16-00-810-805-A. FOUND NO EVIDENCE OF SMOKE OR FIRE ON FWD OR AFT CARGO. CLEANED AND INSPECTED FWD AND AFT CARGO SMOKE DETECTORS. NO DEFECTS WERE NOTED. ACCOMPLISHED COND
- [SDR YENA2021070200427](https://openairdocs.org/sdr/YENA2021070200427.md): Slide · abnormal · Jul 9, 2021 · N706JB · Airbus A320232 · Escape Slide
  > DURING HEAVY MAINTENANCE, SAFETY PIN CANNOT BE INSERTED ON EMERGENCY EVACUATION SLIDE/RAFT VALVE REGULATOR DOOR 832 AT AFT GALLEY AREA. PERFORMED CONTROLLED DEPLOYMENT OF ESCAPE SLIDE DOOR 832 IAW AMM 25-62-00-710-001-A AND PERFORMED OPERATIONAL TEST IS OK.
- [SDR YENA2020013060075](https://openairdocs.org/sdr/YENA2020013060075.md): Battery · no test · Jan 26, 2020 · N706JB · Airbus A320232 · Emergency Lighting
  > ON BATTERY CAPACITY CHECK (12WL) THE BATTERY FAIL, REPLACED THE BATTERY (12WL) IAW AMM 33-51-00.
- [SDR YENA2018092100353](https://openairdocs.org/sdr/YENA2018092100353.md): Battery · discharged · Sep 20, 2018 · N706JB · Airbus A320232 · Emergency Lighting
  > FLT 225, JFK-TPA. EPSU BATTERY 11WL FAILS EMERGENCY LIGHT SYSTEM TEST. R&R EPSU 11WL BATTERY IAW AMM 33-51-38, SYSTEM OPS CHECKS GOOD.
- [SDR YENA201808070941](https://openairdocs.org/sdr/YENA201808070941.md): Skin Panel · corroded · Sep 11, 2018 · N706JB · Airbus A320232 · Wing, Plate/Skin
  > SUPPLEMETAL INFORMATION (DIFFICULTY DATE CHANGE): DURING HEAVY MAINTENANCE, WAS FOUND WITH CORROSION TO THE UPPER AND LOWER SURFACES OF TOP SKIN PANEL 2 BETWEEN WX3622 – WX4490.52 AT THE TRAILING EDGE OVERHANG ON THE LEFT HAND WING. NDT INSPECTION REPORTS INDI
- [SDR YENA2018101010653](https://openairdocs.org/sdr/YENA2018101010653.md): Spar · corroded · Sep 11, 2018 · N706JB · Airbus A320232 · Wing Spar
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REAR SPAR T/E LOWER SURFACE BTW RIB 7 TO RIB 8 ON LT WING; PERFORMED PERMANENT REPAIR ON REAR SPAR T/E UPPER AND LOWER SURFACE BTW RIB 7 TO RIB 9 ON LT WING IAW EA 57-0223 -18 REV 0 AND EC A18-704-01 THIS R
- [SDR YENA2018101010652](https://openairdocs.org/sdr/YENA2018101010652.md): Spar · corroded · Sep 11, 2018 · N706JB · Airbus A320232 · Wing Spar
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON REAR SPAR T/E LOWER SURFACE BTW RIB 7 TO RIB 8 ON LT WING 1EA; PERFORMED PERMANENT REPAIR ON REAR SPAR T/E UPPER AND LOWER SURFACE BTW RIB 7 TO RIB 9 ON LT WING IAW EA 57-0223 -18 REV 0 AND EC A18-704-01 TH
- [SDR YENA2018101010651](https://openairdocs.org/sdr/YENA2018101010651.md): Support Frame · corroded · Sep 11, 2018 · N706JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON SUPPORT FRAME FROM FR 69 TO 70 AND STR 23L AT AFT GALLEY AREA; REPLACED SUPPORT FRAME LOC FR 69 TO FR 70 AND STR AT AFT GALLEY AREA IAW SRM 51-72-11, SRM 51-42-11 AND DRAWING D53474180. ALL WORK ACCOMPLISHE
- [SDR YENA2018101010650](https://openairdocs.org/sdr/YENA2018101010650.md): Door Sill · corroded · Sep 11, 2018 · N706JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LOWER SILL AT LEVEL FR 66 AND S-23R AT AFT GALLEY AREA; REPLACED LOWER SILL AND FASTENERS LOC AT LEVEL STR 23R AND BTW FR 66 TO 68 AT AFT GALLEY AREA IAW SRM 51-42-11 AND DRAWING D53480505 SRM 51-72-11. ALL
- [SDR YENA2018101010649](https://openairdocs.org/sdr/YENA2018101010649.md): Floorbeam · corroded · Sep 11, 2018 · N706JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM -Y254 BTW FR 12 TO 18 AT FWD GALLEY AREA; REPLACED FLOORBEAM -Y254 IAW SRM 51-72-11. WORK ACCOMPLISHED ON NR 2018-261159.
- [SDR YENA2018101010648](https://openairdocs.org/sdr/YENA2018101010648.md): Floorbeam · corroded · Sep 11, 2018 · N706JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM +Y254 AT FRAME 18 +3 INCHES AT FWD GALLEY AREA; PERFORMED PERMANENT REPAIR LOCATED ON FLOORBEAM +254 AT FRAME 18 +3 IAW SRM 53-11-14-300-002. WORK ACCOMPLISHED ON NR 2018-261162.
- [SDR YENA2018101010647](https://openairdocs.org/sdr/YENA2018101010647.md): Floorbeam · corroded · Sep 11, 2018 · N706JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM -Y765 BTW FR 67 TO FR 69 AFT GALLEY AREA; REPLACED FLOORBEAM -Y765 IAW SRM 53-72-11. WORK ACCOMPLISHED ON NR 2018-261212.
- [SDR YENA2018101010646](https://openairdocs.org/sdr/YENA2018101010646.md): Floorbeam · corroded · Sep 11, 2018 · N706JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM -Y765 BTW FR 67 TO FR 69 AFT GALLEY AREA; REPLACED FLOORBEAM IAW SRM 53-72-11. WORK ACCOMPLISHED ON NR 2018-261212.
- [SDR YENA2018101010645](https://openairdocs.org/sdr/YENA2018101010645.md): Floorbeam · corroded · Sep 11, 2018 · N706JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM -Y765 BTW FR 67 TO FR 69 AFT GALLEY AREA; REPLACED FLOORBEAM -Y765 IAW SRM 51-72-11. WORK ACCOMPLISHED ON NR 2018-261212.
- [SDR YENA2018101010644](https://openairdocs.org/sdr/YENA2018101010644.md): Floorbeam · corroded · Sep 11, 2018 · N706JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM -Y765 BTW FR 67 TO FR 69 AFT GALLEY AREA; REPLACED FLOORBEAM -Y765 IAW SRM 51-72-11. WORK ACCOMPLISHED ON NR 2018-261212.
- [SDR YENA2018101010643](https://openairdocs.org/sdr/YENA2018101010643.md): Seat Track · corroded · Sep 11, 2018 · N706JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON SEAT TRACK =Y1292 LOCATED AT FR 66 AT AFT GALLEY AREA; REPLACED SEAT TRACK =Y1292 IAW SRM 51-72-11. WORK ACCOMPLISHED ON NR 2018-261210.
- [SDR YENA2018101010642](https://openairdocs.org/sdr/YENA2018101010642.md): Seat Track · corroded · Sep 11, 2018 · N706JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON SEATTRACK +Y1292 LOCATED AT FR 66 AT AFT GALLEY AREA; REPLACED SEAT TRACK IAW SRM 51-72-11. WORK ACCOMPLISHED ON NR 2018-261210.
- [SDR YENA2018101010641](https://openairdocs.org/sdr/YENA2018101010641.md): Floorbeam · corroded · Sep 11, 2018 · N706JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BEAM FLOOR STRUCTURE LOCATED AT +Y1175 AND FR68 AT AFT GALLEY AREA; REPLACED FLOORBEAM LOCATED +Y1175 AND BTW FR 67+18" TO FR 69 IN AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472780.
- [SDR YENA2018101010640](https://openairdocs.org/sdr/YENA2018101010640.md): Floorbeam · corroded · Sep 11, 2018 · N706JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BEAM FLOOR STRUCTURE LOCATED AT +Y1175 + AND FR 68 AT AFT GALLEY AREA; REPLACED FLOORBEAM LOCATED AT +Y1175 IAW SRM 51-72-11. REF NR 2018-261213.
- [SDR YENA2018101010639](https://openairdocs.org/sdr/YENA2018101010639.md): Floorbeam · corroded · Sep 11, 2018 · N706JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM Y765 BETWEEN FR 67 TO FR 69 AT AFT GALLEY AREA; REPLACED FLOORBEAM Y765 IAW SRM 51-72-11. WORK ACCOMPLISHED ON NR 2018-261211.
- [SDR YENA2018101010638](https://openairdocs.org/sdr/YENA2018101010638.md): Floorbeam · corroded · Sep 11, 2018 · N706JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM Y765 BETWEEN FR 67 TO FR 69 AT AFT GALLEY AREA; REPLACED FLOORBEAM Y765 IAW SRM 51-72-11. WORK ACCOMPLISHED ON NR 2018-261211.
- [SDR YENA2018101010637](https://openairdocs.org/sdr/YENA2018101010637.md): Floorbeam · corroded · Sep 11, 2018 · N706JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM LOCATED -Y1175 AND FR 68 AT AFT GALLEY AREA; REPLACED FLOORBEAM IAW SRM 51-72-11. WORK ACCOMPLISHED OM NR 2018-261214.
- [SDR YENA2018101010636](https://openairdocs.org/sdr/YENA2018101010636.md): Floorbeam · corroded · Sep 11, 2018 · N706JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM LOCATED -Y1175 AND FR 68 AT AFT GALLEY AREA; REPLACED FLOORBEAM IAW SRM 51-72-11. WORK ACCOMPLISHED ON NR 2018-621214.
- [SDR YENA2018101010635](https://openairdocs.org/sdr/YENA2018101010635.md): Floorbeam · corroded · Sep 11, 2018 · N706JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM LOCATED -Y1175 AND FR 68 AT AFT GALLEY AREA; REPLACED FLOORBEAM IAW SRM 51-72-11. WORK ACCOMPLISHED ON NR 2018-261214.
- [SDR YENA2018101010634](https://openairdocs.org/sdr/YENA2018101010634.md): Dummy Rail · corroded · Sep 11, 2018 · N706JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RAIL DUMMY Y503.2 AT FRAME 16 AT FWD GALLEY AREA; REPLACED DUMMY RAIL IAW SRM 51-72-11. WORK ACCOMPLISHED ON NR 2018-261158.
- [SDR YENA201712030976](https://openairdocs.org/sdr/YENA201712030976.md): Transducer · malfunctioned · Dec 3, 2017 · N706JB · Airbus A320232 · Engine Oil Indicating System
  > FT # 41, FLL-MDE. RETURNED TO FIELD (FLL); ENG 2 BEARING 4 OIL SYS "HI-PRESS" MESSAGE ON ECAM/RETURN TO KFLL AS PER COMPANY MX/DISP. R & R ENG #2 XCDR NO4 BEARING PRESS IAW AMM 79-33-16. LEAK CK & OPS CK GOOD. NO FAULTS AT THIS TIME.
- [SDR YENA20151111551](https://openairdocs.org/sdr/YENA20151111551.md): Handle · stuck · Nov 12, 2015 · N706JB · Airbus A320232 · Trailing Edge Flap Control System
  > FLAP HANDLE STUCK AT 2. RETURNED TO FIELD. NO OVERWEIGHT LANDING. R & R FLAP HANDLE IAW AMM 27-51-43, ALL OPS CK OK.

Next page: https://openairdocs.org/aircraft/N706JB/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 = 'N706JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N706JB/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.