N606JB

Service difficulty reports · 54

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 = 'N606JB' 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 YENA2026080700658Fan · failedFLT 588, MCO-ORH. AT FL 350 VERY HEAVY ELECTRICAL ODOR IN COCKPIT. CIRCUIT BREAKER X-18 POPPED AND ODOR SUBSIDED - LT RECIRC INOP FANS; R & R LT RECIRC FAN IAW AMM 21-21-51. OPS CK GOOD PLACARD REMOVED MX4 UPDATEDAug 5, 2026 · N606JB · Airbus A320232 · Air Distribution FanSDR YENA2026030900284Unknown · odorFLT # 1245 ISP-PBI. " ODOR/SMELL DURING DESCENT THRU 9000' IDLE POWER.ONLY IN THE COCKPIT PREVIOSLY WRITTEN UP.DEFECT#4620792.; ACCOMPLISHED INFO NOTICE 2017-T015 M VERIFIED ODOR TO BE A MISCELLANIOUS TYPE 10 A LIGHT CHLORINE ODOR.AS PER TABLE 2.INSPECTED APU Mar 6, 2026 · N606JB · Airbus A320232 · Air Distribution SystemSDR YENA2026030200244Oil System · overservicedFLT #217 PHL-FLL." DIRTY SOCK/OILY SMELL DURING DESCENT @ 10,000' IDLE POWER, VMC,COCKPIT ONLY.; COMPLY INFO NOTICE 2017-T015M. ISOLATE FOR TYPE 1 APU OIL OVERSERVICED. REMOVED EXTR APU OIL IAW AMM 12-13-49. PER TSM 05-50-00-810-085 A/C IS OK FOR SVC "Feb 27, 2026 · N606JB · Airbus A320232 · APU Oil SystemSDR YENA2026012600069Access Door · openFLT 995, MCO- SJO. AIRCRAFT DIVERTED TO FLL. PASSENGER RECORDED A VIDEO OF OPEN LOWER PANEL ON IMBOARD SIDE OF #1 ENGINE DURING FLIGHT. N606-FLT-MCO-SJO-DIVERSION THE A/C DIVERTED TO FLL, THE CREW REPORTED A PANEL WAS OPEN ON THE NBR 1 ENG AND SEEMED TO BE FJan 24, 2026 · N606JB · Airbus A320232 · Nacelle/Pylon, Main FrameSDR YENA2025120901186Unknown · odorFLT 503, JFK-SJU. ODOR DETECTED DURING DESCENT BELOW 10,000. CONFIRMED WITH CABIN CREW. LOCATION OVERWING EXITS STRONGEST, AND FWD. LASTED A MINUTE THEN DISSAPATED. FOUL HEATED PLASTIC TYPE ODOR, FOLLOWED INFO NOTICE 2017-T015L WITH MX-270 PROVIDED. TSM 05-5Dec 8, 2025 · N606JB · Airbus A320232 · Air Distribution SystemSDR YENA2025061300592Door Frame · crackedDURING HEAVY MAINTENANCE: REF AEROMAN WO# 2025 181/1 NR# 2025-325635. CRACK INDICATION FOUND ON LOWER INBOARD HOLE OF DOOR STOP #1, FR68 RH, CRACK INDICATION AT 6 O'CLOCK, VIEW FROM FWD FACE FRAME. CRACK DEPTH: 0.125 INCH. ( FOR TRACKING PURPOSES AREA 1 & 3 );Jun 7, 2025 · N606JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025061300591Door Frame · crackedDURING HEAVY MAINTENANCE: REF AEROMAN WO# 2025 181/1 NR# 2025-325666. CRACK INDICATION FOUND ON LOWER INBOARD HOLE OF DOOR STOP #1, FR68 RH, CRACK INDICATION AT 6 O'CLOCK, VIEW FROM FWD FACE FRAME. CRACK DEPTH: 0.125 INCH. ( FOR TRACKING PURPOSES AREA 2 ); (Jun 7, 2025 · N606JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025061300590Door Frame · crackedDURING HEAVY MAINTENANCE: REF AEROMAN WO# 2025 181/1 NR# 2025-325667. CRACK INDICATION FOUND ON LOWER INBOARD HOLE OF DOOR STOP #1, FR68 RH, CRACK INDICATION AT 6 O'CLOCK VIEW FROM FWD FACE FRAME. CRACK DEPTH: 0.125 INCH. ( FOR TRACKING PURPOSES AREA 4 ); (RESJun 7, 2025 · N606JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025061300589Hinge Fitting · brokenDURING HEAVY MAINTENANCE: BROKEN HINGE FITTING HINGE 3 ELEVATOR LH; REF: ARM W/O 2025-181/1 N/R # 2025-325674. PERFORMED PERMANENT REPAIR ON HINGE FITTING HINGE 3 ELEVATOR LH IAW A320 SRM 55-26-41-300-001, REPAIR IS CATEGORY A.Jun 7, 2025 · N606JB · Airbus A320232 · Elevator StructureSDR YENA2025031700259Unknown · odorFLT#1603, JFK-SJU. 'DURING FINAL DESCENT, SLIGHT ODOR OF OIL IN VENTS IN CLEAR AIR. PACK 1 SET TO OFF, XBLEED SHUT AND ODOR CEASED; C/W INFO NOTICE 2017-T015K SECTION A.ISOLATED FAULT TO TYPE 10 AMBIENT AIR. PERFORMED DECONTAMINATION OF THE ECS LEVEL A PER AMMMar 13, 2025 · N606JB · Airbus A320232 · Air Distribution SystemSDR YENA2024071100951Warning Message · illuminatedFLT#266, RSW-BOS. 'RED ECAM L/G GEAR NOT DOWNLOCKED.' (SUPPLEMENTAL INFORMATION TO FOLLOW)Jul 9, 2024 · N606JB · Airbus A320232 · Landing Gear Position and WarningSDR YENA2022111101118Oxygen Mask · unwanted deployFLT#5, AIRCRAFT PERFORMED AN AIR TURN BACK. O2 MASKS OVER FLIGHT ATTENDANT JUMPSEAT 1 AND 2 DEPLOYED UNCOMMANDED; REMOVED AND REPLACED O2 MASK CONTAINER (28WR) IAW AMM 35-21-41 ALL OPS OK AT THIS TIME.'Nov 7, 2022 · N606JB · Airbus A320232 · Passenger Oxygen SystemSDR YENA2022101401020None · noneFLT#1584, MCO-JFK. 'UNCOMMANDED REDUCTION IN THURST AT 9500 IN CLIMB FROM 1.3 TO 1.2 EPR IN ENGINE #1 FOR APPROX 25SEC CAUSING SIGNIFICANT YAWING MOTION AT THE SAME TIME FUEL IN THE CENTER WENT TO 0 AND GOT A CTR TANK 1 PUMP 1 FAULT; #1 ENG REMOVED AND REPLACEOct 8, 2022 · N606JB · Airbus A320232 · Engine (Turbine/Turboprop)SDR YENA2022100300979Eec · failedFLT#1636, LAX- SFO. (AIRCRAFT PERFORMED AN AIR TURN BACK TO LAX). ' ENGINE ONE STALL CLIMBING OUT OF LAX 10,500 FT #1 ENG WENT TO IDLE AND RELIT. NO ECAM. APPLIED QRH ENG 1 STALL PG 6-31. ENG 1 PARAMETERS ARE NORMAL. RETURNED TO LAX; ACCOMPLISHED TSM 77-00-00Sep 29, 2022 · N606JB · Airbus A320232 · Fuel Controlling SystemSDR YENA2022072200684None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16 LH UPPER O/B SIDE POSITION OPEN FAS TENER HOLE DOOR STOP FITTING Ñ7; REF AEROMAN N/R 2022-355590, REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS LOC BTW FR 15 TO FR 16 AT LEVEL OF DOOR STOP 7Jul 19, 2022 · N606JB · Airbus A320232 · Fuselage Structure (General)SDR YENA2022072200683None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16 LH LOWER O/B SIDE POSITION OPEN FAS TENER HOLE DOOR STOP FITTING Ñ7; REF AEROMAN N/R 2022-355591, REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS LOC BTW FR 15 TO FR 16 AT LEVEL OF DOOR STOP #Jul 19, 2022 · N606JB · Airbus A320232 · Fuselage Structure (General)SDR YENA2022072200682None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16 L/H UPPER I/B SIDE POSITION OPEN FASTENER HOLE DOOR STOP FITTING Ñ7; REF AEROMAN N/R 2022-355592, REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS LOC BTW FR 15 TO FR 16 AT LEVEL OF DOOR STOP #Jul 19, 2022 · N606JB · Airbus A320232 · Fuselage Structure (General)SDR YENA2022072200681None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16 LH UPPER O/B SIDE POSITION OPEN FAS TENER HOLE DOOR STOP FITTING Ñ7; REF AEROMAN N/R 2022-355593, REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS LOC BTW FR 15 TO FR 16 AT LEVEL OF DOOR STOP 7Jul 19, 2022 · N606JB · Airbus A320232 · Fuselage Structure (General)SDR YENA2022072200680None · noneDURING HEAVY MAINTENANCE: CORROSION STRINGER 32L LOCATED BTW FR 53 AND FR 64 IN AFT CARGO COMPA RTMENT; (RESOLVED ON W/O: 1159479 TASKCARD: NR-00010 ) FUR-A320-53-00421, REF AEROMAN N/R 2022-355537, REMOVED CORROSION LOCATED P1. STR32L FR56 PLUS 6.521IN, P2. Jul 19, 2022 · N606JB · Airbus A320232 · Fuselage Structure (General)SDR YENA2022072200679None · noneDURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOCATED BTW FR 60 AND 62 AT LEVEL STR 38R IN AFT CARGO; REF AEROMAN N/R 2022-355522, REMOVED AND REPLACED LOWER SILL, FASTENERS. LOC BTW FR 60 AND FR62 AT LEVEL STR 38R I.A.W. A320 SRM 53-41-49-300-002, A320 SRMJul 19, 2022 · N606JB · Airbus A320232 · Fuselage Structure (General)SDR YENA2022072200678None · noneDURING HEAVY MAINTENANCE: CORROSION ON SHEAR TIE LOC. BTW STR40R TO STR41R AT FR32 IN FWD CARGO COMPARTMENT; REMOVED AND REPLACED NEW SHEAR TIE LOC. BTW STR40R AND STR41R AT FR32 IN FWD CARGO COMPARTMENT IAW A320 SRM 51-42-11 AND DWG D 53231586. ALL WORK ACCOMJul 19, 2022 · N606JB · Airbus A320232 · Fuselage Structure (General)SDR YENA2022072200677None · noneDURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STR41R TO SRT42R AT FR33 IN FWD CARGO COMPARTMENT; REMOVED AND REPLACED NEW SHEAR TIE LOC. BTW STR41R AND STR42R AT FR33 IN FWD CARGO COMPARTMENT IAW A320 SRM 51-42-11 AND DWG D 53231586. ALL WORK ACCOMPLIJul 19, 2022 · N606JB · Airbus A320232 · Fuselage Structure (General)SDR YENA2022072200676None · noneDURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STR42R AND STR43R AT FR32 IN FWD CARGO COMPARTMENT; REMOVED AND REPLACED NEW SHEAR TIE LOC. BTW STR43R AND STR43R AT FR32 IN FWD CARGO COMPARTMENT IAW A320 SRM 51-42-11 AND DWG D 53231586. ALL WORK ACCOMPLJul 19, 2022 · N606JB · Airbus A320232 · Fuselage Structure (General)SDR YENA2022072200675None · noneDURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STR40R AND STR41R AT FR33 IN FWD CARGO COMPARTMENT; ALL WORK ACCOMPLISHED ON AEROMAN NR# 2022-355551. REMOVED AND REPLACED NEW SHEAR TIE LOC. BTW STR40R AND STR41R AT FR33 IN FWD CARGO COMPARTMENT IAW A320Jul 19, 2022 · N606JB · Airbus A320232 · Fuselage Structure (General)SDR YENA2022072200674None · noneDURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOC. BTW STR41R TO STR42R AT FR32 IN FWD CARGO COMPARTMENT; ALL WORK ACCOMPLISHED ON AEROMAN NR# 2022-355543. REMOVED AND REPLACED NEW SHEAR TIE LOC. BTW STR41R AND STR42R AT FR32 IN FWD CARGO COMPARTMENT IAW A320 Jul 19, 2022 · N606JB · Airbus A320232 · Fuselage Structure (General)SDR YENA2021031900182Lug · crackedDURING HMV, LANDING GEAR -MAIN GEAR - INSPECTION SLIDING TUBE / SLAVE LINK LUG CRACK (CLASSIFIED MAJOR)Mar 15, 2021 · N606JB · Airbus A320232 · Main Landing Gear Attach SectionSDR YENA2021012700078Unknown · odorFLT 563, ORD-FLL. INFLT REPORTED BURING SMELL IN BACK OF A/C AND LIVE TV IN ACFT CABIN INOPERABLE. PERFORMED CABIN ORDER INSPECTION, PER TSM 05-50-00-810-831-A. NO 'BURNING SMELL' COULD BE DUPLICATED. TSM 05-50-00-810-831-A WAS FOLLOWED BY CAPTAINS CABIN OJan 23, 2021 · N606JB · Airbus A320232 · Air Distribution SystemSDR YENA2018091190337Battery · failedFLT 2633, BDL-TPA. AFT EMERGENCY LIGHT TEST FAILED FIN 13WL BATTERY. REMOVED & REPLACED EMERGENCY LIGHT BATTERY AT FIN 13WL PER AMM 33-51-38.Sep 9, 2018 · N606JB · Airbus A320232 · Emergency LightingSDR YENA201711250961Amu · faultyFLT 88, FLL-ALB. COMM 1 & 2 ONLY TRANSMIT ON 119.3 RECEIVE ON ALL FREQ. T/S AND FOUND F/O'S BOOMSET DEFECTIVE, REPLACED F/O'S BOOMSET AS REQUIRED. ALSO REMOVED & REPLACED AUDIO MANAGEMENT UNIT (1RN) PER AMM 23-51-34, ALL BITE TEST AND OPS TEST OK. A/C NOW OK FNov 25, 2017 · N606JB · Airbus A320232 · Audio Integrating SystemSDR YENA201706010452Filter · failedDURING DESCENT THROUGH 8000 FEET, SMELLED A STRONG ODOR OF DIRTY SOCKS THROUGH THE PACKS FOR ABOUT 12 MINUTES. DONNED OXYGEN MASKS ALL THE WAY TO LANDING. FLIGHT ATTENDANT ALSO COMPLAINED ABOUT THE ODOR. PERFORMED INFO NOTICE 2017-T015, FOLLOWED PERFORMANCJun 1, 2017 · N606JB · Airbus A320232 · Air Distribution SystemSDR YENA201706010451Filter · failedDURING DESCENT THROUGH 8000 FEET, SMELLED A STRONG ODOR OF DIRTY SOCKS THROUGH THE PACKS FOR ABOUT 12 MINUTES. DONNED OXYGEN MASKS ALL THE WAY TO LANDING. FLIGHT ATTENDANT ALSO COMPLAINED ABOUT THE ODOR. PERFORMED INFO NOTICE 2017-T015, FOLLOWED PERFORMANCJun 1, 2017 · N606JB · Airbus A320232 · Air Distribution SystemSDR YENA20160621589Skin Panel · corrodedDURING MAINTENANCE, CORROSION WAS DISCOVERED ON OVERHANG T/E LOCATED AT RIB 16, TOP SKIN PANEL 2, LOWER SURFACE ON RT WING. PERFORMED PERMANENT REPAIR ON OVERHANG T/E LOCATED AT RIB 16, TOP SKIN PANEL 2, LOWER SURFACE ON RT WING.Jun 21, 2016 · N606JB · Airbus A320232 · Wing, Plate/SkinSDR YENA20160621588Skin Panel · corrodedDURING MAINTENANCE, CORROSION WAS DISCOVERED ON OVERHANG T/E LOCATED AT RIB 17 TOP SKIN PANEL 2 LOWER SURFACE ON RT WING. PERFORMED PERMANENT REPAIR ON OVERHANG T/E.Jun 21, 2016 · N606JB · Airbus A320232 · Wing, Plate/SkinSDR YENA20160621587Skin Panel · corrodedDURING MAINTENANCE, CORROSION WAS DISCOVERED ON OVERHANG T/E AT RIB 15 + 8", TOP SKIN PANEL 2, LOWER SURFACE ON LT WING. PERFORMED PERMANENT REPAIR ON OVERHANG T/E AT RIB 15 + 8", TOP SKIN PANEL 2 ON LT WING.Jun 21, 2016 · N606JB · Airbus A320232 · Wing, Plate/SkinSDR YENA20160621586Skin Panel · corrodedDURING MAINTENANCE, CORROSION WAS DISCOVERED ON OVERHANG T/E LOCATION AT RIB 16 TOP SKIN PANEL 2, LOWER SURFACE ON LT WING. PERFORMED PERMANENT REPAIR ON OVERHANG T/E LOCATED AT RIB 16, TOP SKIN PANEL 2, ON LT WING.Jun 21, 2016 · N606JB · Airbus A320232 · Wing, Plate/SkinSDR YENA20160621585Skin Panel · corrodedDURING MAINTENANCE, CORROSION WAS DISCOVERED ON OVERHANG T/E LOCATION AT RIB 15, TOP SKIN PANEL 2 LOWER SURFACE ON LT WING. PERFORMED PERMANENT REPAIR ON OVERHANG T/E LOCATED AT RIB 15, TOP SKIN PANEL 2 ON LT WING.Jun 21, 2016 · N606JB · Airbus A320232 · Wing, Plate/SkinSDR YENA20160621584Skin · corrodedDURING MAINTENANCE, CORROSION WAS DISCOVERED ON TOP SKIN ON UPPER SURFACE ON LT WING ON RIB 1 AND STR 11. REPAIRED AREA ON TOP SKIN UPPER SURFACE ON LT WING ON RIB 1 AND STR 11.Jun 21, 2016 · N606JB · Airbus A320232 · Wing, Plate/SkinSDR YENA20160621583Skin · corrodedDURING MAINTENANCE, CORROSION WAS DISCOVERED ON TOP SKIN ON UPPER SURFACE LEVEL STR 11, BETWEEN RIB 11 AND RIB 12, LEFT WING. REPAIRED AREA ON TOP SKIN UPPER SURFACE LEVEL STR 11, BETWEEN RIB 11 AND RIB 12 LT WING.Jun 21, 2016 · N606JB · Airbus A320232 · Wing, Plate/SkinSDR YENA20160621582Door Sill · corrodedDURING MAINTENANCE, CORROSION WAS DISCOVERED ON LOWER SILL, LOCATION: FRAME 66, STR 23L AT AFT GALLEY AREA; INSTALLED NEW LOWER SILL LOCATION, FRAME 66 AT LEVEL STR 23L AT AFT GALLEY AREA.Jun 21, 2016 · N606JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA20160621581Door Sill · corrodedDURING MAINTENANCE, CORROSION WAS DISCOVERED ON LOWER SILL LOCATION, FRAME 66, STR 23R AT AFT GALLEY AREA. R & R NEW LOWER SILL.Jun 21, 2016 · N606JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA20160621580Door Sill · corrodedDURING MAINTENANCE, CORROSION WAS DISCOVERED ON LOWER SILL LOCATION, FRAME 68, STR 23R AT AFT GALLEY AREA. R & R LOWER SILL.Jun 21, 2016 · N606JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA20160621579Floorbeam · corrodedDURING MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM LOCATION: -Y1162, LOCATION FRAME 67 + 18" AT AFT GALLEY AREA; R & R FLOORBEAM -Y1162, FR 67 +18" AT AFT GALLEY AREA.Jun 21, 2016 · N606JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA20160621578Floorbeam · corrodedDURING MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM LOCATION: -Y1162, FR 67 +15" AT AFT GALLEY AREA. R & R FLOORBEAM -Y1162, FRAME 67 + 15" AT AFT GALLEY AREA.Jun 21, 2016 · N606JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA20160621577Floorbeam · corrodedDURING MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM LOCATION: -Y1292 BETWEEN FRAME 16 TO FRAME 20 AT FWD GALLEY AREA. R & R FLOORBEAM AT FWD GALLEY AREA.Jun 21, 2016 · N606JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA20160621576Floorbeam · corrodedDURING MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM, +Y1292 BETWEEN FRAME 16 TO FRAME 20 AT FWD GALLEY AREA. REPLACED FLOORBEAM +Y1292 BETWEEN FRAME 16 TO FRAME 20 AT FWD GALLEY AREA.Jun 21, 2016 · N606JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA20160621575Floorbeam · corrodedDURING MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM, -Y765 BETWEEN FRAME 20 TO FRAME 24 AT FWD GALLEY AREA. R & R FLOORBEAM -Y765 BETWEEN FRAME 20 TO FRAME 24 AT FWD GALLEY AREA.Jun 21, 2016 · N606JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA20160621574Floorbeam · corrodedDURING MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM, LOCATION: -Y254, FRAME 20 AT FWD GALLEY AREA; R & R FLOORBEAM -Y254, FRAME 20 AT FWD GALLEY AREA.Jun 21, 2016 · N606JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA20160621573Floorbeam · corrodedDURING MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOORBEAM, LOCATION: +Y1162, FRAME 67+18" AT AFT GALLEY AREA. R & R FLOORBEAM Y1162 FRAME 67 + 18" AT AFT GALLEY AREA IAW SRM 51-72-11.Jun 21, 2016 · N606JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA20160308222Unknown · odorIN-FLIGHT CREW SMELLED ELECTRICAL ODOR IN-FLIGHT ON DESCENT, NO VISIBLE SMOKE OR MALFUNCTIONING EQUIPMENT. NO COCKPIT INDICATIONS; PERFORMED INSPECTION IAW 05-50-00-810-831-A & TSM 24-00-00-810-823-A. NO FINDINGS BOTH APU ENG BLEED INCLUDED. AS A PRECAUTIOMar 8, 2016 · N606JB · Airbus A320232 · Air Distribution SystemSDR YENA20140809152Regulator Valve · failedACFT DIVERTED. CREW REPORTED ON INITIAL CLIMB WITH POWER REDUCTION, ACFT RECEIVED AIR ENG 2 BLEED ABNORMAL PRESSURE ECAM. COMPLIED WITH QRH. PERFORMED TSM TASK 36-11-00-810-810A. FOUND BLEED PRESSURE REGULATOR VALVE 4001HA2 INTERMITTENTLY OPENING WITH 20 PSAug 9, 2014 · N606JB · Airbus A320232 · Pneumatic Distribution System
Back to N606JB