# Service difficulty reports: N606JB

A list on [N606JB](https://openairdocs.org/aircraft/N606JB.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 YENA2026080700658](https://openairdocs.org/sdr/YENA2026080700658.md): Fan · failed · Aug 5, 2026 · N606JB · Airbus A320232 · Air Distribution Fan
  > FLT 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 UPDATED
- [SDR YENA2026030900284](https://openairdocs.org/sdr/YENA2026030900284.md): Unknown · odor · Mar 6, 2026 · N606JB · Airbus A320232 · Air Distribution System
  > FLT # 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
- [SDR YENA2026030200244](https://openairdocs.org/sdr/YENA2026030200244.md): Oil System · overserviced · Feb 27, 2026 · N606JB · Airbus A320232 · APU Oil System
  > FLT #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 "
- [SDR YENA2026012600069](https://openairdocs.org/sdr/YENA2026012600069.md): Access Door · open · Jan 24, 2026 · N606JB · Airbus A320232 · Nacelle/Pylon, Main Frame
  > FLT 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 F
- [SDR YENA2025120901186](https://openairdocs.org/sdr/YENA2025120901186.md): Unknown · odor · Dec 8, 2025 · N606JB · Airbus A320232 · Air Distribution System
  > FLT 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 05-5
- [SDR YENA2025061300592](https://openairdocs.org/sdr/YENA2025061300592.md): Door Frame · cracked · Jun 7, 2025 · N606JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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);
- [SDR YENA2025061300591](https://openairdocs.org/sdr/YENA2025061300591.md): Door Frame · cracked · Jun 7, 2025 · N606JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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); (
- [SDR YENA2025061300590](https://openairdocs.org/sdr/YENA2025061300590.md): Door Frame · cracked · Jun 7, 2025 · N606JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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); (RES
- [SDR YENA2025061300589](https://openairdocs.org/sdr/YENA2025061300589.md): Hinge Fitting · broken · Jun 7, 2025 · N606JB · Airbus A320232 · Elevator Structure
  > DURING 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.
- [SDR YENA2025031700259](https://openairdocs.org/sdr/YENA2025031700259.md): Unknown · odor · Mar 13, 2025 · N606JB · Airbus A320232 · Air Distribution System
  > FLT#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 AMM
- [SDR YENA2024071100951](https://openairdocs.org/sdr/YENA2024071100951.md): Warning Message · illuminated · Jul 9, 2024 · N606JB · Airbus A320232 · Landing Gear Position and Warning
  > FLT#266, RSW-BOS. 'RED ECAM L/G GEAR NOT DOWNLOCKED.' (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA2022111101118](https://openairdocs.org/sdr/YENA2022111101118.md): Oxygen Mask · unwanted deploy · Nov 7, 2022 · N606JB · Airbus A320232 · Passenger Oxygen System
  > FLT#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.'
- [SDR YENA2022101401020](https://openairdocs.org/sdr/YENA2022101401020.md): None · none · Oct 8, 2022 · N606JB · Airbus A320232 · Engine (Turbine/Turboprop)
  > FLT#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 REPLACE
- [SDR YENA2022100300979](https://openairdocs.org/sdr/YENA2022100300979.md): Eec · failed · Sep 29, 2022 · N606JB · Airbus A320232 · Fuel Controlling System
  > FLT#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 77-00-00
- [SDR YENA2022072200684](https://openairdocs.org/sdr/YENA2022072200684.md): None · none · Jul 19, 2022 · N606JB · Airbus A320232 · Fuselage Structure (General)
  > DURING 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 7
- [SDR YENA2022072200683](https://openairdocs.org/sdr/YENA2022072200683.md): None · none · Jul 19, 2022 · N606JB · Airbus A320232 · Fuselage Structure (General)
  > DURING 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 #
- [SDR YENA2022072200682](https://openairdocs.org/sdr/YENA2022072200682.md): None · none · Jul 19, 2022 · N606JB · Airbus A320232 · Fuselage Structure (General)
  > DURING 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 #
- [SDR YENA2022072200681](https://openairdocs.org/sdr/YENA2022072200681.md): None · none · Jul 19, 2022 · N606JB · Airbus A320232 · Fuselage Structure (General)
  > DURING 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 7
- [SDR YENA2022072200680](https://openairdocs.org/sdr/YENA2022072200680.md): None · none · Jul 19, 2022 · N606JB · Airbus A320232 · Fuselage Structure (General)
  > DURING 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.
- [SDR YENA2022072200679](https://openairdocs.org/sdr/YENA2022072200679.md): None · none · Jul 19, 2022 · N606JB · Airbus A320232 · Fuselage Structure (General)
  > DURING 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 SRM
- [SDR YENA2022072200678](https://openairdocs.org/sdr/YENA2022072200678.md): None · none · Jul 19, 2022 · N606JB · Airbus A320232 · Fuselage Structure (General)
  > DURING 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 ACCOM
- [SDR YENA2022072200677](https://openairdocs.org/sdr/YENA2022072200677.md): None · none · Jul 19, 2022 · N606JB · Airbus A320232 · Fuselage Structure (General)
  > DURING 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 ACCOMPLI
- [SDR YENA2022072200676](https://openairdocs.org/sdr/YENA2022072200676.md): None · none · Jul 19, 2022 · N606JB · Airbus A320232 · Fuselage Structure (General)
  > DURING 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 ACCOMPL
- [SDR YENA2022072200675](https://openairdocs.org/sdr/YENA2022072200675.md): None · none · Jul 19, 2022 · N606JB · Airbus A320232 · Fuselage Structure (General)
  > DURING 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 A320
- [SDR YENA2022072200674](https://openairdocs.org/sdr/YENA2022072200674.md): None · none · Jul 19, 2022 · N606JB · Airbus A320232 · Fuselage Structure (General)
  > DURING 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
- [SDR YENA2021031900182](https://openairdocs.org/sdr/YENA2021031900182.md): Lug · cracked · Mar 15, 2021 · N606JB · Airbus A320232 · Main Landing Gear Attach Section
  > DURING HMV, LANDING GEAR -MAIN GEAR - INSPECTION SLIDING TUBE / SLAVE LINK LUG CRACK (CLASSIFIED MAJOR)
- [SDR YENA2021012700078](https://openairdocs.org/sdr/YENA2021012700078.md): Unknown · odor · Jan 23, 2021 · N606JB · Airbus A320232 · Air Distribution System
  > FLT 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 O
- [SDR YENA2018091190337](https://openairdocs.org/sdr/YENA2018091190337.md): Battery · failed · Sep 9, 2018 · N606JB · Airbus A320232 · Emergency Lighting
  > FLT 2633, BDL-TPA. AFT EMERGENCY LIGHT TEST FAILED FIN 13WL BATTERY. REMOVED & REPLACED EMERGENCY LIGHT BATTERY AT FIN 13WL PER AMM 33-51-38.
- [SDR YENA201711250961](https://openairdocs.org/sdr/YENA201711250961.md): Amu · faulty · Nov 25, 2017 · N606JB · Airbus A320232 · Audio Integrating System
  > FLT 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 F
- [SDR YENA201706010452](https://openairdocs.org/sdr/YENA201706010452.md): Filter · failed · Jun 1, 2017 · N606JB · Airbus A320232 · Air Distribution System
  > DURING 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 PERFORMANC
- [SDR YENA201706010451](https://openairdocs.org/sdr/YENA201706010451.md): Filter · failed · Jun 1, 2017 · N606JB · Airbus A320232 · Air Distribution System
  > DURING 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 PERFORMANC
- [SDR YENA20160621589](https://openairdocs.org/sdr/YENA20160621589.md): Skin Panel · corroded · Jun 21, 2016 · N606JB · Airbus A320232 · Wing, Plate/Skin
  > DURING 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.
- [SDR YENA20160621588](https://openairdocs.org/sdr/YENA20160621588.md): Skin Panel · corroded · Jun 21, 2016 · N606JB · Airbus A320232 · Wing, Plate/Skin
  > DURING 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.
- [SDR YENA20160621587](https://openairdocs.org/sdr/YENA20160621587.md): Skin Panel · corroded · Jun 21, 2016 · N606JB · Airbus A320232 · Wing, Plate/Skin
  > DURING 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.
- [SDR YENA20160621586](https://openairdocs.org/sdr/YENA20160621586.md): Skin Panel · corroded · Jun 21, 2016 · N606JB · Airbus A320232 · Wing, Plate/Skin
  > DURING 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.
- [SDR YENA20160621585](https://openairdocs.org/sdr/YENA20160621585.md): Skin Panel · corroded · Jun 21, 2016 · N606JB · Airbus A320232 · Wing, Plate/Skin
  > DURING 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.
- [SDR YENA20160621584](https://openairdocs.org/sdr/YENA20160621584.md): Skin · corroded · Jun 21, 2016 · N606JB · Airbus A320232 · Wing, Plate/Skin
  > DURING 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.
- [SDR YENA20160621583](https://openairdocs.org/sdr/YENA20160621583.md): Skin · corroded · Jun 21, 2016 · N606JB · Airbus A320232 · Wing, Plate/Skin
  > DURING 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.
- [SDR YENA20160621582](https://openairdocs.org/sdr/YENA20160621582.md): Door Sill · corroded · Jun 21, 2016 · N606JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING 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.
- [SDR YENA20160621581](https://openairdocs.org/sdr/YENA20160621581.md): Door Sill · corroded · Jun 21, 2016 · N606JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING MAINTENANCE, CORROSION WAS DISCOVERED ON LOWER SILL LOCATION, FRAME 66, STR 23R AT AFT GALLEY AREA. R & R NEW LOWER SILL.
- [SDR YENA20160621580](https://openairdocs.org/sdr/YENA20160621580.md): Door Sill · corroded · Jun 21, 2016 · N606JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING MAINTENANCE, CORROSION WAS DISCOVERED ON LOWER SILL LOCATION, FRAME 68, STR 23R AT AFT GALLEY AREA. R & R LOWER SILL.
- [SDR YENA20160621579](https://openairdocs.org/sdr/YENA20160621579.md): Floorbeam · corroded · Jun 21, 2016 · N606JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING 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.
- [SDR YENA20160621578](https://openairdocs.org/sdr/YENA20160621578.md): Floorbeam · corroded · Jun 21, 2016 · N606JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING 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.
- [SDR YENA20160621577](https://openairdocs.org/sdr/YENA20160621577.md): Floorbeam · corroded · Jun 21, 2016 · N606JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING 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.
- [SDR YENA20160621576](https://openairdocs.org/sdr/YENA20160621576.md): Floorbeam · corroded · Jun 21, 2016 · N606JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING 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.
- [SDR YENA20160621575](https://openairdocs.org/sdr/YENA20160621575.md): Floorbeam · corroded · Jun 21, 2016 · N606JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING 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.
- [SDR YENA20160621574](https://openairdocs.org/sdr/YENA20160621574.md): Floorbeam · corroded · Jun 21, 2016 · N606JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM, LOCATION: -Y254, FRAME 20 AT FWD GALLEY AREA; R & R FLOORBEAM -Y254, FRAME 20 AT FWD GALLEY AREA.
- [SDR YENA20160621573](https://openairdocs.org/sdr/YENA20160621573.md): Floorbeam · corroded · Jun 21, 2016 · N606JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING 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.
- [SDR YENA20160308222](https://openairdocs.org/sdr/YENA20160308222.md): Unknown · odor · Mar 8, 2016 · N606JB · Airbus A320232 · Air Distribution System
  > IN-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 PRECAUTIO
- [SDR YENA20140809152](https://openairdocs.org/sdr/YENA20140809152.md): Regulator Valve · failed · Aug 9, 2014 · N606JB · Airbus A320232 · Pneumatic Distribution System
  > ACFT 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 PS

Next page: https://openairdocs.org/aircraft/N606JB/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 = 'N606JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N606JB/reports

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