N822DX
Service difficulty reports · 151
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 = 'N822DX' 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.
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 = 'N822DX' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DALA2021050402547Light · intermittentSHIP 6822 DOOR 4L DIFFICULT TO ARM AND SLIDE LIGHT WILL NOT LIGHT. CORRECTIVE ACTION: OPEN/CLOSED 4L DOOR, ARMED/DISARMED DOOR MULTIPLE TIMES. DOOR OP CKS GOOD, SLIDE LIGHT CKS GOOD. (7463574)SDR DALA2022020200686None · noneSHIP 6822 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 583990-14 REV A. CORRECTIVE ACTION: SUMMARY: AREA WAS INSPECTED PER ER/A 583990-14AD REV.A SECTION V AND DISCREPANCIES WERE FOUND. AREA WAS REPAISDR DALA2022020200685None · noneSHIP 6822 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 583990-14 REV A. CORRECTIVE ACTION: IN REF. ER/A 583990-14AD REV.C SECTION VI PERMANENT REPAIR. (1795664)SDR DALA2021111707110None · noneSHIP 6822 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 583990-14 REV A. CORRECTIVE ACTION: REF ERA 583990-14 REV A. (1795659)SDR DALA2022011900366None · noneSHIP 6822 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 583989-14 REV A. CORRECTIVE ACTION: REPAIRED (PERMANENT REPAIR) PER ER/A 583989-14AD REV.C SECTION V. (1783609)SDR DALA2021120207448None · noneSHIP 6822 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 583989-14 REV A. CORRECTIVE ACTION: REF ERA 583989-14 REV A. (1783611)SDR DALA2020091503072Battery Pack · inoperativeSHIP 6822, DURING INSPECTION FOUND EMERGENCY SEAT LIGHTS FROM ROW 27 DEF-31 DEF INOPERATIVE. CORRECTIVE ACTION: REPLACED BATTERY M1383 AND CHARGER. SYSTEM OPERATION IS NORMAL.SDR DALA2020091503070Battery Pack · inoperativeSHIP 6822, DURING INSPECTION FOUND EMERGENCY OVERHEAD LIGHT AT ROW 30/31 DEF INOPERATIVE. CORRECTIVE ACTION: REPLACED BATTERY M11383 AND CHARGER. SYSTEM OPERATION IS NORMAL.SDR DALA2020083102881Transceiver · malfunctionedTHE CREW PERFORMED AN AIR TURN BACK FOLLOWING DUE TO THE LOSS OF BOTH THE LT & RT HF RECEIVERS. SELCAL CHECK ALSO FAILED. CORRECTIVE ACTION: MAINTENANCE REPLACED BOTH THE LT & RT HF TRANSCEIVERS. IT WAS NOTED THAT BOTH HF SENSE CONTROLS WERE TURNED DOWN. TURNESDR DALA2020031101792Cover · detached(AIRCRAFT 6822, L/P 6960476) EXIT LIGHT COVER AT ROW 36 DETACHED FROM CEILING. CORRECTIVE ACTION: SECURED LIGHT COVER AND ASSEMBLY.SDR DALA2019122427528Clamp · crackedLH ENG DRAG FTG CLAMP-UP & DIAG BRACE, STEP 27. CRACK INDICATION WAS IN HOLE NR 13, WAS FOUND. REPLACED PER ERA 583990-14AD REV. ORIG. SECTION 1 AND ETI-57-19-190 REV 13.SDR DALA2019122427527Fitting · corrodedLT ENG DRAG FTG CLAMP-UP & DIAG BRACE, STEP 26 CORROSION IN HOLES # 2, 3, 5, 8, AND 9 WAS FOUND. REPAIRED PER ERA 583990-14AD REV. ORIG. SECTION 1 AND ETI-57-19-190 REV 13.SDR DALA2019122427526Brace · corrodedLEFT ENG DRAG FITTING CLAMP & DIAG BRACE, STEP 27. CORROSION IN HOLES # 13, 14, AND 18, WAS FOUND. REPLACED PER ERA 583990-14AD REV. ORIG. SECTION 1 AND ETI-57-19-190 REV 13.SDR DALA2019122327491Brace · crackedLH ENG DRAG FTG CLAMP-UP & DRAG BRACE. CRACK INDICATIONS WERE FOUND IN HOLES NBR 3 AND 5 WERE FOUND. REPAIRED PER ERA 583990-14AD REV. ORIG. SECTION 1 AND ETI-57-19-190, REV. 13.SDR DALA2019122327490Skin · corrodedCORROSION ON COUNTERSINKS ON LH UPPER SKIN IN DRAG FITTING HOLES NBR 1, 2, 3, 4, 5, 7, 8, 9, 10, 11, 13, 14 AND 18 IN REF NRC 305 AND 306. REPAIRED PER ERA 583990-14AD REV. ORIG. SECTION 1 AND ETI-57-19-190 REV 13.SDR DALA2019122327489Shim · migratedMIGRATED SHIM ON DRAG FITTING/FRONT SPAR, AT LH ENG DRAG FTG CLAMP-UP & DIAG BRACE. REPLACED PER ERA 583990-14AD REV. ORIG. SECTION 1 AND ETI-57-19-190 REV 13.SDR DALA2019122317486Skin · crackedCRACK INDICATIONS WERE FOUND IN HOLES # 4, 5, 8 & 11 AND CORROSION WAS FOUND IN HOLES #1 & 3. REPAIRED PER ERA 583989-14AD REV. ORIG. SECTION 1 AND ETI-57-19-188 REV. 7.SDR DALA2023063005270Unknown · unknownSHIP 6822 BROKEN LH WING FIXED LEADING EDGE UPPER SURFACE FSS 416 (REF ABOVE INBOARD EDGE OF SLAT 3). CORRECTIVE ACTION: SUMMARY; OF NRC S/N 00330: LH WING FIXED LEADING EDGE UPPER SURFACE FSS 416 (REF ABOVE INBOARD EDGE OF SLAT 3) WAS REPAIRED PER B-757-200 SSDR DALA2023063005269Unknown · unknownSHIP 6822 CRACK RH WING FIXED LEADING EDGE STA 425.50. CORRECTIVE ACTION: SUMMARY; OF NRC S/N 00070: RH WING FIXED LEADING EDGE STA 425.50 WAS REPAIRED PER B-757-200 S.R.M. (1397302)SDR DALA2021121707865Wedge · debondedSHIP 6822 DISBOND OF 2.5" X 1.8" ON LE SLAT 3 TRAILING EDGE WEDGE OSS. 51O. LH WING. CORRECTIVE ACTION: SUMMARY IN REFERENCE WITH NRC S/N 00081 LH WING SLAT 3 TRAILING EDGE WEDGE UPPER SKIN, BTW STA OSS 510. WAS REPAIRED PER B757- 200 SRM. (1398198)SDR DALA2019121307279Indicator · out of limitsOUT OF LIMITS COMPENSATOR INDICATOR ON SNUBBER AT L2 DOOR. CORRECTIVE ACTION: UPPER CAM PLATE, LOWER CAM PLATE AND LOWER HINGE LINK, DOOR GUIDE ARM, SPRING CYLINDER COUNTER BALANCE AND SNUBBER WAS REMOVED PER B757-200 AMM 52-11 AND UPPER CAM PLATE, LOWER CAM PSDR DALA2019121327278Indicator · out of limitsOUT OF LIMITS COMPENSATOR INDICATOR ON SNUBBER AT L1 DOOR. CORRECTIVE ACTION: UPPER CAM PLATE, LOWER CAM PLATE AND LOWER HINGE LINK, DOOR GUIDE ARM, SPRING CYLINDER COUNTER BALANCE AND SNUBBER WAS REMOVED PER B757-200 AMM 52-11. UPPER CAM PLATE, LOWER CAM PLATSDR DALA2019110406408Access Door · missing(AIRCRAFT 6822, L/P 6532920) AFTER T/O VIBRATION AND HI PITCHED HUMMING FROM LEFT SIDE OF A/A. COULD FEEL VIBRATION IN FLT. CONTROLS, RUDDER PEDALS AND AIRFRAME. AFTER LEVEL OFF, WENT AWAY, NOTHING ON DESCENT. CORRECTIVE ACTION: DURING W/A FOUND LT SIDE PACK ISDR DALA2019102986247Battery Pack · inoperative(AIRCRAFT 6822, L/P 6532900) WHILE PERFORMING MTC FOUND EMER EXIT LIGHT OUTS AT ROWS 36-40. CORRECTIVE ACTION: R/R BATTERY PACK AT ROW 36ABC IAW B757 AMM 33-51.SDR DALA2019082324935Lanyard · misroutedL1 DOOR WONT ARM - ARM LVR WONT LOCK IN PLACE. FOUND LANYARD FOR SLIDE ROUTED INCORRECTLY - RE-ROUTED LANYARD - NOW CHKS GOOD IAW B757 AMM 52-10. (6054892)SDR DALA2019042952722Unknown · odorSHIP 6822 ONE HOUR INTO FLIGHTF/A'S REPORT SMELLING ELECTRICAL BURNING SMELL BETWEEN AFT LAVS DID NOT INFORM PILOTS.AT TOP OF DESCENT F/A'S SMELL ADDITIONAL CHEMICAL SMELL IN SAME AREA. NOTIFIED PILOTS AT THIS TIME OF BOTH INCIDENT. COMPLETED AMM INSPECTION SDR DALA2022010700149None · noneSHIP 6822 ON ARRIVAL MCO - RAMP REPORTED DENT ON FUSELAGE APPROX. 2 FT FWD AND 1 FT BELOW 4R DOOR. CORRECTIVE ACTION: SUMMARY: DENT ON FUSELAGE STA 1625: STR 18 -19 RH WAS PERMANENT REPAIR PER ETI-57-21-578 REV.3 AND PER ER/A 596321-14 REV. ORIGINAL. (4093414)SDR DALA2017121908706Skin · corrodedCORROSION FOUND ON THE EXTERIOR SKIN, OF THE NR 2 PYLON AFT FAIRING INBOARD SIDE. REPAIRED IAW SRM 54-51-70, AND 51-70-10 REPAIR 2.SDR DALA2017120608453Cowling · erodedNR 2 ENG OUTBD FAN COWL HAS LEADING EDGE EROSION, 15" LONG FROM BOTTOM CENTER. ACCOMPLISHED A PERMANENT REPAIR TO NR 2 ENGINE OUTBD FAN COWL L/E IAW SRM.SDR DALA2017120608451Cowling · erodedNR 2 ENG INBD FAN COWL HAS LEADING EDGE EROSION, 20" FROM BOTTOM CENTER. ACCOMPLISHED A PERMANENT REPAIR TO NR 2 ENGINE INBD FAN COWL L/E IAW SRM.SDR DALA2017041403123Battery Pack · inoperativeNR 2 GALLEY CEILING EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED THE BATTERY IAW AMM 33-57. OPS CHECKED GOOD.SDR DALA2017022201466Power Supply · inoperativeEMER EXTERIOR LITE AT DR4R IS OUT. REPLACED EMER EXIT SLIDE LT PWR SUPPLY PER AMM 33-51, THEN CHECKED & OK FOR SERVICE.SDR DALA2016060104273Actuator · corrodedLEFT PACK RAM AIR INLET DOOR ACTUATOR BODY AND AFT ATTACH LUG EXFOLIATED. R & R LT PACK RAM AIR INLET DOOR ACTUATOR IAW AMM 21-53-03. OPS CHECK GOOD IAW AMM 21-53.SDR DALA2016060104272Lug · corrodedRIGHT PACK RAM AIR INLET DOOR ACTUATOR AFT LUG EXFOLIATED. R & R RT PACK RAM AIR INLET DOOR ACTUATOR IAW AMM 21-53-03. OPS CHECK GOOD IAW AMM 21-53.SDR DALA2016050703784Frame · dentedFWD CARGO RT SIDE FRAME, BS 660 HAS 3 EA DENTS STR 23R TO 25R. ACCOMPLISHED PERMANENT REPAIR ON FWD CARGO RT SIDE FRAME STA 660, STR 23R TO STR 27R REF ER/A 546341-14AD REV ORIGINAL REF THIS LOGPAGE, NRC FOR REPAIR ACCOMPLISHMENT.SDR DALA2016050703783Skin · dentedLEFT WING INBD FLAP UPPER SURFACE HAS DENT 24" FROM OTBD END OF INBD UPPER SKIN PANEL 22" FROM T/E. UPON FURTHER EVALUATION FOUND PANEL TO BE OUT OF REPAIRABLE LIMITS IAW SRM PANEL. WILL BE INSTALLED ON CARD. FOUND LT WING INBD MAIN FLAP UPPER SURFACE INBDSDR DALA2016050703785Frame · dentedTWO DENTS ON AFT CARGO LT FRAME UPPER FLANGE AT BS 1280 ABOVE STR 26L. ACCOMPLISHED PERMANENT REPAIR ON AFT CARGO LT FRAME UPPER FLANGE AT BS 1280 ABOVE STR 26L IAW ER/A 544736-14AD REV A. REFER TO THIS NRC AND THIS LOGPAGE FOR REPAIR.SDR DALA2016050603746Skin · dentedLT WING OTBD AFT FLAP UPPER SKIN HAS THREE DELAMINATED DENTS, 37-46 INCHES FROM INBD END. 7-10 INCHES FROM T/E. ACCOMPLISHED PERMANENT REPAIR ON LT WING OTBD AFT FLAP UPPER SURFACE REF SRM.SDR DALA2016050603744Frame · corrodedCORROSION ON AFT CARGO LT FRAME UPPER FLANGE AT BS 1280 ABOVE STR 23L. ACCOMPLISHED PERMANENT REPAIR ON AFT CARGO LT FRAME UPPER FLANGE AT BS 1280 ABOVE STR 23L IAW ER/A 544736-14AD REV A, REFER TO NRC AND LOG FOR REPAIR.SDR DALA2016050603742Floorbeam · corrodedCORROSION ON FLOORBEAM BS 680, LBL 57.5. ACCOMPLISHED PERMANENT REPAIR ON FLOORBEAM, BS 680, LBL 57.5, REF ER/A 544725-14. REV ORIGINAL.SDR DALA2016050403729Lug · corrodedUPON REMOVAL RT ECS BAY DOOR FWD HINGE FITTING FOUND CORROSION AROUND FASTENER AND BEARING LUG. THE DAMAGE WAS BLENDED AS SHOWN IN FIGURES 1 THRU 4 OF ERA 544735-14.SDR DALA2016050403727Frame · dentedFWD CARGO BAY LT SIDE FRAME BS 540 HAS TWO DENTS BETWEEN STRINGERS 24 AND 25L. ACCOMPLISHED PERMANENT REPAIR IAW ER/A 544720-14AD.SDR DALA2016050403726Frame · dentedTHREE DENTS ON AFT CARGO RT FRAME UPPER FLANGE AT BS 1300 BETWEEN STR 25-26R. ACCOMPLISHED PERMANENT REPAIR IAW ER/A 544742-14.SDR DALA2016050603741Intercostal · corrodedCORROSION ON AFT CARGO BILGE INTERCOSTAL INBD AND OTBD SIDE BETWEEN BS 1400-1420, LBL-16. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS REF SRM. R & R INTERCOSTAL AT AFT CARGO COMPT BETWEEN BS 1400 TO BS 1420, LBL 16 REF DWG AND SRM.SDR DALA2016050203724Actuator · corrodedHORIZONTAL STABILIZER TRIM ACTUATOR, HAS RUST AROUND BASE OF BALLSCREW AND STOP FITTING. HORIZONTAL STABILIZER TRIM ACTUATOR REMOVED AND NEW SERVICEABLE HORIZONTAL STABILIZER TRIM ACTUATOR, BALLSCREW, INSTALLED IAW 757-6801-9822-AMMS 27-41-10-024-001 AND AMM SDR DALA2016050203721Pan · corrodedSURFACE CORROSION ON TOP OF LAV PAN IN AFT CARGO BETWEEN BS 1540-1560. REMOVED CORROSION ON TOP OF LAV PAN IN AFT CARGO ORIG THICKNESS .080 MATERIAL LOSS .028 OUT OF LIMITS IAW SRM 53-00-53.SDR DALA2016050503754Gate · corrodedR1 DOOR LOWER GATE HAS CORROSION ALONG UPPER AND LOWER EDGE. FOUND CORROSION ON R-1 DOOR LOWER GATE LOWER EDGE LENGTH AT 4.97", FOUND UPPER EDGE LENGTH AT 4.09" BOTH OUT OF LIMITS IAW SRM 52-10-02, FIG 101, DETAIL IV. R & R R-1 DOOR LOWER GATE IAW AMM 52-11-SDR DALA2016050403728Structure · damagedDURING REMOVAL OF FUEL TANK SUMP DRAIN VALVE BUSHING THE HOLE WAS FOUND TO BE ELONGATED BEYOND DWG 112N4101 LIMITS AND DOES NOT ALLOW THE CORRECT INSTALLATION OF NEW SUMP DRAIN VALVE BUSHING.SDR DALA2016050503753Intercostal · crackedUPON REMOVAL OF SEAT TRACK AT BS 1320-1340, RBL 45, FOUND INTERCOSTAL WEB CRACK. R & R INTERCOSTAL WEB AT BS 1320-1340, RBL 45 IAW SRM 51-40-02, PG 2, REF DWG 146N5180.SDR DALA2016050503752Seat Track · corrodedCORROSION ON MAIN CABIN SEAT TRACK SUPPORT BS 1640, RBL 24. REMOVED CORROSION ON SEAT TRACK SUPPORT AT BS 1640, RBL 24. MATERIAL LOSS IS .015". ORIGINAL MATERIAL THICKNESS IS .070" REF BAC1508-240/BOEING DWG 146N5126-2. FOUND TO BE OUT OF LIMIT IAW SRM 53-
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