N648NN
Service difficulty reports · 36
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 = 'N648NN' 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 = 'N648NN' 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 VNAA202610060037Hinge Fitting · corrodedCORROSION ON HINGE FITTINGS (4 EA`S) WAS FOUND IN THE BONDING JUMPER SETTLEMENT AREA AT RH WING. AREAS ON HINGE FITTINGS (4 EA`S) IN THE BONDING JUMPER SETTLEMENT AREA AT RH WING WERE REPAIRED PER REO 690-57-51-556 REV --.SDR VNAA202610060036Attach Bracket · corrodedCORROSION ON SUPPORTS (2EAS) THROUGHT ACCESS PANELS 542AZ/642AZ ON WS 29 AT LH/RH W/W MLG BAY. SUPPORTS (2EAS) THROUGHT ACCESS PANELS 542AZ/642AZ ON WS 29 AT LH/RH W/W MLG BAY WERE REPLACED PER SRM 51-42-06-001-001-A01SDR VNAA202610060035Attach Bracket · corrodedCORROSION ON CLIPS (2EAS) THROUGHT ACCESS PANELS 542AZ/642AZ ON WS 48 AT LH/RH MLG W/W BAY. CLIPS (2EAS) THROUGHT ACCESS PANELS 542AZ/642AZ ON WS 48 AT LH/RH MLG W/W BAY WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01SDR VNAA202610060031Attach Bracket · corrodedDURING MODIFICATION OF THE SINGLEPOINT PRESSURE REFUEL DEFUEL CRACK WAS FOUND ON WEB BTW STGR21 AND FS669.40. AFT MOUNTING SUPPORT SINGLE POINT PRESSURE REFUEL DEFUEL BTW STGR21 AND FS669.40 WAS REPAIRED PER REO 690-28-25-051 REV --SDR VNAA202610060027Rib · crackedCRACK ON MACHINED RIB LEADING EDGE SS58.41 AT LEFT WING. MACHINED RIB LEADING EDGE SS58.41 AT LEFT WING WAS REPPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01SDR VNAA202610060026Rib · crackedCRACK ON MACHINED RIB LEADING EDGE SS58.41 AT RIGHT WING. MACHINED RIB LEADING EDGE SS58.41 AT RIGHT WING WAS REPLACED PER SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01SDR VNAA202610060025Hinge · wornFREE PLAY ON BEARING OF RUDDER HINGE FITTING #2 #3 AT REAR SPAR OF HORIZONTAL STABILIZER. RUDDER HINGE FITTING #2 #3 AT REAR SPAR OF HORIZONTAL STABILIZER WERE REPLACED PER RIL #1213 REV. NCSDR VNAA202610060024Bolt · crackedCORROSION ON HARDWARE ON UPPER ATTACHMENT OF RH FLAP MOVEABLE VANE INBOARD ACTUATOR. HARDWARE WITH CORROSION ON UPPER ATTACHMENT OF RH FLAP MOVEABLE VANE INBOARD ACTUATOR WERE REPLACED PER MHIRJ CMM 57-52-02SDR VNAA202610060032Attach Bracket · crackedDURING MODIFICATION OF THE SINGLEPOINT PRESSURE REFUEL DEFUEL CRACK WAS FOUND ON WEB BTW STGR21 AND FS669.40. AFT MOUNTING SUPPORT SINGLEPOINT PRESSURE REFUEL DEFUEL BTW STGR21 AND FS669.40 WAS REPAIRED PER REO 690-28-25-051 REV --.SDR VNAA202610060028Floorbeam · corrodedAFTER REMOVAL OF FITTING AT FS 349 LH SIDE FLOOR STRUCTURE LEVEL ON PASSENGER CABIN: CORROSION WAS FOUND. FITTING AT BS 349 LH SIDE FLOOR STRUCTURE LEVEL WAS EVALUATED WITH EXCESSIVE CORROSION PER SRM 51-10-06-001-001-A01 AND REPLACED PER SRM 51-42-20-001-00SDR VNAA202610060023Canister · crackedCRACK IN CANISTER WELDED NO.3 IN WS=148 AT RH MAIN FUEL TANK. CANISTER WAS REPAIRED PER PER REO 670-57-42-577 REV.-SDR VNAA202610060022Shear Panel · corrodedCORROSION ON SHEAR PANEL STA FS=1096 FROM LBL=28 TO RBL=28 AT AFT BAGGAGE BAY FLOOR STRUCTURE. SHEAR PANEL STA FS=1096 FROM LBL=28 TO RBL=28 AT AFT BAGGAGE BAY FLOOR STRUCTURE WAS REPAIRED PER REO 670-53-61-1080 REV - -SDR VNAA202610060019Floorbeam · corrodedCORROSION ON FITTING OF WEB END FS 349 LBL SIDE AT FLOOR STRUCTURE LEVEL ON PASSENGER CABIN. FITTING OF WEB END FS 349 LBL SIDE AT FLOOR STRUCTURE LEVEL ON PASSENGER CABIN WAS EVALUATED THEREFORE IT IS OUT LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 AND REPLASDR VNAA202610060016Drip Tray · corrodedINITIAL INSPECTION: CORROSION ON DRAIN PAN STA FS=280 LBL 13 AT PASSENGER CABIN. DRIP TRAY ASSY (DRAIN PAN) FS=280 LBL 13 AT PASSENGER CABIN WAS EVALUATED THEREFORE AREA IT IS OUT OF LIMITS PER SRM 53-21-43-101-001-A03 AND REPLACED PER CRJ900 SRM 51-42-10-001SDR VNAA202610060004Channel · damagedCORROSION ON NUT CHANNEL IN THE LH/RH MLG WHEEL WELL STRUCTURE, NEXT TO THE MLG UPLOCKS. NUT CHANNEL IN THE LH/RH MLG WHEEL WELL STRUCTURE, NEXT TO THE MLG UPLOCKS WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-41-02-001-001-A01SDR VNAA202610060003Flap · nickedSEVERAL NICKS BTW FLS=15.00 TO FLS=40.00 INBOARD FLAP AT RH WING. SEVERAL NICKS BTW FLS=15.00 TO FLS=40.00 ON INBOARD FLAP AT RH WING WAS REPAIRED PER CRJ-900 SRM 57-52-01-201-005-A01SDR VNAA202610060021Retainer · corrodedCORROSION ON NUT RETAINER CLIPS OF PASSENGER WINDOWS 22LH AT CPAX. ANCHOR NUT (6EAS) WERE REPLACED ON PASSENGER WINDOWS 22LH AT CPAX PER SRM 52-42-06-001-001-A01SDR VNAA202610060020Rib · corrodedCORROSION ON SETTLEMENT AREA OF THE ACCESS PANELS 621AT, 621AB & 621BR. AT RH WING LEADING EDGE. CORROSION ON SETTLEMENT AREA OF THE ACCESS PANELS 621AT, 621AB & 621BR AT RH WING LEADING EDGE WAS REPAIRED PER REO 690-57-41-634 REV --, REO 690-57-41-636 REV --SDR VNAA202610060018Fitting · corrodedCORROSION ON FWD/AFT HINGE HOUSINGS ON LOWER SILL OF THRESHOLD AT PASSENGER DOOR. FWD AND AFT HINGE (FITTING) HOUSINGS ON LOWER SILL AT PASSENGER DOOR WERE EVALUATED THEREFORE IS OUT LIMITS PER SRM 53-21-23-101-001-A02 AND WERE REPLACED PER SRM 51-42-21-001-SDR VNAA202610060017Angle · corrodedCORROSION ON EDGE OF ANGLES (2 E/AS) BTW FS 316 TO FS 349 ON LOWER SILL OF THRESHOLD AT PASSENGER DOOR. CORROSION ON EDGE OF ANGLES (2 E/AS) BTW FS 316 TO FS 349 ON LOWER SILL OF THRESHOLD AT PASSENGER DOOR WAS REMOVED PER SRM 51-21-06-001-001-A01 AND WAS EVSDR VNAA202610060029Frame · corrodedCORROSION ON FRAME STA 1088 BTW STGR 27RH AND 26RH AT AFT CARGO COMPT. FRAME STA 1088 BTW STGR 27RH AND 26RH AT AFT CARGO COMPT WAS REPAIRED PER REO 690-53-61-1809 REV. - -SDR VNAA202610060015Seat Track · corrodedCORROSION ON RH SIDE SEAT RAIL BTW FS 744 TO FS 752, BTW FS 813 TO FS 830, FS 847+26 TO 847+32, AT PASSENGER CABIN. RH SIDE SEAT RAIL BTW FS 744 TO FS 752, BTW FS 813 TO FS 830, FS 847+26 TO 847+32, AT PASSENGER CABIN WAS EVALUATE AND FOUND EXCESSIVE DAMAGE PSDR VNAA202610060014Seat Track · corrodedCORROSION ON LH SIDE SEAT RAIL BTW FS 699 TO FS 705 AT PASSENGER CABIN. LH SIDE SEAT RAIL BTW FS 699 TO FS 705 AT PASSENGER CABIN WAS FOUND OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG A12)SDR VNAA202610060013Latch · corrodedCORROSION ON LEVER COVER GUARD OF FWD HANDLE MODULE. LEVER COVER GUARD OF FWD HANDLE MODULE WAS REPLACED PER TELAIR INTERNATIONAL CMM BAGGAGE RETRIEVAL SYSTEM 25-50-82SDR VNAA202610060009Intercostal · corrodedCORROSION ON FWD FACE OF THE MIDDLE SUPPORT AT THE SETTLEMENT ACCESS PANEL (642AZ) RH MLG BAY. MIDDLE SUPPORT (INTERCOSTAL) AT THE SETTLEMENT ACCESS PANEL (642AZ) RH MLG BAY WERE EVALUATED THEREFORE IS OUT LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS RSDR VNAA202610060012Support Angle · corrodedCORROSION ON CLIP SUPPORTS AT SETTLEMENT AREA OF FAIRING PANELS 686BB, 686AB, 683AB, 683BB, 583AB, 583BB, 586AB, AND 586BB. CORROSION ON CLIP SUPPORTS AT SETTLEMENT AREA OF FAIRING PANELS 686BB, 686AB, 683BB, 583AB, 583BB, 586AB, AND 586BB WAS REMOVED AND EVSDR VNAA202610060011Rub Strip · corrodedCORROSION ON INTERNAL SKIN CUTOUT AT SETTLEMENT AREA OF MAIN AVIONICS COMPARTMENT DOOR BTW FS364.00 TO FS394.00 AND STGR 25L TO STGR 25R. CORROSION ON STRIPS LH FWD AND AFT AND RH AFT ON INTERNAL CUTOUT AT SETTLEMENT AREA OF MAIN AVIONICS COMPARTMENT DOOR BTWSDR VNAA202610060010Angle · corrodedCORROSION ON MID CAP ANGLE AND LOWER ANGLE KICK PLATE AT PASSENGER DOOR FUSELAGE FRAME, BTW FS 310.00 TO FS 349.00. MID CAP ANGLE AND LOWER ANGLE KICK PLATE AT PASSENGER DOOR FUSELAGE FRAME, BTW FS 310.00 TO FS 349.00 WERE EVALUATED AND FOUND EXCESSIVE CORROSSDR VNAA202610060008Angle · corrodedCORROSION ON ANGLES OF MID INTERCOSTAL OF SETTLEMENT AREA OF ACCESS PANELS (542AZ & 642AZ) AT LH/RH MLG BAY (ZONE 170). ANGLES OF MID INTERCOSTAL OF SETTLEMENT AREA OF ACCESS PANELS (542AZ & 642AZ) AT LH/RH MLG BAY WERE EVALUATED AND FOUND EXCESSIVE DAMAGE PSDR VNAA202610060007Light · corrodedCORROSION ON LH & RH MAINTENANCE LIGHT CASE (DS49 & DS50), AT MLG BAY. LH & RH MAINTENANCE LIGHT CASE AT MLG BAY WERE REPLACED PER CRJ-900 AMM 33-32-07.SDR VNAA202610060006Support Plate · corrodedCORROSION ON MLG HYD LINES SUPPORT PLATE (IN BK, LG EXT, LG RET) AT LH RH W/W MLG. MLG HYD LINES SUPPORT PLATE (IN BK, LG EXT, LG RET) P/N: CC670-10337-1 AND P/N: CC670-10337-2 AT L/H R/H W/W MLG WERE REPLACED PER CRJ900 AMM 20-21-00-910-801-A01SDR VNAA202610060005Support · corrodedCORROSION ON SUPPORTS FS785 LBL14/RBL14,LBL34 AND RBL34 (4EAS) FS813 LBL47 (2EAS) AND RBL47 (1EAS) AND FS847 BTW LBL5 TO RBL3 AT LH/RH WHEEL WELL AREA. CORROSION ON SUPPORTS FS813 LBL47 (2EAS) AND RBL47 (1EAS) AND FS847 BTW LBL5 TO RBL3 AT LH/RH WHEEL WELL ARSDR VNAA202610060002Hinge · corrodedCORROSION ON FITTING SUPPORTS AND HINGES OF ACCESS AFT POTABLE WATER, AFT LAVATORY SERVICE AND FASTENERS AND SHIMS ON HINGES LP GROUND CONNECTION AT AFT FAIRINGS AREA. HINGE ASSY (2EAS) AND BRACKET ASSY (2EAS) OF ACCESS PANEL AFT WATER SERVICE DOOR (195EL) ANSDR VNAA202610060001Hinge · corrodedCORROSION ON FITTING SUPPORTS AND HINGES OF ACCESS AFT POTABLE WATER, AFT LAVATORY SERVICE AND FASTENERS AND SHIMS ON HINGES LP GROUND CONNECTION AT AFT FAIRINGS AREA. HINGE ASSY (2EAS) AND BRACKET ASSY (2EAS) OF ACCESS PANEL AFT WATER SERVICE DOOR (195EL) ANSDR VNAA202610060033Hinge Fitting · mechanic errorMAINTENANCE ERROR: AFTER REMOVAL OF RH AILERON TOOL MARK ON R5 OF CENTER HINGE FITTING OF OUTB AILERON PCU. R5 OF CENTER HINGE FITTING OF OUTB AILERON PCU WAS REPAIRED PER REO 690-57-61-543 REV - -SDR VNAA202610060030Aileron · corrodedREF TO TRFKE00GTBX6. AFTER REMOVAL OF BEARING AND BUSHING ON RH AILERON CORROSION ON LUGS BORES: R2, R3, R4 AND R6 WAS FOUND AT CENTER HINGE FITTING AND UPPER/LOWER HOLES OF OUTB HINGE FITTING. LUGS BORES R4, R6 AT CENTER HINGE FITTING AND UPPER HOLE OF OUTB
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