N1402A, cancelled Oct 17, 2020
Service difficulty reports · 103
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 = 'N1402A' AND deregistration_id = 'N1402A-2020-10-17' 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 = 'N1402A' AND deregistration_id = 'N1402A-2020-10-17' 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 DALA2019051503063Slide · out of limitsFOUND L1 ESCAPE SLIDE INSPECTION OUT OF LIMITS. REPLACED L1 DOOR SLIDE. SYSTEM OPERATION IS NORMAL.SDR DALA2018110206417Structure · crackedBHEC INSPECTION OF BS 1809 RT OUTER STRUCTURE, SHOWS CRACK INDICATIONS AT 3 HOLE LOCATIONS. COMPLIED WITH E/RA 572634-14.SDR DALA2018110206415Hinge Fitting · gougedNR 2 ENGINE, OTBD CORE COWL, CENTER HINGE FITTING WAS GOUGED ON THE FORWARD SIDE. FOUND TO BE OUT OF LIMITS IAW SRM 54-53-90, COMPLIED WITH ER/A 572646-14.SDR DALA2018033002037Skin · crackedDURING SERVICE CHECK, FUSELAGE SKIN AT BS 1654.5, STRINGER 13L FOUND CRACKED. REMOVED THE DAMAGED AREA, PERFORMED EDDY CURRENT, AND INSTALLED A REPAIR DOUBLER AND FILLER IAW SRM 53-80-01, REPAIR 7.SDR DALA2018030401433Angle · crackedFUSELAGE BULKHEAD BS 1809.5 LEFT HALF AFT OUTER ANGLE CRACKED. COMPLIED WITH ERA 566145-14AD.SDR DALA2018030501428Fitting · crackedREMOVED AND REPLACED THE LT INNER TENSION FITTING AT BS 1809 DUE TO CRACKING. COMPLIED WITH ERA 566145-14AD.SDR DALA2018030201426Stringer · crackedLOWER AFT HOLE HAS CRACK INDICATIONS. REPAIRED IAW ERA 566145-14.SDR DALA2018030201425Skin · crackedFUSELAGE SKIN CRACKED AFT OF BS 1654.50, STRINGER 13R. REPAIRED IAW ERA 566160-14.SDR DALA2018022601298Slide · unwanted deployRIGHT SIDE OVER WING SLIDE DEPLOYED. REPLACED SLIDE. SYSTEM OPERATION IS NORMAL.SDR DALA2017062705032Cooling Fan · failedSMOKE IN COCKPIT, FOLLOWED BY FORWARD EQUIPMENT EXHAUST FAN STATUS MESSAGE. FOUND EQUIPMENT COOLING FAN INOPERATIVE AND REPLACED.SDR DALA2017060904596Seat Track · corrodedFOUND CORROSION ON SEAT TRACK, RBL 54.75, BS 852, REPLACED.SDR DALA2017051503966Seat Track · corrodedCORROSION ON RBL 33 SEAT TRACK, BS 852. REPLACED THE SEAT TRACK.SDR DALA2017051503965Seat Track · corrodedCORROSION ON SEAT TRACK, RBL 88.5, BS 852. REPLACED THE SEAT TRACK.SDR DALA2017051503964Seat Track · corrodedCORROSION ON RBL 74.75 SEAT TRACK AT BS 852. REPLACED THE SEAT TRACK.SDR DALA2017051303963Skin · corrodedFUSELAGE SKIN BULGING WITH FASTENERS PULLING, BS 1219, STRINGER 32L, APPROXIMATLEY 8 INCH AREA, 12 INCHES AFT OF PREVIOUS REPAIR. REPAIRED IAW ERA 558384-14.SDR DALA2017051503959Stringer Splice · corrodedSTRINGER SPLICE 34L, BS 1219 - 1241 CORRODED. REPAIRED IAW ERA 558384-14.SDR DALA2016120809816Wire · openRED EMERGENCY LIGHT AT DOOR 1R CLOSET WALL INOPERATIVE. FOUND OPEN WIRES AT FLOOR SPLICED IN LIGHT ASSEMBLY. SYSTEM OPERATION IS NORMAL.SDR DALA2016110208197Light · inoperativeR1 DOOR SLIDE LIGHT INOPERATIVE. MAINTENANCE REPLACED SLIDE LIGHT ASSEMBLY AND ADJUSTED TO SECURE LENS WITHIN LIGHT. SYSTEM OPERATION IS NORMAL.SDR DALA2016102507642Lens · wrong partEMERGENCY ESCAPE LIGHTS AT SEAT 26B LENS INCORRECT COLOR. REPLACED CLEAR LENS WITH RED LENS. SYSTEM OPERATION IS NORMAL.SDR DALA2016110208218Floor Panel · crackedDURING SERVICE CHECK FOUND A FLOOR PANEL CRACKED IN AFT CARGO AT STA 1200 BETWEEN RBL 20.5 AND 44.0 RT SIDE. C/W ERA 552002-14.SDR DALA2016021601132Connector · disconnectedEMERGENCY EXIT LIGHT AT 29AB ARE INOPERATIVE. MAINTENANCE RECONNECTED WIRE AT CONNECTOR. SYSTEM OPERATION IS NORMAL.SDR DALA2015082305237Electrical Box · contaminatedF/A REPORTED ELECTRICAL ODOR IN FIRST CLASS NEAR SEAT 4AB. TROUBLESHOT ENTIRE FIRST CLASS SECTION FOR ELECTRICAL ODOR, NONE FOUND. SUSPECT PASSENGER CHARGING UNIT. REPLACED VIDEO SEAT ELECTRIC BOX UNDER ROW 3A/D DUE TO EVIDENCE OF LIQUID SPILLAGE ON UNIT. SDR DALA2015051903358Floor Support · corrodedCABIN FLOOR SUPPORT UPPER CHORD CORRODED AT RBL 33.06, BS 852-915. REPAIRED IAW SRM 53-00-51.SDR DALA2015051903357Floor Support · corrodedCABIN FLOOR SUPPORT UPPER CHORD CORRODED AT RBL 74.18 AND BS 852. REPAIRED IAW SRM 53-00-51.SDR DALA2015051903356Floor Support · corrodedCABIN FLOORBEAM UPPER TEE CORRODED AT RBL 54.81, BS 852-903. REPAIRED IAW SRM 53-00-51.SDR DALA2015031202220Fuse · failedFOUND EMERGENCY LIGHTS ROWS 1 AB - 12 FG INOPERATIVE. MAINTENANCE REPLACED BLOWN FUSE. SYSTEM OPERATION IS NORMAL.SDR DALA2014071404134Power Supply · inoperativeLEFT EXTERIOR EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENENACE REPLACED THE POWER SUPPLY M738.SDR DALA13068361402Light · inoperativeEMERGENCY ESCAPE PATH LIGHT AT MID LAV AREA UNDER F/A SEAT INOPERATIVE. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT ASSY. CHECKED NORMAL.SDR DALA13034071402Connector · disconnectedEMERGENCY EXIT LIGHT AT SEAT 20G INOPERATIVE. MX RECONNECTED MATE-N-LOCK CONNECTOR AT LAMP ASSY. SYS OPS IS NORMAL.SDR DALA13028331402Fitting · crackedNR 2 PYLON CRACK INDICATION FOUND ON RT UPPER LINK PITCH LOAD FITTING AT MOST OTBD AFT FASTENER HOLE REPAIRED IAW PRI 514654-14AD, REV 0, REV 1, REV 2 AND REV 3. REPAIR COMPARED AND COMPLIED WITH ER/A 514654-14AD.SDR DALA13028321402Skin · crackedNR 2 PYLON, CRACK INDICATION FOUND ON RT UPPER WING SKIN LOAD FITTING AT MOST OTBD AFT FASTENER HOLE. WORK CARRIED OUT IAW PRI 514654-14AD, REV 0, REV 1 AND REV 2 AND REV 3.SDR DALA13028251402Fitting · damagedDURING HFEC OPEN HOLE INSPECTION ON RT WING NR 2 PYLON AFT DIAGONAL BRACE FITTING, FOUND OTBD FASTENER HOLE (01 EA) WITH HOLE EDGE DAMAGE ON LOWER WING SURFACE SIDE. OTBD FASTENER HOLE DAMAGE REWORKED IAW PRI 514643-14AD, REV 0 AND REV 1.SDR DALA13028241402Spar Web · canningNR 2 PYLON MID SPAR WEB FOUND OIL CANNING AND DEEP CHAFING AT LT SIDE, REPAIR CARRIED OUT IAW ERA 514639-14.SDR DALA13027261402Longeron Fitting · crackedCRACK INDICATION FOUND APPROX 0.3" IN LENGTH DURING HFEC ON RT SIDE UNDERWING LONGERON FITTING. FITTING REPAIRED IAW ER/A 514635-14AD.SDR DALA13027241402Failsafe · crackedULTRASONIC INSPECTION, FOUND CRACK INDICATION AT RT BS 955, FAILSAFE STRAP AT LOWER OF THE THE 3 FASTENER HOLES REPAIR COMPARED AND COMPLIED WITH ER/A 514032-14AD REV ORIGINAL.SDR DALA13027231402Failsafe · crackedULTRASONIC INSPECTION FOUND CRACK INDICATION AT LT BS 955, FAILSAFE STRAP AT LOWER OF THE 3 FASTENER HOLES. 3 FASTENER HOLES REPAIRED IAW PRI 514031-14AD, REV 0. REPAIR COMPARED AND COMPLIED WITH FINAL ER/A 514031-14AD.SDR DALA13027221402Skin · corrodedFOUND ON RT WING UPPER SURFACE, WITHIN FILLET AREA AT WBL 102 TO WBL 106 AND 11" FWD OF RT WING REAR SPAR. REPAIR COMPARED AND COMPLIED WITH FINAL ER/A 514645-14.SDR DALA13027211402Skin · corrodedRT WING UPPER FILLET AREA-CORROSION FOUND ON WING UPPER SURFACE BELOW BRACKET, WITHIN FILLET AREA AT WBL 101 TO WBL 102.5 AND FWD OF RT WING REAR SPAR 22.5" TO 23.5". REPAIR CARRIED OUT IAW PRI 514645-14.SDR DALA13028231402Skin · corrodedLEFT WING UPPER FILLET AREA-CORROSION FOUND ON LT WING UPPER SURFACE AT WBL 101 TO WBL 104.5 AND FWD OF LT WING REAR SPAR 14" TO 18.5" AS MARKED. REPAIR CARRIED OUT IAW ER/A 514644-14, REV ORIGINAL.SDR DALA13028221402Skin · corrodedCORROSION FOUND LT WING UPPER SURFACE AT WBL 101.5 TO WBL 104.5 AND 8.5 INCHES TO 12 INCHES FWD OF LT WING REAR SPAR CORRODED AREA. REPAIR CARRIED OUT IAW PRI 514644-14, REV 0.SDR DALA13027201402Skin · corrodedLT WING UPPER FILLET AREA-CORROSION FOUND ON LT WING UPPER SURFACE BELOW BRACKET, AT WBL 101 TO WBL 103.5 AND FWD OF LT WING REAR SPAR 22" TO 24". REPAIR CARRIED OUT IAW PRI 514644-14, REV 0 AND REV 1.SDR DALA13027191402Frame · corrodedCORROSION ON CABIN FRAME BS 1197+132 INBD FACE BETWEEN STRINGER 12-13L, CARRIED OUT REPAIR IAW ER/A514973-14.SDR DALA13027181402Frame · crackedCRACK INDICATION FOUND ON FRAME DURING HFEC INSPECTION ON LT BS 859.5, LBL 89, WL 200 FRAME INNER CHORD TRANSITION RADIUS APPROX 0.5". FRAME REPAIRED.SDR DALA13027171402Frame · crackedCRACK INDICATION FOUND DURING HFEC INSPECTION ON RT BS 883.5, RBL 89, WL 200 FRAME INNER CHORD TRANSITION RADIUS APPROX. 0.5" IN LENGTH AS MARKED. FRAME INNER CHORD REPAIR CARRIED OUT.SDR DALA13027031402Frame · crackedCRACK INDICATION FOUND DURING HFEC INSPECTION ON RT BS 903.5, RBL 89, WL 200 FRAME INNER CHORD TRANSITION RADIUS APPROX 1.0" IN LENGTH. RT BS 903.5, RBL 89, WL 200 FRAME REPAIR CARRIED OUT IAW WC 5311-01195-09-03B.SDR DALA13026321402Longeron · corrodedLONGERON 38R FOUND CORRODED AT BS 1540. BULK CARGO IAW SRM 53-00-03, FIG 201, REPAIR 2, REV 92. NEW STRINGER ANGLE AND CHANNEL FABRICATED USING MATERIAL 7075-0-0.050" AND 7075-0-0.040" AND INSTALLED REPAIR PARTS AT STA 1510 AND STA 1542 S38R IAW SRM 53-00-03SDR DALA13026061402Frame · crackedBS 1809, BULKHEAD RT FWD OUTER CHORD CRACKED AT STR 7-8R, REPAIRED IAW SRM 53-80-08, REPAIR 9.SDR DALA13026051402Frame · crackedDURING HFEC INSPECTION ON BS 1809 BULKHEAD LT FWD OUTER CHORD AT STR 6L TO 7L FOUND CRACKED. REPAIRED SRM 53-80-08, REPAIR 9, REV 92.00.SDR DALA13026331402Floorbeam · corrodedAFT CARGO FLOORBEAM SEVEN AREAS FOUND CORRODED BS 1153, RBL 20-42. REMOVED AND INSTALLED WITH NEW SPLICE IAW SRM 51-40-02.SDR DALA13023441402Floorbeam · corrodedCABIN FLOORBEAM AT BS 325 BETWEEN RBL 20 - 54.75 FOUND CORRODED. REPAIRED FROM LBL 45 TO RBL 60.
Back to N1402A, cancelled Oct 17, 2020