N946AT
Service difficulty reports · 270
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 = 'N946AT' 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 = 'N946AT' 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 DALA2019101205868Frame Angle · corrodedCORROSION FRAME CLIP STA. Y=908 BTW L= 29R/28L, Y=927 BTW L= 29R/29L, Y=954 BTW L= 29L/28R, Y=974 BTW L= 29R/26L AND Y=1002 BTW L= 29L/29R AT AFT CARGO COMPARTMENT. (CORROSION LEVEL 2): FRAME CLIPS STA Y= 974 AND 1002 WERE REPLACED PER B717-200 SRM 51-41-02-0GSDR DALA2019101205867Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN BTW STA 1025 AND 1035 STRINGERS 13 AND 15 LH SIDE. EXTERNAL FUSELAGE SKIN BTW STA 1025 AND 1035 STRINGERS 13 AND 15 LH SIDEL WAS REPAIRED PER ER/A 582117-14 REV.ORIGINAL (SECTION I PERMANENT REPAIR) AND ETI-17-19-175 REV.2. (LP1SDR DALA2019101205866Frame · crackedCRACK ON FRAME STA Y= 1178.225 CANT BTW PROJECTION LONGERON 17 AND 16 RH AT AFT ACCESSORY COMPARTMENT. DOUBLER ON FRAME STA Y=1178.225 CANT BTW PROJECTION LONGERON 17 AND 16 RH AT AFT ACCESSORY COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G AND DWG SR95SDR DALA2019101105830Frame · crackedCRACK ON FRAME STA 1037 AND LONGERON 17L (CPAX) (SM). NRC 00529: FRAME STA 1037 AND LONGERON 17L WAS REPAIRED PER ER/A 581846-14 REV. ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-581846 ADDED FOR AC 9506. (LP #1309535)SDR DALA2019101105829Door Frame · crackedCRACKED DOOR JAMB ON THE TOP AT LH FWD OVERWING EMERGENCY EXIT DOOR (PTAS). NRC 00065: DOOR JAMB ON THE TOP AT LH FWD OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER B-717-200 SRM 53-20-15-2R PROCEDURE 8 REPAIR 8 FIGURE 201. (LP #1309531)SDR DALA2019101005820Access Panel · corrodedCORROSION ON COUNTERSINK AREA ON ACCESS PLATES #620EB, 520LB, AND 620FT. CORROSION ON COUNTERSINK AREA ON ACCESS PLATES #620EB, 520LB, AND 620FT WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR.26. REMAINING MATERIAL IS OUT OF LIMITS PER B717-200 SRM 57-10-01 RESDR DALA2019101005819Bracket · corrodedEXCESSIVE CORROSION ON LOWER BRACKET BTW STA Y=1022 AND 1037 AT AFT CARGO COMPARMENT. (CCT). NRC 00646: CORROSION LEVEL 2, LOWER BRACKET BTW STA Y=1022 AND 1037 AT AFT CARGO COMPARMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND DWG #5936667 REV. BU.SDR DALA2019100905787Longeron · corrodedCORROSION ON LONGERONS ENDS #25 AND 27 OF CCT BTW STA=1002 RH SIDE (SM). NRC 00593: COROSION LEVEL 2, LONGERONS ENDS #25 AND 27 OF CCT BTW STA=1002 RH SIDE WERE REPLACED PER B717-200 SRM 51-41-05-0G. (LP #1306330)SDR DALA2019100905786Frame · crackedCRACK WITH 0.125 IN OF LENGTH WAS FOUND ON OVERWING FRAME AT STA Y=674.000 RH. OVERWING FRAME AT STA Y=674.000 RH WAS REPLACED PER B717-200 CARD 5310-01436-03B. (LP #1306202)SDR DALA2019100705768Frame · crackedCRACK ON FRAME LONGERON 17R AND STA 1037 (CPAX) (SM). NRC 00535: FRAME LONGERON 17R AND STA 1037 WERE REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 4.SDR DALA2019100705767Floor Support · damagedENLOGATED HOLE OF FLOOR SUPPORT W1 X=7 BTW STA=235 AND STA=240 CABIN PAX (SM). NRC 00415: FLOOR SUPPORT W1 X=7 BTW STA=235 AND STA=240 CABIN PAX WAS REPLACED PER B717-200 SRM 53-10-51-0I-2 AND SRM 51-41-05-0G.SDR DALA2019100705766Rub Strip · corrodedCORROSION ON FUEL ACCESS CUTOUTS (RUBSTRIPS) #520CT, 520DT, 520FT, AND 141AL AT LH WING. (AI). NRC 0564: CORROSION LEVEL 2, FUEL ACCESS (RUBSTRIPS) #520CT, 520DT, 520FT, AND 141AL WERE REPLACED PER B717-200 SRM 57- 10-01-2R-3. (LP #1303518)SDR DALA2019100705765Rub Strip · corrodedCORROSION AT CUTOUTS (RUBSTRIPS) #620CT, 620DT, 620FT, AND 141AR RH WING. ORIGINAL THICKNESS ARE .020" AND REMAINING THICKNESS ARE .011" THEREFORE ARE OUT OF LIMITS IN REF NRC 00565. NRC 0627: CORROSION LEVEL 2, FUEL ACCESS (RUBSTRIPS) #620CT, 620DT, 620FT, ANSDR DALA2019100765764Access Panel · corrodedCORROSION ON COUNTERSINK AREA ON ACCESS PLATES 520FT AND 141AR. CORROSION ON COUNTERSINK AREA ON ACCESS PLATES #520FT AND 141AR ARE OUT OF LIMITS IAW SRM 57-10-01 REPAIR 2 PAR. 5 C. (CONDITION III) TABLE 201 AND WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26SDR DALA2019100765763Doubler · corrodedCORROSION ON DOUBLER REPAIR EXTERNAL SKIN OF AFT LAVATORY. DOUBLER REPAIR EXTERNAL SKIN OF AFT LAVATORY WAS REPLACED PER ER/A 542102-14 REV. ORIGINAL, SECTION 1.SDR DALA2019100765762Cusp Web · crackedCRACK ON CUSP WEB MEMBRANE CABIN PAX BTW STA 433 TO 435 RH SIDE (SM). NRC 00650: CUSP WEB MEMBRANE CABIN PAX BTW STA 433 TO 435 RH SIDE WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG 211.SDR DALA2019100765761Longeron · crackedCRACKED LONGERON 4LH STA 1022 AT CPAX. NRC 00534: LONGERON 4LH STA 1022 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-05-2R.SDR DALA2019100765760Cusp Web · corrodedEXCESSIVE CORROSION ON CUSP MEMBRANE WEB LH SIDE FROM STA Y=832 TO STA Y=851 IS OUT OF LIMITS. CUSP MEMBRANE WEB LH SIDE FROM STA Y=832 TO STA Y=851 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG. 215.SDR DALA2019100985784Door Frame · crackedCRACK ON DOOR JAMB OF WHEEL WELL NLG BTW STA=40 AND STA=50 RH SIDE (SM). NRC 00441: DOOR JAMB OF WHEEL WELL NLG BTW STA=40 AND STA=50 RH SIDE WAS REPAIRED PER B717-200 SRM 53-10-14-2R-2 FIG. 201. (LP #1300863)SDR DALA2019100985783Door Frame · crackedCRACK ON DOOR JAMB OF WHEEL WELL NLG BTW STA=40 AND STA=50 LH SIDE. DOOR JAMB OF WHEEL WELL NLG BTW STA=40 AND STA=50 LH SIDE WAS REPAIRED PER B717-200 SRM 53-10-14-2R-2 FIG. 201. (LP #1300907)SDR DALA2019100505773Cusp Web · corrodedEXCESSIVE CORROSION ON STA Y=516 TO Y=522 RH SIDE CUSP WEB AREA IS OUT OF LIMITS. NRC 00644: CORROSION LEVEL 2, RH SIDE CUPS WEB ON STA Y= 516 TO Y=522 WAS REPAIRED PER B-717-200 SRM 53-00-55-2R-4 FIG 216.SDR DALA2019100855772Access Panel · corrodedCORROSION ON COUNTERSINK ON ACCESS PLATES #520CT AND 620CT (AI)(AD). NRC 00571: CORROSION LEVEL 2, FUEL ACCESS PLATES 520CT AND 620CT WERE REPLACED PER AMDS 2040-0010 AND 2040-00 12. (LP #1300191)SDR DALA2019100405728Cusp Web · crackedCRACK ON CUSP WEB MEMBRANE CABIN PAX BTW STA 560 TO 567 LH SIDE (SM). LH SIDE CUPS WEB ON STA Y=560 TO Y=567 WAS REPAIRED PER B-717-200 SRM 53-00-55-2R-4 FIG 215.SDR DALA2019100405726Floor Support · corrodedCORROSION ON FLOOR SUPPORT 160G OF W1 AREA CABIN PAX (SM). CORROSION LEVEL 2. FLOOR SUPPORT 160G OF W1 AREA WAS REPLACED PER B717-200 SRM 51-41-05-0G AND 53-10-51-0I-2. CORROSION ON FLOOR SUPPORT 160G OF W1 AREA CABIN PAX WAS OUT OF LIMITS PER B717-200 SRM 53-SDR DALA2019100405724Access Panel · corrodedCORROSION ON COUNTERSINK ON ACCESS PLATES #520DT, 520CB, AND 520GB (AI). NRC 00570: CORROSION LEVEL 2, CORROSION ON COUNTERSINK ON ACCESS PLATES #520DT, 520CB, AND 520GB WAS REMOVED PER B717-200 SRM 51-10-04-0G. CORROSION WAS OUT OF LIMITS PER B717-200 SRM 57-SDR DALA2019100405723Floor Panel · crackedCRACKED FLOOR PANEL #211ANF IN COCKPIT. (CPIL). NRC 00602: FLOOR PANEL #211ANF WAS FABRICATED, REPLACED, AND IDENTIFIED PER B717-200 SRM 53-20-50-2R-3. (LP #1299518)SDR DALA2019100405722Floor Panel · delaminatedDELAMINATED FLOOR PANEL #222YF PAX CABIN. CPAX (W -1). NRC 00600: FLOOR PANEL 222YF WAS FABRICATED, REPLACED, AND IDENTIFIED PER B-717-200 SRM 53-20-50-2R-3. (LP #1299472)SDR DALA2019100405721Floor Support · corrodedCORROSION FLOOR SUPPORT STA X-44 BTW Y1022 TO Y1076 (W2). NRC 00449: CORROSION LEVEL 2, FLOOR SUPPORT STA X-44 BTW Y1022 TO Y1076 (W2) WAS REPLACED DUE TO EXCESSIVE DAMAGE PER B717-200 SRM 51-30-05-0G. AND DWG 9981474 REV: L , CORROSION ON FLOOR SUPPORT STA X-SDR DALA2019100405720Cusp Web · crackedCRACK ON CUSP MEMBRANE WEB RH SIDE FROM STA Y=715 TO STA Y=734 AT PAX CABIN. (CPAX) NRC 00490: CUSP MEMBRANE WEB RH SIDE FROM STA Y=715 TO STA Y=734 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG. 206. (LP #1299273)SDR DALA2019100305652Longeron · crackedCRACK ON LONGERON 17L AND STA 1037 (CPAX) (SM). NRC 00532: LONGERON 17L AND STA 1037 WAS REPAIRED PER B717-200 SRM 53-00-05-2R-2. (LP #1298001)SDR DALA2019100305651Floor Support · crackedCRACK ON FLOOR SUPPORT OF W1 X=11 BTW STA 218 CABIN PAX (W1). NRC 00414: FLOOR SUPPORT OF W1 X=11 BTW STA 218 WAS REPLACED PER B717-200 SRM 51-41-02-0G. (LP #1297992)SDR DALA2019100305650Retainer · crackedCRACK ON RETAINER AT AFT UPPER CORNER OF THE COCKPIT RH SLIDING WINDOW CUT OUT ON REFERENCE OF NRC NBR 00132 (CPIL) (SM). NRC 00520: RETAINER WAS REPAIRED PER B717-200 SRM 56- 10-02-2R-1. CRACK WAS CONFIRMED AND STOPPED ON EXISTING FASTENER HOLE PER NDTSPM PARSDR DALA2019100305649Former · crackedCRACKED FORMER BTW STA Y674 AND X33 AT KEEL BEAMS INTERNAL STRUCTURE (FUS). NRC 00422: CRACKED FORMER BTW STA Y674 AND X33 WAS REPAIRED PER B717-200 SRM 51-70-11 -2R REP 1 FIG 201. (LP #1297596)SDR DALA2019100305648Former · crackedCRACKED FORMER BTW STA Y696 AND X28 AT KEEL BEAMS INTERNAL ESTRUCTURE (FUS). NRC 00421: FORMER BTW STA Y696 AND X28 WAS REPAIRED PER B717-200 SRM 51-70-11-2R REP 1 FIG 201.SDR DALA2019092805578Retainer · crackedCRACK ON RETAINER AT AFT UPPER CORNER OF THE COCKPIT LH SLIDING WINDOW CUT OUT ON REFERENCE OF NRC NBR 00131 (CPIL). NRC 00518: UPPER CORNER OF THE COCKPIT LH SLIDING WINDOW WAS REPAIRED PER B717-200 SRM 56-10-02-2R-1. (LP #1290372)SDR DALA2019092705566Pan · crackedCRACK ON UPPER/FWD RING PAN BTW STA Y=696/715 RH SIDE AT PAX CABIN (CPAX). NRC 00369: RING PAN UPPER/FWD BTW STA Y=696/715 RH SIDE AT PAX CABIN WAS REPAIRED PER B717-200 SRM 56-20-02-2R PROCEDURE 1, REPAIR 1. (LP #1288626)SDR DALA2019092705565Pan · crackedCRACK ON UP/AFT RING PAN BTW STA Y=813/832 RH SIDE AT PAX CABIN (CPAX). NRC 00368: RING PAN UP/AFT BTW STA Y=813/832 RH SIDE AT PAX CABIN WAS REPAIRED PER B717-200 SRM 56-20-02-2R PROCEDURE 1, REPAIR 1. (LP #1288615)SDR DALA2019092705564Pan · crackedCRACK ON UP/AFT RING PAN BTW STA Y=851/870 LH SIDE AT PAX CABIN (CPAX). NRC 00367: RING PAN UP/AFT BTW STA Y=851/870 LH SIDE AT PAX CABIN WAS REPAIRED PER B717-200 SRM 56-20-02-2R PROCEDURE 1, REPAIR 1. (LP #1288594)SDR DALA2019092705563Pan · crackedCRACK ON LWR/FWD RING PAN BTW STA Y=889/908 LH SIDE AT PAX CABIN (CPAX). NRC 00366: RING PAN LWR/FWD BTW STA Y=889/908 LH SIDE AT PAX CABIN WAS REPAIRED PER B717-200 SRM 56-20-02-2R PROCEDURE 1, REPAIR 1. (LP #1288590)SDR DALA2019092705562Pan · crackedCRACK ON LWR/FWD RING PAN BTW STA Y=655/636 LH SIDE AT PAX CABIN (CPAX). NRC 00363: RING PAN LWR/FWD BTW STA Y=655/636 LH SIDE AT PAX CABIN WAS REPAIRED PER B717-200 SRM 56-20-02-2R PROCEDURE 1, REPAIR 1. (LP #1288586)SDR DALA2019092705561Pan · crackedCRACK ON UP/AFT RING PAN BTW STA Y=813/832 LH SIDE AT PAX CABIN (CPAX). NRC 00365: RING PAN UP/AFT BTW STA Y=813/832 LH SIDE AT PAX CABIN WAS REPAIRED PER B717-200 SRM 56-20-02-2R PROCEDURE 1, REPAIR 1. (LP #1288575)SDR DALA2019092705560Pan · crackedCRACK ON LWR/FWD RING PAN BTW STA Y=617/636 LH SIDE AT PAX CABIN. NRC 00362: RING PAN LWR/FWD BTW STA Y=617/636 LH SIDE AT PAX CABIN WAS REPAIRED PER B717-200 SRM 56-20-02-2R PROCEDURE 1, REPAIR 1. (LP #1288531)SDR DALA2019092705559Pan · crackedCRACK ON LWR/FWD RING PAN BTW STA Y=794/813 LH SIDE AT PAX CABIN (CPAX). NRC 00364: RING PAN LWR/FWD BTW STA Y=794/813 LH WAS REPAIRED PER B717-200 SRM 56-20-02-2R PROCEDURE 1, REPAIR 1. (LP #1288517)SDR DALA2017110407938Skin · damagedVERTICAL STAB LOWER LE SKIN AT ZFS 52 WORN AND CHAFED. SKIN SPLICE ON INNER SURFACE 15 INCHES ALONG LEADING EDGE. REPAIRED IAW PRI 562910-14AD REV. 0, REV 1, AND REV. 2 AND ER/A 562910-14AD REV. ORIGINAL.SDR DALA2017110407937Skin · damagedVERTICAL STABILIZER LEADING EDGE HAD SIGNS OF DISTRESS TO COUNTERSINKS, ALL FASTENERS ARE LOOSE. REPAIRED IAW PRI 562910-14AD REV 0, REV 1. AND REV 2, ER/A 562910-14AD, REV ORIGINAL.SDR DALA2017110407936Spar Cap · damagedRT VERTICAL STABILIZER FRONT SPAR CAP FORWARD FLANGE, FIRST HOLE BELOW LEADING EDGE SKIN SPLICE IS OUT-OF-ROUND & UNABLE TO PERFORM OPEN-HOLE HFEC INSPECTION. REPAIRED IAW PRI 561916-14AD, REV 0, & 1, AND ER/A 561916-14AD, REV ORIG.SDR DALA2017110307934Threshold · corrodedCORROSION AT FWD LAVATORY ENTRY DOOR LOWER THRESHOLD. REPAIRED IAW PRI 561911-14, REV 0, AND ER/A 562911-14, REV ORIGINAL.SDR DALA2017110307929Skin · crackedFUSELAGE SKIN HAS A CRACK EMANATING FROM FASTENER HOLE 6 INCHES ABOVE RT PYLON, BS 1076. REPAIRED THE SKIN IAW PRI 562852-14, REV 0, REV 1, REV 2, AND ER/A 562852-14, REV ORIGINAL.SDR DALA2017110307927Skin · crackedFUSELAGE SKIN HAS A CRACK EMANATING FROM FASTENER HOLE AT BS 1095, 8 INCHES ABOVE THE LT PYLON. PERFORMED HFEC IAW AMM NDT SPM 06-10-01.001. REPAIRED THE SKIN IAW PRI 562854-14, REV 0, REV 1, AND REV 2, AND ER/A 562854-14, REV ORIGINAL.SDR DALA2017110207913Pan · corrodedAFT LOWER LEFT FUSELAGE, LAVATORY SERVICING PAN HAS MULTIPLE AREAS OF CORROSION. REPAIRED IAW ER/A 561915-14, REV ORIG.
Back to N946AT