N979Z, cancelled Oct 19, 2005
Service difficulty reports · 48
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 = 'N979Z' AND deregistration_id = 'N979Z-2005-10-19' 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 = 'N979Z' AND deregistration_id = 'N979Z-2005-10-19' 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 ZW0A0107802Gyro · failedON TAKEOFF BOTH COMPASS CARDS SPUN RAPIDLY. NO FLAGS PRESENT. BOTH SYSTEMS DISAGREED WITH THE STANDBY/WET COMPASS. RETURNED TO STL. REPLACED THE NR 1 DG PN 2588302-4, THE NR 2 FLUX VALVE PN 2587794, AND THE NR 2 COMPASS RACK PN 614937-101. CHECK-C 12-3-00 STLSDR TWAA0010704Valve · wornLOST CABIN PRESSURIZATION AND PSU OXYGEN MASKS DEPLOYED. REPLACED THE RT FLOW CONTROL VALVE. CHECK-C 10-4-99 MCI. ---CLOSED---SDR TWAA9914004Stringer · crackedDURING OP 16 MAINT CHECK FOUND CABIN STRINGER 4L CRACKED AT FORMER STA 200. REPLACED STRINGER FROM APPROX STA 230 TO 170. INSTALLED REPAIR SPLICE AT STA 170 PER SRM 53-02, FIG 18.SDR TWAA9911906Seat Track · corrodedDURING OP 16 MAINT CHECK, CHAIR TRACK NUMBER 4 WAS CORRODED AT FLANGE, STA 857 THRU 965. NEW TRACK INSTALLED PER SPM 6-70-01. SPLICE PER SRM 53-05, FIG 4F SHEET 1.SDR TWAA9911903Bulkhead · crackedDURING OP 16 MAINT CHECK, THE RT BULKHEAD WAS CRACKED 3 INCHES LONG, LOCATED 1 INCH ABOVE FLOOR AND 5 INCHES FROM SIDEWALL ON FWD SIDE, STA 965. REMOVED AND REPLACED BULKHEAD PER SPM 6-70-01.SDR TWAA9911902Bulkhead Angle · crackedDURING OP 16 MAINT CHECK, FOUND AFT PRESS BULKHEAD, FWD SIDE DIAGONAL BRACE ATTACH ANGLE ON PRESSURE BULKHEAD, STA 996 AT UPPER END, CRACKED BETWEEN LONGERON 3L AND 4L. REMOVED CRACKED ANGLE AND FABRICATED NEW ANGLE. PAINTED AND REINSTALLED IN ACCORDANCE WITSDR TWAA9911905Longeron · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION IN CABIN AT LONGERON 18R, APPROX STA 946 ON WEB. REPLACED WEB PER SPM 6-70-01, ITEM 4 B-1.SDR TWAA9911904Longeron · corrodedDURING OP 16 MAINT CHECK, FOUND IN CABIN THERE WAS CORROSION ON LONGERON 18 WEB, STA 938R. REPLACED WEB PER SRM 6-70-01, ITEM 4 B-1.SDR TWAA9911211Support · corrodedDURING OP 16 MAINT CHECK, FOUND CENTER FLOOR SUPPORT BEAM AT STA 148 TO 218, WAS CORRODED. REPLACED PART PER SRM 6-70-01.SDR TWAA9911205Longeron · crackedDURING OP 16 MAINT CHECK, FOUND LONGERON CRACKED AT UPPER TIE POINT, STA 965, LONGERON 16R. REPAIRED PER SRM 53-02, FIG 18 PAGE 52, DRAWING 5911427.SDR TWAA9911204Support · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR PANEL SUPPORT AT STA 180, BL 0 TO RBL 45 IN. REPLACED PART PER SPM 6-70-01.SDR TWAA9911110Jamb · crackedDURING OP 16 MAINT CHECK IN THE FWD CARGO DOOR OPENING, FOUND A CRACK IN SUBSURFACE OF FUSELAGE AT LOWER AFT DOOR JAM AREA. INSTALLED A TWO PIECE DOUBLER. CRACK CONTAINMENT AS PER SRM 53-05, FIG 105, SHEET 1,2,3 AND 4, VIEW 7011C, DRAWING NUMBER 5910142, SHESDR TWAA9911109Angle · crackedDURING OP 16 MAINT CHECK AT STA 980, BETWEEN LONGERON 28L AND 27L, INTERCOSTAL ATTACH ANGLE WAS CRACKED. REPLACED CRACKED ANGLE WITH ANGLE OF SAME MATERIAL AS EXISTING, 7075-T6, PER SPM 6-70-01. REPLACED HI-LOCKS PER SRM 51-30-5, PAGE 12.SDR TWAA9911108Former · crackedDURING OP 16 MAINT CHECK, FOUND CRACK IN FORMER .5 INCHES IN LENGTH AT STA 965, LT FWD SIDE, AT JUNCTION OF LOWER LEG OF ENG MOUNT. INSTALLED CHORD ANGLE PART NR 9912243-9, AS PART OF MO 72J14 PHASE G, PER SPM 6-70-01.SDR TWAA9911107Angle · crackedDURING OP 16 MAINT CHECK, FOUND IN LT SIDE OF CABIN AT STA 965 FORMER TO LONGERON 17L HAD ATTACH ANGLE CRACKED. REPLACED ANGLE PART NR 2916078-501, PER SPM 6-70-01.SDR TWAA9911106Web · crackedDURING OP 16 MAINTENANCE, AFT PASSENGER DOOR WAS CRACKED AT PAN, FWD SIDE OF DOOR, ABOVE UPPER LATCH FITTING. REMOVED AND REPLACED WEB PER SRM 6-70-01, PAGE 2, ITEM 4A AND DRAWING NR 9915565.SDR TWAA9911105Angle · crackedDURING OP 16 MAINTENANCE CHECK, AFT CARGO AREA STATION 945, BETWEEN LEFT LONGERON NR 29 AND NR 30, FRAME ANGLE SPLICE WAS CRACKED AT A RIVET. REPLACED ANGLE WITH NEW PART PER SPM 6-70-01.SDR TWAA9911104Web · crackedDURING OP 16 MAINTENANCE CHECK, FOUND RT MLG WHEEL WELL CRACKED AT AFT INBD CORNER OF RT MLG WHEEL WELL, 30 INCHES FROM CABIN FLOOR. STOP DRILLED CRACK AND REPAIRED PER SRM 53-01 PAGE 10. INSTALLED FASTENERS PER SPM 6-30-07.SDR TWAA9910911Frame · crackedDURING OP 16 MAINT CHECK, FOUND CRACK IN RADIUS OF FRAME 9911505-6 APPROXIMATELY .75 INCH IN LENGTH, FWD OF RT CENTER WINDSHIELD POST, STA 83.5 AT X=-10. REPAIRED FRAME PER SRM 53-05, FIG 34.SDR TWAA9910910Frame · crackedDURING OP 16 MAINT CHECK, FOUND CRACK IN FRAME NUMBER 9911505-5 ALONG RIVETS APPROXIMATELY 1.25 INCHES IN LENGTH, FWD OF LT CENTER WINDSHIELD POST, STA 83.5 AT X=+10. REPAIRED FRAME PER SRM 53-03, FIG 34.SDR TWAA9910909Angle · crackedDURING OP 16 MAINT CHECK, FOUND ANGLE FROM FLOORBEAM TO INTERCOASTAL CRACKED AT STA 929, RBL 23 INCHES. REPLACED EXTRUSION PER SPM 6-70-01, PAGES 2 AND 3.SDR TWAA9910908Former Foot · crackedDURING OP 16 MAINT CHECK, FOUND CRACK AT FORMER FOOT AT AFT SIDE OF FORMER STA 1109, 10 INCHES LT SIDE OF LONGERON NUMBER 1. INSTALLED NEW FORMER FOOT PER SRM 51-30-2 AND SRM 51-30-5, AND TWA SPM 6-70-01.SDR TWAA9910907Former Foot · crackedDURING OP 16 MAINT CHECK, FOUND A CRACK AT THE FORMER FOOT AT THE AFT SIDE OF FORMER STA 1109, EIGHT INCHES RIGHT SIDE OF LONGERON 1. INSTALLED NEW FORMER FOOT PER SRM 51-30-2 AND SRM 51-30-5, AND TWA SPM 6-70-01.SDR TWAA9910906Stringer · crackedDURING OP 16 MAINT CHECK, FOUND STRINGER 4L CRACKED AT FORMER STA 200. REPLACED STRINGER FROM APPROX STA 230 TO 170. INSTALLED REPAIR SPLICE AT STA 170 PER SRM 53-02, FIG 18.SDR TWAA9910904Angle · crackedDURING OP 16 MAINT CHECK, FOUND FLOORBEAM SUPPORT ANGLE CRACKED AT STA 617, RBL 23 INCHES. REPLACED PARTS PER SPM 6-70-01, PAGE 3.SDR TWAA9910705Angle · crackedDURING OP 16 MAINT CHECK, FOUND AFT FUSELAGE RT SUPPORT ANGLE CRACKED AT LOWER LOUVER SUPPORT. REPLACED ANGLE PER SPM 6-70-01.SDR TWAA9910703Floorbeam · crackedDURING OP 16 MAINT CHECK, FOUND FLOOR SUPPORT BEAM CRACKED AT LT SIDEWALL STA 680. CONFIRMED BY NDT. REPLACED FLOOR SUPPORT PER SPM 6-70-01.SDR TWAA9910905Stringer · crackedDURING OP 16 MAINT CHECK, FOUND CABIN STRINGER 2L CRACKED AT FORMER STA 200. REPLACED CRACKED SECTIONS AND INSTALLED SPLICE PER SRM 53-02, PAGE 48 FIG 18, STA 188 TO 229.SDR TWAA9910704Angle · crackedDURING OP 16 MAINT CHECK, FOUND ANGLE FROM FLOORBEAM TO INTERCOSTAL CRACKED AT STA 897, RBL 23. REMOVED OLD ANGLE, FABRICATED NEW ANGLE, REINSTALLED NEW ANGLE AT STA 897, RBL 23, PER SPM 6-70-01.SDR TWAA9910702Splice · lightning strikeDURING OP 16 MAINT CHECK, FOUND STATIC BURN ON RIVET IN PRODUCTION SPLICE, STA 237 AND 218, RL 28 AND 29. REPLACED RIVET PER SRM 53-04, FIG 38.SDR TWAA9910701Support · crackedDURING OP 16 MAINT CHECK, THE VERTICAL SUPPORT FROM CARGO BIN TO FLOORBEAM WAS CRACKED AT TOP, STA 756 RBL 22 INCHES, AFT SIDE OF BEAM. STOP DRILLED CRACK PER SRM 53-01, PAGE 10. INSTALLED REPAIR ANGLES.SDR TWAA9909911Stiffener · crackedDURING OP 16 MAINT CHECK, FOUND COCKPIT VERTICAL STIFFENER 9957860-6, RT SIDE AT APPROXIMATELY 69.5, X=-10, CRACKED IN THE RADIUS. CRACK APPROXIMATELY 1 INCH LONG. REPLACED THE STIFFENER PER SPM 6-70-01, ITEM 4, B(2)A.SDR TWAA9909908Doubler · crackedDURING OP 16 MAINT CHECK, FOUND CRACK IN P/N 5912350-20 DOUBLER APPROXIMATELY 1.75 INCHES FORE AND AFT AT INBD END OF FRAME 9911505-6. FWD OF RT CENTER WINDSHIELD POST AT STA 83.5, X=-10. REMOVED DOUBLER PER SRO9530268 DRAWING. INSTALLED 912350-92 FILLER ANSDR TWAA9909907Doubler · crackedDURING OP 16 MAINT CHECK, FOUND NOSE HAD CRACK IN PART NBR 5912350-19 DOUBLER APPROXIMATELY .5 INCH FORE AND AFT AT INBD END OF FRAME 9911505-5. FORWARD OF LT CENTER WINDSHIELD POST AT STA 83.5 AT X=-10. INSTALLED NEW PART PER SPM 6-70-01.SDR TWAA9909909Longeron · damagedDURING OP 16 MAINT CHECK, FOUND STATIC BURN AT STA 180 TO 200, LONGERON 4L AND 5L, WAS GROUND BEYOND LIMITS. REPAIRED PER SRM 53-04, FIG 38 SHEET 18 VIEW E.SDR TWAA9909910Rib · crackedDURING OP 16 MAINT CHECK, FOUND STA ZPS 52 RIB CRACKED LT LOWER CORNER, STA ZFS 52 RIB CRACKED LOWER CORNER, AND STA ZFS 45 RIB CRACKED IN THE LOWER CORNER. REPAIRED PER SSRM 55-30-02.SDR TWAA9909604Stiffener · crackedDURING OP 16 MAINT CHECK, FOUND VERTICAL STIFFENER NUMBER 9957860-5, LT SIDE AT APPROXIMATELY STA 69.5, X=+10, CRACKED IN THE RADIUS. CRACK APPROXIMATELY .5 INCH LONG. REPLACED VERTICAL STIFFENER PER DRAWING PO9530268.SDR TWAA9909603Intercostal · crackedDURING OP 16 MAINT CHECK, INTERCOSTAL WAS CRACKED APPROXIMATELY .25 INCH IN BEND RADIUS AT FWD LOWER CORNER JUST AFT OF STA 69.5, RBL 12.5. MANUFACTURED NEW INTERCOSTAL PER DRAWING PO9530268. PRIMED AND INSTALLED.SDR TWAA9909602Intercostal · crackedDURING OP 16 MAINT CHECK, FOUND INTERCOSTAL CRACKED APPROXIMATELY .25 INCH IN BEND RADIUS AT FWD LOWER CORNER JUST AFT OF STA 69.5, LBL 12.5 IN. MANUFACTURED NEW INTERCOSTAL PER DRAWING PO9530268. PRIMED AND INSTALLED.SDR TWAA9909605Skin · crackedDURING OP 16 MAINT CHECK, FOUND CRACK APPROXIMATELY 1 INCH AT TOP OF WING LEADING EDGE AT APPROXIMATELY 18 IN OTBD OF NR 7 LEADING EDGE SLAT TRACK. REPAIRED PER SRM 57-06A.SDR TWAA9908904Bulkhead Brace · crackedDURING OP 16 MAINT CHECK, FOUND AFT PRESSURE BULKHEAD, FORWARD SIDE DIAGIONAL BRACE ON PRESSURE BULKHEAD AT STA 996, CRACKED AT UPPER END BETWEEN LONGERON 3L AND 4L. REMOVED, FABRICATED AND REINSTALLED ANGLE AT UPPER DIAGONAL BRACE, STA 996 BETWEEN L3L ANG L4SDR TWAA9908903Stiffener · crackedDURING OP 16 MAINT CHECK, FOUND COCKPIT VERTICAL STIFFENER NUMBER 9911503-167 WAS CRACKED IN THE RADIUS APPROXIMATELY 1.5 INCH LONG, APPROX 2 INCHES BELOW TOP OF STIFFENER AT STA 69.5, AFT SIDE OF BULKHEAD ON X=-12 ON RT SIDE. MADE UP DOUBLER AND INSTALLED PESDR TWAA9909601Longeron · crackedDURING OP 16 MAINT CHECK, FOUND A CRACK IN LONGERON 5R, APPROXIMATELY .75 INCH LONG THROUGH RIVET STA 679. REPAIRED PER DRAWING SR09530128.SDR TWAA9909103Spar · corrodedDURING OP 16 MAINT CHECK FOUND THE HORIZONTAL STABILIZER UPPER SPAR CAP BARREL NUT LEFT SIDE AFT HOLE WAS CORRODED. REPAIRED PER ARA 16167.SDR TWAA9909102Spar · corrodedDURING OP 16 MAINT CHECK FOUND THE HORIZONTAL STABILIZER UPPER SPAR CAP BARREL NUT HOLE, RIGHT SIDE AFT, THE HOLE WAS CORRODED. REPAIRED PER ARA 16167.SDR TWAA9907509Spar · corrodedDURING OP 16 MAINT CHECK, FOUND THE HORIZ STABILIZER UPPER SPAR CAP BARREL NUT HOLES, RT SIDE AFT HOLE, AND LT SIDE AFT HOLE, WERE CORRODED. REPAIRED PER ARA 16167.SDR TWAA9805401Cofee Maker · shortedSTL - FLT 531 - NR 2 COFFEE MAKER SHOT FLAMES AND SMOKE. TURNED OFF COFFEE MAKER. REPLACED COFFEE MAKER. CHECK-C 12-3-97 STL. (X)SDR TWAA9613702Downlock Switch · malfunctionedSTL - FLT 631 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, RIGHT MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. CYCLED LANDING GEAR. FOUND RIGHT MAIN LANDING GEAR DOWNLOCK SWITCH, MFG PN H14-6, MALFUNCTIONING. REPLACED RIGHT MAIN LANDING GEAR DOWNL
Back to N979Z, cancelled Oct 19, 2005