N969Z, cancelled May 5, 2007
Service difficulty reports · 20
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 = 'N969Z' AND deregistration_id = 'N969Z-2007-05-05' 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 = 'N969Z' AND deregistration_id = 'N969Z-2007-05-05' 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 TWAA9908707Longeron · crackedACCOMPLISHING MC8-AD-AM FOUND THE RT LONGERON FLANGE ON LONGERON 1 CRACKED ONE INCH AT BELT RING STA 642. SPLICED IN NEW LONGERON SECTION PER SRM 53-02, FIG 18. CHECK-C 4-12-99 STL.SDR TWAA9906201Splice · crackedDURING CHECK-C MAINT, FOUND LONGERON 28L SPLICE AT STA 370, CRACKED AND CORRODED. CRACK .75 IN LONG. INSTALLED REPAIR PER SRM 53-02, FIG 18.SDR TWAA9814702Power Supply · inoperativeFLOOR EGRESS LIGHTS REPORTED INOP ROWS 12 TO 16. REPLACED POWER SUPPLY. CHECK-C 11-22-97 STL.SDR TWAA9814318Intercostal · corrodedINTERCOASTAL 28R RBL 14 IN AT STA 120 TO 130, REMOVED FOR CORROSION AND CRACK. MADE 9911549-2 FROM 7075-0 AND HEAT TREATED TO T6 CONDITION AND INSTALLED WITH HI-LOKS AND RIVETS. CHECK-C 11-22-97 STL.SDR TWAA9814317Jamb · corrodedDOOR JAMB STRUCTURE REMOVED AT ELECTRONIC COMPT DOOR FOR CORROSION DAMAGE STA 134 TO 160, LONGERON 28L TO 28R WITH ATTACH STRUCTURE. ACCOMPLISHED ARA 9240 REV A. INSTALLED DOOR JAMB STRUCTURE PER DWG 5910343. CHECK-C 11-22-97 STL.SDR TWAA9814316Angle · corrodedFORMER FOOT ANGLE LONGERON 26R TO 27R STA 160 REMOVED FOR CORROSION. REMOVED AND REPLACED FORMER FOOT REF DOUGLAS DWG 9911515. CHECK-C 11-22-97 STL.SDR TWAA9814315Angle · corrodedFORMER FOOT ANGLE LONGERON 26L TO 27L REMOVED FOR CORROSION. REMOVED AND REPLACED FORMER FOOT REF DOUGLAS DWG 9911515. CHECK-C 11-22-97 STL.SDR TWAA9814314Angle · corrodedCHORD ANGLE REMOVED FOR CORROSION DAMAGE STA 110 TO 129, LBL 14 IN. INSTALLED NEW CHORD ANGLE REF DOUGLAS DWG 5911401. CHECK-C 11-22-97 STL.SDR TWAA9814313Former · corrodedFORMER RING REMOVED STA 134, LONGERON 24L TO L24R DUE TO CORROSION DAMAGE. INSTALLED NEW FORMER RING REF DOUGLAS DWG 9911512 AND ARA 9240. CHECK-C 11-22-97 STL.SDR TWAA9814312Skin · corrodedSTA 110 TO 174 BELLY SKIN REMOVED FOR CORROSION DAMAGE FROM LONGERON 26L TO 26R. REMOVED AND REPLACED SKIN PER ARA 9240. CHECK-C 11-22-97 STL.SDR TWAA9814311Skin · corrodedDURING ROUTINE MAINT, FOUND CORROSION ON ELECTRONIC COMPT DOOR DOUBLER AND EXTERIOR SKIN AROUND DOOR. REMOVED AND REPLACED SKIN AND DOUBLER PER ARA 9240. CHECK-C 11-22-97 STL.SDR TWAA9813419Longeron · corrodedINTERCOASTAL LONGERON 28L STA 130 TO 160 HAD CORROSION DAMAGE. INSTALLED INTERCOASTAL PER DWG 5910343. COMPLIED WITH ARA 9240 REV A. CHECK-C 11-22-98 STL.SDR TWAA9713501Angle · crackedSTL - REPAIRED ONE QUARTER INCH CRACK IN VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE LEFT SIDE AT STATION 910. (M)SDR 96ZZZX4911Longeron · crackedSTL - DURING O-15, FOUND A .25 INCH CRACK IN LONGERON 13R, STA 768. REPAIRED PER SRM 53-02, FIGURE 2. AIRCRAFT TOTAL TIME: 63,463 HOURS; 76,506 CYCLES.SDR 96ZZZX4910Longeron · crackedSTL - DURING OP-15, FOUND A .25 INCH CRACK IN LONGERON 26L, STA 313. REPAIRED PER SRM 53-02, FIGURE 4. AIRCRAFT TOTAL TIME: 63,463 HOURS; 76,506 CYCLES.SDR 96ZZZX4901Longeron · crackedSTL - DURING OP-15, FOUND A .25 INCH CRACK IN LONGERON 27L AND .50 INCH CRACK IN OUTBOARD HAT SECTION, STA 313. REPAIRED PER SRM 53-02, FIGURE 2. AIRCRAFT TOTAL TIME: 64,463 HOURS; 76,506 CYCLES.SDR 96ZZZX4899Longeron · crackedSTL - DURING OP-15, FOUND .50 INCH CRACK IN LONGERON 28L, STA 313. REPAIRED PER SRM 53-02, FIGURE 2. AIRCRAFT TOTAL TIME: 63,463 HOURS; 76,506 CYCLES.SDR 96ZZZM1335Longeron · crackedSTL - DURING OP-15, FOUND .5 INCH CRACK IN RIGHT FLANGE, LONGERON 1, STATION 566. INSTALLED LONGERON REPAIR SPLICE PER SRM 53-02, FIGURE 4. (M)SDR 96ZZZM189Skin · crackedSTL - DURING SPECIAL CHECK, FOUND ONE AND TWO INCH CRACKS IN FUSELAGE SKIN BETWEEN RIVETS AT STATION 817, LONGERON R9, AND A 1 INCH FUSELAGE SKIN CRACK AT STATION 817, LONGERONS R7-R8. REPAIRED PER SERVICE BULLETIN A53-147, AND DRAWING J060143. (M)SDR 95ZZZW739Longeron · crackedDURING SPECIAL CHECK, FOUND A TWO INCH CRACK IN LONGERON 19L, STATION 218. REPAIRED PER SRM 53-02.
Back to N969Z, cancelled May 5, 2007