Boeing 747-146
Service difficulty reports · 211
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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 aircraft_model_key = '747146' 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 aircraft_model_key = '747146' 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 CKSA98053Angle · corrodedDURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, FS 2380 LT SIDE FLOORBOARD ATTACH ANGLE HAS AREAS OF CORROSION. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS AS PER B747 SRM 53-10-01. INSTALLED ATTACH ANGLE IAW B747 SRM 51-10-01 AND 51-SDR CKSA98052Stiffener · corrodedDURING CPCP INSPECTION FOUND LEVEL 2 CORROSION. CORROSION RT WING NR 26 L/E FLAP STIFFENER (CTR) OTBD END BOTH SIDES. REMOVED AND REPLACED THE 65B10783-1 HAT SECTION IAW B747 SRM 51-30-02 AND 51-10-1. CORROSION TASK CARD NUMBER C57-510-01 PART 2 OF 4. NON-RSDR CKSA98051Rib · corrodedDURING CPCP INSPECTION FOUND LEVEL 2 CORROSION. CORROSION ON RT WING RIB STA 1010 OVER SLAT CAVITY ON RT SIDE OF RIB AND FWD TOP OF RIB. REMOVED CORROSION IAW SRM 51-10-01. CHECKED RIB THICKNESS FOUND MINIMUM NOMINAL .035 MAX NOMINAL THICKNESS .070 OUT OF LSDR CKSA98050Doubler · corrodedDURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, FS 1480 AFT WEB DOUBLER CORRODED LBL 97. REMOVED CORROSION IAW B747 SRM 51-10-01, FOUND OUT OF LIMIT. REMOVED AND REPLACED WEB DOUBLER IAW B747 SRM 51-10-01 AND 51-30-02. CORROSION TASK CARD NUMBER C53-190-01.SDR CKSA98049Stiffener · corrodedDURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, FS 1480 AFT SIDE WEB LWR STIFFENER AT LBL 97 CORRODED FILLET AREA. REMOVED CORROSION IAW B747 SRM 51-10-01 FOUND OUT OF LIMIT. REMOVED AND REPLACED CORRODED STIFFENER IAW B747 SRM 51-10-01 AND 51-30-02. CORROSSDR CKSA98048Bracket · corrodedDURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, RT WING FWD FILLET RIB FS 840 BETWEEN STRINGER 47R AND 47L MOUNT BRACKETS HAVE CORROSION. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. REMOVED AND REPLACED MOUNT BRSDR CKSA98047Angle · corrodedDURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, LITE SURFACE CORROSION AFT OF NR 2 DME. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. REMOVED AND REPLACED ATTACH ANGLE IAW B747 SRM 51-10-01 AND 51-30-02. CORROSIOSDR CKSA98046Angle · corrodedDURING CPCP INSPECTION FOUND LEVEL 2 CORROSION. CORROSION ON ANGLES AND STRAPS ATTACHED TO TOP OF FRAME AT BS 1920 ABOVE S-41R. CORROSION ON ANGLES - 65B04866-2 AND 65B01856-80 OUT OF LIMITS IAW B747 SRM 53-10-1. REMOVED AND INSTALLED ANGLES IAW B747 SRM 51SDR CKSA98045Skin · corrodedDURING CPCP INSPECTION FOUND LEVEL 2 CORROSION. CORROSION ON INTERNAL SKIN AT UPPER FWD CORNER OF C-2 DOOR CUTOUT BS 1850. REMOVED CORROSION IAW B747 SRM 51-10-1. PERFORMED ULTRASONIC THICKNESS CHECK, MINIMUM NOMINAL THICKNESS .135. CORROSION FOUND TO BE OUSDR CKSA98044Skin · corrodedDURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, LT OVERWING SKIN AT WBL 128.45 HAS A 4 X 4 AREA OF CORROSION 2 FT FWD OF MID SPAR. REMOVED CORROSION IAW B747 SRM 51-10-1. ULTRASONIC THICKNESS CHECK, MINIMUM NOMINAL THICKNESS AT WING SKIN EDGE .195 TO .230 INSDR CKSA98043Skin · corrodedDURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, LT OVERWING SKIN AT WBL 128.45 HAS A 4 X 4 AREA OF CORROSION 2 FT 4 FWD OF MID SPAR. REMOVED CORROSION IAW B747 SRM 51-10-1. ULTRASONIC THICKNESS CHECK, MINIMUM NOMINAL THICKNESS .335 TO .340 IN 2 BY 2.5 AREA ASDR CKSA98042Intercostal · corrodedDURING CPCP INSPECTION FOUND LEVEL 2 CORROSION. CORROSION ON INTERCOSTAL WEB AFT OF BS 1700 AT S-30L. CORROSION OUT OF LIMITS IAW B747 SRM 53-10-1. INSTALLED REPAIR IAW B747 SRM 51-40-2. CORROSION TASK CARD NUMBER C53-110-01 PART 3 OF 5. NON-ROUTINE TASK SDR CKSA98041Support · corrodedDURING CPCP INSPECTION, FOUND CORROSION ON SEAT TRACK AND FLOOR SUPPORT FLANGES FROM BS 1160 TO 1265 RBL 11.33. REMOVED DAMAGED AREA AT BS 1265 RBL 11.33 AND FABRICATED PARTS IAW AIA/E/2732. INSTALLED SEAT TRACK IAW AIA/E/SKETCH 2732. CORROSION TASK CARD NUSDR CKSA98040Seat Track · corrodedDURING CPCP INSPECTION FOUND LEVEL 2 CORROSION. CORROSION ON SEAT TRACK AND FLOOR SUPPORT FLANGES FROM BS 1180 TO 1265 LBL 11.33. REMOVED AND REPLACED SEAT TRACK FS 1180 TO 1265 LBL 11.33 IAW B747 SRM 51-30-02. CORROSION TASK CARD NUMBER C53-210-05 PART 1 OSDR CKSA98039Seat Track · corrodedDURING CPCP INSPECTION FOUND LEVEL 2 CORROSION. CORROSION ON SEAT TRACK BS 1140 TO 1160 LBL 11.33. REMOVED AND REPLACED SEAT TRACK FS 1140 TO 1160 AND LBL 11.33 IAW B747 SRM 51-30-02. CORROSION TASK CARD NUMBER C53-210-05 PART 1 OF 1. NON-ROUTINE TASK CARDSDR CKSA98038Seat Track · corrodedDURING CPCP INSPECTION FOUND LEVEL 2 CORROSION. CORROSION IN SEAT TRACK BS 1020 LBL 11.33. REMOVED AND REPLACED SEAT TRACK BS 1020 LBL 11.33 IAW B747 SRM 51-30-02. CORROSION TASK CARD NUMBER C53-210-05 PART 1 OF 1. NON-ROUTINE TASK CARD NUMBER 12541.SDR CKSA98037Seat Track · crackedDURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, CRACK ON SEAT TRACK VERT FLANGE AT BS 1000 LBL 11.33. VERIFIED END OF CRACK WITH EDDY CURRENT. STOP DRILL END OF CRACK USING NR 10 DRILL BIT. INSTALLED REPAIR PARTS IAW DWG AIA/E/2731. CORROSION TASK CARD NUMSDR CKSA98036Frame · crackedDURING CPCP INSPECTION FOUND LFT SIDEWALL AREA, BS 520, FRAME CRACKED ALONG PREVIOUS DOUBLER REPAIR (REFERENCE: BETWEEN S31L AND S32L AREA). REMOVED PREVIOUS DOUBLER IAW B747 SRM 51-30-02. PERFORMED HFEC ON WEB PER BOEING SRM 53-10-04 END OF CRACK VERIFIED ASDR CKSA98035T-Chord · corrodedDURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, I/B CARRIAGE FWD ACCESS HOLE AFT EDGE CORRODED BETWEEN NUT PLATES AND T-CHORD. REPAIRED CORROSION DAMAGE TO T-CHORD IAW AIA EDR NR B4-05552 DATED 11-21-97. CORROSION TASK CARD NUMBER C57-560-10 PART 1 OF 2. NOSDR CKSA98034Frame · damagedDURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, TOP OF L/E JUST O/B OF O/B CARRIAGE PILLOWING. REMOVED DAMAGED UPPER STRAP (FRAME ASSY) IAW B747 SRM 51-30-02. INSTALLED NEW FRAME ASSY IAW B747 SRM 51-30-02. REPAIR ACCOMPLISHED USING B747 SRM 51-10-1 (REPLACSDR CKSA97586Seal · wornON DESCENT, SMOKE ENTERED CABIN ISOLATED TO NR 1 ENG WHEN HIGH STAGE LIGHT ON. PERFORMED MAINTENANCE CHECKLIST FOR INOPERATIVE ENGINE FERRY FLIGHT AS REQUIRED FOR THREE ENGINE. FERRY. THIS ACFT HAS BEEN INSPECTED AND FOUND SAFE FOR INTENDED THREE ENGINE FERRSDR CKSA97583Support · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: CORROSION STA 1372 LBL10 TO RBL10 FLOOR SUPPORT. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-03. REMOVED AND REPLACED FLOOR SUPPORT IAW B747 SRM 51-10-01 ANDSDR CKSA97582Support · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: CORROSION ON FLOOR SUPPORT STA 1416 LBL 10 TO RBL 10. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-03. REMOVED AND REPLACED FLOOR SUPPORT IAW B747 SRM 51-10-0SDR CKSA97581Seat Track · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: SEAT TRACK FLANGE CORRODED AT SCREW HOLES STA 1301 TO 1372 LBL 10. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND OUT OF LIMITS IAW B747 SRM 53-10-01 FIG 1. REMOVED AND REPLACED SEAT TRACK IAW B747 SSDR CKSA97580Seat Track · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: CORRODED SEAT TRACK FLANGE LBL 30 STA 1301 TO 1372 AT SCREW HOLES. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND OUT OF LIMITS IAW B747 SRM 53-10-01 FIG 1. REMOVED AND REPLACED SEAT TRACK IAW B747 SSDR CKSA97579Support · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: FLOOR SUPPORT BETWEEN SEAT TRACKS LBL 10 AND LBL 30 STA 1301 CORRODED. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-03. REPLACED FLOOR SUPPORT IAW B747 SRM 51SDR CKSA97578Support · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: FLOOR SUPPORT BETWEEN LBL 10 AND RBL 10 STA 1301 CORRODED. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-03. REMOVED AND REPLACED FLOOR SUPPORT IAW B747 SRM 51SDR CKSA97577Support · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: FLOOR SUPPORT BETWEEN LBL 10 AND RBL 10 STA 1321 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW B747 SRM 51-10-01 AND 51-30-02. CORROSION TASK CARD NUMBER C53-210-06. NON-ROUTINE TASK CARD NUMBER 1SDR CKSA97576Support · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: FLOOR SUPPORT BETWEEN LBL 10 AND RBL 10 STA 1331 CORRODED. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND OUT OF LIMITS IAW B747 SRM 53-10-03. REMOVED AND REPLACED FLOOR SUPPORT IAW B747 SRM 51-10-01SDR CKSA97575Support · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: FLOOR SUPPORT BETWEEN LBL 10 AND RBL 10 STA 1341 CORRODED. REMOVED CORROSION IAW B747 SRM 51-10-1. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-03. REMOVED AND REPLACED FLOOR SUPPORT IAW B747 SRM 51-SDR CKSA97574Seat Track · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: SEAT TRACK FLANGES CORROSION AT SCREW HOLES RBL10 STA 1265 TO 1372. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND OUT OF LIMITS IAW B747 SRM 53-10-01 FIG 1. REMOVED AND REPLACED SEAT TRACK IAW B747 SSDR CKSA97573Seat Track · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: SEAT TRACK FLANGES CORRODED AT SCREW HOLES RBL 30 STA 1265 TO 1372. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND OUT OF LIMITS IAW B747 SRM 53-10-01 FIG 1. REMOVED AND REPLACED SEAT TRACK IAW B747 SDR CKSA97261Doubler · corrodedDURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION ALONG EDGE OF LAP SEAM AT STRINGER 34R STA 2280 TO 2350 MARKED J-9. REPAIRED (2024-T3) IAW BOEING 747 SRM 53-30-03 FIGURE 22. PERMANENT REPAIR TO BE INSTALLED AT C-CHECK REFERENCE CARRY OVER NSDR CKSA97260Skin · corrodedDURING CPCP CHECK, INSPECTION FOUND LEVEL 2 CORROSION. STA 2180 TO 2190 SKIN SWOLLEN AROUND FASTENERS IN LAP SEAM AT STRINGER 46L MARKED J-8. REPAIRED (2024-T3) IAW BOEING SRM 53-10-03 AND 53-30-03. CORROSION TASK CARD NUMBER C53-100-01. NON-ROUTINE TASK CSDR CKSA97259Doubler · corrodedDURING CPCP CHECK, INSPECTION FOUND LEVEL 2 CORROSION. FASTENERS BULGING AT FS 2180 STRINGER 44L THROUGH STRINGER 45L. REPAIRED (2024-T3) IAW BOEING SRM 53-10-03 AND 53-30-03. CORROSION TASK CARD NUMBER C53-100-01. NON-ROUTINE TASK CARD NUMBER 103359.SDR CKSA97258Doubler · corrodedDURING CPCP CHECK, INSPECTION FOUND LEVEL 2 CORROSION. EXFOLIATION CORROSION ON EXTERIOR FUSELAGE SKIN AT FS 1960 BETWEEN STRINGER 46L AND STRINGER 47L. REPAIRED (2024-T3) IAW BOEING SRM 53-30-03. CORROSION TASK CARD NUMBER C53-100-01. NON-ROUTINE TASK CARDSDR CKSA97257Doubler · corrodedDURING CPCP CHECK, INSPECTION FOUND LEVEL 2 CORROSION. BS 1319 RIGHT WLG W/W PRESSURE PANEL CORRODED AT OUTBOARD FRAME, MARKED L-14. REMOVED CORROSION IAW SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. TREATED AND PRIMED IAW B747 SRM 51-10-SDR CKSA97072Doubler · crackedDURING WALKAROUND INSPECTION, FOUND CRACK FORWARD LOWER CARGO DOOR EXTERNAL SKIN (MARKED). REPAIRED IAW BOEING SRM 52-00-03 FIGURE 4.SDR CKSA97020Stringer · corrodedDURING WALKAROUND INSPECTION, FOUND LEVEL 2 CORROSION, CORROSION BULGE AND CRACK LOWER BELLY STA 2320 STRINGER NBR 47. CUTOUT CORRODED AND CRACKED AREA AND REPAIRED IAW B747 SRM 53-30-03 FIGURE 1. NON-ROUTINE TASK CARD NR 94085.SDR CKSA97019Angle · corrodedDURING WALKAROUND INSPECTION, FOUND LEVEL 2 CORROSION, APPROXIMATELY STA 1520 FILLET ATTACH ANGLE CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. INSTALLED REPAIR ON FILLET ATTACH ANGLE STA 1520 IAW B747 SRM 53-50-04 FIGURE 2. NON-ROUTINE TASK CARD NSDR CKSA97018Angle · corrodedDURING WALKAROUND INSPECTION, FOUND LEVEL 2 CORROSION, STA 1480 LEFT SIDE LOWER FILLET ATTACH ANGLE CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. INSTALLED REPAIR ON LOWER FILLET ATTACH ANGLE LEFT SIDE, STA 1480 IAW B747 SRM 53-50-04 FIGURE 2. NONSDR CKSA97017Frame · corrodedDURING WALKAROUND INSPECTION, FOUND LEVEL 2 CORROSION, LOWER FUSELAGE FILLET PANEL FRAME CORRODED STA 987 RBL 14 TO RBL 24 UPPER CHORD. REMOVED CORRODED AREA FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-50-04, 51-10-01, 51-30-02, 51-10-02. NON-ROUTINE TASSDR CKSA97016Stringer · corrodedDURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION, AFT OF STA 2200 LOWER RIGHT SIDE AT APPROXIMATELY 36 HAS BULGE. REMOVED AND REPLACED STRINGER SPLICE IAW B747 SRM 51-10-01 AND 51-30-02. CORROSION TASK CARD NR C53-100-01 PART 6 OF 10. NON-ROUTINE TASK CSDR CKSA97015Frame · corrodedDURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION, LOWER FUSELAGE FILLET PANEL FRAME CORRODED, STA 960 LBL 22 TO RBL 9. REMOVED CORROSION, CLEANED AND TREATED AREA AND INSTALLED FRAME FLANGE REPAIR IAW BOEING 747 SRM 53-50-04 FIGURE 1. CORROSION TASK CARSDR CKSA97014Intercostal · corrodedDURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION, LOWER FUSELAGE INTERCOSTAL, STA 955 LBL 6. REMOVED AND REPLACED INTERCOSTAL IAW B747 SRM'S 51-10-01 AND 51-30-02. CORROSION TASK CARD NR C53-100-01 PART 3 OF 10. NON-ROUTINE TASK CARD NR 94130.SDR CKSA97013Panel · corrodedDURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION, FILLET PANEL APPROXIMATELY STA 1460 BETWEEN MAIN LANDING GEAR DOORS, JUST AFT OF APU SHROUD FUEL DUMP HAS CORROSION. REMOVED AND REPLACED PANEL IAW B747 SRM 51-10-1, CLEANED AND TREATED CORROSION IAW B747SDR CKSA96134Skin · corrodedRJAA - DURING C-1 CHECK INSPECTION FOUND: BULGE FUSELAGE BOTTOM SKIN OF BS 1840 THROUGH BS 1845 S51R (AFT CARGO AREA). PERFORMED BLEND AWAY THE DAMAGED EDGE OF STRINGER DOUBLER. PERFORMED REPAIR PER REF TWX JAL-NRT-96-0805 RE 1996-08-29 MNZ/E. JOB CONTROL SDR CKSA96133Skin · corrodedRJAA - DURING C-1 CHECK INSPECTION FOUND: BULGE - FUSELAGE BOTTOM SKIN BS 1857-BS1865 S50L. PERFORMED REPAIR PER REF TWX JAL-NRT-96-0805 RE 1996-08-29 MNZ/E. JOB CONTROL NR J028. WORK PERFORMED BY JAPAN AIRLINES (JACZ109F).SDR CKSA96132Skin · corrodedRJAA - DURING C-1 CHECK INSPECTION FOUND: BULGE - FUSELAGE BOTTOM SKIN AT BS 1855 THROUGH BS 1863 S49R (AFT CARGO LOWER). PERFORMED BLEND OUT SKIN FOR CORROSION AND PERFORMED BLEND OUT STRINGER DOUBLER LOWER FACE PER SRM 53-30-1 P1 AND SRM 51-10-01 PAR 7. PSDR CKSA96131Skin · corrodedRJAA - DURING C-1 CHECK INSPECTION FOUND: BULGE AND CRACK NR 3 NAC STRUT INBOARD SKIRT BEAM SKIN. REPLACED BEAM SKIN PER SRM 51-10-01 PAR 9. JOB CONTROL NR J994. SOURCE CONTROL NR 7TK7273. WORK PERFORMED BY JAPAN AIRLINES (JACZ109F).
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