JASC 5313
Service difficulty reports · 36,313
Reports filed under 5313 · Fuselage Main, Longeron/Stringer, 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 jasc_code = '5313' 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 jasc_code = '5313' 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 UPS96821305Longeron · crackedINSPECTION TYPE: CS2. LONGERON 24L CRACKED (3 EA) AT BOTTLE BOLT HOLE FS 857. REPLACED LONGERON SECTION PER DAC DRAWINGS NR 5779948 AND 5779938.SDR UPS96821232Longeron · crackedINSPECTION TYPE-CS2, LONGERON 24R AT FS 857, CRACKED AT BOTTLE BOLT HOLE. REPLACED LONGERON PER DRAWING NR 5750198 DAC.SDR 9619289928Longeron · corrodedDURING M-CHECK, FOUND CORROSION ON LONGERON 23L FROM FS 870 TO 937. REPAIRED LONGERON PER EA DC9-53-033.SDR 9619601162Longeron · corrodedDURING T-CHECK, FOUND CORROSION ON THE FUSELAGE OVERWING EXTERNAL LONGERONS 30L, 32L, 37L, AND 32R FROM FS 1407 - FS 1548. REPAIRED LONGERONS PER EA 11-110189.SDR UPS96421126Stringr · crackedINSPECTION TYPE-C, AFT CARGO COMP FOUND CRACK IN STRINGER FLANGE AT S32 LT BS 1650. REMOVED DAMAGED SECTION OF STRINGER FLANGE AND REPAIRED STRINGER FLANGE ACC TO SRM 53-10-03 FIG 2.SDR 96UAL900676Bulkhead Angle · crackedMULTI-SITE CRACKS FOUND AT BODY STATION 178 BULKHEAD CHORD ANGLE AND AT STRINGER 17R TEE COMMON TO THE BULKHEAD ANGLE. THE CRACKS WERE APPROXIMATELY 2 INCHES AND 1 INCH RESPECTIVELY. CRACKS WERE DUE TO FATIGUE. BULKHEAD CHORD ANGLE REPAIRED PER 737 STRUCTURASDR Y2PA960072Longeron · corrodedDURING C AND D BRIDGING AND ALIGNMENT CHECK INSPECTION, FOUND STATION 229 TO 280 LONGERON 28R CORRODED. REMOVED AND REPLACED LONGERON 28R STATION 229 TO 280 IAW DC9 SRM 51-01 AND 51-30-5. NON-ROUTINE WORK CARD NR 96-0196 AND 96-0249. REPORT GENERATED BY AMESDR Y2PA960071Longeron · crackedDURING C AND D BRIDGING AND ALIGNMENT CHECK INSPECTION, FOUND 6 INCH CRACK IN LONGERON 30 STATION 360 TO 366. REMOVED AND REPLACED LONGERON 30 STATION 360 TO 366 IAW DC9 SRM 51-01 AND 51-30-5. NON-ROUTINE WORK CARD NR 96-0196 AND 96-0264. REPORT GENERATED BSDR AALA961292Stringer · corrodedTUL - FOUND CORRODED STRINGER 27R STATION 560-564. CUT OUT CORRODED SECTION OF STRINGER AND INSTALLED STRINGER REPAIR PER SRM 53-10-3 FIG 1. (M)SDR AALA961288Stringer · corrodedTUL - FOUND STRINGER 28L HAS CORROSION, STATION 487. REPAIRED PER SRM 53-10-3 FIG 1. (M)SDR UPS96821174Longeron · corrosionINSPECTION TYPE-CS2, HEAVY CORROSION ON LONGERON 28L FS 1765 OUTBOARD LEG. REPAIRED PER UPS EO.SDR UPS96821173Longeron · corrosionINSPECTION TYPE-CS2, HEAVY CORROSION ON LONGERON 26R, FS 1706. REPAIRED PER UPS EO.SDR UPS96821128Longeron · crackedINSPECTION TYPE CS2, LONGERON 5R CRACKED AT THE VERTICAL STAB FS 1740. REPAIRED PER UPS EO.SDR UPS96221039Stringer · corrodedINSPECTION TYPE-C, AFT CARGO COMPARTMENT CORROSION ON STRINGER 28L AT STA 990. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-3, 51-30-2.SDR CKSA96103Longeron · corrodedDURING C-2 CHECK, INSPECTION FOUND FS 1280 L-35 LT LONGERON HAS SURFACE CORROSION. CORROSION FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0. REPAIRED LONGERON 35 LT IAW DC8 SRM 53-2-2 AND 51-1-21. TREATED AND PRIMED IAW DC8 SRM 51-1-8. TASK NR 80549, CORROSION CARSDR CKSA96094Stringer · corrodedDURING C-2 CHECK, INSPECTION FOUND STRINGER 24R CORRODED BETWEEN FS 310 AND FS 295. REMOVED AND REPLACED STRINGER IAW DC8 SRM 51-1-8, 51-1-21, 51-1-20D, AND 51-1-22. TASK NR 80999, CORROSION CARD NR 5570-0551.SDR CKSA96093Stringer · corrodedDURING C-2 CHECK, INSPECTION FOUND STRINGER 24R CORRODED BETWEEN FS 295 AND FS 275. REMOVED AND REPLACED STRINGER IAW DC8 SRM 51-1-8, 51-1-21, 51-1-20D, 51-1-22 AND 53-2-2 FIGURE 10. TASK NR 81001 CORROSION CARD NR 5570-0551.SDR AALA961268Stringer · corrodedTUL - FOUND CORROSION ON SKIN AND STRINGER. REMOVED FASTENERS, CLEANED SKIN. INSTALLED STRINGER REPAIR PER SRM 53-10-5 FIG 1. (M)SDR 96FDEA01407Stringer · crackedNR 0451 AND 004, WHILE WORKING NR 0219 FOUND STRINGER 19 RT AT BS 640 TO BE CRACKED.SDR W8PA960127Stringer · corrodedCORROSION ON STR 27L, BS 1010, WL 186. REMOVED AND REPLACED STRINGER FROM BS 995 TO BS 1016 PER SRM 53-00-03. (X)SDR UPS96821021Longeron · corrosionINSPECTION TYPE SPEC, LONGERON 32L HAS HEAVY CORROSION AT FS 8 TO 70. REPLACED LONGERON SECTION PER SRM 51-1-21 AND SRM 51-3-0.SDR UPS96821020Longeron · crackedINSPECTION TYPE SPEC, LONGERON 36 CRACKED AT FS 70 TO 60. REPLACED LONGERON SECTION FS 60 TO 70 PER SRM 51-1-21 AND SRM 51-1-20D.SDR UPS96821019Longeron · crackedINSPECTION TYPE SPEC, LONGERON 335R CRACKED AT FS 60 TO 70. REPLACED LONGERON SECTION PER SRM 51-1-20D AND SRM 51-1-21.SDR W8PA960126Stringer · corrodedCORROSION IN STR 26R, BS 1010, WL 186 IN AFT EQUIPMENT. FABRICATED AND INSTALLED STRINGER. (X)SDR UPS96821023Longeron · corrosionINSPECTION TYPE SPEC, HEAVY CORROSION ON LONGERON 33R, FS 8 TO 70. REPLACED LONGERON SECTION PER SRM 51-3-0.SDR SWAA960865Stringer · crackedDURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER 9R CRACKED AT BS 727B. REPAIRED PER BOEING SRM.SDR SWAA960861Stringer · crackedDURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER 10R CRACKED AT BS 727B. REPAIRED PER BOEING SRM.SDR CALA9601289Stringer · corrodedINSPECTION FOUND STRINGER 30 CORRODED BETWEEN STA 1166 AND 1148. A STRINGER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-3-10, FIGURE 1, SHEET 1 TO 4.SDR AALA961261Stringer · corrodedTUL - FOUND CORROSION BETWEEN STRINGER AND FUSELAGE SKIN AT STATION 879 STRINGER 43L, FUSELAGE SKIN HAD CRACKS BETWEEN FASTENERS. STRINGER SPLICED PER SRM 53-10-100 VOL 1. (M)SDR 9618711162Longeron · corrodedDURING T-CHECK, FOUND CORROSION ON LONGERON 52 AT FS 1781. REPAIRED LONGERON (P/N AGA7045) PER EA 11-106299.SDR RRXA96132Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND EXFOLIATION CORROSION DAMAGE TO LONGERON 21R PAST LIMITATIONS IAW DC-8 SRM, AT Y=1640. INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-11, TREATED AREA IAW DC-8 SRM 51-1-8.SDR USAA960564Stringer · corrodedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 7 INCH CORRODED AREA STRINGER 27L, STATION 967. CUT OUT DAMAGE AND INSTALLED STRINGER SPLICE REPAIR. REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)SDR USAA960562Stringer · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH CRACKS IN FASTENER HOLES FOR STRINGER 15R TO STATION 532. CUT OUT DAMAGED AREA AND FABRICATED AND REPLACED DAMAGED SECTION WITH STRINGER. REPAIRED SPLICE REPAIR PER SRM 53-10-3 FIG 1. (M)SDR USAA960559Stringer · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH CRACKS AT FASTENER HOLES STATION 532, STRINGER 15R. REMOVED DAMAGED SECTION OF STRINGER AND PERFORMED STRINGER SPLICE REPAIR. REPAIRED PER SRM 53-10-3. (M)SDR CA960826015Z Member · cracked(CAN) LH VERTICAL Z MEMBER AT STA.X97.0 FOUND CRACKED. HORIZONTAL BEAM AT STA.X97.0 ALSO CRACKED. RH VERTICAL Z MEMBER AT SAME STA. MISSING RIVETS. CRACKS REPAIRED AS PER DEHAVILLAND SUPPLIED DRAWINGS.SDR C2XA96IA212Stringer · corrodedIAH - DURING C-CHECK INSPECTION, STRINGER 18 ON THE RIGHT FUSELAGE WAS FOUND TO BE CORRODED BETWEEN FRAME 38.5 AND FRAME 40. MAINTENANCE REMOVED THE DAMAGED SECTION OF STRINGER AND PERFORMED A SPLICE REPAIR PER EMB SRM 53-00-01, AND THE AIRCRAFT WAS APPROVED SDR C2XA96IA211Stringer · corrodedIAH - DURING C-CHECK INSPECTION, STRINGER 19 ON THE RIGHT FUSELAGE WAS FOUND TO BE CORRODED BETWEEN FRAME 38.5 AND FRAME 40. MAINTENANCE REMOVED THE DAMAGED SECTION OF STRINGER AND PERFORMED A SPLICE REPAIR PER EMB SRM 53-00-01, AND THE AIRCRAFT WAS APPROVED SDR C2XA96IA210Stringer · corrodedIAH - DURING C-CHECK INSPECTION, STRINGER 20 ON THE RIGHT FUSELAGE WAS FOUND TO BE CORRODED FROM FRAME 38.5 TO FRAME 40. MAINTENANCE REMOVED THE DAMAGED SECTION OF STRINGER AND PERFORMED A SPLICE REPAIR PER EMB SRM 53-00-01, AND THE AIRCRAFT WAS APPROVED FOR SDR 96FDEA1395Stringer · corrodedNR0711 AND 031, WHILE WORKING ON NR0698 FOUND CORROSION ON STRINGER 30 BS 964.SDR 96FDEA01395Stringer · corrodedNR0711 AND 031, WHILE WORKING ON NR0698 FOUND CORROSION ON STRINGER 30 BS 964. *S/D* REMOVED CORROSION ON SIR 30 BS 964, OUT OF LIMITS IAW FEDEX SRM 53-10-01. REPAIRED STRINGER IAW FEDEX SRM 53-10-03.SDR UPS96221031Stringer · corrodedINSPECTION TYPE-C, CORROSION (C53-113-01.00-01) BROKEN STAND-OFF FOR CLAMP STA 571, LBL 8, WL 148, STR 27 LEFT. CORROSION OUT OF LIMITS IN A 1 INCH BY 1 INCH AREA, CUTOUT DAMAGED AREA, FABRICATED REPAIR PARTS AND REPAIRED PER SRM 53-10-3.SDR UPS96220979Stringer · corrodedINSPECTION TYPE-C, CORROSION (C53-113-01.00-01) BROKEN STAND-OFF FOR CLAMP STA 571, LBL 8 WL 148, STR 27 LEFT. CORROSION OUT OF LIMITS IN A 1 BY 1 AREA, FABRICATED REPAIR PARTS AND REPAIRED PER SRM 53-10-3.SDR UPS96821012Longeron · corrodedINSPECTION TYPE: C. LONGERON NR 24L FROM STA 1600 - 1640 CORRODED. FABRICATED REPAIR FILLER AND DOUBLER IAW DC8 SRM'S 53-4-1 AND 53-2-1, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR IAW DC8 SRM 51-1-20D. PAINT TO BE ACCOMPLISHED ON UPS N/ 468SDR RRXA96081Longeron · corrodedDURING C-CHECK, FOUND CORROSION ON LONGERON 27R AT GROUND AIR CONDITION CONNECTOR PANEL DOME NUT AT Y=42. REMOVED DOME NUTS, REMOVED CORROSION AND FOUND CORROSION WAS BEYOND LIMITS. REMOVED AND REPLACED LONGERON 27R IAW DC-8 SRM 51-1-20D. INNER DOOR DOUBLESDR 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 96FDEA01380Stringer · corrodedNR0129 AND 025, CORROSION (C53-224-02, -1) ON STR 6L BS 700 TO 680. *S/D* CORROSION ON STR NR 6L BS 700 TO 680 WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REPAIRED STRINGER PER FEDEX SRM 53-10-3 FIG 3.SDR 96FDEA01379Stringer · crackedNR0672 AND 024, WHILE WORKING NR201 FOUND STR TO BE CRACKED AT BS 1082 WL 138 STR 29L.
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