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 DLL17954191Longeron · crackedTHE OUTER CAP ANGLE OF THE LT UPPER LONGERON IN THE FUSELAGE AFTER BODY AT STA 1860 WAS FOUND CRACKED IN THE RADIUS. REPAIRED PER DL ERA 271830-14.SDR UPS804631Longeron · corrosionWHILE IN FOR D-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 34L STA 420. INSTALLED REPLACEMENT LONGERON PER SRM 51-1-21 AND 51-1-20D.SDR UPS804610Longeron · crackedWHILE AT DALFORT FOR C-CHECK, MAINTENANCE FOUND LONGERON 36, LT AND RT SIDES CRACKED AT FS 220 TO 320. REPLACED LONGERON SECTION PER SRM 51-1-20D.SDR 95ZZZX6321Stringer · crackedFUSELAGE STRINGER CRACKED AT STA 500, STR 19L. DETECTED DURING ROUTINE C-CHECK INSPECTION. SUSPECT CAUSE BY STRESS LOADS FROM BAGGAGE LOADING. ROUTINE MAINTENANCE INSPECTIONS SHOULD DETECT ANY FURTHER DAMAGE. CONTROL NR 9519RI625.SDR 95FDEA01472Stringer · corrodedCORROSION ON STR 3 PLACES, BS 525, 528 AND 530 LBL 15 WL 150. MECHANICALLY REMOVED CORROSION ON STR 27 BS 525 TO 530 LBL 15 WL 150, FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1 AND 53-10-0. REPAIRED STR 7 AT BS 525 TO 530 LBL 15 WL 150 PER FEDEX SRM 53-1SDR MWEA95334Longeron · corrodedDURING INSPECTION, LONGERON 30 AT STA 661 WAS FOUND CORRODED BEYOND LIMITS UNDER FLANGE AT FRAME ATTACH POINT. MAINTENANCE REMOVED AND REPLACED LONGERON IAW SRM 53-01 PG 1, RETURNED A/C TO SERVICE.SDR 95ZZZX6427Longeron · crackedDURING ROUTINE MAINTENANCE, A AND P MECHANIC FOUND UPPER RT FUSELAGE LONGERON CRACKED COMPLETELY THROUGH. AIRFRAME AT 726 HOURS SINCE NEW. THIS WAS BROUGHT TO THE ATTENTION OF ASI. SAFETY RECOMMENDATION WAS SENT TO AAI-200 ON 10-27-5.SDR USAA951050Stringer · corrosionROA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 12 INCHES, STRINGER 27L AT BSL 967. INSTALLED STRINGER SPLICE PER SRM 53-10-3. REPAIRED PER SRM 53-10-3, FIG 1. (M)SDR UPS204602Stringer · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01-68-01), ON AND AROUND FASTENERS ON STRINGER 4R STA 618 TO 624. REPAIRED STRINGER PER SRM 53-10-1, 53-10-3, 51-10-2, 53-10-4, 51-30-2 AND MM 51-20-151.SDR UPS204586Stringer · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.00-01), STR 4L STA 323, 344 TO 348. REPAIR WAS MADE.SDR DL72L953930Stringer · damagedDURING CV-2 CHECK, STA 990 FRAME WAS CUT TO FACILITATE MTC OF STRINGER 29L REF NR 95. REPAIRED PER M/M 53-12-0 PG 806 AND 807 FIG 805.SDR 9515979855Longeron · corrodedDURING H-CHECK, FOUND CORROSION ON LONGERON 30 AT FS 873. REPAIRED LONGERON (P/N 5924878-503), PER EA 98-102581.SDR UPS204573Stringer · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 3 LT STA 1130 - 1180. REPAIRED STRINGER PER SRM 53-10-3.SDR UPS204572Stringer · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AND BARE METAL ON STRINGER 6 LT, STA 990 - 1050. REMOVED DAMAGED SECTION OF STRINGER AND SPLICED IN A NEW SECTION IAW SRM 53-10-3 BETWEEN BS 990 - 1050.SDR UPS204571Stringer · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AND BARE METAL ON STRINGER 5 LT STA 990 - 1050. CUT OUT DAMAGED SECTION OF STRINGER BETWEEN BS 990 - 1050 AND SPLICED IN A NEW SECTION IAW SRM 53-10-3.SDR UPS204570Stringer · corrosionWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AND BARE METAL ON STRINGER 4 LT STA 990 - 1050. CUT OUT DAMAGED SECTION OF STRINGER BETWEEN BS 990 - 1050 AND SPLICED IN NEW SECTION IAW SRM 53-10-3.SDR UPS204563Stringer · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON STR 6R FROM ST 680 - 700. CUT OUT DAMAGED SECTION OF STRINGER AND SPLICED IN NEW SECTION IAW 727 SRM 53-10-3.SDR UPS204551Stringer · corrosionWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-0.1-08-01) ON STR 6L STA 660-680. REPAIRED IAW SRM 53-10-3, 51-10-2, 51-10-3.SDR UPS204545Stringer · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.00-03) ON STRINGER 1 STA 1110-1130. CORROSION MECHANICALLY REMOVED IAW SRM 51-10-6. REPAIRED STR 1 STA 1110-1130 IAW SRM 53-10-3.SDR UPS204535Stringer · corrosionWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON NR 1 STRINGER (LOWER) RWS 226-230, LOCATED ON TOP SIDE OF BOTTOM HORIZONTAL LEG OUT OF LIMITS. REMOVED AND REPLACED STRINGER PER E.O. 757-57-1641. UPON REMOVAL OF STRINGER, FOUND DAMGED SHEAR TIE AND ANGLESDR 95FDEA01462Stringer · damagedFASTENERS PULLED THROUGH SIDE OF STR 24R STA 460 TO 484. REMOVED FASTENERS AND REPAIRED STR PER SRM 51-10-3.SDR 9515913209Longeron · corrodedDURING IL CHECK, FOUND CORROSION ON STR 43R BETWEEN FRAMES 32 TO 35. REPAIRED STRINGER (P/N D532-31511-200), PER EA 32-99209.SDR 9515903209Longeron · corrodedDURING IL CHECK, FOUND CORROSION ON STR 42R BETWEEN FRAMES 33 TO 34. REPAIRED STRINGER (P/N D532-31523-200), PER EA 32-99207.SDR 9515893209Longeron · corrodedDURING IL CHECK, FOUND CORROSION ON STR 41R BETWEEN FRAMES 30 TO 31. REPAIRED STRINGER (P/N D532-31542-200, D532-31543-200), PER EA 32-99208.SDR 95ZZZX6814Fitting · rustedPIPER SB 962 DATED 9-29-93, DOES NOT COVER RE-INSPECTION OF AREA AFFECTED SOON ENOUGH. RUST CANNOT BE SEEN UNDER FITTINGS AND BETWEEN AIRCRAFT SKIN. DISSIMILAR CORROSION SETS UP CAUSING ADDITIONAL DAMAGE. SUBMITTER RECOMMENDS COMPLETE REMOVAL OF FITTINGS, ASDR 96ZZZX1861Longeron · corrodedDURING C- AND D-CHECK, FOUND LONGERON 24L AT STA 996, AFT SIDE OF PRESSURE BULKHEAD IS CORRODED. REPAIRED IAW DC9 SRM CH 53. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610.SDR 9515852290Longeron · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON STR 29L BETWEEN BS 950A TO 1000. REPAIRED STRINGER (P/N 65-56441-3), PER EA 22-99254.SDR USAA951075Longeron · crackedPIT - DURING C-1 CHECK INSPECTION, FOUND .75 INCH CRACK AT STATION 680, LONGERON 6L. REMOVED DAMAGED SECTION OF LONGERON AND SPLICED IN A NEW SECTION PER SRM 53-02. (M)SDR ABXA9500925Longeron · corrodedDURING 826AX MOD, FOUND LONGERON L27L CORRODED AT FS 1080 IN THE AFT CARGO PIT. REPAIRED LONGERON L27L AT FS 1080 IAW ABX REA D853-12471MR.SDR AWXA9500659Stringer · corrodedPHX - DURING SCHEDULED C13 INSPECTION, FOUND CORROSION BEYOND LIMITS ON STRINGER 28L BS 910 IN AFT CARGO PIT. FABRICATED AND INSTALLED NEW STRINGER PER SRM 53-10-3 FIGURE 1. (M)SDR AWXA9500654Stringer · corrodedPHX - DURING SCHEDULED C13 INSPECTION, FOUND STRINGER 28L AT BS 910 CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED STRINGER PER SRM 53-10-3. (M)SDR AWXA9500653Stringer · crackedPHX - DURING SCHEDULED C13 INSPECTION, FOUND CRACK IN FUSELAGE FRAME AT BS 360 BETWEEN STRINGER 20L AND STRINGER 21L. STOP DRILLED CRACK AND REPAIRED PER EO 53-11-04. (M)SDR ABXA9600176L0ngeron · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 20 CORRODED AT THE LEFT TRAPEZOIDAL PANEL JUST FORWARD OF FS 737. REPLACED LONGERON 20L IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5.SDR USAA951002Stringer · corrodedROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 1 INCH CORRODED AREA STRINGER 27L BETWEEN STATION 986-1016. SPLICED NEW STRINGER, REPAIRED PER SRM 53-10-3. (M)SDR UPS204489Stringers · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION IN VARIOUS SPOTS ON STRINGER 5, 6, 7, 8 AT STATION 277 - 294, LBL 29 - 47 AND WL 268 - 287. MAINTENANCE REPLACED STRINGERS 7 AND 8L ON UPS EO 5310-1259F, STRINGERS 5 AND 6L WERE REMOVED AND REPLACED IAW SRM.SDR UPS204485Stringer · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK IN STRINGER 16 AT STATION 294.5, LBL 59 AND WL 217. MAINTENANCE REMOVED AND REPLACED PART OF THE STRINGER IAW UPS EO B727-5310-1259F.SDR UPS204474Stringer · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AND BARE METAL ON STRINGER 5L AND STATION 1130 - 1180. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED PER SRM 53-10-3, 53-10-2, 51-30-3, 51-10-2 AND 51-10-6.SDR UPS204473Stringer · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AND BARE METAL ON STRINGER 4R AT STATION 1110 - 1180. MAINTENANCE REMOVED THE DAMAGED AREA, FABRICATED AND INSTALLED IAW SRM 53-10-1, 53-10-2, 51-10-6, 53-10-3, 51-30-2.SDR UPS204472Stringer · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 7L STATION 1110 - 1176. MAINTENANCE REMOVED THE DAMAGED AREA, FABRICATED REPAIR PARTS, AND INSTALLED IAW SRM 53-10-3 AND SRM 51-30-2.SDR 95FDEA01490Stringer · crackedMAIN CARGO INTERIOR STRUCTURE. STR 16R CRACKED IN OUTER FLANGE, AFT OF STA 720B FRAME, FWD OF ICE LIGHT HOUSING. STOP DRILLED CRACK, INSTALLED REPAIR DOUBLER PER SRM 53-10-3 FIG 2.SDR SWAA950636Stringer · crackedDURING SCHEDULED D-CHECK, FOUND STRINGERS CRACKED AT BS 747, BS 767 S9R AND AT BS 639 S3L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR 95FDEA01394Stringer · crackedNR 0398 (PATTERN CARD 72C235-02) CRACK IN STR 15L AT FASTENER. FORWARD SIDE OF ICE LIGHT BETWEEN FUSELAGE STA 720B - 720C. STOP DRILLED CRACK. INSTALLED REPAIR DOUBLER PER SRM 53-10-3, FIG 2.SDR USAA951134Stringer · corrosionCLT - DURING A PCI INSPECTION, A 10 INCH BY 1 INCH CORROSION WAS FOUND AT STRINGER 28R, RBL 6 BETWEEN BS 350 AND 360. REPLACED END STRINGER 28R, RBL 6. (M)SDR USAA951089Stringer · corrodedCLT - DURING A PCI INSPECTION, FOUND CORROSION 10 INCHES BY 1 INCH ON STRINGER 28R, RBL 6 BETWEEN BS 350 AND 360. CORROSION TASK NR C53-202-02/PCI 1227, CORROSION LEVEL 2. REPLACED END STRINGER 28R, RBL 6. (M)SDR USAA951083Longeron · crackedPIT - DURING Q-1 CHECK INSPECTION, FOUND .5 INCH CRACK IN END OF LONGERON 2L STATION 1401. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 5 AND USAIR EA NR 28221. (M)SDR USAA951079Longeron · holePIT - DURING Q-1 CHECK INSPECTION, FOUND .5 INCH BY 1 INCH HOLE TAIL COMPARTMENT STATION 1418, LONGERON 8R. SPLICED IN NEW SECTION OF LONGERON. (M)SDR USAA951077Longeron · corrodedPIT - DURING Q-1 CHECK INSPECTION, FOUND LEVEL 1 CORROSION ON LONGERON 28L, AT STATION 1330, CORROSION REF C57-53300. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02. (M)SDR ABXA9500773Longeron · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION ON LONGERON 30, STA 794. REPAIRED IAW ABX REA D953-12820-MR.SDR 95FDEA01379Stringer · corrosionCORROSION ON STR 27L AT VARIOUS LOCATIONS FROM BS 680 TO 740 WL 145. REMOVED CORROSION ON STR 27L FROM BS 680 TO 740 AND FOUND OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED STR 27L FROM BS 680 TO 740 AND INSTALLED NEW STR 27L FROM 680 TO 740.SDR CAL950845Longeron · corrodedHOU - INSPECTION FOUND CORROSION ON LONGERON 30 IN AFT BAGGAGE BIN FROM STATION 935 TO 990. THE CORRODED SECTION OF LONGERON WAS CUT OUT AND A NEW SECTION WAS SPLICED IN PER SRM 53-02, FIG 16. (M)
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