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 UPS97821962Longeron · crackedINSPECTION TYPE-C, FS 1691, LONG 30R IS CRACKED. REMOVED AND REPLACED STR 30R FROM STA 1690 TO 1766 IAW SRM 53-2-2 FIG 10 AND SRM 51-3-0.SDR UPS97821961Longeron · corrodedINSPECTION TYPE-C, FS 1765, LONG 34R IS CORRODED. REMOVED AND REPLACED STRINGER 34R FROM STA 1690 TO 1766 IAW SRM 53-2-2 FIG 10 AND SRM 51-1-21.SDR UPS97222105Stringer · corrodedINSPECTION SI-CHECK, CORROSION ON STRINGER 2R BS 620-740. REMOVED CORROSION PER SRM 53-10-1. REPAIRED STRINGER PER SRM 53-10-3 FIG 2 AND EWO 97-2051 AT BS 700-720.SDR UPS97222096Stringer · corrodedINSPECTION SI-CHECK, CORROSION ON STRINGER 56 620-680. REMOVED CORROSION FROM 620 TO 630 OUT OF LIMITS. REPAIRED PER ENG FILE NR 727-53-1853, 631 TO 680 WAS WITHIN LIMITS IAW SRM 53-10-1.SDR DL73K970120Stringer · crackedTHE LT KEEL CHORD STR 27L WAS FOUND CORRODED AND CRACKED AT STA 727A. THE DAMAGE IS SEVERE ENOUGH THAT THE CHORD WILL HAVE TO BE REPLACED. THIS WILL REQUIRE 5 FRAMES, STA 727B THROUGH STA 807 TO BE CUT TO ALLOW REPLACEMENT OF THE CHORD.SDR CALA9700208Longeron · crackedINSPECTION FOUND A .25 INCH CRACK IN LONGERON 17L AT STA 237. A NEW LONGERON SECTION AND SPLICE SECTION WERE INSTALLED IAW SRM 53-02, FIGURE 2.SDR CALA9700205Longeron · crackedINSPECTION FOUND A 1 INCH CRACK IN AFT CARGO LONGERON 30 AT FORWARD BULKHEAD STA 756. REPAIRED IAW SRM 53-02, FIGURE 12.SDR CALA9700196Longeron · corrodedINSPECTION FOUND LONGERON 28L CORRODED BETWEEN STA 230 TO 235. A NEW LONGERON SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 2.SDR CALA9700191Longeron · crackedINSPECTION FOUND A 1 INCH CRACK IN LONGERON 17R AT STA 960. A NEW LONGERON SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 2.SDR CALA9700190Longeron · crackedINSPECTION FOUND A .5 INCH CRACK IN LONGERON 17R AT STA 256. REPAIR SPLICES WERE INSTALLED IAW SRM 53-02, FIGURE 2.SDR AALA970179Stringer · corrodedTUL - CORROSION INSIDE STR 26R, FS 680 TO FS 690. CUT OUT DAMAGED SECTION OF STRINGER REPAIR AT STR 26R STA 680 - STA 690 PER SRM 53-10-3. TST: 54,657 HOURS. CYCLES, 33,951 (X)SDR 9701179977Longeron · crackedDURING PERIODIC CHECK, FOUND LONGERON 30 SPLICE JOINT AT FS 551 CRACKED AT BOTH ENDS. REMOVED AND REPLACED SPLICE PER EA 99-112011.SDR UPS97222277Stringer · corrodedINSPECTION TYPE-SI, CORROSION ON STR 5L STA 360-400. REMOVED CORROSION PER SRM 53-10-1, REPAIRED STR PER SRM 53-10-3 FIG 2.SDR UPS97221982Stringer · crackedINSPECTION TYPE: SI CRACK IN STRINGER 9R AT FRAME 400 MARKED. REMOVED FASTENERS, STOP DRILLED CRACK AND VERIFIED CONTAINMENT, FABRICATED AND INSTALLED PARTS IAW SRM 53-10-2, MM 51-20-21, 53-10-3.SDR UPS97221981Stringer · corrodedINSPECTION TYPE: SI CORROSION ON STRINGER 8 RBL 380-460. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS, IAW SRM 53-10-1, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-10-3, 51-30-2, 53-10-4.SDR UPS97221957Stringer · crackedINSPECTION TYPE-SI, CRACK IN STRINGER 16 RT AT FRAME STA 480 AND 500 ON UPPER FLANGE, MARKED. STOP DRILL CRACK, CONTAINMENT VERIFIED BY NDI, FABRICATED REPIAR PARTS IAW SRM 53-10-3, INSTALLED REPAIR PARTS IAW SRM 53-10-3, SRM 51-20-1.SDR DHL9780324CStringer · corrodedAT C-CHECK, NR 2 LOWER CARGO COMPT BS 460 STR 31L HAS EXFOLIATING CORROSION. REMOVED CORRODED FITTING, FABRICATED NEW SPLICE FITTING PER EO 97-53-0116, INSTALLED NEW SPLICE PER THE EO AND SRM 51-1-20.SDR C2XA97IA028Stringer · corrodedIAH - DURING C-CHECK INSPECTION, STRINGER 15R WAS FOUND TO BE CORRODED AT FRAME 40. MAINTENANCE PERFORMED A STRINGER SPLICE REPAIR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR UPS97821933Longeron · corrodedINSPECTION TYPE-C, LONGERON 36 CORRODED AT STA 1690. REMOVED CORRODED SECTION OF LONGERON 36 FROM STA 1690 TO STA 1730 PER SRM 53-2-2. FABRICATED AND REPLACED LONGERON PER SRM 53-2-2 AND 51-3-0.SDR TWAA9710009Stringer · corrodedMCI - DURING OP-16, FOUND CORROSION ON FORMER FRAME 27L, FS 1307, STRINGER 20-22R. REPLACED FORMER FRAME PER SRM 51-01, PAGE 1. (M)SDR 9700859977Longeron · crackedDURING PERIODIC CHECK, FOUND LONGERON 30 SPLICE CRACKED AT FS 551. REPAIRED SPLICE PER EA 99-112011.SDR USAA970015Stringer · corrosionROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCHES OF STRINGER 27L CORRODED AT STATION 947.5. INSTALLED STRINGER REPAIR PER SRM 53-10-3.(M)SDR USAA970014Stringer · corrosionROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 22 INCH OF STRINGER 27 L CORRODED AT STATION 966. INSTALLED STRINGER REPAIR PER SRM 53-10-3. (M)SDR USAA970013Stringer · corrosionROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 16 INCHES OF STRINGER 27L CORRODED AT STATION 986.5. INSTALLED STRINGER REPAIR PER SRM 53-10-3. (M)SDR AALA970166Stringer · corrodedAFW - FOUND CORRODED STRINGER. REPAIRED STRINGER IAW SRM 53-10-3. (M)SDR AALA970108Stringer · crackedTUL - TWO CRACKS IN STRINGER END AT WING LIGHT, FORWARD SIDE. CUT OFF APPROX 12 INCHES OF STRINGER AND INSTALLED NEW PIECE WITH REPAIR CHANNELS PER SRM 53-103 FIG 1. (M)SDR AALA970089Longeron · corrodedTUL - CORROSION ON LONGERON 43L, STATION 824. REPLACED SECTION OF LONGERON PER SRM 53-10-00. (M)SDR UPS97222164Stringer · corrodedINSPECTION TYPE-C, STR 20R AT STA 304 TO 312 EXFOLIATED CORROSION OUT OF LIMITS. CUT OUT DAMAGED STR STA 304 TO 312, FABRICATED AND INSTALLED STRINGER REPAIR PER SRM 53-10-3, 51-30-2.SDR AALA970167Stringer · corrodedAFW - FOUND STRINGER CORRODED. REPAIRED PER SRM 53-10-3. (M)SDR AALA970071Stringer · corrodedTUL - FOUND STRINGER 22L AND END FITTING CORRODED FROM STATION 1178 TO 1183. REPLACED STRINGER 22L AFT END FITTING AT STATION 1183 AND SPLICED STRINGER PER SRM 53-10-3 AND CUT OUT SECTION OF SKIN AND INSTALLED FILLER AND DOUBLER PER SRM 53-30-3. (M)SDR ZIAA979001Longeron · corrodedDURING C-CHECK, FOUND CORROSION IN FORWARD PIT AROUND LONGERON TO FRAME ATTACH BOLTS, LONGERON 28 LEFT TO 29 RIGHT F/S 500 AND FUSE SKIN TO LONGERON ATTACH RIVETS LONG 29 RIGHT F/S 500. ALSO, LONGERON 30 RIGHT HAD A 5 INCH CRACK AT FS 510. REMOVED CORROSION SDR VJ970045Longeron · corrodedDURING C-CHECK, FOUND CORROSION IN FORWARD PIT AROUND LONGERON TO FRAME ATTACH BOLTS, LONGERON 28 LT TO 29 RT, FS 500 AND FUSELAGE SKIN TO LONGERON ATTACH RIVETS LONGERON 29 RT FS 500, ALSO LONGERON 30 RT HAD A 5 INCH CRACK AT FS 510. REMOVED CORROSION AND TRSDR USAA970011Stringer · corrosionROA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH CORROSION STRINGER 27L, BS 965 TO 969. REMOVED CORROSION AND INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3. (M)SDR 97ZZZX883Longeron · crackedDURING C-CHECK, FOUND CORROSION IN FORWARD PIT AROUND LONGERON TO FRAME ATTACH BOLTS, LONGERON 28 LT TO 29 RT, FS 500 AND FUSELAGE SKIN TO LONGERON ATTACH RIVETS LONGERON 29 RT FS 500, ALSO LONGERON 30 RT HAD A 5 INCH CRACK AT FS 510. REMOVED CORROSION AND TRSDR 97ZZZM235Longeron · crackedDURING C-CHECK, FOUND CORROSION IN FORWARD PIT AROUND LONGERON TO FRAME ATTACH BOLTS, LONGERON 28 LEFT TO 29 RIGHT F/S 500 AND FUSE SKIN TO LONGERON ATTACH RIVETS LONG 29 RIGHT F/S 500. ALSO, LONGERON 30 RIGHT HAD A 5 INCH CRACK AT FS 510. REMOVED CORROSION SDR USAA970006Stringer · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 56 INCH CORRODED AREA AT STRINGER 27L, BS 939 - BS 995. SPLICED IN NEW SECTION OF STRINGER, REPAIRED PER EA 41963. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M)SDR USAA970002Stringer · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 12 INCH STATION 902 TO STATION 914, STRINGER 26L. INSTALLED REPAIR SPLICE, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C 53-107-02, CORROSION LEVEL 2. (M)SDR 97FDEA00030Stringer · corrosionNR 0595 002 CORROSION (C53-224-01) ON STRINGER 4 RT BS 460 TO 360. *S/D* REMOVED DAMAGED STR 4 RT, BS 410 TO 450. FABRICATED NEW PARTS AND INSTALLED PER FED-EX 727 SRM 53-10-3.SDR SWAA970036Stringer · crackedDURING SCHEDULED D-CHECK, FOUND STRINGER 21L ON I/B FLANGE AT BS 974, AT BS 500D TO 520, S25L, AND AT BS 380, S22L CRACKED. REPAIRED PER BOEING SRM.SDR ABXA9700729Longeron · crackedDURING C-CHECK, FOUND LONGERON 17L CRACKED AT FRAME STA 980 REPAIR DOUBLER, (AD 92-22-08). REPLACED SECTION OF LONGERON 17 LEFT BETWEEN FS 955 AND FS 996 IAW DC-9 SRM CHAPTER 53-02, FIGURE 2.SDR 97FDEA00070Stringer · corrodedNR 0353 020. CORROSION (C53-224-01) ON STRINGER 2 RT BS 560-BS 520. REMOVED CORRODED STRINGER 2 RT FROM BS 510-570 AND FABRICATED AND INSTALLED REPAIR PARTS ON AIRCRAFT PER FED-EX SRM 53-10-3.SDR VJ970117Stringer · corrosionCORROSION WAS FOUND IN THE RIGHT WING INTERNAL, AROUND THE BARREL NUT HOLE AND UPPER CHORD ON THE STRINGER 16, STATION 58-63. MECHANICALLY REMOVED CORROSION IAW DC-9 SRM 51-10-3. TREATED AND PRIMED AREAS IAW DC-9 SRM 51-22-1. ALL AREAS WITHIN LIMITS IAW EO SDR VJ970041Longeron · crackedFORWARD PIT WAS CRACKED AT STATION 580 LONGERON 29L, ON THE LONGERON. REMOVED FASTENERS, REMOVED CRACK LONGERON, DRILLED NEW LONGERON AND SPLICE, TREATED AND INSTALLED IAW DC-9 SRM 53-02 FIG 14, 51-30-2, 51-30-5. (M)SDR SWAA970007Stringer · crackedDURING SCHEDULED D-CHECK, FOUND STRINGER 16L CRACKED AT BS 500A PLUS 16.5. REPAIRED PER BOEING SRM.SDR AALA970661Stringer · corrodedAFW - FOUND STRINGER 29L BETWEEN STATION 950E AND 950F HAD CORROSION BLENDED BEYOND SRM LIMITS. INSTALLED A REPAIR STRAP PER MRB 727-0015. (M)SDR AALA970197Stringer · corrodedTUL - CORROSION IN AND ON STRINGER 27R FROM STATION 620 TO STATION 630. REMOVED CORROSION, REPAIRED FUSE STRINGER PER SRM 53-10-3 FIG 1. (M)SDR AALA970183Stringer · corrodedTUL - STR 28L BETWEEN STA 580 - STA 600 HAS CORROSION ON OUTBOARD LEG. REMOVED CORROSION. REPAIRED PER SRM 53-10-3, FIGURE 2. TST: 54,657 HOURS. CYCLES, 33,951. (X)SDR AALA970056Stringer · corrodedTUL - CORROSION ON STRINGER 52 AT STATION 879. CUT OUT CORROSION AND SPLICED IN NEW SECTION OF STRINGER PER SRM 51-10-00 VOL 1. (M)SDR 97ZZZM155Longeron · crackedFORWARD PIT WAS CRACKED AT STATION 580 LONGERON 29L, ON THE LONGERON. REMOVED FASTENERS, REMOVED CRACK LONGERON, DRILLED NEW LONGERON AND SPLICE, TREATED AND INSTALLED IAW DC-9 SRM 53-02 FIG 14, 51-30-2, 51-30-5. (M)SDR 97ZZZM152Stringer · corrodedTHE AFT CARGO HAS SEVERAL SPOTS OF CORROSION ON UPPER ANGLE OF STRINGER 29R, BETWEEN STATION 889 AND 937. REMOVED CORROSION AND FOUND IT TO BE OUT OF LIMITS, IAW DC-9 SRM 51-10-3, RECEIVED NEW INTERCOSTAL, DRILLED HOLES AND DEBURRED IAW DC-9 SRM 51-10-4, INST
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