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 P5CA9601061Stringer · crackCRACK BEYOND EXISTING REPAIR ON STA 1900 LT SIDE ABOVE STRINGER 41 TO 42. REPAIRED PER SRM 53-10-04.SDR P5CA9601056Stringer · crackedFOUND 2 CRACKS IN AFT ROW STA 460 BETWEEN STRINGER 14E AND 15 RT. REPAIRED IAW SB53-2289.SDR P5CA9601050Stringer · corrodedCORROSION STRINGER 7 TO 9 BETWEEN STA 1580 TO 1600 LT. CORROSION REMOVED AND AREA TREATED PER 51-10-01.SDR P5CA9601049Stringer · corrodedCORROSION STRINGER 2 RT BETWEEN STA 1580 TO 1600. CORROSION BLENDED OUT SURFACE, SMOOTHED PER SRM 51-10-01 AND 51-10-02.SDR P5CA9601048Stringer · corrodedCORROSION TIE CLIP AT STA 1520 NEAR STRINGER 2 RT. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.SDR P5CA9601045Stringer · corrodedCORROSION ON STRINGER 5 AT STA 1420. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.SDR P5CA9601044Stringer · corrodedCORROSION ON STRINGER 8, 9, 10 LT BETWEEN STA 1380 TO 1400. CORROSION BLENDED OUT SURFACE, SMOOTHED PER SRM 51-10-01 AND 51-10-02.SDR P5CA9601043Stringer · corrodedCORROSION ON STRINGER 7 LT AT STA 1420 TO 1440. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.SDR P5CA9601042Stringer · corrodedCORROSION ON STRINGER 10 LT AND ON FRAME STA 1440. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.SDR P5CA9601041Stringer · corrodedCORROSION ON STRINGER 1 BETWEEN STA 1260 TO 1320 LT. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01.SDR 96FDEA01422Stringer · corrodedNR 0597 AND 036, BULGE IN SKIN AT BS 1157, STR 27 L.SDR 96FDEA01352Stringer · corrodedFORWARD CARGO BS 720 STR 23R HEAVY CORROSION INSIDE STRINGER ON LOWER LEG. REMOVED CORROSION AND INSTALLED STRINGER REPAIR PER SRM 53-10-3.SDR 9617889984Longeron · corrodedDURING H-CHECK, FOUND CORROSION ON THE KEEL CENTER SECTION (LONGERON 29R) AT FS 690. REPAIRED KEEL (P/N 5911418-101) PER EA 99-110728.SDR 9617879984Longeron · corrodedDURING H-CHECK, FOUND CORROSION ON LONGERON 29L FROM FS 676 TO 685. REPAIRED LONGERON (P/N 5911418-99) PER EA 99-110723.SDR 96ZZZM1349Longeron · corrodedMCI - DURING OP-16, FOUND CORROSION ON LONGERON 5-30 TOP LEFT FLANGE, AFT OF FORMER BS 1309. REPAIRED PER SRM 51-01. (M)SDR 96ZZZM1345Longeron · corrodedMCI - DURING OP-16, FOUND CORROSION ON LONGERON 25R INBOARD FLANGE AT FASTENER HOLES, STATION 1309. REPLACED TRACK STATION 1300 TO 1322 PER SRM 51-01, PAGE 1, ITEM C AND INSTALLED SPLICE PER SRM 53-03, FIGURE 5. (M)SDR 96ZZZM1343Stringer · corrodedMCI - DURING OP-15, FOUND CORROSION ON FORMER, ABOVE STRINGER 30, BS 207, AFT OF DOOR. REMOVED CORROSION PER SRM 51-10-3 AND REINSTALLED FASTENERS PER SRM 51-30-0. (M)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 SWAA960778Stringer · crackedDURING SCHEDULED SV CHECK, FOUND STRINGER CRACKED AT BS 767, S10R. REPAIRED PER BOEING SRM.SDR SWAA960777Stringer · corrodedDURING SCHEDULED SV CHECK, FOUND STRINGER CORRODED AROUND FASTENER HOLES FROM BS 360 TO BS 420, WL 305. REPAIRED PER BOEING SRM.SDR 96FDEA01327Stringer · corrodedNR0328 AND 001, CORROSION (C53-111-01, -2) ON STR 27L BS 720A PLUS 10 WL 150 LBL 15. *S/D* REMOVED DAMAGED SECTION FROM 720A PLUS 7 TO 720A PLUS 10. REPAIRED STR SECTION PER FEDEX SRM 53-10-1, 53-10-3 FIG 1.SDR 9617659996Longeron · corrodedDURING M-CHECK, FOUND CORROSION ON LONGERON 19L AT FS 905. REPAIRED LONGERON PER EA DC9-53-028.SDR UPS96220848Stringer · corrodedINSPECTION TYPE: SI. CORROSION ON STRINGER 2 RT STA 110-1130. REPAIRED STR 2 RT IAW TRAMCO E.W.O. 96-2444. CORROSION REMOVAL REWORK WAS DEEMED OUT OF LIMITS IAW SRM 53-10-1.SDR UPS96220847Stringer · corrodedINSPECTION TYPE: SI. CORROSION ON STRINGER 3 RT STA 360-440. REMOVED CORROSION REWORK DEEMED OUT OF LIMITS IAW SRM 53-10-1. REPAIRED STR 3 RT IAW TRAMCO E.W.O. 96-2444.SDR AWXA960386Stringer · corrodedPAE - FLT 7803 - DURING ROUTINE SCHEDULED C-8 MAINTENANCE CHECK, FOUND EVIDENCE OF CORROSION, FUSELAGE SKIN BULGING AT BS 945, STR 26L. REPAIRED CORRODED STRINGER PER SRM 53-30-3, FIG 6 AND SRM 53-10-3, FIG 1. (M)SDR ASAA9610096Stringer · crackedSEA - DURING D-CHECK, A CRACK WAS IDENTIFIED AT THE ENDS OF STRINGER 16R, BS 500B, WHICH TERMINATES AT THE RIGHT WING LEADING EDGE LIGHT. REPAIRED PER EA 5310-1456 AND BOEING SERVICE BULLETIN 737-53-1145. (M)SDR USAA960546Longeron · crackedPIT - DURING Q4-C6 CHECK, FOUND .25 INCH CRACK IN LONGERON AT BELT FRAME 24 RIGHT BETWEEN STA 446 - STA 465. REMOVED CRECKED SECTION, INSTALLED NEW LONGERON AND SPLICES PER TYPICAL REPAIR 53-10-07, FIGURE NR 2. (X)SDR SWAA960796Stringer · corrodedDURING SCHEDULED D-CHECK, FOUND STRINGER 27L CORRODED FROM BS 947 TO BS 1012. REPAIRED PER BOEING SRM.SDR SWAA960756Stringer · crackedDURING SCHEDULED D-CHECK, FOUND STRINGER 22R CRACKED AT BS 495. REPLACED PER BOEING SRM.SDR P5CA9600665Stringer · corrodedFOUND LEVEL ONE CORROSION ON STRINGER 47 NEAR STATION 1920 RT SIDE. REMOVED CORROSION AND TREATED AREA IAW SRM 51-10-01.SDR P5CA9600608Stringer · corrodedFOUND CORROSION ON STRINGER 51 BETWEEN STA 1940 TO 1960 RT SIDE. REMOVED LEVEL ONE CORROSION AND TREATED AREA IAW SRM 51-10-01. CORROSION FOUND TO BE WITHIN LIMITS OF SRM 53-10-01.SDR P5CA9600606Stringer · corrodedFOUND CORROSION ON STRINGER 42 BETWEEN STA 1980 TO 2000 RT SIDE. REMOVED LEVEL ONE CORROSION AND TREATED AREA AS PER SRM 51-10-01. CORROSION FOUND TO BE WITHIN LIMITS OF SRM 53-10-01.SDR DLL10961848Longeron · corrodedTHE FUSELAGE NOSE WHEELWELL LONGERON AT LBL 22 WAS FOUND WITH EXTENSIVE CORROSION AT FS 328. DUE TO THE EXTENT OF THE CORROSION, THE LONGERON WILL BE CUT AT FS 339 AND A NEW REPLACEMENT SECTION WILL BE SPLICED IN.SDR 96FDEA01318Stringer · corrosionNR0440, FWD CARGO BS 720 STR 23R HEAVY CORROSION INSIDE STR ON LOWER LEG. *S/D* REMOVED CORROSION AND INSTALLED STRINGER REPAIR PER 53-10-3.SDR UPS96220849Stringer · corrodedINSPECTION TYPE: SI. CORROSION ON STRINGER 2 RT STA 580-622. FOUND CORROSION OUT OF LIMITS PER SRM 51-10-6 AND SRM 51-10-1. REMOVED AND REPLACED STRINGER 2 RT STA 580-622 PER SRM'S 51-10-3, 51-30-2, 51-10-2.SDR MWEA96400Longeron · corrodedDURING D-CHECK, LONGERONS 16L AND 17L WERE FOUND CRACKED AT STA 965 AND LONG 17L CRACKED AT STA 980. INSTALLED REPAIR IAW SRM 53-02, PAGE 2A.SDR MWEA96394Longeron · corrodedDURING D-CHECK, LONGERON 29L WAS FOUND TO HAVE VARIOUS AREAS OF CORROSION STA 229 THROUGH 579. INSTALLED NEW LONGERON IAW SRM 53-01.SDR MWEA96393Longeron · crackedDURING D-CHECK, LONGERON 30 FOUND WITH MILD CORROSION FROM STA 417 T0 579. INSTALLED NEW LONGERON IAW SRM 53-01.SDR MWEA96388Longeron · corrodedDURING D-CHECK, LONGERON 29R FOUND WITH CORROSION FROM STA 436 TO 522. FOUND CORROSION OUT OF LIMITS AND REPLACED WITH NEW LONGERON SECTION IAW SRM 53-01.SDR MWEA96370Longeron · corrodedDURING D-CHECK, LONG 30 END FITTING WAS FOUND CORRODED FROM STA 579 TO 604. FABRICATED SPLICE FITTING IAW DAC DWG 3924809 AND INSTALLED IAW SRM 53-01.SDR MWEA96362Longeron · crackedDURING D-CHECK, LONGERON UPPER FLANGE FOUND CRACKED AT STA 313 TO 332 AT LONG 29L. FABRICATED A LONG SECTION AND REPAIR SPLICES AND INSTALLED IAW SRM 53-02 AND 53-02, FIG 14.SDR MWEA96346Longeron · crackedDURING D-CHECK, LONGERON 4L FOUND CRACKED IN FRAME AT STA 200. SPLICED IN NEW SECTION OF LONGERON IAW SRM 53-02 FIG 2.SDR MWEA96321Longeron · crackedDURING D-CHECK, CRACKED LONGERONS WERE FOUND IN AFT ACCESSORY COMPT LONG 2L AND 2R AT STA 1076. FABRICATED LONGERONS IAW SRM 53-02, FIG 8 AND INSTALLED IAW SRM 53-01, PAGE 1.SDR 96UAL900586Stringer · corrodedFOUND ONE POPPED AND SEVERAL DISHED RIVETS ON BELLY SKIN FROM STATION 760 TO 780. INTERNAL INSPECTION FOUND CORRODED STRINGERS 47L AND 47R, STATION 760 TO 780. REMOVED STRINGERS 47L AND 47R FROM STATION 740 TO 780. REMOVED LIGHT SURFACE CORROSION ON SKIN, ASDR 9617496614Longeron · corrodedDURING P-CHECK, FOUND CORROSION IN THE LEFT OVERWING LONGERON AT BS 1300. REPAIRED LONGERON (P/N 65B10097-11) PER EA 66-101907.SDR SWAA960742Stringer · crackedDURING SCHEDULED 1/2 D CHECK, FOUND STRINGER 16R CRACKED BETWEEN 500A AND 500B. REPAIRED PER BOEING SRM.SDR RAIA960746Stringer · corrodedFOUND STRINGER 21 HAS CORROSION AT FRAME 38 AND 39. REPLACED STRINGER SECTION. (M)SDR RAIA960744Stringer · corrodedFOUND STRINGER 17 HAS CORROSION BETWEEN FRAME 36 AND 40 AND 41 TO 42. REPLACED STRINGER SECTION PER SRM 53-00-00 FIG 428. (M)SDR CALA9601198Longeron · crackedINSPECTION FOUND LONGERON 5R CRACKED AT STA 737. A NEW SECTION OF LONGERON WAS SPLICED IN IAW SRM 53-02, FIGURE 2.SDR CALA9601192Longeron · crackedINSPECTION FOUND LONGERON 3L CRACKED AT STA 160. THE CRACKED SECTION OF LONGERON WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 2.
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