JASC 5313
Service difficulty reports · 36,310
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 QXEA2011092900910Stringer · corrodedSTRINGER 31P IS CORRODED AFT OF FR 176. REMOVED CORROSION IAW SRM 51-21-00-00-02. AREA FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3961. COMFIRMED CRACK FREE AREA REF NTM 51-00-01-250-801. COMPLETED REPAIR IAW RD 8/4-53-3961.SDR SWAA116802Stringer · corrodedDURING SCHEDULED 28Y CHECK, FOUND STRINGER CORRODED AT BS 499, STR 27R. REPAIRED STRINGER PER SRM.SDR FDEA201109244111Stringer · corrodedSTRINGER 28L IS CORRODED BETWEEN BS 520-540. REPAIRED STRINGERSDR FDEA201109244112Stringer · puncturedSTRINGER 28L OTBD FLANGE IS PUNCTURED BTWN BS 460-480. REMOVED, FABRICATED & INSTALLED STRINGER SECTION IAW SRM 53-10-3 FIG 1.SDR FDEA201109244109Stringer · corrodedCORROSION ON STRINGER 28L AT BS 490.SDR UALA2011092605169Stringer · corrodedCORROSION ON STRINGER 28R BETWEEN STA 1372 -1378. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER SPLICE PER SRM ON NR 3175N00238.SDR USAA2011101700046Stringer · damaged2S CHECK - ELONGATED HOLE ON STRINGER BETWEEN FR34 TO FR35, S35L. REPAIRED STRINGER BETWEEN FR34 TO FR35, S35L IAW SRM A320 53-00-13 FIGURE 201.SDR FDEA201109234072Stringer · corrodedCORROSION ON STRINGER 18A, LOWER SHELF AT BS 890, LBL 60. REMOVED DAMAGED STRINGER, FABRICATED NEW, AND INSTALLED IAW DWG 65-22419 & SRM 51-30-2.SDR FDEA201109234073Stringer · corrodedCORROSION ON STRINGER 18A LOWER SHELF AT BS 930, LBL 60. REPAIR ACCOMPLISHED.SDR FDEA201109234096Stringer · corrodedSTRINGER 26L CORRODED BETWEEN BS 720A-720B. CUTOUT DAMAGED SECTION OF THE STRINGER, APPROX CUTOUT DIM: 5". FABRICATED STRINGER FILLER AND STRINGER HAT SECTION REPAIR. INSTALLED REPAIR IAW SRM 53-10-1 FIG 1, SRM 53-10-3 FIG 1, SRM 51-10-2 AND SRM 51-30-2.SDR AALA20110923TUL10Longeron · crackedLEFT SIDE LONGERON 2 LEFT IS CRACKED AFT SIDE OF FRAME 1418. INSTALLED SPLICE REPAIR PER SRM 53-02-00 FIGURE 18.SDR 7AHR2011092021Stringer · corrodedAFT BAGGAGE COMPARTMENT AT BODY STA 947.6, STRINGER 26L, HAS CORROSION OUT OF LIMITS.SDR FDEA201109224062Stringer · corrodedBULGE EXTERIOR FUSELAGE STA 1050 - 1030 BETWEEN STR 26-27L. FOUND STRINGER CORRODED. ACCOMPLISHED STRINGER REPAIR.SDR FDEA201109224019Stringer Splice · corrodedSTRINGER SPLICE 29R HAS CORROSION BETWEEN BS 990-1010. REMOVED STRINGER SPLICE IAW SRM 51-30-2, LOCATED AND DRILLED NEW STRINGER SPLICE IAW DWG 65-56249. INSTALLED NEW STRINGER SPLICE IAW SRM 51-30-2, AND DWG NR 65-56249.SDR FDEA201109224038Longeron · corrodedSTA 1079 TO 1099 LONGERON 45R SURFACE CORROSION FOUND EXEEDED LIMITS. CORROSION ON LONGERON REMOVED AS PER SRM 51-21-01 REV 47. MATERIAL MEASURED THICKNESS 0.096 INCH; MATERIAL REMOVED = 0.040 INCH; MATERIAL REMAINED = 0.056 INCH. FOUND EXCEEDED LIMIT SDR FDEA201109224046Longeron · crackedCRACK INDICATION APPROX 1" IN LENGTH FOUND DURING X-RAY INSP AT STA 6-100 , LONGERON -7R AFT SECTION EDGE. CARRIED OUT REPAIR AS PER SRM 53-00-05 FIG 202 REV 47 & DRAWING AEA7478 REV A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.SDR AALA20110926AFW05Stringer · corrodedDISCOVERED THAT STRINGER 34 RIGHT BETWEEN STATIONS 434 TO 456 HAS AREA OF CORROSION AROUND FASTENER. REMOVED CORROSION PER SRM 51-10-02. CUT AND REMOVED DAMAGE SECTION OF STRINGER. NO CORROSION NOTED ON SKIN. FABRICATED REPAIR PARTS PER SRM 53-30-03-2R. ISDR AALA20110926AFW04Stringer · corrodedDISCOVERED STRINGER 37 RIGHT BETWEEN STASTIONS 434 TO 456 HAS AN AREA OF CORROSION JUST AFT OF STRINGER SPLICE REPAIR., REMOVED DAMAGED SECTION OF STRINGER. FABRICATED REPAIR PARTS PER SRM 53-00-03-2R 2. INSTALLED STRINGER 37R PER SRM 53-00-03.SDR AALA20110926AFW03Stringer Splice · corrodedDISCOVERED THAT STRINGER SPLICE REPAIR ON STRINGER 39 RIGHT BETWEEN STATIONS 434 TO 456 AND STATIONS 412 TO 434 HAS AREAS OF CORROSION ON FLANGES. REMOVED LIGHT SURFACE CORROSION BETWEEN STATIONS 412 AND 434 WITHIN LIMITS PER SRM 53-00-03-1A. ACCOMPLISHED SPSDR AALA20110926AFW02Stringer · corrodedCORROSION FOUND AT STRINGER 35 LEFT BETWEEN STATIONS 412-434. CUT OUT AND REMOVED DAMAGED AREA. ACCOMPLISHED SPLICE REPAIR PER AARD 51-20-00-02 AND SRM 53-00-03.SDR AALA20110926AFW01Stringer · corrodedSTRINGER 37 LEFT BETWEEN STATIONS 434 TO 456 AND STATIONS 412 TO 434 HAS CORROSION ON OUTBOAD SIDE. CUT AND REMOVED DAMAGED SECTION OF STRINGER PER SRM 53-00-03-2R. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-03-2R.SDR QXEA2011092700907Stringer Splice · corrodedSTRINGER 31P SPLICE BETWEEN FR 32.4 AND 47 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-00-00-01.MINIMUM REMAINING THICKNESS .081". CONFIRMED CRACK FREE REF NTM 51-00-02-250-801 AND 51-00-01-250-801. WITHIN LIMITS OF SRM 53-20-43-00-01. ALODINED, PRIMED SRSDR QXEA2011092600891Stringer · corrodedSTRINGER 24P IS CORRODED FR 258.5 TO 301. REMOVED CORROSION IAW SRM 51-21-00-00-02. CONFIRMED AREA CRACK FREE REF NTM RD 8/4-53-3953. MATERIAL LOSS WITHIN LIMITS OF RD 8/4-53-3953. ALODINED AND PRIMED REPAIR IAW RD 8/4-53-3953. COMPLIED WITH TASK CARD RD SDR SWAA116748Stringer · damagedDURING SCHEDULED RON CHECK, FOUND STRINGER HEAT DAMAGED BETWEEN BS 259 TO BS 277, STR 19R. REMOVED AND REPLACED STRINGER SECTION IAW EA AND AAR EA.SDR SWAA116747Stringer · damagedDURING SCHEDULED RON CHECK, FOUND STRINGER HEAT DAMAGED BETWEEN BS 259 TO BS 277, STR 18R. REMOVED AND REPLACED STRINGER SECTION IAW EA AND AAR EA.SDR FDEA201109213986Stringer · corrodedCORROSION ON STRINGER 28L AT BS 490. REMOVED DAMAGED STRINGER SECTION, FABRICATED NEW STRINGER SECTION, SPLICES AND INSTALLED IAW SRM 53-10-3 FIG 1 & SRM 51-30-2.SDR FDEA201109213985Stringer Splice · corrodedSTRINGER SPLICE 28L, CORRODED AT BS 950F. ACCOMPLISHED REPAIR ON NR N00473.SDR FDEA201109213983Stringer · corrodedSTRINGER 29L IS CORRODED BETWEEN BS 1183-1166. CUTOUT DAMAGED STRINGER SECTION, FABRICATED REPAIR FILLER & SPLICE, INSTALLED REPAIR IAW SRM 51-30-2, SRM 53-10-3 FIG 1, & SRM 51-10-2.SDR FDEA201109213984Stringer Splice · corrodedSTRINGER SPLICE 28L IS CORRODED BETWEEN BS 950F-970. REMOVED STRINGER SPLICE IAW SRM 51-30-2, FABRICATED NEW STRINGER SPLICE AND INSTALLED IAW SRM 53-10-3, FIG 1.SDR FDEA201109213982Stringer · corrodedAFT PIT STRINGER 26R IS CORRODED WITH EXFOLIATION AT BS 1148. CUT OUT DAMAGED AREA AND FABRICATED FILLER, SPLICES AND TAPER SHIMS. INSTALLED REPAIR PARTS IAW SRM 53-10-3 FIG 1.SDR QXEA2011092600883Stringer · corrodedSTRINGER 26P HAS AN AREA OF CORROSION AFT OF FR 258.5. REMOVED CORROSION IAW SRM 51-21-00-00-02. FOUND WITHIN LIMITS OF RD 8/4-53-3954. COMPLETED REPAIR IAW RD 8/4-53-3954.SDR AALA20110921TUL03Stringer · damagedSTATION 1540 TO 1560 STRINGER 30 RIGHT DAMAGED. INSTALLED DOUBLER REPAIR SRM 53-00-01-2R-3.SDR QXEA2011092300858Stringer · corrodedSTRINGER 27P IS CORRODED FR 94.8 TO FR 116. REMOVED CORROSION IAW 51-21-00-00-02, MATERIAL LOSS FOUND TO BE WITHIN LIMITS OF RD 8/4-53-3952. TREATED, PRIMED, PAINTED AND APPLIED CIC FLANGE IAW SRM 51-21-10-02-01, 51-25-10-02-01 AND RD 8/4-53-2344.SDR FDEA201109213995Longeron · corrodedFORWARD CARGO AT STA 6-68 TO 6-72 LONGERON 51 FOUND WITH CORROSION, CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS = 0.062"; MATERIAL REMOVED = 0.041"; MATERIAL REMAINED = 0.021" FOUND OUT OF LIMITS IAW SRM 53-00-00, REV 47, FIG 205 LIMITS. SDR TX9Y20110922001Stringer · corrodedDURING INSPECTION OF THIS DATUM AIRPLANE, THE STRINGER 51R (P/N: 65B04483-13) IS FOUND HEAVILY CORRODED ON THE INBOARD SIDE WEB FLANGE AT STA 1958. THE STRINGER AFT END WAS TRIMMED AND A REPAIR SPLICE CHANNEL SIMILAR WITH THE ORIGINAL ONE, BUT WITH EXTENDED CSDR IPXA1M69656Longeron Splice · crackedINSPECTION TYPE:3C, IN FWD AFT FUSELAGE THROUGH ACCESS 311AB, LT SIDE LOWER FUSELAGE LONGERON SPLICE IS CRACKED AT RADIUS, AT 4TH LONGERON FROM ENTRY ACCOMPLISHED STA-SA EA 0115310-01-A3485 I/R AND UPS EO MD11-5310-44562-A.SDR FDEA201109203973Longeron Splice · corrodedLONGERON SPLICE AT BS 1219-1239, LONGERON 12R. FOUND CORRODED. CORRODED LONGERON SPLICE AREA REMOVED AS PER SRM 51-31-01 REV 47. NEW SPLICE FABRICATED AS PER DWG AEA0650 REV E AND INSTALLED AS PER SRM 51-31-01 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2SDR QXEA2011092100853Stringer · corrodedSTRINGER 27P IS CORRODED FR 176 TO 196. REMOVED CORROSION IAW SRM 51-21-00-00-02. REMAINING THICKNESS .058", CONFIRMED CRACK FREE REF NTM 51-00-01-250-801 AND 51-00-02-250-801. FOUND TO BE WITHIN LIMITS OF RD 8/4-53-3934. TREATED PRIMED AND PAINTED IAW RD SDR GLBA20110921GStringer · corrodedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, FOUND CORROSION ON 2" OF STRINGER 16 AT FS 228.25, BELLY OF FUSELAGE. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW EO 11-1900-53-055. MATERIALS UTILIZED ARE INCLUDED IN THE EO.SDR SWAA116683Stringer Splice · crackedDURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CHANNEL CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED CHANNEL PER SRM AND DWG.SDR C2XA11SH142Stringer · corrodedSHV - DURING C-CHECK STRINGER 21R HAS CORROSION BETWEEN FRAMES 7-13. MAINTENANCE REMOVED AND REPLACED STRINGER 21R BETWEEN FRAMES 7-13 IAW EMB-145XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR DALA1156680966Longeron · crackedDURING PSV, PAX MOD VISIT IN MSP FOUND CRACK IN TAIL SECTION LONGERON 2L AT STA 1418. CUT OUT AND SPLICED IN NEW SECTION LONGERON PER MD88 SRM 53-02.SDR ZZDA2011794Stringer · corrodedAFT CARGO COMPARTMENT LONGERON STRINGER AND BRACKET SUPPORT, STA 1037 TO 1053, LONG L22, CORROSION. OPEN DEFECT.SDR FDEA201109193966Stringer Splice · crackedAFT CARGO STA 1620 AT S-25R SPLICE IS DENTED. R & R 5 EA FASTENERS F.O.M IAW SRM 51-40-02. FOUND SPLICE TO BE CRACKED AND OUT OF LIMITS IAW SRM 53-00-03, FIG 101, SH 1, P.101. RECEIVED SPLICE ON MAE TRAVELER T11/894584, PN FX-146N3820-56. REMOVED CRACKED SSDR ZZDA2011773Stringer · crackedAFT FUSELAGE UPPER STRINGER, STA 1146, LONG R2, CRACKED. ACCOMPLISHED UPPER STRINGER REPAIR PER B717 SRM 53-00-05.SDR CALA2011091900610Stringer · corrodedSTRINGER SL-27 BTWN STA 500F TO 500G HAS INTERGRANULAR CORROSION. REMOVED DMG SECTION AND REPAIRED PER SRM 53-00-03 REPAIR 1.SDR FDEA201109173917Longeron · corrodedAFT CARGO BS 1902, LONGERON 43R FOUND WITH CORROSION. CORROSION REMOVED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-00, REV 47, FIG 205. LONGERON TRIMMED OUT IAW SRM 53-00-05, REV 47, FIG 202, REPAIR 1. NEW LONGERON AND 2 REPAIR SPLICES FABRICATED AND INSTALLEDSDR FDEA201109173914Longeron · corrodedCENTER CARGO COMPARTMENT: STA 5-83 TO 5-93, RT LONGERON 33R CORRODED. CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL MATERIAL THICKNESS = 0.060"; MATERIAL REMOVED = 0.030"; MATERIAL REMAINED = 0.030" - FOUND OUT OF LIMITS IAW SRM 53-00-00, REV 47, FISDR JR2R2011091500402Stringer Splice · corrodedSPLICE ON STR 25R CORRODED STA 333. REPLACED STRINGER IAW CRJ-700 SRM 51-42-06, 51-42-21.SDR JR2R2011091500401Stringer · corrodedSTR 25R CORRODED BETWEEN FRAMES STA 333 AND 310. REPLACED STRINGER FROM 280 TO 333 IAW CRJ 700 SRM 51-42-06, 51-42-06.
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