JASC 5311
Service difficulty reports · 61,530
Reports filed under 5311 · Fuselage Main, Frame, 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 = '5311' 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 = '5311' 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 DALA2025123009511Frame · damagedFRAME 64 FWD SIDE. STRINGER 2R NOTED WITH TOOLING DAMAGE ON INBD UPPER RADIUS OF STRINGER. REPAIRED PER SRM 51-73-00. (1376066)SDR DALA2025123009509Frame · damagedFR 64 FWD SIDE AT STRINGER 1R NOTED WITH TOOLING DAMAGE ON INBD UPPER RADIUS OF STRINGER. REPAIRED PER SRM 53-11. (1376058)SDR DALA2025123009508Frame · damagedFORWARD SIDE OF FR 64 AT STRINGER 1R NOTED WITH TOOLING DAMAGE ON OTBD FACE AND UPPER EDGE. REPAIRED PER A330 SRM 53-11. (1376055)SDR DALA2025123009505Frame · damagedFRAME 63 AND STRINGER 1L HAD TOOLING MARKS IN LIP OF J. REPAIRED IAW SRM 51-73-00. (1376045)SDR YENA2025123001298Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND AT OPEN FASTENER HOLE, ZONE 1 VERTICAL STRINGER RADIUS Ñ4 IN CENTER FUSELAGE ON FRAME 36. CRACK DEPTH 0.095 INCH. CRACK DIRECTION 12 OCLOCK VIEW FWD TO AFT; REF AEROMAN NR 2025-623139 WO 2025 278/1 CCOMPLISHEDSDR YENA2025123001297Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND AT OPEN FASTENER HOLE LOC. ZONE 2 VERTICAL STRINGER RADIUS Ñ4 IN CENTER FUSELAGE ON FRAME 36. CRACK DEPTH 0.115 INCH . CRACK DIRECTION 11 AND 12 OCLOCK VIEW FWD TO AFT; REF AEROMAN NR 2025-623135 WO 2025 278/1 CSDR YENA2025123001296Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND AT OPEN FASTENER HOLE LOC. ZONE 2 VERTICAL STRINGER RADIUS Ñ2 IN CENTER FUSELAGE ON FRAME36. CRACK DEPTH 0.118 INCH . CRACK DIRECTION 12 OCLOCK VIEW FWD TO AFT; REF AEROMAN NR 2025-623119 WO 2025 278/1 ACCOMPLISSDR YENA2025123001295Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND AT OPEN FASTENER HOLE LOC. ZONE 1 VERTICAL STRINGER RADIUS Ñ2 IN CENTER FUSELAGE ON FRAME 36. CRACK DEPTH 0.108 INCH . CRACK DIRECTION 12 OCLOCK VIEW FWD TO AFT; REF AEROMAN NR 2025-623122 WO 2025 278/1 CCOMPLISSDR SWAA2026011455698Frame · crackedCRACK FRAME, BS 727D BTW S8 - 9R. PERFORMED A REPAIR ON THE FRAME IAW EA 1-A53-12114.SDR DALA2025122909458Frame · corrodedCORROSION AT AFT CARGO KEEL SPLICE STA 974 L28L TO L28R. REPAIRED FRAME SECTION PER B717 SRM 53-20-07-2R-3 AND REPAIRED SKIN FORMER SECTION PER B717 SRM 53-00-06-2R (1370207)SDR CALA2026011212865Frame · corrodedAFT CARGO, FLOOR AREA, BS 1460, BTWN STG 29R TO STG 30, FRAME HAS CORROSION. PART FABRICATED IN HOUSE PER DWG146N2063 AND DWG 140N2063. PERFORMED A REPAIR IAW 757-5360-13-A4229 1 THROUGH 9 WITH NO DEVIATIONS EC/RA:5360-02086.SDR CALA2026011212864Frame · corrodedAFT CARGO, FLOOR AREA, BS 1420, BTWN S29L - 28R, FRAME HAS CORROSION. PART FABRICATED IAW DWG 146N5426, REV A. PERFORMED A REPAIR IAW 757-5360-13-A4238 F IGURES 1 THROUGH 12 WITH NO DEVIATIONS EC/RA:5360-02087.SDR EE4Y2025122323662Frame · crackedDURING TASK CARD A32X-53-260-005 INSPECTION, RELATED TO AD 2022-15-05, & A320-53-1491, REV 01, FOUND EXISTING REPAIR WITH NO DATA APPROVED RECORD AT UPPER FUSELAGE PAX CABIN FR 68, S22R. REMOVED EXISTING REPAIR PARTS & IAW AIRBUS INSTRUCTIONS DOSSIER 81706624SDR SWAA2026012654652Frame · damagedELONGATED HOLE ON FRAME INNER SECTION, BS 500G, S26L. PERFORMED PERMANENT REPAIR ON THE FRAME BS 500G BTWN S25 - 27L IAW SRM 51-40-02, AND SRM 53-30-07-2R-1, REPAIR 1, ALTERNATIVE 1, FIGURE 202, & FIGURE 204.SDR SWAA2026012254651Frame · damagedONE ELONGATED HOLE ON FRAME INNER SECTION LOCATED ON BS 500F, STRINGER 26L IN THE FWD CARGO BAY. PERFORMED PERMANENT REPAIR ON FRAME BS 500F AND BTW STR 25L TO STR 27L. IAW SRM 51-40-02, AND SRM 53-30-07-2R-1, REPAIR 1, ALTERNATIVE 1, FIGURE 202, AND FIGURE SDR DALA2026082104776Frame · corrodedCORROSION ON FORMER AT FRAME 946 BETWEEN STRINGER 30 AND 29L, REPAIRED FORMER PER B717-200SRM 53-00-06-2R. (1362231) (AIRCRAFT GROUNDED).SDR DALA2026082104775Frame · corrodedCORROSION ON FORMER AT STATION 954, ON BOTH SIDES OF LONGERON 29L, CORRECTIVE ACTION: REPAIRED FORMER PER B717-200SRM 53-00-06-2R. (1362237) (AIRCRAFT GROUNDED).SDR DALA2025122209299Frame · damagedFRAME 24 R, AFT SIDE OF FRAME, HAS TOOLING DAMAGE AND ALSO STRINGER CLIP HAS TOOLING DAMAGE IN SAME AREA. REPAIRED PER ERA 630752-14 REV ORIGINAL. (1361689)SDR SWIA2025122076513Frame · corrodedEXFOLIATED CORROSION FOUND AT FRAME 379.00 INSIDE FWD WASTE SERVICE AREA. STRINGER 25R TO 27R. INSTALLED NEW FRAME 379 IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, DWG SH670-32280, REV H, AND DWG SH670-32050 REV. J. COMPLIED WITH SKYWEST TASK CARD SDR DALA2025122209311Frame · damagedFWD FUSELAGE, FR 23 S5R TO S6R DAMAGED. REPAIRED PER ERA 630770-14 REV ORIG. (1359701)SDR DALA2025122209302Frame Splice · damagedFUSELAGE FR42, S4R TO 5R, TOOLING DAMAGE ON FRAME SPLICE REPAIR. COMPLIED WITH ERA 630752-14. (1359681)SDR U0GA2025121900639Frame · damagedTHIS AIRCRAFT HAS BEEN GROUNDED. THE REPAIR FROM AS FOLLOWS; REMOVE AND REPLACED THE LEFT AND RIGHT BS 5700 FRAME 3P5338A13355 AND 3P5338A13455. IAW PSE/TQ/2024/172423.SDR SWIA2025121875730Frame · crackedDURING AUDIT OF RA 44367, BS 333 UPPER FRAME IS CRACKED BTWN STR 0 - 2L. REPAIRED IAW REO 601R-53-21-3018, REV--, IT WAS FOUND THAT THE SHIMS FOR THE REPAIR ARE THE WRONG DIMENSIONS AND ARE INSTALLED INCORRECTLY. INSTALLED NEW SHIM FABRICATED (ITEM -2) PER SDR SWIA20251223018Frame · damagedFWD FUSELAGE MACHINED, FRAME BS 610 DAMAGED, MAJOR REPAIR, PERFORMED PERMANENT REPAIR OF FRAME BS 610 BY CUTTING OUT DAMAGED AREA LOCATED AT THE 8 CLOCK TO 9 OCLOCK LOCATION AND SPLICING IN NEW PORTION OF FRAME IAW EDT 2025-170-934318, REV C.SDR DALA2025122209314Frame · damagedLEFT FRAME C61 HAD TOOLING DAMAGE ON CLIP. REPAIRED PER ERA 628320-14 REV. ORIG. (1357838)SDR DALA2025122209313Frame · damagedFRAME 61 BETWEEN P7 AND P8RT HAD TOOLING DAMAGE AROUND SEVERAL FASTENERS ALONG TOP ROLL. CLEANED UP TOOLING DAMAGE IAW ER/A 628320-14 REV. ORIG. (1357836)SDR CALA2025122212296Frame · corrodedFRAME 900 LT SIDE, HAD EVIDENCE OF CORROSION. ACCOMPLISHED FRAME WAS REPAIRED ON BS 900 LT SIDE IAW SRM 51-70-11-OG-0, AND BRACKET GUSSETS AND STOP FITTINGS WERE REMOVED AND IN STALLED IAW SRM 51-90-02-OG-0.SDR SWIA2025121900018Frame · damagedFWD FUSELAGE MACHINED, FRAME BS 610 DAMAGED. THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR, FORM M-337 AND ST51-00-00-002-SKY-U CARD REQUIRED (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSSDR SWIA2025121776358Frame · corrodedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA94505-601R-53-61-8235 MXCODEID105229-PR - COMPLY WITH PERMANENT REPAIR ON RA ID: 94505CW TEMPORARY DISPOSITION: FOR BLENDED CORROSION DAMAGE TO FRAME ASSY. FS589.00 ASSY. BETWEEN STR 21R - STR 22R. PERMANENT REPAIR: SDR VNAA20260511005Frame · corrodedFRAME SECTOR AT F.S.319 IS CORRODED AT STRINGER 21L. INSTALLED NEW FRAME AT FS 319, P/N SH670-31891-3, IAW SRM 51-42-06-001-001-A01.SDR SWAA2026012653439Frame · crackedCRACKED FRAME, BS 312, BTW S5 - 6L IN THE FWD GALLEY AREA. PERFORMED A REPAIR ON THE FRAME IAW EA M-22-153-01244. LENGTH OF CRACK: 0.840.SDR DALA2025121809209Frame · dentedFUSELAGE FRAME IS DENTED AT BS 500E, BETWEEN STR 25RT AND 24RT. PERFORMED FRAME REPAIR AT BS 500E BETWEEN STR 23R TO STR 25R, AT FWD CARGO. PER B-737 900 SRM 53-30-07-2R-2 STEP 4 A, B, AND C.SDR 2A6R2025121774403Frame · chafedDURING 600-HOUR INSPECTION, CHAFE DAMAGE WAS DISCOVERED AT THE CENTER OF THE LH AND RH X-FRAME. THE MAX DEPTH OF DAMAGE ON THE LH SIDE IS 0.018” WITH AN AREA OF 0.040” BY 0.035” THE MAX DEPTH OF DAMAGE ON THE RH SIDE IS 0.013” WITH AN AREA OF 0.020” BY 0.010”.SDR LR7A2025121603796Frame · crackedDURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5303, FOUND CRACKED WINDOW FRAME AT FS151, RBL60, WL230. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-30-32. NR# 1001334880SDR SWIA2025121577770Frame · out of limitsINSPECTION OF LOWER FLANGE OF FRAME BEAM AT BS 513. COMPLIED WITH SB 601R-53-088, REV NC, REPAIRED THE BS 513 FRAME SECTOR LOWER FLANGE BTWN BL 27 & BL 45 LT & RT IAW REO 601R-53-41-3429, REV -. ALL STEPS COMPLIED WITH 1 THRU 17. COMPLIED WITH 51-900-1003 SSDR REXA2026052700763Frame · damagedELONGATED HOLE 2 EA AT LOWER SECTION OF FRAME FS 310 ,STRINGER 21L. ELONGATED HOLE 2 EA AT LOWER SECTION OF FRAME FS 310 ,STRINGER 21L WAS REPAIRED PER REO 690-53-21-2086 REV -B STEP 11SDR HNAA2026012900102Doubler · corrodedFR61 FLOOR LEVEL, FRAME DOUBLER CORRODED. REPAIRED IAW SRM 53-31-04.SDR HNAA2026012700087Doubler · corrodedFRAME DOUBLER CORRODED AT FR 61 LT. PERFORMED CUTOUT, FABRICATED & REINSTALLED REPAIR DOUBLER IAW SRM 53-31-04.SDR DALA2025121609169Frame · corrodedCORROSION ON THE UPPER CHORD OF FRAME AT BS 1380, BETWEEN S28 - 27R. REPAIRED THE FRAME IAW ERA 631033-14. (1352802)SDR DALA2025121609168Frame · bentTHE UPPER CHORD OF THE FRAME IS BENT & DAMAGED AT STA.1480 , S26 - 27L. REPAIRED BS 1480 FRAME BETWEEN S26-27L PER ERA 630812-14AD. (1352785)SDR CALA2026090119144Frame · gougedAFT CARGO, FRAME AT BS 727B, STRINGER 24L, UPPER FLANGE FOUND A GOUGED AND DEFORMED ON THE BACK SIDE. ACCOMPLISHED A REPAIR IAW SRM 51-40-02-0G-0, & SRM 53-60-07-2R-3.SDR DALA2025121509146Frame · corrodedDTA MONITOR INSPECTION LOG REF ERA 631033-14 FUSELAGE, BS 1380 FRAME, INNER CHORD RBL 23 CORRODED. REF ERA 631033-14. (1350256)SDR DALA2025121509145Frame · dentedDTA MONITOR INSPECTION LOG REF ERA 630812-14 FUSELAGE FRAME BS 1480, S26L - 27L DENTED. IAW ERA 630812-14. (1350212)SDR SWAA2026011451387Frame · crackedBS 312 FRAME IS CRACKED IN THE RADIUS JUST ABOVE THE L1 DOOR CUT OUT. REMOVED THE CRACK DAMAGE IAW SRM 51-10-02-0G-0. ACCOMPLISHED REPAIR EA M-22-153-01244.SDR YENA2025121601212Frame · corrodedDURING HEAVY MAINTENANCE: AFT FUSELAGE / STRINGER 43LH AT FR 65/ CORROSION - PERMANENT REPAIR; REFERENCES: /1/ STS EA 136-2025-018 /2/ AIRBUS RDAF 81669498/003/2025#A /3/ AIRBUS DOSSIER 81669498. DURING THE CURRENT (10/2025) M1 CHECK FOR A/C N905JB, STS REPORTSDR SWAA2026011451163Stub Frame · crackedONE CRACK NOTED ON R1 DOOR STUB FRAME, BS 294.5+2, 0.1 INCH ABOVE SEAL DEPRESSOR, WL 267. L: 1 INCH. EVALUATED CRACK ON FSD STUB FRAME AND FOUND TO BE OUT OF ALLOWABLE LIMITS. THE DAMAGED FSD STUB FRAME WAS REMOVED AND INSTALLED NEW UPPER STUB FRAME IAW SRMSDR DALA2025121109058Frame · gougedGOUGE ON BS 1640 BETWEEN S15L & 16L JUST FWD OF L4 DOOR. REFERENCE AMDS TASK CARD 2020-2424, STEP 5. GOUGE ON FS 1640 BETWEEN STR 15L AND STR 16L JUST FWD OF L4 DOOR WAS REPAIRED PER ER/A 630534-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR.SDR DALA2025121009005Frame · mechanic errorMISDRILLED NEXT TO BRACKET ON BACKSIDE OF FRAME 61 OUTBOARD OF P'3. CORRECTED PER ERA 630712-14 REV. ORIG. (1344269)SDR 2A6R2025121074402Frame · corrodedDAMAGE TO THE LH EDGE FRAME (PN: 350A21-4913-22) AND RH EDGE FRAME (PN: 350A21-4915-22), IN THE FORM OF CORROSION AND DENTS, WAS IDENTIFIED ACROSS THE ENTIRE LENGTHS OF THE OUTBOARD FACES OF THE FRAMES. BOTH LH AND RH EDGE FRAMES REQUIRED FULL REPLACEMENT. THESDR SWIA2025120877442Frame · corrodedFUSELAGE FRAME FS295 BETWEEN STR 25R - 26R HAD CORROSION, NDT ACCOMPLISHED, INSPECTION IAW MRM INTRODUCTION OF THE FRAME AROUND EACH FASTENER ON THE REPAIRED FLANGE REF STS EA 15-2013-029 REV A. OPENED DISCREPANT HOLES IN ENTIRE STACK UP AT BS 295, STR 2
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