JASC 5311
Service difficulty reports · 61,540
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 N6WA2025012704Frame · chafedCHAFFING ON FRAME AT FS1162 STGR7L. REPAIRED FRAME AT FS1162 STGR 7L IAW STS EA79-2024-299 IR.SDR SWI2025F00438Frame · crackedFS333.00 STRG 1RH - 2RH, FRAMED CRACKED BOTTOM AREA (MARKED) (C-CHECK RO 04/04/2025)PERFORMED REPAIR TO FRAME SECTOR AT FS333.00 BETWEEN STR 1R & STR 2R REF. REO 670-53-21-2552 REV -- DATED 2025-02-28 ALL STEPS COMPLIED WITH. SEE CONTINUE CARD FOR DETAILS. COMSDR SWAA2025021889633Frame · crackedCRACK INDICATION IN LOWER FASTENER HOLE LOCATED AT BS 727 FRAME INNER CHORD AT S-18A LEFT SIDE.CRACK DIRECTION 6 O CLOCK.AFT CARGO COMPARTMENT 2025-91801<[01] TOOL USED P/N: NORTEC 500D; S/N: N500X1693P030456; CAL DUE: 14-APR-25.;[02] STEP 7 TOOL USED: EDDY CUSDR SWAA2025021889629Stub Frame · crackedCRACK INDICATION ON STUB FRAME LOCATED ON BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 0.436 IN. APROX.AT PASSENGER CABIN 2025-91761<[01] REPLACED STUB FRAME AND FASTENERS LOCATED ON BS 296.5 IAW B737-700 SRM 51-40-02 ABD DRAWING 141A8370 SHESDR CALA2025013000244Frame · crackedRH FRAME 68 AT STR 8 HAS CRACK INDICATION ABOVE TOP FASTENER IN FRAME JUST BELOW STR 8 CRACK APPROX .150 INCH LONG. REPAIR PART PER PART 2 OF THE LATEST REVISION OF ECRA 5341-01471 CYCLES. PERFORM REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED ON OR BEFORE THESDR DALA2025012800667Frame · unknownSHIP 658 A.A. AD 5311-01218-01B, EXISTING REPAIR WAS FOUND IN THE INSPECTION AREA AT STA 1640, BTW S-09R AND S-11R. CORRECTIVE ACTION: SUMMARY OF NRC 00159: INSPECTIONS ON FRAME STA 1640, BTW S-09R AND S-11R WERE PERFROMED UNDER ER/A 591104-14AD REV. ORIGINAL.SDR REXA2025022600229Frame · corrodedFRAME AT FS549 HAS CORROSION BETWEEN STGR 17L AND 18L. COMPLIED WITH EA NO: CRJ753-18456 REV IR DATED 02/19/2025.SDR FDEA202501240124Frame · crackedNDT INSP - RH CENTER WING BOX REAR SPAR FR47 BOTTOM PANEL "C" HOLE FOUND CRACKED SINGAL. COMPLIED WITH EA: 6-5710-T0381607 P1. TITLE: WINGS - BASIC WING STRUCTURE - LH WING FR47 REAR SPAR HOLE G CRACK REPAIR - SB A300-57-6113. REPAIRED THE CENTER WING BOX SDR JR2R20250124167Frame · corrodedCORROSION FOUND ON THE AFT SIDE OF FRAME 82 UNDER THE SHEAR TIE BETWEEN STRINGERS 27R AND 28R.SDR REXA2025030300246Frame · corrodedFS379 BETWEEN 20R AND 21R HAS CORROSION. REMOVED DAMAGED FRAME AT FS379 BETWEEN STR20R TO STR24R IAW CRJ-700 SRM 51-42-06-001-001-A01. INSTALLED SKIN RIVETS INTO NEW SERVICEABLE FRAME PN: SH670-32118-3S AND INSTALLED 15EA RIVETS INTO FRAME/REINFORCEMENT ANGLE SDR DALA2025012500624Frame Angle · damagedAIRCRAFT 3017, DAMAGED LH FRAME 74 CLIP PT # D53571133250 BETWEEN STR 28L AND STR 29L. CORRECTIVE ACTION: REPLACED PER AIRBUS REPAIR DRAWING R535-70010-000 REV P. ADDITIONAL INFORMATION 019-0007:1212-6055/017. (LP 0774937)SDR DALA2025012400623Frame Angle · damagedAIRCRAFT 3017, DAMAGED RH FRAME 74 CLIP PT # D53571553215 BETWEEN STR 32R AND STR 31R. CORRECTIVE ACTION: REPLACED PER AIRBUS REPAIR DRAWING R535-70010-000 REV. ADDITIONAL INFORMATION 019-0007:1212-6055/011 00018. (LP 0775709)SDR DALA2025012300575Frame Angle · damagedAIRCRAFT 3017, DAMAGED LH FRAME 74 CLIP PT #D53571553210 BETWEEN STR 29L AND STR 30L. CORRECTIVE ACTION: REPLACED PER AIRBUS REPAIR DRAWING R535-70010-000 REV P.SDR DALA2025012300574Frame Angle · damagedAIRCRAFT 3017, DAMAGED RH FRAME 74 CLIP PT # D53571553220 BETWEEN STR 28R AND STR 27R. CORRECTIVE ACTION: REPLACED PER AIRBUS REPAIR DRAWING R535-70010-000 REV P.SDR DALA2025012300573Frame Angle · damagedAIRCRAFT 3017, DAMAGED RH FRAME 74 CLIP PT # D53571553213 BETWEEN STR 30R AND STR 29R. CORRECTIVE ACTION: REPLACED PER AIRBUS REPAIR DRAWING R535-70010-000 REV P.SDR DALA2025012300572Frame Angle · damagedAIRCRAFT 3017, DAMAGED LH FRAME 74 CLIP PT # D53571553214 BETWEEN STR 31L AND STR 32L..CORRECTIVE ACTION: REPLACED PER AIRBUS REPAIR DRAWING R535-70010-000 REV P. ADDITIONAL INFORMATION 019-0007:1212-6055/008. (LP 0774938)SDR DALA2025012300571Frame Angle · damagedAIRCRAFT 3017, DAMAGED RH FRAME 74 CLIP PT # D53571553230 BETWEEN STR 28R AND STR 29R. CORRECTIVE ACTION: REPLACED PER AIRBUS REPAIR DRAWING R535-70010-000 REV P. ADDITIONAL INFORMATION 019-0007:1212-6055/013. (LP 0774935)SDR DALA2025012300570Frame Angle · damagedAIRCRAFT 3017, DAMAGED LH FRAME 74 CLIP PT # D53571553212 BETWEEN STR 30L AND STR 31L. CORRETIVE ACTION: REPLACED PER AIRBUS REPAIR DRAWING R535-70010-000 REV P.SDR N6WA2025012301Frame · corrodedCORROSION AT FS379 FRAME BOTH SIDES FROM STGR20R-STGR23R. REPLACED FRAME FS379 STGR20R-STGR23R IAW CRJ SRM 51-42-06.SDR REXA2025033100364Frame · corrodedFS 565 IS CORRODED BETWEEN STGR 26L AND STGR 27 IN THE FWD BAGGAGE BAY REMOVED 6 EACH RIVETS FROM FS565 BETWEEN STR 26L AND STR27 TO FACILITATE EVALUATION IAW CRJ700 SRM 51-42-06-001-001-A01. RIVETS REPLACED IAW ENEDAVOR AIR EA CRJ753-18450 REV IR (PRELIMINARSDR SWAA2025022488559Stub Frame · crackedCRACK INDICATION ON STUB FRAME LOCATED BETWEEN BS 294.5 TO BS 296 AND BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 0.687 IN. APPROX. AT PASSENGER CABIN 2025-80595<[01] INSTALLED STUB FRAME LOC. ON BS 296 BTW S-7R TO S-9R AT FWD GALLEY DOOR AREA IAW B7SDR SWAA2025021388430Stub Frame · crackedCRACK FOUND ON FSD STUB FRAME AT BS291.5 + 8.5; .7' ABOVE SEAL DEPRESSOR; .6' IN LENGTH MARKED LOCATION<[01] REMOVED AND REPLACED FSD UPPER STUB FRAME I.A.W SRM 51-40-02-0G-0 AND DWG 141A8370.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWI2025F00079Frame · chafedFRAME AT FS1144.00 AT STRINGER L9 HAS CHAFE DAMAGE FROM WATER SPRAYER LINE. (FILED CLOSED) REPAIRED DAMAGED SECTION OF FRAME AT FS 1144.00 AT STRINGER L9 IAW REO 670-53-2463 REV -- DATE 2025-02-01.SEE CP 29566492 FOR EDDY CURRENT INSPECTION.SDR CALA2025012700221Frame · cracked"REPAIR BEFORE NEXT FLIGHT" LEFT FRAME 16 DOUBLER JOGGLE HOLE LE TTER "C" HAS CRACK INDICATION IN THE FRAME LAYER AT THE 3:0 CLOC K POSITION 100% S.H.. GENERATED BY V062335 ON HAECO LCQ NR 92983 32 / 26332 IAW SRM 51-73-12/001. REPETITIVE INSPECTIONS REQUIRED SDR CALA2025012700220Frame · cracked"REPAIR BEFORE NEXT FLIGHT" RIGHT FRAME 16 DOUBLER JOGGLE HOLE L ETTER "C" HAS A CRACK INDICATION IN THE FRAME LAYER AT THE 9:0 C LOCK POSITION 100% S.H.. IAW SRM 51-73-12/001. REPETITIVE INSPECTIONS REQUIRED PER SRI AND SUBSEQUENT INSPECTIONS AT 5900 FLIGHT SDR SWI2025F00421Frame · corrodedFRAME FS517.00 LOWER FLANGE, FORWARD AND AFT WEBS ARE CORRODED BETWEEN STGR25L & 26L (MARKED) (C-CHECK RO 04/04/2025)REMOVED CORROSION ON FRAME FS517.00 LOWER FLANGE, FORWARD AND AFT WEBS REF CRJ700 SRM 51-21-06-001-001-A01. REMOVED AND REPLACED LH FRAME FS517SDR K11A2025032700305Frame · damagedE/E BAY BILGE FRAME AT STA 360 AND APPROX BETWEEN STRINGERS S28R TO S29R DAMAGED WHERE FRAME MEETS FUSELAGE SKIN.SDR CALA2025012700222Frame · crackedLEFT FRAME 16 DOUBLER JOGGLE HOLE LETTER ''A'' HAS CRACK INDICATIO N IN THE FRAME LAYER AT THE 3 OCLOCK POSITION 100% S.H. SRI 53-11-12-205-008 AT 6800 FLIGHT CYCLES SINCE REPAIR FLIGHT HOURS ARE NOT RELEVANT FOR THESE REPETITIVE INSPECTIONS. EMBODIMENT AND SSDR CALA2025012300187Frame · crackedLEFT FRAME 16 DOUBLER JOGGLE HOLE #7 HAS A CRACK INDICATION IN T HE FRAME LAYER AT THE 3 OCLOCK POSITION 100%SDR DALA2025012300544Frame Angle · damagedAIRCRAFT 3017, DAMAGED LH FRAME 73 CLIP PT # D53571552212 BETWEEN STR 31 AND STR 32. CORRECTIVE ACTION: REPLACED PER AIRBUS REPAIR DRAWING R535-70010-000 REV P. ADDITIONAL INFORMATION 019-0007:1212-6055/002 00006. (LP 0772040)SDR DALA2025012300542Frame Angle · damagedAIRCRAFT 3017, DAMAGED LH FRAME 73 CLIP PT # D53571132266 BETWEEN STR 28L AND STR 29L. CORRECTIVE ACTION: REPLACED PER AIRBUS REPAIR DRAWING R535-70010-000 REV P. ADDITIONAL INFORMATION 019-0007:1212-6055/016 00024. (LP 0772060)SDR DALA2025012300541Frame · damagedAIRCRAFT 3017, DAMAGED RH FRAME 73 CLIP PT # D53571552213 BETWEEN STR 30R AND STR 29R. CORRECTIVE ACTION: REPLACED PER AIRBUS REPAIR DRAWING R535-70010-000 REV P. ADDITIONAL INFORMATION 019-0007:1212-6055/006 00013. (LP 0772056)SDR DALA2025012300540Frame · damagedAIRCRAFT 3017, DAMAGED RH FRAME 73 CLIP PT # D53571552213 BETWEEN STR 31R AND STR 32R. CORRECTIVE ACTION: REPLACED PER AIRBUS REPAIR DRAWING R535-70010-000 REV P. ADDITIONAL INFORMATION 019-0007:1212-6055/005 00012. (LP 0772051)SDR GTIA2025011638685Frame · dentedDENT ON FUSELAGE FRAME 61+18 STRINGER 36+1 LEFT, LENGTH 1.0 WIDTH 1.1 DEPTH .018, RAF-01 -REPAIRED DENT IAW A320 SRM 53-41-11-300 036 AT FR 67+18STR 36 L CAT A REPAIR.SDR DALA2025012100469Frame · bentBENT FRAME STA Y=465 BTW LONG 26L AND LONG 27L AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00279: FRAME STA Y=465 BTW LONG 26L AND LONG 27L AT FWD CARGO COMPARTMENT WAS REPAIRED PER PRI 623357-14 REV 2 AND ERA 623357-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. SDR DALA2025012000447Frame · crackedSHIP 3147 CRACK INDICATION FOUND ON LOWER CORNER OF FRAME RADIUS AREA LH SIDE. CORRECTIVE ACTION: COMPLIED WITH ER/A 622157-14. (0768675)SDR DALA2025012000446Frame · crackedSHIP 3147 CRACK INDICATION FOUND ON LOWER CORNER OF FRAME RADIUS AREA RH SIDE. CORRECTIVE ACTION: COMPLIED WITH ER/A 622157-14. (0768672)SDR SWIA202503170118Frame · corrodedFOUND CORROSION ON FWD WEB FACE AND LOWER FLANGE OF FRAME AT FUSELAGE BELOW FLOOR FS 295 STR24L ( MX# 29494459 JOB OP: HN00214212 ) (C-CHECK RO 3/14/2025) REPAIRED FWD. WEB FACE AND LOWER FLANGE OF FRAME AT FUSELAGE BELOW FLOOR FS295 STR24L IAW REO 670SDR DALA2025012000466Frame · crackedCRACK ON FRAME DOUBLER STA Y=1178 CANT BTW LONGERON 2-3LH AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 264: FRAME DOUBLER STA Y=1178 CANT BTW LONGERON 2-3LH AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-30-08-2R PROCEDURE 7 REPAIR 7. (LP #07673SDR YENA2025012100079Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN FASTENER HOLE FRAME 16 UPPER CORNER DOU BLER JOGGLE AREA HOLE C AT 3 OCLOCK LH SIDE CRACK LENGTH APROX. 0.169 INCH; (RESOLVED ON W/O: 1331840 TASKCARD: NR-00033) FUR-A320-53-01966, REF AEROMAN N/R 2024-SDR GTIA2025050938907Frame · damagedPENETRATION DAMAGE, ELONGATED HOLE, FOUND AT FRAME 52 BETWEEN STRINGERS 4R AND 5R. RAF-01 3409900-02 CREATED.-PENETRATION DAMAGE FR 52 54R-55R REPAIRED ON WO 344021 EA 5341-2507 RAF-01 3409900-02SDR CALA2025022800465Frame · damagedR/H SIDE NEED INSTRUCTIONS TO REMOVE AND REPLACE THE FRAME AND FAIL-SAFE STRAP AT STA 663.75 NEAR S-18A REF AAR N/R 9928969 PREFORM INSPECTION R/H STA 663.75 REAR SPAR FRAME ASSEMBLY ON A/C N34222 I.A.W PT,2 OF LATE ST REV OF ECRA 5340-02218 PER ECRA 5340-0221SDR IPXA2025021340099Frame · crackedCRACKS FOUND ON RH FR 47 HORIZONTAL JUNCTION HOLES F, B AND Q REVIEWEDROTO PERFORMED ON HOLE B. NO DEFECTS FOUND IAW NTM 51-10-01. T96525 T91779. COMPLIED WITH EO# 300-5710-27-A3775 PRELIM 1 STEP #2SDR CALA2025021400356Frame · crackedFOUND CRACK ON AFT CARGO COMPARTMENT FRAME UPPER FLANGE AT STA 9 47.5 BTW S26R AND S-27R (REF. AAR NR 1000025895) AIRCRAFT FLIGHT CYCLES, BUT BEFORE 75,000 TOTAL AIRCRAFT FLIGHT E REPAIR AT STA 947.5 BETWEEN STRINGERS 26R AND 27R ON AIRCRAFT -08511. CYCLES, PESDR IPXA2025021237849Frame · crackedCRACK FOUND ON LH FR47 HORIZONTAL JUNCTION HOLE S. ACCOMPLISH THE REPAIR PER EA 300-5710-27-A3774 REV. -.SDR IPXA2025012426474Frame · dentedREF HEAVY CHECK REPAIR T3F18E0051QEH, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. ACCOMPLISHED REPAIR PER EA 757-5360-01-B0334 IR. OSD: 1/24/2025SDR IPXA2025012326458Frame · dentedREF HEAVY CHECK REPAIR T3F18E0051QE4, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. ACCOMPLISHED REPAIR PER EA 757-5360-01-B0331 IR.SDR IPXA2025012426435Frame · dentedREF HEAVY CHECK REPAIR T3F18E0051QE6, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. ACCOMPLISHED REPAIR PER EA 757-5360-01-B0330 IR. OSD: 1/24/2025SDR IPXA2025012326400Frame · dentedREF HEAVY CHECK REPAIR T3F18E0051QC2, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. ACCOMPLISHED REPAIR PER EA 757-5330-01-B0328 IR. OSD: 1/24/2025SDR IPXA2025012326442Frame · dentedREF HEAVY CHECK REPAIR T3F18E0051QCU, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. ACCOMPLISHED REPAIR PER EA 757-5330-01-B0337 IR. OSD: 1/24/2025
Back to JASC 5311