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 IPXA2025012326367Frame · dentedREF HEAVY CHECK REPAIR T3F18E0051QBG, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. ACCOMPLISHED REPAIR PER EA 757-5330-01-B0326 IR. OSD: 1/24/2025SDR IPXA2025012326402Frame · dentedREF HEAVY CHECK REPAIR T3F18E0051QCB, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. ACCOMPLISHED REPAIR PER EA 757-5330-01-B0329 IR. OSD: 1/24/2025SDR IPXA2025012326492Frame · dentedREF HEAVY CHECK REPAIR T3F18E0051QFY, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. ACCOMPLISHED REPAIR PER EA 757-5360-01-B0335 IR. OSD: 1/24/2025SDR DALA2025011600398Spar · damagedSHIP 3147 SECONDARY FINDING ELONGATE HOLE (1 E/A) LOC AT LEVEL RIB 14 ON REAR SP AR UNDER FITTING AREA ON L/H WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 622832-14. (0763414)SDR VNAA20250116066Frame · corrodedFRAME AT FS 661 BOTTOM CL AFT END OF FWD CARGO COMPARTMENT IS CORRODED COMPLETELY THROUGH TO THE SHEAR TIE ON THE FRONT SIDE WITH A HOLE APPROXIMATELY 1". CORRECTIVE ACTION: CUT AWAY DAMAGED PORTION OF FRAME AND INSTALLED REPAIR PARTS IAW MHIRJ REO 670-53-31-9SDR WRXR202501161111Frame · corrodedFRAME FS879 IS CORRODED BETWEEN STRINGERS 26L AND 26R C/T KEEL BEAM ATTACHMENT FITTINGS. FOUND UPON CLEANING OF BLUE WATER SPILL. EVALUATED AREA, FRAME STATION 879, BETWEEN STR 26L-26R ORIGINAL MATERIAL .063" MATERIAL REMAINING .046" MATERIAL LOSS .017" ALLOWASDR VNAA20250116041Frame · crackedFS 333.00 FRAME IS CRACKED BETWEEN STRINGER 2R AND 3R. REPAIRED BY CUTTING OUT DAMAGED PORTION AND SPLICING IN NEW REPAIR PARTS IAW MHIRJ REO 670-53-21-2465 REV-- DATED 10-21-24SDR SWAA2025022086137Stub Frame · crackedFWD GALLEY DOOR CUTOUT; UPPER FWD STUB FRAME HFEC SURFACE INSPECTION; FOUND 1' CRACK IN STUB FRAME AT JOGGLE; .70' ABOVE SEAL DEPRESSOR. MARKED IN BLACK. REF. CARD TTG8Q00TSZ8V INSP - FORWARD GALLEY DOOR (R1) BEAR STRAP BS 290-296 BETWEEN S-8R AND S-9R - GROUPSDR SWAA2025021386454Frame · crackedCRACKED FRAME AT AFT PAX CABIN S-8R BS907.<[01] INSTALLED REPAIR PARTS AT BS907 BETWEEN S-7R TO S-9 IAW SRM 51-40-02-0G-0 AND EA NO 25-153-00138 REV A;[02] VERIFIED CORRECTIVE ACTIONSDR YENA2025011600064Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 R/H SIDE HOLE 6 (CONFIRM INDICATION USIN G BOROSCOPE) IN PASSENGER CABIN (1 EA); (RESOLVED ON W/O: 1347560 TASKCARD: NR-00031) REF AE WO 2024-413/1. N/R# 2024 - 749156 PERFORMED REPAIR ON HOLE 6 LOC. FRAMESDR YENA2025011600063Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 RH SIDE HOLE A (CONFIRM INDICATION USING BOROSCOPE) IN PASSENGER CABIN (2 EA); (RESOLVED ON W/O: 1347560 TASKCARD: NR-00032) REF AE WO 2024-413/1. N/R# 2024 - 749159. PERFORMED REPAIR ON HOLE A LOC. FRAME SDR YENA2025011600060Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 RH SIDE HOLE C (CONFIRM INDICATION USING BOROSCOPE) IN PASSENGER CABIN (1 EA); (RESOLVED ON W/O: 1347560 TASKCARD: NR-00037) REF AEM WO 2024-413/1, NR 2024-749160 ,PERFORMED PERMANENT REPAIR ON HOLE C(LEADSDR DALA2025011600360Frame · corrodedCORROSION ON FRAME BTW STA Y=851 BTW L29L TO L29R, AND STA Y=870 BTW L29L TO L29R AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00839: CORROSION LEVEL 2. CORROSION ON FRAME BTW STA Y=851 BTW L29L TO L29R, AND STA Y=870 BTW L29L TO L29R AT AFT CARGO COMPARMENT WERE RSDR DALA2025011300244Frame · crackedSHIP 3147 CRACK INDICATION ON FRAME 16 LH ON HOLE H2, DIRECTION OF CRACK IS 11 OCLOCK. CORRECTIVE ACTION: COMPLIED WITH ER/A 622250-14. (0757757)SDR IPXA2025020939803Bracket · crackedFR10 R/H SIDE HAS A CRACKED CEILING CORNER BRACKET. DOT 60-001. INSTALLED BRACKET IAW A300-600 SRM 51-40-21, HILOCK P/N: DAN5-6-4, BATCH # 0004128103.SDR CALA2025011300108Frame · crackedEA 5380-01113 REV B OP 020 - RH BS2370 PIVOT BULKHEAD FWD CHORD 1EA FASTENER HOLE FOUND CRACK. . FUSELAGE RH BS 2370 PIVOT BULKHEAD FWD CHORD REPLACED AS PER EA 5380-01113 REV B OP 024.SDR DALA2025011300271Frame · cracked-AD- CRACK ON UPPER RADIUS OF THE FRAME TAB ON THE OVERWING FRAME AT STA Y=715 LH WAS FOUND IN REF TASK CARD 5310-01436-04B JOB #079-0002, STEP 13. SUMMARY OF NRC 00397: FRAME WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G UNDER AMDS 5310-01436-03A.SDR CALA2025011300078Frame · damagedREMOVED AND RE-INSTALL APPLICABLE COMPONENTS COMMON TO FRAME 55A TO ACCOMPLISH PARTIAL FRAME REPLACEMENT. ACCOMPLISHED REPAIR OF FR55A IAW UAL ECRA 5341-01470 THIS REPAIR HAS BEEN APPROVED AS A CAT A REPAIR WITH NO ADDITIONAL INSPECTI ON REQUIRMENTS. IT IS ASDR SWAA2025022084619Frame · crackedMAIN CABIN STA 440 FRAME HAS EVIDENCE OF CRACK AROUND FASTENER OF RAIL SUPPORT BRACKET I/B OF STR 8 L/H. REMOVED DAMAGE AND REPAIRED FRAME AT STA 440 S-8L IAW EA 25-153-00218.SDR SWAA2025022084621Frame · crackedMAIN CABIN STA 380 FRAME HAS EVIDENCE OF CRACK AROUND FASTENER OF RAIL SUPPORT BRACKET I/B OF STR 8 L/H. REPAIRED PER EA 25-153-00153 TTG8Q00YDMJL;[02] REPAIRED FRAME AT BS380; BETWEEN S-7L AND S-8L; IAW EA 25-153-00153.SDR SWAA2025022084618Frame · cracked(DOT#147-48) MAIN CABIN STA 400 FRAME HAS EVIDENCE OF CRACK AROUND FASTENER OF RAIL SUPPORT BRACKET I/B OF STR 8 L/H<[01] REPAIRED FRAME AT BS400; BETWEEN S-7L AND S-8L; IAW EA 25-153-00154.;[02] VERIFIED ITEM 1<BR>C/W;[03] C/WSDR EE4Y2025010921509Frame · crackedPER CUSTOMER REQUEST A PERMANENT REPAIR SHOULD BE PERFORMED ON CENTER FUSELAGE II, FRAME 52 RH WFF RIB, FOLLOWING THE REPAIR INSTRUCTIONS IAW ETD2017-190-105548 AND SATETED IN THE COOPESA ENGINEERING ORDER COO-EO-2024-21163 R00 DTD OCT 28 2024.SDR IPXA2025012990283Frame · crackedFWD E/E COMP INSIDE COMP LH SIDE STA 457-475 FUSELAGE FRAME HAS CRACKED. OSD: 1/30/2025SDR IPXA2025012890648Frame · crackedFWD E/E COMP INSIDE COMP RH SIDE STA 457-475 FUSELAGE FRAME HAS CRACKED. 74-036 ATA CODE 53. ACCOMPLISHED REPAIR PER EO-92673-REQ1 AND VT-SAA EA 011-5310-01-B0324, REV. I/R. OSD: 1/29/2025SDR SWI2025F00389Frame · corrodedFORWARD BAGGAGE BAY FS501.00 FRAME BETWEEN STGR24L-25L CORRODED (C-CHECK RO 3/18/2025) REPAIRED FORWARD BAGGAGE BAY FS501.00 FRAME BETWEEN STGR24L-25L REF REO 690-53-31-915 REV. -- DATED 2025-02-07 COMPLIED STEPS 1 -16. COMPLIED WITH 51-900-1002-SKY. LSDR SWAA2025020584039Frame · crackedCRACK ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA 2024-779365<[01] REPAIRED FRAME ON BS 312 BETWEEN S-5L AND S-6L AT FWD GALLEY AREA IAW B737-800 EA EA-GENERAL M-22-153-01244. SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPAIRED FRAME ON BS 312 BESDR DALA2025010700150Frame · crackedSHIP 694 INITIAL. AD//AA: DURING HFEC INSPECTION CRACK AT LH RADIUS ON INNER CHORD FORWARD RETURN-FLANGE AT STGR 14L, STA 1640 WAS FOUND. CORRECTIVE ACTION: SUMMARY OF NRC 00102: FRAME BS1640 S-14 LH INNER CHORD FLANGE WAS REPAIRED PER ER/A 623028-14AD REV. ORSDR SWI2025F00187Frame · crackedFS333.00 FRAME CRACKED NEXT TO STR 2L (C-CHECK RO 2/27/2025) REPAIRED FS333.00 FRAME NEXT TO STR 2L REF REO 601R-53-21-3715 REV --(P1) DATE 2025-01-13, AND REO 601R-53-21-3715 REV -- DATED 2025-01-17. PRESSURE LEAK CHECK GOOD. SEE CONTINUATION FOR WORKSDR IPXA2025011950782Frame · brokenMDC, FRAME 38.1 R/H. P/N B53781038215, BROKEN. DOT 3325-1. LL07167. REMOVED AND REPLACED SUPPORT ON FRAME RH 38.1 PN#53781038215, IAW SRM 51-40-21 USED THE SAME FASTNERS, PAINT PN#ECL-G-101 BATCH:4340756 APPLIED TOP COAT IAW SRM 51-75-10 CUP PN# 02-012-176.SDR CALA2025011400113Frame · crackedLH DOUBLE JOGGLE FR 16 HOLE #6 HAS CRACK INDICATION IN FRAME LAYER . REPAIRED FR16 L/H DOUBLE JOGGLE HOLE #6 FRAME LAYER BY REAMING TO REMOVE CRACK IAW A319 SRM 53-11-12-300-012 PER ECRA 5311- 03320 .SDR IPXA2025011349181Frame · damagedFAULT: Z100 STR OPEN UP FLOOR PANELS, MBA SYSTEM, SIDEWALLS, AND TRANSITION PANEL TO F.O.M FS 1500 FRAME REPAIR AT STR 26R. INSTALLED SIDEWALL PANELS 162BW, 154JW IAW B757-200 SRM 51-40-02 AND INSTALLED LOWER AFT MBA SYSTEM AFT/AFT #8 AND #9, IAW B757-200 AMMSDR DALA2025010700149Frame · crackedSHIP 694 DTA MONITOR INSPECTION LOG REF ERA 623028-14 FUSELAGE / FRAME / LHS BS1640 / S-14L / INNER CHORD FLANGE / CRACK. CORRECTIVE ACTION: REF ERA 623028-14AD. (0748149)SDR DALA2025010700129Frame · cracked-AD- CRACK OF 1.00 IN ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT STA Y=696.000 RH (REF CARD 5310-01436-01D). SUMMARY OF NRC 0470: OVERWING FRAME AT STA Y=696.000 RH WAS REPLACED PER B717-200 SRM 51-41-05-0G, 51-41-02-0G, 51-41-01-0G, AND CARD 53SDR 2A6R2025010672305Frame · crackedDURING 1000 HOUR INSPECTION, CRACK DAMAGE WAS DISCOVERED ON THE LH UPPER AND RH LOWER FRAME 5 MEDICAL INTERIOR MOUNT LOCATIONS. THE CRACKS WERE LESS THAN 1.5” IN LENGTH AND FIT THE CRITERIA AND APPLICABILITY FOR THE GENERIC AIRBUS REPAIR DESIGN APPROVAL SHEETSDR 2A6R2025010672304Frame · chafedDURING 1000 HOUR INSPECTION, CHAFE DAMAGE WAS DISCOVERED ON THE FRAME 4 INNER SKIN PANEL (PN: L533M1407205). A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PROCEDURE WAS COMPLIED WITH PER AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC135-53-2024-366SDR SWAA2025020382883Frame · crackedCRACK WEB FRAME LOCATED STA 259 AND BTW STR 9L TO STR 10L AT PASSENGER CABIN 2024-773970<[01] EQUIPMENT P/N PHASEC 3D; S/N 800YBRK; DUE DATE 16-JUL-25 WAS USED ON STEP 5;[02] PERFORMED PERMANENT REPAIR ON WEB FRAME LOCATED STA 259 AND BTW STR 6L TO STR 11L AT SDR SWAA2025013182871Stub Frame · crackedCRACK STUB FRAME ON DOOR CUT OUT LOCATED STA 294.5 AND BTW STR 8R TO STR 9R AT PASSENGER CABIN 2024-773960<[01] REPLACED STUD FRAME LOC. BTW STR 7R TO STR 10R IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PARAGRAPH 9; DWG 141A8370 SHEET 9 REV D AND DWG 141SDR SWAA2025012882811Stub Frame · crackedDURING HFEC INSPECTION OF STUB FRAME FOUND CRACK ABOVE SEAL DEPRESSOR BS 291.5 + 8 WL266 L: 1.7' MARKED.<[01] REJECTED: DURING OK TO INSTALL NEW STUB FRAME; FOUND FASTENER HOLE DAMAGE OUT OF TOLERENCE AND NOT TRUE AND ROUND. LOCATED AT FSD FWD FRAME UPPER FITTSDR DALA2025010600084Frame · crackedSHIP 3147 FR20 RH DOUBLE JOGGLE INSPECTION CRACK INDICATION WAS FOUND AFFECTING HOLE #4. CORRECTIVE ACTION: REPAIRED PER ER/A 622252-14AD. (0743295)SDR AALA202504015605Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT FR 16 RIGHT HAND AND # 7 DOOR STOP FITTING. REPAIRED FRAME PER EA 361321.SDR U2RA2025020400008Spar · corrodedCORROSION DAMAGE WAS FOUND ON WING CENTER SECTION REAR SPAR WEB P/N 111U1007-1 AFT SURFACE SAT JETTISON PUMP CUTOUT. DAMAGE WAS BLENDED OUT HOWEVER THE REMOVAL MATERIAL THICKNESS WAS MORE THEN 15%OF ORIGINALSDR IPXA2024123176779Bracket · crackedAFT CARGO FRAME 54 AT Y0 HAS 1EA CRACKED BRACKET- NO DOT- SH48554 INSTALLED THE NEW BRACKET AT FR-54 Y0 IAW SRM 51-40-21. HI-LO P/N: HL18PB5-5, B/N: 0004211840, NUT PLATE P/N: ABS0337-01A, B/N: 0004352855, RIVET BLIND P/N: CCP264SS3-03, B/N: 0004336657, COLLARSDR IPXA2024123176810Bracket · crackedAFT CARGO FRAME 54 AT -Y1959 HAS 1EA CRACKED BRACKET- NO DOT- SH48554 INSTALLED BRACKET AT AFT CARGO FRAME 54 AT -Y1959IAW A300 SRM 51-40-21.SDR IPXA2024123176805Bracket · crackedAFT CARGO FRAME 54 AT Y953 HAS 2EA CRACKED BRACKETS- NO DOT- SH48554 INSTALLED BRACKET AT AFT CARGO FRAME 54 AT -Y1959 IAW A300 SRM 51-40-21.SDR DALA2025010212124Frame · corrodedAFT EQUIPMENT BAY FRAME 81 (JUST FWD OF ACCESS DOOR 867) AFT FACE HAS CORROSION BETWEEN L36-R36 (FOUND DURING INSPECTION OF ACCESS DOOR 867). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0775:2090-2106/002 00252 REMSDR 2A6R2024123072101Frame · crackedDURING 800 HOUR INSPECTION, DAMAGE TO THE FORWARD BOTTOM FRAME 1 IN THE FORM OF A CRACK WAS DISCOVERED AT LBL 195MM AND IS APPROXIMATELY 1.2” IN LENGTH. A DETAILED DESCRIPTION OF THE DAMAGE AND APPROVED REPAIR PROCEDURES ARE PROVIDED IN AIRBUS REPAIR DESIGN ASDR SWIA2025022841228Frame · damagedREMOVE/REINSTALL RH FRAME FS485 STRG. 20R TO 22R TO PROVIDE ACCESS FOR STGR. 21R REPAIR FOR JOB HN00209212 CAMP 29379424. CAMP# 29388808. (C-CHECK RO 2/26/2025) REMOVED AND INSTALLED RH FRAME WITH SPLICE REPAIR @FS485 STGR20R TO 22R IAW DRW. SH690-33224SDR U2RA2025020400006Strap · chafedDURING INSPECTION OF DATUM AIRCRAFT, CHAFING DAMAGE WAS FOUND ON BSTA 1265 FRAME STRAP PIN 65B15428-604 BETWEEN S-17R/S-18R, AT R3 MED CUTOUT.SDR REXA2024123001616Frame · corrodedFRAME FS863 BETWEEN STRINGER 27 AND 26R IS CORRODED. REPAIRED FRAME F.S.863 IAW ENDEAVOR AIR EA CRJ753-17338 REV IR DATED 10/9/2024SDR CALA2024123003187Frame · crackedAD RELATED TASK (AD 2022-08-08). TWO CRACK INDICATIONS HOLE #A A T 9 AND 3 HRS O''CLOCK POSITION IN FRAME LAYER WITH 100% FSH (BOT H) AT RH FRAME 16 UPPER DOUBLE JOGGLE AREA "REPAIR BEFORE NEXT F LIGHT". TO ACCOMPLISH INITIAL INSP OF RH FR16 UPPER DOUBLE JOGG
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