JASC 5311
Service difficulty reports · 61,524
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 N6W2026F00001Intercostal · corrodedCORROSION ON INTERCOSTAL AT BS 349 - 364 STRINGER 26R AND STRINGER 27. R & R INTERCOSTAL AT BS 349 - 364, STRINGER 26R AND STRINGER 27 IAW SRM 51-42-06.SDR IPXA2026061936748Strap · corrodedFOUND CORROSION ON FRAME STRAP P/N 148N6613-2 STA 1885.20 S25R TO S25L. INSTALLED 1 EA NEW STRAP IAW SRM 51-40-02-0G-0 AND DWG 148N6613.SDR VNAA202606180006Frame · corrodedFS 280 J ANGLE CORRODED. REMOVED FS 280 J ANGLE IAW SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE J ANGLE ASSY IAW SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE J ANGLE ASSY IAW SRM 51-42-06-001-001-A01, & 51-4SDR VNAA202606180005Frame · corrodedFWD SIDE OF FRAME BS 319 CORRODED BETWEEN STGR 24L-25L. FRAME.SDR U2RA2026072100044Frame · crackedCRACK FOUND IN OPEN HOLE INSPECTION AT RT STA 1120 TENSION TIE FRAME WEB 65B01749-22. REPAIRS COMPLETED PER BOEING BCS CASE 06372730SDR U2RA2026072000041Frame · crackedA CRACK DAMAGED WAS FOUND ON THE FRAME WEB AT STA 1160 AND BETWEEN S-9R- 10R WHILE PERFORMING SERVICE BULLETIN 747-53A2702 REV 02. PERFORMED CLASS B REPAIR PER CASE 06372691SDR U2RA2026072000040Frame · crackedDURING OPEN HOLE INSPECTION, CRACK FOUND AT BS 800 BETWEEN S-16R & S-17R. PERFORMED PERMANENT REPAIR AIW BOEING BCS MUA-MUA-26-0081-09B AND DWG 65B26468.SDR U2RA2026072000039Frame · crackedDURING OPEN HOLE INSPECTION, 2 CRACKS FOUND AT BS800 BETWEEN S-15L TO S-17L. PERFORMED CLASS B REPAIR IAW BCS CASE # 06372411SDR SWAA2026071733143Frame · out of alignmentDOES NOT MATCH 5311-I-17336-NG WITH FIGURE 15 STEP 20 STA 328 FRAME STRAP CONFIGURATION LOCATED ON S-20R TO S-22R. AS PER EA 26-153-01613; THE CONFIGURATION IS ACCEPTABLESDR LR7A2026061603823Frame · crackedDURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5302, FOUND LH AFT RING SEGMENT CRACKED AT FS869, LBL65, WL195. REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-50-07. NR# 1001384883.SDR SWIA2026061577542Frame · corrodedEVIDENCE OF CORROSION FORMING IN MULTIPLE SMALL AREAS AT APPROX FS1015-FS1031 STGR 27-STGR 26R BETWEEN THE TAPE C-CHECK RO 10062026REPAIRED CORROSION GOUGE DAMAGE BETWEEN FS1000-1047 STGR27-21R ON THE EXTERNAL SKIN IAW MHIRJ REO 670-53-61-2740 REV-- DATED 2SDR REXA2026082601687Frame · crackedCRACK ON FRAME AT INTERNAL FUSELAGE STRUCTURE OVER FS333.00 AND BTW STGR 2L TO 2R. FRAME AT INTERNAL FUSELAGE STRUCTURE FS333.00 AND BTW STGR 2L TO 9R. WAS REPLACE PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01SDR SWAA2026071793286Frame · crackedCRACKED FRAME ON BS 947.5 BTW STR 25L TO STR 25R AFT CARGO BAY. REPLACED THE FRAME IAW SRM 51-40-02-0G-0 AND DRAWING 147A0040 SHEET 55 REV B.SDR SWIA2026061377701Frame · corrodedFRAME FS34900 HAS CORROSION ON THE LOWER FLANGE STGR26L - 26R MARKED IN RED C-CHECK RO 10132026INSTALLED NEW LOWER FRAME SECTOR FS34900 BETWEEN STGR 23LH AND STGR 24REF IAW CRJ900 SRM 51-42-06-001-001-A01 REV 38 DATED JUL 252020 AND DWG SH690-31350 REV M AND SDR SWIA2026061377657Frame · corrodedFRAME FS36400 FORWARD LOSER FLANGE HAS A PIT OF CORROSION JUST OUTBOARD OF THE INTERCOSTAL BETWEEN STGR27 AND 26L MARKED IN RED C-CHECK RO 10132026REPAIRED FRAME FS36400 FORWARD LOWER FLANGE JUST OUTBOARD OF THE INTERCOSTAL BETWEEN STGR27 AND 26L REF CRJ900 SDR SWAA2026061811667Frame · crackedCRACKED FRAME, BS 312 BTW STR 5L - STR 6L IN THE FWD GALLEY AREA. FAULT RESOLVED ON OTHER FAULT IAW SWA MPM 52.2.5 SEE TTG8Q01C77VD.SDR DALA2026061203550Frame · dentedDURING WALK AROUND FOUND DENT ON RH FWD FUSELAGE 100 MM AFT RADOME FRAME. RELEASED PER A330 SRM 53-00-11-283-011 FIG 002 ITEM 19// REPAIR DEFERRED FOR 200 FC FROM ACTUAL FLIGHT. (8179333) AIRCRAFT WAS GROUNDED.SDR DALA2026061203549Frame · dentedDURING WALK AROUND FOUND DENT ON RH FWD FUSELAGE 180 MM AFT RADOME FRAME. RELEASED PER A330 SRM 53-00-11-283-011 FIG 002 ITEM 19// REPAIR DEFERRED FOR 200 FC FROM ACTUAL FLIGHT. (8179332) AIRCRAFT WAS GROUNDED.SDR DALA2026061203548Frame · dentedDURING WALK AROUND FOUND DENT ON RT FWD FUSELAGE 40 MM AFT RADOME FRAME. RELEASED PER A330 SRM 53-00-11-283-011 FIG 002 ITEM 19// REPAIR DEFERRED FOR 200 FC FROM ACTUAL FLIGHT. (8179331) AIRCRAFT WAS GROUNDED.SDR SCNA20260715302Frame · crackedWO 94270 NR00210: CRACK IN FRAME AT STA 312 & BTW S-5L & S-6L, PASSENGER CABIN. - - CRACK IN FRAME AT STA 312 & BTW S-5L & S-6L, PASSENGER CABIN WAS REPAIRED PER B737-800 SRM 53-10-07-2R-1 REPAIR 1.SDR SCNA20260715300Frame Angle · corrodedCORROSION FRAME CLIP (4EAS) ON STA 500H AND STGR26L TO 26R, (2EAS) ON STA 500G AND STGR 28L TO 26R, (1EA) ON STA 500C AND STGR 28R TO 27R, (2EAS) ON STA 500B AND STGR 27L TO 27R, (1EA) ON STA 500A AND STGR 28L TO 27L, (1EA) ON STA 500 AND STGR 28R TO 27R AT FWSDR SCNA20260625263Frame · crackedCRACK IN FRAME AT BS 312 & BTW S-5L & S-6L, PASSENGER CABIN. CRACK IN FRAME AT BS 312 & BTW S-5L & S-6L, PASSENGER CABIN WAS REPAIRED PER SRM 53-10-07-2R-1 REPAIR 1.SDR CALA2026061117005Frame · damagedAFT CARGO BAY AT FR. 1520 RT SIDE BTWN STRG 23 - 24 ON FREE FLANGE AREA FOUND 2EA HOLES. REPAIR ACCOMPLISHED PER UAL ECRA 5360-02166 AND VT MAE EA 757-5360-13-A4511 REV -SDR JR2R20260609242Frame · corrodedUPON REMOVAL OF SHEAR TIE AT FR88 BETWEEN STR27R AND STR28R, FOUND FRAME CORRODED ON THE AFT SIDE AND ON THE LOWER FLANGE BOTTOM SIDE. REPAIRSDR SWIA2026060876804Frame · corrodedA-BAY FRAME AT BS 333 APPROXIMATE STR 18L CORRODED NEAR GROUNDING STUDS. REMOVED AND INSTALLED NEW A-BAY FRAME AT FS333 BTWN STR 18L - STR 21L IAW SRM 51-42-06-001-001-A01, SRM 51-42-021-001-001-A01, AND DWG SH670-31810, REV AE. PERFORMED PRESSURE LEAK TEST OSDR VNAA202607120017Frame · damagedFOLDED FRAME (FS1015.00) BTW STGR 17L TO 19L ON LOWER SURROUND STRUCTURE AT AFT BAGGAGE BAY DOOR. FOLDED FRAME (FS1015.00) BTW STGR 17L TO 19L ON LOWER SURROUND STRUCTURE AT AFT BAGGAGE BAY DOOR WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 AND SRM 51-42-SDR DALA2026060803427Frame · corrodedCORROSION LEVEL 2 IN FRAME STA 1440 BTW S-30 TO S-29R AND BWT S-29L TO S-28L AT AFT CARGO COMPARTMENT. FRAME STA 1440 BTW S-30 TO S-29R AND BWT S-29L TO S-28L AT AFT CARGO COMPARTMENT WAS REPLACED PER B757-300 SRM 51-40-02-0G PAR. 4, B AND PAR. 7, D. (LP 163SDR DALA2026060903491Frame · corrodedCORROSION ON FR81 INNER AND OUTER SURFACES APPROX. 4 IN FROM STRINGER 19L TOWARD RT (INTERCOASTAL LOWER FR80-81) AT AFT EQUIPMENT COMPARTMENT DOOR CUTOUT SURROUND STRUCTURE (MARKED). REMOVED AND REPLACED FRAME AT FR 81 BETWEEN STRINGER 17R TO STRINGER 18L PER SDR DALA2026060903490Frame · corrodedWHILE WORKING ON FR81 INNER AND OUTER SURFACES DAMAGE ON CC# 00187, FOUND FR80 WITH CORROSION BETWEEN LBL 7 AND RBL7. REMOVED AND REPLACED FRAMES AT FR 80 L/H AND R/H SIDE OF BELLY PER A220 ASRP BD500-A-J51-42-20-00AAA-078A-A AND BOMBARDIER DWG C01401201 REV RSDR ABXR2026060400009Frame · corrodedCORROSION AT STA. 1219 RBL22 "J" FRAME FOUND TO BE OUT OF LIMITS IAW B767 SRM 53-00-511.SDR SWAA2026070608713Frame · crackedCRACKED FRAME, BS 312, STR 5L - 6L AT FWD GALLEY AREA. REPAIRED THE FRAME IAW EA M-22-153-01244.SDR IPXA2026061741991Frame · gougedFRAME 1380 RT SIDE HAS MULTIPLE GOUGES TO THE FRAME INNER CHORD (EXTERIOR RADIUS) BETWEEN S-25R TO S-27R. ACCOMPLISHED THE CATEGORY B REPAIR PER EO-97741-REQ1 AND VT-MAE EA 757-5360-27-A4515 REV.SDR DALA2026060103335Frame · noneERA 593799-14AD FUSELAGE FRAME STA 1460 & STRINGERS 23L-27L, EXISTING REPAIR. REF ERA 593799-14AD. (1621334) AIRCRAFT WAS GROUNDEDSDR SWIA2026052977179Frame · chafedBS 654. 50 FRAME HAD CHAFE DAMAGE AT THE AFT INBD EDGE, APPROX 015 LONG AND 035 DEEP, BTWN STR 13R & 14R. REPAIRED BS 654. 50 IAW REO 601R-53-61-8548, REV -. COMPLETED SKYCARD 51-900-1003-SKY. NO WEIGHT CHANGE. SEE CONTINUE CARD FOR DETAILS OF WORK PERFOSDR CALA2026060316787Frame · dentedJACKSCREW COMP FUSELAGE FRAME STA 1064 DENTED AT S16L - S17. TRIMMED DAMAGED AREA AND INSTALLED REPAIR ON FUSELAGE FRAME BS 1064 BTWN S16L - 17L REF. TRIMMED DAMAGED AREA AND INSTALLED REPAIR ON FUSELAGE FRAME REPAIR TO THE INNER CHORD FREE FLANGE OF THE STA SDR FDEA202605290658Frame · crackedRH CENTER BOX REAR SPAR FR47 BOTTOM PANEL "D" HOLE FOUND CRACKED SIGNAL. REPAIRED THE "D" HOLE ON RH CENTER WING BOX REAR SPAR FR47 BOTTOM PANEL PER EA 6- 5710-T0387476 P1. EA TITLE: WINGS - BASIC WING STRUCTURE - CRACK HOLE D AT FR47 RHS DURING SB57-6086 SDR DALA2026052803237Window Frame · crackedAIRCRAFT 3241, CRACK INDICATION FOUND IN FASTENER HOLE LOCATED AT THE RH FR4 LATERAL WINDOW UPPER JUNCTION. CRACK DEPTH = 0.079 INCHES, CRACK DIRECTION 2 O CLOCK. IN COCKPIT. AA NUMBER 5311-01236-02. AD RELATED, WORK CARD 531 1-01236-02. CORRECTIVE ACTION: PERSDR SWIA2026052777196Frame · corrodedBS 319 FRAME WAS CORRODED BTWN STR 20L - 21L. REMOVED AND REPLACED THE FRAME IAW SRM 51-42-21 & 51-42-06. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY. NO WEIGHT CHANGE.SDR SWIA2026052776212Frame · damagedREWORK - DAMAGE ON AFT SIDE OF FRAME 89 BETWEEN STRINGERS 27R - 28R. REPAIRED DAMAGE ON FRAME 89, BETWEEN STRINGERS 27R-28R, BY CUTTING OUT DAMAGED AREA AND THEN INSTALLING A FABRICATED FILLER, DOUBLERS, AND SPLICES REF ETD2026-170-009364.SDR SWAA2026063006488Frame · crackedBS 312 FRAME CRACKED WL 283 LBL 35 ABOVE FWD ENTRY UPPER SILL WEB. ACCOMPLISHED REPAIR OF FRAME AT BS 312, WL 283, LBL 35, BTW S5L AND S6L IAW EA M-22-153-01244.SDR SWAA2026062906534Frame · crackedCRACK INDICATION ON FRAME WEB SURFACE AROUND FASTENER LOCATED AT BS 328 BETWEEN S-20R TO S-21R IN AVIONIC BAY. REPAIRED WITH THE REPLACEMENT OF FRAME AND STRAP LOCATED AT BS 328 BETWEEN S-19R TO S-27R IN AVIONIC COMPARTMENT IAW EA 26-153-01437-WIP1 AND EA 26-SDR SWAA2026061106481Frame · damagedFWD CARGO LT SIDE FRAME AT BS 500D, STR 25L HAS ELONGATED NR 13 HOLE.THE HOLE IS MEASURED 0.187 WIDE BY 0.262 LENGTH. WORK ACCOMPLISHED PER EA 26-153-01419.SDR SWAA2026061106480Frame · damagedFWD CARGO LT SIDE FRAME AT BS 500C, STR 25L HAS ELONGATED NR 13 HOLE. THE HOLE SIZE IS MEASURED 0.187 WIDE BY 0.277 LENGTH. WORK IS ACCOMPLISHED IAW EA 26-153-01416.SDR 2A6R2026052675602Frame · chafedCHAFING DAMAGE WAS DISCOVERED ON ACSN 0493 AT THE RH FRAME 4 INBOARD SKIN. THE DAMAGE MEASURES APPROXIMATELY 0.062” TALL BY 0.175” WIDE WITH A MAXIMUM DEPTH OF .032” (THRU THICKNESS). A DETAILED DESCRIPTION OF THE DAMAGE REPAIR AND APPROVED REPAIR PROCEDURES ASDR 21GA2026052623805Frame · crackedCRACK FOUND IN CENTER WING REAR SPAR AT STATION 953 BBL 1RSDR UIEA2026041900221Frame · noneAFT CARGO STA 1800 FRAME WEB NEAR STR 38R - STR 40R FOUND UNIDENTIFIED EXISTING REPAIR(<P>EXISTING REPAIR PART REINSTALLED AS PER BOEING NCR 408271F. NO FURTHER DEFECTS NOTED</P>)SDR SWAA2026062505438Stub Frame · crackedCRACK INDICATION ON STUB FRAME LOCATED BETWEEN BS 294.5 TO BS 296.5 AND BETWEEN S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 0.250 IN. APPROX.AT PASSENGER CABIN. REPLACED STUB FRAME LOCATED ON BS 296.5 BETWEEN STR 7R AND STR 9R UPPER POSITION AT FWD GALLSDR CALA2026052116440Frame · dentedAFT CARGO BAY BS 1220, STR 26L , FRAME HAS DENT ON FREE FLANGE AREA. REPAIR PARTS FABRICATED. ACCOMPLISHED BS 1220, STR 26L FRAME REPAIR IAW ECRA 5360-021 45 AND VT MAE EA 757-5360-13-A4444 REV-.SDR SWIA2026051977209Frame · corrodedFWD SIDE OF FRAME 559.112 HAS EVIDENCE OF CORROSION BTWN STR 26L - 26R. REMOVED DESCREPANT FRAME ANGLE LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-06, 51-42-21, 51-23-00, 51-25-06, 51-25-00 .SDR 4VAA202605190019Frame · chafedDURING INSPECTION, CHAFE DAMAGE WAS FOUND AT THE FORWARD CARGO DOOR RAIL FRAME. THE FORWARD CARGO DOOR RAIL FRAME WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060682.
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