JASC 5311
Service difficulty reports · 61,549
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 SWAA2016011247925Frame · crackedFRAME CRACKED AT BS 480. REPAIRED FRAME IAW EA.SDR SWAA2016011247924Frame · crackedFRAME CRACKED AT BS 400, STRINGER 8R. REPAIRED FRAME IAW EA.SDR DALA2015121807808Frame · crackedHFEC INSPECTION FOUND 01 EA CRACK ON LT-BS 859.5. FRAME INNER CHORD TRANSITION RADIUS IAW W/C 5311-01195-01 AND THE REPAIR WC 5311-01195-09A MUST BE ACCOMPLISHED. PRIOR TO FURTHER FLIGHT.SDR AALA20151217005Frame · wornWORN AREA ON FRAME 1510, ALONG AFT BOTTOM SIDE. INSTALLED DOUBLER ON 1510 FRAME 3" X 12" IAW WITH EA 256856.SDR TIPR2015121724350Frame · crackedFRAME CRACKED AT BS 760 BETWEEN STRINGERS 8 AND 9 RT. REPAIRED IAW SRM 53-00-07, REPAIR 1.SDR COEA2015121636811Frame · corrodedFRAME 28 HAS CORROSION ON AFT SURFACE BETWEEN STRINGERS 20L & 21L BELOW FAILSAFE ANGLE. REPLACED THE FRAME.SDR SWAA2016013048460Frame · corrodedFRAME CORRODED AT BS 500, STRINGER 26R. REPAIRED FRAME IAW ER & EA.SDR SWAA2016010547647Frame · crackedFUSELAGE FRAME CRACKED AT STATION 500C, STRINGER 20L - 21L. REPAIRED FRAME IAW SRM.SDR SWAA2016020248600Frame · crackedFORWARD GALLEY AREA, STUB FRAME WEB CRACKED AT BS 296.4, STRINGER 7R. REPAIRED STUB FRAME IAW EA.SDR REXA2015121501241Frame · corrodedFS 605.00 FRAME HAS CORROSION AT STRINGER 27. REPAIRED CORROSION DAMAGE ON FRAME AT STRINGER 27 IAW EA 253-03844.SDR ASOA2015121514265Frame · crackedPRIOR TO INSTALLING FASTENERS ON FLANGE OF FRAME 319.00 WHICH WERE REMOVED DUE TO CORROSION. MECHANIC FOUND CRACK AT VERY CORNER FASTENER HOLE. COMPLIED WITH EA 20-2015-363 P1. RECEIVED AND COMPLIED WITH FINAL EA 20-2015-363. RECEIVED AND COMPLIED WITH ECTSDR SWAA2016011347954Frame · crackedFRAME CRACKED AT BS 360, BETWEEN STRINGER 13R - 14R. REPAIRED FRAME IAW EA.SDR SWAA2015122247318Frame · corrodedFUSELAGE FRAME CORRODED AT BS 303.9, STRINGER 17L. REPAIRED FRAME IAW EA.SDR DALA2015121507676Frame · crackedUPPER RADIUS OF FRAME TAB ON OVERWING FRAME BS 962 CRACKED. REPLACED FRAME AT BS 962 IAW AMDS 5310-01375-09-RT.SDR FDEA201512144002Frame · dentedBS 231 FRAME DENT & GOUGE AT BL 0. COMPLIED WITH EA F-5310-T0322174 P 1.SDR SWAA2016010647724Failsafe · corrodedFAIL SAFE CHORD CORRODED AT BS 947.5, BETWEEN STRINGER 24R - 25L. R & R CHORD IAW SRM & DWG.SDR DALA2015121407672Frame · crackedCRACK ON FORWARD LT WHEEL WELL FRAME. REMOVED, FABRICATED AND INSTALLED FRAME IAW DWG 5930584.SDR DALA2015122107779Frame · damagedFUSELAGE FRAME HAS TWO HOLES MISDRILLED, BS 1000, RBL 10. ROUTED OUT DAMAGE ON FRAME IAW SRM 53-00-07, REPAIR 1 PERFORMED HFEC OF CUTOUT AND HFEC INSPECTION OF EXITING FASTENER HOLES IAW SRM 53-00-07, REPAIR 1 FIG 204 NO CRACKS FOUND MADE INSURANCE CUT IAW SSDR LR7A2015121200754Frame · crackedDURING SCHEDULED C-1 CHECK, UNDER JOB CARD HC5711, FOUND LT CTR WING REAR SPAR WEB CRACKED AT FS597, CWS72, WL260. REPAIRED IAW SMP 583, SRM FIG 57-30-22.SDR LR7A2015121200753Frame · warpedDURING SCHEDULED C-1 CHECK, FOUND RT AFT FUSELAGE INTERIOR BS 722 RING SEGMENT RIB WARPED. REPAIRED IAW SMP 583, SRM 51-140-21.SDR LR7A2015121200746Frame · crackedDURING SCHEDULED C-1 CHECK, FOUND BS 847 FRAME ATTACHMENT CRACKED AT WL 190, RBL 65. REPAIRED IAW SMP 583, SRM 53-50-10.SDR LR7A2015121200745Frame · crackedDURING SCHEDULED C-1 CHECK, FOUND CRACKS ON LOWER FRONT SPAR CAP. REPAIRED IAW SMP 583, SRM 57-30-22.SDR LR7A2015121200744Frame · crackedDURING SCHEDULED C-1 CHECK, FOUND CRACKS ON BS 517 LWR FRONT SPAR CAP. REPAIRED IAW SMP 583, SRM 57-30-14.SDR LR7A2015121200743Frame · corrodedDURING SCHEDULED C-1 CHECK, FOUND BS 707 RING SEGMENT CRACKED AT WL 140 - 143, RBL 70. REPAIRED IAW SMP 583, SRM 51-60 & 51-70.SDR LR7A2015121200739Frame · crackedDURING SCHEDULED C-1 CHECK, FOUND BS 517, FRONT SPAR WEB CRACKED. REPAIRED IAW SRM FIG. 57-30-22.SDR LR7A2015121200732Frame · crackedDURING SCHEDULED C-1 CHECK, FOUND RT CENTER WING BS 597 REAR SPAR WEB CRACKED. REPAIRED IAW SMP 583, SRM 57-30-22.SDR LR7A2015121200720Frame · damagedDURING SCHEDULED C-1 CHECK, FOUND BS 297 RT RING SEGMENT WITH MULTIPLE ELONGATED HOLES, WL 150, WL 160, AND WL 165. REPAIRED IAW SRM 51-140-21.SDR LR7A2015121200719Frame · corrodedDURING SCHEDULED C-1 CHECK, FOUND LT BS 357 RING SEGMENT CORRODED AT WL 140, AND ELONGATED HOLES AT WL 165 - 170. REPAIRED IAW SRM 51-140-21.SDR LR7A2015121200718Frame · corrodedDURING SCHEDULED C-1 CHECK, FOUND BS 337 LT RING SEGMENT WITH CORROSION AT WL 140, AND ELONGATED HOLES AT WL 165 - 175. REPAIRED IAW SMP 583, SRM 51-140-21.SDR LR7A2015121200717Frame · damagedDURING SCHEDULED C-1 CHECK, FOUND BS 317 LT RING SEGMENT HAD MULTIPLE ELONGATED EXCESS HOLES WL 165 - 175, AND CORROSION AT WL 140. REPAIRED IAW SMP 583, SRM 51-140-21.SDR LR7A2015121200716Frame · damagedDURING SCHEDULED C-1 CHECK, FOUND EXCESS HOLES AND ELONGATED HOLES IN LT RING SEGMENT, BS 250, WL 165 - 175. REPAIRED IAW SMP 583, SRM 51-140-21.SDR LR7A2015121200715Frame · damagedDURING SCHEDULED C-1 CHECK, FOUND LT BS 297 RING SEGMENT HAD MULTIPLE ELONGATED AND EXCESS HOLES, WL 165 - 175. REPAIRED IAW SMP 583, SRM 51-140-21.SDR LR7A2015121200714Frame · damagedDURING SCHEDULED C-1 CHECK, FOUND BS 277 LT RING SEGMENT AND REINFORCE ANGLE AT WL 160 HAD ELONGATED HOLE. REPAIRED IAW SMP 583, SRM 51-140-12.SDR LR7A2015121200713Frame · damagedDURING SCHEDULED C-1 CHECK , FOUND MULTIPLE EXCESS HOLES, WITH ELONGATED HOLES AT BS 257 LT RING SEGMENT, WL 165 - 175, LBL 70. REPAIRED IAW SMP 583, SRM 51-140-21.SDR LR7A2015121200708Frame · crackedDURING SCHEDULED C-1 CHECK, FOUND LT AFT FUSELAGE INTERIOR BS 803 BULKHEAD FRAME CRACKED AT WL 190, LBL 75, AND WL 198 - 220. REPAIRED IAW SMP 583, SRM 51-140-12.SDR LR7A2015121200700Frame · crackedDURING SCHEDULED C-1 CHECK, FOUND CABIN BS 667, LT RING SEGMENT WITH MISDRILLED HOLES AT WL 160 & WL 165, AND STRESS CORROSION CRACKING AT WL 140. REPAIRED IAW SMP 583, SRM 51-140-21.SDR LR7A2015121200695Frame · corrodedDURING SCHEDULED C-1 CHECK, FOUND CABIN BS 337 RT RING SEGMENT WITH CORROSION AT WL 140 TO 190. REPAIRED IAW SMP 583 SRM 51-140-21.SDR LR7A2015121200694Frame · corrodedDURING SCHEDULED C-1 CHECK, FOUND CABIN FS 330 RT RING SEGMENT WITH CORROSION AT WL 140 TO 141. REPAIRED IAW SMP 583, SRM 51-140-21.SDR LR7A2015121200690Frame · crackedDURING SCHEDULED C-1 CHECK, FOUND LT AFT FUSELAGE INTERIOR BS 1012 BULKHEAD OTBD CAP CRACKED. REPAIRED IAW SRM 51-60 & 51-70.SDR LR7A2015121200686Frame · crackedDURING SCHEDULED C-1, CHECK, FOUND AFT FUSELAGE INTERIOR BS 847 RING FORMER, CANTED WEB CRACKED AT WL 190, RBL 70. REPAIRED IAW SMP 583, SRM 53-50-10.SDR LR7A2015121200676Frame · crackedDURING SCHEDULED C-1 CHECK , FOUND CABIN OVERHEAD BS 617 RING SPLICE CRACKED AT LBL 20, WL 282. REPAIRED IAW SMP 583, SRM 51-60 & 51-70.SDR LR7A2015121200661Frame · crackedDURING SCHEDULED C-1 CHECK, FOUND AFT FUSELAGE INTERIOR BS 847 RING, CANTED WEB, CRACKED AT WL 190, LBL 70. REPAIRED IAW SMP 583, SRM 53-50-10.SDR DALA2015121407586Frame · corrodedSEVERAL CORROSION POINTS ON FRAME CLIPS BS 1288 FROM LONGERON 28L - 28R. FRAME CLIP AND SPLICES WERE REPLACED BY EXCESS COROOSION IAW SRM 53-03, FIG 3.SDR CA151217003Frame · corroded(CAN) DURING CHECK CORROSION WAS FOUND IN AVIONICS BAY ON ATTACHED FLANGE OF 5EA FRAMES. REMOVAL OF CORROSION WAS PERFORMED IAW SRM 51-21-06, AFTER BLEND OUT NDT INSPECTION FOR CRACKS AND REMAINING THICKNESS WAS PERFORMED WITH NO FINDINGS. FOR DETAILS OF DAMAGSDR SWAA2016020248599Frame · crackedFORWARD CARGO COMPARTMENT, FRAME CRACKED AT BS 500B, BETWEEN STRINGER 21L - 22L. REPAIRED FRAME IAW EA.SDR SWAA2016010647723Frame · corrodedFRAME WEB CORRODED AT BS 947, LBL 8. R & R FRAME IAW SRM & DWG.SDR CALA2015121494891Frame · corrodedFRAME 65, BETWEEN STRINGERS 33R & 34R, ELONGATED HOLE UNDER FASTENER. REMOVED FASTENER & FRAME CLIP FROM STRINGER 35R TO 40R, FWD SIDE IAW SRM 53-00-1 2. RESTORED PROTECTIVE FINISH IAW SRM 51-75-12, NO SRI REQUIRED.SDR DALA2015121307597Frame · corrodedCORROSION ON FRAME CLIP, BS 1520 CANT BETWEEN LONGERON 23L TO VENTRAL STAIRWAY DOORJAMB IN AFT ACCESSORY COMPARTMENT. REPAIRED IAW ETI-90-15-116 AND SRM 51-30-05, ERA 541570-14, REV O.SDR FDEA201512113978Frame · damagedFORWARD ACCESSORY COMPARTMENT INTERIOR FRAME AT BS 231.25, BL 0 HAS A HOLE WORN THROUGH RADIUS. COMPLIED WITH EA F-5310-TO322113 P1.SDR FOTR20151211001Frame · dentedFWD FUSELAGE BS 231, BL 0 FRAME IS DENTED.
Back to JASC 5311