JASC 5312
Service difficulty reports · 20,045
Reports filed under 5312 · Fuselage Main, Bulkhead, 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 = '5312' 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 = '5312' 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 06FDEA04060Bulkhead · crackedRT AIR COND COMPT CRACK 2.5" LONG ON BULKHEAD AT STA 478 X = -24 Z = -39. TRIMMED CRACK AND INSTALLED FILLER AND 2 DOUBLERS IAW SRM 53-00-01 FIG 10 SHT 5 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER NR I020585/N00585 AND SRM 53-00-01 VOL 1 AND TOUCH UP SDR KCSA061542Pressure Panel · corrodedCORROSION ON UPPER SURFACE OF PRESSURE DECK WEB AT BS 1358, WL 190, LBL 112.SDR IXXA06SMN383SPressure Panel · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT MAIN LANDING GEAR WHEEL WELL PRESSURE WALL SKIN CORRODED AT STATION 902.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP, NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. SDR TRAX200601041Bulkhead · corrodedFUSELAGE STA 280 BULKHEAD, CORROSION ON WEB AND FLOOR SUPPORT ANGLES BETWEEN RBL 9 AND LBL 9. EC/TC REO 601R-53-11-926 COMPLIED WITH.SDR KCSA061539Pressure Panel · corrodedRIGHT WING GEAR WHEEL WELL UPPER PRESSURE DECK HAS CORROSION AT STA 1348, RBL 107, WL 190.SDR TRAX200601034Bulkhead · crackedSTA 280 BULKHEAD WEB CRACKED JUST OUTBOARD OF RBL 9. REMOVED AND REPLACED 280 WEB SECTION PER REO 601R-53-11-926. JOB COMPLETE.SDR TRAX200601033Bulkhead · crackedSTA 280 BULKHEAD WEB CRACKED AT LBL 9 EMERGENCY GEAR EXTENSION PULLEY BRACKET. REPAIRED DAMMAGE IAW REO 601R-53-11-126, ALL WORK DOCKUMENTED ON N/R-00138 MS7022223 JOB COMPLETE.SDR SWIA200617589Bulkhead · crackedCRACK IN CLIP ON AFT SIDE OF REAR PRESSURE BULKHEAD AT FS 625.0 LT STRINGER 15, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP PANEL 601-35012-51 P/O 71471 AT FS 625.0 LT STRINGER 15 IAW CRJ200 REO 601R-53-61-422.SDR QXEA200603090Bulkhead · corrodedC3 YYC - FLIGHT DECK BULKHEAD AT FS 280 AFT RIGHT SIDE LOWER WEB HAS CORROSION ALONG FLOOR LEVEL. REPAIRED IAW REO670-53-11-052.SDR QXEA200603089Bulkhead · corrodedC3 YYC - FLIGHT DECK BULKHEAD AT FS 280 AFT LEFT LOWER WEB HAS CORROSION ALONG FLOOR LEVEL. REPAIRED IAW REO670-53-11-052.SDR TRAX200601016Bulkhead · corrodedTHE 280 BULKHEAD WEB CORRODED - BL13-16 RT - FLOOR LEVEL. RT SIDE 280 BULKHEAD WEB ALSO FOUND CORRODED AFTER REMOVAL OF 280 FRAME, REMOVED CORROSION FROM RT AND LT WEB, REQUIRES THICKNESS CHECK. ALL WORK IAW REO 670-53-11-052 AJ21906. COMPLIED WITH EO700-53SDR DLM88060938Bulkhead · corrodedDURING CURRENT VISIT, LOWER TEE CHORD OF PRESSURE BULKHEAD WAS FOUND WITH CORROSION DAMAGE. TEE REPLACED PER EA 09-086680-12, HOWEVER REPLACEMENT CHORD HAD SHORT EDGE MARGIN CONDITIONS AT SEVERAL LOCATIONS. BOEING REPAIR STRAP INSTALLED PER 458447-14SDR SWAA064381Bulkhead · crackedDURING SCHEDULED 20Y CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 10, WL 194. REPAIRED WEB SECTION PER SRM.SDR 2006UALA02171Stiffener · crackedRH MLG WW FWD BULKHEAD VERTICAL "Z" ANGLE STIFFENER AT RBL 7 CRACKED HORIZONTALLY APPROX. 30" FROM WHEEL WELL. MAJOR REPAIR: FABRICATED AND INSTALLED U CHANNEL AND STRAP REPAIR. REFERENCE MM 57-12-96 REPAIR NR 3.SDR 06FDEA03955Bulkhead · damagedEXISTING REPAIR FOUND AT CENTER CARGO COMPT STA 1841 BULKHEAD WEB LT SNRM N00405: EXISTING REPAIR AT CENTER CARGO COMPT STA 1841 BULKHEAD WEB LT EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED PER DELTA ENGINEERING REPAIR/AUTHORIZATION 381015-14, EO 1-5100-7-5001ASDR LR7A06200Web · crackedDURING SCHEDULED C6 CHECK PER JOB CARD HC5212, FOUND CARGO DOOR REAR BULKHEAD WEB SKIN CRACKED AT FS 1041, LBL40 - RBL40. REPLACED WEB IAW SMP583 51-60 & 51-70.SDR KNNA20060001AAngle · corrodedCOMPRESSION CHORD CRACKED ON BULKHEAD OF BS 727, BL 0 (TOP) FWD WALL OF THE AFT CARGO COMPARTMENT. PROVIDE REPAIR INSTRUCTIONS ON REPAIR OF CRACKED WEB ANGLE IN WHEEL WELL AFT BULKHEAD BS 727 BL 0.SDR TRAX200601002Bracket · crackedCARGO DOOR SUPPORT BEAM PRESSURE BULKHEAD BRACKET CRACKED.SDR KCSA061491Bulkhead · damagedBS 2360 BULKHEAD WEB DAMAGED AT LBL 48, WL 275.SDR TRAX200600971Bulkhead · crackedNUTPLATE ISOLATORS ON AFT PRESSURE BULKHEAD CRACKED AT LBL 9.0 AND RBL 9.0.SDR UPS06848362Stiffener · corrodedEVIDENCE OF CORROSION FOUND ON AFT SIDE OF AFT PRESSURE BULKHEAD APPROX 18" FROM RT SIDE OF AIRCRAFT BEHIND CENTER HORIZONTAL STIFFENER. ALSO, FOUND POWDER ON TOP OF STIFFENER BELOW AREA IN QUESTION. A/C FERRIED TO SAA DEF D336666 XFER TO NRC 802138. BLENDESDR KCSA061485Bulkhead · gougedBS 2360 .5 INCH CREASE IN AFT PRESSURE BULKHEAD AT WL 203 LBL 98.SDR KCSA061484Bulkhead · damagedSTA 2360 DAMAGED AREA AT WL 213 LBL 67 AFT SIDE OF AFT PRESSURE BULKHEAD.SDR KCSA061483Web · damagedDAMAGE TO WEB AT STA 2360 WL 230 LBL 63 ON AFT SIDE OF AFT PRESSURE BULKHEAD.SDR KCSA061478Bulkhead · dentedFOUND 6 DENTS ON BS 2360 PRESSURE BULKHEAD WEB AT WL199, LBL30 TO LBL45.SDR KCSA061475Bulkhead · damagedSTA 2360 AFT PRESSURE BULKHEAD DAMAGED AT WL 320 LBL 9 AT FASTENER.SDR KCSA061473Bulkhead · dentedDENT IN BS 2360 BULKHEAD WEB AT LBL 44, WL 199.SDR KCSA061472Bulkhead · dentedTWO DENTS IN BS 2360 WEB AT LBL 96, WL 215.SDR KCSA061466Bulkhead · corrodedCORROSION ON PRESSURE DECK SPLICE AT BS 1405, WL 190 BETWEEN RBL 40 AND RBL 52.SDR SWIA200617574Bulkhead · cracked280 BULKHEAD, FRAME BELOW FLOOR IS CRACKED JUST ABOVE RADIUS AT RBL 12.0, DISCOVERED DURING C-CHECK INSPECTION. COMPLIED WITH REPAIR ON RBL12.0 PER REO 601 53-11-138.SDR SWIA200617573Bulkhead · cracked280 BULKHEAD, BENEATH FLOOR HAS 4 CRACKED CLIPS RBL 9 INBD AND OTBD, LBL 9 INBD AND OTBD, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED TWO OTBD CLIPS AT LBL9 AND RBL9 PER REO 601R 53-11-136.SDR SWIA200617572Bulkhead · cracked280 BULKHEAD, FRAME BELOW FLOOR IS CRACKED AT LBL 12.5, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER REO 601R 53-11-136.SDR DLM88060884Tee Fitting · damagedDURING THE CURRENT MTC CHECK EO 09-086680-12 WAS BEING ACCOMPLISHED AND THE REPLACEMENT PRESSURE BULKHEAD TEE CHORD WAS FOUND TO HAVE SHORT EDGE MARGIN ON EXISTING FASTENERS DURING INSTALLATION. DUE TO THIS, A TITANIUM REPAIR STRAP APPROVED BY MFG IS INSTALLESDR 06FDEA03775Bulkhead · crackedRT AIR COND COMPT FOUND 1 CRACK 2" LONG ON HORIZ BLKHD AT STA 495 X = -24. REMOVED EXISTING REPAIR IAW SRM 51-33-01 VOL 2. CUT OUT CRACKED AREA AT SUPPORT BEAM WEB. INSTALLED NEW PARTS IAW SRM 53-30-00 FIG 6 VOL 1 COMBINING DETAIL "E" AND "J" VOL 1. REINSSDR SWAA064091Pressure Panel · crackedDURING SCHEDULED 22Y CHECK, FOUND NLG W/W CEILING PANEL CRACKED AT BS 252, RBL 8. REPAIRED PANEL PER ACO.SDR KCSA061440Pressure Panel · crackedMAIN DECK PRESSURE DECK WEB CRACKED ON W/W CUTOUT BETWEEN BS 1405 AND 1410, RBL 43 TO RBL 51.SDR KCSA061462Bulkhead · dentedBS 2360 BULKHEAD WEB DENTED BETWEEN STR 38R AND STR 40R, RBL 54, W/L 200.SDR KCSA061442Bulkhead · corrodedBS 2360 BULKHEAD CORRODED FROM STR 36R TO STR 36L.SDR QXEA200602899Bulkhead · corrodedC3 YYC - FS 280 BULKHEAD LOWER WEB IS CORRODED BEHIND THE CROSSBEAM AT RBL18, 33, AND 39. REPAIRED IAW REO 670-53-11-052.SDR DL76G060888Bulkhead · crackedTHE NLG WHEELWELL, STA. 287 BULKHEAD, LBL 25 VERTICAL CHORD WAS CRACKED. THE CRACK WAS STOP DRILLED INSTEAD OF CUT OUT AS SPECIFIED IN THE SRM. THE EXISTING REPAIR WAS REMOVED AND THE CRACKED AREA CUT OUT AND A REPAIR ANGLE WAS REINSTALLED IAW THE SRM. REF ADSDR 06FDEA03738Pressure Blkhd · crackedCLG W/W FOUND 1 CRACK 1" LONG ON VERTICAL BLKHD BTWN STA 1401 STA 1381 X = 32. DISASSEMBLED PNEU DUCTS ASSY ON BLKHD IAW MM 36-14-02-04. REMOVED SENSING ELEMENT IAW MM 36-23-00-00. REMOVED RIVETS ON STIFFENERS AND ON REINFORCE DOUBLER IAW SRM 51-35-01 VOL 2.SDR DALA1102780137Bulkhead · unknownFUSELAGE NLG WHEEL WELL AFT BULKHEAD STA 287, LBL 25 CHORD, WL 173. REPAIRED IAW ERA 458240-14AD.SDR ABXA060296Bulkhead · crackedCRACK 3.5 INCH LONG AT FS 977 AFT SIDE WL 30 RIGHT ON CANTED BULKHEAD SKIN RUNNING LENGTH WISE ALONG STIFFENER. REPAIRED AREA IAW B767 SRM 53-50-51.SDR UPS06448683Pressure Panel · corrodedINSPECTION TYPE:C LEFT B/G WHEEL WELL STA 1416 I/B AREA LBL 6 UPPER PRESSURE FLOOR ATTACH SURFACE FOUND CORROSION AS MARK. CORROSION BLEND OUT 0.033" X 1/2" X 2" EXCEED SRM LIMIT. LEFT BLG WHEEL WELL BS 1416 I/B AREA PRESSURE WEB REPAIRED AS PER SRM 53-10-07SDR AWXA200601822Vertical Beam · crackedMCN - MAJOR REPAIR - C-16 CHECK - FOUND VERTICAL BEAM WEB CRACKED, BS 178, RBL 17.1, WL 185. REPAIRED VERTICAL BEAM WEB, BS 178, RBL 17.1, WL 185 IAW B737-300 SRM 53-10-08-2R12, FIGURE 201.SDR AWXA200601823Bulkhead · crackedMCN - MAJOR REPAIR - C-16 CHECK - FOUND VERTICAL BEAM WEB CRACKED, BS 178, LBL 17.1, WL 230. REPAIRED VERTICAL BEAM WEB, BS 178, LBL 17.1, WL 230 IAW B737-300 SRM 53-10-08-2R12, FIGURE 201.SDR 2006UALA02004Pressure Panel · crackedBS 663 LBL 30 WHEEL WELL PRESSURE DECK HAS 2 EA CRACKS. MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED DOUBLER AND FILLER REPAIR. REFERENCE MM53-21-98.SDR SWAA064020Pressure Panel · crackedDURING SCHEDULED 10Y CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 665, RBL 39. REPAIRED PRESSURE WEB IAW SWA EA.SDR DL76S060889Bulkhead · crackedTHE NLG BULKHEAD AFT WEB AND CHORD AT STA. 287, RBL 25 HAS DRILL DAMAGE TO THE WEB AND CHORD AND THE CHORD WAS STOP DRILLED INSTEAD OF CUT OUT AS REQUIRED PER THE SRM. THE EXISTING REPAIR ANGLE WAS REMOVED AND THE CRACKED CHORD WAS CUT OUT. THE DRILL DAMAGEDSDR KCSA061423Bulkhead · dentedFOUND 2" DENT IN BS 2360 PRESSURE BULKHEAD APPROX W/L 325, RBL 45.
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