JASC 5312
Service difficulty reports · 20,047
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 CALA0400053Bulkhead · canningINSPECTION FOUND AFT PRESSURE BULKHEAD WEB REPAIR LIFTING OFF AT EDGES AT STA 1016. INSTALLED INTERIM REPAIR PER PART 1 OF ECRA 5311-01174. A DIP WAS ISSUED TO REINSPECT THE REPAIR AT INTERVALS NOT TO EXCEED 12,000 CYCLES.SDR DL73S040070Bulkhead · corrodedCORROSION WAS NOTED ON THE BS 1016 PRESSURE BULKHEAD, AT BL 0 AND AFFECTED BOTH THE WEB AND CHANNEL STIFFENERS. CORROSION WAS REMOVED AND DAMAGE REPAIRED PER ERA 385929-14.SDR SWAA040234Stiffener · crackedDURING SCHEDULED C2 CHECK, FOUND AFT PRESS BULKHEAD ZEE STIFFENERS CRACKED AT 12 AND 7 O'CLOCK POSITIONS. REPAIRED STIFFENERS PER SRM.SDR SWAA040233Cap · crackedDURING SCHEDULED C2 CHECK, FOUND AFT PRESS BULKHEAD AT BS 1016, CRACKED AT CENTER CAP. REPAIRED PER EA.SDR SWAA040222Bulkhead · corrodedDURING SCHEDULED SERVICE CHECK, FOUND BULKHEAD WEB CORRODED AT BS 1016, BL 0. REPAIRED WEB PER ACO.SDR AWXA200400117Bulkhead · crackedLCQ - MAJOR REPAIR - DURING C-15 CHECK A .5 INCH CRACK WAS FOUND IN BS 178 BULKHEAD VERTICAL BEAM WEB AT RBL 17.1, WL 228. MAINTENANCE STOP DRILLED CRACK IN BS 178 BULKHEAD VERTICAL BEAM WEB AT RBL 17.1, WL 228; PERFORMED A HFEC INSPECTION TO VERIFY CRACKS COSDR AWXA200400139Beam · crackedLCQ - MAJOR REPAIR - DURING C-15 CHECK A .125 INCH CRACK WAS FOUND AT TOOLING HOLE OF BS 178 BULKHEAD VERTICAL BEAM LBL 5.7, WL 178. MAINTENANCE ENLARGED TOOLING HOLE TO NEXT SIZE AND PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; INSTALLED SOLID RIVET SDR AWXA200400132Pressure Panel · crackedMCN - MAJOR REPAIR - DURING C-13 CHECK A .125 INCH CRACK WAS FOUND ON PRESSURE WEB AT BS 665, LBL 30, WL 203. MAINTENANCE CUT OUT CRACKED SECTION OF WEB AT BS 665, LBL 30, WL 203; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-60-SDR CALA0400033Pressure Panel · crackedINSPECTION FOUND A 1.5 INCH CRACK IN RIGHT PRESSURE DECK AT STA 664. REPAIRED PRESSURE WEB DECK IAW SRM 53-60-51, FIGURE 203 AND ECRA 5312-01024.SDR SWAA040144Support · corrodedDURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO COMPARTMENT BULKHEAD CENTER LOWER SUPPORT CHORD CORRODED AT BS 948. REPAIRED PER SRM.SDR SWAA040143Pressure Panel · crackedDURING SCHEDULED 1/2D CHECK, FOUND PRESSURE DECK CRACKED AT BS 663, LBL 30. REPAIRED PRESSURE DECK PER SRM.SDR AUS20040392Bulkhead · cracked(AUS) FUSELAGE BULKHEAD CRACKED IN AREA DESCRIBED IN AD/CESSNA180/75AMDT2. CRACK LENGTH APPROXIMATELY 38.1MM (1.5IN). AD IS NOT APPLICABLE TO THIS MODEL AIRCRAFT.SDR ABXA040045Bulkhead · crackedFITTING BELOW UPPER HINGE INSIDE AFT PRESSURE BULKHEAD DOOR WAS CRACKED. REPLACED DOOR FITTING IAW DC-9 SRM.SDR GTIA040120Stanchion · crackedFTW - FOUND MID PIT BULKHEAD FRAME STANTION IS CRACKED LEFT. STOP DRILLED CRACK. FABRICATED REPAIR ANGLES. INSTALLED REPAIR ANGLES. (M)SDR CALA0400032Pressure Panel · damagedINSPECTION FOUND DAMAGE TO THE PRESSURE DECK WEB AT STA 665 TO 675, RBL 35 TO 45. THE PRESSURE WEB DECK WAS REPAIRED IAW ECRA 5312-01023.SDR C2XA04SH013Firewall · crackedDURING C CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RT MOUNT. MAINTENANCE REMOVED AND REPLACED THE APU FIREWALL IAW EA 5340-01016. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR GTIA040074Door Frame · corrodedFTW - FOUND AFT PRESSURE BULKHEAD DOOR JAMB THRESHOLD SEAL TORN. AFTER REMOVED TORN SEAL FOUND CORROSION. CUT OUT DAMAGED AREA AT LOWER AFT DOOR JAMB. FORMED DOUBLER. FABRICATED FILLER. INSTALLED DOUBLER AND FILLER. (M)SDR USAA04000BBulkhead · crackedFOUND WEB CRACKED .5 INCH, BULKHEAD WEB BS 178, WL 218, RBBL 5.7. INSTALLED DOUBLER PER EO 5300V153. (M)SDR ASAA0410011Pressure Panel · damagedOKC - DURING SCHEDULED D-CHECK, FOUND THE PRESSURE WEB AT FUSELAGE STATION 260.5, STRINGER 27L HAS ELONGATED HOLES. REPAIRED WEB PER SRM AND EA. (M)SDR ASAA0410009Fitting · crackedOKC - DURING SCHEDULED D-CHECK, FOUND THE BULKHEAD FITTING AT FUSELAGE STATION 727, RIGHT BUTTOCK LINE 45.5 CRACKED. REPLACED FITTING PER EA. (M)SDR DHL2004753502Pressure Panel · crackedDURING C-CHECK, NOSE SECTION LWR LOBE INTERIOR PRESS WEB AT BS 294S PREVIOUS CRACK REPAIR DO NOT MEET SRM. REMOVED PREVIOUS REPAIR AT NOSE SECTION LWR LOBE INT PRESS WEB BS 294 IAW B-727 SRM 51-30-2. CUT OUT DAMAGED IAW B-727 SRM 51-40-2 FIG 3. REPAIR DOUBLSDR 0400109906Channel · crackedDURING L-CHECK FOUND CRACK IN AFT PRESSURE BULKHEAD CHANNEL. REPAIRED IAW EA 99-197419.SDR USAA04000ABulkhead · crackedFOUND BULKHEAD WEB CRACKED .5 INCH, 178 BULKHEAD WEB AT LOWER LT RADAR ANTENNA MOUNT. REPAIRED PER DRAFT EA 77664 PATCH AND SRM 53-10-08 FIG 211. (M)SDR 0400186740Bulkhead · corrodedDURING H-CHECK FOUND CORROSION ON LOWER BULKHEAD CHORD AT BS 1000 S 41L. REPAIRED PER EA 67-165093.SDR 0467400018Bulkhead · corrodedDURING H-CHECK FOUND CORROSION ON LOWER BULKHEAD CHORD AT BS 1000 S 41L. REPAIRED PER EA 67-165093.SDR MWEA030500Bulkhead · crackedLOWER LT VENTRAL DOOR CORNER WEB IS CRACKED. INSTALLED DOUBLERS TO BOTH LOWER DOOR CORNERS OF THE AFT PRESSURE BULKHEAD.SDR SWAA032833Pressure Panel · crackedDURING SCHEDULED PM CHECK, FOUND NLG W/W LT SIDEWALL CRACKED BELOW ACCESS PANEL AT BS 247. REPAIRED WEB PER SWA EA.SDR CALA0300723Bulkhead · corrodedINSPECTION FOUND CORROSION ON APB WEB FORWARD FACE IB OF S27L ALONG LOWER RIVET ROW AT STA 1016. THE CORRODED SECTION OF WEB WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-80-08 AND MFG DRAWING NR 65C28106-1.SDR AWXA200400013Beam · crackedLCQ - MAJOR REPAIR - DURING C-17 CHECK A .5 INCH CRACK WAS FOUND AT 2 INCH HOLE ON BS 178 BULKHEAD RT VERTICAL BEAM WEB RBL 17.1, WL 192.5. MAINTENANCE CUT OUT DAMAGED AREA ON BS 178 BULKHEAD VERTICAL BEAM WEB RBL 17.1, WL 192.5; FABRICATED A NEW SECTION OF WSDR AWXA200400012Beam · crackedLCQ - MAJOR REPAIR - DURING C-17 CHECK A .25 INCH CRACK WAS FOUND AT INSULATION HOLE ON BS 178 BULKHEAD VERTICAL BEAM WEB RBL 17.1, WL 183. MAINTENANCE CUT OUT DAMAGED AREA ON BS 178 BULKHEAD VERTICAL BEAM WEB RBL 17.1, WL 183; FABRICATED A NEW SECTION OF WEBSDR C2XA03SH515Firewall · crackedSHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO CRACKED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 135 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 2003UALA00983Bulkhead · damagedSTA. 178 VERTICAL WEB AT RBL 5.7 HAS TOOLING MARKS IN UPPER SECTION. MAJOR REPAIR ACCOMPLISHED. REPLACED WEB.SDR ASAA0380836Bulkhead · gougedOAK - DURING 15K CHECK, FOUND AFT PRESSURE BULKHEAD TEE IS GOUGED ON FORWARD SIDE. SPLICED IN NEW TEE SECTION PER EA 5310-02288. (M)SDR DL767031124Panel · gougedTHE GORE PANEL ON THE AFT P-DOME WAS FOUND WITH A GOUGE NEAR STIFFENER 11R. THE GOUGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 087997-14AD.SDR DL767031122Panel · crackedINSPECTION OF THE AFT P-DOME GORE PANELS PER AD 88-19-03 REVEALED A CRACK AT A FASTENER LOCATION COMMON TO THE STIFFENER 13R LAP JOINT. THE CRACK WAS REMOVED WITH A CUTOUT TO THE GORE PANEL AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 088005-14AD.SDR DL767031121Lap Joint · crackedDURING INSPECTION OF THE AFT P-DOME AT FS 1582 A CRACK WAS FOUND AT A FASTENER COMMON TO THE STIFFENER 5L WEB LAP JOINT. THE CRACK WAS REMOVED BY TRIMMING OUT THE LAP JOINT. THE CUTOUT WAS REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 088021-14AD.SDR ARWA20031207Bulkhead · corrodedNR 970. DURING (C) CHECK INSPECTION, NLG WW RT TUNNEL STATION 8.000 PRESSURE BULKHEAD FORWARD FACE. NOSE LANDING GEAR RT FITTING WITH CORROSION AT L-31.SDR DL76S031113Bulkhead · bird strikeTHE WEB OF THE FWD PRESSURE BULKHEAD AT FS 132.5 WAS PUNCTURED AS A RESULT OF A BIRD STRIKE BETWEEN LBL 10.6 & 16. THE VERTICAL BEAMS AT LBL 10.6 & 16 WERE DENTED. THE DAMAGED AREA OF WEB WAS REMOVED WITH A CUTOUT AND THE DENTED FLANGES OF THE BEAMS TRIMMED SDR WVE2003F00026Bulkhead · crackedLT PRESSURE BULKHEAD WEB AT FS1098, BL3441, STR8-9, FOUND TO BE CRACKED. CUT OUT DAMAGED WEB. PERFORMED AN EDDY CURRENT INSPECTION TO ENSURE ALL DAMAGE WAS REMOVED AND NO CRACKS EXIST. NO INDICATIONS FOUND. WET INSTALLED FABRICATED FITTING PN 670-53-61-026SDR DL73S031089Bulkhead · corrodedCORROSION WAS FOUND ON THE AFT PRESSURE BULKHEAD AT BS 1016 AND BL 0, BETWEEN S26L AND 26R. CORROSION WAS REMOVED THEN REPAIRED PER ERA 385921-14AD.SDR COMA0360553Bulkhead · chafedRIGHT FORWARD SIDE OF FS 621 BULKHEAD IS CHAFED AT FOUR LOCATIONS. REMOVED FASTENERS, BLENDED OUT DAMAGED AREAS, PERFORMED EDDY CURRENT INSPECTION, ALODINED AND INSTALLED FASTENERS IAW WVAC EO 601R-53-4466.SDR COMA0360549Bulkhead · chafedTHE RT FORWARD SIDE OF THE AFT PRESSURE BULKHEAD AT FS 621 IS CHAFED .012 INCH DEEP X .150 INCH WIDE AT RBL 36, WL 103. THE DAMAGE WAS CAUSED FROM BAGGAGE BAY LINER HARDWARE BEING TOO LONG. THE DAMAGED AREA WAS REMOVED AND REPAIR PARTS WERE FABRICATED AND INSDR C2XA03SH495Firewall · crackedDURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE APU FIREWALL IAW EA 5340-01015 AND EMB 145 SRM 53-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SWAA032695Bulkhead · crackedPAE - DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 178.5, LBL 24, WL 207. REPAIRED PER SRM. (M)SDR SWAA032678Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT BL 0. REPAIRED WEB SECTION PER SWA EA.SDR DHL2003742536Bulkhead · crackedDURING C-CHECK, BS 1183 BL 36 RT WL 237 FWD SIDE BULKHEAD HAS VERTICAL BEAM IS CRACKED IN RADIUS. STOP DRILLED CRACK & INSTALLED REPAIR KIT 65C34406-13 PO 3348157 PER S/B 727-53-0192 & DRAWING 65C34406.SDR DHL200342536Bulkhead · crackedDURING C-CHECK , N/R 60796 BS 1183 BL 36 RT WL 237 FWD SIDE BULKHEAD HAS VERT BEAM IS CRACKED IN RADIUS. STOP DRILLED CRACK & INSTALLED REPAIR KIT 65C34406-13 PO 3348157 PER S/B 727-53-0192 & DRAWING 65C34406.SDR LR7A03110Pressure Panel · crackedDURING SCHEDULED B3 INSPECTION PER JOB CARD HB5301 FOUND FS 517 RT MLG WHEEL WELL SKIN CRACKED AT BELLY SKIN ATTACHMENT RBL 35, WL 126. REPAIRED IAW SRM SMP 583 51-140-12. NR 2018.SDR LR7A03109Pressure Panel · crackedDURING SCHEDULED B3 INSPECTION PER JOB CARD HB5301 FOUND FS 517 LT MLG WHEEL WELL SKIN CRACKED AT BELLY SKIN ATTACHMENT LBL 35, WL 126. REPAIRED IAW SRM SMP 583 51-140-12. NR 2017.SDR DHL2003742525Bulkhead · crackedDURING C-CHECK, AFT PRESS BULKHEAD BS 1183 BS 1183 VERTICAL BEAM LBL 36 CRACKED IN THE RADIUS WL 249. REPAIRED BS 1183 VERTICAL BEAM LBL 36 USING KIT 65C34406-12 PO 3348172 IAW B-727 S/B 727-53-0192 REVISION AND DWG 65C34406.
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