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 96ZZZM420Blkhd Beam · crackedDURING C-CHECK, FOUND CABIN FS 1183 LBL 27 VERTICAL BEAM HAS APPROXIMATELY 10 INCH CRACK STARTING APPROXIMATELY 48 INCHES ABOVE FLOOR LEVEL. STOPPED DRILL .25 DIAMETER HOLES STATION 1183 LBL 27 IAW REF SRM 51-10-1 AND S/B 727-53-0182. NDT CHECKED STOP DRILLESDR 96ZZZM417Blkhd Beam · crackedDURING C-CHECK, FOUND CABIN STATION 1183 BULKHEAD VERTICAL BEAM HAS 4 INCH LONG CRACK COMING FROM FLOOR AT LBL 37. DRILLED .25 IN DIAMETER STOP HOLE AT CRACK END PER SRM 51-10-1 REF S/B 727-53A-0173. INSTALLED REPAIR PER SB 727-53-0173 AND BOEING DRAWING 65CSDR 96ZZZM416Blkhd Beam · crackDURING C-CHECK, FOUND CABIN FS 1183 RBL 37 BULKHEAD VERTICAL BEAM HAS CRACK INDICATION AFT INBOARD FLANGE IN RADIUS 29 INCHES ABOVE FLOOR LEVEL. STOP DRILLED CRACK PER SB 727-53-0192. HFEC INSPECTED STOP DRILL HOLES AND NO FURTHER CRACK PROGRESSION NOTED IAWSDR 9513969946Bulkhead · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION BETWEEN THE LONGERON 29L AND 30 ATTACH CASTINGS AND THE FS 756 BULKHEAD. REPLACED BOTH CASTINGS PER SRM 51-01 AND DWG 3911418.SDR RAAAE895023Bulkhead · damagedDURING SCHEDULED NR 4 CHECK, FOUND FS -200 PRESSURE BULKHEAD DENTED, GOUGED AND RIVET HEAD DAMAGED AT RBL 34. REMOVED DAMAGED AREA INSTALLED DOUBLER PER SRM 51-31-1, FIGURE 1, SHEET 2. (X)SDR DLL13953648Fitting · crackedCOMPLYING WITH INSPECTION SI 7-66332-12 AND AD T95-18-52, FOUND STRINGER TO AFT P-DOME SPLICE FITTING CRACKED AT STRINGER NR 11. SCHEDULED THE FITTING REPLACEMENT PER DL ERA 271759-14.SDR DLL10954528Blkhd Fitting · crackedDURING ACCOMPLISHMENT OF AN INSPECTION OF THE AFT PRESSURE BULKHEAD STR SPLICE FITTINGS PER SI 7-66332-12, THE STR 4 AND 8 FITTING WERE FOUND TO BE CRACKED. REPAIRED PER DL ERA 271738-14AD.SDR DLL10953630Fitting · crackedCOMPLYING WITH AD T95-18-52, DL INSPECTION SI 7-66332-12, AFT P-DOME TO STRINGER SPLICE FITTINGS WERE FOUND CRACKED AT STRINGERS NR 4 AND NR 8. THE FITTINGS WERE SCHEDULED FOR REPLACEMENT.SDR EISA95310Bulkhead · crackedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE AFT BULKHEAD CENTER PANEL, FORWARD CARGO PIT HAS CRACKED AND TORN FASTENER HOLES IN BOTTOM END OF PANEL. DRESSED OUT CRACKED AND TORN AREA. FABRICATED AND INSTALLED TWO DOUBLERS IAW B727 SRM 51-4SDR DLL10954530Blkhd Fitting · crackedDURING ACCOMPLISHMENT OF AN INSPECTION OF THE AFT PRESSURE BULKHEAD STR SPLICE FITTINGS PER SI 7-66332-12, THE STR 8 AND 58 FITTINGS WERE FOUND TO BE CRACKED AND COMPLETELY SEVERED. REPAIRED PER DL ERA 272751-14AD.SDR DLL13954213Blkhd Cap · crackedPREVIOUSLY STOP DRILLED CRACKS IN NLG W/W AFT BULKHEAD ARE EXTENDED BEYOND THOSE STOP DRILLS. ACCOMPLISHED REPAIRS PER DL ERA 271754-1AD.SDR DLL12953700Blkhd Web · crackedWHILE REPLACING A LEFT WHEELWELL FIBERGLASS PANEL ATTACH ANGLE LOCATED ON THE FS 1363 BULKHEAD, A 1.5 INCH CRACK WAS FOUND ON THE FS 1363 BULKHEAD WEB UNDER THE PANEL ATTACH ANGLE. THE DAMAGE WAS REPAIRED PER SRM 53-11-00, PG 949 .SDR DLL12953646Fitting · crackedCOMPLYING WITH INSPECTION SI 7-66332-12 AND AD T95-18-52, FOUND STRINGER TO AFT P-DOME SPLICE FITTING CRACKED AT STRINGER NR 58. THE FITTING WAS SCHEDULED FOR REPLACEMENT.SDR DLL10953645Fitting · crackedCOMPLYING WITH INSPECTION SI 7-66332-12 AND AD T95-18-52, FOUND STRINGER TO AFT P-DOME SPLICE FITTINGS CRACKED AT STRINGERS NR 8, 10 AND 58. THE FITTINGS WERE SCHEDULED FOR REPLACEMENT PER DL ERA 271733-14AD REV D.SDR DLL10953644Fittings · crackedCOMPLYING WITH DL INSPECTION SI7-66332-12 AND AD T95-18-52, FOUND STRINGER TO AFT P-DOME SPLICE FITTINGS AT STRINGERS NR 5, 10 AND 61 CRACKED. THE FITTINGS WERE SCHEDULED FOR REPLACEMENT.SDR RRXA95005Bulkhead Doubler · corrodedCORROSION ON FRAME AND BULKHEAD AT Y= 680 TO 683 BETWEEN LONGERONS L35L TO L35R. REMOVED FRAME SECTION, SPLICE AND DOUBLERS. FABRICATED AND INSTALLED REPAIR ANGLES TO FRAME AND REPAIR DOUBLER TO BULKHEAD IAW COTNEY ENGINEERING ORDER SKA 95148-3 AND SRM 51-1-SDR DLL13954200Blkhd Fittings · crackedDURING THE ACCOMPLISHMENT OF AN INSPECTION OF THE AFT PRESSURE BULKHEAD STRINGER SPLICE FITTINGS PER SI 7-66332-12, THE STR 11 FITTING WAS FOUND TO HAVE CRACKS, IT IS 7075-T6 FORGED AL. ACCOMPLISHED REPAIRS PER DL ERA 271759-14AD.SDR DL72S953573Bulkhead · crackedINSIDE VENTRAL STABILIZER AT STA 1303, BULKHEAD LOWER VERTICAL WALL ABOVE S-DUCT HAS CRACK AT LT CORNER. CRACK WAS FOUND AT HMV, REPAIRED PER SRM 53-10-4 FIG 17.SDR MWEA95273Blkhd Skin · crackedCRACK IN AFT PRESSURE BULKHEAD SKIN AT 6 O'CLOCK POSITION BELOW PLUG DOOR JAMB 1.083 LONG. REMOVED EXITING REPAIR, VERIFIED LENGTH OF CRACK AND INSTALLED REPAIR IAW 51-30-2 AND 51-30-5.SDR MWEA95272Blkhd Skin · crackedTWO CRACKS IN AFT PRESSURE BULKHEAD SKIN AT RECEPTACLE HOLE, APPROXIMATLY 1 O'CLOCK POSITION .25 INCH AND .75 INCH LONG. STOP DRILLED CRACK AND INSTALLED REPAIR TO THE TWO CRACKS IAW SVC RWK 5934886-509.SDR DLL10953687Fitting · crackedCOMPLYING WITH DL INSPECTION SI 7-66332-12, AND AD T95-18-52, AFT P-DOME TO STRINGER SPLICE FITTINGS WERE FOUND CRACKED AT STRINGERS NR 8 AND NR 58. FITTINGS WERE SCHEDULED FOR REPLACEMENT.SDR ABXA9500864Blkhd Web · crackedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 84-07-04 AND 90-18-03, AND SB 53-174 REV 3, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT FOUR HOLES AT THE TEE SPLICE PLATE ABOVE FRP, RIGHT SIDE. REPAIRED IAW DC-9 SB 53-174.SDR 96ZZZM523Press Blkhd · crackedDURING C-CHECK, FOUND 5 INCH BY 2 INCH LONG CRACKS IN AFT PRESSURE BLKHD. REPAIRED PER DOUGLAS SRM 53-2-5.SDR UPS804269Bulkhead · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT MLG WHEEL WELL AFT PRESSURE BULKHEAD, B/S 980 AT LONGERON 31R CORRODED BEYOND LIMITS. REPAIR BULKHEAD B/S 980 AT LONGERON 31R IAW DC8-5310-7307A.SDR DLL10953686Fitting · crackedCOMPLYING WITH DL INSPECTION SI 7-66332-12 AND AD T95-18-52, AFT P-DOME TO STRINGER SPLICE FITTINGS WERE FOUND CRACKED AT STRINGERS NR 5 AND NR 10. FITTINGS WERE SCHEDULED FOR REPLACEMENT.SDR DLL10953631Fitting · crackedCOMPLYING WITH DL INSPECTION SI7-66332-12 AND AD T95-18-52, FOUND STRINGER TO AFT P-DOME SPLICE FITTINGS CRACKED, AT STRINGERS NR 8, 10, 56, 58 AND 61. FITTINGS WERE REPLACED.SDR DLL10953527Blkhd Fittings · crackedDURING ACCOMPLISHMENT OF AN INSPECTION FOR THE AFT PRESSURE BULKHEAD, THE STR 58 AND STR 61 FITTINGS WERE FOUND TO BE CRACKED. THE FITTINGS ARE TO BE RELEASED ON A TIME LIMITED BASIS AND WILL BE REPLACED WITHIN 150 FLIGHT CYCLES, PER DL ERA 271719-14.SDR DL72S953548Blkhd Stiffener · crackedAT CV3 IN ATL, A CRACK WAS FOUND EMANATING FROM THE BOTTOM OF THE LT FLANGE ON THE FS 1183 BULKHEAD VERTICAL STIFFENER AT RBL 8. THE CRACK WAS 1 INCH LONG. REPAIRED DAMAGE PER DL ERA 302413-14AD. AUTHORIZED BY B727-53-0175 REV. 2.SDR CAL950798Blkhd Chord · crackedGSO - INSPECTION FOUND A 1.5 INCH CRACK IN BS 727 BULKHEAD LEFT OUTBOARD CHORD AT STRINGER 18A. THE CHORD WAS REMOVED AND REPLACED IAW EA 5310-01638, OPERATION NR 2. (M)SDR CAL950795Blkhd Chord · crackedGSO - INSPECTION FOUND A 1.5 INCH CRACK IN BS 727 BULKHEAD RIGHT OUTBOARD CHORD AT STRINGER 18A. THE RIGHT OUTBOARD CHORD WAS REMOVED AND REPLACED IAW EA 5310-01638. (M)SDR ABXA9500863Blkhd Web · crackedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 81-26-03, 90-18-03 AND SB 53-147 REV 7, ASB 53-147 REV 4, FOUND CRACKS ON THE AFT PRESSURE BULKHEAD WEB AT SPLICE ABOVE LONGERON 13R AND 11R. REPAIRED IAW ABX REA D953-12628-SB.SDR DLL10954542Blkhd Web · crackedTHE FUSELAGE STATION 1363 BULKHEAD CAP AND WEB ARE CRACKED BETWEEN STRINGERS 47 AND 48 AT APPROX WL 160. REPAIRED PER DL ERA 271718-14.SDR DLL10953688Fittings · crackedCOMPLYING WITH DL INSPECTION SI 7-66332-12 AND AD T95-18-52, AFT P-DOME TO STRINGER SPLICE FITTINGS WERE FOUND CRACKED AT STRINGERS NR 8 AND NR 58. FITTINGS WERE SCHEDULED FOR REPLACEMENT.SDR DLL10953647Fitting · crackedCOMPLYING WITH INSPECTION SI 7-66332-12 AND AD T95-18-52, FOUND STRINGER TO AFT P-DOME SPLICE FITTINGS CRACKED AT STRINGERS NR 5 AND NR 58. FITTINGS SCHEDULED FOR REPLACEMENT PER DL ERA 272720-14.SDR SWAA950599Blkhd Web · crackedDURING SCHEDULED 1/4 D-CHECK, FOUND CRACKS AT BS 178 BULKHEAD WEB AT LBL 5.7 AND RBL 5.7, ALONG SIDE I/B ROW OF FASTENER HOLES BETWEEN WL 207 AND 218. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR ABXA9500869Blkhd Plate · gougedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 84-07-04 AND 90-18-03 AND SB 53-174 REV 3, FOUND RIGHT AFT PRESSURE BULKHEAD SPLICE PLATE GOUGED. REPLACED SPLICE PLATE IAW DC-9 SRM 53-11-3 AND 51-30-5.SDR ABXA9500868Blkhd Plate · gougedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 84-07-04 AND 90-18-03 AND SB 53-174 REV 3, FOUND RIGHT AFT PRESSURE BULKHEAD SPLICE PLATE GOUGED. REPLACED SPLICE PLATE IAW DC-9 SRM 53-11-3 AND 51-30-5.SDR ABXA9500867Blkhd Plate · gougedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 84-07-04 AND 90-18-03 AND SB 53-174 REV 3, FOUND LEFT AFT PRESSURE BULKHEAD SPLICE PLATE GOUGED. REPLACED SPLICE PLATE IAW DC-9 SRM 53-11-3 AND 51-30-5.SDR ABXA9500866Blkhd Plate · gougedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 84-07-04 AND 90-18-03 AND SB 53-174 REV 3, FOUND LEFT AFT PRESSURE BULKHEAD SPLICE PLATE GOUGED. REPLACED SPLICE PLATE IAW DC-9 SRM 53-11-3 AND 51-30-5.SDR 9513339163Bulkhead · corrodedDURING H-CHECK, FOUND AFT PIT FORWARD BULKHEAD LOWER CHORD CORRODED IN SEVERAL AREAS AT FS 642 BETWEEN LONGERONS 28L AND 28R. SPLICED IN NEW SECTION OF T-CHORD PER EA 91-097635.SDR DLL13953489Blkhd Angle · crackedRAPID DEPRESSURIZATION 33,000 FEET, SOURCE UNKNOWN. LOUD BANG, UNABLE TO REGAIN CONTROL OF PRESSURIZATION. ABLE TO HOLD CABIN ALTITUDE TO 7,000 AT A/C ALTITUDE OF 14,000, RETURNED TO LAX. FOUND AFT PRESSURE P-DOME CHORD ANGLE THAT ATTACHED P-DOME TO FUSELAGSDR ABXA9500865Blkhd T-Cap · gougedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 84-07-04 AND 90-18-03 AND SB 53-174 REV 3, FOUND LEFT AFT PRESSURE BULKHEAD T-CAP AFT SIDE GOUGED. BLENDED IAW DC-9 SRM 51-01 FIG 1.SDR 9513309607Bulkhead · crackedDURING ACCEPTANCE CHECK, FOUND HORIZONTAL STIFFENER TO FRAME CRACKED AT FS 996 AFT PRESSURE BULKHEAD. FABRICATED AND INSTALLED REPAIR ANGLE PER EA 96-098097.SDR DLL10954183Blkhd Skin · oversized holesWHILE ACCOMPLISHING RE-WORK OF 1363 BLKHD, SEVERAL HOLES THROUGH THE FUSELAGE SKIN AND THE MOD DOUBLERS UNDER THE CAP WERE FOUND WITH OVERSIZED FASTENER HOLES ON THE LT SIDE, REPAIRED IAW DL ERA 271609-14AD.SDR DL72S953886Bulkhead · fastener subWHILE ACCOMPLISHING EO 4-40130-3AD, AFT ENTRY DOORWAY AND BODY STATION 1183 BULKHEAD REINFORCEMENT, SEVERAL FASTENERS CALLED FOR BY THE DRAWING, COULD NOT BE INSTALLED DUE TO FRAME INTERFERENCE. THESE FASTENERS WILL BE SUBSTITUTED TO FACILITATE THE MODIFICATISDR DL72S953462Blkhd Doubler · trimmmedDURING ACCOMPLISHMENT OF BACO S/B 727-53-0055, R9, REINFORCEMENT OF THE BS 1183 BULKHEAD AS MANDATED BY AD 90-06-09. WHILE ACCOMPLISHING MODIFICATION TO THE BS 1183 LT AFT DOOR FRAME, THE DOUBLER WAS TRIMMED INADVERTENTLY. IN ACCORDANCE WITH BACO TWX-DAL-ATLSDR 9513029163Bulkhead · crackedDURING H-CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AROUND PERIMETER OF PLUG DOOR OPENING. STOP DRILLED CRACK AT LOWER LEFT RADIAL NR 16. REPAIRED RIGHT UPPER RADIAL PER SB 53-127.SDR SWAA950609Blkhd Strap · crackedDURING SCHEDULED 1/4 D-CHECK, FOUND WEB AND STRAP CRACKS AT BS 178 BULKHEAD, INBOARD ROW OF FASTENERS, LBL 5.7 FROM WL 184 TO 201. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950608Blkhd Web · crackedDURING SCHEDULED 1/4 D-CHECK, FOUND WEB AND STRAP CRACKS AT BS 178 BULKHEAD, INBOARD ROW OF FASTENERS, RBL 5.7 FROM WL 184 TO 201. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950607Blkhd T-Chord · crackedDURING SCHEDULED 1/4 D-CHECK, FOUND TWO CRACKS AT T-CHORD BS 178 BULKHEAD AFT SIDE, WL 184, ONE I/B AND ONE O/B. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
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