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 CA160314012Bulkhead · cracked(CAN) DURING INSPECTION FOUND THREE CRACKS ON PRESSURE BULKHEAD BS 621, REPAIR TO BE DONE IAW GREO 601R-53-61-1285 REV D.SDR DALA2016031501938Gusset · crackedLT PYLON BULKHEAD UPPER GUSSET IS CRACKED AT BS 1022, LONGERON 7L. REPAIRED IAW SRM 51-70-11, REPAIR 1.SDR FDEA201603101193Bulkhead · crackedRIGHT STATION 1156, BULKHEAD T CAP HORIZONTAL LEG HAS A CRACK INDICATION, BETWEEN TWO FASTENER HOLES, JUST ABOVE LONGERON 39R, BELOW THE SPLICE PLATE. REPAIRED IAW SRM 53-40-00 FIG.24 VOL 2.SDR ASAA2016031016135Support Angle · corrodedFWD CARGO BAY BS 500G LOWER BULKHEAD SUPPORT ANGLE HAS AREAS OF CORROSION. ACFT GROUNDED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-30-53-1A-1, REMOVED SUPPORT ANGLE IAW SRM 51-40-02-0G-0, FABRICATED REPAIR ANGLE IAW SRM 51-40-05-0G-0, RESTORESDR 2016FA0000126Firewall · buckledUPON REMOVAL OF THE ENGINE COWL FOR MAINTENANCE, DISCOVERED THE LOWER FIREWALL SECTION IS BUCKLED & WRINKLED NEAR THE NLG REINFORCEMENT PLATE.SDR FDEA201603091192Bulkhead · crackedRIGHT STATION 1156 BULKHEAD T CAP, VERTICAL LEG HAS A CRACK INDICATION, AT THE 2ND FASTENER HOLE FROM THE TOP, ON THE OTBD SIDE OF THE BULKHEAD STIFFENER, AT X= -72.5 & LONGERON 40R. REPAIRED IAW EA 8-5310--T0324511.SDR ASAA2016030916075Bulkhead Web · crackedLEFT MLG WHEEL WELL FWD BULKHEAD WEB POSSIBLE CRACK ABOVE AILERON AUTOPILOT VALVE. ACFT GROUNDED. REMOVED DAMAGE AND ACCOMPLISHED DOUBLER REPAIR IAW SRM 57-10-10-2R-3, REPAIR 3. REPAIR 3 IS CATEGORY B WITH AN INSPECTION THRESHOLD DUE 56,000 FLIGHT CYCLES. RSDR ASOA2016030914614Angle · crackedAFT PRESSURE BULKHEAD BS 621 AFT SIDE, ONE ANGLEP CRACKED AT RBL 50, STR 14R. REMOVED AND REPLACED THE AFT PRESSURE BULKHEAD ANGLE IAW SRM 51-42-21, AND SRM 51-40-11SDR SWAA2016031149808Pressure Panel · crackedCENTER WING REAR SPAR, VAPOR WEB CRACKED, AT BS 663, LBL 34. REPAIRED WEB IAW EA.SDR SWAA2016031749978Bulkhead · crackedMAIN LANDING GEAR WW BULKHEAD WEB CRACKED AT STA 663, RBL42, WL 199. REPAIRED WEB IAW SR.SDR DALA2016030901780Bulkhead · nickedNICKS FOUND ON REAR FACE OF LOWER T-CAP AT BS 1338, P DOME, BETWEEN PROYECTION OF LONGERONS 27 LT AND 29 LT, REF CARD 4, ZONE 59 20000102603. T-CAP AT BS 1338, P-DOME BETWEEN PROYECTION OF LONGERON 23 LT AND 23 RT WAS REPLACED IAW SRM 51-30-2 AND 51-30-5 ANSDR FQAR20160307010Doubler · crackedDURING INSPECTION, A BULKHEAD DOUBLER IN THE EMPENNAGE WAS FOUND CRACKED. THE DEFECT WAS VISIBLE BY REMOVING A FAIRING THAT JOINS THE EMPENNAGE AND VERTICAL FIN AND LOOKING UP AND AFT. THE DOUBLER HAD 2 CRACKS; 1 TO THE SIDE OF THE UPPER, 2ND FROM RIGHT MOSTSDR REXA2016030600372Bulkhead · damagedFOUND REAR PRESS BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130, APPROX .500" IN LENGTH 90% FSH, FAILED NDT INSPECTION. CONTINUATION CARD 8798015 OP 33. REPAIRED REAR PRESS BULKHEAD WEB AT FS 621 IAW REO 601R-53-61-1541 REF F DATED 2014 11 12. THIS SDR REXA2016030600361Bulkhead · chafedFS 621 BULKHEAD FWD FACE HAS MULTIPLE CHAFES, FROM PANEL SCREWS ON SKIN, RIVET HEADS & Z MEMBER. CONTINUATION CARD 8798011 OP 207. REPAIRED CHAFES ON FS 621 BULKHEAD FWD FACE & Z MEMBER IAW REO 601R-53-61-2155 & SRM 51-12-00. THIS IS A MAJOR REPAIR.SDR FDEA201603051191Bulkhead · crackedLEFT STATION 1156, PRESS BULKHEAD T CAP AT LONGERON 37L, HAS A CRACK INDICATION AT THE NR 1 AFT HOLE ON THE HORIZONTAL LEG, UNDER THE SPLICE PLATE. REPAIRED IAW EA 8-5310-T0324309.SDR DALA2016030902611Frame · crackedMAIN CABIN BS 1022, LONG 7L BULKHEAD FORMER CRACKED. INSTALLED REPAIRS PARTS IAW ERA 544111-14, REV "O". REPAIRED MAIN CABIN LONGERON 7L BULKHEAD FORMER IAW ER/A 544111-14 REV ORIGINAL, BY FABRICATING -1 AND -2 REPAIR ANGLE, TAPER SHIM, AND FILLER. INSTALLESDR SWAA2016030949775Bulkhead · crackedBULKHEAD WEB CRACKED AT BS 663.75, LBL 19. REPAIRED WEB IAW EA.SDR UIEA2016030700126Bulkhead · crackedFS 48, STATION 2658, RBL 34-38, WL313, BULKHEAD WEB CRACKED. REPAIRED IAW R1-53-83-11265 REV A.SDR SIMA20160304002Stiffener · crackedFS 202.75 BULKHEAD STIFFENER POST AT LBL 30 FAILED NDT INSPECTION. FOUND A CRACK APPROX 10" LONG. PERFORMED MAJOR REPAIR TO FS 202.75 BULKHEAD STIFFENER POST AT LBL 30 IAW REO 670-53-11-1132 DATED 2016 02 23.SDR REXA2016030300398Bulkhead · crackedPRESSURE BULKHEAD FS 202.75 AT BL 23.71 IS CRACKED AT THE PARKING BRAKE CABLE PASS THROUGH HOLE. REMOVED CRACK BY PERFORMING CUT OUT & INSTALLED ALL REPAIR PARTS & COMPLIED WITH REO 601R-53-11-563.SDR WVER0303201600010Angle · damagedMULTIPLE GOUGES AND TOOLING DAMAGE ON LT FS 202.75, BULKHEAD UPPER CAP ANGLE.SDR REXA2016030200357Bulkhead · gougedFORWARD SIDE OF FS 621, BULKHEAD HAS 2 GOUGES INBD OF J6CD, TOP SECTION OF BULKHEAD APPROX 1"" LONG X .010"" DEEP. REPAIRED FS 621 BULKHEAD IAW REO 601R-53-61-5661.SDR SWAA2016030449643Bulkhead · crackedWING CTR SECTION REAR SPAR BULKHEAD CRACKED AT BS 663, LBL 36. REPAIRED BULKHEAD IAW EA.SDR SIMA20151022009Angle · crackedFS 202.75 BULKHEAD RT CAP ANGLE AT STRINGER 13R FAILED NDT INSPECTION, FOUND A 2" CRACK. PERFORMED MAJOR REPAIR TO FS 202.75, BULKHEAD RT CAP ANGLE IAW REO 670-53-11-1133.SDR REXA2016003010389Bulkhead · gougedREAR PRESS BULKHEAD FWD FACE, ABOVE FLOOR, RT LOWER SIDE, WEB IS GOUGED. CUT OUT DAMAGE & INSTALLED REPAIR IAW REO 601R-53-61-1285 REV D VIEW R.SDR SIMA20160301003Bulkhead · corrodedRIGHT LOWER BULKHEAD WEB AT FS 280.00 CORRODED. COMPLIED WITH EO CR-53MR-174 INSTALLATION OF CROSSBEAM AT FS 280.00.SDR FDEA201603010746Tee Fitting · crackedRIGHT BS 1156, PRESS BULKHEAD TEE CAP FWD FLANGE HAS A 1.5 INCH CRACK JUST ABOVE SPLICE PLATE AT LONGERON 37R. THE CRACK PROPAGATED THROUGH THE RADIUS VERTICALLY & EXTENDING BEHIND THE BULKHEAD STIFFENER AT X=88.270. REMOVED FASTENERS, CUT & REMOVED SECTION SDR LR7A2016030100767Bulkhead Web · crackedDURING FS 93, BULKHEAD REPAIRS, FOUND CANTED BULKHEAD WEB CRACKED AND TORN FROM RAPID DEPRESSURIZATION. REPAIRED IAW SMP 583, SRM FIG 51-140-17.SDR LR7A2016030100766Angle · corrodedDURING FS 93 BULKHEAD REPAIRS, FOUND LOWER BULKHEAD P/N 362755-4 ANGLE CORRODED AT NUMEROUS AREAS. REPAIR BY REPALCEMENT ACCOMPLISHED IAW SRM CH 51-60 AND 51-70, WITH MEMBERS SPLICED AT BL0, WL182.SDR LR7A2016030100764Web · crackedDURING FS93, BULKHEAD REPAIRS, FOUND LOWER WEBS CRACKED AT RADOME LATCHING POINTS. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM 51-60 AND 51-70.SDR FQAR20160301008Doubler · crackedDURING A ROUTINE INSPECTION, A DOUBLER INSTALLED ON A BULKHEAD IN THE EMPENNAGE WAS FOUND TO BE CRACKED. THE CRACKED DOUBLER WAS MADE VISIBLE BY REMOVING THE FAIRING BETWEEN THE VERTICAL FIN AND AFT FUSELAGE AND LOOKING AFT AND UP WITH A MIRROR AND FLASHLIGHT.SDR WVER0301201600008Stiffener · damagedFWD SIDE OF BULKKHEAD AT FS 202.75, LBL 30.0 STIFFNER HAS AN INDICATION .2 LONG AT THE UPPER EDGE OF FLANGE, FAILED NDT.SDR CA160301017Bulkhead · cracked(CAN) DURING C-CHECK CRACK WAS FOUND ON FS 559.0 PRESSURE BULKHEAD WEB BL 18.0 RT SIDE.SDR EPUA2016030216001Bulkhead · crackedWHILE INSPECTING ACFT IAW SEB 93-5 R1, THE ACFT WAS NOTED AS HAVING CRACKS ON BOTH LT & RT BULKHEADS AT FS 27 AT THE LOWER LIFT STRUT ATTACHMENT FITTING. IN ORDER TO REMEDY THIS CONDITION, MFG SUPPLIED SERVICE KIT SK207-19, WAS INSTALLED AS A PERMANENT REPAIRSDR FQAR20160229008Bulkhead · crackedDURING ROUTINE MAINTENANCE, A BULKHEAD AND DOUBLER WERE FOUND CRACKED IN THE EMPENNAGE. THE CRACKS WERE VISIBLE ONLY BY REMOVING THE FAIRING BETWEEN THE VERTICAL FIN LEADING EDGE AND EMPENNAGE AND SEARCHING WITH A MIRROR AND LIGHT. THE BULKHEAD AND DOUBLER ARESDR DALA2016102807817Bulkhead · corrodedAFT CARGO BAY BILGE AREA BS 813 BETWEEN LONGERON 28 AND 29R BULKHEAD HAS CORROSION. REPAIRED IAW ER/A 540745-14 REV O.SDR REXA2016022800289Bulkhead · chafedFS 621 BULKHEAD IS CHAFED IN MULTIPLE LOCATIONS, FROM CARGO LINER SCREWS. CONTINUATION CARD 8788611 OP 171 & 187. REPAIRED CHAFE IN 621 BULKHEAD IAW STEPS 1 - 12 FOR WORK PERFORMED. THIS IS A MAJOR REPAIR IAW 601R-53-61-1285 REV D 2155 REV A & - 5648.SDR REXA2016022700391Bulkhead · crackedREAR PRESS BULKHEAD IS CRACKED AT LINTLE FITTING EDGE. REPAIR REAR PRESS BULKHEAD BY LINTLE FITTING IAW REO 601R-53-61-1230 REV F.SDR REXA2016022700313Bulkhead · damagedFOUND REAR PRESS BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX .100" IN LENGTH, 50% FSH, FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-1230 REV F DATED 10 31 11. THIS IS A MAJOR REPAIR.SDR DALA2016102807816Angle · corrodedLEFT WHEEL WELL FORWARD BULKHEAD UPPER ANGLE IS CORRODED 19 INCHES OUTBOARD OF INBOARD WHEEL WELL BULKHEAD. REMOVED CORROSION, ROTOR PEENED AND RESTORED FINISH IAW ER/A 540747-14 ORIGINAL AND PRI ER/A540747-14 REV 0.SDR REXA2016022500419Bulkhead · chafedCARGO BAY AFT PRESS BULKHEAD FWD FACE ABOVE FLOOR HAS SMALL CHAFED AREAS IN 8 PLACES. REMOVED 8 EACH CHAFE MARKS & FOUND 17 EACH CHAFE MARKS TO BE WITHIN LIMITS AFTER BLEND OUT IAW REO 601R-53-61-2155 REV A . PAD UP .051" MIN REMAINING, .051" MIN ALLOWED, 06SDR P5CA2016022900045Bulkhead Web · damagedAFT PRESSURE BULKHEAD WEB DAMAGED AT BS 1582, APPROXIMATELY RBL 80, WL 270. REPAIRED IAW IAW REA MF01083R0211, REV C.SDR SWAA2016022649441Pressure Deck · crackedLEFT WW PRESS DECK WEB CRACKED AT BS 663.75, LBL 35. REPAIRED WEB IAW EA.SDR DALA2016022501397Bulkhead · crackedUPPER CABIN LT ENGINE PYLON SUPPORT BULKHEAD, BS 1022 IS CRACKED ON AFT SIDE AT LONGERON 7L. MARKED, VERIFIED WITH EDDY CURRENT. CUT OUT DAMAGE AS MARKED BS 1022 L7L IAW SRM 51-70-11, FIG 201. HFEC OF CUTOUT SHOWED NO DEFECTS IAW NOT SPM 06-10-01. 001 TAG 678SDR ASOA2016022314543Stiffener · crackedSTIFFENER ON REAR PRESSURE BULKHEAD AT LBL 36, FS 621 IS CRACKED. REMOVED CRACKED STIFFNER ANGLE ON RT PRESSURE BULKHEAD AT LBL36, FS621.00 IAW SRM 51-42-06. LOCATED, DRILLED NEW STIFFNER ANGLE IAW SRM 51-40-11. INSTALLED FASTENERS AT LBL36 FS621, REF SRM 5SDR SWAA2016030249565Pressure Panel · crackedLEFT MAIN WW SPAR VERTICAL PRESS WEB CRACKED, AT BS 663, LBL 34.5. REPAIRED WEB IAW SRM.SDR DALA2016022401588Frame · crackedDURING LFEC INSPECTION OF FWD OUTER CHORD. FUSELAGE, BS 1809.5 BULKHEAD, LT FWD OUTER CHORD CRACK AND REPAIRED IAW ERA 534310-14.SDR ASAA2016022315651Retainer · crackedFS 289 BULKHEAD SEAL RETAINER CRACKED AT T/E CAVITY. ACFT GROUNDED. R & R 1152953-2AAR FITTING IAW SRM 51-40-02. DOT REMOVED.SDR SWAA2016022649438Pressure Panel · crackedMAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, LBL 28. REPAIRED WEB IAW SRM.SDR EPUA2016022316001Bulkhead · crackedWHILE INSPECTING ACFT IAW SEB 93-5 R1, THE ACFT WAS NOTED AS HAVING CRACKS ON BOTH LT & RT BULKHEAD AT FS 27 AT THE LOWER LIFT STRUT ATTACH FITTING. IN ORDER TO REMEDY THIS CONDITION, SUPPLIED SERVICE KIT SK207-19 WAS INSTALLED AS A PERMANENT REPAIR.
Back to JASC 5312