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 QXEA2012062800587Bulkhead Web · damagedNOSE WHEEL WELL LT VERTICAL WEB HAS CRACK AND DENT AT THE UPPER CENTER FLANGE. CONFIRMED CRACK AND CONFIRMED DENT OF VERTICAL WEB IS CRACK FREE REF NTM 51-00-06-910-801 PT 1. SMOOTHED GOUGES IN HORIZONTAL WEB IAW SRM 51-14-00-02-03. MIN REMAINING THICKNESS SDR SWAA2012072306099Bulkhead · crackedVERTICAL BEAM WEB CRACKED AT BS 178, AT RBL 17. REPAIRED WEB IAW SRM.SDR SWAA2012070905631Bulkhead · crackedVERTICAL BEAM WEB CRACKED AT BS 178, LBL 17.0. REPAIRED WEB IAW SRM.SDR SWAA2012070505536Bulkhead · crackedBS 663 BULKHEAD CRACKED AT RBL 40, WL 197. REPAIRED BULKHEAD PER SRM.SDR REXA2012080101076Bulkhead · dentedFS 621 BETWEEN LBL 18 AND LBL 27 HAS SMALL DENT JUST ABOVE FLOOR LINE. REPAIRED IAW REO 601R-53-61-4755.SDR REXA2012073101075Bulkhead · damagedTWO SCREW SHANK MARKS ON FS 621 BULKHEAD. REPAIRED IAW REO 601R-53-61-2155.SDR SWAA2012071905966Pressure Panel · crackedRIGHT VERTICAL WEB CRACKED AT BS 663, BETWEEN RBL 24.75 TO RBL 45.50. REPAIRED WEB PER EA.SDR USAA2012062700011Bulkhead · crackedFORWARD PRESSURE BULKHEAD INSPECTION. BULKHEAD SKIN CRACKED AT BS 178, WL 218, RBL 17. REPAIRED CRACK IAW B737 SRM 53-10-08-2R - REPAIR 9.SDR USAA2012062700008Bulkhead · crackedFORWARD PRESSURE BULKHEAD INSPECTION. BULKHEAD SKIN CRACKED AT BS 178, WL 218 FROM LBL 5.7 TO LBL 17. REPAIRED CRACK IAW B737 SRM 53-10-08-2R - REPAIR 9.SDR REXA2012080401077Angle · crackedAFT SIDE OF FS 621 BULKHEAD LEFT OBLIQUE ANGLE IS CRACKED. REPAIRED IAW REO 601R-53-61-100 AND 601R-53-61-422.SDR GLBA201206250004Pressure Blkhd · crackedDURING A SCHEDULED ROUTINE INSP, FOUND A CRACK IN THE FWD LWR LT PRESSURE BULKHEAD AT FS 84, 2" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-034.SDR GLBA2012062500003Bulkhead · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FWD LWR RT PRESSURE BULKHEAD AT FS 84, 1" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-035.SDR SWAA2012072306098Bulkhead · corrodedPRESSURE BULKHEAD SKIN CORRODED AT BS 1016, BETWEEN STR 26L TO STR 27R. REPAIRED SKIN IAW ACO AND DWG.SDR DALA2017031402026Bulkhead Web · crackedDURING INSPECTION, FOUND AN 8 INCH CRACK IN THE VAPOR BARRIER FORWARD LOWER WALL OF RIGHT WHEEL WELL AT RBL 20. MAINTENANCE PERFORMED PERMANENT REPAIR.SDR USAA2012070300005Bulkhead · crackedFORWARD PRESSURE BULKHEAD INSPECTION, FORWARD PRESSURE BULKHEAD SKIN CRACKED AT BS 178, WL 218, FROM RBL 5.7 TO RBL 17. REPAIRED BULKHEAD SKIN IAW B737 SRM 53-10-08-2R-9 DETAIL III.SDR USAA2012070300004Bulkhead · crackedFORWARD PRESSURE BULKHEAD INSPECTION FORWARD PRESSURE BULKHEAD SKIN CRACKED AT BS 178, WL 218, FROM LBL 5.7 TO LBL 17. REPAIRED BULKHEAD SKIN IAW B737 SRM 53-10-08-2R-9 DETAIL III.SDR CA120628008Bulkhead · damaged(CAN) BULKHEAD MISSING 12 ATTACHMENT RIVETS IN AFT CANTED FRAME. NO RIVETS HAD EVER BEEN INSTALLED AT THIS LOCATION AND IT IS NOTED THAT THE ATTACHMENT OF THE FUSELAGE DORSAL FIN WOULD INTERFERE WITH THE INSTALLATION OF BULKHEAD RIVETS.SDR U2RA201206260006Splice Plate · crackedNLG WHEEL WELL BS 400 RT AFT CORNER SKIN SPLICE PLATE HAS 5 CRACKS. CRACK LENGTH .030". REF AD 2010-26-07, S/B 747-53A2305.SDR REXA2012062100931Bulkhead · crackedFS 280 BULKHEAD LOWER WEB CRACKED AT RBL 9. REPAIRED RT BULKHEAD IAW EO C53144.SDR MASA2012062534932Bulkhead · corrodedFS 280 BULKHEAD IS CORRODED AT LBL 9 AND RBL 9 DOOR POSTS. REPAIRED PER EO CL600-2C10-53-L01336, LBL 9 AND RBL 9.SDR MASA2012062234922Bulkhead · corrodedFS 290 BULKHEAD IS CORRODED AT LBL 9 AND RBL 9 DOOR POST. REPAIRED PER EO CL600-2C10-53-L01336.SDR 2012FA0000388Bulkhead · crackedDURING THE ACFT ANNUAL INSPECTION, FOUND FATIGUE CRACKS IN THE AFT FUSELAGE BULKHEAD AT STATION 332. THIS BULKHEAD IS ALSO THE WHERE THE MAIN SPARS OF HORIZONTAL STABILIZERS ATTACH. THIS IS THE SECOND HIGH TIME ACFT WE HAVE FOUND WITH THESE FATIGUE CRACKS ATSDR SWAA2012062505208Bulkhead · crackedBULKHEAD CRACKED AT BS 663, LBL 28. REPAIRED BULKHEAD IAW EA.SDR REXA2012062600866Bulkhead · damagedA DRILL START WAS NOTED AT FS621 BULKHEAD AT WL113 MEASURING 0.023 INCH DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230 REV F.SDR ASOA2012062501821Post · crackedBULKHEAD VERTICAL POST AT LBL 18 OTBD SIDE IS CRACKED IN RADIUS ON BOTTOM EDGE OF POST. REMOVED AIR FILTER FOR ACCESS IAW AMM 21-24-01-000-801. INSTALLED AIR FILTER IAW AMM 21-24-01-400-801. REMOVED AIR FILTER HSG BY REMOVING BOLTS, 8 EA FROM SUPPORT STRUCTSDR REXA2012062000861Bulkhead · chafedAFT PRESSURE BULKHEAD CHAFED JUST ABOVE FLOORBOARD. DAMAGE REMOVED IAW REO 601R-53-61-2155 RESULTING IN 0.001 INCH REMOVED.SDR ASOA2012070201848Post · corrodedFS 349 BULKHEAD POST HEAVILY CORRODED. REMOVED AND REPLACED POST IAW SRM 51-42-21 & 51-42-06.SDR U2RA201206260004Bulkhead · crackedNLG WHEEL WELL BS 400 LT AFT CORNER SKIN CHORD FOUND CRACKED. CRACK LENGTH .3". REF AD 2012-26-07, S/B 747-53A2305.SDR SWAA2012071605833Pressure Panel · crackedPRESSURE WEB CRACKED AT BS 663, RBL 32. REPAIRED WEB PER ER AND EA.SDR U2RA201206260005Splice Plate · crackedNLG WHEEL WELL BS 400 LT AFT CORNER SKIN SPLICE PLATE FOUND CRACKED. 2 EACH CRACKS, CRACK LENGTH .3", REF AD 2012-26-07, S/B 747-53A2305.SDR DALA1237659256Bulkhead · corrodedFOUND AFT PRESSURE BULKHEAD FWD FACE AT BOTTOM, Y CHORD DOUBLER CORRODED BETWEEN L28L - L29R BS 1395. REMOVED DAMAGED Y-CHORD DOUBLER, LOCATED AND DRILLED NEW DOUBLER AND INSTALLED DOUBLER IAW SRM 51-30-02 VOL II, SRM 51-30-05 VOL II, SRM 51-10-05 VOL II AND SDR SWAA2012062605316Bulkhead · crackedPRESSURE BULKHEAD CRACKED AT BS 663, RBL 35. REPAIRED BULKHEAD PER ER AND EA.SDR REXA2012070100871Stiffener · chafedFS 621 BULKHEAD AFT VERTICAL STIFFENER AT BL0 CHAFED 0.050 INCH DEEP BY 0.4 INCH LONG. REPAIRED IAW BOMBARDIER REO 601R-53-61-1523 AND 601R-53-61-4565.SDR ALGA2012061900001Bulkhead · crackedWHILE PERFORMING 100 HOUR INSPECTION, FOUND UPPER LT ATTCHMENT FITTING CRACKED AFTER REMOVING TAILBOOM FOUND AIRFRAME TO TAILBOOM BULKHEAD CRACKED ON FUSELAGE.SDR DALA1237449256Pressure Blkhd · damagedFOUND AFT PRESSURE DOME HAS DAMAGE FWD FACE LONGERON 28L TO 29R. CUTOUT DAMAGED AREA AT AFT PRESSURE DOME. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW SRM 53-10-03 FIG 1 VOL 1.SDR A6WA201240655Bulkhead · dentedBS 280 BULKHEAD DENTED IN TWO PLACES ON RT AFT INBD SIDE NEAR EDGE FROM CONTACT FROM GALLEY DOOR. CUTOUT DAMAGE ON BULKHEAD AND FABRICATED, INSTALLED REPAIR IAW REO 601R-53-11-1727, REV E.SDR COEA2012061317917Pressure Deck · corrodedHEAVY CHECK / LEVEL 2 CORROSION: RIGHT MLG WHEEL WELL PRESSURE DECK, 2ND STIFFENER 7.25 INCHES AFT OF FRAME 25 HAS AREAS OF LEVEL 2 CORROSION. REPLACED WITH OEM PART.SDR U2RA201206160002Pressure Panel · crackedLT LANDING GEAR WHEEL WELL CANTED PRESSURE DECK CLOSEOUT PANEL FOUND CRACKED. REF AD 2003-01 SB 747-51A2057. CRACK LENGTH 1".SDR CA120731004Bulkhead · cracked(CAN) BS 621, PRESSURE BULKHEAD CRACKING.SDR ASOA2012061501800Stiffener · crackedBULKHEAD STIFFNER AT RBL 26 BS 280 BULKHEAD CRACKED, FOUND DURING WEB REMOVAL. REMOVED BULKHEAD STIFFENER AT RBL 26 FS280 IAW SRM 51-42-06. DRILLED NEW STIFFENER IAW SRM 51-40-11-001-001. OK TO INSTALL MAC42QC 06/09/12. INSTALLED BULKHEAD STIFFENER AT RBL SDR QXEA2012061100450Bulkhead Web · corrodedFWD DRAFT BULKHEAD SUPPORT WEB AT STA X32.400 HAS AREAS OF CORROSION. REMOVED FWD BULKHEAD SUPPORT WEB IAW SRM 51-40-07-02-01. MATCH DRILLED AND PREPPED SUPPORT WEB FOR INSTALL IAW SRM 51-40-07-02-01 AND 51-42-05-02-01. INSTALLED NEW SUPPORT WEB IAW SRM 51-SDR REXA2012061100850Stiffener · chafedFS 621 BULKHEAD AFT VERTICAL STIFFENER AT BL0 CHAFED 0.3 INCH BY 0.1 INCH BY 0.015 INCH DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-1523.SDR UALA2012061103182Attach Bracket · gougedFR 70 RT SIDE ATTACH BRACKET AT PRESSURE BULKHEAD IS GOUGED. REMOVED DAMAGE AND INSTALLED FREEZE PLUG PER SRM AND REINSTALLED FITTING PER SRM REF WU F4400T. MAJOR REPAIRSDR REXA2012060900691Stiffener · chafedFS 621 BULKHEAD AFT VERTICAL STIFFENER AT BL0 CHAFED FROM ISOLATION VALVE 0.4 INCH BY 0.2 INCH BY 0.053 INCH DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-1523.SDR A6WA201240682Bulkhead · gougedPRESSURE BULKHEAD FS 202.75 IS GOUGED JUST OTBD OF PARKING BRAKE CONTROL CABLE PASS THRU. REPAIRED BULKHEAD IAW REO 601R-53-11-563, REV B, REPAIR TYPE V.SDR COMA2012061850046Bulkhead · crackedAFT PRESSURE BULKHEAD AT FS 621.00 AND RBL 27.00 HAS A CRACK 32.15 INCHES UP FROM WL 72.00. COMPLIED WITH PATCH REPAIR IAW BOMBARDIER GREO 601R-53-61-1285.SDR FDEA201206072123Bulkhead Web · crackedNLG WHEEL WELL LT BULKHEAD FWD CORNER HAS A CRACK IN THE WEB. COMPLIED WITH EA 8-5310-161338 AND SRM 53-30-00, FIG 6.SDR SWAA2012070205493Bulkhead · crackedVERTICAL BEAM WEB CRACKED AT BS 178, LBL 5.7. REPAIRED WEB IAW EO AND EA.SDR SWAA2012061204863Bulkhead · crackedVERTICAL PRESSURE BULKHEAD CRACKED AT BS 663, RBL 40. REPAIRED BULKHEAD PER ER AND EA.SDR FDEA201206042126Bulkhead Web · crackedLEFT MLG WW HAS A CRACK ON INBD BULKHEAD. REPAIRED IAW EA 8-5310-157338, PART 1, STEPS 1 THROUGH 4.
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