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 SWIA201743376Isolator · crackedBS 621 PRESSURE BULKHEAD FORWARD FACE HAD NUMEROUS ISOLATOR BRACKETS CRACKED OR BENT. REMOVED AND REPLACED THE ISOLATORS WITH NEW IAW SRM.SDR SWAA2017061214218Bulkhead · crackedRT SIDE BS 540 LOWER BULKHEAD CHORD HOLE AT AFT FASTENER ROW SECOND HOLE FROM TOP FOUND TO BE CRACKED. REPAIRED CHORD IAW ER & EA.SDR FDEA201705191462Bulkhead · crackedTHE AFT NLG WW BULKHEAD IS PUNCTURED AT BL 0 APPROX WL 154, BS 395. REPAIRED IAW EA F- 5330-T0333140. MAJOR REPAIR.SDR KY7A201710180001Flange · crackedWHILE PERFORMING INSPECTIONS REQURIED BY AD 2014-06-01, FOUND A 1.5 INCH CRACK IN THE BS 69.21 BULKHEAD FLANGE BETWEEN STRINGERS 8 AND 9. THE FLANGED WAS REPAIRED.SDR 2017FA0000397Bulkhead · crackedCRACKS WERE FOUND IN THE AFT BULKHEAD AND ALL FIVE VERTICAL FIN ATTACHMENT BOLTS WERE FOUND LOOSE. THIS WAS CAUSED BY THE AFT BULKHEAD BEING UNDER DESIGNED.SDR U2RA201705180001Bulkhead Web · chafedAPU COMPARTMENT FORWARD BULKHEAD CHAFED AT BS 1885 AND RBL 6, APPROXIMATELY 8 INCHES FROM LOWER EDGE OF BULKHEAD. REPAIRED THE FIREWALL IAW SRM 53-80-08, REPAIR 2.SDR DALA2017051904025Bulkhead · corrodedCORROSION ON SKIN AT FORWARD PRESSURE BULKHEAD, BS 994 BELOW SLANT PANEL LBL 25 TO 60 AT MAIN LANDING GEAR WHEEL WELL. REPAIRED IAW ERA 558080-14AD, REV O.SDR DALA2017051704017Bulkhead · crackedHFEC INSPECTION FOUND 01EA CRACK ON LT NOSE WHEEL WELL BULKHEAD CHORDS AND REPAIRED.SDR SWIA201743426Bulkhead Web · no testFOUND REAR PRESSURE BULKHEAD WEB HAS 9 AREAS THAT FAILED NDT INSPECTION. REPAIRED THE PRESSURE BULKHEAD WEB.SDR DALA2017051604016Bulkhead · corrodedCORROSION LEVEL 2 LEFT MLG WHEEL WELL FWD SPAR BULKHEAD AT BS 955 LBL 70 FOUND CORROSION. REPAIRED PER ERA 555745-14.SDR SWAA2017051813837Pressure Panel · crackedMAIN WHEEL WELL PRESSURE WEB CRACKED AT BS 663, LBL 35. REPAIRED WEB PER SRM.SDR VNAA20170517HMV06Bulkhead Web · corrodedFS 280 BULKHEAD RT LOWER WEB IS CORRODED BETWEEN RBL 12 AND 42. REPLACED THE BULKHEAD WEB.SDR UIEA2017042600645Splice · crackedWHILE PERFORMING NDT OPEN HOLE INSPECTION ON THE BS 2598 BULKHEAD, RIGHT FWD INNER CHORD AND SPLICE FITTING, FOUND UPPER HOLE CRACKED IN SPLICE FITTING ONLY.SDR UIEA2017042600646Splice · crackedWHILE PERFORMING NDT OPEN HOLE INSPECTION ON THE BS 2598 BULKHEAD, RIGHT SPLICE FITTING AND FRAME SUPPORT FOUND UPPER HOLE CRACKED IN SPLICE FITTING ONLY . REMOVED AND REPLACED THE RT SPLICE FITTING IAW SRM 51-40-02.SDR VNAA20170517HMV05Bulkhead Web · corrodedBS 280 BULKHEAD LT LOWER WEB IS CORRODED AT LBL 12. INSTALLED A NEW LT LOWER WEB.SDR UIEA2017042600664Frame Splice · crackedWHILE PERFORMING NDT OPEN HOLE INSPECTION ON BS 2598 BULKHEAD, LEFT FWD INNER FRAME AND SPLICE FITTING, FOUND LOWER HOLE CRACKED IN SPLICE FITTING ONLY. REAMED TO .3235 IAW MESSAGE PMO-TLS-17-0015-51B.SDR SWAA2017052313930Bulkhead · crackedCENTER WING BULKHEAD WEB CRACKED AT STA 663, LBL 30 TO LBL 35. REPAIRED WEB PER EA.SDR SWIA2017062043393Bulkhead Web · gougedGOUGES NOTED ON THE BS 621 BULKHEAD WEB, FWD FACE, BELOW CARGO DOOR TRACK ALONG LBL 36.2. REPAIRED THE BULKHEAD WEB IAW REO.SDR SWIA2017062043391Bulkhead Web · crackedCRACK NOTED ON THE BS 621 BULKHEAD WEB, FWD FACE, ALONG LBL 27.5, UPPER CARGO DOOR TRACK FITTING TO WEB INTERFACE. PERFORMED PERMANENT REPAIR IAW REO. PRESSURE CHECK OF REPAIRED AREA WAS FOUND TO BE GOOD, NO LEAKS WERE NOTED IAW AMM.SDR SWAA2017051613698Pressure Panel · crackedLT WHEEL WELL VAPOR BARRIER WEB CRACKED AT BS 663, LBL 42. REPAIRED WEB PER SRM.SDR SWAA2017051713799Pressure Panel · crackedVERTICAL WEB CRACKED AT BS 663, LBL 30. REPAIRED WEB PER EA.SDR DALA2017051103818Pressure Panel · crackedSIDE BOX BEAM FLANGE AT FRAME 43 HAD A CRACK INDICATION ON LT SIDE PRESSURE PANEL. REPLACED THE PRESSURE PLATE IAW AMDS CARD 5310-01450-02SDR SIMA20170510001Stiffener · crackedFUSELAGE BULKHEAD AT BS 202.75 STIFFENER AT RBL 30 LOWER END FOUND BENT AND CRACKED. REPAIRED IAW ERS-CR-53MR-2412.SDR DALA2017051103761Bulkhead · gougedAFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR INTERNAL STRUCTURE IS GOUGED IN SEVERAL AREAS AT LOWER RT SECTION WHERE FLIGHT ATTNANTS SEAT IS MOUNTED. REPAIRED IAW SRM 52-10-02-2R, OPTION 2.SDR SWAA2017051613693Pressure Panel · crackedRT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 43.5. REPAIRED WEB PER SRM.SDR DALA2017050903827Bulkhead Web · corrodedCORROSION ON AFT PRESSURE BULKHEAD WEB, BS 1395 LONGERONS 24L-24R. CORROSION WAS REMOVED IAW ETI 90-17-021 AND ERA 556396-14, REV O.SDR AALA201706169038Pressure Panel · crackedCRACK INDICATION ON LEFT SIDE FORWARD CARGO BAY IN OPEN FASTENER HOLE, INTERNAL STRUCTURE ON LONGITUDINAL BEAM, AT FRAME 36 AND 3 INCHES OUTBOARD TO Y1292. REPAIRED THE PRESSURE PANEL IAW EO 5316Y209.SDR AALA201706169037Pressure Panel · crackedCRACK INDICATION ON LEFT SIDE FORWARD CARGO BAY IN OPEN FASTENER HOLE, INTERNAL STRUCTURE ON LONGITUDINAL BEAM, AT FRAME 36 AND 3 INCHES INBOARD SIDE TO Y1292. REPAIRED THE PRESSURE PANEL IAW EO 5316Y209.SDR AALA201706169036Pressure Panel · crackedCRACK INDICATION ON LEFT SIDE FORWARD CARGO BAY, IN OPEN FASTENER HOLE AT INTERNAL STRUCTURE ON LONGITUDINAL BEAM, AT FRAME 36 AND 1 INCH INBOARD SIDE TO Y1292. REPAIRED THE PRESSURE PANEL IAW EO 5316Y209.SDR AALA201706169035Pressure Panel · crackedAIRCRAFT IN BASE MAINTENANCE. CRACK INDICATION ON LEFT SIDE IN FORWARD CARGO BAY, IN OPEN FASTENER HOLE AT INTERNAL STRUCTURE ON LONGITUDINAL BEAM, AT FRAME 36 AND 2 INCHES OUTBOARD TO Y1292. REPAIRED PRESSURE PANEL BETWEEN FR 35 AND FR 36 PER EO #5316Y209.SDR AALA20170506003Bulkhead Web · crackedLEFT MAIN LANDING GEAR WHEEL WELL VERTICAL PRESSURE DECK WEB CRACKED AT BS 663.75, LBL31.83 TO LBL43.80. REPAIRED IAW SRM 57-10-10-2R-3 ALTERNATIVE 2.SDR AALA20170506002Web · crackedCENTER WING REAR SPAR RIGHT MAIN LANDING GEAR WHEEL WELL VERTICAL PRESSURE DECK WEB CRACKED AT FUSELAGE STATION 663.75, RBL31.83 TO RBL43.80. REPAIRED IAW SRM 57-10-10-2R-3 ALTERNATIVE 2.SDR AALA201705049028Web · crackedCENTER WING REAR SPAR IN LEFT WHEEL WELL, VAPOR BARRIER HAS A 6 INCH CRACK. ACCOMPLISHED INTERIM FIBERGLASS SEALANT PATCH REPAIR IAW SRM 57-10-10-2R-2.SDR ASOA201705031541Stiffener · crackedFWD SIDE OF BULKHEAD AT FS 202.75 FOUND INDICATION ON TOP OF STIFFENER RBL 30 APPROXIMATELY 1/4" L, STIFFENER FAILED NDT INSPECTION. REPAIRED RBL 30 POST AT FS 202.75 IAW SRM 53-11-10-201-005-A01.SDR ASOA201705031540Stiffener · crackedFWD SIDE OF BULKHEAD AT FS 202.75 FOUND INDICATION ON TOP OF STIFFENER LBL 30 APPROXIMATELY 1/4" L, STIFFENER FAILED NDT INSPECTION. REPAIRED LBL 30 POST AT FS 202.75 IAW SRM 53-11-10-201-005-A01.SDR SWAA2017050413559Bulkhead · crackedLT MAIN WHEEL WELL FORWARD BULKHEAD VERTICAL CRACKED AT BS 663. REPAIRED BULKHEAD PER EA.SDR SWIA2017050243254Bulkhead Web · crackedREAR PRESSURE BULKHEAD WEB HAS SIX CRACK INDICATIONS. REPAIRED THE BULKHEAD WEB IAW REO.SDR SWIA2017050243252Bulkhead Web · damagedBS 621 BULKHEAD WEB FAILED NDT INSPECTION AT LINTEL FITTING. REPAIRED THE BULKHEAD WEB IAW REO.SDR SWAA2017060614161Bulkhead Web · crackedMAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 45. REPAIRED THE BULKHEAD WEB IAW SRM.SDR SWAA2017060614160Bulkhead Web · crackedMAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN RBL 35 TO 45. REPAIRED THE BULKHEAD WEB IAW SRM.SDR SWAA2017051613716Pressure Panel · crackedRT MAIN WHEEL WELL SPAR VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 41. REPAIRED WEB PER SRM.SDR DALA2017050203579Bulkhead Web · crackedDURING INSPECTION, FOUND PASSENGER CABIN AREA ABOVE MLG WHEEL WILL BS 663 VERTICAL WEB IS CRACKED RBL 35 WL 199. MAINTENANCE PERFORMED A REPAIR IAW SRM 57-10-10, REPAIR 3.SDR DALA2017050203578Bulkhead Web · crackedDURING INSPECTION, FOUND PASSENGER CABIN AREA ABOVE MLG WHEEL WILL BS 663 VERTICAL WEB IS CRACKED RBL 35 WL 199. MAINTENANCE PERFORMED REPAIR IAW SRM 57-10-10, REPAIR 3.SDR ASOA201705013126Channel · crackedRIGHT CHANNEL CRACKED ON FORWARD PRESSURE BULKHEAD IN NOSE WHEEL WELL. THE CHANNEL WAS REPLACED IAW SRM 51-40-02.SDR SWAA2017050313535Bulkhead Web · crackedBULKHEAD WEB CRACKED AT BS 663, LBL 41, THREE INCHES ABOVE CENTER TANK. REPAIRED THE BULKHEAD WEB IAW SRM.SDR UIEA2017050900740Web · crackedMAIN DECK BS 1180, LBL 110 VERTICAL WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-51-2R-8, REPAIR 8.SDR UIEA2017050900741Web · crackedMAIN DECK BS 1200, LBL 110 VETICAL WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-51-2R-9, REPAIR 9.SDR UIEA2017050900742Web · crackedMAIN DECK BS 1220, LBL 110 VERTICAL WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-51-2R-5, REPAIR 5.SDR UIEA2017050900743Web · crackedMAIN DECK BS 1220, RBL 110, VERTICAL WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-51-2R-5, REPAIR 5.SDR UIEA2017050900750Barrier · crackedMAIN DECK BS 2360, RBL 55 VERTICAL BARRIER FOUND CRACKED IN TWO LOCATIONS. REPAIRED IAW SRM 51-10-02, AND 51-40-02.
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