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 SWAA105011Bulkhead · crackedDURING SCHEDULED 22Y CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, BL 0. REPAIRED WEB PER SRM.SDR SWAA105010Bulkhead · crackedDURING SCHEDULED 22Y CHECK, FOUND WEB CRACKED AT BS 178, LBL 17.0. REPAIRED WEB PER SRM.SDR ASOA201001184Bulkhead · crackedVERIFY CRACK START AND STOP ON FWD SIDE OF 559. BULKHEAD AT RBL 18 POST. PERFORMED EDDY CURRENT INSP ON FWD SIDE OF PRESSURE BULKHEAD AT FS 559.00, RBL 18.0 IAW MAC NDT INSP PROCEDURE ET-2 MARKED ENDS OF CRACK. (CLOSED)SDR VGQY2010082600123Splice Plate · crackedHFEC INSP FOUND SPLICE PLATE CRACK APPROX 1 INCH ON BS 400 S45R O/B LWR CHORD OF BULKHEAD AREA. CRACKED END STOP DRILLED AS PER SRM 53-30-03 FIGURE 35 REVISION 117. HFEC INSPECTION CARRIED OUT AROUND STOP DRILL HOLE AND FOUND CRACKED CONTAINED. FABRICATED SDR COMA2010082650185Post · crackedFOUND FS 409+128 LOWER BULKHEAD OUTBOARD RBL 18 POST CRACKED AT LOWER RADIUS. REPAIRED FS 409+128 RBL 18 POST ON OUTBOARD LOWER PART OF BULKHEAD IAW BOMBARDIER REO 601R-53-41-056.SDR USAA2010092092037Bulkhead · crackedCLT - Q2 - MAJOR REPAIR - CRACK ON WEB BETWEEN VERTICAL CHORDS OF BULKHEAD AT BS 178 - 2 INCHES, RBL 28, WL 207. REPLACED WEB BETWEEN VERTICAL CHORDS OF BULKHEAD AT BS 178 - 2 INCHES, RBL 28 IAW B737 SRM 51-40-02 & BOEING DRAWING 65-45833.SDR 2010FA0000959Bulkhead · crackedCRACK FOUND ON UPPER FWD SECTION OF THE LT BULKHEAD ASSY, DIRECTLY UNDER THE PILOT`S RUDDER PEDALS. CRACK DISCOVERED DURING A 100 HR INSP.SDR CALA2010083000403Pressure Panel · corrodedB757-53-3-0449 CTN CP53-252-01. AFT WET AREA PRESSURE DECK UPPER SURFACE HAS CORROSION AT STA 1710& BL 0. REPAIRED AFT WET AREA PRESSURE DECK UPPER SURFACE AT STA 1710& BL 0. REF SRM 53-60-51 REPAIR 2 ALT 1.SDR CALA2010083000402Pressure Panel · corrodedB757-53-3-0449,CTN CP53-252-01L. AFT WET AREA PRESSURE DECK UPPER SURFACE HAS CORROSION STA 1681 AND BL 0 THRU RBL 48 SEVERAL PLACES. REMOVED CORROSION ON AFT WET AREA PRESSURE DECK UPPER SURFACE AT STA 1681 BL 0 THRU RBL 48. REF SRM 53-00-51. RBL 21 THRU SDR COMA2010082550184Angle · crackedFOUND CAP ANGLE CRACKED AT FS 559.00, LBL 18.00. COMPLIED WITH REPAIR TO PRESSURE BULKHEAD STRUCTURE FS 559.00 23L-23R IAW REO 601R-53-41-260 AND DEVIATION REO 601R-41-609.SDR COMA2010082550182Angle · crackedFOUND CAP ANGLE CRACKED IN RADIUS AT FS 559.00, RBL 18.00. COMPLIED WITH REPAIR TO PRESSURE BULKHEAD STRUCTURE FS 559.00 23L-23R IAW REO 601R-53-41-260 AND DEVIATION REO 601R-41-609.SDR CALA2010082500401Pressure Panel · corrodedAFT WET AREA PRESSURE DECK UPPER SURFACE HAS CORROSION STA 1681 AND BL 0 THRU LBL 48 SEVERAL PLACES MARKED. REMOVED CORROSION ON AFT WET AREA PRESSURE DECK UPPER SURFACE AT STA 1681 BL 0 THRU LBL 48 REF BOEING 757 SRM 53-00-51. LBL 10 - 14 INSTALLED REPAIR 2SDR C8GA2010000029Bulkhead · corrodedWHILE IN HEAVY MX PERFORMING INSP, THE INTERNAL CABIN AFT PRESSURE BULKHEAD RT STATION 1183 LOWER LOBE WEB WAS CORRODED. FABRICATED LOWER LOBE WEB FROM 2024 T3 .040" R & R LOWER LOBE, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.SDR TRBACPCP2010049Bulkhead · corrodedDURING THE SCHEDULED HEAVY CHECK INSP, CORROSION WAS FOUND ON THE FWD PRESSURE BULKHEAD WEB IN 8 AREAS. COMPLIED WITH SRI DO/TS-4275/10-13979 REF NDT REPORT AMS 100810-15 FOR HFEC AND U.T. VALUES NO DEFECTS NOTED. ACCOMPLISHED EO E2-57MR-259. COMPLIED WITH SSDR COMA2010082450181Bulkhead · crackedBULKHEAD WEB CRACKED ABOVE CARGO DOOR TRACK, AT FS 621, LBL 27.50, WL 130. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1541, REV B.SDR COMA2010082450180Bulkhead · crackedBULKHEAD WEB CRACKED AROUND LINTEL ATTACH FITTING AT FS 621, LBL 36.2. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1230 REV D.SDR SWAA104940Bulkhead · crackedDURING SCHEDULED 12Y CHECK, FOUND FWD PRESSURE BULKHEAD WEB CRACKED AT BS 663.75, RBL 36. REPAIRED WEB PER EA.SDR DALA1024730617Pressure Panel · corrodedMAIN CABIN PRESSURE DECK HAS AREAS OF CORROSION STA 1680-1685, BL0 - RBL54 ON TOP OF EXISTING DOUBLER. REMOVED AND REPLACED DOUBLER .SDR DALA1024640617Pressure Panel · corrodedCABIN SAFTEY PRESSURE DECK CORRODED AT STA 1680-1720 LBL 50. REPAIRED IAW SRM 51-60-51.SDR DALA1024580617Pressure Panel · corrodedCABIN AFT PRESSURE DECK CORRODED. INSTALLED REPAIR DOUBLER IAW SRM 51-40-02.SDR VNAA2010083000012Bulkhead · crackedDURING SCHEDULED MAINTENANCE A CRACK AT FS 559 RIGHT BULKHEAD WEB .3 IN LONG. REPAIRS WERE MADE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.SDR ASOA201001159Bulkhead · crackedBULKHEAD AT FS 202 CRACKED WHERE PARKING BRAKE COMES THROUGH. REPAIRED CRACK AT FS 202 WHERE PARKING BRAKE COMES THRU AIW REO 601R-53-11-563. OPS CHECK C/W, NO DEFECTS NOTED IAW AMM 32-45-00-710-801.SDR ASOA201001151Bulkhead · crackedREAR PRESSURE BULKHEAD WEB AFT SIDE RT FS 621 TO 625 ANGLE, STR 14 IS CRACK. REMOVED ANGLE PN 601-35012-52 IAW SRM 51-42-21, PG 19. AFTER REMOVING ANGEL, FOUND ELONGATED HOLES IN INTERCOSTAL. WAITING ENGINEERING DISPOSITION. INSTALLED NEW ANGLE PN 601-350SDR EE4Y100357Structure · corrodedFWD CARGO COMPARTMENT BULKHEAD BS 540 BTWN STR 22L AND 23L CHORD HORIZ FLANGE WITH CORROSION (THE CORROSION REQUIRES A MAJOR REPAIR).SDR IPXA10B62937Rib · crackedINSPECTION TYPE:C, RT WING L/E CAVITY RIB AT ILE 756 FOUND CRACK AT MID AREA. RT WING L/E CAVITY RIB AT ILE STA 756.95. REPAIRED IAW HXRS R57-41-36809 REV A AND EO B747-5740-39903-A. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR. ORG MAT'L IS FORGING 7075T73SDR FDEA201008183036Bulkhead · corrodedAFT PRESSURE BULKHEAD SUPPORT WEB AT STATION 1680-1720 HAS CORROSION IN SEVERAL AREAS. REMOVED AFT PRESSURE BULK HEAD SUPPORT WEB OVER 20 EA AREA (PLACES) CHECKED LIMITS ON WEB, ORIG MAT .071 REMOVED .040 FOUND TO BE OUT OF LIMITS IAW SRM 53-0051 FIG 101 DSDR BQVA2010082300007Bulkhead · corrodedSUSPECTED CORROSION FOUND DURING INSPECTION OF THE FS 580 BULKHEAD SKIN SPLICE, AREA LONGERONS AND STRINGERS 24 L/R IN ACCORDANCE WITH CMP 539540. AFTER FURTHER NDT THE AREA WAS FOUND TO HAVE MINOR SURFACE CORROSION WHICH WAS REMOVED AND TREATED. FINDINGS WSDR FDEA201008183035Web · corrodedAFT PRESSURE BULKHEAD SUPPORT WEB AT STATION 1680-STATION1720 HAS CORROSION IN SEVERAL AREAS.SDR EE4Y100338Bulkhead · corrodedLOWER FUSELAGE, FWD CARGO COMPARTMENT, STA 540 BULKHEAD BETWEEN STRINGER 22 LT AND 23 LT CHORD HORIZONTAL FLANGE WITH CORROSION. THE CORROSION REQUIRES A MAJOR REPAIR.SDR AALA20100908TUL02Bulkhead · canningOIL CANNING FOUND ON STATION 1016 AFT BULKHEAD TOP LEFT CORNER. INSTALLED REPAIR DOUBLER PER EA B737-53-012896.SDR AALA20100823TUL01Bulkhead · corrodedSTATION 1088 BULKHEAD HAS CORROSION AROUND AUXILIARY POWER UNIT INLET PLENUM. REMOVED AND INSTALLED UPPER ANGLE PER SRM 51-10-02-OG.SDR USAA2010081791699Bulkhead · corrodedMIA - C20 - MAJOR REPAIR - AFT PRESSURE BULKHEAD LOWER FORWARD WEB HAS CORROSION FROM BL 0 ANGLE STIFFENER TO LBL 6, AT BS 1016, WL 196. REPAIRED AFT PRESSURE BULKHEAD LOWER FORWARD WEB AT BS 1016 BETWEEN BL 0 TO LBL 6, WL 196 IAW TYPICAL REPAIR 53-83-01.SDR VGQY2010081600105Bulkhead · crackedDURING STA 2598 MODIFICATION, STA 2598 LT LWR BULKHEAD FOUND CRACK. COMPLIED WITH EN 1161-10.SDR COMA2010081650175Bulkhead · crackedBULKHEAD WEB CRACKED AROUND PARK BRAKE CABLE CUTOUT, FS 202.75, LBL 23.71. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-11-563 AND DEVIATION REO 601R-53-11-1958.SDR 2010FA0000830Rib · crackedCRACK FOUND NR3 RIB UPPER FLANGE, RT AND LT WING. CHRONIC PROBLEM.SDR COMA2010081350173Bulkhead · crackedAT FS 621.00 FORWARD SIDE OF THE REAR PRESSURE BULKHEAD, THE LINTLE FITTING AREA AT LBL 27.50 IS CRACKED. REPAIRED AFT PRESSURE BULKHEAD IAW REO601R-53-61-1230 REV D, DATED JULY 19, 2006.SDR A6WA201040736Bulkhead · damagedRT FS280 BULKHEAD HAS A CREASE ON AFT SIDE MEASURING 20" IN LENGTH, CREASE STARTS @ 45" ABOVE FLOOR LEVEL ON INBD SIDE AND PROTRUDES DOWN AND OTBD. REPAIRED RT FS 280 BULKHEAD WEB IAW REO 601R-53-11-1954.SDR 2010FA0000958Bulkhead · crackedCRACK FOUND ON UPPER FWD SECTION OF THE LT BULKHEAD ASSY, WHERE BULKHEAD ATTACHES TO FIREWALL. DIRECTLY UNDER THE PILOTS RUDDER PEDALS. CRACK DISCOVERED DURING A 100 HR INSPECTION.SDR SWIA201024699Bulkhead · crackedCRACK AT FS 559.0 BULKHEAD. (C-CHECK) REPAIR PER REO.SDR ASOA201001096Bulkhead · crackedFOUND FS 559 LT CAP ANGLE AT LBL 18.0 HAS INDICATION NOTED APPROX .2" IN LENGTH 80 PERCENT FSH AND FS 559 RT BULKHEAD WEB AT WL 59.10 INBD OF RBL 18.0 HAS INDICATION NOTED APPROX .2" IN LENGTH 60 PERCENT FSH, FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO 601SDR EE4Y100332Bulkhead · dentedFUSELAGE BULKHEAD BS 1016, AFT FACE, WEB DENTED AT WBL 166, RBL 7. THE DENT REQUIRES A MAJOR REPAIR.SDR A6WA201040735Bulkhead · chafedRT FS 280 BULKHEAD HAS 2 EA AREAS OF CHAFING ON INBD AFT SIDE. 1 MEASURES 2" LENGTH & 2ND MEASURES 1.5" IN LENGTH AT IS 21" FROM FLOOR. REPAIRED FS280 BULKHEAD @ RBL 11.00 BETWEEN STR 13A & STR 14A IAW REO 601R-53-11-1727.SDR SWIA201024774Bulkhead · crackedFS 621 BULKHEAD CRACKED AT LINTEL FITTING. (C CHECK) REPAIR PER REO.SDR ASOA201001092Bulkhead · crackedPERFORMED EDDY CURRENT INSP OF FWD PRESSURE BULKHEAD WEB AT FS 202.75 AT BRAKE CABLE ATTACH POINT IAW NDT INSP PROCEDURE ET.2. FWD PRESSURE BULKHEAD WEB IS CONFIRMED CRACKED AT THE 8 O'CLOCK AND 11 O'CLOCK POSITIONS LOOKING AFT AT BULKHEAD. BOTH INDICATIONS ASDR ABXA201008200117Pressure Panel · chafedPRESSURE DOME CHAFED ON TS6 BETWEEN RS18 AND RS19. BLENDED AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-80-08. REMOVED AND REPLACED TEAR STRAP USING 2024T3 .040 IAW SRM 51-40-02. REMOVED LINER TO GAIN ACCESS TO RIVETS. RE-INSTALLED LINER IAW SRM 51-40-02.SDR SWAA104714Support Angle · corrodedDURING SCHEDULED 6Y CHECK, FOUND FWD CARGO AFT CENTER BULKHEAD LOWER SUPPORT ANGLE CORRODED AT BS 500D, WL 156. REMOVED AND REPLACED ANGLE PER SRM.SDR FDEA201008102898Bulkhead · crackedCRACK COMING FROM RIVET HEAD BS 1183, BULKHEAD LBL 58 BETWEEN STR 18R TO 19R LEVEL. CUTOUT CRACKED AREA, FABRICATED REPAIR DOUBLER & FILLER & INSTALLED REPAIR PARTS AT BS 1183 LBL 58 IAW SRM 51-30-2, SRM 51-10-2 & EA 7-5310-135579.SDR AW6A201040583Pressure Blkhd · crackedFS 559, RBL 9.0 INBD SIDE CRACKED AT BOTTOM EDGE FROM LOWEST FASTENER INCORPORATED REO 601R-53-41-260 REV D DATED 09/17/09 ALONG WITH REO 601R-53-41-609 REV B DEVIATION E DATED 12/18/09.SDR QML3MR0241Bulkhead · crackedDURING OTHER MX 1 CRACK WAS FOUND IN BULKHEAD 222-031-505-001 AT ATTACHMENT POINT OF BEAM SUPPORT PN 222-031-519-103.SDR SWIA201024913Bulkhead · crackedCRACK INDICATION NOTED TO FS 559.0 PRESSURE BULKHEAD AT LT SIDE AS NOTED. (C-CHECK) REPAIRED PER REO.
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