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.

SDR SWIA201126630Bulkhead · crackedFS 621 BULKHEAD CRACKED ABOVE UPPER CARGO DOOR TRACK FITTING. (C-CHECK) REPAIR PER REO.Jun 25, 2011 · N948SW · Cndair CL6002B19SDR VNAA2011062600027Bulkhead · crackedDURING SCHEDULED MAINTENANCE IT WAS FOUND THE FS 202.0 BULKHEAD HAD A CRACK ADJACENT TO THE HOLE WHERE PARKING BRAKE CABLE PASSES THROUGH. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Jun 25, 2011 · N220PS · Cndair CL6002B19SDR VNAA2011062600026Bulkhead · crackedDURING SCHEDULED MAINTENANCE THE FS 559.0 RIGHT BULKHEAD WEB WAS FOUND CRACKED. THE FS 559.0 BULKHEAD WEB WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Jun 25, 2011 · N220PS · Cndair CL6002B19SDR SWAA2012052104153Bulkhead · crackedBULKHEAD WEB CRACKED AT BS 663 , RBL 35. REPAIRED WEB PER EA AND ER.Jun 24, 2011 · N735SA · Boeing 7377H4SDR UIEA2011062400338Fitting · crackedCRACKS WERE FOUND ON THE EXTENSION FITTING, SKIN, BULKHEAD CHORD, OUTER CHORD SPLICE FITTING, BULKHEAD WEB AND WEB SPLICE PLATE. CORROSION WAS ALSO FOUND ON THE INBD SIDE OF THE LOWER BULKHEAD CAP FITTING.Jun 24, 2011 · N517MC · Boeing 747243BSDR REXA201100411Bulkhead · damagedFS 621 BULKHEAD IS DAMAGED FROM SCREW CONTACT AT WL 102.5 LBL 17.5 AND 27. AREA APPEARS TO BE PREVIOUSLY REPAIRED. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.Jun 24, 2011 · N8896A · Cndair CL6002B19SDR REXA201100410ABulkhead · damagedFS 621 BULKHEAD IS DAMAGED FROM SCREW CONTACT AT WL 86, RBL 7.5. DAMAGE IS APPROX 0.125" LONG X 0.125" WIDE X 0.003" DEEP. REPAIRED IAW REO 601R-53-61-2155.Jun 24, 2011 · N8896A · Cndair CL6002B19SDR REXA201100399Bulkhead · scratchedFS 621 BULKHEAD IS SCRATCHED AS WL 140, RBL 16. DAMAGE IS APPROXIMATELY .5" LONG X 0.010" WIDE X 0.003" DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.Jun 24, 2011 · N8896A · Cndair CL6002B19SDR ASAA1149957Support Angle · crackedAFT PIT AFT BULKHEAD LOWER SUPPORT ANGLE CORRODED. REMOVED CORROEDED ANGLE. FABRICATED AND INSTALLED NEW ANGLE IAW B737 400 SRM 51 40 02 FIG.2.Jun 23, 2011 · N771AS · Boeing 7374Q8SDR ASAA1149956Support Angle · corrodedAFT PIT AFT BULKEAD LOWER SUPPORT ANGLE CORRODED. REMOVED CORRODED ANGLE, FABRICATED AND INSTALLED NEW ANGLE IAW B737 400 SRM 51 40 02 FIGURE 2.Jun 23, 2011 · N771AS · Boeing 7374Q8SDR ASOA201101229Bulkhead Web · failedFOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX 1" IN LEGNTH 100 PERCENT FSH FAILED NDT INSPECTION. REPAIRED IAW EC/TC REO 601R-53-61-1230.Jun 23, 2011 · N973EV · Cndair CL6002B19SDR ASOA201101236Isolator · brokenREAR PRESSURE BULKHEAD FWD FACE HAS 6 BROKEN ISOLATORS. INSTALLED NEW SERVICEABLE ISOLATORS PN SL2337-3 IAW SRM 51-42-13. REPAIR CLASSIFIED AS MINOR IAW SOP 5702.Jun 22, 2011 · N973EV · Cndair CL6002B19SDR REXA201100397Bulkhead · scratchedFS 621 BULKHEAD IS SCRATCHED AT WL 140, RBL 16. DAMAGE IS APPROXIMATELY .5" LONG X 0.010" WIDE X 0.003" DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.Jun 22, 2011 · N8896A · Cndair CL6002B19SDR REXA201100396Bulkhead · damagedFS 621 BULKHEAD IS DAMAGED DUE TO SCREW CONTACT AT WL 102.5, RBL 17.5, 27, AND 36. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.Jun 21, 2011 · N8896A · Cndair CL6002B19SDR REXA201100394Angle · damagedFS 621 BULKHEAD STIFFENER ANGLE IS DAMAGED FROM SCREW CONTACT ALONG THE TOP EDGE OF ANGLE WL 119.5 AT LBL 9, 17.5, 27, AND RBL 9. REPAIRED IAW SRM 53-00-00, AND 52-12-00.Jun 21, 2011 · N8896A · Cndair CL6002B19SDR UALA2011062103036Bulkhead · puncturedPUNCTURE IN PRESSURE BULKHEAD JUST FWD OF BS 1605.5 AT APPROX S36L (6 O'CLOCK POSITION). MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER, TEAR STRAP DOUBLER, AND FILLER PER EA PD67-53-030 AND EVA 80918 ON NR 2682N00227.Jun 20, 2011 · N673UA · Boeing 767322SDR SWIA201126702Bulkhead · crackedFS 621 BULKHEAD CRACKED. (C-CHECK) REPAIR PER REO.Jun 20, 2011 · N507CA · Cndair CL6002B19SDR REXA201100393Angle · crackedFS 559 SEMI-PRESSURE BULKHEAD LT CAP ANGLE CRACKED APPROXIMATELY .3 INCH LONG AT LBL 18.0. REPAIRED IAW BOMBARDIER REOS 601R-53-41-260 REV E, AND 601R-53-41-609 REV B, AND BOMBARDIER SERVICE CORPORATION EO'S 601R-53-21611 AND 601R-53-21625.Jun 19, 2011 · N8747B · Cndair CL6002B19SDR REXA201100500Angle · crackedFS 559 PRESSURE BULKHEAD LT CAP ANGLE CRACKED APPROX .300" LONG, 55 PERCENT FSH AT LBL18, FAILED NDT INSPECTION. COMPLY WITH REPAIR OF FS 559 BULKHEAD WEB IAW BOMBARDIER REO 601R-53-41-260 REV E, BOMBARDIER REO 601R-53-41-609 REV B, BOMBARDIER SERVICE CORPORAJun 17, 2011 · N8747B · Cndair CL6002B19SDR USAA2011062200003Bulkhead · crackedPIT - FPBH - CRACK IN WEB OF VERTICAL BEAM BS 179, WL 183, RBL 5.7. REPAIRED WEB OF VERTICAL BEAM BS 179, WL 183, RBL 5.7 IAW EA 200125.Jun 17, 2011 · N440US · Boeing 7374B7SDR SWIA201126513Bulkhead · crackedFS 559 PRESSURE BULKHEAD CRACKED AT RIGHT SIDE. (C-CHECK) REPAIR PER REO.Jun 16, 2011 · N909SW · Cndair CL6002B19SDR ASAA1149880Bulkhead · corrodedFWD SIDE OF AFT PRESSURE BULKHEAD RBL 2 JUST AFT OF BS 1016 CHORD HAS CORROSION ON SKIN UPPER SURFACE. REPAIRED PER ASA EA 400 53EA 05662 AND ER 11 02904.Jun 16, 2011 · N792AS · Boeing 737490SDR K11A2012070316005Splice Plate · corrodedLOWER CANTED BULKHEAD SPLICE PLATE HAS CORROSION, 1X1 INCH (NR 21904).Jun 14, 2011 · N916CK · Doug DC933FSDR DALA1141019019Pressure Panel · crackedDURING PSV IN MSP A 2.5 INCH LONG CRACK COMMON TO THE CANTED PRESSURE PANEL JAMB PAN LOCATED AT STA 69. THE CRACK IS LOCATED IN THE LOWER RADIUS OF THE VERTICAL LEG OF THE PAN. REPAIRED PER ER/A 493840-14 REV 1.Jun 14, 2011 · N919DE · Doug MD88SDR SWAA114327Bulkhead · crackedDURING SCHEDULED 14Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17.0. REPAIRED WEB PER SRM.Jun 14, 2011 · N647SW · Boeing 7373H4SDR ASAA1149866Support · corrodedDURING AFT PIT AFT BULKHEAD SUPPORT INSTALL FOUND LT BULKHEAD LOWER SUPPORT CORRODED ABOVE STR 25L. REMOVED ANGLE FABRICATED AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 30 01 AND 51 40 02.Jun 14, 2011 · N768AS · Boeing 737490SDR SWIA201126499Bulkhead · crackedFS 559 PRESSURE BULKHEAD CRACKED AT LEFT SIDE. (C-CHECK) REPAIR PER REO.Jun 13, 2011 · N909SW · Cndair CL6002B19SDR KCSA111151Forging · crackedBS 1241 RT BULKHEAD FORGING CRACKED AT AFT BOLT HOLE.Jun 13, 2011 · N793CK · Boeing 747222BSDR SWAA114245Pressure Deck · crackedDURING SCHEDULED OTS CHECK, FOUND LT MLG WHEEL WELL PRESSURE DECK WEB CRACKED AT BS 670, LBL 35. REPAIRED WEB PER SRM.Jun 12, 2011 · N602SW · Boeing 7373H4SDR REXA201100391Bulkhead · chafedFS 621 BULKHEAD CHAFED AT WL 103, LBL 16 (0.155"L X 0.140"W X 0.007" DEEP), RBL 18 (0.160"L X 0.118"W X 0.005" DEEP), RBL 27 (0.175"L X 0.150"W X 0.007" DEEP), AND RBL 36 (0.190"L X 0.185"W X 0.007" DEEP). REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.Jun 12, 2011 · N8888D · Cndair CL6002B19SDR REXA201100390Bulkhead · crackedFS 280 BULKHEAD WEB FOUND CRACKED OUTBOARD OF LBL 9 AND RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-926.Jun 12, 2011 · N8888E · Cndair CL6002B19SDR VNAA2011061500012Bulkhead · crackedDURING SCHEDULED MAINTENANCE IT WAS FOUND THE FS 202.0 BULKHEAD HAD A CRACK ADJACENT TO THE HOLE WHERE PARKING BRAKE CABLE PASSES THROUGH. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Jun 11, 2011 · N228PS · Cndair CL6002B19SDR VNAA2011061500011Bulkhead · crackedDURING SCHEDULED MAINTENANCE THE FS 280.0 BULKHEAD WEB WAS FOUND CRACKED. THE FS 280.0 BULKHEAD WEB WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Jun 11, 2011 · N228PS · Cndair CL6002B19SDR A6WA201140645Doubler · bentDOUBLER ON AFT SIDE OF RT 280 BULKHEAD BENT. R & R DOUBLER ON AFT SIDE OF RT 280 BULKHEAD IAW SRM 51-42-06.Jun 10, 2011 · N434AW · Cndair CL6002B19SDR LR7A2011061400209Manifold · crackedDURING SCHEDULED C-5 CHECK IAW JOB CARD HC5301, FOUND LT MAIN WHEEL WELL MANIFOLD CRACKED ATFS 533 & FS 567. REPAIR ACCOMPLISHED BY REPLACEMENT IAW SMP583, CHAPTER 51-70.Jun 10, 2011 · N406LC · Lkheed 382GSDR LR7A2011061400206Manifold · crackedDURING SCHEDULED C-5 CHECK, FOUND RT MAIN WHEEL WELL MANIFOLD WITH RIVET HOLE CRACKS AT FS 533 TO 607, LBL 62.5, WL 146. REPAIR ACCOMPLISHED BY REPLACEMENT IAW SMP583, CHAPTER 51-70.Jun 10, 2011 · N406LC · Lkheed 382GSDR SWAA114226Bulkhead · crackedDURING SCHEDULED 16Y CHECK FOUND, PRESSURE BULKHEAD VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB PER ER AND EA.Jun 10, 2011 · N608SW · Boeing 7373H4SDR USAA2011061300012Bulkhead · corrodedMCN - C21 - LEVEL 2 EXFOLIATION CORROSION ON FORWARD SIDE OF AFT PRESSURE BULKHEAD AT BS 1016 BETWEEN S27L TO S26R. REPAIRED FORWARD SIDE OF AFT PRESSURE BULKHEAD AT BS 1016 BETWEEN S27L TO S26R IAW EA 130594.Jun 9, 2011 · N303AW · Boeing 7373G7SDR USAA2011061000012Stiffener · crackedMCN - C21 CHECK CRACKS ON AFT PRESSURE BULKHEAD VERTICAL STIFFENER FASTENER HOLES AT BS 1016, BETWEEN BL 1L TO BL 1R. REPAIRED AFT PRESSURE BULKHEAD VERTICAL STIFFENER AT BS 1016, BETWEEN BL 1L TO BL 1R IAW EA 130594, STEP 15.Jun 9, 2011 · N303AW · Boeing 7373G7SDR REXA201100376Bulkhead · damagedFS 621 BULKHEAD FWD SIDE HAS SCREW MARKS FROM ACCESS PANEL HARDWARE AT LBL 18, LBL 27, RBL 18, RBL 27, AND RBL 36, WITH NONE DEEPER THAN 0.002". REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.Jun 9, 2011 · N8390A · Cndair CL6002B19SDR SWIA201126440Bulkhead · crackedFS 621 PRESSURE BULKHEAD CRACKED NEAR LINTEL FITTING. (C-CHECK) REPAIR PER REO.Jun 8, 2011 · N952SW · Cndair CL6002B19SDR REXA201100369Bulkhead · crackedEXCESSIVE CRACKING AND CORROSION WAS FOUND ON THE FS 280 BULKHEAD. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B AND BOMBARDIER SERVICE CORP EO 601R-53-21476D.Jun 8, 2011 · N8409N · Cndair CL6002B19SDR ASOA201101162Bulkhead · corrodedRT 280 BULKHEAD HAS HEAVY CORROSION AFT SIDE JUST ABOVE FLOOR LEVEL AT RBL 12. BLENDED LIGHT SURFACE CORROSION ON BULKHEAD IAW SRM 51-21-06, ORIGINAL MAT'L THICKNESS OF .040, MAT'L LOSS OF .003 NOTED, REMAINING MAT'L THICKNESS OF .037, FOUND TO BE WITHIN LIMIJun 7, 2011 · N751EV · Cndair CL6002C10SDR UIEA2011060700300Bulkhead Web · crackedDURING C-CHECK, A CRACK WAS FOUND IN THE PRESSURE WEB. THE CRACK WAS LOCATED AT THE 11 O'CLOCK POSITION, EXTENDING THROUGH TWO (2) FASTENER HOLES OTBD OF THE RT 2ND INTERMEDIATE STIFFENER FROM THE TOP. THE CRACK EXTENDED 0.1875 IN INBD AND 0.125 IN OTBD AS SJun 7, 2011 · N522MC · Boeing 7472D7BSDR ASOA201101139Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT LBL 27.50 INBD FAILED NDT INSPECTION. REPAIRED REAR PRESSURE BULKHEAD WEB IAW REO 601R-53-61-1541.Jun 7, 2011 · N909EV · Cndair CL6002B19SDR JR2R2011060700239Fitting · crackedPAX DOOR LINTIAL CRACKED AT 280 BULKHEAD.Jun 7, 2011 · N927LR · Cndair CL6002D24SDR FDEA201106062135Frame · corrodedAFT PRESSURE BULKHEAD BOTTOM FWD SIDE AT FR 80/82 CIRCUMFERENTIAL STRAP CORRODED 7 IN LENGTH X 4 IN WIDTH BETWEEN STR 54R TO 56R. REMOVED CIRCUMFERENTIAL STRAP STRINGER 51R TO 54L IAW SRM 51-40-21. VERIFIED NO FURTHER CORROSION DAMAGE FOUND. INSTALLED NEJun 6, 2011 · N716FD · Airbus A300B4622SDR AALA20110611TUL01Bulkhead · corrodedSTATION 1088 BULKHEAD HAS CORROSION IN AREA OF AUXILIARY POWER UNIT INLET DUCT. UPPER ANGLE REPLACED ON APU INLET STATION 1088 PER AARD 51-10-05 AND EA 737-53-017392.Jun 6, 2011 · N927AN · Boeing 737823SDR DALA1137736802Bulkhead · corrodedSTA 324 BULKHEAD UPPER CHORD CORRODED. REPAIR C/W PER ERA 492992-14 - RBL 33 TO RT END OF PART.Jun 6, 2011 · N703TW · Boeing 7572Q8SDR REXA201100334Bulkhead · crackedONE CRACK MEASURED TO BE 0.300" IN LENGTH AT AFT PRESSURE BULKHEAD (FS 621) LEFT SIDE LINTEL FITTING. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230 REV D.Jun 6, 2011 · N8794B · Cndair CL6002B19
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