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 SWIA201024371Bulkhead · crackedFS 202 BULKHEAD CRACKED AT PARKING BRAKE CABLE RUN. (C CHECK) REPAIRED PER REO.Mar 29, 2010 · N492SW · Cndair CL6002B19SDR COMA2010033050073Bulkhead · crackedREAR PRESSURE BULKHEAD WEB IS CRACKED AT LINTEL ATTACHMENT FS 621. REPAIRED REAR PRESSURE BULKHEAD WEB AT LINTEL ATTACHMENT IAW REO 601R-53-61-1230.Mar 29, 2010 · N936CA · Cndair CL6002B19SDR SWIA201023949Bulkhead · crackedPRESSURE BULKHEAD AT FS 559 CRACKED. (C CHECK) REPAIRED PER REO.Mar 27, 2010 · N918SW · Cndair CL6002B19SDR QMLR3253UBulkhead · crackedDURING OTHER MX, 2 CRACKS WERE FOUND IN BULKHEAD, PN 222-031-505-001 AT ATTACHMENT POINT OF NODAL BEAM SUPPORT, PN 222-031-519-103.Mar 26, 2010 · N416MA · Bell 222USDR EE4Y1003040Bulkhead · crackedDURING THE INSPECTION NOSE WHEEL WELL STA Y37, -X23,-Z28 PRESSURE BULKHEAD AFT FACE COOPESA FOUND CHORD CRACKED.Mar 26, 2010 · N784TW · Doug DC915SDR SWIA201023911Bulkhead · crackedFS 559 PRESSURE BULKHEAD CRACKED AT CAP ANGLE RADIUS. (C CHECK) REPAIRING PER REO.Mar 24, 2010 · N961SW · Cndair CL6002B19SDR ASOA201000424Bulkhead · crackedREAR PRESSURE BULKHEAD IS CRACKED AT LINTEL FITTING. ACCOMPLISHED LINTEL FITTING/ AFT PRESSURE BULKHEAD REPAIR IAW PL601R-53-61-1230, C/W RII OF REAR PRESSURE BULKHEAD LINTEL FITTING.Mar 24, 2010 · N972EV · Cndair CL6002B19SDR TRBACPCP2010036Bulkhead · corrodedCORROSION ON CONTACT POINT AT FWD PRESSURE BULKHEAD. C/W SRI DO/TS-1767/10-13252, REF NDT REPORT AMS INC 100326-25 FOR UT AN HFEC VALUES. NO CRACKS NOTED AT THIS TIME. C/W ATR72 SRAS DO/TS - 1767/10 5668 SUPPLEMENTARY INSP, DUI OF BLENDED AREAS EVERY 2 YRS FORMar 23, 2010 · N434AT · Aerosp ATR72212SDR SWIA201023937Bulkhead · crackedFS 621 FORWARD AFT PRESSURE BULKHEAD CRACKED AT SPLICE. (C CHECK) REPAIRED PER REO.Mar 23, 2010 · N918SW · Cndair CL6002B19SDR SWIA201023935Bulkhead · crackedFS 621 AFT PRESSURE BULKHEAD WEB CRACKED AT LINTEL FITTING AND AT TOP OF AFT CARGO DOOR TRACK. (C CHECK) REPAIRED PER REO.Mar 23, 2010 · N918SW · Cndair CL6002B19SDR SWIA201023909Bulkhead · crackedFS 621 PRESSURE BULKHEAD WEB CRACKED AT LINTEL FITTING. (C CHECK) REPAIRED PER REO.Mar 23, 2010 · N918SW · Cndair CL6002B19SDR ASOA201000415Bulkhead · corrodedFS 621.00, PRESSURE BULKHEAD WEB FWD FACE HAS A 90 PERCENT FSH HFEC INDICATION NOTED APPROX 0.2" LONG AT THE BOTTOM INBD CORNER OF THE LINTEL FITTING. FAILS NDT AT THIS TIME. REPAIR PER EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETE AND THE REPAIR C/W THE REQUMar 22, 2010 · N681BR · Cndair CL6002B19SDR ASOA201000414Bulkhead · crackedBS 202.75 PRESSURE BULKHEAD CRACKED AT BRAKE CABLE FEED THROUGH HOLE. C/W EC/TC REO 601R-53-11-563 AND REO 601R-53-11-563 REV.Mar 22, 2010 · N681BR · Cndair CL6002B19SDR 2010FA0000253Seal · brokenACFT HAD A RAPID CABIN PRESSURE RISE AT ABOUT 28,000 FT AGL DURING CLIMB OUT. PILOTS DECLARED AN EMERGENCY AND MADE AN EMERGENCY DECENT. OXYGEN MASKS DEPLOYED AT ABOUT 13,000 FT AND CABIN REACHED ABOUT 15,000 FT. AS THE ACFT REACHED 10,000 FT AGL PILOTS WITHMar 21, 2010 · N633AT · Cessna 500CESSNASDR SWIA201024340Bulkhead · crackedFS 621 PRESSURE BULKHEAD CRACKED AT SPLICE. (C CHECK) REPAIRED PER REO.Mar 20, 2010 · N918SW · Cndair CL6002B19SDR SWIA201024339Bulkhead · crackedFS 621 BULKHEAD CRACKED AT LINTEL FITTING. (C CHECK) REPAIRED PER REO.Mar 20, 2010 · N918SW · Cndair CL6002B19SDR SWIA201024338Bulkhead · crackedFS 621 FORWARD AFT PRESSURE BULKHEAD CRACKED AT TOP OF AFT CARGO DOOR TRACK. (C CHECK) REPAIRED PER REO.Mar 20, 2010 · N918SW · Cndair CL6002B19SDR COMA2010032250065Bulkhead · crackedFOUND CRACK IN REAR PRESSURE BULKHEAD WEB ASSEMBLY ABOVE CARGO DOOR TRACK AT FS 621.00. REPAIRED REAR PRESSURE BULKHEAD WEB AT FS 621.00 IAW REO 601R-53-61-1541 REV B.Mar 20, 2010 · N937CA · Cndair CL6002B19SDR FDIA2010F00071Seal · brokenACFT HAD A RAPID CABIN PRESSURE RISE AT ABOUT 28,000 FEET AGL DURING CLIMB OUT. PILOTS DECLARED AN EMERGENCY AND MADE AN EMERGENCY DECENT. OXYGEN MASKS DEPLOYED AT ABOUT 13,000 FT AND CABIN REACHED ABOUT 15,000 FEET. AS THE ACFT REACHED 10,000 FT AGL PILOTS WIMar 17, 2010 · N633AT · Cessna 500CESSNASDR SWIA201023850Bulkhead · crackedCRACK ON FORWARD PRESSURE BULKHEAD BL 23.71. (A CHECK) REPAIRED PER REO.Mar 17, 2010 · N927SW · Cndair CL6002B19SDR AALA20100316TUL18Pressure Panel · crackedCRACK IN RIGHT WHEEL WELL PRESSURE DECK STATION 1003 OUTBOARD SIDE. CRACK STOP DRILLED AND DOUBLER INSTALLED PER AARD53-30-00-13 AND SRM 53-01-00.Mar 16, 2010 · N426AA · Doug DC982SDR USAA2010040790726Bulkhead · corrodedSAL - C22 - MAJOR REPAIR - CORROSION ON FUSELAGE BULKHEAD LOWER CHORD AT BS 227.8 BETWEEN BL 0 TO RBL 8. REPAIRED FUSELAGE BULKHEAD LOWER CHORD AT BS 227.8 BETWEEN BL 0 TO RBL 8 IAW EA 132932.Mar 16, 2010 · N156AW · Boeing 7373G7SDR ASOA201000408Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH. FAILED NDT INSP. REPAIR IAW REO EC/TC 601R-53-61-1230 HAS BEEN COMPLETE AND THE REPAIR COMPLIES WITH THE REQUIREMENTS OF Mar 16, 2010 · N917EV · Cndair CL6002B19SDR SWIA201023865Angle · crackedFS 559 BULKHEAD CAP ANGLE RADIUS CRACKED. (C CHECK) REPAIRED PER REO.Mar 16, 2010 · N699BR · Cndair CL6002B19SDR ASOA201000396Bulkhead · crackedAFT PRESSURE BULKHEAD IS CRACKED LINTEL ATTACH BRACKET. INSTALLED LINTEL FITTING IAW STEP 5,13,14,19-24 KJ161732 INSTALLED SOLID RIVETS AROUND FILLER COMMON TO LINTEL FITTING AND SOLIDS THROUGH FUSELAGE FWD OF FS 621 IAW REO 601R-53-61-1230. INSTALLED FASTENMar 16, 2010 · N858AS · Cndair CL6002B19SDR COMA2010031650062Bulkhead · crackedFORWARD PRESSURE BULKHEAD CRACKED AROUND THE PARKING BRAKE CUTOUT, FS 202.75, LBL 23.71. CUT OUT DAMAGE AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-11-563, AND EA 10-5311-02896.Mar 16, 2010 · N597SW · Cndair CL6002B19SDR AALA20100315TUL03Angle · crackedAFT PRESSURE BULKHEAD LEFT T-ANGLE SHOWS INDICATION OF CRACK LONGERON 14 LEFT. REMOVED AND REPLACED T ANGLE PER IAW EA 009163.Mar 15, 2010 · N403A · Doug DC982SDR SWAA101563Pressure Panel · crackedDURING SCHEDULED 14Y CHECK, FOUND LT WHEEL WELL OVERHEAD BULKHEAD PRESSURE DECK WEB CRACKED AT BS 665, LBL 31. REMOVED AND REPLACED WEB PER SRM.Mar 15, 2010 · N628SW · Boeing 7373H4SDR SWAA101512Splice · crackedDURING SCHEDULED 18Y CHECK, FOUND PRESSURE BULKHEAD CHORD SPLICE CRACKED AT BS 727, RBL 45. REMOVED AND REPLACED SPLICE PER SRM.Mar 14, 2010 · N359SW · Boeing 7373H4SDR SWAA101511Splice · crackedDURING SCHEDULED 18Y CHECK, FOUND PRESSURE BULKHEAD CHORD SPLICE CRACKED AT BS 727, LBL 45. REMOVED AND REPLACED SPLICE PER SRM.Mar 14, 2010 · N359SW · Boeing 7373H4SDR AALA20100313TUL03Doubler · corrodedCARGO AFT CX CORROSION FORWARD SIDE OF AFT PRESSURE BULKHEAD PLOW ANGLE DOUBLER. DOUBLER WAS OUT OF LIMITS PER SRM 53-01. NEW AFT PRESSURE BULKHEAD DOUBLER (DELTA PLATE) WAS INSTALLED PER BOEING DRAWING PL5910130 AND SRM 51-30-05.Mar 13, 2010 · N7537A · Doug DC982SDR EE4Y1003021Bulkhead · corrodedDURING INSPECTION LOWER FUSELAGE AFT CARGO COMPARTMENT RT AFT PRESSURE BULKHEAD INNER SKIN WITH CORROSION.Mar 13, 2010 · N784TW · Doug DC915FSDR EE4Y1003010Bulkhead · corrodedDURING THE LOWER FUSELAGE AFT COMPARTMENT INSPECTION COOPESA FOUND LT AFT PRESSURE BULKHEAD INNER SKIN CORRODED.Mar 12, 2010 · N784TW · Doug DC915FSDR VNAA2010031700008Bulkhead · crackedDURING SCHEDULED MAINTENANCE A CRACK WAS FOUND AT PRESSURE BULKHEAD WEB. CRACK WAS REPAIRED AND AIRCRAFT WAS RELEASED FOR SERVICE.Mar 11, 2010 · N215PS · Cndair CL6002B19SDR COMA2010031050059Bulkhead · crackedFORWARD PRESSURE BULKHEAD CRACKED AROUND THE PARKING BRAKE CUTOUT, 7:00 POSITION, FS 202.75, LBL 23.71. CUT OUT DAMAGE AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-11-563, AND EA 10-5311-02893.Mar 10, 2010 · N739CA · Cndair CL6002B19SDR COMA2010030950057Bulkhead · crackedREAR PRESSURE BULKHEAD CRACKED AT RBL 18.00, ABOVE WL 106.17, FS 621.00. CUT OUT DAMAGE AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1285, REV A.Mar 9, 2010 · N739CA · Cndair CL6002B19SDR COMA2010030850055Bulkhead · crackedREAR PRESSURE BULKHEAD CRACKED AT CARGO DOOR TRACK ATTACH, LBL 27, FS 621.00. CUT OUT DAMAGE AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1541, REV B.Mar 8, 2010 · N739CA · Cndair CL6002B19SDR ASAA11410044Fitting · gougedSILL INSTALLED AFT ENTRY DOOR LWR MAIN: APB FLOOR SUPPORT FITTING BOLT HOLE IS GOUGED AT BOLT 81L. REPLACED APB FITTING IAW B737 400 SRM 51 40 02 AND 51 40 05.Mar 7, 2010 · N768AS · Boeing 737490SDR ASAA1149854Support Fitting · gougedAFT PRESSURE BULKHEAD SUPPORT FITTING BOLT HOLE IS GOUGED AT BOLT 81L. REMOVED AND REPLACED AFT PRESSURE BULKHEAD FITTING IAW B737 400 SRM 51 40 02 AND 51 40 05.Mar 7, 2010 · N778AS · Boeing 7374Q8SDR 2010F00061Bulkhead · distortedWITH ACFT PARKED IN STRONG TAIL WIND NEAR GROSS WEIGHT WITH CG NEAR AFT LIMIT, ACFT SETTLED ON TAIL TIE DOWN ASSY AFTER PILOT EXITED THE COCKPIT. THE LOWER PORTION OF THE 2612059-2 BULKHEAD WAS DAMAGED AND WILL HAVE TO BE REPAIRED IAW THE FAA APPROVED MFG SRM Mar 7, 2010 · N865MA · Cessna 208BSDR SWIA201023800Bulkhead · crackedFS 621 BULKHEAD CRACKED AT TOP OF CARGO DOOR TRACK. (C CHECK) REPAIRED PER REO.Mar 7, 2010 · N962SW · Cndair CL6002B19SDR SWAA101312Bulkhead · crackedDURING SCHEDULED 20Y CHECK, FOUND PRESSURE BULKHEAD CRACKED AT BS 178, LBL 17.0. REPAIRED BULKHEAD PER AEM EO.Mar 7, 2010 · N510SW · Boeing 7375H4SDR AALA20100307TUL02Doubler · corrodedAFT CARGO CORROSION FORWARD SIDE OF AFT PRESSURE BULKHEAD PLOW ANGLE DOUBLER STATION 1338 LONGERON 30. REPLACED DOUBLER PER SRM 51-01-00 AND SRM 51-30-00.Mar 6, 2010 · N7537A · Doug DC982SDR SWIA201023785Bulkhead · crackedFS 621 BULKHEAD FORWARD FACE ABOVE CARGO DOOR FITTING CRACKED. (C CHECK) REPAIRED PER REO.Mar 6, 2010 · N593ML · Cndair CL6002B19SDR AALA20100305TUL08Pressure Panel · crackedCRACK IN PRESSURE DECK STATION 965. INSTALLED DOUBLER.Mar 5, 2010 · N7535A · Doug DC982SDR AALA20100307TUL06Pressure Panel · crackedRIGHT WHEEL WELL CRACK IN PRESSURE DECK UNDER FUEL SHROUD SHIELD SUPPORT CLIP. REPAIRED CRACK PER SRM 53-01 FIGURE 2 SHEET 3.Mar 5, 2010 · N7535A · Doug DC982SDR AALA20100305TUL03Stiffener · crackedFORWARD RIGHT SIDE OF THE PRESSURE BULKHEAD 4TH FROM TOP HORIZONTAL STIFFENER IS CRACKED AT THE OUTBOARD END LOWER SIDE ATTACH ANGLE. REMOVED AND REPLACED STIFFENER ATTACH ANGLE PER SRM 51-10-1 AND 51-30-2.Mar 5, 2010 · N7535A · Doug DC982SDR ASOA201000357Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB LBL 27.50 APPROX WL 130 HAS INDICATION NOTED APPROX .2" IN LENGTH 90/5 FSH JUST ABOVE AFT CARGO DOOR TRACK FAILED NDT INSP. AREA MARKED ON ACFT. COMPLIED WITH EC/TC REO 601R-53-61-1541 AND MET ALL THE REQUIREMENTS OF REO 601R-Mar 5, 2010 · N827AS · Cndair CL6002B19SDR AALA20100304TUL01Stiffener · crackedFORWARD RIGHT SIDE OF THE PRESSURE BULKHEAD TOP HORIZONTAL STIFFENER IS CRACKED AT THE OUTBOARD END LOWER SIDE. REMOVED AND REPLACED STIFFENER PER SRM 51-10-1 AND 51-30-2.Mar 4, 2010 · N7535A · Doug DC982SDR DALA104849872Bulkhead · crackedDURING "H" CHECK FOUND CRACK IN MAIN CABIN AFT BULKHEAD RT OUTBOARD ATTACH BRACKET AT Z34. REPAIRED PER SRM 53-10-25.Mar 4, 2010 · N781NC · Doug DC951
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