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 SWIA200923272Bulkhead · crackedFORWARD PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE LIGHTENING HOLE. (SVC CHECK) / REPAIRED PER REO.SDR SIMA200934903Bulkhead · dentedDURING THE MAINTENANCE BASE VISIT INSPECTION FOUND THE AFT PRESSURE BULKHEAD HAS A DENT, (AT 4 O’CLOCK POSITION VIEWED FROM INSIDE AFT AVIONICS COMPARTMENT LOOKING AFT). THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED DOUBLER REPAIR TO BULKHEAD IAW AEAI EO-SDR SWIA200923824Angle · crackedFS 559 BULKHEAD LOWER CAP ANGLE RADIUS CRACKED. (C CHECK) REPAIRED PER REO.SDR COMA2009121450227Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD CRACKED ABOVE CARGO DOOR TRACK. REPAIRED CRACK ABOVE CARGO DOOR TRACK IAW REO 601R-53-61-1541.SDR COMA2009121450226Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD CRACKED AROUND LINTEL FITTING. REPAIRED CRACK AT LINTEL FITTING IAW REO 601R-53-61-1230.SDR SWIA200923823Isolator · crackedFS 621 BULKHEAD ISOLATOR CRACKED. (C CHECK) REPLACED PER SRM.SDR SWIA200923821Fitting · crackedFS 621 PRESSURE BULKHEAD LINTEL FITTING CRACKED. (C CHECK) REPAIRED PER REO.SDR SWIA200923820Bulkhead · crackedFS 559 PRESSURE BULKHEAD CRACKED. (C CHECK) REPAIRED PER REO.SDR VNAA2009121500001Bulkhead · crackedDURING INSPECTION A CRACK WAS FOUND ON THE REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL FITTING AT FS 621.15. AREA WAS REPAIRED USING REO 601R-53-61-1230 REV. AIRCRAFT WAS RELEASED FOR SERVICE.SDR ASOA200901385Bulkhead · damagedFOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDING THE LINTEL FITTING HAS INDICATION NOTED APPROX .3" IN LENGTH 90 PERCENT FSH FAILED NDT INSP. REPAIRED IAW EC/TC REO 601R-53-61-1230.SDR CA100107007Bulkhead · cracked(CAN) BULKHEAD AT FS 246.75 CRACKED UNDER FLOOR, WATERLINE 85.0, BUTTOCK LINE 25.0 LEFT. (TC NR 20100107007)SDR ASOA200901371Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX .3" IN LENGTH 80 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED PER EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETED AND THE REPAIR C/W THE REQUIREMENTS OF ECSDR SWIA200923218Bulkhead · crackedFS621 PRESSURE BULKHEAD WEB CRACKED AT AFT CARGO DOOR ROLLER GUIDE TRACK. (C-CHECK) REPAIRED PER REO 601R-53-61-1541.SDR ASOA200901353Bulkhead · crackedFOUND F.S. 559 RT SIDE BULKHEAD WEB HAS 2 INDICATIONS NOTED. C/W EC/TC 601R-53-41-260 IAW REO 601R-53-41-260 REV D.SDR SWIA200923274Bulkhead · crackedFS621 PRESSURE BULKHEAD CRACKED AT LINTEL FITTING. (C CHECK) REPAIRED PER REO.SDR A6WA201040026Bulkhead · crackedRT CAP ANGLE OF PRESSURE BULKHEAD STRUCTURE IS CRACKED AT FS 559.00, RBL 18.0, WL 47.0. RT CAP ANGLE OF PRESSURE BULKHEAD STRUCTURE AT FS 559.00, RBL 18.0, WL 47.0, REPAIRED IAW REO 601R-53-41-260, REV "D" DEVIATION E AND REO 601R-53-41-609, REV A AND REO 601SDR AALA20091202TUL11Stop Fitting · crackedAFT PRESSURE BULKHEAD JAMB HAS CRACKED STOP. INSTALLED NEW STOP.SDR SWAA097587Bulkhead · crackedDURING SCHEDULED MV2 CHECK, FOUND LT MLG MAIN WHEEL WELL FWD BULKHEAD WEB CRACKED AT BS 663.75, LBL 43. REPAIRED WEB PER EA.SDR SWAA097586Beam · crackedDURING SCHEDULED 12Y CHECK, FOUND BULKHEAD VERTICAL BEAM CRACKED AT BS 727, RBL 35.5. REPAIRED BEAM PER AAR EA.SDR SWIA200923207Bulkhead · crackedFORWARD PRESSURE BULKHEAD CRACKED AT PARKING BRAKE ACTUATOR ARM ACCESS PORT. (SVC CHECK)REPAIRED PER REO.SDR AALA20100112TUL06Bulkhead · gougedBULKHEAD WEB NEAR LEFT STATION 1809 OUTER CHORD WAS GOUGED. BLENDED WEB UNDER ENGINEERING AUTHORIZATION B767-53-008055.SDR ASAA0977111Skin · gougedRT HORIZONTAL STAB FIXED L/E SKIN IS GOUGED. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED.SDR A6WA201040027Bulkhead · mislocatedQTY (1) REDUNDANT HOLE AND QTY (2X) DRILL MARKS EXISTS IN PRESSURE BULKHEAD WEB AT FS 559.00, RBL 22.5, WL 50.0 QTY (1) REDUNDANT HOLE AND QTY (2X) DRILL MARKS REPAIRED IAW REO 601R-53-41-1117.SDR COMA2009113050218Bulkhead · crackedFOUND CRACK ON FWD PRESSURE BULKHEAD AROUND PARKING BRAKE CABLE AT FS 202.75. REPAIRED FWD PRESSURE BULKHEAD IAW EA 10-5311-02824.SDR AALA20091125AFW01Bulkhead · crackedCRACK INDICATIONS WERE FOUND ON THE FORWARD LOWER HOLE COMMON TO THE BULKHEAD LEFT FORWARD OUTER CHORD AND STRINGER 12A LEFT TENSION FITTING AT STATION 1809.5. THE FASTENER HOLE WAS OVERSIZED TO 0.2782 INCHES. BOEING APPROVED THE OVERSIZED HOLE TO 2ND OVER WSDR LR7A2009121000146Bulkhead Web · crackedDURING SCHEDULED B-2 CHECK IAW JOB CARD HB3200, FOUND LT MWW UPPER BHD WEB CRACKED AT FS572, WL200, LBL72 / REPAIRED IAW LAC MEA 382-53-09-034. NR 2031.SDR SWAA097533Stiffener · crackedDURING SCHEDULED MV2 CHECK, FOUND LT MAIN WHEEL WELL BULKHEAD SUPPORT STIFFENER CRACKED AT BS 633, LBL 6. REPAIRED STIFFENER PER EA.SDR SWAA097507Bulkhead · crackedDURING SCHEDULED 16Y CHECK, FOUND PRESSURE BULKHEAD WEB CRACKED AT BS 1016, BETWEEN STR 7R TO STR 15R. REPAIRED WEB AT SRM.SDR CA091204004Bulkhead · cracked(CAN) BULKHEAD CTR PORTION OF UPPER FLANGE CRACKED. THIS PART IS UNDER NON REMOVABLE FLOOR PANEL. FLOOR PANEL ALSO CRACKED AT END OF MUTIPLE STIFFENING BUMPS.SDR AALA20091123AFW01Bulkhead · crackedCRACK INDICATIONS WERE FOUND ON THE AFT UPPER HOLE COMMON TO THE OUTER CHORD AND S-12A RIGHT TENSION FITTING AT BULKHEAD RT FWD OUTER CHORD. THE FASTENER HOLE WAS OVERSIZED TO 0.2782 TO REMOVE ANY INDICATIONS. BOEING APPROVED THE OVERSIZED HOLE TO 2ND OVER WSDR K11A2009112372505Angle · crackedAFT PRESSURE BULKHEAD UPPER ANGLE CRACKED 4 INCH CRACK.SDR K11A2009112372503Stiffener · crackedAFT PRESSURE BULKHEAD HORIZONTAL STIFFENER CRACKED.SDR SWAA097377Stiffener · crackedDURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT STIFFENER CRACKED AT FWD BULKHEAD BS 727, LBL 12. REMOVED AND REPLACED STIFFENER PER BAC DWG.SDR SWIA200923812Bulkhead · corrodedLEFT BULKHEAD WEB CORRODED. (C CHECK) REPAIRED PER SRM.SDR USAA2010010590030Bulkhead · crackedSAL - Q4 - MAJOR REPAIR - CRACK ON FORWARD SIDE OF BS 178 PRESSURE BULKHEAD WL 234 BETWEEN LBL 10 TO LBL 17. REPAIRED BS 178 PRESSURE BULKHEAD WL 234 BETWEEN LBL 10 TO LBL 17 IAW B737 SRM 53-10-08 REPAIR 9 & EO 5300V153.SDR SWIA200923160Bulkhead · crackedFS 621 BULKHEAD FORWARD FACE CRACKED ABOVE CARGO DOOR FITTING. (C-CHECK) REPAIRED PER REO.SDR A6WA201040012Bulkhead · crackedCRACK FOUND ON FWD PRESSURE BULKHEAD AT FS 202.75, LBL 23.71, WL 69 IN PARKING BRAKE CABLE AREA. FWD PRESSURE BULKHEAD AT FS 202.75, LBL 23.71, WL 69, REPAIRED IAW REO 601R-53-11-563.SDR SWIA200923180Bulkhead · crackedFS 559 PRESSURE BULKHEAD CRACKED. (C-CHECK) REPAIRED PER REO.SDR USAA2010012590178Angle · corrodedSAL - Q4 - MAJOR REPAIR - LEVEL 2 FILIFORM CORROSION ON STIFFENER ANGLE AT BS 1016 BETWEEN S26L TO S25R AFT PRESSURE BULKHEAD. REPAIRED STIFFENER ANGLE AT BS 1016 BETWEEN S26L TO S25R AFT PRESSURE BULKHEAD IAW EA 32767.SDR A6WA200940808Bulkhead Web · crackedFS 621.00, PRESSURE BULKHEAD WEB FOUND CRACKED AT UPPER END OF AFT CARGO TRACK LBL 27.50, WL 130.00. PRESSURE BULKHEAD WEB AT FS 621.00, LBL 27.50, WL 130.00. REPAIRED IAW REO 601R-53-61-1541, REV B. (K)SDR DL76L091854Pressure Panel · gougedPRESSURE WEB GOUGED UPPER SURFACE AT APPROX STA 970R AND RBL 90. REPAIR IN ACCORDANCE WITH ERA 478288-14.SDR REXA200900124ABulkhead · crackedFOUND CRACKS AT FS 559 BULKHEAD WEB HAS 2 INDICATIONS OF CRACKS NOTED ON RT SIDE WL 59.10 I/B OF RBL 18 APPROX .3 INCH IN LENGTH AND WL 58.70 O/B OF RBL 9, APPROX .2 INCH IN LENGTH AND RT FS 559 CAP ANGLE HAS INDICATION NOTE AT RBL 18 APPROX .2 INCH IN LENGTH SDR SWIA200923728Bulkhead · crackedFS 559 PRESSURE BULKHEAD CRACKED. (C CHECK) REPAIRED PER REO.SDR A6WA200940807Bulkhead · crackedFS 621.00, AFT PRESSURE BULKHEAD FOUND CRACKED AT LINTEL FITTING AREA W/L 110.00. REPAIR PERFORMED ON AFT PRESSURE BULKHEAD AT FS 621.00, W/L 110.00 IAW REO 601R-53-61-1230, REV D. (K)SDR ASOA200901315Bulkhead · crackedFOUND 202 BULKHEAD CRACKED BETWEEN 12 AND 1 O`CLOCK.SDR COMA2009111950214Bulkhead · crackedDURING EDDY CURRENT INSPECTION FOUND A CRACK AT THE FS 621.00, LBL 27.50, AFT PRESSURE BULKHEAD. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND FILLER IN ACCORDANCE WITH REO 601R-53-61-1541 REV-A.SDR SWIA200923109Bulkhead · crackedFS 621 BULKHEAD CRACKED. (C-CHECK) DAMAGE WITHIN LIMITS. BLENDED PER REO.SDR SWIA200923566Bulkhead · crackedFS 559 BULKHEAD CRACKED AT LBL 18 ON FRAME CAP ANGLE. (C CHECK) REPAIRED PER REO.SDR QXEA2009111600959Bulkhead · corrodedLT BULKHEAD AT STA 280 LOWER WEB IS CORRODED. BLENDED AWAY CORROSION IAW REO 670-53-11-052. UT THICKNESS IAW NDTM PART 1, 51-00-004 AND REO 670-53-11-052. FOUND TO BE OUT OF LIMITS IAW REO 670-53-11-052. REMOVED LWR WEB IAW REO 670-53-11-052. PREPARED NEWSDR A6WA200940804Bulkhead · crackedCRACK FOUND ON AFT PRESSURE BULKHEAD AT END OF CARGO TRACK FS 621.00, LBL 27.50, WL 130.00. REPAIR PERFORMED ON AFT PRESSURE BULKHEAD AT END OF CARGO TRACK FS 621.00, LBL 27.50, WL 130.00 IAW REO 601R-53-61-1541, REV B. (K)
Back to JASC 5312