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 SWIA200923272Bulkhead · crackedFORWARD PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE LIGHTENING HOLE. (SVC CHECK) / REPAIRED PER REO.Dec 13, 2009 · N461SW · Cndair CL6002B19SDR 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-Dec 13, 2009 · N607AE · Emb EMB145SDR SWIA200923824Angle · crackedFS 559 BULKHEAD LOWER CAP ANGLE RADIUS CRACKED. (C CHECK) REPAIRED PER REO.Dec 12, 2009 · N913SW · Cndair CL6002B19SDR COMA2009121450227Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD CRACKED ABOVE CARGO DOOR TRACK. REPAIRED CRACK ABOVE CARGO DOOR TRACK IAW REO 601R-53-61-1541.Dec 12, 2009 · N721CA · Cndair CL6002B19SDR COMA2009121450226Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD CRACKED AROUND LINTEL FITTING. REPAIRED CRACK AT LINTEL FITTING IAW REO 601R-53-61-1230.Dec 12, 2009 · N721CA · Cndair CL6002B19SDR SWIA200923823Isolator · crackedFS 621 BULKHEAD ISOLATOR CRACKED. (C CHECK) REPLACED PER SRM.Dec 10, 2009 · N915SW · Cndair CL6002B19SDR SWIA200923821Fitting · crackedFS 621 PRESSURE BULKHEAD LINTEL FITTING CRACKED. (C CHECK) REPAIRED PER REO.Dec 10, 2009 · N915SW · Cndair CL6002B19SDR SWIA200923820Bulkhead · crackedFS 559 PRESSURE BULKHEAD CRACKED. (C CHECK) REPAIRED PER REO.Dec 10, 2009 · N915SW · Cndair CL6002B19SDR 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.Dec 10, 2009 · N246PS · Cndair CL6002B19SDR 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.Dec 10, 2009 · N879AS · Cndair CL6002B19SDR CA100107007Bulkhead · cracked(CAN) BULKHEAD AT FS 246.75 CRACKED UNDER FLOOR, WATERLINE 85.0, BUTTOCK LINE 25.0 LEFT. (TC NR 20100107007)Dec 9, 2009 · Beech B200SDR 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 ECDec 9, 2009 · N901EV · Cndair CL6002B19SDR SWIA200923218Bulkhead · crackedFS621 PRESSURE BULKHEAD WEB CRACKED AT AFT CARGO DOOR ROLLER GUIDE TRACK. (C-CHECK) REPAIRED PER REO 601R-53-61-1541.Dec 8, 2009 · N417SW · Cndair CL6002B19SDR 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.Dec 4, 2009 · N901EV · Cndair CL6002B19SDR SWIA200923274Bulkhead · crackedFS621 PRESSURE BULKHEAD CRACKED AT LINTEL FITTING. (C CHECK) REPAIRED PER REO.Dec 3, 2009 · N457SW · Cndair CL6002B19SDR 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 601Dec 2, 2009 · N427ZW · Cndair CL6002B19SDR AALA20091202TUL11Stop Fitting · crackedAFT PRESSURE BULKHEAD JAMB HAS CRACKED STOP. INSTALLED NEW STOP.Dec 2, 2009 · N590AA · Doug DC983SDR 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.Dec 2, 2009 · N715SW · Boeing 7377H4SDR SWAA097586Beam · crackedDURING SCHEDULED 12Y CHECK, FOUND BULKHEAD VERTICAL BEAM CRACKED AT BS 727, RBL 35.5. REPAIRED BEAM PER AAR EA.Dec 2, 2009 · N701GS · Boeing 7377H4SDR SWIA200923207Bulkhead · crackedFORWARD PRESSURE BULKHEAD CRACKED AT PARKING BRAKE ACTUATOR ARM ACCESS PORT. (SVC CHECK)REPAIRED PER REO.Dec 1, 2009 · N925SW · Cndair CL6002B19SDR AALA20100112TUL06Bulkhead · gougedBULKHEAD WEB NEAR LEFT STATION 1809 OUTER CHORD WAS GOUGED. BLENDED WEB UNDER ENGINEERING AUTHORIZATION B767-53-008055.Nov 30, 2009 · N374AA · Boeing 767323SDR ASAA0977111Skin · gougedRT HORIZONTAL STAB FIXED L/E SKIN IS GOUGED. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED.Nov 30, 2009 · N611AS · Boeing 737790SDR 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.Nov 27, 2009 · N427ZW · Cndair CL6002B19SDR COMA2009113050218Bulkhead · crackedFOUND CRACK ON FWD PRESSURE BULKHEAD AROUND PARKING BRAKE CABLE AT FS 202.75. REPAIRED FWD PRESSURE BULKHEAD IAW EA 10-5311-02824.Nov 26, 2009 · N588SW · Cndair CL6002B19SDR 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 WNov 25, 2009 · N374AA · Boeing 767323SDR 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.Nov 25, 2009 · N406LC · Lkheed 382GSDR SWAA097533Stiffener · crackedDURING SCHEDULED MV2 CHECK, FOUND LT MAIN WHEEL WELL BULKHEAD SUPPORT STIFFENER CRACKED AT BS 633, LBL 6. REPAIRED STIFFENER PER EA.Nov 25, 2009 · N511SW · Boeing 7375H4SDR SWAA097507Bulkhead · crackedDURING SCHEDULED 16Y CHECK, FOUND PRESSURE BULKHEAD WEB CRACKED AT BS 1016, BETWEEN STR 7R TO STR 15R. REPAIRED WEB AT SRM.Nov 24, 2009 · N378SW · Boeing 7373H4SDR 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.Nov 23, 2009 · Beech 200BEECHSDR 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 WNov 23, 2009 · N374AA · Boeing 767323SDR K11A2009112372505Angle · crackedAFT PRESSURE BULKHEAD UPPER ANGLE CRACKED 4 INCH CRACK.Nov 23, 2009 · N725CK · Boeing 727224SDR K11A2009112372503Stiffener · crackedAFT PRESSURE BULKHEAD HORIZONTAL STIFFENER CRACKED.Nov 23, 2009 · N725CK · Boeing 727224SDR 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.Nov 23, 2009 · N700GS · Boeing 7377H4SDR SWIA200923812Bulkhead · corrodedLEFT BULKHEAD WEB CORRODED. (C CHECK) REPAIRED PER SRM.Nov 21, 2009 · N712SK · Cndair CL6002C10SDR 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.Nov 21, 2009 · N450UW · Boeing 7374B7SDR SWIA200923160Bulkhead · crackedFS 621 BULKHEAD FORWARD FACE CRACKED ABOVE CARGO DOOR FITTING. (C-CHECK) REPAIRED PER REO.Nov 21, 2009 · N459SW · Cndair CL6002B19SDR 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.Nov 20, 2009 · N427ZW · Cndair CL6002B19SDR SWIA200923180Bulkhead · crackedFS 559 PRESSURE BULKHEAD CRACKED. (C-CHECK) REPAIRED PER REO.Nov 20, 2009 · N459SW · Cndair CL6002B19SDR 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.Nov 19, 2009 · N450UW · Boeing 7374B7SDR 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)Nov 19, 2009 · N428AW · Cndair CL6002B19SDR DL76L091854Pressure Panel · gougedPRESSURE WEB GOUGED UPPER SURFACE AT APPROX STA 970R AND RBL 90. REPAIR IN ACCORDANCE WITH ERA 478288-14.Nov 19, 2009 · N188DN · Boeing 767332SDR 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 Nov 19, 2009 · N8646A · Cndair CL6002B19SDR SWIA200923728Bulkhead · crackedFS 559 PRESSURE BULKHEAD CRACKED. (C CHECK) REPAIRED PER REO.Nov 18, 2009 · N459SW · Cndair CL6002B19SDR 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)Nov 17, 2009 · N428AW · Cndair CL6002B19SDR ASOA200901315Bulkhead · crackedFOUND 202 BULKHEAD CRACKED BETWEEN 12 AND 1 O`CLOCK.Nov 16, 2009 · N860AS · Cndair CL6002B19SDR 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.Nov 16, 2009 · N973CA · Cndair CL6002B19SDR SWIA200923109Bulkhead · crackedFS 621 BULKHEAD CRACKED. (C-CHECK) DAMAGE WITHIN LIMITS. BLENDED PER REO.Nov 16, 2009 · N432SW · Cndair CL6002B19SDR SWIA200923566Bulkhead · crackedFS 559 BULKHEAD CRACKED AT LBL 18 ON FRAME CAP ANGLE. (C CHECK) REPAIRED PER REO.Nov 15, 2009 · N432SW · Cndair CL6002B19SDR 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 NEWNov 15, 2009 · N617QX · Cndair CL6002C10SDR 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)Nov 14, 2009 · N438AW · Cndair CL6002B19
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