JASC 5312
Service difficulty reports · 20,047
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 AU970623Bulkhead · cracked(AUS) LH AND RH FUSELAGE DOOR FRAME BULKHEADS CRACKED BEHIND LAP JOINTSDR ABXA9701371Bulkhead Clip · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD FORWARD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 15 RIGHT. REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.SDR CALA9701219Bulkhead · crackedINSPECTION FOUND AN 8 INCH CRACK IN FORWARD PRESSURE BULKHEAD OF NOSE WHEEL WELL ON LT SIDE APPROXIMATELY THREE INCHES OUTBOARD OF DOOR STOP. DOUBLERS WERE FABRICATED AND INSTALLED IAW BOEING DRAWING NR 65C17111.SDR 97FDEA00330Bulkhead Web · crackedNR 0759 029, NUMEROUS CRACKS IN 950 BULKHEAD WEB, LBL 60, WL 188 TO 199.SDR CALA9700923Bulkhead Web · corrodedINSPECTION FOUND WEB AND ANGLE CORRODED AT BULKHEAD IN AFT BAGGAGE BIN STA 1338, FROM L26L TO L24R. THE ANGLE AND WEB WERE REMOVED AND REPLACED IAW SRM 53-01.SDR 97ZZZM723Bulkhead · corrodedDURING C-CHECK INSPECTION, DISCOVERED CORROSION BETWEEN THE FUSELAGE SKIN AND THE AFT FLANGE FO THE STA 2360 PRESSURE BULKHEAD AFT OUTER CHORD. THE CORROSION EXTENDED ALONG THE ENTIRE WIDTH OF THE AFT CHORD FROM STRINGER 46R TO 51R. REPAIRED BY TRIMMING AWAYSDR SWIA97905Bulkhead · crackedDISCOVERED CRACK IN PRESSURE BULKHEAD (P/N 601R3208-123), JUST FORWARD OF WING LEADING EDGE FS 409+128.SDR SWIA97904Bulkhead · crackedDISCOVERED CRACK IN PRESSURE BULKHEAD (P/N 601R3208-123), JUST FORWARD OF WING LEADING EDGE FS 409+128.SDR SWIA97903Bulkhead · crackedDISCOVERED CRACK IN PRESSURE BULKHEAD (P/N 601R3208-123), JUST FORWARD OF WING LEADING EDGE FS 409+128.SDR SWIA97902Bulkhead · crackedDISCOVERED CRACK IN PRESSURE BULKHEAD (P/N 601R3208-123), JUST FORWARD OF WING LEADING EDGE FS 409+128. CRACK EXTENDED 160 INTO THE WEBBING AND CREATED CABIN PRESSURIZATION LOSS.SDR SWIA97901Bulkhead · crackedDISCOVERED CRACK IN PRESSURE BULKHEAD (P/N 601R3208-123), JUST FORWARD OF WING LEADING EDGE FS 409+128.SDR SWIA97900Bulkhead · crackedDISCOVERED CRACK IN PRESSURE BULKHEAD (P/N 601R3208-123), JUST FORWARD OF WING LEADING EDGE FS 409+128.SDR SWIA97899Bulkhead · crackedDISCOVERED CRACK IN PRESSURE BULKHEAD (P/N 601R3208-123), JUST FORWARD OF WING LEADING EDGE FS 409+128.SDR IXXA9700104Bulkhead Web · crackedDURING ROUTINE C-CHECK INSPECTION, THE AFT PRESSURE BULKHEAD WEB WAS FOUND CRACKED AT FUSELAGE STATION 1766, TX26 AND TZ67. REPAIR ACCOMPLISHED STOP DRILLING OF CRACK, FABRICATION AND INSTALLATION OF A REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANSDR 9711699987Bulkhead · crackedDURING M-CHECK, FOUND SEVERAL CRACKS IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE BULKHEAD FS 110. REPAIRED PER EA 99-112947.SDR P5CA9701068Bulkhead Web · corrodedLEVEL 2, LT WLG W/W CANTED BULHEAD WEB BULGED UP AT BS 1245, LBL 10. TRIMMED WEB BONDSKIN AREA 4 BY 6 AND DOUBLER REPAIRED PER BOEING SRM 51-40-02.SDR AU970826Bulkhead · cracked(AUS) FUSELAGE FORWARD PRESSURE BULKHEAD AT STATION 178 CRACKED IN SIXPLACES - FOUND USING EDDY CURRENT AND ULTRASONIC INSPECTIONS IAWER B73-53-10-39ASDR SWAA970532Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND CRACK INDICATION AT BS 178 BULKHEAD, WL 199.25 TO 199.75. REPAIRED PER TRAMCO EWO 97-0268 AND BOEING SRM.SDR SWAA970531Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND CRACK INDICATION AT BS 178 BULKHEAD, WL 212.25 TO 213. REPAIRED PER TRAMCO EWO 97-0268 AND BOEING SRM.SDR SWAA970528Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND CRACK INDICATION AT BS 178 BULKHEAD, WL 198 TO RBL 4.7. REPAIRED PER BOEING SRM.SDR CALA9701030Bulkhead · crackedINSPECTION FOUND A 2.5 INCH CRACK IN BULKHEAD AT APU LOAD CONTROL CUTOUT, BS 870. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5310-01544.SDR SWAA970525Bulkhead · oil canningDURING SCHEDULED C4 CHECK, FOUND AFT PRESSURE BULKHEAD OIL CANNING AT BS 1016. REPAIRED PER BOEING SRM.SDR CA970620018Cap · corrosion(CAN) HEAVY CORROSION ON LOWER CAP BULKHEAD 983 BETWEEN STR 30-34. REPAIRED.SDR AU970829Bulkhead · cracked(AUS) FUSELAGE FORWARD PRESSURE BULKHEAD WEB CRACKED IN FIVE PLACES - FOUND DURING EDDY CURRENT AND ULTRASONIC INSPECTION IAW ERB73-53-10-39ASDR AU970828Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD CRACKED IN THE FOLLOWING AREAS:-1. LH FORWARD PRESSURE BULKHEAD SIDE CHORD RADIUS AT WL 195 - CRACK LENGTH 63.5MM (2.5IN)2. LH INTERCOSTAL ADJACENT TO BULKHEAD AT WL 1953. RH INTERCOSTAL ADJACENT TO BULKHEAD AT WL 195SDR AU970600Door Post · cracked(AUS) FUSELAGE BULKHEAD DOOR POST FRAME CRACKEDSDR AU970563Bulkhead · cracked(AUS) LH AND RH LOWER DOOR POST BULKHEADS PNO 0512187-1 (LH) AND PNO0512187-2 (RH) CRACKED - FOUND DURING INSPECTION IAW SERVICEBULLETIN SEB 97-1SDR CALA9700916Bulkhead Web · crackedINSPECTION FOUND THREE CRACKS IN CANTED BULKHEAD WEB AT FS 1463 BELOW LONGERON 6R IN THE AFT ACCESSORY COMPARTMENT. THE CRACKS MEASURED FROM 1 TO 2 INCHES IN LENGTH. A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 53-14-4.SDR MWEA97440Bulkhead Doubler · crackedDURING D-CHECK, NR 2 HORIZ FORMER/DOUBLER AFT FWD RT SIDE CRACKED. MAINT REPAIRED IAW DAC J060110 VIEW W-W.SDR MWEA97439Bulkhead Doubler · crackedDURING D-CHECK, NR 3 HORIZ FORMER/DOUBLER ANGLE CRACKED. MAINT REPAIR IAW DAC DRWG J060110.SDR MWEA97438Bulkhead Angle · crackedDURING D-CHECK, NR 5 HORIZ FORMER/DOUBLER ANGLE CRACKED. MAINT REPAIRED IAW DAC DRWG J060110 VIEW T-T AND SRM 51-30-05.SDR MWEA97437Bulkhead Former · crackedDURING D-CHECK, NR 6 HORIZ FORMER/DOUBLER CRACKED. MAINT REPAIRED IAW DAC DRWG J060110 VIEW S-S.SDR MWEA97436Bulkhead Doubler · crackedDURING D-CHECK, NR 5 HORIZ DOUBLED CRACKED. MAINT REPAIRED IAW DAC DRWG J060110 VIEW T-T.SDR P5CA9700677Bulkhead · corrodedLEVEL 1 CORROSION, M/D CANTED PRESSURE BULKHEAD TO WING CTR SECTION TOP SKIN JOINT WITH ATTACHMENT FTG REMOVED BS 1241, LBL L11. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.SDR CALA9700892Bulkhead Support · corrodedINSPECTION FOUND T-SECTION FLOOR SUPPORT BEAMS ON FORWARD FACE OF AFT PRESSURE BULKHEAD AT LT AND RT SIDES CORRODED. SPLICE REPAIRS WERE PERFORMED IAW SRM 53-00-01 AND 53-40-00, PAGE 93, FIGURE 16.SDR SWAA970515Bulkhead Angle · corrodedDURING SCHEDULED D-CHECK, FOUND FLOOR TO BULKHEAD SUPPORT ANGLE CORRODED AT BS 500D. REPLACED PER BOEING SRM.SDR DHL9780540CBulkhead Angle · crackedAT C-CHECK, EMPENNAGE AFT OF PRESSURE DOME BULKHEAD FS 1781 LT SIDE ATTACH ANGLES 18 AND 19 TO PRESSURE DOME HAS HAIRLINE CRACK. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER DOUGLAS SRM 53-2-0 FIG 1B.SDR DHL9770266DBulkhead Web · crackedAT D-CHECK, CRACK ON WEB AT ANGLE ATTACH POINT AFT OF FS 1183 BLKHEAD AND RBL 8 APPROX 24 ABOVE TAILSKID CUT OUT. REMOVED TAILSKID DOOR FOR ACCESS. STOP DRILLED END OF CRACKS, HFEC, NO CRACKS BEYOND STOP DRILL. TRIMMED OUT WEB AROUND CRACK PER S/B 53-175. SDR AU970561Bulkhead · cracked(AUS) LH AND RH LOWER AFT DOOR POST BULKHEADS PNO 0512176-1 (LH) ANDPNO 0512187-2 (RH) CRACKED - FOUND DURING INSPECTION IAW CESSNA SEB 97-1SDR P5CA9700820Bulkhead Angle · crackedLWR FX INTERIOR STA 250 TO 260 FWD BULKHEAD FWD FACE ATT VERT ANGLE. REPAIRED PER BOEING SRM 51-40-04.SDR ABXA9701029Bulkhead Door · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD VENTRAL DOOR LT BEAM (P/N 3917853-1) CRACKED. REMOVED AND REPLACED BEAM IAW DC9 SRM 51-30-5.SDR MWEA97394Bulkhead Skin · crackedCRACK IN AFT SIDE OF AFT PRESSURE BULKHEAD SKIN ON RT SIDE OF VENTRAL DOOR JAMB. REMOVED AND REPLACED REPAIR IAW SRM 53-05 FIG 76.SDR CALA9700772Bulkhead Tee · corrodedINSPECTION FOUND T-SECTION FLOOR SUPPORT BEAM ON FORWARD FACE OF REAR PRESSURE BULKHEAD, LT SIDE CORRODED. A SPLICE REPAIR WAS INSTALLED IAW SRM 53-40-00 PAGE 93, FIGURE 16.SDR CKSA97252Bulkhead · crackedDURING HARD LANDING INSPECT, FOUND AFT PRESSURE BULKHEAD PIE SECTION AT 11 O'CLOCK POSITION OUTBOARD FASTENER ROW 16TH FROM TOP HOLE EMITS CRACK. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR ON AFT PRESSURE BULKHEAD PIE SECTION AT 11 O'CLOCK POSITION OTHER FASSDR CKSA97224Bulkhead Web · buckledDURING HARD LANDING INSPECTION, FOUND AFT PRESSURE BULKHEAD PIE SECTION SKIN AT 11 O'CLOCK POSITION BUCKLED. REMOVED AND REPLACED WEB GORE PER BOEING ENGINEERING RECOMMENDATIONS AND MSG CKF-ORD-97-0017RE PROCEDURES, EA 97-136, AND BOEING 8110-3 DATED 18 MAY 9SDR CKSA97215Bulkhead Web · bulgedDURING HARD LANDING INSPECTION, FOUND SEVERAL BULGES ON FS1480 BULKHEAD IN LEFT BODY MLG WELL. OK TO INSTALL REPAIR DOUBLER IAW BOEING DRAWING 65B15085 DATED 26 APR 97, BOEING ENGINEER RECOMMENDS REPAIR TO THE BUCKLE AREA LOCATED AT THE LEFT SIDE PER BOEING MSDR CKSA97214Bulkhead Web · bulgedDURING HARD LANDING INSPECTION, FOUND SEVERAL BULGES ON FS1480 BULKHEAD IN RIGHT BODY MLG WELL. BOEING ENGINEER RECOMMENDS REPAIR TO THE BUCKLE AREA LOCATED AT RIGHT SIDE PER BOEING MSG CKS-ORD-97-0037RE, CKF-ORD-97-0039RE AND BOEING DRAWING 65B28016-14. BOESDR P5CA9700919Bulkhead Skin · delaminatedLEFT WLG STN 1241 CANTED BULKHEAD FOUND SKIN DELAMINATED AT LBL 90 APPROX. REPAIRED PER BOEING SRM 51-40-15. PAINT TOUCH UP PER MM 51-24-11.SDR P5CA9700909Bulkhead Angle · crackedAFT CARGO STA 1480 BULKHEAD ATT ANGLE FOUND CRACKED AT RBL 38, LOCATED BETWEEN NR 5 AND NR 6 HORIZ STIFFENER COUNT FROM TOP. REPLACED SUPPORT WEB AND ANGLE PER BOEING SRM 51-10-01 AND INSTALLED PER SRM 51-30-02.SDR P5CA9700737Bulkhead Skin · delaminatedLEFT WLG STN 1241 CANTED BULKHEAD FOUND SKIN DELAMINATED AT LBL 90. REPAIRED PER BOEING SRM 51-40-15, PAINTED PER MM 51-24-1.
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