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 ABXA9900596Bulkhead Angle · crackedDURING C-CHECK, FOUND CRACKED ANGLE ON AFT PRESSURE BULKHEAD AT LONGERON 15 LEFT. REPLACED ANGLE IAW DC9 SRM 51-30-5.SDR ABXA9900595Bulkhead Angle · crackedDURING C-CHECK, FOUND CRACKED ANGLE ON AFT PRESSURE BULKHEAD AT LONGERON 14 RIGHT. REPLACED ANGLE IAW DC9 SRM 51-30-5.SDR ABXA9900594Bulkhead Angle · crackedDURING C-CHECK, FOUND A CRACKED ANGLE ON THE AFT PRESSURE BULKHEAD AT LONGERON 12 RIGHT. REPLACED ANGLE IAW DC9 SRM 51-30-5.SDR ABXA9900593Bulkhead Angle · crackedDURING C-CHECK, FOUND A CRACKED ANGLE ON THE AFT PRESSURE BULKHEAD AT LONGERON 16 RIGHT. REPLACED ANGLE IAW DC9 SRM 51-30-5.SDR 99ZZZX2792Firewall · crackedFOUND FIREWALL CRACKED AT LOWER COWLING SHOCK MOUNT BRACKET ADJACENT TO BATTERY TRAY. CRACK EXTENDED FROM BRACKET ATTACH RIVET HOLE VERTICALLY AND WAS APPROXIMATELY 1.75 INCHES LONG. CRACK WAS STOP DRILLED AND PATCHED WITH DOUBLER IAW CESSNA SBA 98-57-02.SDR 99ZZZX2788Firewall · crackedCW CESSNA SB 98-53-02. FOUND FIREWALL CRACKED 1.25 INCHES AT LOWER COWLING MOUNT BRACKET ADJACENT TO FIREWALL. CRACK EXTENDED VERTICALLY BETWEEN TWO RIVET HOLES OF INNER BRACKET. AIRCRAFT NOT AFECTED BY SERVICE BULLETIN BY S/N.SDR 20000502AP014Bulkhead · crackedDURING A ROUTINE ACE CAMP INSPECTION NR 6, HEAVY AFT FUSELAGE AND EMPENNAGE, FOUND MULTIPLE CRACKS IN CANTED BULKHEAD, STATION 588.10, IN EXCESS OF CRACK LIMITS PROVIDED IN BEECHCRAFT SERVICE BULLETIN 2564, REV 1 INCORPORATION OF SB 2564 KIT NR 129-4005-1S BEISDR SWAA991185Bulkhead · crackedDURING SCHEDULED RON, FOUND BS 1016, STRINGER 6L AFT BULKHEAD CRACKED. REPAIRED BULKHEAD PER SWA RA NR 1-253-2116.SDR AU990732Bulkhead · cracked(AUS) FUSELAGE AFT BULKHEAD LOCATED AT STN 209.0 CRACKED IN THE UPPER RT CORNER ADJACENT TO THE RT HORIZONTAL STABILIZER ATTACHMENT FITTING.SDR 99ZZZX2924Bulkhead · crackedDURING AN ANNUAL INSPECTION, FOUND MAIN BULKHEAD P/N 1156 CRACKED IN THE WING STRUT AREA. CAUSE UNKNOWN.SDR EIA990245Bulkhead Ftg · crackedHKG - DURING C/D CHECK, BS 1241 BULKHEAD FITTING AT RIGHT SIDE, CRACK FOUND OF OUTBOARD FITTING LEG UPPER MOST BOLT HOLE. REPAIRED FITTING PER RS-R-53-43-34090 REV B, 8110-3. (M)SDR 9903259750Bulkhead Channel · crackedDURING PERIODIC CHECK, AFT PRESSURE BULKHEAD SILL CHANNEL WAS FOUND WITH 2 INCH CRACK FROM FASTENER TO LIP OF FLANGE AT FLOOR. REPAIRED PER EA 97-164468 (P/N 5910130-37).SDR USAA990692Bulkhead · corrodedPIT - DURING Q2 CHECK, FOUND CORROSION SEVERAL INCHES IN 3 DIFFERENT DIRECTIONS AT STATION 996 LONG 18 AREA AT BULKHEAD/FLOORBEAM AND BELL FRAME TIE IN. CORROSION LEVEL 1/2, CORROSION TASK NR C57-53300. REMOVED AND REPLACED T-CAP SECTION. (M)SDR SWAA991165Bulkhead · corrodedDURING SCHEDULED D-CHECK, FOUND 5 CRACKS AT BS 178 BULKHEAD BETWEEN LBL 6 RBL 6. REPAIRED BULKHEAD PER SRM.SDR USAA990686Bulkhead Web · crackedPIT - DURNG PILOT REPORT, FOUND 1.5 INCH HORIZONTAL CRACK AT FORWARD PRESSURE BULKHEAD WEB LOWER LEFT BEHIND NLG TRUNNION 2 INCHES ABOVE BULKHEAD SKIN CLIP. REMOVED DAMAGE. INSTALLED DOUBLER AND FILLER PER EA 52402. (M)SDR SWAA991142Bulkhead · crackedDURING SCHEDULED C1 CHECK, FOUND BS 1016 BULKHEAD CRACKED AT STRINGER 6L. REPAIRED BULKHEAD PER SWA RA NR 1-253-2113.SDR EIA990228Bulkhead Web · crackedHKG - DURING C/D CHECK, LEFT BS 1480 BULKHEAD AREA STRINGER 36L, CHORD FASTENER HOLE CRACKED. BULKHEAD FASTENER HOLE REPAIRED AND STRINGER END REPLACED PER RS-R-53-43-34100, 8110-3. (M)SDR SWAA991140Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND CRACKED BULKHEAD, BS 178, LBL 6.5. REPAIRED BULKHEAD PER SRM.SDR SWAA991141Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND CRACKED BULKHEAD, BS 178, RBL 1 - LBL 1. REPAIRED BULKHEAD PER SRM.SDR DL73K991521Bulkhead · crackedDURING CORROSION VISIT, 3 INCH CRACK IN 178 BULKHEAD WAS REPAIRED PER SRM 53-10-11 FIG 1 REFER TO NR62.SDR SWAA991122Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND 2 EA CRACKS, BS 178 BULKHEAD RBL 1 AND LBL1. REPAIRED BULKHEAD PER SRM.SDR DL757991495Bulkhead · damagedTHE SUBJECT AIRCRAFT SUFFERED A HARD LANDING ON THE NOSE GEAR WHICH CAUSED BUCKLING OF THE FS 395 BULKHEAD LOWER CHORD AND WEB AND WRINKLING OF THE ADJACENT LT AND RT SKIN PANELS. THE SKIN PANELS, BULKHEAD CAP AND WEB WERE REMOVED AND REPLACED WITH NEW PARSDR ABXA9900565Bulkhead Beam · crackedTHE J-BEAM ON AFT SIDE OF AFT PRESSURE BULKHEAD AT STATION 1766 WAS CRACKED. REPAIRED IAW ABX REA D853-28119MR.SDR 99UAL900380Bulkhead Fitting · misdrilledTWO PRODUCTION HOLES WERE FOUND MISDRILLED AT S29L END FITTING (P/N 65-60208-1), LOCATED AT BS 1183 BULKHEAD CHORD (P/N 65-16350-5) WL 150,LBL 10. THE INBOARD HOLE WAS REPAIRED WITH A FREEZE PLUG, WHILE THE OUTBOARD HOLE WAS OVERSIZED. THIS REPAIR WAS APPROVSDR SWAA991105Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND CRACK 3 INCHES LONG, BS 1016 BULKHEAD, STRINGER 6L. REPAIRED BULKHEAD PER XEA X2-53-248.SDR P5CA9900630Bulkhead · crackedCRACKS FOUND ON BS 1000 IN THE RADIUS BETWEEN STR 46 AND 47 LEFT AND RIGHT SIDES. STOP DRILLED, EDDY CURRENT PER SB 530-2316R1 AND SRM 51-10-01 FIG 2.SDR P5CA9900629Bulkhead Flange · crackedFOUND CRACK ON FLANGE OF PRESSURE BULKHEAD AT BS 140 WL 280 BL 10L. TRIMMED DAMAGED AREA AND FABRICATED NEW ANGLE PER SRM 51-40-03 AND 51-10-02.SDR DLL10991484Bulkhead Web · crackedWHILE ACCOMPLISHING HFEC INSPECTIONS OF THE UPPER GORE WEB OF THE AFT P-DOME, A 2.5 INCH CRACK WAS FOUND IN THE WEB AT LBL 10. THE CRACK IS TYPICAL OF LAC S/B 093-53-258 (MANDATED PER AD 95-17-03). THE CRACK WAS REPAIRED WITH A DOUBLER AND TRIPLER PER THE S/SDR AU990961Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD RT SIDE CHORD RADIUS CRACKED AT FLOOR LEVEL. FOUND DURING EDDY CURRENT INSPECTION IAW ER B73-53-10-39.SDR MWEA99374Bulkhead · crackedAFT CANTED BULKHEAD HAS A 1.5 INCH CRACK THROUGH GUIDE PIN HOLE. MTC FABRICATED AND INSTALLED DOUBLER.SDR SWAA991085Bulkhead · crackedDURING SCHEDULED D CHECK, FOUND FUSELAGE BULKHEAD CRACKED, BS 727, LBL 16, WL 176. REPAIRED BULKHEAD PER ER NR 99-5455.SDR CALA9900722Bulkhead Angle · wornINSPECTION FOUND ANGLE STIFFENER WORN THREE QUARTERS OF WAY THROUGH FROM STAINLESS LINE ON LT SIDE OF APB AFT FACE. REPAIRED IAW ECRA 5330-02837.SDR ASAA9910176Bulkhead Chord · crackedPHX - DURING SCHEDULED D-CHECK, THE BULKHEAD VERTICAL CHORD STATION 178 LBL 5.7 AT WL 190 CRACKED. REPAIRED PER SRM 53-10-11. (M)SDR ASAA9910175Bulkhead · crackedPHX - DURING SCHEDULED D-CHECK, THE BULKHEAD AT STATION 178 RBL 11 AND WL 218 FORWARD SIDE CRACKED. REPAIRED PER SRM 53-10-11. (M)SDR ASAA9910173Bulkhead Chord · crackedPHX - FOUND SCHEDULED D-CHECK, THE BULKHEAD SIDE CHORD RADIUS STATION 178 AT WL 207 FOUND CRACKED. REPAIRED PER SB 737-53A1173. (M)SDR ASAA9910152Bulkhead Web · crackedPHX - DURING SCHEDULED D-CHECK, THE WEB ON THE AFT SIDE OF BULKHEAD STATION 182 RBL 20 WAS FOUND CRACKED. REPAIRED PER SRM 51-40-2. (M)SDR USAA069961Bulkhead · crackedAFT AIRSTAIR EXTERNAL ACCESS PANEL 3902, BS 1183 PRESSURE BULKHEAD CRACKED AT EDGE OF RADIUS BLOCK RBL 16, AT 8 INCHES UP FROM BOTTOM, AND FROM 10 INCH ABOVE BOTTOM TO 14 INCH ABOVE BOTTOM. INSTALLED DOUBLER REPAIR AT FS 1183 PRESSURE BULKHEAD AT EDGE OF RADISDR TWAA9908904Bulkhead Brace · crackedDURING OP 16 MAINT CHECK, FOUND AFT PRESSURE BULKHEAD, FORWARD SIDE DIAGIONAL BRACE ON PRESSURE BULKHEAD AT STA 996, CRACKED AT UPPER END BETWEEN LONGERON 3L AND 4L. REMOVED, FABRICATED AND REINSTALLED ANGLE AT UPPER DIAGONAL BRACE, STA 996 BETWEEN L3L ANG L4SDR ABXA9900845Bulkhead · corrodedDURING D-CHECK, FOUND THE FORWARD PRESSURE PANEL, LEFT FORWARD CORNER OF KEEL AREA FINGER DOUBLER CORRODED. REPLACED FINGER DOUBLER IAW DC9 SRM 51-30-2.SDR USAA990565Bulkhead · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH, 1 INCH AND .75 INCH CRACK AT STATION 178 RIGHT SIDE PLUS 6 INCHES WL 200 AT 4.75 AND 6.75 BULKHEAD. INSTALLED DOUBLER PER SRM 53-10-07. (M)SDR USAA990564Bulkhead · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 178 BULKHEAD RBL 314 WL 187. INSTALLED DOUBLER PER SRM 53-10-08 FIG 203. (M)SDR UIEA9933Bulkhead Splice · crackedCRACKS FOUND ON WEB SPLICE PLATE HOLES NR 11 RIGHT AND NR 23 RIGHT. HOLE NR 11 RIGHT, INSTALLED SEPRATE BUSHINGS IN EACH PART PER SB 747-53A2390 FIG 14. HOLE NR 23 RIGHT, REPAIRED OVERSIZE HOLE IN WEB SPLICE PLATE BULKHEAD. CHORD AND WEB PER BUSHING REPAIR SDR UIEA9932Builkhead Splice · crackedCRACKS FOUND ON WEB SPLICE PLATE HOLES NR 11 LEFT AND NR 21 LEFT. HOLES NR 11 LEFT, INSTALLED SEPARATE BUSHINGS IN EACH PART PER SB 747-53A2390 FIG 14. HOLE NR 21 LEFT, REPAIRED OVERSIZE HOLE IN BULKHEAD. CHORD AND WEB PER BUSHING REPAIR PER SB 747-53A2390 SDR GAIA9991Bulkhead Chord · corrodedFOUND DURING SCHEDULED MAINTENANCE AT AAR/OKC MAINTENANCE FACILITY. AT STATION 351.2, FOUND SKIN BULGING AND RIVETS PULLING THROUGH AT STRINGER 26L. REPAIRED FRAME IAW BOEING SRM 51-40-3 AND FVI DRAWING 53-99084-11. THE AIRCRAFT WAS RETURNED TO SERVICEABLE SDR GAIA9978Bulkhead Beam · gougedFOUND DURING ROUTINE SCHEDULED MAINTENANCE AT AAR/OKC MAINTENANCE FACILITY. LEFT SUPPORT BEAM FOR 9G BULKHEAD IS GOUGED AND RUBBED 72 INCH ABOVE FLOOR AT LBL 45. BLENDED GOUGE IAW B727 SRM AND FVI DRAWING 63-99094-1. THIS REPAIR HAS BEEN APPROVED BY THE FAASDR SWAA991052Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD CRACKED AT LBL 9, WL 234. REPAIRED BULKHEAD PER SRM.SDR RRXA991095Bulkhead · leakingAT APPROXIMATELY FLT LEVEL 230 CABIN PRESS WENT TO 10,000 FT, LEVEL OFF A FLT 220 TO MAINTAIN CABIN PRESSURIZATION. AIRCRAFT FERRIED TO EDDF FOR REPAIR. AFT PRESURE BULKHEAD REPAIRED PER BOEING ROD SKETCH 99-06-22-001, REF : EWA M/A NR AM-5312-01:00 AND WORKSDR RRXA991686Bulkhead · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BULKHEAD MOUNT AT Y=1360 BETWEEN LONGERONS 34 LEFT TO 34 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED MOUNT, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW MOUNT IAW DCSDR RRXA991484Bulkhead · crackedDURING A MAINTENANCE VISIT FOUND CRACK, AFT PRESSURE BULKHEAD AT STA 1766, BETWEEN LONGERONS 10 LEFT AND LONGERON 11 LEFT, APPROX 3-1/2 CRACK BETWEEN BL 35.0 RIGHT AND BL 35.750 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DCSDR RRXA991482Bulkhead · crackedDURING A MAINTENANCE VISIT FOUND CRACK, AFT PRESSURE BULKHEAD AT STA 1766 BETWEEN LONGERONS 10 RIGHT AND LONGERON 11 RIGHT, APPROX 3.75 INCH CRACK BETWEEN BL 33.50 LEFT AND BL 37.00 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW
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