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 SWAA980346Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND 178 BULKHEAD WEB CRACKED AT WL 234 RBL 11.7 AND 12.7. REPAIRED PER BOEING SRM.SDR SWAA980345Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND 178 BULKHEAD WEB CRACKED AT WL 211 TO 212, RBL 6.7 AND WL 211 TO 212.5, LBL 6.7. REPAIRED PER BOEING SRM.SDR SWAA980344Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND 178 BULKHEAD WEB CRACKED AT WL 196.5+0 200, LBL 4.7 AND WL 199 TO 200 LBL 6.7. REPAIRED PER BOEING SRM.SDR SWAA980343Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT RBL 1 LBL 1, WL 187. REPAIRED PER BOEING SRM.SDR DL72S980616Bulkhead Ftg · damagedTHE BORE OF FS 870 BLKHD LT TERMINAL FITTING WAS O/S TO 4.605 DIAMETER TO REMOVE TOOLING DAMAGE. REWORKED PER ERA 331517-14.SDR AU980322Bulkhead · cracked(AUS) FUSELAGE LOWER CENTER SECTION FRAME/BULKHEAD CRACKED. THE MAIN CRACKING WAS FROM THE OUTBOARD CUTOUT FOR THE RT MAIN LANDING GEAR LEG. CRACKING WAS ALSO COMMENCING ON THE OPPOSITE CUTOUT AND ALSO ON THE OUTER EDGE WHERE THE OUTBOARD CASTING BOLTS TO THSDR CALA9800546Bulkhead Panel · crackedINSPECTION FOUND THE NLG WHEEL WELL FORWARD BULKHEAD TOP RIGHT PANEL, TOP LEFT PANEL, AND TOP CENTER PANELS CRACKED AT FASTENER HOLES. THE CRACKS WERE .5 TO 1 IN LENGTH. THE CRACKED AREAS WERE CUTOUT IAW SRM 51-40-2. REPAIR DOUBLERS AND FILLERS WERE FABRICASDR MWEA98359Clips · crackedFOUND THE AFT PRESSURE BULKHEAD RT RADIAL FORMER CRACKED ON OUTBOARD END. MTC TRIMMED OUT FORMER AND FITTED WITH NEW CLIPS.SDR MWEA98353Blkhd Doubler · crackedFOUND A RADIAL CRACK ON AFT PRESSURE BULKHEAD DOOR JAMB UPPER LEFT CORNER OF -13 DOUBLER. MTC REMOVED AND REPLACED -13 DOUBLER.SDR MWEA98352Blkhd Skin · crackedFOUND VERTICAL CRACK ON AFT PRESSURE BULKHEAD UPPER LEFT CORNER OF VENTRAL DOOR JAMB ON 3 WEB SKIN. MTC SPLICED NEW 3 SECTION SKIN.SDR MWEA98351Jamb · crackedFOUND CRACK IN AFT PRESSURE BULKHEAD FORWARD SIDE UPPER LEFT CORNER OF DOOR JAMB ON JAMB FLANGE. MTC SPLICED NEW JAMB SECTION.SDR MWEA98350Jamb · crackedFOUND CRACK ON AFT VENTRAL DOOR JAMB WEB LEFT SIDE. MTC SPLICED IN NEW SECTION WITH DOUBLER AND FILLER.SDR DLL19980580Bulkhead Cap · corrodedTHE LOWER CAP OF THE FS 983 BULKHEAD WAS FOUND CORRODED NEAR RBL 42.5 STR 28. THE LOWER FLANGE OF THE CAP WAS CUTOUT TO REMOVE THE DAMAGE. TWO REPAIR ANGLES WERE INSTALLED PER ER/A 364233-14, REV C TO REPAIR THE DAMAGE.SDR SWAA980311Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND CRACK INDICATION NOTED AT BS 178 BULKHEAD WEB AT LBL 57 WL 201.5 TO 202.75, LBL 5.7 WL 197.5 TO 198.75, LBL 5.7 WL 210.5-212.75, LBL 6 WL 200.5-201, LBL 9.75 TO 10.5 WL 218, RBL 5.0 WL 217 TO 218.75, RBL 5.0 WL 200.75 TO 201.5, SDR SWAA980302Skin · crackedDURING SCHEDULED SERVICE CHECK, FOUND SKIN 6 FASTENER HOLES CRACKED AT BS 947 STR 4L, 3 FASTENER HOLES CRACKED AT BS 1006 STR 4L AND 5 FASTENER HOLES CRACKED AT BS 1006 TO 1016 STR 10L. REPAIRED PER BOEING SRM.SDR 9807449933Bulkhead Web · crackedDURING M CHECK, FOUND A CRACK IN THE WEB OF THE FS 37 BULKHEAD AS VIEWED THROUGH ACCESS HOLE ABOVE THE LEFT UPPER RADOME GUIDE PIN HOLE. REPAIRED PER EA 99-154843.SDR 9807439933Bulkhead Web · crackedDURING M CHECK, FOUND CRACK IN THE WEB OF FS 37 BULKHEAD AS VIEWED THROUGH THE ACCESS HOLE ABOVE THE RIGHT UPPER RADOME GUIDE PIN. REPAIRED PER EA 99-154843.SDR 9805579920Doubler · crackedDURING L CHECK, FOUND CRACK IN AFT PRESSURE BULKHEAD VENTRAL DOOR CUTOUT LEFT -9 DOUBLER. REPAIRED PER EA 99-1562620.SDR TWAA9806815Bulkhead Angle · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND L ANGLE ON AFT PRESSURE BULKHEAD CRACKED AT S996, BELOW CUSP ANGLE LBL 58.5. REPLACED L ANGLE PER SRM 51-01, PAGE 1 ITEM C. (M)SDR SWA980263Bulkhead · corrodedDURING SCHEDULED D-CHECK, FOUND CORROSION AT BS 500D STR 26L TO 26R LOWER CENTER BULKHEAD SUPPORT ANGLE. REPAIRED PER BOEING SRM.SDR SWA980255Bulkhead Shroud · damagedDURING SCHEDULED D-CHECK, FOUND AT BS 727 BULKHEAD CEILING TO BULKHEAD APU DUCT SHROUD DAMAGED. REPAIRED PER BOEING MM.SDR IXXA9800048Bulkhead Cap · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON THE AFT PRESSURE BULKHEAD UPPER CAP AT FUSELAGE STATION 1606. REPAIR WAS ACCOMPLISHED BY STOP DRILLING OF CRACK, FABRICATION AND INSTALLATION OF A REPAIR ANGLE DOUBLER AND TRIPLER IN ACCORDANCE WITH FSDR ABXA9800192Bulkhead Tee · crackedDURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD NR 6 TEE CRACKED. REPLACED TEE IAW ABX EA 53-12-3.SDR SWA980234Bulkhead Panel · damagedDURING SCHEDULED D-CHECK, FOUND AT BS 727 BULKHEAD PANEL IS DAMAGED. REPAIRED PER BOEING MM.SDR SWA980232Bulkhead Angle · corrodedDURING SCHEDULED D-CHECK, FOUND CORROSION ON AFT BULKHEAD SUPPORT ANGLE AT BS 947.5. REPAIRED PER BOEING SRM.SDR AU980270Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD AT WL 207 CRACKED IN LT CHORD. WEB ALSO CONTAINED THREE CRACKS.SDR 98ZZZX1138Bulkhead · crackedBULKHEAD FOUND CRACKED DURING ANNUAL INSPECTION PER AD 72-07-09. EFFECTIVE DATE 4-1-72.SDR 98ZZZX1112Support · buckledDURING ANNUAL INSPECTION, FOUND REAR CABIN BULKHEAD SUPPORT (PN 0811075-10) BUCKLED. UPON FURTHER DISASSEMBLY, FOUND FITTING SEVERELY CORRODED.SDR DHL9872678DBulkhead Angle · crackedAT D CHECK, AFT CARGO BS 950 VERTICAL BULKHEAD WALL SUPPORT ANGLE IS CRACKED AT FLOOR LEVEL ATTACH POINT. INSTALLED ANGLE REPAIR PER SRM 51-40-4, 3 BY 2. N/R 3886.SDR CKSA98094Bulkhead Cap · crackedDURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION: BULKHEAD CAP 6:00 POS AT STA 1792 PREVIOUS REPAIR CRACKED. REMOVED DAMAGE. FABRICATED REPAIR DOUBLER IAW L1011 SRM 53-11-00 FIG 848. INSTALLED REPAIR IAW L1011 SRM 53-11-00 FIG 848. CORROSION TASK CARSDR VJ9800044Bulkhead · corrodedTWO FASTENER HEADS POPPED AND BULGING UNDER PRESSURE DOME AT STA 597, RBL 18. DRILLED NEW PANEL, FABRICATED FINGER DOUBLERS PLUS 2 ADDITIONAL DOUBLERS IAW DC9 SRM 51-10-2. TREATED AND PRIMED AREAS IAW DC9 SRM 51-10-3, INSTALLED NEW PRESSURE BULKHEAD PANEL, SDR DHL9872666DBulkhead Angle · corrodedAT D CHECK, AFT CARGO BS 1166 BULKHEAD CEILING ATTACH ANGLE CORRODED ON UPPER AND LOWER SURFACES FROM RBL 53 TO 23. REPLACED ATTACH ANGLE PER SRM 51-30-2. N/R 3694.SDR SWAA980209Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED SEVERAL PLACES. REPAIRED PER BOEING SRM.SDR MWEA98298Blkhd Stiffener · corrodedSTIFFENER AT LONGERON 13L OF CANTED BULKHEAD 1121 WAS FOUND EXFOLIATED. FABRICATED AND INSTALLED REPLACEMENT STIFFENER.SDR MWEA98297Bulkhead Skin · corrodedAPB SKIN WS FOUND CORRODED ON THE LOWER END FROM LONGERON 26 LEFT TO 22 RIGHT DAMAGED OUT OF LIMITS FROM LONGERON 28L TO 29R. CUT OUT DAMAGED AREAS FABRICATED AND INSTALLED DOUBLER REPAIR.SDR 98ZZZX1178Bulkhead · crackedBULKHEAD FOUND CRACKED AT RIGHT RUDDER STOP APPROXIMATELY .50 INCH LONG. REMOVED AND REPLACED BULKHEAD ASSY. THIS REPORT SUBMITTED IN C/W AD 72-07-09.SDR 98FDEA00159Bulkhead Tee · crackedN00474, Y-1156 PRESS BULKHEAD TEE-CAP RT END HAS TWO CRACKS IN LONG 39 AREA. FIRST CRACK MOVES DOWN CANTED VERT LEG TO RADIUS (2.4). SECOND MOVES DOWN CANTED VERT LEG THROUGH RADIUS AND AFT IN AFT HORIZ. LEG AND DISAPPEARS UNDER FITTING (2 VISIBLE). MODIFY SDR AU980492Bulkhead · cracked(AUS) LT AND RT FUSELAGE DOORPOST BULKHEADS CRACKED.SDR ABXA9800204Bulkhead Web · crackedFUSELAGE STA 857 LBL 16 THE MAIN LANDING GEAR FORWARD BULKHEAD WEB IS CRACKED AT THE ADF ANTENNA LEAD ACCESS PANEL. REPAIRED IAW DC8 SRM 51-3-0.SDR 98FDEA00152Bulkhead · crackedCENTER WHEEL WELL COMPARTMENT RIGHT HAND VERTICAL BULKHEAD CRACKED AT UPPER AFT CORNER, APPROX FUS STA 1501. *S/D* INSTALLED DOUBLER AS PER SRM 53-00-01. N/R N00355.SDR AALA980431Bulkhead Beam · crackedTUL - FORWARD SIDE 1183 BULKHEAD LBL 8, VERTICAL STIFFENER CRACKED IN RADIUS OUTBOARD SIDE ABOVE RADIUS BLOCK. STOP DRILLED END OF CRACK AND INSTALLED REPAIR DOUBLERS IAW SB 727-53-0175, FIG 3. TST: 57,207 HOURS. CYCLES: 35,211. (X)SDR 9807579996Bulkhead Chord · corrodedDURING M CHECK, FOUND CORROSION ON UPPER SURFACE OF LOWER FORWARD FLANGE OF FS 110 BULKHEAD T CHORD OUTBOARD OF RIGHT TRUNNION SUPPORT BEAM IN THE NOSE LANDING GEAR WHEEL WELL. REPAIRED PER EA 99-156582.SDR MWEA98277Bulkhead Web · elongated holesTHE AFT PRESSURE BULKHEAD WEB HAS 3 ELONG HOLES ON LT SIDE DOOR JAMB STA Z34 TO 48. MTC FABRICATED REPAIR DOUBLER AND BUSHINGS IAW SVC MSP-0172/PDG ATA 09-053-30-01 DATED 09FEB98.SDR MWEA98275Bulkhead Tee · corrosionTHE AFT PRESSURE BULKHEAD VENTRAL DOOR JAMB LOWER RT HORIZONTAL TEE HAS CORROSION. MTC FABRICATED REPLACEMENT TEE.SDR MWEA98274Bulkhead Clip · corrodedTHE AFT PRESSURE BULKHEAD VENTRAL DOOR JAMB LOWER RT TEE ANGLE ABOVE GUSSETT AND RT TEE CLIP INBOARD OF GUSSET AROUND FASTENERS HAS CORROSION. MTC REMOVED CORROSION.SDR CKSA98190Bulkhead Web · puncturedDURING ROUTINE C-2 CHECK INSPECTION, FOUND NUMEROUS PUNCTURES ON LOWER END OF 9G BULKHEAD. FABRICATED REPAIR DOUBLERS TO REPAIR PUNCTURES ON LOWER END OF 9G BULKHEAD, DRILLED AND DEBURRED DOUBLERS AND BULKHEAD, TREATED, PRIMED AND INSTALLED DOUBLERS IAW DC8 SSDR CKSA98189Bulkhead Angle · brokenDURING ROUTINE CPCP INSPECTION, FOUND BULKHEAD ATTACH ANGLE RT SIDE BETWEEN C AND D PITS FS 1320 HAS AREA BROKEN OUT AT TWO HOLES WHERE ATTACH ANGLE ATTACHES TO FRAME. REPAIRED BROKEN BULKHEAD ATTACH ANGLE RT SIDE BETWEEN C AND D PITS IAW DC8 SRM 53-2-0 FIG 1SDR MWEA98248Blkhd Stiffener · corrodedTHE STIFFENER ON LONGERON 14R CANTED BULKHEAD 1121 WAS FOUND CORRODED. REMOVED AND REPLACED STIFFENER.SDR MWEA98247Blkhd Stiffener · corrodedTHE LONGERON 10R STIFFENER ON THE AFT SIDE OF THE STA 1121 CANTED FRAME WAS FOUND CORRODED. REMOVED AND REPLACED STIFFENER.SDR MWEA98246Blkhd Stiffener · corrodedTHE 1121 CANTED BULKHEAD LONGERON 13L STIFFENER WAS FOUND CORRODED. REMOVED AND REPLACED STIFFENER.
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