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 98ZZZX4541Bulkhead · crackedPARTS ARE THE COMPONENTS OF STA 90.00. THEY RIVET TOGETHER. THIS AREA IS WHERE THE FLOAT KIT IS INSTALLED. RIGHT AND LEFT FLOAT ATTACH AREA WAS CRACKED IN MANY PLACES. THIS AIRCRAFT HAS BEEN ON FLOATS MOST OF ITS LIFE. SUBMITTER SUGGESTED INSPECTION OF THSDR UPS98828210Bulkhead · crackedINSPECTION TYPE:D AT LONGERON 10L AT STA 1766 HAS A CRACK AT BULKHEAD. REMOVED STRAP FROM ACCESS. STOP DRILLED IAW DC8 SRM 53-7-5 FIG 9. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED STRAP IAW DC8 SRM 51-1-70DSDR UPS98828120Rib · crackedINSPECTION TYPE-D, CRACKED RIB AT XFS 385.25 LWR RIB LT L/E. REPAIRED IAW SRM 57-2-0.SDR RRXA99985Bulkhead · misdrilledDURING A MAINTENANCE VISIT, FOUND TRIPLE DRILLED RTAFT PRESS BULKHEAD, AT STA= 1766. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED MISDRILLED HOLES BY RIVET INSTALLATION IAW FAA APPROVED TIMCO DER ENGINEERISDR ABXA9801066Bulkhead Clip · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD 2ND RADIAL CRACKED AT END CLIP. REPLACED CLIP IAW DC9 SRM 51-30-5.SDR SWAA982581Bulkhead · crackedDURING SCHEDULED TRAN CHECK, FOUND CRACKED 178 BULKHEAD, RBL 4, WL 211.75-212 TO 25. CUT OUT CRACKED AREA AND REPAIRED PER BOEING SRM.SDR RRXA99645Bulkhead Web · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO BULKHEAD WEB AND FITTING BETWEEN STA -12 TO STA -32 AND LONGERON 23 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW WEB AND FITTISDR DL72S982206Bulkhead Web · crackedWEB AT STA 970 LOWER BULKHEAD WEB CRACKED RBL 10. REMOVED DAMAGED WEB AS PER SRM 51-40-2. FABRICATED REPAIR PARTS IAW SRM 53-10-9 FIG 4. OK TO INSTALL. STARTED INSTALLING REPAIR DOUBLER. COMPLETED REPAIR PER SRM 53-10-9 FIG 4.SDR DL72S982153Blkhd Stiffener · crackedTHE FS 1183 BULKHEAD VERTICAL STIFFENER AT RBL 36.83 WAS FOUND WITH TYPICAL CRACKING AT WL 240. THE CRACKED STIFFENER WAS REPAIRED PER BAC S/B 727-53-0192 AND DOCUMENTED PER ER/A 365894-14.SDR ABXA9801054Bulkhead Channel · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD DOOR HAD A CRACK ON BOTTOM CHANNEL. REPLACED LOWER CHANNEL IAW DC9 SRM CHAPTERS 51-10-2, 51-30-1 AND 51-30-5.SDR ABXA9801055Bulkhead Clip · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD 4TH RADIAL STIFFENER LEFT ATTACH CLIP CRACKED. REPLACED CLIP IAW DC9 SRM 51-30-1 AND 51-30-5.SDR 98ZZZX4068Web · buckledDURING ANNUAL INSPECTION, THE FRONT SPAR CARRY-THROUGH STRUCTURE FORWARD WEB WAS FOUND BUCKLED BELOW THE LT WING ATTACH FITTING. THE DAMAGE EXTENDED BETWEEN THE LOWER SKIN AND THE FITTING HORIZONTALLY FOR APPROX 12 INCHES. THERE WAS ADDITIONAL DEFORMATION INBOSDR DL73K982137Bulkhead Web · crackedTHE FS 178 BULKHEAD WEB WAS FOUND WITH A CRACK AT LBL 5.7, WL 212. THE WEB HAD A PREVIOUS REPAIR IN THE AREA FOR 3 OTHER CRACKS WHICH WERE CUTUOUT OF THE WEB. THE EXISTING REPAIR DOUBLER WAS REMOVED, THE NEW CRACK CUTOUT, THE WEB INSPECTED FURTHER AND A NESDR CKSA98610Blkhd Doubler · corrodedDURING ACCOMPLISHMENT OF CPCP TASK CARD 559R-0551, FOUND AFT BAGGAGE COMPARTMENT BULKHEAD DOUBLER CORRODED, FS 1218 BETWEEN LONGERON 24R AND 25R. REMOVED CORROSION IAW SRM 51-1-8, FOUND OUT OF LIMITS IAW SRM 53-2-0. INSTALLED NEW ANGLE IAW SRM 51-3-0, 51-1-SDR CKSA98609Blkhd Doubler · corrodedDURING ACCOMPLISHMENT OF CPCP TASK CARD NUMBER 559R-0551, FOUND AFT BAGGAGE COMPT BULKHEAD DOUBLER CORRODED LOCATION STA 1200, LONGERON 23R TO LONGERON 24R, CORROSION FOUND TO BE LOCAL. REMOVED CORROSION IAW SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW SRM 53-2SDR ABXA9800892Bulkhead · corrodedDURING C-CHECK, FOUND FALSE BULKHEAD, STATION 996 EXFOLIATED JUST ABOVE LONGERON 30. REPAIRED BULKHEAD IAW ABX REA D953-25069.SDR SWAA982506Bulkhead Skin · crackedDURING SCHEDULED 1/2D CHECK, FOUND HFEC INDICATION AT A1 CRACKED 178 BULKHEAD SKIN AT BS 178, LBL 1, WL 188 AFT SIDE. REPAIRED PER BOEING SRM.SDR AALA981962Bulkhead · crackedTUL - BULKHEAD 303 AT STRINGER 16L, BELOW DOOR STOP CASTING CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER PER ESO 11697, DATED 10/2/98. (M)SDR 9810459910Bulkhead · crackedDURING SURVEILLANCE INSPECTION, FOUND CRACK ON UPPER LEFT CORNER OF AFT PRESSURE BULKHEAD VENTRAL DOOR CUTOUT. REPAIRED PER EA 99-160501 (P/N 5910130-9).SDR TWAA9816504Bulkhead · corrodedDURING CHECK-C MAINT, FOUND AFT CARGO BIN WITH CORROSION AT BOTTOM OF AFT PRESSURE BULKHEAD, STA 1168, LBL 1 IN. INSTALLED NEW T PART NR 5910130-65, AND NEW GUSSET PER SRM 53-13-3, FIG 8 PAGE 19 AND 20.SDR SPAA9800007Bulkhead Web · corrodedDURING COMPLIANCE WITH AD 84-20-03, CORROSION WAS FOUND ON THE AFT PRESSURE BULKHEAD WEB, CHORDS, ANGLES AND FITTINGS AT BS 1016. REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH AN ALTERNATE METHOD THAT WAS APPROVED BY BOEING ENGINEERING. FAA FORM 8110-3 AND ACCOSDR AALA981869Bulkhead · corrodedTUL - FOUND 740 AFT BULKHEAD SKIN AND DOUBLER CORRODED. REMOVED CORROSION. REPLACED DOUBLER AND INSTALLED DOUBLER REPAIR PER SRM 51-40-2 PAGE 6B. (M)SDR SWAA982438Bulkhead Chord · crackedDURING SCHEDULED 1/2D CHECK, FOUND LT SIDE BULKHEAD CHORD CRACKED AT BS 178, LBL 32, WL 207. REPAIRED PER BOEING SRM.SDR SWAA982409Bulkhead Support · corrodedDURING SCHEDULED 1/2D CHECK, FOUND CORRODED AT AFT BULK HEAD PANEL SUPPORT ANGLE AT BS 500D. REMOVED AND REPLACED PER BOEING SRM.SDR MWEA98982Angle · crackedFOUND CRACK ON AFT SIDE OF AFT PRESSURE BULKHEAD -37 ANGLE. MTC FABRICATED AND INSTALLED DOUBLER REPAIR.SDR SWAA982389Bulkhead · corrodedDURING SCHEDULED D CHECK, FOUND CORRODED FLOOR TO BULKHEAD SUPPORT ANGLE AT BS 947.5 RBL 20, LBL 20. REMOVED AND REPLACED PER BOEING SRM.SDR SWAA982380Blkhd Bracket · crackedDURING SCHEDULED 1/2D CHECK, FOUND 1016 PRESS BULKHEAD FWD SIDE CENTERLINE AFT CLOSET TOP RT SUPPORT BRACKET CRACKED. REMOVED AND REPLACED PER BOEING SRM.SDR SWAA982375Bulkhead · crackedDURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED UNDER STRAP AT LBL 5.7, WL 201. REMOVED AND REPLACED PER TRAMCO ER 98-0891.SDR SWAA982374Bulkhead · crackedDURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED UNDER STRAP AT LBL 4.7, WL 200. REMOVED AND REPLACED PER TRAMCO ER 98-0891.SDR SWAA982373Bulkhead · crackedDURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED UNDER STRAP AT RBL 6.7, WL 212.5. REMOVED AND REPLACED PER TRAMCO ER 98-0891.SDR SWAA982372Bulkhead · crackedDURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED UNDER STRAP AT RBL 4.7, WL 212.5. REMOVED AND REPLACED PER TRAMCO ER 98-0891.SDR SWAA982371Bulkhead · crackedDURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED UNDER STRAP AT RBL 02, WL 207. REMOVED AND REPLACED PER TRAMCO ER 98-0891.SDR SWAA982370Bulkhead · crackedDURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED UNDER STRAP AT LBL 4.7, WL 201. REMOVED AND REPLACED PER TRAMCO ER 98-0891.SDR SWAA982369Bulkhead · crackedDURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED UNDER STRAP AT LBL 4.7, WL 198.5. REMOVED AND REPLACED PER TRAMCO ER 98-0891.SDR SWAA982368Bulkhead · crackedDURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD CRACKED UNDER STRAP AT LBL 4.7, WL 201. REMOVED AND REPLACED PER TRAMCO ER 98-0891.SDR EIAA980308Blkhd Stiffener · crackedPHX - DURING C-CHECK, AFT RPESSURE BULKHEAD AFT SIDE HAS A CRACKED STIFFENER AT 4 O'CLOCK AND 5 O'CLOCK POSITIONS. REPAIRED PER SRM 53-11-3. (M)SDR DL72S982075Bulkhead Beam · crackedFUSELAGE BULKHEAD FS 1183 LBL 18 VERTICAL BEAM, REPAIR FOR CRACK. A .75 INCH TYPICAL CRACK WAS FOUND IN RADIUS OF THE LBL 18 VERTICAL BEAM LOWER END ON THE FS 1183 BULKHEAD. THE CRACKED BEAM WAS REPAIRED PER BAC S/B 727-53-0202. THE REPAIR WAS DOCUMENTED PESDR TWAA9816312Buklhead Web · crackedDURING OP 16 MAINT CHECK, FOUND AT RT FUSELAGE BULKHEAD WEB AT STA 965.091, PYLON FROM SPAR LOWER CAP, HIGH FREQ EDDY CURRENT INDICATED CRACK IN LOWER OTBD BOLT HOLE. REAMED HOLE SIZE TO .02807 AND ELIMINATED.SDR SWAA982363Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CRACKED AFT SIDE OF BLKHD WL 195, RBL 26. REMOVED AND REPLACED PER BOEING SRM.SDR TSAA9853517Press Bulkhead · crackedDURING HEAVY CHECK, FOUND LEFT WHEEL WELL AREA BS 727 PRESSURE BULKHEAD CRACK APPROX 2.5 INCH LONG, LOWER CHORD. REPLACED LOWER CHORD IAW ECO 1785. (M)SDR SWAA982343Bulkhead Skin · crackedDURING SCHEDULED 1/2D CHECK, FOUND CRACKED 178 BULKHEAD SKIN AT BS 178, RBL 1, WL 188 AFT SIDE. REMOVED AND REPLACED PER BOEING SRM.SDR VJ9800536Bulkhead Angle · crackedATTACH ANGLE VERTICAL LEG ON SHEAR BEAM AT BS 664, S18R CRACKED BETWEEN THREE FASTENERS AND SHEAR BEAM AT BS 664, S18AL CRACKED IN RADIUS AT BULKHEAD ATTACH POINT. REMOVED, FABRICATED AND INSTALLED NEW ANGLE IAW B737 SB 53-1066, REPAIR KIT 65C29228-29. REMOSDR SWAA982301Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND CRACKED BULKHEAD AT RBL 5, WL 202, FWD SIDE. REPAIRED PER BOEING SRM.SDR SWAA982300Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND CRACKED BULKHEAD AT RBL 5, WL 199, FWD SIDE. REPAIRED PER BOEING SRM.SDR ABXA9800851Bulkhead Tee · corrosionDURING C-CHECK, FOUND CORROSION ON UPPER SURFACE OF THE FORWARD LEG OF THE TEE-ANGLE AT STATION 756 BL O.O. REPAIRED BULKHEAD TEE-ANGLE IAW REA D953-24842-MR.SDR SWAA982257Bulkhead Chord · crackedDURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD SIDE CHORD LT SIDE CRACKED AT WL 207. REPAIRED PER BOEING SRM.SDR SWAA982256Bulkhead Web · crackedDURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL .5, RBL .5, WL 187. REPAIRED PER BOEING SRM.SDR SWAA982255Bulkhead · crackedDURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD SIDE CHORD RT SIDE CRACKED AT WL 207. REPAIRED PER BOEING SRM.SDR SWAA982254Bulkhead Web · crackedDURING SCHEDULED D CHECK, FOUND OF BS 178 BULKHEAD WEB CRACKED UNDER STRAP AT LBL 6.7, WL 212. REMOVED AND REPLACED PER BOEING SRM.SDR AU981440Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD FORWARD FACE LOCATED AT STA 178 CRACKED IN THE FOLLOWING AREAS: 1. FORWARD PRESSURE BULKHEAD WEBS CRACKED IN FOUR PLACES IN THE AREA BELOW THE RADAR ANTENNA MOUNT POINTS. 2. VERTICAL CHORD RADIUS ON THE REAR FACE OF THE BULKH
Back to JASC 5312