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 97ZZZX2006Bulkhead Web · crackedDURING 'C' CK INSPECTION ACCOMPLISHED VISUAL AND DYE PENETRANT INSPECTION OF THE AFT PRESS BULKHEAD WEB IAW SB 53-73 REV 1. FOUND A CRACK AT RT FWD SIDE OF THE APB WEB AT I/B SIDE OF VERTICAL STIFFENER ABOVE FASTENER ROW. ACCOMPLISHED TERMINATING ACTION BY RSDR USAA970172Bulkhead · chafedPIT - DURING Q1 CHECK, FOUND CHAFE .50 INCH LONG BY .016 INCH DEEP AFT SIDE OF REAR PRESSURE BULKHEAD JUST FWD AND ABOVE THE 'X' FEED VALVE. INSTALLED DOUBLERS PER EA 46859. (X)SDR USAA970170Bulkhead · gougePIT - DURING Q1 CHECK, FOUND .010 INCH DEEP GOUGE ON THE AFT PRESS BULKHEAD FWD FACE BEHIND THE RIGHT THRUST REVERSER PULLEY. INSTALLED DOUBLER PER EA 46791. (X)SDR USAA970169Bulkhead · gougePIT - DURING Q1 CHECK, FOUND .018 INCH GOUGE ON THE AFT PRESS BULKHEAD FWD FACE BEHIND THE LEFT THRUST REVERSER PULLEY SECTOR. INSTALLED DOUBLER PER EA 46791. (X)SDR 9709506603Bulkhead Web · corrodedDURING TRANSITION CHECK, FOUND CORROSION AT BOTTOM OF CANTED BULKHEAD WEB FS 1241, LBL 35 - 50. REPAIRED PER EA 66-120416.SDR 9708989966Bulkhead · crackedDURING M-CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE BULKHEAD AT FS 83. REPAIRED PER EA 99-112876.SDR MWEA97329Bulkhead Angle · corrodedDURING INSPECT, RT BULK LWR SKIN AFT ATTACH ANGLE FS 965 CORRODED BEYOND LIMITS. MAINT REPAIRED IAW SRM 51-30-5.SDR MWEA97328Bulkhead Web · corrosionDURING INSPECT, RT FWD FACE APB LONG 24R MOD CORROSION FOUND. MAINT REPAIRED IAW DAC TELEX SVC-MSP-0234/AJC 25 FEB 97.SDR MWEA97318Bulkhead Skin · corrodedDURING INSPECT, AFT PRES BULK SKIN AT FS 996 FROM 23L TO 25R CORRODED BEYOND LIMITS. MAINT REPAIRED IAW SRM 53-03 FIG 9.SDR 97ZZZX2298Ring Assy · crackedRIGHT LOWER 137.50 BULKHEAD RING ASSY CRACKED 1 INCH UP AND COMPLETELY THROUGH SKIN ATTACH TURN-BACK. THIS CRACK IS RELATED TO FLOAT LIGHT INSTALLATION.SDR 97ZZZM580Bulkhead Web · crackedDURING C-CHECK INSPECTION, ACCOMPLISHED VISUAL AND DYE PENETRANT INSPECTION OF THE AFT PRESS BULKHEAD WEB IAW S/B 53-73 REV 1. FOUND A CRACK ON RIGHT FORWARD SIDE OF THE APB WEB AT INBOARD SIDE OF VERTICAL STIFFENER ABOVE FASTENER ROW. ACCOMPLISHED TERMINATISDR SWAA970405Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT RBL 4.7, WL 199 TO 197.75. REPAIRED PER TRAMCO EWO 97-0198.SDR SCNA97130Bulkhead · crackedDURING HEAVY MAINTENANCE VISIT, CRACK IN BULKHEAD 1223 IN AFT AIRSTAIR AREA. REMOVED CRACK IN BULKHEAD, FABRICATED AND INSTALLED WEB AND L-ANGLE REPAIR IAW B727 SRM 51-40-02 AND 51-20-03.SDR ABXA9700925Bulkhead Web · crackedDURING C-CHECK, FOUND THE UPPER CARGO BULKHEAD AT F/STA 786 LT WEB CRACKED. REPAIRED IAW ABX REA D953-19255-MR.SDR GAIA2097Bulkhead · crackedDURING C-CHECK INSPECTION, A ONE INCH CRACK WAS FOUND IN RIGHT FUSELAGE STATION 766.63 HORIZONTAL STABILIZER ATTACH POINT BULKHEAD. THE BULKHEAD WAS REPAIRED IAW TRACOR MSG NR 505-97-WLD-047 DATED 2-26-97 TFS/ASD FAA DER APPROVED. (M)SDR DHL9780137CBulkhead · crackedAT C-CHECK, IN ACCESSORY COMP SUSPECT CRACK ON PRESSURE BULKHEAD BETWEEN STR 29 AND 30. CONFIRMED CRACK BY DYE PEN. STOP DRILLED CRACK. FABRICATED REPAIR ANGLES PER EO 97042501, TREATED AND PAINTED. INSTALLED ANGLES PER EO AND SRM 51-121 AND 51-1-20D.SDR 9712259615Bulkhead Web · corrodedDURING M-CHECK AND PRIOR TO ENTERING SERVICE, FOUND CORROSION ON CANTED PRESSURE WEB AT FS 690 BETWEEN LBL 20 TO LBL 60. REPAIRED PER EA 99-100062.SDR RRXA97155Bulkhead Web · cutDURING A MAINTENANCE VISIT, FOUND CUT IN BULKHEAD WEB, AT Y=980 AND X=+59. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH C44-R30.SDR SWAA970400Bulkhead Support · corrodedDURING SCHEDULED D-CHECK, FOUND FLOOR TO BULKHEAD SUPPORT AT BS 500D CORRODED FROM RBL 17 TO LBL 5. REPAIRED PER BOEING SRM.SDR SWAA970399Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BULKHEAD BS 178 CRACKED, AT WL 212 TO 212.5, LBL 6.7. REPAIRED PER T1-353-046.SDR DL72S970784Blkhd Stiffener · crackedCRACKS WERE FOUND IN THE VERT STIFF AT RBL 36.83 AND LBL 36.83 ON THE FWD SIDES OF THE BS 1183 BLKHD. THE CRACKS ARE APPROX 1.5 LONG AND ARE LOCATED AT APPROX WL 238 IN THE O/B RADIUS OF THE AFT CHORD. THIS AREA IS ADDRESSED BY S/B 727-53-0192 (EO 4-59821-3)SDR DHL9780105CBulkhead · crackedAT C-CHECK, AFT PRESSURE BULKHEAD AT FS 1766 RIGHT SIDE AT LONGERON 11 BETWEEN STIFFENER 5772638-51 AND -49, THERE IS A 3.50 CRACK ON THE BULKHEAD. CUT OUT CRACKED AREA OF SKIN, FABRICATED REPAIR AND INSTALLED PER SRM 53-2-5.SDR DHL9780103CBulkhead · crackedAT C CHECK, AFT PRESSURE BULKHEAD FWD SIDE AT FUSELAGE STATION 1766 LEFT AT LONGERON 11 BETWEEN STIFFENER 5772638-49 AND STIFFENER -51 , HAS A 2.75 IN CRACK. CUT OUT CRACKED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-2-5 .SDR USAA970139Bulkhead Skin · crackedINT - DURING 'Q-5' CHECK VISUAL INSPECTION, FOUND 3 CRACKS IN BULKHEAD 1 INCH, 1 INCH AND 2.0 INCH 178 BULKHEAD SKIN RLB 5, LBL 7, 6 INCH - 9 INCH BELOW FLOOR LEVEL. INSTALLED DOUBLER, REPAIRED PER TR 53-10-07. (X)SDR USAA970136Bulkhead Angles · crackedPIT - DURING Q1 VISIT, FOUND 1 INCH CRACK LEFT SIDE, .50 INCH CRACK RIGHT SIDE AT FUSELAGE CTR PRESS BULKHEAD ANGLE CRACK, STR NR 11 AND STR NR 64. INSTALLED ANGLE REPAIRS PER US AIRWAYS EA NR 46607. (X)SDR UPS97822831Bulkhead · corrodedINSPECTION TYPE-C, AFT PRESS BULKHEAD STA 1766 HAS CORROSION AROUND VHF 1 RUN G FEED THROUGH DISCOUNT COUPLING. REPAIRED IAW TIMCO REO NR 03035, REV A AND DC8-53-1787.SDR SWAA970396Bulkhead · dentedDURING SCHEDULED C4 CHECK, FOUND AFT PRESSURE BULKHEAD DENTED AT FLOOR LEVEL, BS 1016. REPAIRED PER BOEING SRM.SDR UPS97822897Bulkhead Beam · corrodedINSPECTION TYPE-D, CORROSION REMOVAL ON AFT PRESSURE BLKHD VERT BEAM AT FS 1754 BL 0 TO LBL 2 IS OUT OF LIMITS AND HAS CRACK AT BOTTOM FASTENER HOLE TO EOP (REF N/R 535205). FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-2-0 FIG 1B, 51-1-20, 51-1-21, AND DHSDR IXXA9700094Bulkhead Angle · crackedDURING ROUTING C-CHECK INSPECTION, A ONE INCH CRACK WAS FOUND ON THE AFT PRESSURE BULKHEAD CIRCUMFERENTIAL MOUNT ANGLE AT FUSELAGE STATION 1766, STIFFENER 3 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED ANGLE, FABRICATION AND INSTALLATION OF A NEW MOUNT ANGLESDR EIAA970109Bulkhead Support · crackedHKG - DURING C5/D INSPECTION, FOUND EMP TAIL COMPARTMENT REAR PRESSURE B/HD SUPPORT CHORD CRACKED AT STATION 2598, WL 320 RBL 40 TO RBL 41. REPAIRED PER SRM 53-10-04 FIG 72. (M)SDR ABXA9700751Blkhd Stiffener · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER CRACKED AT LONGERON 14R. REPLACED STIFFENER IAW DC9 SRM 51-30-5.SDR ABXA9700750Blkhd Stiffener · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER CRACKED AT LONGERON 15R AND 16R. REPLACED STIFFENER IAW DC9 SRM 51-30-5.SDR DL73E970716Bulkhead Web · crackedDURING ACCOMPLISHMENT OF SI 3-69482-12, FOUR CRACKS WERE DISCOVERED ON THE FWD FACE OF THE FS 178 BULKHEAD WEB. THIS ER/A GIVES INSTRUCTIONS TO INSTALL A 0.050 2024-T3 REPAIR DOUBLER.SDR USAA970131Bulkhead · chafedPIT - DURING RON VISIT, FOUND A .3750 INCH CHAFE MARK .029 INCH DEEP AT AFT SIDE OF AFT PRESSURE BULKHEAD, LOWER RIGHT SIDE, STA 996. INSTALLED TWO DOUBLERS AT RT T/R BELLCRANK PER EA NR 46732. (X)SDR TWAA9807902Bulkhead · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND AT BS 996, THE AFT PRESS BULKHEAD 'T' CAP ANGLE FROM FLOOR TO STRINGER 19R HAD CRACK. REPLACED ANGLE PER SRM 51-00-P27 ITEM B. (M)SDR ABXA9701074Bulkhead Fitting · crackedDURING D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD DOOR FRAME ATTACH FITTING CRACKED JUST ABOVE STIFFENER AT Z14R BETWEEN LONGERONS 16 AND 17 RIGHT. REPLACED FITTING IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.SDR ABXA9701073Bulkhead Fitting · crackedDURING D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD DOOR FRAME ATTACH FITTING CRACKED JUST ABOVE STIFFENER Z34 RIGHT AT LONGERON 14 RIGHT. REPLACED FITTING IAW DC9 SRM 51-30-2.SDR AU970637Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD CRACKED IN THE FOLLOWING AREAS:-1. FORWARD FACE OF BULKHEAD WEB CONTAINED THREE CRACKS IN AREA BELOW RADAR SCANNING MOUNTING BRACKETS AT RBL 5.7 - CRACK LENGTHS 15MM (0.59IN) - 14MM (0.55IN) AND 3MM (0.118IN) - FOUND USING ULTRASDR ABXA9701047Bulkhead Web · crackedDURING D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LEFT HAND DOUBLER HAD A BEND RADIUS CRACK. REPAIRED IAW ABX REA D953-18897-MR.SDR DLL10970636Bulkhead Web · crackedDURING INSPECTION PER DAL EO 7-69959-12AD, THE FS 1363 BULKHEAD WEB SECTION I/B OF OF LBL 42.5 WAS FOUND WITH TWO CRACKS AT APPROX WL 133. THE SUBJECT WEB SECTION IS MADE FROM 0.085 THICK 7075-T6 AL CLAD.SDR ABXA9700767Blkhd Recepticle · crackedDURING C-CHECK WHILE ACCOMPLISHING AD 79-24-01, THE AFT PRESSURE BULKHEAD DOOR RETAINER RECEPTICLE WAS FOUND CRACKED. THE RECEPTICLE WAS REPLACED IAW DC9 SRM.SDR HAL9752Bulkhead Web · crackedAFT PRESSURE BULKHEAD FORWARD FACE AREA, 2 EACH CRACKS IN UPPER DOOR CUT-OUT. LEFT UPPER CORNER HAS CRACK WHICH HAS EXTENDED BEYOND ORIGINAL STOP DRILL AND IS NOW 2.5 INCHES LONG. RIGHT UPPER CORNER HAS EXTENDED BEYOND ORIGINAL STOP DRILLED, AND IS NOW 1.8 ISDR 97ZZZX2688Bulkhead Web · crackedAFT PRESSURE BULKHEAD FORWARD FACE AREA, 2 EACH CRACKS IN UPPER DOOR CUT-OUT. LEFT UPPER CORNER HAS CRACK WHICH HAS EXTENDED BEYOND ORIGINAL STOP DRILL AND IS NOW 2.5 INCHES LONG. RIGHT UPPER CORNER HAS EXTENDED BEYOND ORIGINAL STOP DRILLED, AND IS NOW 1.8 ISDR HALA9756Bulkhead Angle · crackedAFT PRESSURE BULKHEAD INT RIGHT OUTBOARD HORIZONTAL ANGLE STIFFENERS AT STRINGER 14, 15 AND 16 HAVE CRACKS 5. REMOVED AND REPLACED ANGLES PER SRM 53-05 FIG 93. INSTALLED PER SRM 51-30-2, 51-10-3 ON APB INT FWD SIDE AT STRINGER 15, 16 STATION 1167. COMPLETE SDR ABXA9701078Bulkhead Jamb · crackedDURING D-INSPECTION, FOUND TWO CRACKS IN THE AFT PRESSURE BULKHEAD DOOR JAMB, RIGHT UPPER CORNER. REMOVED AND REPLACED CRACKED Y-DOUBLER IAW DC-9 SRM CHAPTER 51-30-5.SDR ABXA9700455Bulkhead Skin · gougedDURING C-CHECK, FOUND GOUGES ON THE AFT PRESSURE BULKHEAD SKIN FORWARD SIDE AT LONGERON STA 23R. BLENDED OUT GOUGES, INSTALLED DOUBLER IAW ABX REA NR D953-18898-MR.SDR W8PA970501Bulkhead · crackedFOUND CRACK AT BS 663.75 BULKHEAD FROM RBL 43 TO RBL 55, WL 156 TO WL 167. REPAIRED CRACK, BS 663.75, RBL 43 TO RBL 55, WL 156 TO WL 167. (M)SDR SWAA970357Bulkhead Angle · crackedDURING SCHEDULED D-CHECK, FOUND BULKHEAD SUPPORT ANGLE CRACKED AT BS 727, WL 162. REPLACED PER BOEING SRM.SDR DL72W970633Bulkhead Web · crackedBS 1183 BULKHEAD FOUND CRACKED IN THE WEB. STOPPED DRILLED AND REPAIRED TO SRM 53-10-9, FIG. 4.SDR W8PA970231Bulkhead Support · corrodedAFT CARGO BAY AFT BULKHEAD SUPPORT IS CORRODED. REMOVED AND REPLACED VERTICAL BULKHEAD SUPPORT, BS 948, WL 173-200, RBL 17.5. (M)
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