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 MWEA97229Plug Door · crackedDURING INSPECTION, FOUND AFT PRESSURE BULKHEAD PLUG DOOR CRACKED IN OUTER EDGE PAN RADIUS, APPROX 2.25 INCHES IN LENGTH. MAINTENANCE REPAIRED PLUG DOOR IAW SRM 52-05 FIG 21.SDR DLL10970712Bulkhead · crackedUPON INSPECTION, A CRACK WAS FOUND IN THE NLG FITTING AT STA 449 BULKHEAD. THIS CRACK BEGINS IN A SEAL RETAINER HOLE AT LBL 21, AND EXTENDS APPROXIMATELY 2.0 AFT TO THE 449 BULKHEAD. THE CRACK IS WELL INTO THE RADIUS OF THE NLG FITTING, BUT IT DOES NOT YET ESDR 97ZZZX3464Rib · defectiveATW - PERFORMED BAE AVRO RIL HC571H9033 TO RIGHT WING RIB ZERO AND FAXES PC/RJ0652-95 AND DJR/RJ0634-96. C/W BAE AVRO RIL HC571H9033 TO RIGHT WING RIB ZERO AND FAX ES PC/RJ0652-95 AND DJR/RJ0634-96.SDR HALA9767Bulkhead · corrodedAFT ACCESSORY COMP BULKHEAD 1230 HAS LEVEL 2 CORROSION AT ATTACH POINT TO SKIN FROM LONG 24L TO RBL 22. REMOVED CORROSION PER SRM 51-10-3 MATERIAL LOSS WITHIN LIMITS PER SRM 53-01 FIG 1. PRIME PER SRM 57-10-3. INSTALLED FABRICATED REPAIR WEB AND 5 L-ANGLES SDR ABXA9701082Blkhd Stiffener · crackedDURING D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER Z74R AT FS 1072 AND LONGERON 3 RIGHT CRACKED. REPLACED END CLIP IAW DC-9 SRM CHAPTER 51-30-2.SDR ABXA9701081Blkhd Stiffener · crackedDURING D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER Z24L END CLIPS CRACKED AT FS 1072 AND LONGERON 15L. REPLACED STIFFENER END CLIPS IAW DC-9 SRM CHAPTER 51-30-1.SDR SWAA970338Bulkhead · crackedDURING SCHEDULED D CHECK, FOUND BULKHEAD BS 178 CRACKED AT WL 234, LBL 10 AND AT RBL 10. REPAIRED PER BOEING SRM.SDR ABXA9701080Blkhd Stiffener · crackedDURING D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER Z24R END CLIPS CRACKED AT FS 1072 AND LONGERON 15 RIGHT. REPLACED STIFFENER END CLIPS IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.SDR ABXA9701083Blkhd Stiffener · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER Z34L CRACKED AT FS 1072 AND LONGERON 14 LEFT. REPAIRED IAW DC-9 SB 09530166 AND DC-9 SRM CHAPTERS 51-30-1, 51-30-2 AND 51-30-5.SDR MWEA97226Bulkhead Door · crackedA 2 INCH CRACK IN AFT PRESS BLKHD PLUG DOOR. MAINT REPAIRED IAW SRM 52-05 FIG 21.SDR ABXA9701063Blkhd Stiffener · crackedDURING D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER AT Z48R CRACKED BETWEEN LONGERONS 11 AND 12 RIGHT. REPLACED STIFENER IAW DOUGLAS DRAWING NUMBER 991558.SDR ABXA9701062Blkhd Stiffener · crackedDURING D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER Z34R CRACKED AT LONGERON 14 RIGHT. REPLACED STIFFENER IAW DOUGLAS DRAWING NR 9915558.SDR UPS97222812Bulkhead Ftg · crackedINSPECTION TYPE-D, CRACK FOUND IN RT BS 870 FTG. REPAIRED IAW B727-5310-3057 APP 8.3.SDR CKSA97118Bulkhead Web · corrodedDURING C-1 CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON BULKHEAD WEB AT FS 980, 6 INCHES ON TOP OF LONGERON 24 LT AND UNDER HAT SECTION STIFFENER. REMOVED DAMAGE, INSTALLED DOUBLER REPAIR IAW DC8 SRM 53-2-1 FIGURE 7. CLASS 2 REPAIR, REQUIRE AN INITIAL INSPECSDR CALA9700450Bulkhead · crackedINSPECTION FOUND, THREE CRACKS IN LOWER FORWARD AREA OF CANTED BULKHEAD, AT STA 1463. THE CRACKS WERE .5 INCH TO 1.5 INCH LONG. A WEB WAS INSTALLED IAW SRM 51-30-05.SDR CKSA97028Bulkhead Angle · crackedDURING CPCP CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD RT SIDE APPROXIMATELY STRINGER 13 ATTACH ANGLE CRACKED IN RADIUS BELOW DOUBLER. REPAIRED IAW DC8 SRM 53-2-5 FIG 9. CORROSION TASK CARD NUMBER 6610-0553. NON-ROUTINE TASK CARD NUMBER 82849.SDR ABXA9701060Blkhd Stiffener · crackedDURING D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER Z14R CRACKED BETWEEN LONGERONS 16 AND 17 RIGHT. REPLACED STIFFENER IAW DOUGLAS DRAWING NR 9915558.SDR 9708171143Bulkhead Channel · corrodedDURING M-CHECK, FOUND CORROSION IN SEVERAL AREAS ON THE FOURTH AND FIFTH CHANNELS DOWN FROM THE TOP OF THE BS 2007 BULKHEAD. PRIMED AND INSTALLED REPAIR PER EA 11-122886.SDR USAA970101Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO 1.5 INCH CRACKS IN AFT SIDE OF BULKHEAD SKIN BS 178 LBL 5, WL 203 AND 195. INSTALLED BULKHEAD REPAIR AND REPAIRED PER TR NR 53-10-11. (M)SDR DLL10970703Bulkhead Cap · crackedTHE RHS FUSELAGE SKIN WAS FOUND WITH AN APPROX 2 INCH LONG CRACK AT WL 146, JUST FORWARD OF FS 983 AND ABOVE STRINGER 21, THE CRACK EXTENDS HORIZONTALLY THROUGH TWO FASTENER HOLES. ANOTHER 1 INCH LONG CRACK WAS FOUND IN THE HORIZ FLANGE OF THE BULKHEAD CAP, ESDR SWAA970305Bulkhead Support · corrodedDURING SCHEDULED D-CHECK, FOUND SIDEWALL TO BULKHEAD SUPPORT CORRODED AT BS 520, LBL 25, WL 157. REPLACED PER BOEING SRM.SDR DL73E970673Bulkhead · fatiguedDURING INSPECTIONS PER SI 3-69482-12, THE STATION 178 BULKHEAD WAS FOUND CRACKED IN THREE LOCATIONS RBL 5.7, WL 202 LBL 5.7, WL 198, LBL 5.7, WL 202.SDR AALA970573Bulkhead · corrodedTUL - FORWARD SIDE OF BULKHEAD STA 351 HAS CORROSION ON AREAS WHERE DRAG BRACE WAS ATTACHED, RBL 6 INCHES TO LBL 6 INCHES LOCATED AT 6 INCHES TO 12 INCHES ABOVE SHELF ANGLE. REMOVED CORROSION PER SRM 51-10-06 AND INSTALLED DOUBLER PER ESO 11697 DATED 2-24-97.SDR MWEA97170Bulkhead Tee · corrodedDURING INSPECTION, FS 756 BOTTOM AT PRESS BULK VERTICAL TEE CORRODED. MAINT REPAIRED IAW SRM 53-03 FIG 7 AND DAC TELEX SVC-MSP-0016/RMK 01/08/97.SDR CKSA97073Bulkhead Web · crackedDURING ACCOMPLISHMENT OF AD 90-24-11 CLOSE VISUAL INSPECTION OF BS 1183 PRESSURE BULKHEAD WEB AND STRAP IAW FIGURE 1 OF SB 727-53A0171 REV 1 OR 2: CRACKS FOUND AROUND 3 RIVETS IN WEB OF AFT PRESSURE BULKHEAD STA 1183. REPAIRED AFT PRESSURE BULKHEAD IAW B727 SSDR AU970254Bulkhead · corroded(AUS) FUSELAGE REAR BULKHEAD CORRODED IN AREA OF STABILATOR ATTACHMENT BRACKETS - RIVETS POPPED AT FRAME OF FORWARD FIN ATTACHMENT AREA- FOLLOWING REMOVAL OF TOP AFT FUSELAGE SKIN AND SKIN ON FIN AND STABILISER. WIDE SPREAD SURFACE CORROSION WAS FOUND WHERE SDR USAA970087Bulkhead · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK 178 BULKHEAD. STOP DRILLED ENDS OF CRACK, INSTALLED DOUBLER AND FILLERS. REPAIRED PER TR 53-10-07 SRM 51-10-2. (M)SDR DL72S970498Bulkhead Support · wornFOUND DURING MV2 F1 - STA 720D VERTICAL BULKHEAD SUPPORTS WORN AT UPPER ATTACH POINTS LT ABOVE STRINGER 26 LT AND RT ABOVE STR 26 RT. INSTALLED REPAIR PER SRM 53-10-9 FIG. 9.SDR EISA97055Bulkhead Angle · crackedAFT AIRSTAIR AFT BULKHEAD, LEFT LOWER AT STATION 1183, CRACK JUST LEFT OF ENTRY DOOR. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-10-2. (M)SDR CALA9700338Bulkhead · corrodedINSPECTION FOUND BULKHEAD AND SKIN CORRODED IN FORWARD CARGO BILGE AREA AT STA 560, STRINGER 28R. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A SKIN REPAIR WAS INSTALLED IAW SRM 53-30-3.SDR CALA9700574Bulkhead Web · crackedINSPECTION FOUND BULKHEAD WEB CRACKED ON BOTH LT AND RT SIDE AT BS 400 WL 160, BL 90. THE CRACK LENGTH WAS NOT IDENTIFIED. THE WEB WAS REPAIRED IAW ECRA 5310-03459.SDR USAA970096Bulkhead · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO .5 INCH CRACKS BS 178 BULKHEAD LBL 4.75 WL 198 WL 201. STOP DRILLED AND INSTALLED DOUBLER, REPAIRED PER TR 53-10-07 REV A. (M)SDR HALA9758Bulkhead Jamb · crackedAPB DOOR JAMB IS CRACKED IN BOTH CORNER RADIUS AND HAS EXTENSIVE CORROSION AT RBL 6 AND LBL 6. FABRICATED AND TREATED REPAIR PARTS PER SRM 53-05 FIG 34 AND SRM 51-10-3. (M)SDR CALA9700384Bulkhead · crackedINSPECTION FOUND A SIX INCH CRACK IN BULKHEAD AT STA 178, WL 208, RBL 18. ALSO, A SIX INCH CRACK WAS FOUND IN BULKHEAD AT STA 178, WL 208, LBL 16. THE CRACKED AREAS WERE REMOVED IAW SRM 53-10-11. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-1SDR CALA9700346Bulkhead Web · crackedINSPECTION FOUND A 1.5 INCH CRACK BETWEEN BOLTS OF BULKHEAD WEB BELOW THE APU LOAD CONTROL VALVE, BS 870. REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW ECRA 5310-01544.SDR AU970264Bulkhead · corroded(AUS) FORWARD CENTRE BULKHEAD LOCATED UNDER FLOOR SEVERELY CORRODED - SEE MDR 97/0252 FOR ADDITIONAL INFORMATIONSDR AU970260Bulkhead · corroded(AUS) REAR FUSELAGE BULKHEAD CORRODED IN AREA OF DORSAL FIN ATTACHMENT- SEE MDR 97/0252 FOR ADDITIONAL INFORMATIONSDR AU970251Bulkhead · cracked(AUS) FUSELAGE LH BULKHEAD CRACKEDSDR ABXA9700518Bulkhead Tee · crackedDURING C-CHECK, THE AFT PRESSURE BULKHEAD TEE WAS FOUND CRACKED AT LONGERON 14 LEFT. WHILE ACCOMPLISHING AD 96-16-04. THE TEE WAS REPLACED IAW SRM 51-30-2.SDR ABXA9700073Bulkhead Tee · crackedEDDY CURRENT INDICATES CRACK IN AFT PRESSURE BULKHEAD TEE, THIRD RADIAL FROM FLOOR, LEFT SIDE. INSTALLED SPLICE REPAIR IAW DC-9 SRM 51-30-1.SDR DLL15970413Bulkhead Panel · corrosionTHE AFT PRESSURE BULKHEAD LOWER GORE PANEL WAS FOUND CORRODED IN SEVERAL AREAS BETWEEN STRINGERS 31 AND 33. THE BONDED GORE DOUBLER WAS FOUND CORRODED BETWEEN STRINGERS 24 AND 33. THE DAMAGE WILL BE REPAIRED PER ER/A 304834-14 REVISION 'A'.SDR DLL15970411Bulkhead Frame · corrosionTHE AFT P-DOME ZEE FRAME WAS FOUND WITH CRACKS DUE TO CORROSION IN THE ZEE ANGLE AND WEB. THE DAMAGED FRAME SEGMENTS WERE CUT AND REMOVED AND WILL BE SPLICE REPAIRED. THE ZEE FRAME WAS REMOVED BETWEEN THE S-29 FACTORY SPLICE LOCATION AND S-37. THE WEB WAS RSDR CALA9700315Bulkhead Tee Cap · corrodedINSPECTION FOUND CORROSION ON BULKHEAD TEE CAP AT STA 110, LONGERON 29L. THE CORRODED AREA OF TEE CAP WAS CUT OUT, A REPAIR WAS INSTALLED IAW ECRA 5310-03443, SRM 53-04, FIGURE 14, SRM 53-01, FIGURE 2, SHEET 4 AND SRM 53-02, FIGURE 2.SDR 97ZZZM417Bulkhead Fitting · crackedBULKHEAD FITTING CRACKED 3 INCHES. TIME LIMITED REPAIR INSTALLED PER EA 42071 AND DWG 65C 29229. (M)SDR SWAA970266Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED UNDER STRAP AT RBL 4.7, WL 198.75 TO 199.75, AND AT WL 201.5 TO 202.5. REPAIRED PER BOEING SRM.SDR SWAA970265Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED UNDER STRAP AT RBL 6.7, WL 211.5 TO 212.75. REPAIRED PER BOEING SRM.SDR DL73E970376Bulkhead Web · crackedDURING INSPECTIONS PER SI 3-69482-12, THE STATION 178 BULKHEAD WAS FOUND CRACKED IN THREE LOCATIONS. THE WEB WILL BE REPAIRED WITH A DOUBLER PER ER/A 304846-14.SDR SWAA970247Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD SIDE CHORD CRACKED LEFT SIDE. REPAIRED PER BOEING SRM.SDR SWAA970246Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT WL 234, RBL 13. REPAIRED PER BOEING SRM.SDR EIAA970036Bulkhead · corrodedMZJ - DURING REPLACEMENT OF THE LT BODY GEAR ASSY, WIDESPREAD CORROSION WAS FOUND IN THE LT O/B BODY GEAR TRUNNION SUPPORT ASSY. CORROSION WAS FOUND IN THE BS 1480 BULKHEAD FWD FITTING INTERFACE SURFACE AT WL 116 AND 127. CORROSION WAS FOUND IN THE AFT SURFA
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