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 UPS05844896Pressure Blkhd · crackedINSPECTION TYPE C-1, AFT PRESSURE BULKHEAD CRACKED 1.75 IN LONG AT RBL 26 AND 66 IN FROM FLOOR. CUT OUT DAMAGE SECTION, FABRICATED REPAIR DOUBLER, FINGER DOUBLER, AND FILLER AND INSTALLED IAW SRM 53-2-5 FIG 14A.SDR UPS05844916Bulkhead · crackedINSPECTION TYPE:C1 683 BULKHEAD CRACKED LBL 10 - RBL 24. CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53 -2-5 FIG 13.SDR ASOA05554Bulkhead · corrodedDURING A C-CHECK, THE PILOTS BULKHEAD WEB AT FS 280 BETWEEN LBL 9 AND RBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PILOTS BULKHEAD WEB AT FS 280 BETWEEN LBL 9 AND RBL 9 IAW EO. (K)SDR USAA050786Bulkhead · crackedFOUND BULKHEAD WEB WITH TWO CRACKS .125 INCH, WL 234, RBL 10.0 BS 178. INSTALLED DOUBLER PER EO 5300V153 AND SRM 53-10-08. (M)SDR P5CA0501368Pressure Panel · crackedNOSE WHEEL WELL WEB AT STATION BS 400 STR 47R FOUND CRACKED AT RETRACT ACTUATOR CUTOUT. NOSE WHEEL WELL WEB REPAIRED AS PER BOEING MESSAGE 1-1MCB8E AND FAA FORM 8100-9.SDR 0501286717Pressure Panel · crackedDURING LINE CHECK FOUND CRACK IN RIGHT HAND NOSE WHEEL WELL SIDE PANEL WEB. REPAIRED PER EA 67-204659.SDR COMA0570072Bulkhead · corrodedLT AND RT LOWER WEBS BELOW FLOOR AT FS 280 ARE CORRODED FROM LBL36 TO RBL36. REMOVED CORRODED WEBS AND INSTALLED NEW WEBS IAW REO 6670-53-11-052 REV A.SDR UPS05444715Pressure Panel · crackedAD LT NLG WW SIDE PANEL WEB FOUND 2 LOCATIONS CRACKED BETWEEN STA 265 AND 280, WL 160 AND 170. CRACK LENGTH APPROX 1 INCH. LT NLG WW SIDE PANEL WEB REPAIRED AT BETWEEN BS 265 AND 280 WL 160 AND 170 AREA AS PER SRM 53-10-04 FIG 116. SUBSEQUENT INSP NECESSARYSDR SWAA051749Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 1016 PRESSURE BULKHEAD WEB CRACKED AT STR 15R. REPAIRED BS 1016 BULKHEAD WEB PER BFG ER.SDR COMA0570064Bulkhead · corrodedFS 280 BULKHEAD LOWER WEBS ARE CORRODED BEYOND LIMITS FROM LBL 36 TO RBL 36. REPLACED THE FS 280 BULKHEAD LOWER WEBS IAW BOMBARDIER REO 670-53-11-052 REV A REPAIR 2.SDR SWAA051730Pressure Panel · crackedDURING SCHEDULED 1/2D CHECK, FOUND NLG W/W CEILING PANEL CRACKED AROUND LT & RT BRAKE MOUNT PADS. REPAIRED PANEL PER SWA EA & SRM.SDR AWXA200500699Stiffener · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK DISCOVERED 2 CRACKS .113 INCHES IN LENGTH ON ANGLE LOCATED AT BULKHEAD STA 178 LBL 5.7 WL 184. MAINTENANCE CUT OUT AND REMOVED DAMAGED AREA FROM BULKHEAD LOCATED AT STA 178. FABRICATED REPAIR ANGLES, STRAPS, FILLERS IAWSDR VTZA200500113Bulkhead · crackedRIGHT SIDE COPILOTS BULKHEAD AT FS 280 RBL 9.0 IS CRACKED AT 1.0 INCH IN WEB RADIUS.SDR AWXA200500764Pressure Blkhd · corrodedDURING C-13 CHECK DISCOVERED CORROSION ON AFT PRESSURE BULKHEAD STA 1016, WL 150 TO WL 155, STR 27R, ON FORWARD SIDE AND RUNNING UNDER LEVELING COMPOUND. MAINTENANCE REMOVED CORROSION ON AFT PRESSURE BULKHEAD STA 1016, WL 150 TO WL 155, STR 27R, ON FORWARD SISDR SWAA051693Pressure Panel · crackedDURING SCHEDULED 1/2D CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, LBL 30. REPAIRED WEB PER SRM.SDR AWXA200500693Stiffener · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK FOUND SUPPORT ANGLE CRACKED AT BS 178 WL 230 RBL 17.1. MAINTENANCE REMOVED CRACKED SUPPORT ANGLE AND FABRICATED SUPPORT ANGLE IAW BOEING DWG 65-17582. INSTALLED FABRICATED REPAIR PARTS AT BS 178 WL 230 RBL 17.1 IAW BOEISDR ASAA0590110Angle · corrodedPAE - DURING CHECK, FOUND CORROSION ON FORWARD CARGO BAY AFT BULKHEAD LOWER SUPPORT ANGLE. REPAIRED IAW SRM 51-40-02. (M)SDR AWXA200500834Angle · corrodedMCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED CORROSION ON AFT PRESSURE BULKHEAD CENTER STIFFENER ANGLE AT BS 1016, FROM WL 150 TO WL 180, BL 0. MAINTENANCE REMOVED CORROSION ON STIFFENER ANGLE AT BS 1016, FROM WL 150 TO WL 180, BL 0 AND FOUND TO BE OUT OSDR ASOA05493Pressure Panel · corrodedDURING A C-CHECK, THE PRESSURE FLOOR AT FS 424-449.85 LT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PRESSURE FLOOR AT FS 424-449.85 LT IAW EO. (K)SDR ASOA05491Pressure Panel · corrodedDURING A C-CHECK, THE PRESSURE FLOOR BETWEEN FS 449.85-473.15, BL45 TO THE FLOOR UNDER THE LT AND RT OVERWING EXITS WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PRESSURE FLOOR BETWEEN FS 449.85-473.15, BL45 TO THE FLOOR UNDER THE LT ASDR ASOA05495Bulkhead · corrodedDURING C-CHECK, THE PILOTS BULKHEAD WEB FS 280 BETWEEN LBL 9 AND RBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PILOTS BULKHEAD WEB FS 280 BETWEEN LBL 9 AND RBL 9 IAW EO. (K)SDR AWXA200500692Bulkhead · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK FOUND 3 CRACKS .271 INCHES LONG AT FRAME WEB STA 178 WL 230 RBL 17.1. MAINTENANCE REMOVED DAMAGED AREA FROM FRAME WEB STA 178 WL 230 RBL 17.1 AND FABRICATED WEB AND TAPERED SHIMS IAW BOEING 737-300 SRM 53-10-08-2 FIG 212SDR SWAA051633Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 1016 AFT PRESS BULKHEAD WEB CRACKED AT STR 7R. REPAIRED BS 1016 AFT PRESS BULKHEAD WEB PER SWA EA.SDR AWXA200500690Bulkhead · crackedDURING C-21 CHECK FOUND A CRACK .275 INCHES IN LENGTH AT BULKHEAD WEB BS 178, WL 234, AND LBL 14. MAINTENANCE REMOVED CRACKED AREA AT BULKHEAD WEB BS 178, WL 234, LBL 14 AND FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 53-10-08-2 FIG 209. INSTALLED FSDR ABXA050149Bulkhead · crackedLEFT BULKHEAD SPAR STUB (HORIZONTAL WEB) AT FS 1039 APPROX LONGERON 15 LEFT CRACKED ON BOTTOM COMING FROM INBOARD FORWARD BOLT HOLE. STOP DRILLED/REPAIRED IAW DC-9 SRM 53-01.SDR SWAA051619Stringer · crackedDURING SCHEDULED D-CHECK, FOUND BS 1016 AFT PRESS BULKHEAD RADIAL STRINGER CRACKED AT 8 O'CLOCK POSITION. REPAIRED RADIAL STRINGER PER SRM.SDR SWAA051623Bulkhead · canningDURING SCHEDULED HC2 CHECK, FOUND BS 1016 AFT PRESS BULKHEAD OIL CANNED AT STR 2L. REPAIRED AFT PRESS BULKHEAD PER SWA EA.SDR COMA0560329Rib · crackedRT BATT RIB CRACKED. REPAIRED IAW REO 601R-57-51-046.SDR 2005FA0000981Bulkhead · crackedBULKHEAD CRACKED APPROX .3750 INCH ON UPPER LT AREA ON BEND RADIUS, BULKHEAD TIES IN VERTICAL AND HORIZONTAL STABILIZERS TOGETHER. FATIGUE DUE TO HIGH TT ON AIRFRAME, PROBABLE CAUSE? (SW01200504869) (K)SDR K2Z2005F00000Bulkhead · crackedCRACKS FOUND IN BOTH SIDES, UPPER CORNER OF RUDDER CABLE CUTOUT BETWEEN COUTOUT AND FLANGE. DYE PENETRANT INSPECTION OF FRONT FLANGE REVEALED NO DEFECTS. INSPECTION OF THIS BULKHEAD PREVIOUSLY ACCOMPLISHED AT 3607. NOT REQUIRED FOR INSPECTION IAW AD. RECOMSDR AWXA200500686Bulkhead · crackedMCN - MAJOR REPAIR - DURING C-21 CHECK FOUND A CRACK .375 INCH AT 178 BULKHEAD WEB, WL 207, RBL 10. MAINTENANCE REMOVED DAMAGED AREA FROM 178 BULKHEAD WEB, WL 207, RBL 10 IAW BOEING 737-300 SRM 53-10-08 FIG 209. FABRICATED DOULBER AND INSTALLED REPAIR PARTS SDR SWAA051593Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE BS 1016 PRESS BULKHEAD DOME WEB CRACKED AT BL 0, WL 249. REPAIRED WEB PER BFG ER.SDR COMA0570058Bulkhead · corrodedFS 280 BULKHEAD LOWER WEBS ARE CORRODED BEYOND LIMITS FROM LBL 36 TO RBL 36. REPLACED THE FS 280 BULKHEAD LOWER WEBS IAW BOMBARDIER INC REO 670-53-11-052 REV A REPAIR NR 2.SDR UPS05844759Panel · corrodedHEAVY CORROSION ON LT WW CEILING STA 860 LBL 61. CUT OUT DAMAGE AND INSTALLED REPAIR PARTS IAW EO DC8-5310-22401-A AND SAA SK 840-807868.SDR 2005FA0000796Doubler · corrodedTHESE FIREWALL DOULBLERS ARE INSTALLED FROM FACTORY WITH SOME STRUCTURAL STEEL RIVETS PASSING THROUGH THESE ALUMINUM DOUBLERS, CAUSING CORROSION TO FORM ON BOTH LT AND RT DOUBLERS VERY NEAR ENGINE DYNAFOCAL MOUNT LOCATIONS, REQUIRING REPLACEMENT OF BOTH DOUBLESDR SWAA051523Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE BULKHEAD WEB CRACKED AT BS 178, LBL 25, WL 207. REPAIRED WEB PER SRM.SDR SWAA051502Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE BULKHEAD WEB CRACKED AT BS 178, LBL 25, WL 207. REPAIRED WEB PER SRM.SDR UPS05844704Bulkhead · crackedFWD ACCESSORY COMPARTMENT 680 BULKHEAD HAS CRACKS IN 4 PLACES. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53 -2-5 FIG 13, 51-1-20D, AND 51-1-21.SDR COMA0570053Bulkhead · corrodedFS 280 LEFT AND RIGHT LOWER BULKHEAD WEBS (FLOOR LEVEL) ARE CORRODED BEYOND LIMITS. PERFORMED A MAJOR REPAIR TO FS 280 LOWER BULKHEAD WEBS BY REMOVING AND REPLACING CORRODED WEBS IAW CRJ 700 SRM 51-42-06-001-001-A01 P/NS 670-53-11-052-1 AND 670-53-11-052-2.SDR P5CA0501356Bulkhead · crackedBS 1241 LEFT SIDE CANTED BULKHEAD HAS CRACK IN WEB AREA ABOVE BULKHEAD FITTING. ACCOMPLISHED REPAIR PER BOEING INSTRUCTIONS 1-1I9Y5F AND FAA FORM 8100-9.SDR 0500949859Bulkhead · crackedDURING M-CHECK FOUND CRACK IN FORWARD PRESSURE BULKHEAD AT RIVET BELOW UPPER LT AND RT RADOME ALIGNMENT PIN AT BS 37. REPAIRED PER EA 98-203219.SDR 2005FA0000844Bulkhead · crackedBULKHEAD CRACKED AT TOP PORTION AT JOGGLED AREA BELOW AFT HORIZONTAL ATTACH BRACKET/SPAR CRACK TO BE ABOUT .2500 INCH ON RT, ABOUT 1 INCH ON LT, CAUSE PROBABLY DUE TO HIGH AIRFRAME TT AND FATIGUE. (SW01200504562) (K)SDR 2005FA0000842Bulkhead · crackedTAIL BULKHEAD AT STA 272.0, FOUND CRACKS ON TOP PORTION IN BEND RADIUS AREA, APPROX .5 INCH TO .2500 INCH LONG ON TOP, LT AND RT AREA. PROBABLE CAUSE SEEMS TO BE FATIGUE DUE TO HIGH TOTAL TIME ON AIRFRAME. (K)SDR SWAA051440Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE VERTICAL BEAM WEB CRACKED AT BS 178 BULKHEAD, RBL 17.1, WL 230. REMOVED AND REPLACED VERTICAL BEAM WEB PER SRM.SDR SWAA051409Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT LBL 5.7, WL 178. REPAIRED WEB PER SRM.SDR 05FDEA01286Bulkhead · crackedCENTER CARGO STA 1841 FLOOR AREA BULKHEAD APPROX X= -23 WEB FOUND CRACKED. CRACKED WEB AT CENTER CARGO STA 1841 FLOOR AREA BULKHEAD X= -23 CUT AT STA 1841 X= -23 AND REMOVED AS PER SRM 53-00-01 FIGURE 10 VOLUME I. REPAIR WEB AND DOUBLER FABRICATED AND INSTALLSDR 05FDEA01285Bulkhead · crackedCENTER CARGO, STA 1841 FLOOR AREA BULKHEAD APPROX X= 3 WEB FOUND CRACKED. CRACKED AREA OF WEB AT CENTER CARGO STA 1841 FLOOR AREA BULKHEAD X= 3 TRIMMED OUT AS PER SRM 53-00-01 FIGURE 5 VOLUME I. REPAIR FILLER AND DOUBLER FABRICATED AND INSTALLED AS PER SRMSDR 05FDEA01283Doubler · crackedLANDING GEAR, CENTER LANDING GEAR LEFT HAND FORWARD BULKHEAD SIDE DOUBLER CRACKED. DOUBLER REMOVED AND NEW DOUBLER INSTALLED AS PER SRM 51-33-01 VOLUME II. THIS REPAIR CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.SDR 05FDEA01282Doubler · crackedLANDING GEAR, CENTER LANDING GEAR RIGHT HAND FORWARD BULKHEAD SIDE DOUBLER CRACKED. DOUBLER REMOVED AND NEW DOUBLER INSTALLED AS PER SRM 51-33-01 VOLUME II.SDR UPS05444661Bulkhead · corrodedINSPECTION TYPE:C, RT WLG W/W FWD BULKHEAD LOWER AREA CORROSION REVEALED AT STA 1241 RBL 75-99. CORROSION BLEND OUT 0.063 X .875 X 1.25 INCH EXCEED SRM 57-10-01 FIG 1 LIMITS. RT WLG W/W FWD BULKHEAD LOWER AREA RBL 75-99 AREA CORROSION REMOVED & REPAIRED AS P
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