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 UPS03841221Bulkhead · crackedINSPECTION TYPE: C2, AFT PRESSURE BULKHEAD WEB IS CRACKED AT LBL 26 AND 36, 67 ABOVE CABIN FLOOR CUTOUT DAMAGED AREAS,NDT VERIFIED NO CRACKS AT CUTOUTS,FABRICATED AND INSTALLED DOUBLERS AND FILLERS I.A.W. DWG. SRO08530007SDR UPS03841218Bulkhead · crackedINSPECTION TYPE: C2, AFT PRESSURE BULKHEAD WEB IS CRACKED AT STA 1766 AT RBL 26 AND 36. CUTOUT DAMAGED AREAS AT RBL 26 AND 36,NDT VERIFIED NO CRACKS AT CUTOUTS, FABRICATED AND INSTALLED DOUBLERS AND FILLERS IAW SRO8530007.SDR CALA0300484Pressure Panel · crackedINSPECTION FOUND A 1 INCH CRACK IN CEILING WEB OF LT WHEEL WELL AT BS 663, LBL 32. THE CRACKED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-60-51, FIGURE 203.SDR ABXA030359Pressure Panel · crackedPRESSURE PANEL LEFT WHEEL WELL AT FS 718 LEFT BUTT LINE 36 APPROXIMATELY, CRACKED. REPAIRED RPESSURE PANEL IAW REA D953-48107.SDR 03FDEA01337Pressure Panel · gougedNOSE LANDING GEAR FWD RT PRESSURE ACCESS PANEL SKIN CUTOUT IS GOUGED. REPAIRED FWD RT PRESSURE ACCESS PANEL SKIN AT NOSE LANDING GEAR. ALL WORK DONE IAW SRM 51-40-2.SDR AWXA200300997Bulkhead · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK A .375 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT RBL 17.1, WL 230. MAINTENANCE CUT OUT DAMAGE ON BS 178 BULKHEAD WEB AT RBL 17.1, WL 230. PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED SDR AWXA200300996Bulkhead · crackedDURING C-16 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT LBL 17.1, WL 230. MAINTENANCE CUT OUT DAMAGE ON BS 178 BULKHEAD WEB AT LBL 17.1, WL 230. PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A NEW SECTION OF WEB ANDSDR C2XA03SH272Firewall · crackedSHV DURING C CHECK APU FIRE WALL AT LEFT HAND SIDE HAS A CRACK ALONG THE BOTTOM PORTION OF SUPPORT FLANGE AT 10 O'CLOCK POSITION. MAINTENANCE REPAIRED AFFECTED SECTION IAW CONTINENTAL EXPRESS EC 5330-01267. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA03SH273Firewall · crackedSHV DURING C CHECK APU FIREWALL CRACKED AT THE RIGHT HAND UPPER VERTICAL STIFFENER. MAITENANCE REPAIRED AFFECTED SECTION IAW CONTINENTAL EXPRESS EC 5330-01202. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA03SH274Firewall · crackedSHV DURING C CHECK THE APU FIREWALL WAS FOUND CRACKED AT THE RIGHT HAND APU SUPPORT. MAINTENACE REPAIRED AFFECTED SECTION IAW CONTINENTAL EXPRESS EC 5330-01267. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR SWAA031847Bulkhead · corrodedDURING SCHEDULED SERVICE CHECK, FOUND BS 1016 BULKHEAD WEB CORRODED BETWEEN STR 24L AND STR 24R ON FWD SIDE. REPAIRED BULKHEAD WEB PER SRM AND SWA ACO.SDR DL73S030771Bulkhead · corrodedWEB CORROSION REPAIR INSPECTION OF THE FS 1016 BULKHEAD WEB REVEALED CORROSION AT THE BL 0 STIFFENER NEAR THE BOTTOM OF BULKHEAD AT WL 190-200. AN OIL CAN CONDITION WAS DISCOVERED JUST OUTBOARD OF THE CORROSION AREA. BOTH DAMAGES WERE REMOVED WITH A WEB CSDR ABXA030349Pressure Panel · corrodedPRESSURE PANEL DOUBLER WAS BULGING LEFT BUTT LINE 8 TO LEFT BUTT LINE 16, FS 756. REPLACED LOWER T-ANGLE OF FLOORBEAM FS 756, BUTT LINE 56 RIGHT TO BUTT LINE 54 IAW DC-9 SRM 51-30-2, 51-30-5 AND REA D953-48132.SDR AMWA21Bulkhead · crackedWHILE TROUBLESHOOTING A PRESSURIZATION DISCREPANCY USING A PRESSURE CART, AIR FLOW WAS NOTED COMING FROM UNDER THE RIGHT AVIONICS SHELF. FURTHER INVESTIGATION REVEALED A CRESENT SHAPED CRACK IN THE FWD PRESSURE BULKHEAD AT FS 84 BELOW THE SHELF. THE CRACK RUSDR 2003F00575Pressure Blkhd · crackedWHILE TROUBLESHOOTING A PRESSURIZATION DISCREPANCY USING A PRESSURE CART, AIR FLOW WAS NOTED COMING FROM UNDER THE RIGHT AVIONICS SELF. FURTHER INVESTIGATION REVEALED A CRESENT SHAPED CRACK IN THE FORWARD PRESSURE BULKHEAD AT FS. 84, BELOW SELF. THE CRACK RUNSDR S03453084Bulkhead · corrodedB18752 FUSELAGE BULKHEAD 1480 WEB CORROSION AT LBL 47.7. REPAIR IAW EO 742-53-10-0043.SDR SWAA031808Pressure Panel · crackedDURING SCHEDULED 1/2D CHECK, FOUND MAIN W/W FWD PRESS BULKHEAD CRACKED AT BS 663, WL 200 AND LBL 33. REPAIRED BULKHEAD PER SWA EA.SDR SWAA031807Pressure Panel · crackedDURING SCHEDULED 1/2D CHECK, FOUND NLG W/W UPPER WEB CRACKED AT THE LT/RT TIRE BRAKE ATTACH HOLES. REPAIRED UPPER WEB PER SWA EA.SDR SWAA031809Bulkhead · crackedDURING SCHEDULED C3 CHECK, FOUND AFT PRESS BULKHEAD CRACKED AT BS 1016, BETWEEN STR 4L AND STR 7L AT THE Y CHORD. REPAIRED AFT PRESS BULKHEAD PER SWA EA.SDR WVE2003F00011Pressure Blkhd · crackedTHE LT AND RT SIDE WEBS OF THE AFT PRESSURE BULKHEAD ARE CRACKED AROUND HYDRAULIC UNION CUT OUTS AT FS 1098.2, BETWEEN STRINGERS 8 AND 9. CAUSE: STRESS. THE CRACKED AREAS WERE CUT-OUT AND REPAIR PARTS (MACHINED FITTINGS) WERE INSTALLED IAW REO.SDR 03FDEA01185Skin · gougedNOSE WHEEL WELL SKIN GOUGED AROUND PANEL OPENING 3223 (4 PLACES) 247 - 250. BLENDED GOUGE IN WW SKIN AT BS 237. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. DAMAGE WILL BE REPAIRED ON N00468.SDR CA030728002Pressure Panel · cracked(CAN) DURING GROUND PRESSURIZATION RUN FOR T/S. VISUAL INSPECTION FOUND 12 INCH CRACK IN UPPER WHEEL WELL PRESSURE SKIN ALONG AIRCRAFT CENTER LINE AT EDGE OF STRINGER BETWEEN FRAMES 29 TO FRAME 32. AIRCRAFT WAS PREVIOUSLY SUBJECT TO A COMPANY SPECIAL INSPECTIOSDR 03673Bulkhead · damagedDURING HEAVY INSPECTION MULTIPLE REDUNDANT HOLES AND GOUGES WERE FOUND IN THE AFT PRESSURE BULKHEAD AT FS621. DAMAGE WAS REPAIRED IAW REO 601R-53-61-748. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.SDR LR7A03073Pressure Panel · crackedDURING SCHEDULED C5 INSPECTION PER JOB CARD HC5323 FOUND LT MLG WHEEL WELL FS 577 WEB CRACKED APPROX 1.75 INCHES AT LBL 61, WL 150. REPAIRED IAW SRM SMP 583 51-140-17. NR 2153.SDR LR7A03057Pressure Panel · crackedDURING SCHEDULED C5 INSPECTION PER JOB CARD HC5324 FOUND LMLG FS 517 WEB CRACKED AT LBL 61, WL 160 APPROX 1.5 IN. REPAIRED IAW LAC MEA 382-53-03-057. NR 2092.SDR LR7A03055Pressure Panel · crackedDURING SCHEDULED C5 INSPECTION PER JOB CARD HC5324 FOUND RMLG FS 517 WEB CRACKED AT RBL 61, WL 160 APPROX 1.5 IN. REPAIRED IAW LAC MEA 382-53-03-057. NR 2087.SDR LR7A03051Web · crackedDURING SCHEDULED C5 INSPECTION PER JOB CARD HC5315 FOUND RH FS 924 BULKHEAD LOWER WEB CRACKED APPROX 2.0 IN. AT RBL 65, WL 200. REPLACED WEB IAW SRM SMP 583 51-60 AND 51-70. NR 2008.SDR SWAA031663Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 207, RBL 14 AND WL 203, RBL7. REPAIRED BULKHEAD WEB PER SRM.SDR SWAA031616Pressure Panel · crackedDURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 663, RBL 43. REPAIRED BEADED WEB PER SRM.SDR CALA0300398Pressure Panel · crackedINSPECTION FOUND A 1.5 INCH CRACK IN PRESSURE DECK AT BS 663, LBL 31. THE CRACKED AREA WAS CUT OUT AND REPAIR PARTS WERE INSTALLED IAW SRM 53-60-51.SDR UPS03441104Pressure Panel · corrodedINSPECTION TYPE:C NOSE WHEEL WELL COMPARTMENT TUNNEL - AT STA 240 CEILING AREA THE CABIN HORI FLOOR SUPPORT WEB AREA AFT SURFACE CORROSION FOUND AT BL 0. FLOOR SUPT WEB REPAIRED IAW SRM 51-40-02 FIG.1 DUE TO BLENDED DEPTH 0.043 INCH, WIDTH .7500 INCH AND SDR DL73S030666Pressure Panel · crackedFUSELAGE STA 727 BLKHD, MLG WW, UPPER CHORD - REPAIR: A 0.5 INCH CRACK WAS PREVIOUSLY REPAIRED IN TEH UPPER CHORD OF THE SUBJECT BULKHEAD NEAR BL 0. THE CRACK WAS IN THE UPPER FLANGE OF THE COMPRESSION CHORD AND RAN THROUGH A FASTENER HOLE. DURING THE CURRENSDR UPS03441115Pressure Panel · crackedINSPECTION TYPE:C NLG W/W BOX STRUCTURE LT BS 320 VERTICAL BEAM WEB FOUND APPROX .125 INCH CRACK AT LOWER STAND OFF HOLE BETWEEN 1ST AND 2ND STAND OFF HOLE (COUNT FROM TOP). VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01 PG 8.SDR UPS03441114Pressure Panel · crackedINSPECTION TYPE:C NLG W/W BOX STRUCTURE LT BS 300 VERTICAL BEAM WEB FOUND APPROX .125 INCH CRACK AT LOWER STAND OFF HOLE BETWEEN 1ST AND 2ND STIFFENER CLIP (COUNT FROM TOP). VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01 PG 8.SDR UPS03241061Pressure Panel · crackedINSPECTION TYPE:C NLG WHEEL WELL RT CEILING PRESSURE PANEL HAS A CRACK FROM OUTBOARD EDGE OF PANEL TO BOLT HOLE. PANEL REPAIRED IAW 2003-041-005. REFERENCE UPS ENGINEERING FILE NR 727-53-20125.SDR AWXA200300856Bulkhead · crackedMCN - MAJOR REPAIR - DURING C-14 CHECK A .375 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB, RBL 17.1, WL 183. MAINTENANCE CUT OUT DAMAGED SECTION OF BULKHEAD WEB, RBL 17.1, WL 183; FABRICATED A DOUBLER AND NEW SECTION OF WEB; INSTALLED REPAIR PARTS IAW B737-30SDR AWXA200300898Bulkhead · crackedMCN - MAJOR REPAIR - DURING C-14 CHECK A .7500 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT RBL 7-7.5, WL 226. MAINTENANCE CUTOUT DAMAGED SECTION OF BS 178 BULKHEAD WEB AT RBL 7-7.5, WL 226; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED ASDR AWXA200300896Bulkhead · crackedMCN - MAJOR REPAIR - DURING C-14 CHECK A .75 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT RBL 5, WL 226-227. MAINTENANCE CUTOUT DAMAGED SECTION OF BS 178 BULKHEAD WEB AT RBL 5, WL 226-227; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A RSDR AWXA200300873Stiffener · crackedDURING C14 CHECK A .5 INCH CRACK WAS FOUND INBOARD SIDE BS 178 BULKHEAD VERTICAL TEE AT CENTER RADIUS LBL 5.7, WL 183-184. MAINTENANCE CUT OUT DAMAGED AREA OF VERTICAL TEE AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED 5 EACH REPAIR ANGSDR AWXA200300895Bulkhead · crackedMCN - MAJOR REPAIR - DURING C-14 CHECK A .5 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT LBL 14, WL 218.5. MAINTENANCE CUTOUT DAMAGED SECTION OF BS 178 BULKHEAD WEB AT LBL 14, WL 218.5; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPASDR AWXA200300847Pressure Panel · crackedDURING C-14 CHECK A .75 INCH CRACK WAS FOUND ON PRESSURE WEB AT BS 664, LBL 34. MAINTENANCE CUT OUT DAMAGE ON PRESSURE WEB AT BS 664, LBL 34; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A STIFFENER, DOUBLER AND 3 EACH FILLERS PER B737-30SDR CALA0300371Pressure Panel · crackedINSPECTION FOUND A 3 INCH CRACK IN PRESSURE DECK AT STA 665, RBL 35, JUST O/B OF J-BOX IN RT WHEEL WELL CEILING. THE PRESSURE DECK WAS REPAIRED IAW SRM 53-60-51, PAGE 213-221.SDR SWAA031494Pressure Panel · cracked(AIR TURNBACK, AIRCRAFT WOULD NOT PRESSURIZE. FOUND WEB CRACKED IN NLG W/W AT BS 259, WL 174. REPAIRED NLG W/W WEB PER SWA EA.SDR SWAA031465Strap · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BLKHD STRAP CRACKED AT BL 0, WL 175 TO WL 242. REPAIRED STRAP PER SRM.SDR QXEA200300839Bulkhead · damagedPDX - INSTALLATION OF DOUBLER FOR RE-INFORCEMENT OF THE LEFT SIDE REAR PRESSURE BULKHEAD WHERE EDP LINES PASS THROUGH. REPAIRED IAW REO 670-53-61-034 AND REO 29-08-B, ITEM 4 PAGE 9.SDR 0301186717Bulkhead · crackedDURING L-CHECK FOUND CRACK ON RT WING LANDING GEAR PRESSURE DECK CANTED BULKHEAD AT BS 1243 RBL 75. REPAIRED PER EA 67-165075.SDR SWAA031433Bulkhead · corrodedDURING SCHEDULED SPECIAL VISIT, FOUND AFT PRESS BULKHEAD CORRODED AT BS 1016, LBL 3. REPAIRED BULKHEAD PER SRM.SDR SWAA031413Beam · crackedDURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 5.7. REPAIRED VERTICAL BEAM WEB PER SRM.SDR UIEA200300038Pressure Panel · crackedDURING C-CHECK, NOSE GEAR WHEEL TOP AT BS 366 LBL 11 FOUND CRACK FROM EDGE AND EXTENDED INBOARD APPROXIMATE 1 INCH IN LENGTH. DEFECT FOUND DURING L-CHORD REPLACEMENT AT STATION BS 340, LBL 11.33. REPAIR CARRIED OUT AS PER BOEING TELEX SEP-SIN-03-40H AND 8110SDR SWAA031406Beam · crackedDURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, WL 230 AND RBL 17.1. REMOVED AND REPLACED VERTICAL BEAM WEB PER SRM.
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