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 UPS05444307Pressure Panel · crackedINSPECTION TYPE:SV NOSE WHEEL WELL RT SIDE PANEL FROM BS 280-300 WL 170 CRACK INDICATION FOUND AT FASTENER LOCATION NR 6, 10, 12 AT WEB. CRACK LENGTH 3 INCHES. CRACKED WEB REPAIRED AS PER EO B747-5310-20502-C ITEM (6) INSTRUCTION AND SRM 53-10-04 FIGURE 116.SDR UPS05444306Pressure Panel · crackedINSPECTION TYPE:SV NOSE WHEEL WELL LT SIDE PANEL FROM BS 260-280 WL 150 CRACK INDICATION FOUND BETWEEN NR 8, 13 AT WEB AREA. CRACK LENGTH 6 INCHES. CRACKED WEB REPAIRED AS PER EO B747-5310-20502 APPENDIX C ITEM (6) INSTRUCTION AND SRM 53-10-04 FIGURE 116.SDR UPS05444305Pressure Panel · crackedINSPECTION TYPE:SV NOSE WHEEL WELL LT SIDE PANEL FROM BS 280-300 WL 160 CRACK AT NR 12 TO NR 14 & NR 16 FASTENER AREA. CRACK LENGTH 5 INCH. CRACKED SIDE PANEL REPAIRED AS PER EO B747-5310-20502 APPENDIX C ITEM (6) INSTRUCTION AND SRM 53-10-04 FIGURE 116.SDR UPS05444304Pressure Panel · crackedINSPECTION TYPE:SV NOSE WHEEL WELL RT SIDE PANEL FROM BS 260 - 280 WL 170 CRACK INDICATION FOUND AT FASTENER NR 8 AT WEB AREA. CRACK LENGTH 1 INCH. CRACKED WEB REPAIRED AS PER EO B747-5310-20502-C ITEM 6 INSTRUCTION AND SRM 53-10-04 FIGURE 116.SDR UPS05444302Pressure Panel · crackedINSPECTION TYPE:SV NOSE WHEEL WELL TOP PANEL FROM BS 300 TO 320 AT LBL 20 CRACK INDICATION FOUND AT FASTENER NR 8, 9, 14, 15 & 16. CRACK LENGTH 5 INCHES. CRACKED TOP PANEL REPAIRED AS PER HX RS R53-10-35292 & UPS EO B747-5310-22075-A.SDR VTZA200500057Bulkhead · crackedRIGHT SIDE CO-PILOTS BULKHEAD AT FS 280 RBL 9.0 IS CRACKED AT 1.0 INCH IN WEB RADIUS.SDR VTZA200500056Bulkhead · crackedLEFT SIDE PILOTS BULKHEAD AT FS 280 LBL 9.0 IS CRACKED AT 1.0 INCH IN WEB RADIUS.SDR DHL2005740503Bulkhead · corrodedAFT CARGO COMPT AFT BULKHEAD BS 1183 RBL 18 TO 38 WL167 STIFFENER AND CLIP CORRODED. REMOVED STIFFENER AT AFT CARGO BLKHD BS 1183 RBL 18 TO 38 IAW B727 SRM 51-30-2. FABRICATED STIFFENER FROM BAC 1518-356 7075T6 PO NR 5080179 SIZE 20 INCH AND 2 EA FILLER FROMSDR C2XA05SH025Rib · crackedSHV - DURING C-CHECK, THE LT WINGS NR 1 FLAP TORQUE BOX HAS CRACK INDICATION ON FASTENERS O/B FWD AND AFT. MAINTENANCE OVERSIZED LT TORQUE BOX NR 1 O/B HOLE FWD AND AFT TO .277 INCH PER EMB 145 SRM 51-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR QXEA200500690Bulkhead · chafedPDX - UPPER CENTER RADOME SCREW HAS CHAFED BULKHEAD AT STATION X66, Z120. REPAIRED IAW HORIZON AIR EA 2-53-620.SDR UPS05444303Pressure Panel · crackedINSPECTION TYPE:SV NW-LT SIDE WALL WEB CRACK AT 4 EA HOLE LOCATION AT BS 280 - 300 WL 170 AREA. CRACK LENGTH 4 INCHES. NW-LT SIDE WALL WEB CRACK AREA REPAIR AS PER EO B747-5310-20502 APPENDIX C ITEM 6 INSTRUCTION & SRM 53-10-04 FIGURE 116.SDR UPS05444353Fitting · crackedINSPECTION TYPE:C RIGHT BS 1480 B/H NR 16 HOLE FOUND CRACK AT OUTER CHORD SPLICE FITTING RUNNING OUTBOARD APPROX 0.030 INCH LONG (CRACK LENGTH 0.030 INCH). RIGHT BS 1480 B/H NR 16 HOLE OVERSIZED TO 0.406 INCH & CRACK FREE AS PER EO B747-5310-10732.SDR UPS05444334Splice · crackedINSPECTION TYPE:C RH BS 1480 B/H #18 HOLE FOUND CRACK AT WEB SPLICE PLATE RUNNING UP APPROX 0.080" LONG ( CRACK LENGTH 0.080" ) NR 18 BOLT HOLE OVERSIZED TO 0.532" AT SPLICE PLATE HFEC INSP C/OUT FOUND CRACK FREE BUSHING REPAIRED AS PER EO B747-5310-10732.SDR UPS05444333Bulkhead · crackedINSPECTION TYPE: C, RT BS 1480 B/H NR 7 HOLE FOUND CRACK AT FX, SKIN RUNNING AFT APPROX .0625 INCH LONG, CRACK LENGTH .0625. HOLE OVERSIZED TO 0.687" AS PER EO B747-5310-10732 AND BUSHING INSTALLED.SDR SWAA051121Bulkhead · canningDURING SCHEDULED HC2 CHECK, FOUND BS 1016 AFT PRESSURE BULKHEAD OIL CANNED AT STR 3L. REPAIRED AFT PRESSURE BULKHEAD PER SRM.SDR SWAA051120Pressure Panel · crackedDURING SCHEDULED 1/4D CHECK, FOUND 2 EA BEADED PRESSURE WEB CRACKS AT BS 664, LBL 31 & LBL 38. REPAIRED WEB PER SWA EA.SDR QXEA200500793Bulkhead · corrodedYYC - FUSELAGE INTERIOR, LEFT LOWER WEB OF FUSELAGE STATION 280 BULKHEAD IS CORRODED ALONG THE FLOOR LINE. REPAIRED IAW REO 670-53-11-052, REV A.SDR QXEA200500794Bulkhead · corrodedYYC - FUSELAGE INTERIOR, RIGHT LOWER WEB OF FUSELAGE STATION 280 BULKHEAD IS CORRODED ALONG THE FLOOR LINE. REPAIRED IAW REO 670-53-11-052, REV A.SDR SWAA051070Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND 2 EA CRACKS AT BS 1016 BULKHEAD WEB DOME CAP, 12 O'CLOCK POSITION. REPAIRED PER SWA EA.SDR 05FDEA00953Bulkhead · damagedDURING AIRPLANE'S CONVERSION FROM P TO F FOUND: EXISTING REPAIR ON BULKHEAD, AT STA 595, X=56 LT SIDE. NO ACTION REQUIRED. REPAIR IS IAW SRM 53-20-00 FIG 6 SHEET 5.SDR DL73S050211Bulkhead · crackedTHE AFT PRESSURE P-DOME WEB WAS FOUND WITH CRACKS AS FASTENER HOLES COMMON TO THE Y-CHORD AT STRINGER 6L. THE CRACKS ARE TYPICAL OF AD 99-08-23. THE CRACKS WERE REMOVED WITH A CUTOUT AND REPAIRED WITH ALUMINUM DOUBLERS PER B737 SRM AND PER ER/A 097892-14AD.SDR ASOA05354Bulkhead · corrodedDURING HANGAR MAINTENANCE, THE FS 280 LT AND RT LOWER BULKHEAD WEB WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 280 LT AND RT LOWER BULKHEAD WEB IAW EO. (K)SDR 05FDEA00889Bulkhead · crackedCENTER CARGO HAS CRACK ON BULKHEAD AT STA 184 X=5. REPAIRED AS PER SRM 53-00-01, VOL I, FIG. 10.SDR UIEA200500049Panel · crackedD-CHECK, DURING SCHEDULED INSPECTION, CRACKS WERE FOUND AT THE LOWER CORNERS OF STA 400 BULKHEAD WEB PRESSURE PANEL CUTOUT. ANOTHER CRACK WAS FOUND ON THE LOWER IB SIDE OF THE PRESSURE PANEL ASSY. THE CRACKS ON THE STA 400 WERE TRIMMED OUT. REPAIRED DOUBLERSDR AWXA200500457Vertical Beam · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK A .25 INCH CRACK WAS FOUND IN BS 178 BULKHEAD VERTICAL BEAM WEB AT RBL 17.1, WL 230. MAINTENANCE CUT OUT DAMAGED AREA OF VERTICAL BEAM WEB AT BS 178 BULKHEAD, RBL 17.1, WL 230; PERFORMED HFEC INSPECTION OF CUTOUT TO VERISDR AWXA200500461Frame · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK A .25 INCH CRACK WAS FOUND IN BS 178 BULKHEAD SIDE CHORD AT RBL 60, WL 207. MAINTENANCE REMOVED CRACKED SIDE CHORD AT BS 178 BULKHEAD, RBL 60, WL 207; FABRICATED A NEW REPLACEMENT CHORD PER DWG 65-16300; INSTALLED REPAIRSDR AWXA200500460Frame · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK A .25 INCH CRACK WAS FOUND IN BS 178 BULKHEAD SIDE CHORD AT LBL 60, WL 207. MAINTENANCE REMOVED CRACKED SIDE CHORD AT BS 178 BULKHEAD, LBL 60, WL 207; FABRICATED A NEW REPLACEMENT CHORD PER DWG 65-16300; INSTALLED REPAIRSDR AWXA200500459Bulkhead · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK 4 EACH CRACKS WERE FOUND EXTENDING PAST STOP DRILL HOLE AND PREVIOUS REPAIR IN BS 178 BULKHEAD WEB AT RBL 5.7, WL 195. MAINTENANCE CUT OUT DAMAGED AREA OF WEB AT BS 178 BULKHEAD, RBL 5.7, WL 195; PERFORMED HFEC INSPECTIOSDR AWXA200500458Bulkhead · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK A .25 INCH CRACK WAS FOUND EXTENDING PAST STOP DRILL HOLE AND PREVIOUS REPAIR IN BS 178 BULKHEAD WEB AT LBL 5.7, WL 195. MAINTENANCE CUT OUT DAMAGED AREA OF WEB AT BS 178 BULKHEAD, LBL 5.7, WL 195; PERFORMED HFEC INSPECTSDR AWXA200500456Vertical Beam · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK 2 EACH .25 INCH CRACKS WERE FOUND IN BS 178 BULKHEAD VERTICAL BEAM WEB AT LBL 17.1, WL 230. MAINTENANCE CUT OUT DAMAGED AREA OF VERTICAL BEAM WEB AT BS 178 BULKHEAD, LBL 17.1, WL 230; PERFORMED HFEC INSPECTION OF CUTOUT SDR ASOA05296Frame · crackedDURING A C-CHECK, THE FRAME FS 640 BETWEEN STRINGER 9 AND 12 LT WAS FOUND TO BE CRACKED BEYOND LIMITS IN THE RADIUS FORWARD SIDE ABOVE THE BOX BEAM. MAINTENANCE IS REPAIRING THE FRAME FS 640 BETWEEN STRINGER 9 AND 12 LT IAW EO. (K)SDR USAA050527Access Panel · corrodedBFM - FOUND ACCESS PANEL CRACKED AND CORRODED 1.5 INCH CRACK, 3 INCH CORROSION .050 DEEP, RIGHT W/W LOWER PANEL. FABRICATED NEW PART PER 51-40-02. (M)SDR SWAA050978Panel · crackedDURING SCHEDULED 1/2D CHECK, FOUND NLG W/W CEILING PANEL CRACKED AT LT & RT BRAKE MOUNT PADS. REPAIRED PER SWA EA & SRM.SDR VTZA200500036Bulkhead · crackedRIGHT SIDE PILOTS BULKHEAD AT FS 280 RBL 9.0 IS CRACKED AT 1 INCH IN WEB RADIUS.SDR VTZA200500035Bulkhead · corrodedBULKHEAD AT FS 280 BETWEEN RBL 9.0 AND LBL 9.0 HAS LEVEL 2 CORROSION ON WEB .020 INCH DEEP.SDR 0500829606Vertical Support · crackedDURING H-CHECK, FOUND CRACK IN BULKHEAD VERTICAL SUPPORT AT BS 756 L26L AND L26R. REPAIRED PER EA 96-202532.SDR DLM88090197Pressure Panel · leakingMLG WHEEL WELL SLANT PRESSURE PANEL REPAIR IAW 09-085387-12 C/W 09-085387-12.SDR 05FDEA00650Bulkhead · corrodedAFT CARGO HAS EXFOLIATING CORROSION AT STA 1841 BULKHEAD LT SIDE X = 24. AFT CARGO AT STA 1841 BULKHEAD LT SIDE X:24 REPAIRED AREA AS PER SRM 53-00-01 VOL I FIG 10. MINOR REPAIR AS PER GMM 6-2-100.SDR ASOA05309Bulkhead · corrodedDURING HANGER MAINTENANCE, THE LT AND RT FS 280 LOWER WEB AT THE BULKHEAD WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT AND RT FS 280 LOWER WEB AT THE BULKHEAD IAW EO. (K)SDR SWAA050900Bulkhead · crackedDURING SCHEDULED C4 CHECK, FOUND 2 EA FUSELAGE CRACKS AT AFT PRESSURE BULKHEAD, BS 1016, STR 4L & BETWEEN STR 6R TO STR 7R. REPAIRED AFT PRESSURE BULKHEAD PER SWA EA.SDR 05FDEA00635Bulkhead · corrodedLOWER CHORD OF BS 950 CANTED BULKHEAD IS CORRODED, RBL 23. REPLACED BS 950 LOWER CHORD PER SRM 51-40-3 & 51-30-2.SDR 1838110Bulkhead · crackedFRAME FOUND CRACKED WHEN ASSIST STEP WAS REMOVED FOR REPAIR. THE FLOOR MUST BE REMOVED TO ACCESS THE ATTACHMENT NUTS. THE BULKHEAD HAD BEEN PREVIOUSLY REPAIRED (AIRCRAFT HAD BEEN INVOLVED IN A GEAR UP INCIDENT IN THE PAST) AND WAS CRACKED PAST THE REPAIR DOUBLSDR 0500556743Doubler · crackedDURING "L" CHECK, FOUND THREE CRACKED FASTENER HOLES ON DOUBLER AROUND APU PRESSURE PANEL CUTOUT AT BS 2360. REPAIRED PER EA 165204.SDR UIEA200500026Bulkhead · crackedDURING INSPECTION, .5 INCH CRACK FOUND ON RT WHEEL WELL SLOPING PRESSURE DECK AT STATION 1240, RBL 35. THE CRACK ORIGINATED FROM THE WATER LINE CONNECTOR HOLE AND EXTENDS UPWARDS. THE CRACKED SLOPING PRESSURE DECK WEB WAS TRIMMED OUT AND REPAIRED WITH DOUBLESDR 2005FA0000640Bulkhead · crackedFOUND DURING INSPECTION. NO EXTERNAL INDICATIONS. NO DAMAGE HISTORY. BULKHEAD AFT FUSELAGE CRACKED AND KINKED. (K)SDR 2005FA0000639Bulkhead · crackedFOUND DURING INSPECTION, MINER SKIN WRINKLES LT OF FIN. PREVIOUS DAMAGE TO RUDDER FROM THE REAR FORWARD. (K)SDR UPS05844266Bulkhead · crackedINSPECTION TYPE: C2, FWD ACCESSORY COMPT FS 683 BULKHEAD CRACKED .5 INCH LONG AT LOWER END OF VERTICAL STIFFENER LBL 18. REPAIRED FS 683 BULKHEAD IAW DC-8 SRM 53-2-5 FIG 13, 51-1-21, AND 51-1-20D.SDR VTZA200500014Bulkhead · crackedRIGHT SIDE PILOTS BULKHEAD AT FS 280 RBL 9.0 IS CRACKED AT 1.0 INCH IN WEB RADIUS.SDR 0500566743Fitting · crackedDURING L-CHECK, FOUND CRACK AND CORROSION AT BS 1480 BULKHEAD CAP FITTING LOWER FLANGE SURFACE BETWEEN S36L AND S40L. REPAIRED PER EA 67-165203.SDR QXEA200500550Bulkhead · corrodedYYC - FUSELAGE INTERIOR, FUSELAGE STATION 280 BULKHEAD LEFTHAND LOWER WEB IS CORRODED ALONG THE FLOOR CROSSBEAM. REPAIRED IAW REO 670-53-110-052, REV A.
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