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 05FDEA02359Bulkhead · damagedUPPER FUSELAGE STA 265 UPPER FWD PRESSURE BULKHEAD EXISTING 1EA REPAIR DOUBLER ON EXTERNAL SKIN. REPAIR PER SRM 53-00-01 VOL 1 FIG 4 SHEET 2.SDR SWAA052362Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE WEB CRACKS AT BS 178 BULKHEAD, RBL 5 & LBL 5, WL 200. REPAIRED WEB PER SRM.SDR SWAA052374Pressure Panel · crackedDURING SCHEDULED SERVICE CHECK, FOUND NLG W/W RT FWD UPPER ACCESS CUTOUT, AFT INBD CORNER CRACKED AT BS 251.6, LBL 2.0. REPAIRED WEB PER SWA EA.SDR VTZA200500142Bulkhead · crackedRT SIDE PILOTS BULKHEAD AT FS 280 RBL 9.0 IS CRACKED AT 1.0" IN WEB RADIUSSDR UPS05845196Pressure Panel · corrodedINSPECTION TYPE:C1 FOUND EXFOLIATION CORROSION AND CRACKS ON COCK PIT SUBFLOOR AT STA -67 RBL 60 INSIDE RIGHT NOSE TUNNEL. CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR IAW DWG SRO8530 026 AND DC-8 SRM 51-1-20D.SDR 05FDEA02193Bulkhead · crackedRIGHT AIR CONDITIONING COMPT LOWER BULKHEAD FOUND 1 EACH CRACK 0.5 INCH LONG ON WEB AT STA 540. REPAIR PER SRM 53-00-01 FIG 7-9 VOL 1.SDR 05FDEA02174Bulkhead · crackedAIR CONDITIONING COMPT RIGHT SIDE FOUND 6 EACH CRACKS 0.5 INCH LONG ON BULKHEAD SKIN STA 500. REPAIR PER SRM 53-30-00 FIG 6 VOL 1.SDR LR7A05098Pressure Panel · crackedDURING SCHEDULED C-5 INSPECTION PER JOB CARD HC5323, FOUND FS 576 LT MLG WHEEL WELL CHINE ANGLE TO CHINE CAP WEB CRACKED .125 INCH AT BOLT HOLE, LBL 62, WL 145. REPAIRED IAW SRM SMP 583 51-140-17, NR 2059.SDR LR7A05097Flange · crackedDURING SCHEDULED C-5 INSPECTION PER JOB CARD HC3215, FOUND FS 93 BULKHEAD LOWER FLANGE CRACKED 2.5 INCH IN RADIUS AT RBL 22, WL 146. REPAIRED IAW SRM SMP 583 53-30-11, NR 2002.SDR UPS05845000Bulkhead · crackedSTAB ACCESS COMPT FWD BULKHEAD LEDGE NR 3 CRACKED AT ANGLE ATTACH, LWR (MARKED). REMOVED LT AFT BULKHEAD WALL PANEL OF MAIN CARGO DECK TO FACILITATE SHEET METAL REPAIR. CONT. TO LP 414978 NR 2: REMOVED RIVETS AND BOLTS FROM PRESS BULKHEAD TO FACILITATE REPAIRSDR COMA0570090Bulkhead · 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 SWAA052201Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT DOME CAP, 1 O'CLOCK POSITION. REPAIRED WEB PER SWA EA.SDR UPS05445068Bulkhead · crackedFX BS 260 CANTED BULKHEAD WEB FOUND CRACKED AT WL 176 LBL 67, CRACK LENGTH 1/4". FX BS 260 CANTED BULKHEAD WEB REPAIRED AT WL 176 LBL 67 AREA AS PER SRM 53-10-04 FIG 6.SDR MALA050610Bulkhead · wornWHILE ACCOMPLISHING TASK CARD 0638, NOTED WEAR MARKS ON THE FORWARD WALLS OF THE MAIN LANDING GEAR BAYS LEFT AND RIGHT SIDES.SDR ASOA05630Pressure Panel · corrodedDURING A C-CHECK, CORROSION WAS FOUND BEYOND LIMIT ON THE PRESSURE FLOOR SKIN LT SIDE BETWEEN 409 AND 128 TO 559 RBL 36 AND 45. MAINTENANCE HAS SUBMITTED A DAMAGE REPORT AND IS AWAITING AN REO FOR REPAIR. THIS MRR WILL REMAIN OPEN UNTIL THE PROPER DOCUMENTATSDR ASOA05629Pressure Panel · corrodedDURING A C-CHECK, CORROSION WAS FOUND BEYOND LIMITS ON THE PRESSURE FLOOR SKIN RT SIDE BETWEEN 409 AND 128 TO 559 RBL 36 AND 45. MAINTENANCE HAS SUBMITTED A DAMAGE REPORT AND IS AWAITING REO FOR REPAIR. THIS MRR WILL REMAIN OPEN UNTIL THE PROPER DOCUMENTATIOSDR SWAA052216Pressure Panel · crackedDURING SCHEDULED SERVICE CHECK, FOUND NLG WW LEFT UPPER ACCESS CUTOUT, AFT INBOARD CORNER CRACKED AT BS 249, LBL 2. REPAIRED WEB PER SWA EA.SDR SWAA052172Bulkhead · crackedDURING SCHEDULED C1 CHECK, FOUND FUSELAGE WEB CRACKED AT AFT PRESSURE BULKHEAD, BS 1016, STR 6R. REPAIRED AFT PRESSURE BULKHEAD WEB PER SRM.SDR SWAA052215Panel · crackedDURING SCHEDULED C4 CHECK, FOUND LEFT MLG W/W UPPER FWD CEILING PANEL CRACKED AT BS 664, LBL 39. MX FERRY TO DAL, REPAIRED PANEL PER SWA EA.SDR SWAA052125Vertical Beam · crackedDURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD RT VERTICAL BEAM WEB CRACKED AT RBL 17, WL 227. REPAIRED BEAM PER SRM.SDR 2005UALA00680Pressure Panel · crackedLT MLGWW UPPER PRESSURE DECK HAS CRACK AT STA 664 LBL 32. MAJOR REPAIR ACP'D PER MM53-21-98, INSTALLED DOUBLER REPAIR.SDR SWAA052115Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND 4 EA CRACKS AT BS 1016 PRESS BULKHEAD WEB, STR 1 TO STR 7R. REPAIRED WEB PER SWA EA.SDR SWAA052111Pressure Panel · crackedDURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS WEB CRACKED AT BS 664, LBL 39. REPAIRED WEB PER SWA EA.SDR SWAA052110Pressure Panel · crackedDURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESS WEB CRACKED AT BS 665, RBL 38 & RBL 40. REPAIRED WEB PER SRM.SDR SWAA052132Pressure Panel · crackedDURING SCHEDULED C2 CHECK, FOUND NLG W/W RT SIDE WEB CRACKED AT BS 259, WL 174. REPAIRED WEB PER SWA EA.SDR SWAA052060Pressure Panel · crackedDURING SCHEDULED SERVICE CHECK, FOUND RT NLG W/W FWD PRESSURE SIDE PANEL CRACKED AT BS 243.7, WL 168.5. REPAIRED PANEL PER SWA EA.SDR SWAA052062Bulkhead · crackedDURING SCHEDULED C2 CHECK, FOUND FUSELAGE WEB CRACKED AT AFT PRESSURE BULKHEAD, BS 1016, STR 6L. REPAIRED AFT PRESSURE BULKHEAD WEB PER SRM..SDR 05FDEA01948Bulkhead · corrodedBS 870 BULKHEAD HAS CORROSION ON FWD AND AFT SIDE AT WIRE CONNECTOR ATTACH PLATE, LBL 42. REMOVED CORROSION, FABRICATRED, ALODINED, PRIMED AND INSTALLED REPAIR PARTS PER SRM 53-10-1, 51-30-2 AND 53-10-9.SDR UPS05845012Bulkhead · crackedRT AFT PRESS BULKHEAD FWD SIDE CRACKED HORIZONTALLY .375 LONG AT RBL 35 AT APPROX 55 INCHES ABOVE FLOOR LINE AT EXISTING REPAIR DOUBLER. CUT OUT DAMAGED AREA ON BULKHD IAW SRM53-2-5 FIG 14A. FABRICATED FILLER AND INSTALLED IAW SRM 53-2-5 FIG 14A, LOCATION OFSDR USAA050853Pressure Panel · crackedCLT - FOUND PRESSURE DECK CRACKED .750 INCH, STATION 664 LBL 32.5. REMOVED DAMAGED DAMAGED AREA, INSTALLED REPAIR IAW SRM 53-60-04. (M)SDR AWXA200500872Frame · crackedDURING C16 CHECK, DISCOVERED 178 BULKHEAD CHORD CRACKED IN TWO PLACES, 1.1 INCHES IN LENGTH AND 1.3 INCHES IN LENGTH, AT BS 178, WL 184, BL 5.7L. MAINTENANCE REMOVED BOTH CRACKS ON CHORD LOCATED AT BS 178 BULKHEAD, WL 184, BL 5.7L IAW BOEING 737-300 SRM 53-10SDR AWXA200500870Bulkhead · crackedDURING C16 CHECK, DISCOVERED BULKHEAD AT BS 178, CENTER WEB, CRACKED 1.1 INCHES IN LENGTH AT BL 6.5R, WL 201. MAINTENANCE REMOVED DAMAGED SECTION OF WEB, LOCATED AT BS 178, BL 6.5R, WL 201, IAW BOEING 737-300 SRM 53-10-08-2 FIG 212. FABRICATED THREE FILLERS,SDR ASOA05587Bulkhead · crackedDURING A C-CHECK IN MCN, THE CO-PILOTS BULKHEAD WEB AT FS 280 WAS FOUND TO BE CRACKED BEYOND LIMITS APPROXIMATELY TWO INCHES OUTBOARD OF RBL 9. MAINTENANCE IS REPAIRING THE CO-PILOTS BULKHEAD WEB AT FS 280 OUTBOARD OF RBL 9 IAW BOMBARDIER REO 601R-53-11-627. SDR AWXA200500839Bulkhead · crackedMCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED 178 BULKHEAD WEB CRACKED AT 4 FASTENERS LOCATED AT WL 234, FROM BL 9L TO BL 13.5L. MAINTENANCE REMOVED DAMAGED AREA ON BULKHEAD WEB IAW BOEING 737-300 SRM 53-10-08. FABRICATED FILLER AND DOUBLER IAW BOEING 737SDR DHL2005802507Stiffener · crackedITEM REF. NR 030753: FWD ACCESSORY COMPT. FWD PRESSURE BULKHEAD STIFFENER CRACK 2.000 STA 8.000 LBL 20. REMOVED CRACKED STIFFENER IAW SRM 51-1-21 PG.1. FABRICATED NEW STIFFENER IAW SRM 53-3-3 FIG. 3. HEAT TREATED IAW SRM 51-1-1 PG. 1,13,17. INSTALLED NEW STIFFSDR DU4R0507146Bulkhead · crackedCRACK APPROX 8 IN BELOW WL 207 INBD SIDE RBL 5.7 APPROX 1.5" IN LENGTH AT BS 178 BULKHEAD.SDR DU4R0507145Bulkhead · crackedCRACK APPROX. 5.5 INCHES BELOW WL 207 IB SIDE LBL 5.7 APPROX. 1.2 INCH IN LENGTH AT BS 178 BULKHEAD.SDR UPS05845380Pressure Panel · corrodedINSPECTION TYPE:C1 LEFT W/W SKIN HEAVILY CORRODED INSIDE HAT CHANNEL STA 979 LBL 40. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW UPS EO DC8-5310 -22753-A AND SAA SK 809-850352.SDR SWAA051948Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND 2 EA CRACKS AT BS 1016 PRESSURE BULKHEAD DOME CAP WEB, 6 & 7 O'CLOCK POSITIONS. REPAIRED WEB PER BFG ER.SDR SB05078Seal · leakingCREW REPORTED A LOSS OF CABIN PRESSURIZATION. CREW ACCOMPLISHED AN EMERGENCY DESCENT, DECLARED AN EMERGENCY AND DIVERTED TO RIC WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO OXYGEN MASKS WERE DEPLOYED. MAINTENANCE FOUND AND RESECURED LOOSE POTABLE WASDR 2005UALA00617Bulkhead · cutDAMAGE CUT THROUGH SKIN FWD OF PRESSURE BULKHEAD APPROX 6 INCHES LONG AND 8-9 INCHES WIDE. INSTALLED DOUBLER REPAIR AND SPLICED STRINGER SECTION REF UA EVA-50432 AND SRM53-00-11 FI G 227.SDR UPS05444781Pressure Panel · crackedLT NWW SIDE PANEL FOUND CRACKED AT BTN BS 280 AND 300 WL 150 APPROX 1 INCH CRACK LENGTH 1 INCH. REPAIRED AS PER SRM 53-10-04 FIG 116.SDR UPS05444780Pressure Panel · crackedLT NWW SIDE PANEL FOUND CRACK AT BTN BS 260 AND 280 WL 150, CRACK LENGTH 1 INCH. REPAIRED AS PER SRM 53-10-04 FIG 116.SDR UPS05444779Pressure Panel · crackedLT NWW SIDE PANEL FOUND CRACKED AT BTN BS 280 AND 300 WL 160 APPROX 2 INCH. REPAIRED AS PER SRM 53-10-04 FIG 116.SDR UPS05444778Pressure Panel · crackedLT NWW SIDE PANEL FOUND CRACK AT BTWN BS 280 AND 300, WL 170 APPROX 1 IN, CRACK LENGTH 1 IN. LT NWW SIDE PANEL REPAIRED AS PER SRM 53-10-04 FIG 11.SDR UPS05444777Pressure Panel · crackedRT NWW SIDE PANEL FOUND 2 EA CRACK BOTH APPROX 1 INCH AT BTN BS 260 AND 280, WL 150, CRACK LENGTH 1 IN. RT NWW SIDE PANEL REPAIRED AS PER SRM 53-10-04 FIG 116.SDR AWXA200500786Bulkhead · crackedDURING C16 CHECK FOUND BULKHEAD 178 CRACKED 1.5 INCHES IN LENGTH LOCATED AT WL 234, BL 12L. MAINTENANCE REMOVED THE DAMAGED AREA AT BULKHEAD 178, WL 234, BL 12L IAW 53-10-08-1. FABRICATED FILLER AND DOUBLER REPAIR PARTS IAW SRM 53-10-08-1 FIG 209. INSTALLEDSDR AWXA200500785Bulkhead · crackedDURING C16 CHECK DISCOVERED 178 BULKHEAD WEB CRACKED AT WL 234, BL 12R. MAINTENANCE REPAIRED CRACK AT 178 BULKHEAD BY CUTTING OUT THE DAMAGED AREA IAW MFG SRM 53-10-08-2 FIG 209. FABRICATED DOUBLER AND FILLER IAW MFG SRM 53-10-08-2 FIG 209. INSTALLED FABRICSDR AWXA200500765Stiffener · corrodedDURING C-13 CHECK FOUND CORROSION PRESENT ON STIFFENER CHANNEL LOCATED AT AFT PRESSURE BULKHEAD FORWARD SIDE AT BS 1016, WL 155, BL 0. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW BOEING 737-300 SRM 53-80-08-1 FIG 101. MAINTENANCE REMOVED CORROSION ON STIFFSDR UPS05844897Pressure Blkhd · crackedINSPECTION TYPE C-1, AFT PRESSURE BULKHEAD IS CRACKED 0.5 IN LONG AT LBL 35 AND 66 IN FROM FLOOR. CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR FILLER IAW DC-8 SRM 53-2-5 FIG 14. THE -27 AND -25 DOUBLERS INSTALLED BY PREVIOUS REPAIR.
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