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 ARWA20020804Bulkhead · crackedDURING C-CHECK, AFT PRESSURE BULKHEAD UPPER RIGHT SIDE WITH 1.5 INCH CRACK STA 1766. CUT OUT DAMAGE AREA AND FABRICATED FILLER, FINGER DOUBLER AND DOUBLER IAW DRAWING SR08530007; INSTALLED PARTS IAW DRAWING SR08530007.SDR CA020723007Bulkhead · cracked(CAN) DURING A ROUNTINE STRUCTURAL 1500 HOUR INSPECTION THE FOLLOWING CRACKS WERE FOUND. B.S. 178 PRESSURE BULKHEAD WL 166.5 RBL 5.5.SDR 2002UALA01086Pressure Panel · crackedMLG CEILING HAS CRACK FORWARD AND OUTBOARD OF AILERON TOWER SHAFT. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBLER.SDR ABXA020159Bulkhead · damagedAFT PRESSURE BULKHEAD SIDE SKIN SPLICED AT Z 14.00. SPLICE NOT IAW DOUGLAS AFT PRESSURE BULKHEAD RE-WORK. SPLICED NEW SECTION (LOWER) OF RIGHT AFT PRESSURE BULKHEAD WEB IAW REA D953-44534-MR AND DOUGLAS DWG J060088.SDR GTIA020820Bulkhead · crackedFTW - FORWARD PIT AFT BULKHEAD FORWARD FACE HAS CRACKED AT UPPER ANGLE LBL 26 INCHES. DRILLED STOP CRACK ON UPPER FLANGE STATION 541 LBL 26. DRILLED AND LOCATED, INSTALLED. (M)SDR AUS20020861Bulkhead · cracked(AUS) LOWER REAR PRESSURE BULKHEAD CRACKED. CRACK IS LOCATED IN THE AREA ONE ROW OF RIVETS DOWN FROM THE LAP JOINT AND DIRECTLY ABOVE THE OUTFLOW VALVE. CRACKING IS SIMILAR TO THAT DESCRIBED IN AD/B200/67 BUT WAS NOT FOUND DURING THE AD CHECK. THE AIRCRAFT HASSDR AALA20020082Bulkhead · dentedTUL - FOUND LARGE DENT ON INBOARD BULKHEAD IN RIGHT A/C BAY. REPAIRED DAMAGE BY INSTALLING DOUBLER PER ESO 51000. (M)SDR AALA20020135Bulkhead · gougedTUL - FOUND SCRATCHES AND GOUGES ON INBOARD BULKHEAD IN LEFT AC BAY. REPAIRED DAMAGE BY INSTALLING DOUBLER PER ESO 51000. (M)SDR AALA20020148Bulkhead · dentedTUL - FOUND DENT IN INBOARD BULKHEAD IN LEFT AC BAY. REPAIRED DAMAGE BY INSTALLING DOUBLER PER ESO 51000. (M)SDR AALA20020064Bulkhead · gougedTUL - FOUND SCRATCHES AND GOUGES ON INBOARD BULKHEAD IN RIGHT A/C BAY. REPAIRED DAMAGE BY INSTALLING DOUBLERS PER ESO 51000 DATED 6-19-02. (M)SDR AUS20020704Rivet · failed(AUS) AVIONICS SHELF SUPPORT ANGLE RIVET CORRODED AND RIVET HEADSHEARED. RIVET WAS THE FOURTH RIVET FROM THE INBOARD END. FOUND DURING INSPECTION OF FORWARD PRESSURE BULKHEAD LOCATED AT FS 84.SDR ABXA020045Bulkhead · crackedCRACK IN LEFT BULKHEAD WEB, FS 1041 AT LONGERON 17L, INBOARD END. REPAIRED BULKHEAD IAW DC-9 SRM 53-01.SDR USAA020252Bulkhead · corrodedPIT - FOUND Y-CHORD AND BULKHEAD CORRODED, BS 1016 AFT PRESSURE BULKHEAD AT FLOOR LINE CENTER. CORROSION LEVEL 2, REMOVED CORROSION AND INSTALLED DOUBLERS PER EA 74025. (M)SDR ABXA020096Pressure Panel · corrodedMAIN CABIN, STATION 857 TO 880, BUTT LINE 0, CORROSION FOUND UNDER FINGER DOUBLER AND UNDER CABLE SUPPORT BRACKET. REPAIRED AREA IAW REA D853-43928-MR.SDR UPS02238852Pressure Panel · corrodedINSPECTION TYPE:C+SI, NLG W/W RIGHT CEILING PANEL CORRODED. REMOVED AND REPLACED AFT CORNER . MATERIAL REMOVED IAW SRM 51-10-01. CARRIED OUT REPAIR OF AFFECTED AREA IAW SMRO EO 2002-035-016.SDR ABXA020093Doubler · corrodedRIGHT WHEEL WELL UPPER PRESSURE DECK REPAIR DOUBLER EXFOLIATED ABOVE LONGERON 24, FS 879. REPAIRED AREA IAW ABX REA D853-43932-MR.SDR MWEA020406Shear Tie · crackedAFT ACCESSORY COMPARTMENT BULKHEAD FRAME STATION 1038 SHEAR TIE IS CRACKED JUST ABOVE LONGERON 18 LEFT. -- REMOVED SHEAR TIE SEGMENT. FABRICATED AND INSTALLED SHEAR TIE SEGMENT AND CLIPS.SDR AUS20020702Rivet · corroded(AUS) AVIONICS SHELF SUPPORT ANGLE RIVET CORRODED AND RIVET HEADSHEARED. FOUND DURING INSPECTION OF FORWARD PRESSURE BULKHEAD LOCATED AT FS 84.SDR 2002UALA00994Bulkhead · crackedSTATION 178 BULKHEAD WEB IS CRACKED AT BL 0 JUST ABOVE LOCALIZER ANTENNA MOUNT (VIEWED FROM AFT SIDE). MAJOR REPAIR ACCOMPLISHEDSDR AWXA200200546Bulkhead · crackedYVR - MAJOR REPAIR - DURING C-15 INSPECTION A WEB CRACK WAS FOUND AT FOUR RIVETS AT STA 1016 S-6L NEAR THE FWD SIDE OF THE PRESSURE BULKHEAD. DAMAGED AREA WAS CUT OUT AND HVEC WAS PERFROMED AND INSPECTED PER NDT MANUAL PART 6 , 51-00-00 FIG. 23. NO CRACKS FOUSDR SWIA200211046Firewall · crackedLEFT SIDE APU FIREWALL HAS SMALL CRACK AT LARGE CANNON PLUG TOP, RIGHT MOUNT SCREW. STOP-DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-10-00.SDR 159PL0019Bulkhead · crackedFwd side of BS178 bulkhead cracked at WL235 Lt. & Rt. sides (4 cracks total)SDR USAA020209Bulkhead · corrodedPIT - FOUND CHORDS AND WEBS CORRODED 5 INCH BY 6 INCH AREA, FORWARD SIDE AFT PRESSURE BULKHEAD BS 1018 BL 00 4 INCH BY 5 INCH. CORROSION LEVEL 2. BULKHEAD WEB AND CHORDS INSTALLED DOUBLERS PER EA 74025. (M)SDR USAA020208Bulkhead · crackedPIT - FOUND SKIN CRACKED 1.125 INCH BY 6.625 INCH CRACK, BETWEEN STRINGER 16 AND 17 OUTERSKIN STATION 178. DOUBLER INSTALLED PER EO 5300V157. (M)SDR USAA020207Bulkhead · crackedPIT - FOUND SKIN CRACKED 7.875 INCH BY 6.75 INCH, BETWEEN STRINGER 16/17, OUTER SKIN STATION 178. DOUBLER INSTALLED PER EO 5300V157. (M)SDR AALA20020803Bulkhead · worn(AFT PRESSURE BULKHEAD) WORN AREA ON AFT PRESSURE BULKHEAD LEFT AND BELOW PRESSURE RELIEF VALVE. BLENDED OUT WORN AREA TO A DEPTH OF .010. DYE CHECKED AREA. NO CRACKS FOUND. ALODINED AND PRIMED BLEND AREA THEN INSTALLED DOUBLER PER ESO.SDR SWAA021225Web · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234 AND RBL 10.5. REPAIRED WEB PER SRM.SDR AUS20020703Rivet · corroded(AUS) AVIONICS SHELF SUPPORT ANGLE RIVET CORRODED AND RIVET HEADSHEARED. FOUND DURING INSPECTION OF FORWARD PRESSURE BULKHEAD LOCATED AT FS 84.SDR AUS20020525Bulkhead · cracked(AUS) REAR FUSELAGE BULKHEAD CRACKEDIN AREA OF TOP LH HORIZONTALATTACHMENT BOLT LOCATION.SDR SWAA021196Web · crackedDURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, WL 181.5 AND RBL 5.7. REPAIRED WEB PER SRM.SDR 2002UALA00940Pressure Panel · corrodedAFT CABIN PRESSURE DECK CORRODED AT STATION 1684 RBL 52 IN. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR RYN2002F00018Pressure Panel · crackedC-CHECK, FOUND CRACK IN WEB, AT LEFT MAIN LANDING GEAR, LOWER HALF OF OUTBOARD SIDE, AT STATION 870, WATER LINE 148.SDR RYN2002F00017Pressure Panel · crackedC-CHECK, FOUND CRACK AT RIGHT MAIN LANDING GEAR WEB, LOWER HALF OUTBOARD SIDE, AT STATION 870, WATER LINE 148.SDR 2002UALA00936Bulkhead · crackedSTATION 178 BLKHD HAS NUMEROUS CRACKS LOCATED AT STA 178, WL 188, LBL 1.5, STA 178, WL188, RBL 1.5, STA 178, WL 202M LBL 7. STA 178, WL206.5, RBL 1, STA 178, RBL 5, WL 198. MAJOR REPAIR ACCOMPLISHED. BULKHEAD DOUBLER AND STRAP REPAIR MANUFACTURED AND INSTALLESDR MWEA020380Pressure Panel · gougedCENTER WING FORWARD LOWER BULKHEAD WEB HAS 1 VERY DEEP GOUGE ON FORWARD SURFACE AT STATION 606 & LONGERON 25 LEFT. FABRICATED AND INSTALLED DOUBLER.SDR AUS20020647Lap Joint · scratched(AUS) BULKHEAD LAP JOINT SCRATCHED.SDR SWAA021118Web · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 201 AND RBL 5.0. REPAIRED WEB PER SRM.SDR MWEA020365Web · crackedAFT ACCESSORY COMPARTMENT BULKHEAD WEB AT FRAME STATION 1038 IS CRACKED AT LIGHTNING HOLE AT LONGERON 12 LEFT. -- FABRICATED AND INSTALLED REPAIR DOUBLER.SDR GTIA020598Bulkhead · corrodedFTW - FOUND E/E COMPARTMENT AFT PRESSURE BULKHEAD HAS CORROSION BETWEEN L27 AND L29 STATION 218. CUT DAMAGE WEB SECTION. FABRICATED DRILLED UP AND LOCATED NEW SECTION OF WEB AND REPAIR STRAP. INSTALLED NEW WEB SECTION. (M)SDR 2002UALA00900Bulkhead · damagedSTATION 178 FORWARD BULKHEAD SKIN HAS EXCESSIVE MATERIAL LOSS. STATION 178 WL 239 RBL 12. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.SDR CA020522000Plate · cracked(CAN) THE BULKHEAD REINFORCEMENT PLATE (KIT P/N 764 028)WAS FOUND CRACKED AT AFT FUSELAGE STA 317.75 WITHIN THE SAME INSPECTION AREA OUTLINED ON PIPER SB 636A. THE REINFORCEMENT PLATE IS A PART OF PIPER KIT 764 028 INSTALLED UNDER AD96-12-12 WITH ABOUT 2000 HSDR CA020517009Bulkhead · cracked(CAN) BULKHEAD CRACKED BELOW FLOOR AT STATION 227.125 CENTER SECTION. SHEET METAL REPAIRS TO BE CARRIED OUT PRIOR TO FURTHER FLIGHT.SDR UPS02438647Bulkhead · corrodedINSPECTION TYPE:C, BS 980 RT BULKHEAD WEB STR R38 1 HOLE COMMON TO BATHTUB UPPER FITTING FOUND CORROSION FROM 5 O/C TO 9 O/C POSITION (LOOK FROM FWD). BS 980 RT BULKHEAD WEB STR R38 HOLE COMMON TO BATHTUB UPPER FITTING REPAIRED AS PER RS R53-23-34817.SDR SWAA021047Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED (2 EA) AT BS 178, WL 234 AND LBL 15. REPAIRED WEB PER SRM.SDR TSAA0253134Pressure Panel · corrodedFOUND CORROSION ON NOSE LANDING GEAR BULKHEAD AT BS 227.8. CUT OUT CORROSION AND VERIFIED REMOVED BY VISUAL INSPECTION. FABRICATED CHORD AND REPAIR ANGLES. INSTALLED CHORD AND REPAIR ANGLES. COMPLETED REPAIR.SDR 2002UALA00856Bulkhead · crackedPRESSURE BULKHEAD WEB CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBLER.SDR SWAA021042Web · corrodedDURING SCHEDULED D CHECK, FOUND VERTICAL WEB CORRODED AT BS 545, WL 152 AND LBL 41. REPAIRED WEB PER BFG ER.SDR UPS02438485Bulkhead · crackedINSPECTION TYPE:C FX- LT BS 1480 BULKHEAD WEB CRACKED AT STR 34L AS MARKED. BULKHEAD WEB REPAIRED AS PER SRM 51-40-02.SDR QXEA0200823Bulkhead · chafedPDX - LOWER PRESSURE BULKHEAD SKIN CHAFED. NOSE LANDING GEAR BAY Z115.50 Y3R Z87. REPAIRED IAW HORIZON AIR EA 2-53-395.SDR ABXA010908Tee Chord · crackedAFT PRESSURE BULKHEAD NR 2 TEE HAD 2 VERTICAL CRACKS APPROXIMATELY 1 INCH IN LENGTH AT LONGERON 14 RIGHT AND LONGERON 16 RIGHT. REPLACED THE NR 2 TEE IAW EA 53120033-006 AND REA D953-44179.
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