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 USAA960393Bulkhead Ftg · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 1156 OUTBOARD OF LEFT OUTBOARD PIVOT FITTING BULKHEAD. INSTALLED DOUBLER, REPAIRED PER EO 5391G569. (M)SDR DL72S961145Bulkhead Web · crackedTHE BS 1183 BULKHEAD WEB WAS FOUND CRACKED AT RBL 26. THERE IS A 1 INCH CRACK AT WL 170. THE WEB IS A BONDED ASSEMBLY OF 2024-T3 CLAD WITH A LOCAL THICKNESS OF 0.050 INCH. THE CRACK LOCATION IS OUTSIDE OF THE INSPECITON AREA SPECIFIED BY BOEING SERVICE BULLSDR 96ZZZX2479Bulkhead · crackedDOOR SILL DOUBLER FOUND CRACKED. CONNECTED CABIN BULKHEADS ALSO FOUND CRACKED.SDR AU960476Bulkhead · cracked(AUS) FORWARD DOOR POST BULKHEAD CRACKED ON BOTH SIDES - FOUND DURING INSPECTION IAW AD/C180/75 AMDT 1SDR USAA960370Bulkhead · crackedPIT - DURING C-4 CHECK INSPECTION, FOUND A 1.25 INCH AND 3 INCH CRACK IN REAR PRESSURE BULKHEAD Z-63 LEFT SIDE OF DOOR FRAME AT STATION 996. CUT OUT CRACKED AREAS AND INSTALLED FILLER AND DOUBLER PER USAIR EA NR 32410A. (M)SDR ABXA9700103Bulkhead · crackedDURING ACCEPTANCE INSPECTION, CRACKS WERE FOUND IN THE AFT PRESSURE BULKHEAD DOOR JAMB AT THE UPPER FOWARD RIGHT CORNER. THE FRAME WAS REPLACED AND THE SKIN WAS REPAIRED IAW THE DC-9 SRM 53-05 FIG 76.SDR 96ZZZX3107Bulkhead Strip · corrodedATW - FRAME 18 RT BULKHEAD FLOOR STRIP HAS SURFACE CORROSION. REMOVED SURFACE CORROSION, ALODINED, PRIMED AND PAINTED ALLOWABLE PER SRM.SDR SWAA960204Bulkhead Skin · wrinkledDURING SCHEDULED C-CHECK, FOUND SKIN WRINKLED AT AFT PRESSURE BULKHEAD AT BS 1016, BETWEEN S9L TO S11L. REPAIRED PER BOEING SRM.SDR DL72S960976Blkhd Stiffener · crackedA CRACK WAS FOUND EMANATING FROM THE BOTTOM OF THE LT FLANGE ON THE VERTICAL STIFFENER FS 1183 AT RBL 8. THE CRACK WAS APPROXIMATELY 0.25 INCH IN LENGTH. S/B 727-53-0175, REV 2, WHICH IS REQUIRED BY A.D. 90-06-09, CONTAINS INSPECTION, MODIFICATION, AND REPAISDR 96FDEA00750Bulkhead · corrodedCORROSION (C53-100-01, 4) ON FWD SIDE OF 178 BULKHEAD, RBL 21-26 WL 218. CORROSION WAS REMOVED WITHIN LIMITS ON BULKHEAD PER SRM 53-10-1, WEB WAS REPLACED.SDR DLM88960897Blkhd Tee Cap · damagedTHE LOWER TEE CAP SECTION OF THE AFT PRESSURE BULKHEAD AT FS 1338 WAS FOUND DAMAGED AND REQUIRED REPLACEMENT. THE DAMAGED TEE CAP WAS REMOVED AND REPLACED PER DL ERA 273379-14.SDR DL72L960773Press Blkhd · crackedADDITIONAL CRACKING OF .75 WAS FOUND ON PRESSURED DECK AT FS 289 RBL4.5. REPAIRS ACCOMPLISHED PER DL ERA 258994-14 REV A.SDR AU960507Bulkhead · cracked(AUS) FORWARD DOOR BULKHEAD CRACKEDSDR AU960475Bulkhead · cracked(AUS) LH AND RH DOOR POST BULKHEADS AND PLATES CRACKED BETWEEN NOTCH AND VACANT BOLT HOLESDR AALA960530Blkhd Plate · corrodedAFT SIDE OF STATION 1338 AFT PRESSURE BULKHEAD LOWER SIDE IN AFT CARGO COMPARTMENT HEAVY CORROSION ON PLATE. INSTALLED NEW DOUBLER PLATE SRM 53-14-3. (M)SDR CAL960505Bulkhead Skin · corrodedGSO - CORROSION FOUND AT BS 540 BETWEEN 27L AND 26L. REMOVED DAMAGE FROM WEB. FABRICATED FILLER, DOUBLER AND SHIMS. ALODINED AND PRIMED FILLER DOUBLER AND SHIMS. INSTALLED FILLER, DOUBLER AND SHIMS IAW SRM 51-10-02 AND EC/RA 5710-01723. (X)SDR CAL960506Bulkhead Skin · corrodedGSO - CORROSION FOUND AT BS 540 BETWEEN 27R AND 26R. REMOVED CORRODED AREA AROUND PNEUMATIC DUCT. FABRICATED FILLER AND DOUBLER. ALODINED AND PRIMED AS REQUIRED. INSTALLED FILLER AND DOUBLER IAW B737 SRM 51-10-2, SRM 51-30-2, AND EC/RA 5710-01723. (X)SDR CAL960457Blkhd Bracket · crackedHOU - INSPECTION FOUND A 1 INCH CRACK IN BRACKET AT AFT PRESSURE BULKHEAD, LONGERON 24R. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-60-0 AND SRM 51-30-25. (X)SDR UPS96205831Blkhd Angle · corrodedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED WHILE WORKING AC/CG, DISCOVERED CORROSION AT BS 480 29 ON BULKHEAD Z-ANGLE. REMOVED CORROSION, REWORK OUT OF LIMITS IAW SRM 53-10-1, REMOVED AND REPLACED Z-ANGLE 51-20-1 AND IAW SRM 51-10-1 AND 51-30-2.SDR UPS96205829Blkhd Sheartie · corrodedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON UPPER END OF SHEARTIE AT BS 351, RBL 45, WL 168, FORWARD SIDE OF BS 351 BULKHEAD. CORROSION OUT OF LIMITS, REPAIRED WEB AND SHEARTIE IAW SRM 51-30-2, 53-10-3, 53-10-4, 51-10-2, 51-40-2, AND 51-40-3.SDR MWEA96091Bulkhead · gougedFOUND GOUGE MARKS ON AFT SIDE OF AFT PRESSURE BULKHEAD FWD OF RT APU DOOR HINGE. INSTALLED DOUBLER REPAIR IAW SRM 53-03 FIG 22.SDR DLL10960910Bulkhead · crackedWHILE PERFORMING THE FS 1212 CANTED BULKHEAD INSPECTION PER SI 7-70645-12, A CRACK WAS FOUND AT LBL 10.0. THE CRACK WAS TRIMMED OUT AND REPAIRED PER DL ERA 273562-14.SDR CA960424023Bulkhead · cracked(CAN) DURING A 100 HOUR ANNUAL INSPECTION A CRACK WAS FOUND ON THE AFT BULKHEAD AT STA. 230.1. THE BULKHEAD IS AN ATTACH FOR THE VERTICAL FIN. THE CRACK IS LOCATED ON THE RIGHT HAND SIDE FROM THE CUT OUT FOR THE RUDDER CABLES AND MIGRATES TOWARD THE LOWER RIGHSDR 96ZZZX2417Bulkhead · crackedON INSTALLATION OF HORIZONTAL STABILIZER ATTACH BULKHEAD MOD PER SB SEB 88-3, DYE PENETRANT INSPECTION OF BULKHEAD REVEALED SEVERAL CRACKS AROUND THE TOP RIVET HOLE UNDER THE LT DOUBLER, .3125 INCH LONG, AND VISIBLE BEYOND DOUBLER ON RT FORE AND AFT DOUBLERS. SDR DL73E960741Bulkhead Web · crackedBULKHEAD 178 WAS FOUND CRACKED BENEATH THE VERTICAL STIFFENERS AT LBL 5.7 AND RBL 5.7. DAMAGE REMOVAL RESULTED IN CUT OUTS ON THE LT SIDE 3.5 AND 6 ABOVE WL 195, SAME FOR THE RT SIDE. THE WEB IS MANUFACTURED FROM 0.040 CLAD 2024-T3. ACCOMPLISHED REPAIRS PERSDR DL72K960706Blkhd Clip · crackedFOUND DURING A-2 LETTER CHECK, FS 1342 BULKHEAD AND UPPER ATTACH CLIP CRACKED 1.5 INCH AT RT SIDE AND CRACKED BEYOND STOP DRILL ON LT SIDE. REPAIRED PER MM 53-11-0.SDR UPS96405959Bulkhead Web · damagedWHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED BULK CARGO COMP. FOUND SEVERAL HOLE DAMAGES ON BULKHEAD WEB AT BS 2160, LT OF ACCESS DR. REMOVED DAMAGED SECTION OF BULKHEAD WEB AND REPAIRED WEB ACCORDING TO SRM 51-40-02.SDR 96FDEA00769Bulkhead · ripplesFUSE RIPPLES IN 1183 BULKHEAD AT BOTTOM INSIDE TAIL SKID COMP. REPAIRED RT 1183 BULKHEAD AT TAIL SKID AREA PER ESO 11782 DATED 03-18-96 AND EA NR 7-5310-28179 DATED 3-26-96.SDR UPS96205848Bulkhead · corrodedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED FINDING CORROSION ON AFT SIDE OF BS 294.5 BULKHEAD ALONG TOP OF HORIZONTAL CHORD BETWEEN RBL 4 + 25 WL 182. OUT OF LIMITS. REPAIRED 294.5 FROM LBL 26-RBL26 IAW SRM 51-10-1, 51-10-2, 51-20-4, 51-30-2, 51-30-5, 51-40SDR AALA960474Blkhd Beam · crackedFOUND VERTICAL BEAM CRACKED AT STATION 1183 RBL 36, BOTH SIDES APPROX 30 INCHES ABOVE FLOOR LINE. REPAIRED IAW BOEING 727 SB NR 727-53-0192. (M)SDR DL73S961624Bulkhead Web · crackedDURING INSPECTION PER SI 3-69482-12, THE WEB OF FS 178 BULKHEAD WAS FOUND WITH FOUR CRACKS, EACH MEASURING APPROX 1 INCH, AT LBL 5.7 AND WL 195 AND RBL 5.7 AND WL 195. THE WEB IS MANUFACTURED FROM 0.040 CLAD 2024-T3, ER/A ISSUED FOR REPAIR.SDR DL72S960690Bulkhead · crackedSTA 870 BLKHD CRACKED AT RBL 10 JUST BELOW APU BLEED VALVE ON FWD SIDE APPROX 10. REPAIRED PER SRM 53-10-9 NR 09/010.SDR SWAA960180Bulkhead Web · crackedDURING SCHEDULED D-CHECK, FOUND 1.8 INCH CRACK AT BS 178 BULKHEAD PRESSURE WEB, LBL 11.3 WL 219. REPAIRED PER BOEING SRM.SDR SWAA960179Bulkhead Web · crackedDURING SCHEDULED D-CHECK, FOUND 2 INCH CRACK AT BS 178 BULKHEAD PRESSURE WEB, RBL 9.7 WL 219. REPAIRED PER BOEING SRM.SDR QXEA9600125Blkhd Web · crackedREAR PRESSURE BULKHEAD 4 CRACKED BETWEEN BEAMS 425R AND 1050R AT HORIZONTIAL BEAM. CRACK RADIATES HORIZONTIALLY UNDER SUPPORT BRACKET BETWEEN HYDRAULIC LINES AND CANNON PLUGS. CRACK NOTED DURING C-CHECK AND REPAIRED I/A/W SRM.SDR QXEA9600117Blkhd Angle · crackedFORWARD PRESSURE BULKHEAD CONNECTION ANGLE BETWEEN STRINGERS 2 AND 3 IS CRACKED 6 INCHES LEFT OF CENTER LINE BETWEEN 2ND AND 3RD HILOCK. CRACK LENGTH IS APPROX 1 INCH. CRACK NOTED DURING C-CHECK AND REPAIRED I/A/W SRM.SDR QXEA9600116Blkhd Beam · crackedA 4 TO 5 INCH CRACK ON FORWARD PRESSURE BULKHEAD AT BEAM NR 6 COPILOTS SIDE. CRACK NOTED DURING C-CHECK. CRACK REPAIRED I/A/W SRM.SDR QXEA9600115Blkhd Frame · crackedCRACK NOTED ON FORWARD PRESSURE BULKHEAD FRAME 880/1550 LOWER CHORD LBL CRACK LENGH APPROX 2.5 INCH, LBL 3 TO 6. CRACK REPAIRED I/A/W EA 28-53-328.SDR QXEA9600114Blkhd Beam · crackedAFT SURFACE OF FRONT PRESSURE BULKHEAD IS CRACKED AT RT HORIZONTAL BEAM NR 3, CRACK LENGTH IS APPROX 5 INCHES. CRACK NOTED DURING C-CHECK. CRACK REPAIRED I/A/W SRM.SDR QXEA9600113Blkhd Stiffener · crackedA CRACK THROUGH RIVET ON VERTICAL STIFFENER BETWEEN NR 3 AND 4 HORIZONTAL BEAMS RT SIDE OF FRONT PRESSURE BULKHEAD FORWARD SIDE. CRACK NOTED DURING C-CHECK. CRACK REPAIRED I/A/W SRM.SDR 96ZZZX1778Bulkhead · crackedDURING AN ANNUAL INSPECTION, THE LOWER REAR CABIN DOORPOST BULKHEAD WAS FOUND CRACKED ON THE LEFT AND RIGHT SIDES AT THE POINT WHERE THE CABIN FLOOR AND BULKHEAD MEET. THE CRACK BEGINS AT A RADIUS RELIEF POINT AND PROPAGATES TO THE UPPER MOUNTING HOLE OF THE SDR 96FDEA00711Bulkhead · crackedAFT CARGO COMPARTMENT FS 1183 BULKHEAD IS CRACKED BL 30 RT, 10 ABOVE STR 26L COMING OUT BEHIND HORIZ STIFFENER. CRACKED AREA OF BULKHEAD REMOVED AND FILLER AND DOUBLER INSTALLED PER BOEING SB 727-53-0215.SDR 96ZZZX1475Bulkhead · crackedINSPECTION FOUND CRACKS IN CORNERS AT BULKHEAD STA 95 UPPER CORNERS.SDR SWAA960163Bulkhead · crackedDURING SCHEDULED 1/4 D-CHECK, FOUND BS 178 PRESSURE BULKHEAD CRACKED 6 INCHES TO 7 INCHES AT WL 219 AND BL 15.5, O/B RT OF RADAR UNIT. REPAIRED PER BOEING SRM.SDR SWAA960162Bulkhead · crackedDURING SCHEDULED 1/4 D-CHECK, FOUND BS 178 PRESSURE BULKHEAD CRACKED SEVERAL PLACES, AT LBL 5.7, WL 192 TO 198.5. REPAIRED PER BOEING SRM.SDR SWAA960153Blkhd Web · crackedDURING SCHEDULED D-CHECK, FOUND BULKHEAD 178 PRESSURE WEB CRACKED AT RBL 9.7, WL 219. ALSO, AT LBL 11.3, WL 219. REPAIRED PER BOEING SRM.SDR 96FDEA00592Blkhd Web · corrodedNR 0518 AND 043, WHILE WORKING NR 0468 FOUND AFT BULKHEAD OF WING CENTER SECTION TO BE CORRODED BS 870 LBL TO RBL 65 WL 178. REMOVED DAMAGED WEB AND INSTALLED NEW WEB AT BS 870 WL 162 TO 188 RBL 65 TO LBL 65.SDR 96FDEA00578Bulkhead Web · corrosionNR0079 AND 006, CORROSION (C53-100-0164) ON FWD SIDE OF 178 BULKHEAD RBL 21 TO 26 WL 218. *S/D* CORROSION WAS REMOVED WITHIN LIMITS ON BULKHEAD PER SRM 53-10-1, WEB WAS REPLACED.SDR USAA960316Bulkhead Skin · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 178 BULKHEAD SKIN. INSTALLED DOUBLER, REPAIRED PER TR 53-10-11. (M)SDR USAA960315Bulkhead Web · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK, 2 INCH CRACK, 1 INCH CRACK AND .5 INCH CRACK AT 178 BULKHEAD WEB AT LOWER LEFT RADAR DISH MOUNT. INSTALLED DOUBLER REPAIR, REPAIRED PER TR 53-10-11. (M)
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