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 95ZZZM98Blkhd Liner · damagedBULK CARGO STATION 2160 SMALL HOLE IN BULKHEAD LEFT SIDE. REPAIRED AS PER BOEING SRM 51-40-02. (M)SDR 95ZZZM153Blkhd Liner · holeBULK CARGO STATION 2160 SMALL HOLE IN BULKHEAD LEFT SIDE. REPAIRED AS PER BOEING SRM 51-40-02.SDR 95ZZZM150Blkhd Liner · holeBULK CARGO STATION 2160 SMALL HOLE IN BULKHEAD NEAR CENTER. REPAIRED AS PER BOEING SRM 51-40-02.SDR SWAA950435Bulkhead · crackedDURING SCHEDULED 1/2 D-CHECK, FOUND BS 178 PRESSURE BULKHEAD CRACKED AT REINFORCING STRAP, LBL 5.7. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950434Blkhd Web · crackedDURING SCHEDULED TRANSITION CHECK, FOUND PRESSURE BULKHEAD WEB CRACKED AT BS 178 RBL 5.5 WL 198. REPAIRED PER TRAMCO EWO 95-0337.SDR P5CA9500225Blkhd Angle · corrodedCORROSION Z-ANGLE, ON THE BULKHEAD BS 1240 RIGHT SIDE, LEVEL 1. CORROSION REMOVED PER SRM 51-10-01 AND 51-10-02.SDR MWEA95210Door Frame · crackedDURING ROUTINE INSPECTION, A 3 INCH CRACK WAS FOUND IN RADIUS OF DOOR FRAME STRUCTURE IN AFT PRESSURE BULKHEAD RT SIDE. MAINTENANCE INSTALLED SPLICE REPAIR IAW DOUGLAS TELEX NR SVC-ORD-0062/DMF. REF REWORK DWG J060110 2N 56 THROUGH 60. PERFORMED PRESSURIZEDSDR UPS203310Angle · corrodedWHILE IN SI CHECK, MAINTENANCE FOUND CORROSION AROUND NUTPLATE HOLES ON BULKHEAD SUPPORT ANGLE AT BS 480 RBL 31 TO 39, WL 160. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-30-2, 51-30-8, 51-20-4 AND 53-10-1.SDR DLL10952695Bulkhead · crackedREF EO 07-69959-12 OPN 0205 HFEC INSP LT FS 1363 BULKHEAD. CRACK INDICATION BETWEEN NR 4 AND 5 BULKHEAD WEB STIFFENERS INBD IND, FOUND AT HMV. REPLACED BULKHEAD PER ERA 271056-14 REV B.SDR 95ZZZX3147Bulkhead · crackedUPON INSPECTION FOR COMPLIANCE WITH AD 82-27-08, THE FOLLOWING DISCREPANCIES WERE NOTED: A. FS 240.62 BULKHEAD (PN 77554002) HAD 2 CRACKS APPROXIMATELY 2 INCHES LEFT AND RIGHT OF THE TAIL TIE-DOWN FITTING. THE CRACKS EXTENDED THROUGH THE BULKHEAD FLANGES.SDR USAA950697Blkhd Angle · crackedPIT - DURING Q-5 CHECK INSPECTION, FOUND .25 INCH CRACK IN ANGLE AT STA 1338 TOP CENTER OF AFT PRESSURE BULKHEAD FWD SIDE. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLERS PER SRM 53-01 PG 9. (W)SDR CAL950447Chord · corrodedGSO - THE MAIN CABIN BS 1183 BULKHEAD REINFORCEMENT CHORD AT BS 1176.9 AT RT CUSP TO AFT ENTRY DOOR CUTOUT HAD CORROSION AND BLUE WATER STAINS. THE REINFORCEMENT CHORD WAS REMOVED AND REPLACED IAW SRM 51-10-1. (M)SDR USAA950630Bulkhead · crackedPIT - DURING Q-4/CX-5 INSPECTION, FOUND .5 INCH CRACK AND BUCKLING AT 965 RT BULKHEAD BETWEEN LONGERON 17R AND 18R FLOOR LEVEL. SPLICED IN NEW WEB SECTION FROM LONGERON 18R TO 17R PER SRM 53-03 FIG 19 AND USAIR EA 30491. (W)SDR 9508996718Bulkhead · corrodedDURING PERIODIC CHECK (LON), FOUND CORROSION ON THE RIGHT BODY MAIN LANDING GEAR WELL PRESSURE DECK WEB FS 1394, RBL 91 - 97. REPAIRED PER EA 67-98212.SDR UPS203294Blkhd Flange · corrodedWHILE IN C CHECK, MAINTENANCE FOUND CORROSION AROUND NUT PLATE HOLES ON BOTTOM OF FWD FLANGE OF BEAM AT STA 870, LBL6-15, WL 207. REPAIRED FWD FLANGE OF 870 BULKHEAD UPPER CHORD PER UPS EO B727-5310-7012A.SDR 95ZZZM85Blkhd Stiffener · corrodedLEVEL 2 CORROSION FOUND AFT SIDE FS 980.00 BULKHEAD AT LONGERON 30L ATTACHMENT. MECHANICALLY REMOVED CORROSION, TREATED, PRIMED AREA, AND INSTALLED REPAIR DOUBLER IAW DER DRAWING ARW 5598-3.SDR 9508369886Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN THE CANTED BULKHEAD TO VENTRAL STAIR OPENING ATTACH FITTING FS 1292, LEFT SIDE WEB. REPLACED FITTING P/N 3957175-501 PER SRM 51-30-5.SDR 9508149959Bulkhead · crackedDURING PERIODIC CHECK, FOUND CRACK IN THE INTERCOSTAL SUPPORT FITTING BETWEEN LONGERONS 27R TO 28R, FS 996. REPLACED THE FITTING PER SRM 51-30-2.SDR SWAA950391Bulkhead · crackedFOUND PRESSURE BULKHEAD CRACKED AT BS 727, AFT WALL OF WHEEL WELL. REPAIRED PER SWA RA 253-1194.SDR 95ZZZX3280Bulkhead · crackedDURING ANNUAL INSPECTION, CRACKS WERE FOUND ON BULKHEAD EXTENDING INBOARD AND OUTBOARD FROM UPPER END OF DOUBLER PN 1212127-3 BOTH LEFT AND RIGHT SIDE. AT THAT TIME CHECKED THE THREE OTHER 182'S UNDER THIS OPERATOR'S CONTROL. FOUND SIMILAR CRACKS IN N181P, SSDR 95ZZZX3279Bulkhead · crackedDURING ANNUAL INSPECTION, CRACKS WERE FOUND ON BULKHEAD EXTENDING INBOARD AND OUTBOARD FROM UPPER END OF DOUBLER PN 1212127-3 BOTH LEFT AND RIGHT SIDE. AT THAT TIME CHECKED THE THREE OTHER 182'S UNDER THIS OPERATOR'S CONTROL. FOUND SIMILAR CRACKS IN N181P, SSDR ABXA9500743Blkhd Angle · damagedDURING D - CHECK INSPECTION, FOUND THE BULKHEAD AT FS 1041, LOWER ATTACH ANGLE FASTENER HOLES OVERSIZED ON THE LEFT SIDE. REPLACED ATTACH ANGLE IAW DC-9 SRM, CHAPTER 51-30-4.SDR DLL13952696P-Dome · corrodedAT HMV, FOUND P-DOME CORRODED, LOWER WEB AFT OF FS 1809 STRINGER 1809. REMOVED CORROSION, FABRICATED NEW SECTION, AND INSTALLED PER SRM 53-11-00 FIG 848.SDR DLL10960486Blkhd Cap · crackedTWO CRACKS WERE FOUND IN BLKHD CAP AT LBL 42.5 AND 74.5. THE CRACKS ARE LOCATED IN THE VERTICAL BLKH ATTACH FLANGE AND EMANATES FROM FASTENER HOLES. THE CRACKS HAVE BEEN REMOVED BY OVERSIZING THE SUBJECT FASTENER HOLES. ALSO, THE BLKHD WAS FOUND CRACKED AT SDR 95ZZZX4162Blkhd Web · corrodedDURING A C-CHECK INSPECTION, CORROSION WAS FOUND AT STA 351.2 FORWARD BULKHEAD WEB SHEAR TIE AND ADJACENT AREA. AS THE CORROSION WAS FOUND IN NUMEROUS AREAS, THE BULKHEAD WEB WAS REPLACED. THE REPAIR WAS ACCOMPLISHED WITH THE HELP OF BOEING AIRCRAFT COMPANY.SDR 95ZZZX2709Bulkhead · crackedFOUND DURING PROGRESSIVE INSPECTION AT ATCA. THE UPPER LEFT CORNER OF THE AFT BULKHEAD CRACKED APPROXIMATELY 1 INCH ALONG BULKHEAD BEND. ALSO, TWO CORNER CRACKS IN THE UPPER DOUBLER AT AFT BULKHEAD.SDR 95ZZZX3012Bulkhead · crackedFORWARD OF BULKHEAD CRACK FOUND - UNKNOWN ORIGIN. CRACK FOUND DURING ANNUAL INSPECTION OF LT MLG OUTB THROUGH-BOLT.SDR 95ZZZX2780Bulkhead · crackedAFTER REMOVAL OF SHIMS IN ORDER TO COMPLY WITH TB 206L-94-169. FORWARD RING WAS FOUND CRACKED UNDER SHIM AT LT LOWER ATTACH POINT. APPARENTLY, THIS IS A STRESS CRACK CAUSED BY WORKING RIVETS IN THE INTERCOSTAL ASSEMBLY.SDR 9510879995Bulkhead · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FS 37 FORWARD PRESSURE BULKHEAD AT THE 10 O'CLOCK POSITION NEAR THE RADOME CENTERING PIN. REPAIRED PER EA 99-93550.SDR 9508241158Bulkhead · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON THE CENTER ACCESS PRESSURE BULKHEAD FS 1156 AT LONGERON 43R. REPAIRED PER EA 11-98042.SDR 95ZZZX2324Bulkhead · corrodedSEVERE CORROSION ON BULKHEAD LOCATED AT STA 228.3. THE CORROSION IS AT THE UPPER PART OF THE BULKHEAD WHERE THE FORWARD STEEL ATTACHMENT FITTING IS LOCATED. THIS STEEL FITTING SERVES AS THE FORWARD VERTICAL STABILIZER ATTACHMENT POINT. PIPER SB 977 DOES NOTSDR 9508979982Bulkhead · corrodedDURING PERIODIC CHECK, FOUND CORROSION IN THE RIGHT MAIN LANDING GEAR WELL PRESSURE PANEL FS 718, RBL 50-58. REPAIRED PER EA 99-094841.SDR 9507639989Bulkhead · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION BETWEEN THE APB T-FITTING AND BULKHEAD SKIN FS 996, LBL 38 TO BL 0 AND RBL 18. REPAIRED PER EA 99-094812. MFG PART NUMBER 5910130-65.SDR DL72S951871Web · crackedDURING HMV, FOUND STA 870 WEB CRACKED AT APU BLEED VALVE CUTOUT. REPAIRED PER SRM 53-10-9.SDR 9507216613Bulkhead · crackedDURING PERIODIC CHECK, FOUND A CRACK AND CORROSION IN THE SLANTED PRESSURE PANEL LOWER EDGE FS 1241, RBL 76. REPAIRED PER EA 66-97906.SDR USAA950480Angle · crackedPIT - DURING FC- CHECK INSPECTION, FOUND 4 INCH CRACK BETWEEN STRINGER 72 AND 74 AFT SIDE OF FORWARD PRESSURE BULKHEAD CONNECTION ANGLE. SIP INSPECTION REF 53-10-06. STOP DRILLED CRACK FABRICATED AND INSTALLED NEW CONNECTION ANGLE DOUBLER PER SRM 53-11-08 PGSDR SWAA950318Blkhd Web · crackedDURING SCHEDULED MAINT CHECK, FOUND PRESSURE BULKHEAD WEB CRACKED AT BS 178, LBL 57 AND WL 201. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950311Bulkhead · crackedDURING SCHEDULED MAINT CHECK, FOUND BULKHEAD CHORD CRACKED AT BS 178, WL 195, ACCESS PLATE CUTOUT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR ABXA9500374Doubler · crackedDURING COMPLIANCE OF AD 85-01-02, SB 53-137, FOUND LEFT UPPER CORNER OF AFT PRESSURE BULKHEAD VENTRAL DOOR DOUBLER CRACKED IN RADIUS. REPAIRED IAW DC-9 SB 53-137, SERVICE REWORK DRAWING SR0J060088 AND ABX REA D953-11481-SB.SDR DLL10951686Angle · corrodedAFT P-DOME CIRCUMFERENTIAL ATTACH ANGLE IS CORRODED AT STRINGER 27 AND 32. FOUND AT HMV, REPAIRED PER SRM 53-12-00 FIG 801 AND SRM 53-11-00 FIG 848.SDR 95FDEA00469Blkhd Web · carckedCRACK IN 950 BULKHEAD RBL 22 WL 183. REPAIRED CRACK IN 950 BULKHEAD RBL 22 WL 183 PER FEDEX SRM 53-10-9.SDR 95FDEA00468Blkhd Web · crackedCRACK IN 950 BULKHEAD RBL 22 WL 166. REPAIRED CRACK IN 950 BULKHEAD RBL 22 WL 166 PER FEDEX SRM 53-10-9.SDR 95FDEA00463Bulkhead · crackedCRACK IN 950 BULKHEAD LBL 41, WL 182. REPAIRED CRACK IN 950 BULKHEAD AT LBL 41 WL 182 IAW FEDEX 727 SRM 53-10-9.SDR 95FDEA00459Bulkhead · cracked2 CRACKS IN 950 BULKHEAD LBL 5 AND RBL 5 WL 174. REPAIRED CRACKS IN 950 BLUKHEAD AT LBL 5 AND RBL 5 WL 174 PER FEDEX SRM 53-10-9 FIG 2.SDR USAA950585Bulkhead · dentedPIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND DENT IN BOTTOM OF BULKHEAD STATION 965 RT. INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 19. (M)SDR 95ZZZX3097Bulkhead · crackedFOUND 11 INCH CRACK AT THE LEFT SIDE OF BULKHEAD PRESSURE DOME AT BS 680. PERFORMED TEMPORARY REPAIR PER MCDONNELL DOUGLAS RECOMMENDATION.SDR 9506416613Blkhd Web · corrodedDURING PERIODIC CHECK, THE LEFT BODY GEAR WHEEL WELL BULKHEAD WEB AT FS 1480 WAS FOUND CORRODED. REMOVED CORROSION, ROTO PEENED, TREATED, PRIMED, AND INSTALLED STRUCTURE PER EA 66-98011.SDR UPS203079Rib Chord · crackedWHILE IN C-CHECK, MAINTENANCE FOUND CRACKS IN THE RIB CHORD ON THE RIGHT HAND SIDE AT 12 AND 6 O'CLOCK POSITION AT STATION 759, BL 70.5. MAINTENANCE REPAIRED THE CRACKS IAW UPS EO 727-5710-1271G.SDR USAA950426Bulkhead · crackedPIT - DURING Q-1 CHECK INSPECTION, FOUND .25 INCH CRACK AT REAR PRESSURE BULKHEAD STATION 996 TOP RIGHT DOOR FRAME AREA. INSTALLED DOUBLER REPAIR DACO DWG J060088-507. (M)SDR DLL10951834Bulkhead · crackedLT MLG WHEEL WELL AFT BULKHEAD HAS 5 CRACK BETWEEN STIFFENERS (LWR MID AREA).
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