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 96FDEA01455Bulkhead Web · crackedNR 0506 AND 016, CRACKS IN BS 950 BULKHEAD LBL 4.5 AND RBL 4 WL 175. *S/D* REPAIRED CRACKS IN BS 950 BULKHEAD LBL 4.5 AND RBL 4, WL 175 PER FEDEX SRM 53-10-9, PERFORMED FUNCTIONAL TEST PER REDEX MM 36-00 TESTED GOOD.SDR 9619639933Blkhd Fitting · crackedDURING H-CHECK, FOUND A CRACK IN THE LEFT KEEL TO BULKHEAD ATTACH FITTING FS 756. REPLACED FITTING (P/N 3915135-505N) PER SRM 51-30.SDR 96ZZZX5425Bulkhead · crackedREAR BULKHEAD WAS FOUND CRACKED AT THE TAIL WHEEL MOUNTING SHEAR BRACKET. THE SKIN ON BOTH SIDES OF THE TAIL WHEEL MOUNTING BRACKET WERE FOUND CRACKED UPON DISASSEMBLY WITH CORROSION BETWEEN THE BRACKET AND SKIN. SUSPECT CAUSE WAS THE WEARING OF THE SKIN BY SDR 9620099930Blkhd Splice · corrodedDURING H-CHECK, FOUND CORROSION ON THE FS 756 BULKHEAD T-SPLICE BETWEEN LONGERON 29R TO 30. REPAIRED SPLICE (P/N 9958212-3) PER EA 99-110785.SDR SWAA960927Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND CRACK IN AFT SIDE OF PRESSURE BULKHEAD FWD CHORD TO VERTICAL STIFFENER AT BS 178 WL 184 LBL 5.7 AND AT WL 184 LBL 5.7. REPAIRED PER BOEING SRM.SDR DL73S962117Bulkhead Web · crackedDURING INSPECTION, 2 CRACKS WERE DISCOVERED IN THE FWD. FACEOF THE STA. 178 BULKHEAD WEB. FIRST CRACK CUTOUT MEASURES 1 1/8 X 1 AND IS LOCATED AT RBL 5.7 VERTICAL STRAP AT_WL 198. THE SECOND CRACK CUTOUT MEASURES 1.5 X 1 LOCATED_AT THE LBL 5.7 VERTICAL STRAPSDR 9619319933Bulkhead Fitting · crackedDURING H-CHECK, FOUND A CRACK IN THE FORWARD CARGO COMPARTMENT AFT BULKHEAD FITTING AT LONGERON 24L. REPLACED FITTING PER SRM 51-30-2, 51-30-5.SDR DHL9670812CBulkhead Channel · corrodedAT C-CHECK, FWD NOSE COMPT STA 227 BULKHEAD VERTICAL CHANNEL HAS CORROSION STARTING FROM BILGE CENTER LINE. REMOVED AND REPLACED VERTICAL CHANNEL PER SRM 51-10-1.SDR 9619269106Bulkhead Doubler · crackedDURING LINE CHECK, FOUND CRACKS IN THE AFT PRESSURE BULKHEAD UPPER FORWARD DOUBLER AT THE UPPER LEFT AND RIGHT DOOR STOPS IN THE -13 DOUBLER AT THE UPPER LEFT AND RIGHT DOOR CUTOUTS AND IN THE -11 DOUBLER AT THE UPPER DOOR JAMB CORNER. REPAIRED ALL DAMAGE PERSDR DL73E962052Bulkhead · crackedDURING ACCOMPLISHMENT OF SI 3-69482-12, TWO CRACKS FOUND ON THE FORWAD FACE OF THE FS 178 BULKHEAD WEB. THE FIRST CRACK IS LOCATED NEAR THE RBL 5.7 VERTICAL STRAP AT APPROX WL 198, THE SECOND IS LOCATED NEAR THE BL 0 VERTICAL STRAP AT APPROXIMATELY WL 189. SDR 9619259106Bulkhead Doubler · crackedDURING LINE CHECK, FOUND A 0.3 INCH CRACK IN THE AFT PRESSURE BULKHEAD -9 DOUBLER IN THE AFT ENTRY DOOR JAMB. REPLACED DOUBLER SECTION PER EA DC9-53-031.SDR UPS96421100Bulkhead Web · crackedINSPECTION TYPE-C, BULK CARGO COMP FOUND CRACK IN BULKHEAD WEB AT BS 2160, RBL 56 WL 168. REMOVED DAMAGED SECTION OF BULKHEAD WEB AND REPAIRED WEB ACC SRM 51-40-02 FIG 01.SDR UPS96821201Bulkhead Frame · crackedINSPECTION TYPE: CS2. HEAVY CORROSION ON BULKHEAD FRAME FS 980 LONGERON 25R, AND A 3 INCH LONG CRACK BETWEEN LONGERONS 23R-24R. REPAIRED PER UPS EO.SDR 9619099910Bulkhead Fitting · crackedDURING M-CHECK, FOUND A ONE INCH CRACK IN THE AFT PRESSURE BULKHEAD SUPPORT FITTING AT THE UPPER LEFT VENTRAL DOOR ATTACH POINT. REPLACED FITTING PER SRM 51-30-2.SDR 9619049138Bulkhead Doubler · crackedDURING H-CHECK, FOUND CRACKS IN THE AFT PRESSURE BULKHEAD 11 AND 13 DOUBLERS IN THE AFT ENTRY DOOR JAMB UPPER RIGHT CORNER. REPAIRED DOUBLERS (P/N 5910130) PER EA 91-110760.SDR UPS96220972Blkhd Stiffener · corrosionINSPECTION TYPE-C, 740 BULKHEAD VERTICAL STIFFENER HAS CORROSION ON BOTTOM AROUND FASTENERS, RBL 25 WL 146. REMOVED CORROSION AND FOUND OUT OF LIMITS. STIFFENER WAS REMOVED AND INSTALLED NEW STIFFENER. ALL WORK ACCOMPLISHED PER SRM 53-10-11, 51-30-5, 51-20-SDR SWAA960868Bulkhead Skin · crackedDURING SCHEDULED D-CHECK, FOUND BULKHEAD SKIN CRACKED AT BS 178, WL 234, RBL 11 AND 13, EMANATING FROM FASTENER HOLE. REPAIRED PER SWA RA 1-257-0346.SDR AALA961273Blkhd Stiffener · corrodedAFW - FOUND BLENDED CORROSION BEYOND SRM LIMITS ON BULKHEAD STIFFENER. REPAIR PER MRB 757-917. (M)SDR DL72K962048Bulkhead Beam · crackedINSPECTING PER SI 4-58630-12, A 2 INCH CRACK WAS FOUND OUT OF A LIGHTENING HOLE IN VERTICAL BEAM AT LBL 26.83 ON AFT SIDE OF BS 1183 BULKHEAD. THIS IS TYPICAL OF DAMAGE ADDRESSED BY BACO SB 727-53-0182. SI ALLOWS INSTALLATION OF REPAIR PER EO 4-58630-3 ON OSDR CALA9601272Bulkhead Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN AFT PIT FORWARD BULKHEAD FRAME AT STA 756, LONGERON 26R. A DOUBLER WAS INSTALLED IAW SRM 53-01.SDR IXXA96150Bulkhead · crackedDURING ROUTINE C-CHECK INSPECTION, AN 8 INCH CRACK WAS FOUND IN THE PRESSURE BULKHEAD (CABLE FEED THROUGH) AT FUSELAGE STATION 680 LEFT. THE PRESSURE BULKHEAD WAS REPLACED. (M)SDR ARWA9608015Bulkhead · corrodedMAIN CARGO LEVEL 2 CORROSION BULKHEAD LOWER PART, FS 1766 LT. REPAIRED BULKHEAD PER DOUGLAS FAX DATED 24 JULY 1996, ACTION NR 304835, SKETCH 96-07-18-004. FAA APPROVED 8110-3.SDR USAA960555Bulkhead · corrodedPIT - DURING AGING AIRCRAFT VISIT, FOUND LEVEL 1 CORROSION AT AFT PRESSURE BULKHEAD 'T' CAP STATION 996 BETWEEN LONGERONS 19 AND 20 LEFT. CUT OUT CORRODED AREAS AND INSTALLED FILLERS AND DOUBLERS PER SRM 53-03 FIG 101 AND EA 33256. (M)SDR USAA960553Bulkhead · corrodedPIT - DURING AGING AIRCRAFT VISIT, FOUND LEVEL 1 CORROSION AT AFT PRESSURE BULKHEAD 'T' CAP STATION 996 BETWEEN LONGERONS 22 AND 24 LEFT. REPAIRED PER SRM FIG 101 AND EA 33256. CUT OUT CORRODED AREAS INSTALLED FILLERS AND DOUBLERS PER SRM 53-63 FIG 1 AND EA SDR AU961148Doubler · cracked(AUS) EMPENAGE TO FUSELAGE ATTACHMENT BULKHEAD CRACKED - SEE ALSO MDR 95/0816 AND MDR 96/1142 FOR SIMILAR DEFECTSSDR P5CA9600674Bulkhead · corrodedLEVEL 1 CORROSION AT 1350 BULKHEAD LBL 118 WL 168 WHERE HYDRAULIC LINES PASS THROUGH BULKHEAD. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, REPROTECTED PER 51-10-02.SDR AU961142Bulkhead · cracked(AUS) FUSELAGE BULKHEADS CRACKED IN THE FOLLOWING LOCATIONS: 1. PNO 2412001-3 BULKHEAD LOWER LH STN 108.0 - CRACK LENGTH 27MM (1.06IN) 2. PNO 2412001-4 BULKHEAD LOWER RH STN 108.0 - CRACK LENGTH 30MM (1.18IN) 3. PNO 2412004-4 BULKHEAD LOWER RH STN 124.0 - SDR QXEA9600293Bulkhead Beam · crackedREAR PRESSURE BULKHEAD BELOW FLOOR IN AFT CARGO BAY HORIZONTAL BEAM III TOP RADIUS RT EDGE OUTBOARD OF BL 1050R IS CRACKED APPROX .375. CRACK NOTED DURING C-CHECK NR290-112, CRACK REPAIRED IAW EA 4-53-35.SDR QXEA9600292Bulkhead Beam · crackedREAR PRESSURE BULKHEAD BELOW CABIN FLOOR IN AFT CARGO BAY HORIZONTAL BEAM II TOP RADIUS RT EDGE AT BL 1050R IS CRACKED APPROX .500. CRACK NOTED DURING C-CHECK NR290-111, CRACK REPAIRED IAW EA 4-53-38.SDR ABXA9700082Bulkhead Web · drill marksDURING C-CHECK, FOUND DRILL STARTS IN APB WEB. REPAIRED IAW ABX REA D953-15885-MR.SDR SWAA960831Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND CRACK INDICATION AT UPPER RADAR MOUNT AT BS 178 BULKHEAD LBL 6.7, WL 212.3. REPAIRED CRACK PER BOEING SRM.SDR AU961202Rivet · deteriorated(AUS) RH AND LH AFT CANTED BULKHEAD RIVETS DETERIORATED - RIVET HEADS MISSINGSDR 9617869984Bulkhead Cap · corrodedDURING H-CHECK, FOUND CORROSION IN THE FS 598 BULKHEAD T-CAP FROM LONGERON 28L TO 28R. REPAIRED CAP (P/N 5914865-29) PER EA 99-110725.SDR DL72K961921Blkhd Stiffener · crackedDURING INSPECTION, THE BL 0 VERTICAL STIFFENER OF THE FUSELAGE STATION 1183 BULKHEAD WAS FOUND CRACKED AT WL 190. THE CRACK IS 1.75 INCH LONG IN THE AFT RT FLANGE WHERE A BRACKET ATTACHES. IN ACCORDANCE WITH B727 SRM 51-40-1 FIG 1, THE CRACK WAS STOP DRILLEDSDR DLL13961876Bulkhead Web · crackedDURING LTR CHECK, THE 449 BLKHD AT RBL 10 WAS FOUND TO BE CRACKED. THE BLKHD WEB WAS CUTOUT AND A NEW SECTION WAS SPLICED IN.SDR DL73E961922Bulkhead Web · crackedDURING INSPECTION, 2 CRACKS WERE DISCOVERED ON THE FWD FACE OF BS 178 BULKHEAD WEB. CRACKS WERE LOCATED UNDER THE LBL 5.7 AND RBL 5.7 VERTICAL STRAPS. IN ACCORDANCE WITH FAA/DER FORM 8110-3, DER DESIGNATION SO-957, DATED 9 AUG 1996, THE CRACKS WERE TRIMMEDSDR ABXA9700136Bulkhead Tee · corrodedDURING C-CHECK, FOUND STATION 110 BULKHEAD T-CAP CORRODED BETWEEN L26R TO L27R. REPAIRED IAW ABX REA D953-15846-MR.SDR ABXA9700118Bulkhead Tee · damagedDURING C-CHECK, FOUND BUCKING BAR MARKS ON APB UPPER T-CAP. REPAIRED IAW ABX REA D953-15875-MR.SDR DL73E961917Bulkhead Web · crackedDURING INSPECTION, MAINTENANCE DISCOVERED 5 CRACKS ON THE FWD FACE OF THE 178 BULKHEAD WEB. IN ACCORDANCE WITH FAA FORM 8110-3 DTD 8-8-96 BY DER SO-889, EACH OF THE CRACKS WERE CUT OUT AND A REPAIR DOUBLER AND FILLERS WERE INSTALLED.SDR 96ZZZX4206Bulkhead Angle · corrodedCORROSION ON FLOOR TO BULKHEAD SUPPORT ANGLE, BS 948, RBL 21 - LBL 21, WL 180 (OUT OF LIMITS PER SRM 53-60-53). REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-40-02, SRM 51-20-01.SDR RRXA96152Bulkhead Fillet · gougedDURING A MAINTENANCE VISIT, FOUND FILLET BULKHEAD PANEL LEFT SIDE DAMAGED WEB PAST LIMITATIONS IAW DC-8 SRM, AT Y=965 TO Y=990. FABRICATED NEW WEB AND DOUBLER, INSTALLED IAW REO-02128, TREATED REPAIR AREA IAW DC-8 SRM 51-1-8.SDR SWAA960797Bulkhead Chord · crackedDURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD CHORD CRACK AT BS 178, WL 208.5, TO WL 207, LBL 29. REPAIRED PER BOEING SRM.SDR SWAA960795Bulkhead Angle · crackedDURING SCHEDULED D-CHECK, FOUND T-ANGLE CRACK ON AFT SIDE OF BS 178 BULKHEAD, LBL 5.5, WL 183.5. REPAIRED PER BOEING SRM.SDR SWAA960790Bulkhead Web · gougedDURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD WEB GOUGED AT BS 178, RBL 12, WL 239. REPAIRED PER BOEING SRM.SDR SWAA960783Bulkhead · crackedDURING SCHEDULED 1/2 D-CHECK, FOUND PRESSURE BULKHEAD CRACKED AT FLOOR LEVEL FORWARD AT BS 1020, RBL 37. REPAIRED PER BOEING SRM.SDR 9617599104Bulkhead Doubler · crackedDURING LINE CHECK, FOUND A .25 INCH CRACK IN THE AFT PRESSURE BULKHEAD UPPER CORNER DOUBLER AND WEB SKIN. REPAIRED SAME (P/N 5910130-13, -111, -113) PER EA DC9-53-024, SB53-166, AND DWG J060110.SDR UPS96420815Bulkhead Web · crackedINSPECTION TYPE: C. MAIN DECK BS 400 BULKHEAD WEB CRACKED JUST BELOW LT STR 26, BS 400 LT BULKHEAD WEB CRACK REPAIRED IAW SRM 53-10-04, FIG 78.SDR AU961190Bulkhead · cracked(AUS) RH FORWARD DOORPOST BULKHEAD CRACKED IN BEND RELIEF NOTCH - FOUND DURING INSPECTION IAW AD/CESSNA180/75SDR MWEA96334Blkhd Angles · crackedDURING D-CHECK, RT SIDE T-ANGLES WERE FOUND CRACKED AT NR 1, 2, 3 AND 4 POSITIONS AT STA 996 WHERE RT FUS SKIN MEETS AFT PRESSURE BULKHEAD. FABRICATED NEW ANGLES AND INSTALLED IAW DAC DRAWING J060110.SDR CALA9601227Bulkhead Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN FRONT SPAR TO PRESSURE BULKHEAD ATTACH ANGLE AT STA 598, LONGERON 24L. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-0.
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