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 EISA95388Bulkhead · crackedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, A 2 INCH CRACK WAS FOUND AT BS 242, 1 INCH CRACK AT BS 250, 1 INCH CRACK AT BS 251 ON N.W.W LEFT PRESS BULKHEAD. STOP DRILLED CRACKS. FABRICATED REPAIR DOUBLERS AND INSTALLED IAW B727 SRM 51-40-2 ANDSDR 95FDEA01596Blkhd Angle · crackedAFT CARGO RT 1183 BULKHEAD CRACKED HORIZONTAL ANGLE JUST BELOW FLOOR LINE RBL 50. REMOVED DAMAGED PART AND INSTALLED NEW ANGLE PER SRM 51-10-1.SDR 95FDEA01536Bulkhead · crackedAFT CARGO RT 1183 BULKHEAD CRACKED HORIZONTAL ANGLE JUST BELOW FLOOR LINE RBL 50. REMOVED DAMAGED PART, INSTALLED NEW ANGLE PER SRM 51-10-1.SDR 9516459873Blkhd Web · oil cannedDURING H-CHECK, FOUND OIL CANNING IN THE PYLON BULKHEAD WEB FS 1167, LEFT AND RIGHT SIDES. REPAIRED WEB (P/N 9912243-81, -83, -84) PER EA 98-102596.SDR 95ZZZM607Blkhd Angle · corrodedOSC - FOUND CORROSION C-PIT STATION 980 TO 36R AND 34R, BODY TO BULKHEAD ANGLE. CUT OUT DAMAGED AREA, INSTALLED REPAIR AS IT REQUIRED ACCORDING TO SKETCH AIA/E/2104 AND DOUGLAS SRMS 51-1-8 AND 51-1-20D. ENGINEERING DESIGNATION NR SO-782, SKETCH AIA/E/2104.SDR AWXA9500689Bulkhead · crackedTUS-PHX - CABIN WOULD NOT HOLD ALTITUDE WITH LT PACK OFF AND THRUST AT IDLE. DUCT PRESSURE 14 PSI AT 12,000 FEET CABINS CLIMBS AT 1500 FPM. AIRCRAFT CONTINUED TO PHX AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND 10 INCH CRACK IN BULKHEAD AT STATION 227.8. SDR UPS804787Blkhd Beam · cracked(SUPPLEMENTAL MRR) WHILE ON GROUND, MAINTENANCE FOUND AFT PRESSURE BULKHEAD J-BEAMS NR 3 AND NR 4 CRACKED AT CENTER LINE. NR 3 J-BEAM CRACK LENGTH = 3.1250 INCHES, P/N 5772638-33; NR 4 J-BEAM CRACK LENGTH = 3.0 INCHES, P/N 5772638-35. REPAIRED PER E.O. DC8-5SDR 9515569613Blkhd Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 996 AFT PRESSURE BULKHEAD LOWER FRAME FITTING. REPLACED FITTING PER SRM 51-10-03, 51-30.SDR SCNA95209Blkhd Stiffener · corrodedDURING SCHEDULED INSPECTION, CORROSION WAS FOUND ON THE VERTICAL STIFFENER ATTACHED TO THE FORWARD SIDE OF THE STATION 1521 BULKHEAD AT APPROXIMATELY BS 78. THE VERTICAL STIFFENER WAS REPAIRED IAW SUN COUNTRY ENGINEERING ORDER 53-5154-1.SDR 9515549967Blkhd Fitting · crackedDURING H-CHECK, FOUND CRACKS IN THE FS 756 FORWARD BULKHEAD FITTINGS, SECOND FROM THE TOP AND SECOND FROM THE BOTTOM. REPLACED BOTH FITTINGS PER SRM 51-30-02 AND 51-30-05.SDR UPS804738Blkhd Angle · crackedWHILE IN FOR D-CHECK, MAINTENANCE FOUND THE CENTER WING LOWER SURFACE LT AFT CORNER BULKHEAD ATTACH ANGLE CRACKED. MAINTENANCE REMOVED, FABRICATED, AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-20 AND 51-3-0.SDR UPS404641Bulkhead · crackedWHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND SMALL CRACKS ON BS 2160 BULKHEAD AT RBL 53, 10 INCHES ABOVE CARGO FLOOR AND RBL 37, 5 INCHES ABOVE CARGO FLOOR. MAINTENANCE REPAIRED IAW SRM 51-40-02.SDR UPS404636Channel · crackedWHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CHANNEL W/200 RT SIDE OF CENTER VERTICAL BEAM CRACKED AT LOWER POSITION. MAINTENANCE PRESSURE BULKHEAD CHANNEL BELOW W/200 RT SIDE OF CENTER VERTICAL BEAM. CRACK OUT OF LIMITS IAW SRM 53-10-01, REPAIRED IAW SSDR DLL17954193Bulkhead · oversized holesSEVERAL FASTENER HOLES BETWEEN STR 21 AND 22 WERE OVERSIZED TO A .25 DIAMETER. FASTENER REMOVAL ACCOMPLISHMENT OF EO 7-69959-12AD, REPAIRED PER DL ERA 271854-14AD.SDR DLL10954187Blkhd Fitting · crackedDURING THE INSPECTION OF THE AFT PRESSURE BULKHEAD STRINGER SPLICE FITTINGS, STR 10 WAS FOUND TO BE CRACKED. ACCOMPLISHED REPAIRS PER DL ERA 271858-14AD.SDR ABXA9500963Blkhd Skin · damagedDURING C-CHECK INSPECTION, FOUND DAMAGE AT FORWARD SIDE OF AFT PRESSURE BULKHEAD SKIN. REPAIRED IAW ABX REA D953-13005-MR.SDR USAA951098Blkhd Skin · crackedPIT - DURING B-CHECK INSPECTION, FOUND .25 INCH BY .5 INCH BY .022 DEEP CHAF MARK, AFT PRESSURE BULKHEAD AFT SIDE LEFT BULKHEAD SKIN. INSTALLED .063 DOUBLER AND .025 FINGER DOUBLER PER USAIR EA NR 31415.SDR ABXA9500977Blkhd Skin · gougedDURING C-CHECK INSPECTION, FOUND A GOUGE IN THE AFT SIDE OF THE AFT PRESSURE BULKHEAD. REPAIRED IAW ABX REA D953-12990-MR.SDR DLL10954163Blkhd Web · crackedDURING INSPECTION PER DAL S.I. 7-69959-12AD PART 1, THE SUBJECT AIRCRAFT WAS FOUND WITH A CRACK IN THE FUSELAGE FS 1363 BULKHEAD WEB. FURTHER INSPECTION REVEALED A SMALL CRACK AT A FASTENER HOLE LOCATED APPROXIMATELY .4 INCH ABOVE THE WEB CRACK. ACCOMPLISHEDSDR 9516379967Blkhd Web · oil cannedDURING H-CHECK, FOUND OIL CANNING IN THE FS 965 PYLON BULKHEAD WEB, LEFT SIDE. REPAIRED WEB (P/N 9912243-3), PER EA 99-103284.SDR ABXA9500976Blkhd Skin · gougedDURING C-CHECK INSPECTION, FOUND THE INLET DUCT GOUGED THE BULKHEAD SKIN AT STA 1046. REPAIRED IAW ABX REA D953-12991-MR.SDR UPS204576Blkhd Angle · corrosionWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-111-01.00-01) STA 227.8 LBL 40 WL 186 AFT SIDE OF BULKHEAD, SUPPORT ANGLE CORRODED BEYOND LIMITS. REMOVED CORRODED AREA, INSTALLED REPAIR PER SRM 51-40-4.SDR UPS204558Blkhd Angle · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-111-01.00-01) STA 227.8 RBL 38 WL 199 AFT SIDE OF BULKHEAD ON SUPPORT ANGLE. REMOVED CORROSION MECHANICALLY IAW SRM 53-10-1. REMOVED AND REPLACED ANGLE (STIFFENER) IAW SRM 51-30-2, 51-10-1.SDR UPS204537Bulkhead · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND, WHILE WORKING FUSELAGE 13/CL2-115-01, A 3 INCH CRACK ON THE 1183 BULKHEAD, RBL 8, WL 181 - 2L 178. INSTALLED REPAIRS IAW E.O. B727-5311-0635B.SDR 95ZZZX5951Bulkhead · crackedAT ANNUAL INSPECTION, FOUND BULKHEAD CRACKED AT THE 12:00 O'CLOCK POSITION BETWEEN THE RIVETS THAT ATTACH DORSAL FIN ATTACH FITTING. IT IS DIFFICULT TO SEE WHEN INSPECTING AND EASILY MISSED. A SMALL DOUBLER SHOULD BE INSTALLED WHEN THE VERTICAL STABILIZER ISSDR 9515962290Blkhd Dr Frame · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON THE AFT PRESSURE BULKHEAD DOOR FRAME WEB AT THE FLOOR LEVEL FS 1183, LBL 18. REPAIRED FRAME (P/N 65-16350-299) PER EA 22-99355.SDR CAL950883Blkhd Angle · crackedHOU - INSPECTION FOUND A 1 INCH CRACK IN ANGLE CLIP ON AFT PRESSURE BULKHEAD AT OUTBOARD NR 1L HORIZONTAL BEAM. THE CLIP WAS REMOVED AND A NEW CLIP INSTALLED PER DOUGLAS DRAWING 991558. (X)SDR 95ZZZX6029Bulkhead · crackedDURING PRIMARY INSPECTION, FOUND CRACKED BULKHEADS UNDER LEFT CABIN FLOOR, JUST FORWARD OF MAIN CABIN DOOR AREA. THREE ADJACENT BULKHEADS WERE CRACKING IN SAME AREA.SDR DLL10954171Blkhd Splice · crackedDURING INSPECTION OF THE AFT PRESSURE BULKHEAD STRINGER SPLICE FITTINGS, THE STR 10 FITTING WAS FOUND TO BE CRACKED. ACCOMPLISHED REPAIRS PER DL ERA 271943-14AD.SDR 95ZZZM635Blkhd Panel · crackedJFK - DURING C-CHECK, FOUND A 3.5 INCH CRACK IN AFT PRESSURE BULKHEAD TOP LEFT GORE PANEL. REPAIRED PER LOCKHEED SERVICE BULLETIN 93-53-258, PAGES 15 AND 16, FIGURE 4.SDR 9515849752Blkhd Frame · corrodedDURING H-CHECK, FOUND CORROSION IN THE AFT PRESSURE BULKHEAD FRAME FS 1072 FROM LONGERON 17L TO THE CUSP. REPAIRED FRAME (P/N 5910163-73), PER EA 97-101982.SDR DLL13954196Blkhd Strap · crackedTHE BULKHEAD STRAP AT FS 1363 RBL 42.5 WAS FOUND CRACKED. THE SUBJECT STRAP IS M/F .100 7075-T6 CLAD. REPAIRED PER DL ERA 271928-14AD.SDR 95FDEA01479Blkhd Web · corrodedAFT CARGO COMP FS 950 BLKD UPPER FLANGE AND WEB CORRODED BETWEEN RBL 24 - 54. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-10-9 FIG 2, SRM 51-10-9.SDR SCNA95227Blkhd Chord · corrodedDURING HEAVY MAINTENANCE VISIT (HMV), BS 950 BULKHEAD LOWER T-CHORD HAS LEVEL 2 INTERGRANULAR CORROSION AT STRINGER 29R. REMOVED AND REPLACED THE LOWER CHORD IAW B727 SRM 51-40-04 AND SRM 51-10-06.SDR 95ZZZX5989Bulkhead · crackedAFT MOST BULKHEAD CRACKED AT UPPER LEFT RUDDER CONTROL CABLE HOLE.SDR 9515789855Blkhd Web · crackedDURING H-CHECK, FOUND A CRACK IN THE AFT BULKHEAD DOOR JAMB WEB AT THE UPPER HINGE FITTING. REPAIRED WEB (P/N 5917463), PER EA 98-101981.SDR 9515761147Blkhd Skin · corrodedDURING T-CHECK, FOUND CORROSION ON THE CENTER WING FRONT SPAR PRESSURE BULKHEAD FS 1156 AT THE SKIN BETWEEN LONGERONS 47R TO 48R. REPAIRED BULKHEAD PER EA 11-98963.SDR UPS204466Doubler · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE ACCESS PANEL DOUBLER AT STATION 875, LBL 55 AND WL 165. MAINTENANCE REMOVED THE CORRODED DOUBLER, FABRICATED A NEW DOUBLER, AND INSTALLED PER SRM 51-10-2, 51-30-5 AND 51-30-2.SDR SWAA950644Bulkhead · gougedDURING SCHEDULED D-CHECK, FOUND GOUGE IN FWD SIDE OF BS 1156 BULKHEAD AND ON ADJOINING WEB BEHIND RT CENTER SECTION HINGE. REPAIRED PER TRAMCO EWO 95-0560 AND BOEING STRUCTURAL REPAIR MANUAL.SDR UPS204450Blkhd Support · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE FORWARD CARGO BAY AT THE HORIZONTAL ANGLE OF THE 680 BULKHEAD SUPPORT, LBL 13 RBL 17 AND WL 198. MAINTENANCE REPLACED THE SUPPORT IAW SRM 51-20-1, 51-30-5 AND 51-30-2.SDR CAL950852Blkhd Web · crackedHOU - INSPECTION FOUND A 3.5 INCH CRACK ON AFT PRESSURE BULKHEAD WEB AT RIGHT EDGE OF AFT ENTRY DOOR JAMB. THE BULKHEAD WEB WAS REPAIRED IAW ECRA 5310-03164. (M)SDR ABXA9500767Blkhd Skin · crackedDURING C-CHECK INSPECTION, FOUND A 2.125 INCH CRACK AT AFT PRESSURE BULKHEAD SKIN. REPAIRED IAW ABX REA D953-12807-MR.SDR DLL17954195Blkhd Skin · crackedON 8-9-91 CRACKS WERE DISCOVERED IN THE FS 328 CANTED BULKHEAD STRUCTURE DURING HMV. THIS DAMAGE WAS REPAIRED BY LAC DWG 1646545 PER ER/A 226719-14. AFTER THAT, EO 7-53207-3AD WAS ISSUED TO REINFORCE THE FS 328 CANTED BULKHEAD STRUCTURE FOR ALL DAL L1011'S, SDR 9514249949Blkhd Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FS 604 BULKHEAD END CAP AT LONGERON 24L. REPLACED FITTING PER SRM 51-01.SDR IXXA199582Blkhd Stiffener · crackedDURING C-CHECK, AN AFT PRESSURE BULKHEAD HORIZONTAL STIFFENER (THIRD FROM THE BOTTOM AT APPROXIMATELY STATION PLUS X3 TO MINUS X3) WAS FOUND TO BE CRACKED IN THE RADIUS. A DOUBLER REPAIR WAS INSTALLED IAW COTNEY ENGINEERING DRAWING SKA95164-2, DATED 8/23/95. SDR 95ZZZX6020Bulkhead · crackedINSPECTION FOUND CRACKS IN WEB FACE, AREA HUCK BOLT FASTENER. SUBMITTER STATED SB 2269 AND AD 90-08-14 SERIAL NUMBERS SHOULD BE UPGRADED TO INCLUDE TH-1574. THIS AIRCRAFT'S TOTAL TIME IS 6,495 HOURS.SDR EISA95420Blkhd Skin · crackLOWER LOBE INTERIOR 1.5 INCH CRACK IN VERTICAL STRAP AT RBL 46, BULKHEAD 1183 OUTBOARD SIDE. FABRICATED ANGLE AND FILLER IAW SRM 51-40-4 FIG 1 AND SRM 51-30-2. (M)SDR DLL10954204Blkhd Cap · crackedCORROSION WAS FOUND IN THE FUSELAGE SKIN AROUND LBL 22 AND ON THE LOWER SURFACE OF THE BULKHEAD CAP AT LBL 18. A CRACK WAS DISCOVERED UNDER THE BLKHD CAP AT LBL 22, FS 328. REPAIRED PER DL ERA 271812-14AD.SDR DLL10953699Fitting · crackedCOMPLYING WITH DL INSPECTION SI 7-66332-12 AND AD T95-18-52. AFT P-DOME TO STRINGER SPLICE FITTING WAS FOUND CRACKED AT STRINGER NR 10. SCHEDULED FITTING FOR REPLACEMENT PER DL ERA 271811-14AD.SDR ABXA9600171Blkhd Panel · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT SLANT PRESSURE PANEL CORRODED AT FS 699. REPLACED THE RIGHT SLANT PRESSURE PANEL IAW DC-9 SRM 51-30-1.
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