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.

SDR CALA9601226Bulkhead Angle · crackedINSPECTION FOUND A 3 INCH CRACK IN FRONT SPAR TO PRESSURE BULKHEAD ATTACH ANGLE AT STA 598, LONGERON 24R. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-0.Jul 29, 1996 · N70542 · Doug DC932SDR DHL9680617CBulkhead · corrodedAT C-CHECK, RIGHT W/W BULKHEAD UPPER INBD SECT OTBD OF CONTROL PULLEY HAS CORROSION. REPAIRED BULKHEAD PER EA PD 08-53-001 AND SRM 51-1-20D.Jul 26, 1996 · N806DH · Doug DC873FSDR 9617479964Bulkhead Doubler · crackedDURING M-CHECK, FOUND A 3 INCH CRACK IN THE AFT PRESSURE BULKHEAD UPPER CORNER DOUBLER AND WEB SKINS. REPAIRED SAME (P/N 5910130-13, -111, -113) PER EA DC9 53-023.Jul 26, 1996 · N912RW · Doug DC931SDR 96ZZZX4352Bulkhead Beam · corrodedLEVEL 2 CORROSION, FLOOR TO AFT BULKHEAD BEAM AROUND FASTENER HOLE IN C-3 BIN STA 1792, LBL 22. REPLACED BEAM PER SRM 51-10-05. (X)Jul 24, 1996 · N312GB · Lkheed 10113851SDR DL72W961762Bulkhead Web · crackedFOUND CRACK AT RBL 27 OF BS 1183 BULKHEAD WEB. THE DAMAGE CONSISTED OF A .75 INCH CRACK AT WL 170. THE CRACK LOCATION IS OUTSIDE OF THE INSPECTION AREA SPECIFIED BY S/B 727-53-171. REPAIRED PER B727 SRM 53-10-9, FIG. 4.Jul 23, 1996 · N2819W · Boeing 727247SDR 9617849909Bulkhead · crackedDURING M-CHECK, FOUND A 1.1 INCH CRACK IN THE AFT PRESSURE BULKHEAD UPPER INBOARD CORNER IN THE 9 DOUBLER. ALSO, FOUND A 4 INCH CRACK IN THE RIGHT SIDE VENTRAL DOOR JAMB. REPAIRED BOTH PER EA DC9-53-022.Jul 23, 1996 · N959N · Doug DC931SDR IXXA96140Bulkhead · crackedDURING ROUTINE C-CHECK INSPECTION, THE PRESSURE BULKHEAD (CABLE FEED THROUGH) AT FUSELAGE STATION 680 WAS FOUND TO BE CRACKED AT LONGERON 27 LEFT. THE BULKHEAD WAS REPLACED IAW THE AIRCRAFT SRM. (M)Jul 22, 1996 · N61CX · Doug DC862SDR USAA960523Bulkhead Skin · scratchINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .75 INCH SCRATCHAFT PRESSURE BULKHEAD SKIN 5 O'CLOCK POSITION. INSTALLED DOUBLER, REPAIREDPER SRM 53-10-4 FIG 3. (M)Jul 19, 1996 · N283AU · Boeing 7372B7SDR USAA960536Bulkhead · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND APPROX 1 INCHCRACK IN 178 BULKHEAD 2 PLACES RIGHT SIDE AT LOWER RIGHT MOUNT FOR RADAR.INSTALLED DOUBLER AND FILLERS, REPAIRED PER TR 53-10-11.(M)Jul 18, 1996 · N244US · Boeing 737201SDR USAA960535Bulkhead · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 1INCH CRACK IN 178 BULKHEAD TWO PLACES LEFT SIDE AT LOWER LEFT MOUNT FORRADAR. INSTALLED DOUBLERS, REPAIRED PER TR 53-10-11.(M)Jul 18, 1996 · N244US · Boeing 737201SDR 9616719154Bulkhead Angle · crackedDURING H-CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WHEEL WELL RIGHT INBOARD BULKHEAD UPPER ATTACH ANGLE FS 76. REPAIRED ANGLE (P/N 9910073-60) PER EA 91-110861.Jul 18, 1996 · N8913E · Doug DC914SDR USAA960513Blkhd Doubler · crackedPIT - DURING AFT PRESS BULKHEAD MOD, FOUND 4 INCH LONG CRACK AT AFTPRESS BULKHEAD STATION 996 UPPER RT CORNER OF REAR PAX DOORWAY, DOUBLER5910130-11. REPLACED UPPER HALF OF DOUBLER 5910130-11 PER EA 32891A ANDDACO DWG J060088. (M)Jul 17, 1996 · N971VJ · Doug DC931SDR USAASB96131Seals · out of positionBWI - FLT 262 - AFTER TAKEOFF FROM BWI, CAPTAIN WAS UNABLE TOPRESSURIZE AIRCRAFT. FLIGHT RETURNED TO FIELD AT BWI. NO EMERGENCY WASDECLARED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MX CLEANED WATERDRAIN LINES ON BOTH PACKS AND LINES TO LEFT AND RIGHTJul 16, 1996 · N775AU · Boeing 7374B7SDR SWAA96678Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED IN RADIUS CHORD ON LEFT SIDE AT WL 195 TO 196. REPAIRED PER BOEING SRM.Jul 16, 1996 · N315SW · Boeing 7373H4SDR ABXA9700423Bulkhead Dr Jamb · crackedDURING C-CHECK, FOUND A RADIAL CRACK IN RIGHT UPPER CORNER OF APB VENTRAL DOOR JAMB. REPAIRED IAW ABX REA D953-15626-MR.Jul 16, 1996 · N957AX · Doug DC941SDR AALA960908Bulkhead Tee · crackedTUL - DURING C-CHECK, FOUND CRACK IN FS 1156 BULKHEAD RIGHT TEE CAP INBOARD OF FIFTH FASTENER IN THE LOWER ROW OF FASTENERS FROM THE OUTBOARD END. STOP DRILLED CRACK AND INSTALLED DOUBLER PER ESO 7349 DATE 5-14-97 AND SRM 51-35-01 VOL II, SRM 51-21-01, VOL IIJul 15, 1996 · N166AA · Doug DC1010SDR CALA9601093Bulkhead Clip · crackedINSPECTION FOUND A .50 INCH CRACK IN THE LOWER AFT PRESSURE BULKHEAD CLIP ON RT SIDE AT Z= 48.5, STA 996. THE CLIP WAS REMOVED AND REPLACED IAW DOUGLAS DRAWING 9915558.Jul 11, 1996 · N18544 · Doug DC932SDR CALA9601092Bulkhead Clips · crackedINSPECTION FOUND UPPER AND LOWER AFT PRESSURE BULKHEAD CLIPS CRACKED ON LT SIDE AT Z= 48, STA 996. THE CLIPS WERE REMOVED AND REPLACED IAW DOUGLAS DRAWING 9915558.Jul 11, 1996 · N18544 · Doug DC932SDR CALA9601091Clips · crackedINSPECTION FOUND THE UPPER AND LOWER AFT PRESSURE BULKHEAD CLIPS CRACKED ON BOTH THE LT AND RT SIDES AT Z= 14, STA 996. THE CLIPS WERE REMOVED AND REPLACED IAW DOUGLAS DRAWING 9915558.Jul 11, 1996 · N18544 · Doug DC932SDR CALA9601090Bulkhead Clips · crackedINSPECTION FOUND UPPER AND LOWER AFT PRESSURE BULKHEAD CLIPS CRACKED ON BOTH LT AND RT SIDES AT Z= 24, STA 996. THE CLIPS WERE REMOVED AND REPLACED IAW DOUGLAS DRAWING 9915558.Jul 11, 1996 · N18544 · Doug DC932SDR CALA9601059Bulkhead Web · crackedINSPECTION FOUND A 7 INCH CRACK IN PRESSURE BULKHEAD WEB AT WL 218, STA 178 ON BOTH LT AND RT SIDES. BOTH CRACKED AREAS OF BULKHEAD WEB WERE CUT OUT. FILLER AND DOUBLER REPAIRS WERE FABRICATED AND INSTALLED IAW SRM'S 53-10-2, 51-10-2, AND 51-30-2.Jul 10, 1996 · N14245 · Boeing 7372C0SDR AU961046Bulkhead · cracked(AUS) FUSELAGE FRONT DOOR POST BULKHEAD CRACKED ON BOTH SIDES - CRACK LENGTHS - RH SIDE 6.35MM (0.25IN) - LH SIDE 4.762MM (0.1875IN)Jul 10, 1996 · Cessna TU206GSDR 96FDEA01236Bulkhead Tee · crackedAFT CARGO BS 1480 RBL 33 BULKHEAD UPPER CHORD FOUND CRACKED APPROX 3 INCH. *S/D* BS 1480 BULKHEAD UPPER T-CHORD REPLACED AS PER EA NR 310-96 WITH BSB 747-53-2282 REV 01 WORK INSTRUCTION.Jul 10, 1996 · N641FE · Boeing 747245FSDR 9616679104Bulkhead · crackedDURING LINE CHECK, FOUND A 4.5 INCH CRACK IN THE AFT PRESSURE BULKHEAD -13 DOUBLER RADIUS, UPPER RIGHT CORNER. REPAIRED BULKHEAD DOUBLER (P/N 5910130-1) PER EA 91-110928.Jul 10, 1996 · N94S · Doug DC915SDR DL73E961724Bulkhead Web · crackedTHREE CRACKS WERE DISCOVERED ON THE FWD 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 RBL 5.7 VERTICAL STRAP AT WL 200. THE THIRD IS LOCATED NEAR LBL 5.7 AT APPROJul 9, 1996 · N236WA · Boeing 737247SDR SWAA960643Bulkhead Web · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE BULKHEAD WEB CRACKED AT WL 200, LBL 4.7. REPAIRED PER BOEING SRM.Jul 8, 1996 · N315SW · Boeing 7373H4SDR SWAA960642Bulkhead Web · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE BULKHEAD WEB CRACKED AT WL 199.5. REPAIRED PER BOEING SRM.Jul 8, 1996 · N315SW · Boeing 7373H4SDR DHL9671508CBulkhead Angle · chafedAT D-CHECK, AFT SIDE OF STA 1183 BULKHEAD HORIZONTAL Z-ANGLE AT RBL 22 HAS BEEN CHAFED BY VERTICAL FRAME ANGLE. INSTALLED ANGLE REPAIR PER SRM 51-40-3, 1.25 INCHES BY 1 INCH.Jul 8, 1996 · N715DH · Boeing 727155CSDR DHL9671507DBulkhead Angle · chafedAT D C HECK, AFT SIDE OF 1183 BULKHEAD HORIZONTAL Z ANGLE AT LBL 22 HAS BEEN CHAFFED THROUGH BY VERTIAL DOOR FRAME ANGLE INSTALLED ANGLE REPAIR PER SRM 51-40-3 10.5 X 1.5 X 1Jul 8, 1996 · N715DH · Boeing 727155CSDR 96FDEA01241Bulkhead Web · crackedDISCREPANCY: NR 0711. FOUND CRACK ON WHEELWELL BULKHEAD STA 870, WL 190, LBL 50 (CENTER TANK). CORRECTIVE ACTION: REPAIRED PER SRM 53-10-9, FIG 4.Jul 7, 1996 · N195FE · Boeing 72722SDR 96ZZZX3560Bulkhead · crackedBULKHEAD WAS INSPECTED AFTER GROUND ACCIDENT AND FOUND CRACKED AT LOWER INNER FLANGE. THIS PART WAS PENETRANT TESTED IAW MIL-STD-6866 NC/1, DATED OCTOBER 4, 1989. MECHANIC SAID CRACK WAS NOT CAUSED BY ACCIDENT. BULKHEAD WAS REPAIRED AND REINSTALLED.Jul 5, 1996 · N34994 · Cessna 177BSDR DL73S961752Bulkhead Web · crackedDURING MID-VISIT, 178 BULKHEAD WAS FOUND TO BE CRACKED IN WEB. DAMAGE WAS REPAIRED WITH AN ALUMINUM DOUBLER IN ACCORDANCE WITH FAA/DER FORM 8110-3, DER DESIGNATION SO-867.Jul 3, 1996 · N303DL · Boeing 737232SDR GLBA96140Bulkhead · crackedSPQ - AFT CANTED BULKHEAD CRACKED AT THE LEFT RUDDER CABLE PULLEY. REPAIRED WITH USE OF KIT P/N 129-4005-1, REF WO 70383. (M)Jul 2, 1996 · N126UE · Beech 1900CSDR DLL13961881Bulkhead · buckledDURING LTR CHK, THE AFT PRESSURE BLKH AT FS 1809 WAS FOUND TO BE BUCKLED. THE DAMAGED SECTION WAS CUT OUT AND A NEW PART WAS SPLICED IN.Jul 2, 1996 · N789DL · Lkheed 10113851SDR DLL10961879Bulkhead Web · crackedDURING HMV, THE FS 449 BLKHD WAS FOUND CRACKED. THE BLKH WEB WAS CUTOUT AND A NEW SECTION WAS SPLICED IN.Jul 2, 1996 · N729DA · Lkheed 10113851SDR CALA9600997Bulkhead · damagedTHE AIRCRAFT EXPERIENCED A BIRD STRIKE RESULTING IN DAMAGE TO FUSELAGE SKIN AND BS 178 BULKHEAD WEB AT APPROXIMATELY RBL 20, WL 190. THE BULKHEAD WEB WAS REPAIRED IAW ECRA 5310-03301. THE SKIN AT STA 180 WAS REPAIRED PER SRM 53-00-01, FIGURE 27.Jul 2, 1996 · N18350 · Boeing 7373T0SDR UPS96820672Bulkhead Ftg · crackedINSPECTION TYPE-D, BOTH ATTACHMENT FITTINGS TO CANTED BULKHEAD STRUCTURE ARE CRACKED AT FS 1800 LBL AND RBL 9. REPAIRED FITTINGS PER SRM 53-2-0, FIG 1B.Jul 1, 1996 · N750UP · Doug DC871FSDR SWAA960600Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT WL 218, LBL 7 TO 10. REPAIRED PER BOEING SRM.Jun 27, 1996 · N86SW · Boeing 7372H4SDR DL73S961583Bulkhead Web · crackedCRACKS DISCOVERED ON FORWARD FACE OF FS 178 BULKHEAD WEB. THE FIRST CRACK IS LOCATED NEAR THE RBL 5.7 VERTICAL STRAP AT APROX WL 200. THE SECOND IS LOCATED NEAR THE RBL 5.7 VERTICAL STRAP AT APROX WL 203. THE THIRD IS LOCATED NEAR LBL 5.7 AT APPROXIMATELY WJun 27, 1996 · N323DL · Boeing 737232SDR DL73E961584Bulkhead Web · crackedDURING ACCOMP OF SI 3-69482-12, TWO CRACKS WERE DISCOVERED ON THE FORWARD FACE OF THE BS 178 BULKHEAD WEB. FIRST CRACK IS LOCATED UNDER THE RBL 5.7 VERTICAL STRAP AT APPROXIMATELY WL 202 AND THE SECOND IS LOCATED UNDER THE LBL 5.7 VERTICAL STRAP, RANGING BETWJun 27, 1996 · N373DL · Boeing 737247SDR AU960996Bulkhead · cracked(AUS) FORWARD DOORPOST BULKHEAD CRACKEDJun 26, 1996 · Cessna U206FSDR SWAA960586Bulkhead · crackedDURING SCHEDULED D CHECK, FOUND BULKHEAD BS 178 CRACKED AT WL 218, RBL 7 TO 12, AND AT RBL 9.5 TO 12. REPAIRED PER BOEING SRM.Jun 24, 1996 · N86SW · Boeing 7372H4SDR USAA960478Bulkhead · crackedINT - DURING 'Q-6' CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK BS 1156, WL 380 RT OUTBOARD CHORD OF BULKHEAD. STOP DRILLED AND INSTALLED REPAIR. REPAIRED PER EO 5391G569. (X)Jun 20, 1996 · N246US · Boeing 737201SDR USAA960477Bulkhead · crackedINT - DURING 'Q-6' CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK, 178 BULKHEAD. STOP DRILLED CRACK, FABRICATED DOUBLER, FILLERS, AND INSTALLED. REPAIRED PER SRM 51-01-1, TR 53-10-11. (X)Jun 20, 1996 · N246US · Boeing 737201SDR USAA960476Bulkhead · crackedINT - DURING 'Q-6' CHECK VISUAL INSPECTION FOUND 3 CRACKS, 1 INCH, 1 INCH, AND .50 INCH, 178 BULKHEAD. STOP DRILL CRACKS, FABRICATED DOUBLER, FILLERS, AND INSTALLED. REPAIRED PER SRM 51-10-1, TR 53-10-11. (X)Jun 20, 1996 · N246US · Boeing 737201SDR CALA9600865Bulkhead T-Cap · gougedINSPECTION FOUND TWO GOUGES AT TWO BOLT HOLES OF STA 1156 BULKHEAD T-CAP. THE AREA WAS REPAIRED IAW ECRA 5340-01272.Jun 20, 1996 · N68043 · Doug DC1010SDR 9614416612Bulkhead · corrodedDURING P-CHECK, FOUND CORROSION ON THE AFT PRESSURE BULKHEAD LOWER FACEPLATE AT BS 2360, LBL 11. REPAIRED FACEPLATE, EXTRUDED Y-SECTION, (P/N 65B02634-13) PER EA 66-101888.Jun 18, 1996 · N612US · Boeing 747251BSDR UPS96220474Bulkhead Angle · corrodedINSPECTION TYPE SI, CORROSION ON BULKHEAD ANGLE AT BS 480, WL 155, LBL 12, RBL 12. REMOVED AND REPLACED ANGLE IAW 51-30-02, 51-10-05 AND MM 51-20-151.Jun 16, 1996 · N929UP · Boeing 72722CSDR MWEA96172Bulkhead Angle · corrodedDURING CERT INSP, FOUND AFT CARGO COMPT BULKHEAD ANGLE HAD LIGHT CORRSION ON UNDERSIDE AT STA 996 FROM LONGERONS 25R TO 18R. SPLICED IN A NEW ANGLE IAW THE SRM 53-05, FIG 93.Jun 14, 1996 · N206ME · Doug DC932SDR ARWA9606029Press Dome · crackedRT DOME CRACKED AT LOWER INNER RADIUS. REMOVED AND REPLACED DOME PER DRAWING NR 9750428.Jun 14, 1996 · N441J · Doug DC863F
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