JASC 5312

Service difficulty reports · 20,045

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 SWAA083859Pressure Panel · crackedDURING SCHEDULED BRDG CHECK, FOUND NLG W/W LT CEILING PANEL WEB CRACKED. REPAIRED WEB PER SRM.Jul 13, 2008 · N336SW · Boeing 7373H4SDR SWIA200820342Isolator · crackedC-CHECK, THREE ISOLATORS CRACKED AT REAR PRESSURE BULKHEAD FORWARD FACE, REPLACED.Jul 12, 2008 · N440SW · Cndair CL6002B19SDR 08FDEA02841Angle · corrodedBS 740 BULKHEAD LOWER FWD SURFACE, ANGLE LBL 4.5 TO RBL 4.5, WL 146.5 HAS CORROSION ON AFT SURFACE FABRICATED NEW ANGLE REF SRM 51-10-2 PG 2, DWR 65-23555. TREATED AND PRIMED REF 51-10-2 PG 2. THIS IS CLASSIFIED AS A MAJOR REPAIR.Jul 12, 2008 · N273FE · Boeing 727233SDR 08FDEA02834Fitting · corrodedBS 740 BULKHEAD LOWER SURFACE, "T" ANGLE AT RBL 5" WL 146.5 CONNECTION TO DELTA BEAM "T" FLANGE IS CORRODED NEW T ANGLE FABRICATED ON SHOP NON-ROUTINE N00670. REMOVAL AND INSTALLATION ACCOMPLISHED ON N00167. THIS IS CLASSIFIED AS A MAJOR REPAIR.Jul 12, 2008 · N273FE · Boeing 727233SDR 08FDEA02756Bulkhead · crackedFUSELAGE STA 1183 BULKHEAD RT LOWER MIDDLE FLOOR WEB CRACKED. REF EO 7-5320-7- 310 PT 1. REPLACED WEB AND ANGLE REF SRM 51-30-02 PG 4.Jul 8, 2008 · N467FE · Boeing 727225SDR 08FDEA02746Pressure Panel · dentedFOUND NICK IN PRESSURE MEMBRANE AT C 51, TRACK 5, RT REPAIR PERFORMED BY SMOOTH REWORK, NDT FOR CRACK FREE CONDITION IAW RAS 70511614/009/2008 ISS A , APPROVED BY EA 6-5315-120080.Jul 8, 2008 · N743FD · Airbus A300B4622RSDR USAA920081297Bulkhead · crackedCLT-FORWARD PRESSURE BULKHEAD MAJOR REPAIR 03-0553-8-0105/03- CRACK IN BS 178 FORWARD PRESSURE BULKHEAD WEB, WL 218, LBL 11. REPAIRED BS 178 FORWARD PRESSURE BULKHEAD WEB, WL 218, LBL 11 IAW B737 SRM 53-10-08 (B)Jul 7, 2008 · N457UW · Boeing 7374B7SDR USAA920081298Bulkhead · crackedCLT-FORWARD PRESSURE BULKHEAD MAJOR REPAIR 03-0553-8-0105/4- CRACK IN BS 178 FORWARD PRESSURE BULKHEAD WEB WL 210 TO 213, RBL 6.5. REPAIRED BS 178 FORWARD PRESSURE BULKHEAD WEB WL 210-213, RBL 6.5 IAW B737 SRM 53-10-08 (B)Jul 7, 2008 · N457UW · Boeing 7374B7SDR USAA920081325Bulkhead · crackedCLT - FORWARD PRESSURE BULKHEAD - MAJOR REPAIR - CRACK ON WEB AT 178 BULKHEAD WL 226, LBL 17. REPAIRED WEB AT 178 BULKHEAD WL 226, LBL 17 IAW B737 SRM 53-10-08. (S)Jul 7, 2008 · N457UW · Boeing 7374B7SDR CA080703002Bulkhead · cracked(CAN) A HALF-INCH CRACK WAS NOTED RADIATING FROM THE FLANGE BEND RELIEF CUTOUT NEAR THE BOTTOM OF THE LT SIDE OF THE BULKHEAD AT STATION 108 (IMMEDIATELY INSIDE THE BAGGAGE DOOR), JUST ABOVE FLOOR LEVEL. THIS AREA IS NORMALLY COVERED BY PLASTIC INTERIOR PANELJul 3, 2008 · Cessna 172MSDR COMA0860320Bulkhead · crackedCRACK ON FS 202 AROUND PARKING BRAKE CABLE. REPAIRED CRACK ON FS 202 AROUND PARKING BRAKE CABLE IAW EA 10-5311-01914. (A)Jul 3, 2008 · N963CA · Cndair CL6002B19SDR KCSA081307Bulkhead · corrodedRT WHEEL WELL CANTED BULKHEAD AT STA. 1241 HAS CORROSION ON LOWER CHORD INBOARD OF BULKHEAD FITTING RBL 98 (B)Jul 2, 2008 · N712CK · Boeing 747122SDR SWAA083708Pressure Panel · crackedDURING SCHEDULED HC1 CHECK, FOUND LT MLG WHEEL WELL CEILING CRACKED AT BS 664, LBL 31. REPAIRED SKIN PER SRM.Jul 2, 2008 · N617SW · Boeing 7373H4SDR CALA0800667Bulkhead · crackedSTATION 178 BULKHEAD WL 207 LBL 4.5 FASTENER HOLE SHOWS CRACK INDICATION. REAMED HOLE TO .214 IAW ECRA 5310-04794 HFEC IAW B737 NDT MANUAL PT6-51-00-00 SIG.16 OF OPEN HOLE NO CRACKS NOTED. REAMED HOLE TO.246 FOR INSURANCE CUT IAW ECRA 5310-04794 INSTALLED FAJul 2, 2008 · N13624 · Boeing 737524SDR TRAX200800865Bulkhead · crackedFS 559 BULKHEAD WEB HAS INDICATIONS AT WL 58.70 I/B OF RBL 18 APPROX 1.3" IN LENGTH AND O/B OF RBL 9 APPROX .4" IN LENGTH, AND CAP ANGLE AT LBL 18, AND RBL 18 APPROX .5 IN LENGTH FAILED NDT INSP. (B) REPAIRED FS 559 BULKHEAD WEB AND CAP ANGLE ON LT AND RT SIJul 1, 2008 · N827AS · Cndair CL6002B19SDR TRAX200800863Bulkhead · crackedREAR PRESSURE BULKHEAD WEB THAT SURROUND THE LINTEL ATTACHMENT FITTING HAS AN INDICATION NOTED APPROX .2" IN LENGTH 1005 FULL SCREEN HEIGHT FAILED NDT INSP. (B) REPAIR PER EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETED AND THE REPAIR C/W THE REQUIREMENTS OF ECJul 1, 2008 · N827AS · Cndair CL6002B19SDR TRAX200800859Bulkhead · crackedAFT PRESSURE BULKHEAD FS 621 IS CRACKED AT THE LINTEL FITTING AREA. OPEN (B)Jul 1, 2008 · N861AS · Cndair CL6002B19SDR LR7A08087Bulkhead · crackedDURING SCHEDULED B-2 CHECK, PER JOB CARD HB5302, FOUND LT AFT FUSELAGE INTERIOR LOWER BULKHEAD WEB CRACKED THROUGH FASTENER HOLE AT FS 880L, WL200. REPAIR IAW DRAWING 342582 BY FABRICATING AND INSTALLING WEB.Jul 1, 2008 · N404LC · Lkheed 382GSDR LR7A08086Bulkhead · crackedDURING SCHEDULED B-2 CHECK, PER JOB CARD HB5302, FOUND RT AFT FUSELAGE INTERIOR LOWER BULKHEAD WEB CRACKED THROUGH FASTENER HOLE AT FS 880R, WL 200. REPAIR IAW DRAWING 342582 BY FABRICATING AND INSTALLING WEB.Jul 1, 2008 · N404LC · Lkheed 382GSDR TRAX200800852Bulkhead · crackedSUSPECT CRACK AT FWD PRESSURE BULKHEAD FS 202.75 AT THE PILOTS BRAKE CONTROL PUSH/PULL CABLE LOCATION. THIS SDR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (B)Jun 30, 2008 · N861AS · Cndair CL6002B19SDR 08FDEA02512Bulkhead · corrodedNOSE WHEEL WELL AFT WALL (STA 351) SURFACE UNDER DOWN LOCK ACTUATOR MOUNT IS CORRODED. REMOVED CORROSION, NDT, MATERIAL THICKNESS, ORIG. "T" = .072" MAT REMAINING =.065". .007' MAT LOSS. WITHIN LIMITS REF FED EX EA NR 7-5310-113999, TREATED AND PRIMED, AND Jun 27, 2008 · N467FE · Boeing 727225SDR UPS08853099Bulkhead · crackedINSPECTION TYPE:C2 FWD ACCESSORY COMPT BULKHEAD AT STA 683 LBL 21 BELOW FASTENER PATTERN ATTACHING BULKHEAD DOME TO WING LOWER FRONT SPAR WEB HAS 3 INCH CRACK. REMOVED WEB, REPLACED WEB IAW SRM 51-1-21.Jun 26, 2008 · N752UP · Doug DC871FSDR FDEA200806252448Bulkhead · crackedLT MLG WW FOUND CRACK ON VERTICAL BULKHEAD. REPAIRED AREA IAW SRM 53-00-01 FIG 4 VOL I.Jun 25, 2008 · N10060 · Doug DC1010SDR 08FDEA02459Bulkhead · crackedCRACK IN RIGHT WHEEL WELL 870 BULKHEAD BOTTOM SIDE OF APU BLEED VALVE DUCT CUTOUT. FABRICATED REPAIR DOUBLER IAW SRM 53-10-9, & FILLER, INSTALLED REPAIR PARTS IAW SRM 53-10-9 FIG 5.Jun 25, 2008 · N494FE · Boeing 727227SDR 08FDEA02448Bulkhead · crackedLT MLG WW FOUND CRACK ON VERTICAL BULKHEAD.Jun 25, 2008 · N10060 · Doug DC1010SDR 08FDEA02440Bulkhead · corrodedNOSE WHEEL WELL-STA 1090/FR11, LIGHT SURFACE CORROSION FOUND ON W/W FWD WALL, LOCATED RBL8.0 BETWEEN STIFFENERS 5/6. REMOVED THE LIGHT CORROSION PER SRM 51-74-10. APPLIED ALODINE PER SRM 51-21-10. NO CRACK FOUND PER NTM 51-10-08. THE REMAINING THICKNESS ISJun 25, 2008 · N456FE · Airbus A310222SDR CA080625007Bulkhead · cracked(CAN) MAINT WAS CARRYING OUT THE FIRST 1000 CYCLE REPETITIVE INSP AFTER INITIAL 10000 CYCLE STRUCTURAL INSP. FOUND A 4 INCH CRACK IN THE FS 280.275 BULKHEAD WEB, ON THE LT SIDE AT THE STRINGER NR 4 CUTOUT. THE BULKHEAD WAS CRACKED ALL THE WAY THROUGH. THICKNJun 24, 2008 · Beech 300BEECHSDR TRAX200800834Bulkhead · crackedREAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS AN INDICATION NOTED APPROX .2 INCH IN LENGTH 100% FULL SCREEN HEIGHT. FAILED NDT INSPECTION. REPAIRED REAR PRESSURE BULKHEAD AT LINTEL ATTACHMENT FITTING IAW REO 601R-53-61-1230. REJun 24, 2008 · N977EV · Cndair CL6002B19SDR 08FDEA02378Bulkhead · crackedCENTER LANDING GEAR WHEEL WELL STATION 1391 LEFT WEB CORNER DOUBLER FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Jun 23, 2008 · N586FE · Doug MD11FSDR SWAA083458Pressure Panel · crackedDURING SCHEDULED MV2 CHECK, FOUND BEADED PRESSURE DECK WEB CRACKED AT BS 540, LBL 25. REPAIRED WEB PER SRM.Jun 23, 2008 · N369SW · Boeing 7373H4SDR A6WA200840528Bulkhead · crackedCRACK EXIST OF FWD PRESSURE BULKHEAD AT FS 202.0, LBL 23.71, PARKING BRAKE AREA. FWD PRESSURE BULKHEAD AT FS 202 AND LBL 23.71 REPAIRED IAW CRJ 200 REO 601R-53-11-563. (A)Jun 21, 2008 · N446AW · Cndair CL6002B19SDR UIE2008F00007Pressure Panel · crackedNOSE WHEEL WELL TOP PANEL WEB FOUND WITH A CRACK AT BS 304 AT RBL11. CRACK LENGTH IS 2.250 INCHES. INTERIM REPAIR ACCOMPLISHED IAW SRM 53-10-04, FIG 116, SHEETS 1 AND 6 AND FIG 117, SHEETS 1 THRU 10. REQUIRES INITIAL INTERNAL DETAIL VISUAL INSPECTION PRIOR TJun 21, 2008 · N524MC · Boeing 7472D7BSDR UIE2008F00006Pressure Panel · crackedNOSE WHEEL WELL TOP PANEL WEB FOUND WITH A CRACK AT BS 310 AT LBL 10. CRACK LENGTH IS 1.125 INCHES. INTERIM REPAIR ACCOMPLISHED IAW SRM 53-10-04, FIG 116. SHEETS 1 AND 6 AND FIG 117 SHEETS 1 THRU 10. REQUIRES INITIAL INTERNAL DETAIL VISUAL INSPECTION PRIORJun 21, 2008 · N524MC · Boeing 7472D7BSDR USAA920081260Bulkhead · crackedPIT - FORWARD PRESSURE BULKHEAD - MAJOR REPAIR - VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17 JUST BELOW WL 234. REPAIRED VERTICAL BEAM WEB AT BS 178, LBL 17 JUST BELOW WL 234 IAW B737 SRM 53-10-08. (S)Jun 21, 2008 · N530AU · Boeing 7373B7SDR 08FDEA02356Bulkhead · failedPREVIOUS REPAIR LOCATED AT FRAME 80/82 AFT PRESSURE BULKHEAD FORWARD SIDE CIRCUMFERENTIAL STRAP AND FRAME WEB REPAIR BETWEEN STR 48 LT AND 48 RT WITH 2 EA FRAME WEB REPAIR PLATES, 2 CIRCUMFERENTIAL REPAIR SPLICE STRAPS AND 1 CIRCUMFERENTIAL REPAIR SECTION REPAJun 20, 2008 · N443FE · Airbus A310203SDR SWAA083339Bulkhead · crackedDURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6L. REPAIRED WEB PER ER.Jun 18, 2008 · N695SW · Boeing 7373Q8SDR SWAA083353Bulkhead · crackedDURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6L. REPAIRED WEB PER SRM.Jun 18, 2008 · N336SW · Boeing 7373H4SDR SWAA083352Bulkhead · crackedDURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6R. REPAIRED WEB PER SRM.Jun 18, 2008 · N336SW · Boeing 7373H4SDR SWAA083362Stiffener · crackedDURING SCHEDULED SPV CHECK, FOUND AFT PRESSURE BULKHEAD RADIAL STIFFENER CRACKED AT BS 1016, NR 19 POSITION. REMOVED AND REPLACED STIFFENER PER SRM.Jun 18, 2008 · N314SW · Boeing 7373H4SDR SWAA083361Stiffener · crackedDURING SCHEDULED SPV CHECK, FOUND AFT PRESSURE BULKHEAD RADIAL STIFFENER CRACKED AT BS 1016, NR 16 POSITION. REMOVED AND REPLACED STIFFENER PER SRM.Jun 18, 2008 · N314SW · Boeing 7373H4SDR SWAA083355Bulkhead · crackedDURING SCHEDULED SPV CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 15L. REPAIRED WEB PER SRM.Jun 18, 2008 · N314SW · Boeing 7373H4SDR COMA0860293Bulkhead · crackedCRACK ON REAR PRESSURE BULKHEAD AT LBL 36.20 WL 80. REPAIRED REAR PRESSURE BULKHEAD IAW REO 601R-53-61-1285. (S)Jun 17, 2008 · N960CA · Cndair CL6002B19SDR A6WA200840518Bulkhead · puncturedCOCKPIT BULKHEAD FS 280 PUNCTURED AT LBL 34 AND WL 124. COCKPIT BULKHEAD FS 280 AT LBL 34 AND WL 124 REPAIRED IAW REO 601R-53-11-1414. (A)Jun 17, 2008 · N444ZW · Cndair CL6002B19SDR SWIA200820233Bulkhead · crackedONE AFT PRESSURE BULKHEAD ISOLATOR CRACKED. C-CHECK, REPLACED ISOLATOR.Jun 16, 2008 · N492SW · Cndair CL6002B19SDR COMA0860288Bulkhead · crackedREAR PRESSURE BULKHEAD CRACKED AT THE TOP OF LINTEL FITTING. REPAIRED REAR PRESSURE BULKHEAD AROUND LINTEL FITTING IAW REO 601R-53-61-1230. (S)Jun 15, 2008 · N960CA · Cndair CL6002B19SDR USAA920081243Bulkhead · crackedPIT - FPBH - MAJOR REPAIR - E1A53032 - TWO EACH CRACKS AT WEB OF VERTICAL BEAM BS 178, RBL 17 JUST BELOW WL 234. REPAIRED WEB OF VERTICAL BEAM BS 178, RBL 17 JUST BELOW WL 234. (K)Jun 13, 2008 · N531AU · Boeing 7373B7SDR USAA920081218Bulkhead · crackedPIT - FORWARD PRESSURE BULKHEAD - MAJOR REPAIR - EA 53032 - FORWARD PRESSURE BULKHEAD SKIN HAS 2 CRACKS AT BS 178, WL 234, LBL 17. REPAIRED FORWARD PRESSURE BULKHEAD SKIN CRACKS AT BS 178, WL 234, LBL 17 IAW SRM 53-10-08. (K)Jun 13, 2008 · N531AU · Boeing 7373B7SDR QXEA200800669Bulkhead · corrodedRFD C4 CHECK FS 280 SHOWS SIGNS OF CORROSION. BLENDED CORROSION FROM LT FS 280 BULKHEAD. .002 MATERIAL REMOVED, IAW CRJ 700 SRM 53-11-10. BLENDED CORROSION FROM RT FS 280 BULKHEAD, .003 MATERIAL REMOVED. IAW CRJ 700 SRM 53-11-10. TREATED IAW CRJ 700 SRM 5Jun 12, 2008 · N614QX · Cndair CL6002C10SDR IXX2008F00083Bulkhead · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MIDDLE ACCESSORY COMPARTMENT BULKHEAD CRACKED AT STATION 680.000 LT BOTTOM LINE 20-30. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING DOUBLER AND SPLICE. REMOVED DAMAGED AREA. FABRICATED DOUBLER, DOJun 12, 2008 · N721CX · Doug DC872FSDR SWAA083219Stiffener · crackedDURING SCHEDULED 12Y CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 178, RBL 17. REPAIRED STIFFENER PER SRM.Jun 12, 2008 · N634SW · Boeing 7373H4
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