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 SWAA022124Bulkhead · crackedDURING SCHEDULED C3 CHECK, FOUND BS 1016 PRESS BULKHEAD CRACKED (2 EA) AT APPROX 3 O'CLOCK POSITION. REPAIRED BULKHEAD PER SWA EA.Sep 10, 2002 · Boeing 7372H4SDR UPS02439520Splice · crackedINSPECTION TYPE:C RT BS 1480 BULKHEAD AREA HOLE 23 CRACK FOUND AT WEB SPLICE PLATE APPROX .125 INCH RUNNING I/B AND O/B STR R33 TO R34. RT BS 1480 BULKHEAD WEB SPLICE PLATE REPLACED AS PER SRM 51-30-04 DUE CRACKED HOLE REWORKED AND OUT OF SB 747-53A2390 'D' MSep 7, 2002 · N683UP · Boeing 747121SDR UPS02439519Splice · crackedRT BS 1480 BULKHEAD AREA HOLE NR 23 CRACK FOUND AT OUTER CHORD SPLICE FITTING APPROX .125 INCH RUNNING INBOARD AND OUTBOARD STR R33 TO R34, RT BS 1480 BULKHEAD OUTER CHORD SPLICE FITTING HOLE NR 23 REWORKED AND CRACK FREE, OUT OF SB 'D' MAX LIMIT. NEW OUTER CSep 7, 2002 · N683UP · Boeing 747121SDR CA020918006Bulkhead · cracked(CAN) THE ROTOR CONTROL BELLCRANK BULKEAD CRACKED IN MULTIPLE PLACES.Sep 6, 2002 · Bell 204BSDR UPS02439523Pressure Panel · corrodedINSPECTION TYPE:C RT WLG W/W KEEL BEAM TOP PANEL CORROSION REVEALED AT STA 1275-1350 RBL 0-10. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT EXCEEDED SRM 53-10-01 FIG 1 LIMITS. WEB REPAIRED AT STA 1345 RBL 8.Sep 6, 2002 · N683UP · Boeing 747121SDR UPS02839384Pressure Panel · crackedINSPECTION TYPE:N/A LEFT WHEEL WELL AFT FLAP ENCLOSURE, WEB ASSY ON AFT PORTION WHERE ACT RETRACTS IS CRACKED IN UPPER RADIUS. LOCATED & DRILLED NEW WEB FABRICATED NEW STIFFENER FOR SPOILER A PULLEY BRACKET ON I/B WEB PANEL, FABRICATED PER DC-8 SRM 51 W 18126Sep 6, 2002 · N894UP · Doug DC873FSDR 2002UALA01411Bulkhead · crackedSTATION 178 BULKHEAD WEB CRACKED AT RIGHT HAND LOWER RADAR MOUNT OUTBOARD UPPER SIDE RBL 7 INCHES WL 200. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER REPAIR.Sep 5, 2002 · N343UA · Boeing 737322SDR 2002UALA01409Bulkhead · crackedSTATION 178 BULKHEAD WEB CRACKED AT WL 187 RBL 1 INCH. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER REPAIR.Sep 5, 2002 · N343UA · Boeing 737322SDR SWAA022053Bulkhead · crackedDURING SCHEDULED D CHECK, FOUND PRESSURE BULKHEAD CRACKED (2 EA) AT BS 1016, STR 6R AND STR 6L. REPAIRED BULKHEAD PER SRM.Sep 5, 2002 · N686SW · Boeing 737317SDR USAA020350Pressure Panel · crackedPIT - FOUND WEB CRACKED 1 INCH, STATION 672 RBL 42 W/W PRESS PANEL. DOUBLERS, STIFFENER, HEAT TREATED PER SRM 53-60-51 AND EA 74665. (M)Sep 3, 2002 · N335US · Boeing 737301SDR UPS02239399Pressure Panel · crackedINSPECTION TYPE:C SUSPECT CRACK AT BS 246, NLG WHEEL WELL RT PRESSURE WEB 6 INCHES ABOVE SILL CHORD. HFEC IAW NDT MAN 51-00-00 PT 6 FIG 4 CRACK CONFIRMED, DAMAGE CUTOUT IAW SRM 51-10-01, HFEC IAW NDT MAN 51-00-00 PT 6 FIG 4 NDF. REPAIR CARRIED OUT IAW SRM 51Sep 3, 2002 · N941UP · Boeing 72722CSDR UPS02239397Pressure Panel · crackedINSPECTION TYPE:C SUSPECT CRACK IN NOSE WHEEL WELL RT PRESSURE WEB BS 258. HFEC CONFIRMS CRACKS IAW 727 NDT MAN PT6 51-00-00 FIG 4. DAMAGE AREA REMOVED IAW SRM 51-10-01. HFEC CARRIED OUT AND CONFIRMS DAMAGE REMOVAL. REPAIR CARRIED OUT IAW SRM 51-40-02 FIGUSep 3, 2002 · N941UP · Boeing 72722CSDR UPS02239393Pressure Panel · crackedINSPECTION TYPE:C NLG RT PRESSURE WEB HAS SUSPECT CRACK AT BS 286 4 INCHES FROM SILL. HFEC CARRIED OUT IAW NDT MAN PT6 51-00-00 FIG 4 CRACK CONFIRMED AND ENDS MARKED. DAMAGE REMOVED IAW SRM 51-10-01. HFEC INSPECT CUTOUT TO CONFRM DAMAGE REMOVAL. REPAIRED IASep 3, 2002 · N941UP · Boeing 72722CSDR UPS02239250Pressure Panel · crackedINSPECTION TYPE:SEG4 RIGHT WHEEL WELL FWD BULKHEAD, JUST BELOW APU LOAD CONTROL VLV, HAS A 3.5 INCH CRACK TO 4 INCH CRACK CRACKED THROUGH. STOP DRILLED CRACK AS PER B72 7 SRM 51-10-01, ACCOMPLISHED HFEC 51-000-00 FIG 4 NDT INSP CRACK CONTAINMENT CONFIRMED. ISep 2, 2002 · N913UP · Boeing 72762CSDR UPS02239392Pressure Panel · crackedINSPECTION TYPE:C CRACK INDICATION FOUND IN RIGHT WALL OF NOSE WHEEL WELL LOCATED AT B S 264.5 APPROX 7 INCHES FROM CEILING CRACK IS APPROX 2 INCHES LONG. HFEC INSPECT IAW NDT MAN PT6 51-00-00 FIG 4, CRACK CONFIRMED AND ENDS MARKED. DAMAGE REMOVED IAW SRM 51Sep 2, 2002 · N941UP · Boeing 72722CSDR SWIA200211332Bulkhead · crackedFOUND FS 280.0 RBL 9.0 PILOT BULKHEAD LOWER FLANGE CRACKED DURING C-CHECK INSPECTION. HFEC INSPECTION COMPLIED WITH ON CUTOUT REPAIR AS REQUIRED IAW RJ NDTM 51-20-01. NO CRACKS FOUND. PILOT BULKHEAD REPAIRED IAW CRJ REO 601R-53-11-171.Aug 31, 2002 · N413SW · Cndair CL6002B19SDR UPS02239400Pressure Panel · crackedINSPECTION TYPE:C NOSE WHEEL WELL RT SIDE WALL WEB HAS SUSPECT CRACK 3 INCHES ABOVE SILL AT BS 243 APPROX. HFEC CARRIED AND CONFIRMS CRACKS. DAMAGE REMOVED IAW SRM 51-10-01, HFEC C/W ON CUTOUT NDF. REPAIRED IAW SRM 51-40-02 FIGURE 1.Aug 30, 2002 · N941UP · Boeing 72722CSDR GTIA020962Bulkhead · crackedFTW - FOUND RIGHT HPV COMPARTMENT AFT BULKHEAD WEB CRACKED RBL 20 INCHES NEAR DOOR OPENING. FABRICATED DOUBLER REPAIR. INSTALLED THE DOUBLER REPAIR. (M)Aug 29, 2002 · N817NK · Doug DC982SDR SWAA022019Bulkhead · crackedDURING SCHEDULED C1 CHECK, FOUND BS 1016 PRESS BULKHEAD CRACKED AT Y-CHORD AREA, STR 6L. REPAIRED BULKHEAD PER SRM.Aug 29, 2002 · Boeing 7372H4SDR UPS02239288Pressure Panel · crackedINSPECTION TYPE:C SUSPECT CRACK INDICATION FOUND IN NOSE WHEEL WELL SIDEWALL AT BS 276 RT SIDE 3 INCH INDICATION IS LOCATED 24 INCHES FROM NWW CEILING. DAMAGE REMOVED IAW SRM 51-10-1 REPAIRED AREA IAW SRM 51-40-02 FIG 1.Aug 27, 2002 · N941UP · Boeing 72722CSDR 2002UALA01358Pressure Panel · corrodedCABIN PRESSURE DECK BODY STATION 1680-1681 HAS 30 PERCENT MATERIAL LOSS RBL 52.5. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED.Aug 26, 2002 · N546UA · Boeing 757222SDR SWAA021952Pressure Panel · crackedDURING SCHEDULED 1/4D CHECK, FOUND BEADED WEB CRACKED AT BS 663, LBL 33 AND LBL 39. REPAIRED BEADED WEB PER SWA EA.Aug 26, 2002 · N507SW · Boeing 7375H4SDR 2002UALA01339Pressure Panel · crackedMAIN LANDING GEAR WHEEL WELL CEILING CRACKED OUTBOARD AND FORWARD OF AILERON TOWER SHAFT. CRACKS AT BOTH FORWARD CORNERS OF CEILING PANEL PILLOW AND BETWEEN FASTENERS TO CHORD FORWARD OF PILLOW. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBLER.Aug 25, 2002 · N340UA · Boeing 737322SDR SWAA021967Web · crackedDURING SCHEDULED D CHECK, FOUND CREASE BEAM WEB CRACKED BETWEEN BS 616 AND BS 639, STR 17L. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.Aug 25, 2002 · N686SW · Boeing 737317SDR AMTA200201083Bulkhead · corrodedFWD FUSELAGE SECTION, STA 328 PRESSURE BULKHEAD RBL 24 IN FESC 8 INCHES ABOVE SKIN FLOOR HAS EXFOLATION CORROSION ON BULKHEAD AND PROTUDING ALONG AND UNDER STRAP. REPAIRED DAMAGE AREA PER ERA L10-53R-4922 REV IR.Aug 21, 2002 · N195AT · Lkheed 1011SDR SWAA021899Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD CRACKED AT BS 178, WL 188 AND RBL 1.0. REPAIRED BULKHEAD PER SRM.Aug 20, 2002 · N370SW · Boeing 7373H4SDR SWAA021923Bulkhead · crackedDURING SCHEDULED C4 CHECK, FOUND 1016 BULKHEAD CRACKED (3 EA) BETWEEN STR 6L AND STR 7L. REPAIRED BULKHEAD PER SRM.Aug 19, 2002 · Boeing 7372H4SDR UPS02439316Pressure Panel · corrodedINSPECTION TYPE:C RT LG W/W STA 1241 CANTED PRESSURE DECK BULKHEAD 2EA TENSION BOLT HOLES FOUND CORROSION AS RBL 75. RT LG W/W STA 1241 CANTED PRESSURE DECK 2EA TENSION BOLT HOLES OVERSIZED PER SRM 51-30-05. NDT CONFIRMED NO CRACK AND NO CORROSION.Aug 18, 2002 · N672UP · Boeing 747123SDR 2002UALA01322Bulkhead · dentedPRESSURE BULKHEAD ABOVE PANEL 193BL HAS TWO LARGE DENTS. MAJOR REPAIR ACCOMPLISHED. NEW PANEL INSTALLED.Aug 17, 2002 · N119UA · Boeing 747422SDR UPS02439367Pressure Panel · corrodedINSPECTION TYPE:C RH LG W/W BS 1241 CANTED BULKHEAD FOUND CORROSION AT RBL 75-77 WL 166-167. BULKHEAD FOUND CORRODED AT LOCATION BS 1241 TO 1241 WL 166 TO 167, RBL R75 TO R77. CORROSION BLEND OUT EXCEEDS SRM LIMIT. BULKHEAD REPLACED AS PER SRM 51-10-01 HX RAug 16, 2002 · N672UP · Boeing 747123SDR UPS02439348Splice · crackedINSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 18 FOUND CRACK AT WEB SPLICE PLATE, APPROX 0.030 RUNNING O/B. LT BS 1480 BULKHEAD WEB SPLICE PLATE NR 18 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11.Aug 16, 2002 · N672UP · Boeing 747123SDR UPS02439346Splice · crackedINSPECTION TYPE:C RT BS 1480 BULKHEAD NR 24 HOLE FOUND CRACK AT OUTER CHORD SPLICE FITTING RUNNING I/B AFT APPROX 0.09. RT BS 1480 BULKHEAD OUTER CHORD SPLICE FITTING NR 24 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11.Aug 16, 2002 · N672UP · Boeing 747123SDR UPS02439344Splice · crackedINSPECTION TYPE:C RT BS 1480 BULKHEAD NR 23 HOLE FOUND CRACKED AT WEB SPLICE PLATE RUNNING I/B APPROX 0.06. THE WEB SPLICE PLATE REPLACED DUE TO HOLE OVERSIZED AND EXCEEDED LIMIT AS PER SB 747-53A2390 FIG 11.Aug 16, 2002 · N672UP · Boeing 747123SDR UPS02439343Splice · crackedINSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 17 FOUND CRACK AT WEB SPLICE PLATE, APPROX 0.020 INCH RUNNING O/B. LT BS 1480 BULKHEAD WEB SPLICE PLATE NR 17 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11.Aug 16, 2002 · N672UP · Boeing 747123SDR UPS02439342Splice · crackedINSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 16 FOUND CRACK AT OUTER CHORD SPLICE FITTING APPROX 0.02 INCH RUNNING I/B. LT BS 1480 BULKHEAD OUTER CHORD FITTING NR 16 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11.Aug 16, 2002 · N672UP · Boeing 747123SDR UPS02439338Splice · crackedINSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 1 FOUND CRACK AT OUTER CHORD SPLICE FITTING, APPROX 0.04 INCH RUNNING FWD. LT BS 1480 BULKHEAD OUTER CHORD SPLICE FITTING NR 1 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIGAug 16, 2002 · N672UP · Boeing 747123SDR UPS02439337Bulkhead · crackedINSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 15 FOUND CRACK AT BULKHEAD WEB APPROX 0.03 INCH RUNNING O/B. LT BS 1480 BULKHEAD WEB NR 15 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11.Aug 16, 2002 · N672UP · Boeing 747123SDR UPS02439336Splice · crackedINSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 16 FOUND CRACK AT WEB SPLICE PLATE, APPROX .125 INCH, RUNNING O/B. LT BS 1480 BULKHEAD WEB SPLICE PLATE NR 16 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-3A2390 FIG 11.Aug 16, 2002 · N672UP · Boeing 747123SDR UPS02439335Splice · crackedINSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 15 FOUND CRACK AT OUTER CHORD SPLICE FITTING, APPROX 0.030 INCH. LT BS 1480 BULKHEAD OUTER CHORD SPLICE FITTING NR 15 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 74753A2390 FIG 11.Aug 16, 2002 · N672UP · Boeing 747123SDR UPS02439334Bulkhead · crackedINSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 1 FOUND CRACK AT BULKHEAD CHORD, APPROX 0.06 INCH RUNNING FWD. LT BS 1480 BULKHEAD CHORD NR 1 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG 11.Aug 16, 2002 · N672UP · Boeing 747123SDR UPS02439333Splice · crackedINSPECTION TYPE:C LT BS 1480 BULKHEAD AREA HOLE NR 15 FOUND CRACK AT WEB SPLICE PLATE , APPROX 0.02 INCH RUNNING O/B. LT 1480 BULKHEAD WEB SPLICE PLATE NR 15 HOLE OVERSIZED AND CRACK FREE REPAIR BUSHING INSTALLED AS PER SB 747-53A2390 FIG11.Aug 16, 2002 · N672UP · Boeing 747123SDR UPS02439268Pressure Panel · crackedINSPECTION TYPE:C RT LG W/W O/B PRESSURE DECK LWR FACE AT BS 1416 LATERAL O/B NR 2 RIVET HOLE AREA CRACKED TO EDGE. SECTION OF PRESSURE WEB AT RT LG W/W O/B FROM STA 1400 TO 1438 RBL 110 TO MOST O/B AREA REPLACED AS PER SRM 51-10-01 PG 8.Aug 16, 2002 · N672UP · Boeing 747123SDR UPS02439353Splice · crackedINSPECTION TYPE:C RT BS 1480 BULKHEAD NR 24 HOLE FOUND CRACK AT WEB SPLICE PLATE RUNNING I/B APPROX 0.09 AND O/B APPROX .125. THE WEB SPLICE PL ATE CHANGED AS PER SB 747-53A2390. REFER HX RS R-53-43-34884 AND UPS EO B747-5310-17499-A.Aug 15, 2002 · N672UP · Boeing 747123SDR UPS02439310Bulkhead · crackedINSPECTION TYPE:C FUSELAGE RT TUNNEL STA 260 CANTED BULKHEAD WEB RADIUS CRACKED AT WL 180 RBL 70. FUSELAGE RT TUNNEL STA 260 CANTED BULKHEAD WEB RADIUS CRACKED AREA REPAIRED AS PER SRM 53-10-04 FIG 6.Aug 15, 2002 · N672UP · Boeing 747123SDR UPS02239120Pressure Panel · crackedINSPECTION TYPE:C SUSPECT CRACK IN NLG FWD LT PRESS WEB AT BS 243.7. CRACKED AREA REMOVED IAW SRM 51-40-2 FIG 1. HFEC C/O ON THE ABOVE AREA INSP CARRIED OUT IAW B727 NDTM PT 6 51-00-00 FIG 4. RESULT CRACK REMOVED BY CUT OUT, FABRICATED DOUBLER & FILLER IAW Aug 15, 2002 · N926UP · Boeing 72731CSDR MWEA020511Stiffener · crackedRECEPTACLE UNDER RADIAL STIFFENER AT 10 O'CLOCK POSITION #6 LEFT FOUND TO BE CRACKED IN 2 PLACES. -- DRILLED UP AND INSTALLED RECEPTACLE.Aug 14, 2002 · N800ME · Doug DC914SDR MWEA020501Stiffener · crackedAFT PRESSURE BULKHEAD RADIAL STIFFENER ON AFT SIDE AT 10 O'CLOCK POSSITION HAS A SMALL CRACK AT THE RIGHT SIDE. -- FABRICATED AND INSTALLED STIFFENER.Aug 14, 2002 · N800ME · Doug DC914SDR MWEA020500Angle · crackedAFT PRESSURE BULKHEAD RIGHT HAND RADIAL #2 LOWER ANGLE THAT ATTACHES TO JAMB GUSSET HAS A CRACKED ATTACH HOLE. -- FABRICATED AND INSTALLED ANGLE.Aug 14, 2002 · N800ME · Doug DC914SDR MWEA020499Doubler · crackedAFT PRESSURE BULKHEAD PLUG DOOR STOP RECEPTACLE AT UPPER RIGHT CORNER HAS A CRACK EMANATING FROM CUTOUT HOLE TO THE DOOR JAMB EDGE DOT 30. -- FABRICATED AND INSTALLED DOUBLER, FABRICATED AND INSTALLED 8 FASTENERS.Aug 14, 2002 · N800ME · Doug DC914SDR MWEA020492Doubler · crackedAFT PRESSURE BULKHEAD PLUG DOOR STOP RECEPTACLE AT LOWER LEFT CORNER HAS A CRACK EMANATING FROM CUT OUT HOLE TO DOOR JAMB EGDE DOT 31. -- FABRICATED AND INSTALLED DOUBLER.Aug 14, 2002 · N800ME · Doug DC914
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