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 USAA040743Pressure Blkhd · crackedPIT, FPBH, WEB, .1250 INCH CRACK AT RIVET. FWD PRESSURE BULKHEAD, WEB WL 234/RBL 12. WEB REPAIR, FILLER AND DOUBLER IAW SRM 53-10-08, FIG 209 AND EO 5300V153.Oct 11, 2004 · N445US · Boeing 7374B7SDR USAA040747Bulkhead · crackedPIT, C1; WEB SKIN, .2500 INCH CRACK, FWD BULKHEAD, STA 178, WEB STA 212. INSTALLED DOUBLER REPAIR IAW EO 5300V153.Oct 10, 2004 · N504AU · Boeing 7373B7SDR DLM88081759Pressure Panel · damagedFUSELAGE - MLG WHEEL WELL - SLANT PRESSURE PANEL REPAIR IAW 09-085387-12. C/W 09-085387-12 ME01.Oct 9, 2004 · N976DL · Doug MD88SDR CALA0400669Stiffener · corrodedSTIFFENER ON LWR RT SIDE OF APB IS CORRODED AT RBL 1. INSTALLED NEW STIFFENER PER BOEING DRAWING 65C28106.Oct 8, 2004 · N16310 · Boeing 7373T0SDR CALA0400668Stiffener · corrodedLOWER LT SIDE OF APB STIFFENER CORRODED. INSTALLED NEW STIFFENER PER BOEING DRAWING 65C28106.Oct 8, 2004 · N16310 · Boeing 7373T0SDR USAA040748Bulkhead · crackedPIT, C1; SKIN WITH .5 INCH LONG CRACK AT AFT PRESSURE BULKHEAD AT BL0 AND 10 INCHES ABOVE CENTER. INSTALLED DOUBLER IAW SRM 53-80-08.Oct 7, 2004 · N385US · Boeing 7373B7SDR IXXA060074SBulkhead · crackedDURING ROUTINE C CHECK, FOUND WEB CRACKED AT STATION -175 FORWARD BULKHEAD LOWER SECTION. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED WEB. FABRICATED WEB, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW WEB AND FASTENERS AT STATION -175 FORWARD BOct 5, 2004 · N825BX · Doug DC871FSDR SWAA042884Pressure Panel · crackedDURING SCHEDULED RON, FOUND RT NLG WHEEL WELL WEB AT BS 259, WL 174, CRACKED. REPAIRED WEB PER EA.Oct 5, 2004 · N311SW · Boeing 7373H4SDR ASOA04820Pressure Panel · corrodedDURING A C-CHECK, THE PRESSURE WEB BETWEEN FR39 AND FR40 ON THE RT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PRESSURE WEB BETWEEN FR39 AND FR40 ON THE RT SIDE IAW SRM 51-25-01.Oct 4, 2004 · N632AS · Aerosp ATR72212SDR UPS04243411Bulkhead · crackedINSPECTION TYPE:C, BS 178 BULKHEAD: EVIDENCE OF CRACK ON FWD FACE AT RBL 10 WL 235.1 EMANATING FROM FASTENER HOLE. HFEC CARRIED OUT IAW NDTM 51-00-00 FIG 4. CRACK CONFIRMED AND ENDS MARKED. CUT OUT DAMAGED AREA IAW SRM 53-10-9. HFEC CARRIED OUT, NO DEFECTSOct 4, 2004 · N954UP · Boeing 727185CSDR UPS04243395Pressure Panel · crackedINSPECTION TYPE: C, CRACK FOUND ON NWW LEFT SIDEWALL JUST BELOW LEFT AFT SIDE PRESSURE PANEL. HFEC CARRIED OUT IAW B727 NDTM 51-00-00 PT 6 FIG 4, CRACK CONFIRMED, ENDS MARKED. STOP DRILLED CRACKS IAW SRM 51-10-01. HFEC CARRIED OUT AROUND STOP DRILLED AREAS Oct 4, 2004 · N954UP · Boeing 727185CSDR ASAA0410423Pressure Blkhd · crackedPAE - LFEC OF AFT PRESSURE BULKHEAD FOUND CRACK INDICATION AT STR 7 LT OB RIVET. REPAIRED AFT PRESSURE BULKHEAD IAW SRM.Oct 3, 2004 · N742AS · Boeing 737290CSDR LR7A04137Pressure Panel · crackedDURING SCHEDULED C6 INSPECTION PER JOB CARD HC5323 FOUND RH FS 597 - 617 PRESSURE PANEL CRACKED AT, WL 260, RBL 61. REPAIRED IAW LAC MEA 382-53-04-071.Oct 1, 2004 · N401LC · Lkheed 382GSDR LR7A04120Panel · corrodedDURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5323 FOUND LMLG BAY FS 550 PANEL RISERS CORRODED AT WL 190 AND WL 195, LBL 62. REPAIRED IAW EA 382-53-04-079. NR 0480.Oct 1, 2004 · N401LC · Lkheed 382GSDR LR7A04119Panel · corrodedDURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5323 FOUND LMLG BAY FS 540 PANEL RISERS CORRODED AT WL 189, LBL 62. REPAIRED IAW EA 382-53-04-072. NR 0480.Oct 1, 2004 · N401LC · Lkheed 382GSDR LR7A04117Pressure Panel · crackedDURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5316 FOUND FS 477 RT UPPER PRESSURE PANEL AFT SIDE WEB RADIUS CRACKED AT WL 272, RBL 29-35. REPAIRED AND REINFORCED IAW SB 382 53-50 R1 AND DWG SK382-53-167. NR 0416.Oct 1, 2004 · N401LC · Lkheed 382GSDR LR7A04116Bulkhead · crackedDURING SCHEDULED C6 INSPECTION IAW JOB CARD HC3215 FOUND NLG BAY FS 93 BULKHEAD CRACKED ADJACENT TO FWD NLG DOOR LT HINGE FITTING AT WL 156, LBL 16.REPAIRED IAW SRM SMP 583 53-30-10 AND 53-30-1. NR 0415.Oct 1, 2004 · N401LC · Lkheed 382GSDR LR7A04112Pressure Panel · crackedDURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5323, FOUND LT FS 597-617 PRESSURE PANEL CRACKED AT, WL 260, LBL 61. REPAIRED IAW EA 382-53-04-070. NR 0307.Oct 1, 2004 · N401LC · Lkheed 382GSDR LR7A04106Cap · corrodedDURING SCHEDULED C6 INSPECTION PER JOB CARD HC5323 FOUND LT MLG FS 577 BEAM OUTER CAP CRACKED AT WL 228, LBL 67. REPACED CAP IAW DWG 388482 AND SRM SMP 583 51-70.Oct 1, 2004 · N401LC · Lkheed 382GSDR LR7A04104Cap · corrodedDURING SCHEDULED C6 INSPECTION PER JOB CARD HC5324 FOUND RT MLG BAY FS 588 - FS 597, WL187 SHELF OUTER TEE CORRODED AT RBL 67. REPLACE TEE CAP IAW DWG 391491 AND SRM SMP 583 51-70.Oct 1, 2004 · N401LC · Lkheed 382GSDR LR7A04101Panel · crackedDURING SCHEDULED C6 INSPECTION PER JOB CARD HC5324 FOUND RT MLG BAY FS 477 BULKHEAD PANEL CRACKED NEAR EXISTING REPAIR AT RBL 81, WL 180. REPLACED PANEL IAW 3707784 AND SRM SMP 51-70.Oct 1, 2004 · N401LC · Lkheed 382GSDR LR7A04098Beam · crackedDURING SCHEDULED C6 INSPECTION PER JOB CARD FOUND RT MLG FS 557 UPPER BOW BEAM CRACKED AT WL 200, RBL 62. REPAIRED IAW SRM SMP 583 53-40-14.Oct 1, 2004 · N401LC · Lkheed 382GSDR LR7A04095Beam · crackedDURING SCHEDULED C6 INSPECTION PER JOB CARD HC5324 FOUND RT MLG BAY FS 557 BOW BEAM CAP CRACKED AT WL 152, RBL 63. REPAIRED IAW SRM SMP 583 53-40-12.Oct 1, 2004 · N401LC · Lkheed 382GSDR LR7A04094Tee Fitting · corrodedDURING SCHEDULED C6 INSPECTION PER JOB CARD HC5324 FOUND RT MLG BAY FS 557 TO FS 577, WL 175 OUTER SHELF TEE CORRODED AT RBL 67. REPLACED TEE IAW DWG 372478 AND SRM SMP 583 51-70.Oct 1, 2004 · N401LC · Lkheed 382GSDR CQN2004F00000Bulkhead · crackedCRACKS WERE LOCATED AT LT AND RT RELIEF CUTS OF STATION 124.00 UPPER FUSELAGE BULKHEAD. PROBABLE CAUSE FOR LT SIDE IS AUX POWER RECEPTACLE AND RT SIDE COULD BE FROM LANDING STRESSES.Sep 30, 2004 · N9654B · Cessna 172RGSDR SWAA042831Bulkhead · crackedDURING SCHEDULED D CHECK, FOUND BULKHEAD DOME CAP AT BS 1016, STRINGER 15L, CRACKED. REPAIRED SKIN PER ER.Sep 29, 2004 · N659SW · Boeing 737301SDR SWAA042804Bulkhead · crackedDURING SCHEDULED D CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP LAP SPLICE AT BS 1016, STRINGER 23R, CRACKED. REPAIRED BULKHEAD PER ER.Sep 27, 2004 · N659SW · Boeing 737301SDR UPS04443358Bulkhead · crackedINSPECTION TYPE:C, LEFT BS 1480 BULKHEAD APU DUCT CUTOUT 1EA FASTENER HOLE CRACK FOUND RUNNING DOWNWARD APPROX 0.060 INCH LENGTH BS 1480, LBL 100. LEFT BS 1480 BULKHEAD APU DUCT CUTOUT WEB REPAIRED AS PER EO B747-5310-3100-C FIG 4.Sep 25, 2004 · N681UP · Boeing 747121SDR UPS04443369Bulkhead · crackedINSPECTION TYPE: C, LEFT MLG WW AFT BULKHEAD APU BLEED AIR DUCT CUTOUT I/B UPPER AREA CRACKED AT STA 1480, LBL 100. LEFT BLG W/W AFT BULKHEAD APU BLEED AIR DUCT CUTOUT WEB REPAIRED AS PER EO B747-5310-3100-C FIG 4.Sep 24, 2004 · N681UP · Boeing 747121SDR AWXA200401100Fitting · crackedDURING BC-4 CHECK, A 2 INCH CRACK WAS FOUND ON SUPPORT FITTING AT AFT FACE OF PRESSURE BULKHEAD STR 32 LT, FS 35. MAINTENANCE REMOVED CRACKED SUPPORT FITTING AT AFT FACE OF PRESSURE BULKHEAD STR 32 LEFT, FS 35; FABRICATED A NEW REPLACEMENT FITTING PER DWG D53Sep 24, 2004 · N658AW · Airbus A320232SDR QXEA200400691Bulkhead · corrodedUPPER SURFACE OF CABIN FLOOR SUPPORT CHANNEL IMMEDIATELY AFT OF COCKPIT BULKHEAD AT FS 280.00 IS CORRODED FROM LBL 22.0 TO RBL 22.00. REPAIRED IAW EA R-53-203.Sep 22, 2004 · N600QX · Cndair CL6002C10SDR UPS04443353Bulkhead · corrodedINSPECTION TYPE-C, RT WLG W/W FWD BULKHEAD IB MID AREA CORROSION REVEALED AT STA 1241 RBL 2-6. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.082 INCH X 1 INCH X 5 INCH EXCEED SRM 57-10-01 FIG 1 LIMITS. BULKHEAD REPAIRED REFER SRM 57-10-06 FIG 3, Sep 21, 2004 · N681UP · Boeing 747121SDR UPS04243258Pressure Panel · crackedINSPECTION TYPE: C, LT NOSE WHEEL WELL HAS CRACKS ON FASTENER ROW, BS 243, 4 INCHES BELOW FWD PRESSURE PANEL OPENING. HFEC CARRIED OUT IAW NDT MM 51-00-00. RESULT - CRACKS CONFIRMED. FILLER AND DOUBLER FABRICATED AND INSTALLED IAW SRM 51-40-02.Sep 21, 2004 · N944UP · Boeing 72722CSDR SWAA042745Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BULKHEAD DOME CAP AT BS 1016, STRINGER 9L, CRACKED. REPAIRED BULKHEAD DOME CAP PER SRM.Sep 21, 2004 · N659SW · Boeing 737301SDR SWAA042740Fitting · crackedDURING SCHEDULED D-CHECK, FOUND SPAR FITTING AT BS 1016, LBL 1, WL 247, CRACKED. REPAIRED FITTING PER ER.Sep 21, 2004 · N675AA · Boeing 7373A4SDR SWAA042730Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND 3 EACH CRACKS ON THE BULKHEAD WEB AT BS 178, LBL 11, LBL 12 AND RBL 8.5, WL 234. REPAIRED BULKHEAD WEB PER SRM.Sep 20, 2004 · N359SW · Boeing 7373H4SDR SWAA042729Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND 3 EACH CRACKS ON THE AFT PRESSURE BULKHEAD WEB AT BS 1016, 1 O'CLOCK, 2 O'CLOCK AND 5 O'CLOCK POSITIONS. REPAIRED BULKHEAD WEB PER EA.Sep 20, 2004 · N683SW · Boeing 7373G7SDR UIEA200400157Bulkhead · corrodedDURING SCHEDULED MAINTENANCE, FS 1350 BULKHEAD WED FOUND CORRODED NEAR STRINGER 1L LEVEL OF CORROSION, LEVEL 1, MINOR. TRIMED OUT CORRODED AREA. REMOVED NICKS, SCRATCHES, GOUGES, BURRS AND SHARP EDGES FROM THE REPAIR PART. PERFORMED HFEC INSPECTION TO ENSURESep 17, 2004 · N528MC · Boeing 7472D7BSDR COMA0460603Bulkhead · corrodedFS 280 HAS CORROSION ON WEB AT CBP WALLS. REPAIRED IAW REO 601R-53-11-584.Sep 16, 2004 · N965CA · Cndair CL6002B19SDR SWAA042703Stiffener · crackedDURING SCHEDULED 1/4D CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER AT BS 1016, 3 O'CLOCK POSITION, CRACKED. REPAIRED STIFFENER PER SRM.Sep 16, 2004 · N683SW · Boeing 7373G7SDR COMA0460518Bulkhead · corrodedFS 280 HAS CORROSION ON WEB AT BL AFT SIDE AND CRACKS LOCATED OUTBOARD OF LBL/RBL 9. REPAIRED IAW REO 601R-53-11-136.Sep 16, 2004 · N965CA · Cndair CL6002B19SDR P5CA0401214Bulkhead · corrodedBULKHEAD EXIT SIDE UNDER RADOME LT SIDE 3RD BEAM DOWN FROM TOP HAS CORROSION. REMOVED CORROSION, TREATED & PRIMED.Sep 14, 2004 · N858FT · Boeing 747123SDR P5CA0401198Bulkhead · corrodedAFT BULKHEAD UNDER FLOOR & WEB CORRODED. REMOVED STIFFENER & WEB FROM FLOORBEAM, INSTALLED NEW ONE.Sep 14, 2004 · N858FT · Boeing 747123SDR UPS04243251Panel · crackedINSPECTION TYPE:C, HULL PRESSURE LEAK IN NLG WHEEL WELL CEILING PANEL (DUE TO CRACKING) AT BS 260 LBL 20. DAMAGED AREA REMOVED AS REQUIRED IAW SRM 51-40-2. HFEC CARRIED OUT - NO DEFECTS FOUND. REPAIR PARTS FABRICATED IAW SRM 51-40-2. REPAIR PARTS INSTALLEDSep 13, 2004 · N944UP · Boeing 72722CSDR SWAA042644Stiffener · crackedDURING SCHEDULED D CHECK, FOUND VERTICAL STIFFENER AT BS 663, RBL 6, CRACKED. REMOVED AND REPLACED VERTICAL STIFFENER PER SRM.Sep 12, 2004 · N675AA · Boeing 7373A4SDR GAIA04098Pressure Panel · damagedDURING C-CHECK INSPECTION FOUND NOSE WHEEL WELL UPPER WEB AT STA 294.5, PREVIOUS REPAIRS OVERLAPPING AND NO SPACING BETWEEN REPAIRS. REF FASI NR 86354, REMOVED EXISTING REPAIRS AND INSTALLED DOUBLER REPAIR IAW SB 727-53-145 REV 1 AND SRM 51-40-2, FIG 1.Sep 10, 2004 · N180AX · Boeing 727222SDR GAIA04097Pressure Panel · damagedDURING C-CHECK INSPECTION FOUND NOSE WHEEL WELL LT WEB AT STA 268.25, PREVIOUS REPAIRS OVERLAPPING AND NO SPACING BETWEEN REPAIRS. REF FASI NR 86352, REMOVED EXISTING REPAIRS AND INSTALLED DOUBLER REPAIR IAW SB 727-53-145 REV 1 AND SRM 51-40-2, FIG 1.Sep 10, 2004 · N180AX · Boeing 727222SDR GAIA04096Pressure Panel · crackedDURING C-CHECK INSPECTION FOUND NOSE WW RT SIDE WEB STA 268.25 HAS MANY REPAIRS OVERLAPPED. REF FASI NR 86351, INSTALL DOUBLER REPAIR IAW SRM 51-40-2 AND S/E 727 53-0145, REV 1.Sep 10, 2004 · N180AX · Boeing 727222SDR GAIA04157Pressure Panel · crackedDURING C-CHECK INSPECTION FOUND ELECT. COMPARTMENT BS 288, LBL24, PRESSURE WEB FOR NOSE WW CRACKED. REF FASI NR 86933, INSTALLED DOUBLER REPAIR IAW SRM 53-10-2, FIG 1.Sep 10, 2004 · N180AX · Boeing 727222SDR SWAA042627Pressure Panel · crackedDURING SCHEDULED 1/4D CHECK, FOUND BEADED PRESSURE WEB AT BS 663, LBL 33, CRACKED. REPAIRED WEB PER SRM.Sep 10, 2004 · N645SW · Boeing 7373H4
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