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 UPS06446897Stiffener · crackedINSPECTION TYPE:C NWW TOP PANEL BS 260-280 BL 0 STIFFENER FOUND CRACK AT PREVIOUS REPAIRED AREA. CRACK LENGTH .25 INCH. NWW TOP PANEL BS 260-280 BL 0 STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.May 5, 2006 · N521UP · Boeing 747200SDR UPS06446896Stiffener · crackedINSPECTION TYPE:C NWW TOP PANEL BS 280-300 LBL 10 STIFFENER RADIUS AREA FOUND CRACK APPROX .75 INCH. NWW TOP PANEL BS 280-300 LBL 10 STIFFENER REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.May 5, 2006 · N521UP · Boeing 747200SDR TRAX200600162Pressure Panel · corrodedFOUND CORROSION ON PRESSURE DECK AT FS 473 TO 559, BL36-44R. REPAIRED IAW REO 601R-53-41-420. (CLOSED)May 5, 2006 · N845AS · Cndair CL6002B19SDR TRAX200600161Pressure Panel · corrodedFOUND CORROSION ON PRESSURE DECK AT FS 473 TO 559 - BL36 TO 44LT. REPAIRED IAW REO6+01R-53-41-420. (CLOSED)May 5, 2006 · N845AS · Cndair CL6002B19SDR TRAX200600160Pressure Panel · corrodedFOUND CORROSION ON PRESSURE DECK FS409+128 TO 473 - BL36 TO44 RT. REPAIRED IAW REO 601R-53-41-420. (CLOSED)May 5, 2006 · N845AS · Cndair CL6002B19SDR TRAX200600159Pressure Panel · corrodedFOUND CORROSION ON PRESSURE DECK AT FS409+128 TO FS 473 - BL36 TO 44LT. REPAIRED IAW REO 601R-53-41-420. (CLOSED)May 5, 2006 · N845AS · Cndair CL6002B19SDR UIEA200600096Bulkhead · crackedRT SIDE BS 1000 BULKHEAD CHORD AREA, CRACK REVEAL AT BULKHEAD CHORD HEEL AREA APPROX, 2" IN LENGTH JUST BELOW STR 38R. BS 1000 BULKHEAD CHORD BETWEEN STR 36/37R TO STR 40/41R CHORD SEGMENT REPAIRED AS PER SB 747-53A2471 R1. REPEAT INSPECTION IS REQUIRED AS PMay 3, 2006 · N522MC · Boeing 7472D7BSDR UIEA200600095Bulkhead · crackedLT SIDE BS 1000, BULKHEAD CHORD AREA, CRACK REVEALED AT BULKHEAD CHORD HEEL AREA APPROX, 1-1/4" IN LENGTH, JUST BELOW STR 38L. BS 1000 BULKHEAD CHORD BETWEEN STR 36/37L TO STR 40/41L CHORD SEGMENT REPAIRED AS PER SB 747-53A2474 R1. REPEAT INSPECTION IS REQUIMay 3, 2006 · N522MC · Boeing 7472D7BSDR 06FDEA1680Pressure Panel · corrodedDURING AIRPLANE'S CONVERSION FROM P TO F/ACF FOUND: UPPER SURFACE, CENTER TANK, PRESSURE PANEL STA 1381, FROM X = -70 TO X =-105, SEVERE CORROSION. REMOVED RT SLANT PANEL, DISASSEMBLED, REMOVED CORROSION AFT. REMOVED DAMAGED GASKET, CHECKED LIMITS, RESUBMITMay 2, 2006 · N568FE · Doug DC1010SDR DLM88091554Pressure Panel · damagedMLG WHEEL WELL - SLANT PRESSURE PANEL REPAIRED IAW 09-085387-12 ME01. C/W 09-085387-12 ME01.May 1, 2006 · N985DL · Doug MD88SDR N382006F00001Angle · crackedAT 5000 LANDING INSPECTION THE FS 793 AFT BULKHEAD CAP ANGLE NDT INSPECTION WAS PERFORMED AND A CRACK WAS FOUND ON THE RT SIDE ABOUT .3750 INCH LONG. A NEW CAP ANGLE WAS INSTALLED.Apr 28, 2006 · N830EF · Gulstm GIVSDR 2006UALA00872Bulkhead · gougedFWD FACE OF AFT PRESSURE BULKHEAD AT STA 1016 IS GOUGED WITH SCRIBE MARK AROUND PERIMETER OF LT WIRE BUNDLE FEED THRU.Apr 27, 2006 · N933UA · Boeing 737522SDR UPS06146820Bracket · crackedFOUND AFT CARGO FWD BULKHEAD LT OTBD SUPPORT BRACKET CRACKED. REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-40-00.Apr 27, 2006 · N134UP · Airbus A300F4622RSDR UPS06146818Bracket · crackedFOUND AFT CARGO FWD BULKHEAD SUPPORT BRACKET CENTER CRACKED. REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-40-00.Apr 27, 2006 · N134UP · Airbus A300F4622RSDR 0600946719Bulkhead · crackedDURING L-CHECK FOUND CORROSION ON CANTED BULKHEAD WEB AT BS 1241 RBL 37.5. REPAIRED PER EA 67-206232.Apr 27, 2006 · N619US · Boeing 747251FSDR 06FDEA1617Pressure Panel · corrodedDURING AIRPLANE'S CONVERSION FROM P TO F/ACF FOUND: UPPER SURFACE, CENTER TANK, PRESSURE PANEL STA 1381, FROM X = -70 TO X =-105, SEVERE CORROSION. REMOVED RIGHT SLANT PANEL, DISASSEMBLIED, REMOVED CORROSION AFT, REMOVED DAMAGED GASKET, CHECKED LIMITS, RESApr 27, 2006 · N568FE · Doug DC1010SDR 06FDEA1548Bulkhead · crackedFOUND 4 CRACKS 0.50" LONG NLG W/W ON LT BULKHEAD UNDER HEAD RIVETS AT STA 490.250. REPAIRED NOSE GEAR SUPPORT BEAM WEB IAW SRM 53-30-00 FIG 4-6-8 VOL 1. INTEGRATE IN THIS REPAIR ALSO 3 CRACKS REPORTED ON NRC N00680/F176680.Apr 20, 2006 · N365FE · Doug DC1010SDR 06FDEA1546Bulkhead · crackedFOUND 1 CRACK NLG W/W 0.50" LONG ON RT VERTICAL BULKHEAD UNDER HEAD RIVET AT STA 579. REPAIRED NLG W/W WEB IAW SRM 53-00-01 FIG 4 SHT 2 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F176650/N00650.Apr 20, 2006 · N365FE · Doug DC1010SDR 06FDEA1545Bulkhead · damagedFOUND 1 CRACK NLG W/W 0.50" LONG ON LT VERTICAL BULKHEAD UNDER HEAD RIVET AT STA 579. REPAIRED NLG W/W WEB IAW SRM 53-00-01 FIG 4 SHT 2 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F176651/N00651.Apr 20, 2006 · N365FE · Doug DC1010SDR 06FDEA1544Bulkhead · damagedFOUND CRACK NLG W/W 0.50" LONG ON RT VERTICAL BULKHEAD UNDER HEAD RIVET AT STA 490.250. REPAIRED NOSE GEAR SUPPORT BEAM WEB IAW SRM 53-30-00 FIG 6 SHT 8 VOL 1.Apr 20, 2006 · N365FE · Doug DC1010SDR 06FDEA1540Bulkhead · crackedCLG W/W SPACE CRACK 1 INCH LONG ON RT VERTICAL BULKHEAD AT STA 1501 Z-37. PERFORMED HFEL INSP IAW NDT SPM 06-10-01 FOUND CRACK 1.3/8" LONG. TRIMMED OUT CRACKED PORTION ON WEB. REPAIRED IAW SRM 53-00-01 FIG 10 SHT 4 VOL 1. REMOVED AND INSTALLED NEW FITTING Apr 20, 2006 · N365FE · Doug DC1010SDR UPS06246871Pressure Panel · crackedINSPECTION TYPE:C CRACK ON RT NWW BS 268 AT LOWER EDGE OF AFT PRESSURE PANEL CUTOUT. HFEC INSPECTION CARRIED OUT ON ABOVE AREA IAW B727-NDTM 51-00-00 FIG 6. CRACK CONFIRMED. REMOVED INTERCOSTAL AND WEB IAW SRM 51-30-02. FABRICATED NEW WEB AND DOUBLERS IAW Apr 19, 2006 · N954UP · Boeing 727185CSDR UPS06246831Pressure Panel · crackedINSPECTION TYPE:C SUSPECT CRACK ON NWW PRESSURE WEB RT AT BS 330. HFEC CARRIED OUT IAW B727 NDTM 51-00-00 FIG 4 AND CRACK CONFIRMED. DAMAGE REMOVED IAW SRM 51-10-01. REPAIR PARTS FABRICATED IAW SRM 51-40-02. HFEC CARRIED OUT AROUND CUTOUT IAW B727-NDTM 51-Apr 19, 2006 · N954UP · Boeing 727185CSDR TRAX200600121Bulkhead · crackedFOUND 280 WEB IS CRACKED O/B OF LBL9. REPAIRED PILOTS BULKHEAD AT FS 280 LBL 9.0 IAW EO 600-53-0090.Apr 19, 2006 · N842AS · Cndair CL6002B19SDR QXEA200601557Attach Bracket · corrodedYYC - C3 FUSELAGE INTERIOR, FUSELAGE INTERIOR AT FLOOR LEVEL, BULKHEAD ATTACH BRACKET TOP PLATE HAS CORROSION AROUND SCREW HOLE AT STATION X1.00 AND LBL 11.0. REPAIRED IAW Q400 SRM 51-25-10-370-801 AND 51-25-15-370-801.Apr 18, 2006 · N425QX · Bombdr DHC8402SDR TRAX200600068Pressure Panel · corrodedCORROSION FOUND AT NUMEROUS LOCATION ON RT PRESSURE FLOOR DOUBLER. REPAIRED IAW REO 601R-53-41-415.Apr 17, 2006 · N825AS · Cndair CL6002B19SDR TRAX200600104Doubler · corrodedFOUND CORROSION ON PRESS DECK DOUBLER AT FS 448-451 - BL44-42RT (RESOLVED ON W/O: 22159 TASKCARD: N/R-00190). C/W CORROSION ON PRESSURE DECK IAW E/C REO 601R-53-41-413.Apr 17, 2006 · N842AS · Cndair CL6002B19SDR TRAX200600089Pressure Panel · corrodedFOUND CORROSIOIN ON PRESS DECK DOUBLER AT FS 439 - BL44-42RT (RESOLVED ON W/O: 22159 TASKCARD: N/R-00189). COMPLIED WITH CORROSION ON PRESSURE DECK IAW E/C REO 601R-53-41-413.Apr 17, 2006 · N842AS · Cndair CL6002B19SDR TRAX200600087Pressure Panel · corrodedFOUND CORROSION ON PRESS DECK AT FS493 - BL44RT. COMPLIED WITH CORROSION ON PRESSURE DECK IAW E/C REO 601R-53-41-413.Apr 17, 2006 · N842AS · Cndair CL6002B19SDR TRAX200600105Pressure Panel · corrodedFOUND CORROSION ON PRESS DECK AT FS455 - BL44 LT, (RESOLVED ON W/O: 22159 TASKCARD: N/R-00219). BLENDED CORRODED AREA IAW CRJ 200 SRM 51-41-45 REQUEST THICKNESS CHECK OF BLENDED AREA DK 7022603. C/W THICKNESS CHECK AT BLENDED AREA IAW CRJ 200 NDT MANUAL 51-2Apr 17, 2006 · N842AS · Cndair CL6002B19SDR USAA060590Bulkhead · canningFOUND AFT PRESSURE BULKHEAD OIL CAN STA 1016 AT 2 O'CLOCK POSITION. FABRICATED AND INSTALLED REPAIR PARTS IAW EA 97596, DEFECT SIZE: 4" BY 2.5".Apr 17, 2006 · N505AU · Boeing 7373B7SDR KCSA061147Bulkhead · gougedMAIN CABIN STA 2360 PRESSURE BULKHEAD WEB FORWARD SIDE IS GOUGED AROUND FASTENER ADJACENT TO STR 24R.Apr 17, 2006 · N716CK · Boeing 747122SDR UPS06446715Pressure Panel · crackedNOSE WHEEL WELL LT SIDE PANEL WEB FOUND CRACK AT BS 270 WL 170 APPROX 1/8". CRACKED WEB REPAIRED AS PER SRM 53-10-04 FIG 116, UPS MPI NR P18507 ISSUED TO CARRY OUT REPEAT INSPECTION INTERVAL PER SRM 53-10-04 PG 708 FIG 116.Apr 16, 2006 · N672UP · Boeing 747123SDR KCSA061144Bulkhead · corrodedMAIN CABIN STA 2360 BULKHEAD LOWER FORWARD CHORD IS CORRODED IN HOLES AT STRINGER END FITTING STR 48L.Apr 16, 2006 · N716CK · Boeing 747122SDR UPS06846789Bulkhead · crackedFOUND TWO CRACKS ON WEB AFT SIDE OF STA 1766 RT SIDE AT L16R. STOP DRILLED TWO CRACKS AT AFT PRESS BULKHD STA 1766 L16R IAW 53-2-0. FABRICATED AND INSTALLED -1 FILLER, -2 FINGER DOUBLER -3 DOUBLER IAW UPS EO FILE NR DC8-53-20547, SAA EA NR 008-5320-01-A0158 Apr 15, 2006 · N730UP · Doug DC871FSDR SWAA061308Pressure Panel · crackedDURING SCHEDULED A1 CHECK, FOUND NLG W/W CEILING PANELS CUTOUT WEB CRACKED AT BS 251.625 LBL 7.75 AND RBL 7.75. REPAIRED WEB PER SWA EA.Apr 15, 2006 · N506SW · Boeing 7375H4SDR TRAX200600056Bulkhead · crackedFOUND STA 280 BULKHEAD WEB IS CRACKED OB OF RBL 9. REPAIRED IAW EO 600-53-90. (CLOSED)Apr 14, 2006 · N825AS · Cndair CL6002B19SDR EIAA2006051Pressure Panel · crackedDURING CHECK, NOSE WHEEL WELL TOP PANEL FOUND WEB CRACKED APPROX 2 INCHES. CRACK REPAIRED PER SRM 53-10-04, FIG 119.Apr 14, 2006 · N482EV · Boeing 747212BSDR 06FDEA1434Bulkhead · corrodedREAR PRESSURE BULKHEAD INTERIOR SIDE STRG 27 TO 27 FS 80/82 HAS 6 AREAS OF CORROSION AT APPROX STRG 27R, 33-34R, 43R AND 23L AND 31R ON THE INNER RIM ANGLE. REMOVED CORROSION IAW A310-200 SRM 51-74-10. FOUND ALL AREAS OUT OF LIMITS. REPAIRED IAW EA 6-5330Apr 12, 2006 · N455FE · Airbus A310322SDR 06FDEA1432Pressure Panel · corrodedFOUND MAIN WHEEL WELL LT SIDE FS 48-54 WEB HAS 50 SQ IN OF CORROSION. REMOVED CORROSION IAW A310-200 SRM 51-74-10 FOUND 3 SPOTS OUT OF LIMITS. REPAIRED IAW EA 6-5315-98983.Apr 12, 2006 · N455FE · Airbus A310322SDR 061136Bulkhead · dentedBS 2360 BULKHEAD HAS DENTS AT LBL 7.5, WL 347.Apr 12, 2006 · N716CK · Boeing 747122SDR 061135Bulkhead · dentedBS 2360 BULKHEAD HAS DENTS AT RBL 54, WL 313.Apr 12, 2006 · N716CK · Boeing 747122SDR KCSA061130Bulkhead · dentedFOUND BS 2360 BULKHEAD HAS A DENT AT RBL 50, WL 242.5.Apr 11, 2006 · N716CK · Boeing 747122SDR QXEWA20060153Rivet · missingYYC C3 COCKPIT RIGHT HAND ENTRYWAY BULKHEAD INBOARD MISSING RIVET AND HAS LOOSE BRACKET WIRED TO RIVET HOLE AT X-39 Y128 Z141. REPAIRED IAW DHC-8 Q400 SRM 51-42-05-330-001.Apr 10, 2006 · N425QX · Bombdr DHC8402SDR 06FDEA1360Bulkhead · crackedCRACK IN BULKHEAD AT BS 870, LBL 12, WL 138. *S/D* REPAIRED CRACK IN BULKHEAD BS 870, LBL 12, WL 138 IAW SRM 53-10-9 FIG 4.Apr 10, 2006 · N192FE · Boeing 727100SDR 06FDEA1359Bulkhead · crackedCRACK IN BULKHEAD AT BS 870, RBL 12, WL 138. *S/D* REPAIRED CRACK IN BULKHEAD BS 870 RBL 12 WL 138 IAW SRM 53-10-9 FIG 4.Apr 10, 2006 · N192FE · Boeing 727100SDR SWAA061213Pressure Panel · crackedDURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BEADED PRESSURE WEB CRACKED AT BS 664, BETWEEN RBL 39 & RBL 40. REPAIRED WEB PER SRM.Apr 10, 2006 · N355SW · Boeing 7373H4SDR KCSA061114Doubler · crackedFOUND BS 1241 CANTED BULKHEAD DOUBLER CRACKED AT RBL 5.Apr 10, 2006 · N715CK · Boeing 747209BSDR COMA0660295Bulkhead · crackedCRACK FOUND ON FS 559 BULKHEAD JUST INBOARD OF RIGHT AILERON QUADRANT OUTBOARD ATTACH BOLT. REPAIRED IAW REO 601R-53-41-353.Apr 9, 2006 · N912CA · Cndair CL6002B19SDR AWXA200600710Bulkhead · crackedMCN - DURING C19 CHECK DISCOVERED BULKHEAD VERTICAL CHORD WEB CRACKED, 1/8 INCH, AT BS 178, WL 180, BL 5.7R. MAINTENANCE CUT OUT AND REMOVED DAMAGED PART OF VERTICAL CHORD WEB AT BS 178, WL 180, BL 5.7R IAW BOEING 737-300 SRM 53-10-08-2R 12 FIG. 201. INSTALLApr 6, 2006 · N158AW · Boeing 7373G7
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