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 COMA0560515Bulkhead · crackedWHILE PERFORMING TASK CRJ-2-162014, DETAILED INSPECTION OF THE PRESSURE BULKHEAD WEBS AND VERTICAL BEAMS AT FS 559.0, TWO CRACKS WERE DISCOVERED IN THE BULKHEAD WEB RADIATING FROM THE HOLES FOR THE ATTACH BOLTS OF THE RIGHT AILERON CONTROL CABLE REAR QUADRANT Sep 21, 2005 · N949CA · Cndair CL6002B19SDR USAA051132Pressure Panel · crackedFOUND CRACK STA 665, LBL 30. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW TR 53-60-04, DEFECT SIZE: 1.0" CRACK.Sep 20, 2005 · N782AU · Boeing 7374B7SDR 0509003Bulkhead · crackedBS 1016 AFT PRESSURE BULKHEAD WEB TO Y-CHORD ATTACHMENT CRACKED.Sep 19, 2005 · N733TW · Boeing 7372H4SDR SWAA052847Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD WEB CRACKED A LBL 17.1, WL 236. REPAIRED WEB PER SRM.Sep 19, 2005 · N506SW · Boeing 7375H4SDR 05092003Bulkhead · crackedBS 1016 AFT PRESSURE BULKHEAD WEB TO "Y" CHORD ATTACHMENT CRACKED.Sep 19, 2005 · N733TW · Boeing 7372H4SDR SWAA052809Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT DOME CAP, 4 O'CLOCK, 5 O'CLOCK & 7 O'CLOCK POSITIONS. REPAIRED WEB PER SWA EA.Sep 18, 2005 · N334SW · Boeing 7373H4SDR ASOA05765Bulkhead · crackedDURING A C-CHECK IN MCN, THE PRESSURE BULKHEAD AT FS 202.75 WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED PRESSURE BULKHEAD AT FS 202.75 IAW BOMBARDIER REO 601R-53-11-583. (M)Sep 17, 2005 · N841AS · Cndair CL6002B19SDR QXEA200501320Bulkhead · corrodedYYC - FUSELAGE STATION 280 BULKHEAD HAS CORROSION AT RBL 11 TO RBL 15 AND WL 72. REMOVED CORROSION IAW REO 670-53-11-052 REV "A" REPAIR NR 1. REPLACED RT LOWER BULKHEAD WEB IAW REO 670-53-11-052 REV "A" REPAIR NR 2. AREA REMOVED WAS .029".Sep 17, 2005 · N617QX · Cndair CL6002C10SDR GTIA050252Bulkhead · corrodedFTW - FOUND MID CARGO AFT PRESSURE BULKHEAD PANEL (5318C) HAS A PULLED RIVET AND LIGHT SURFACE CORROSION, MISSING CAMLOCKS. CORROSION REMOVED, FOUND CRACK AND OUT OF LIMITS. FABRICATED REPAIR DOUBLER AND FILLER. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER Sep 14, 2005 · N808NK · Doug DC983SDR SWAA052788Pressure Panel · crackedDURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BEADED PRESSURE WEB CRACKED AT BS 663, LBL 31 & RBL 39. REPAIRED BEADED WEB PER SRM.Sep 14, 2005 · N657SW · Boeing 7373L9SDR AWXA200501174Bulkhead · crackedMCN - DURING C18 CHECK DISCOVERED VERTICAL BEAM WEB CRACKED, 1.0" IN LENGTH, AT BS 178, WL 230 AND BL 17.1L. MAINTENANCE CUT OUT DAMAGED SECTION OF WEB IAW BOEING 737-300 SRM 53-10-082R FIG 201. FABRICATED REPAIR WEB AND SHIM IAW BOEING 737-300 SRM 53-10-08-Sep 13, 2005 · N302AW · Boeing 7373G7SDR SWAA052818Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE BULKHEAD WEB CRACKED AT BS 179, LBL 17.1, WL 236. REPAIRED WEB PER SRM.Sep 13, 2005 · N506SW · Boeing 7375H4SDR SWIA200515618Bulkhead · crackedREAR PRESSURE BULKHEAD, AFT SIDE RBL - 36.0 - WL 73.50, CRACKED ON VERTICAL BEAM, FWD RADIUS, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO CRJ REO 601R-53-61-1532.Sep 12, 2005 · N408SW · Cndair CL6002B19SDR SWIA200515608Bulkhead · crackedRT MLG WHEEL BAY, PRESSURE BULKHEAD WEB IS CRACKED BEHIND AILERON QUADRANT, FS 559.00 - RBL 17.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-260 REV A & CRJ REO 601R-53-41-251 REV "A" & CRJ REO 601R-53-41-348.Sep 12, 2005 · N408SW · Cndair CL6002B19SDR USAA051071Bulkhead · damagedMID BULKHEAD O/B FWD UPPER BOLT HOLE PP STA 164.3 DAMAGED. REAMED HOLE, INSTALLED SLEEVE BUSHING, REAMED PER EA 96822, DEFECT SIZE: .8810.Sep 9, 2005 · N628AU · Boeing 7572B7SDR AWXA200501110Bulkhead · crackedMCN - DURING C18 CHECK DISCOVERED VERTICAL BEAM WEB CRACKED, .780 INCHES IN LENGTH, AT BS178, WL 230, BL 17.1L. MAINTENANCE REMOVED DAMAGED PART OF WEB IAW BOEING 737-300 SRM 53-10-08-2R. FABRICATED REPAIR WEB IAW BOEING 737-300 SRM 53-10-08-2R. INSTALLED FSep 8, 2005 · N154AW · Boeing 7373G7SDR AWXA200501112Bulkhead · crackedMCN - DURING C18 CHECK DISCOVERED VERTICAL CHORD CRACKED IN WEB AT BS 178, WL 230, BL 17.1R. MAINTENANCE CUTOUT DAMAGED SECTION OF WEB AT BULKHEAD 178 IAW BOEING 737-300 SRM 53-10-08-2R. FABRICATED WEB IAW BOEING 737-300 SRM 53-10-08-2R. INSTALLED FABRICATESep 6, 2005 · N154AW · Boeing 7373G7SDR DL767050518Bulkhead · crackedDAMAGE FOUND ON FS 1582 BULKHEAD AT STIFFENER 14L LAPJOINT BETWEEN TEAR STRAPS 4 AND 5. REPAIRED USING DOUBLER/STRUCTURAL SHIMS ON AFT SIDE OF BULKHEAD. BOEING APPROVED WITH AMOC TO AD 2005-03-11.Sep 6, 2005 · N103DA · Boeing 767232SDR SWAA052736Pressure Panel · crackedDURING SCHEDULED 5Y CHECK, FOUND RIGHT MLG W/W FWD WEB CRACKED AT BS 663, RBL 14. REPAIRED WEB PER SRM.Sep 4, 2005 · N784SW · Boeing 7377H4SDR 2005UALA00931Bulkhead · gougedAFT PRESSURE BULKHEAD HAS SEVERAL GOUGES AND SCRATCHES AT UPPER ELECTRICAL CONDUIT THROUGH LT SIDE LBL 5 TO LBL 3 WL 84.Sep 3, 2005 · N327UA · Boeing 737322SDR SWAA052695Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT DOME CAP, 5 O'CLOCK POSITION. REPAIRED WEB PER SWA EA.Sep 2, 2005 · N670SW · Boeing 7373G7SDR SWAA052674Stiffener · corrodedDURING SCHEDULED 1/4D CHECK, FOUND LT CHANNEL STIFFENER CORRODED AT BS 1016 BULKHEAD, BL 0. REPAIRED STIFFENER PER BOEING DRAWING.Sep 2, 2005 · N373SW · Boeing 7373H4SDR LR7A05111Bulkhead · crackedDURING SCHEDULED A-CHECK PER JOB CARD HA1200 FOUND LEFT FS 858 BULKHEAD TEE AND WEB CRACKED AT LBL 69, WL 198. REPAIRED IAW LAC MEA 382-53-05-067, LP 21228 ITEM M3.Sep 2, 2005 · N406LC · Lkheed 382GSDR 05FDEA02733Bulkhead · crackedCENTER WHEEL WELL LEFT FORWARD BULKHEAD SPOILER PUSHROD (MJ) FEED THROUGH CUTOUT REINFORCEMENT DOUBLER FOUND CRACKED. CTR WHEEL WELL LT FWD BULKHEAD SPOILER PUSH ROD (MJ) FEEDTHROUGH CUTOUT REINFORCEMENT DOUBLER REMOVED AND REPLACED AS PER SRM 51-31-01 VOL IISep 2, 2005 · N609FE · Doug MD11SDR VTZA200500166Bulkhead · corrodedFS 280 BETWEEN LBL AND RBL 9.0 HAS LEVEL 2 CORROSION.Aug 31, 2005 · N622BR · Cndair CL6002B19SDR VTZA200500157Bulkhead · crackedRT SIDE PILOTS BULKHEAD AT FS 280 RBL 9.0 IS CRACKED AT 1.0" IN WEB RADIUS.Aug 31, 2005 · N679BR · Cndair CL6002B19SDR VTZA200500152Bulkhead · crackedLT SIDE BULKHEAD AT FS 280 IBL 9.0 IS CRACKED AT 1.0" IN WEB RADIUS.Aug 31, 2005 · N622BR · Cndair CL6002B19SDR ASAA0540434Bulkhead · corrodedCORROSION ON AFT PRESSURE BULKHEAD C-CHANNEL. REMOVED DAMAGED SECTION OF AFT PRESSURE BULKHEAD AND VERTICAL STIFFENER, FABRICATED REPAIR PARTS AND INSTALLED IAW EA. (K)Aug 30, 2005 · N771AS · Boeing 7374Q8SDR EIA2005243Bulkhead · crackedFWD CARGO STA 260 S-34R TO S-40R CANTED PRESSURE BULKHEAD WEB FOUND CRACKED. REPAIRED PER EA-53-0997.Aug 30, 2005 · N479EV · Boeing 747132SDR EIA2005242Bulkhead · crackedFWD CARGO STA 260 S-34L TO S-40L CANTED PRESSURE BULKHEAD WEB FOUND CRACKED. REPAIRED PER EA-53-0997.Aug 30, 2005 · N479EV · Boeing 747132SDR SWAA052649Angle · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 1016 AFT PRESSURE BLKHD Z-ANGLE CRACKED AT 6:30 O'CLOCK POSITION. REMOVED AND REPLACED Z-ANGLE PER SRM.Aug 30, 2005 · N670SW · Boeing 7373G7SDR UPS05845611Pressure Panel · corrodedINSPECTION TYPE:C3 CORROSION UNDER STIFFENER ON RIGHT W/W CEILING STA 902 RBL 50-55. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW UPS EO DC8-5310- 23036-A AND SAA SK 801-804599.Aug 29, 2005 · N801UP · Doug DC873FSDR UPS05845546Bulkhead · corrodedHEAVY CORROSION ON VERTICAL STIFFENER ON FWD BULKHEAD RT W/W STA 857, RBL 45, 12" BELOW CEILING. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW DWG 5643433 AND SRM TR 51-2-1 FIG 1.Aug 29, 2005 · N801UP · Doug DC873FSDR UPS05845545Bulkhead · corrodedHEAVY CORROSION ON AFT 980 BULKHEAD LT WW OB CORNER ABOVE LONG 24 LT. REMOVED CORROSION, FABRICATED, AND INSTALLED SHIM IAW SAA SK 801-80457 2.Aug 29, 2005 · N801UP · Doug DC873FSDR UPS05245435Bulkhead · corrodedINSPECTION TYPE: C, CORROSION ON LT WHEEL WELL BULKHEAD AT BS 870 - FWD FACE 25 INCH FROM O/B EDGE AND 20 INCH FROM BOTTOM EDGE. REPAIR CARRIED OUT IAW AAAE RO 2005-081-2 -UPS ENG FILE NUMBER 727-53 -20190.Aug 28, 2005 · N922UP · Boeing 72731CSDR UPS05445379Bulkhead · corrodedINSPECTION TYPE:C L/G - RBLG W/W STA 1480 BULKHEAD FWD FACE FOUND SURFACE CORROSION AROUND L/G RETRACT ACTUATOR UPPER MOUNT AREA. BS 1480 BULKHEAD CORRODED. TIME LIMITED REPAIR AT RBL 85 WL 156 AREA AS PER H HX RS R53-43-35364 AND UPS EO B747-5310-22826-A. Aug 25, 2005 · N526UP · Boeing 747212BSDR SWAA052652Pressure Panel · crackedDURING SCHEDULED RON CHECK, FOUND NLG W/W RT UPPER ACCESS PANEL CUTOUT, AFT INBD CORNER CRACKED AT BS 251.6, LBL 2.0. REPAIRED WEB PER SWA EA.Aug 25, 2005 · N687SW · Boeing 7373Q8SDR CA050829003Bulkhead · cracked(CAN) DURING THE CONTINUING AIRWORTHINESS STRUCTURAL INSPECTION CHAFFING DAMAGE WAS FOUND ON THE AFT SIDE OF THE AFT PRESSURE BULKHEAD. THE LOWER CENTER AND THE LOWER RT INTERCOSTALS RUBBING ON THE BULKHEAD DURING PRESSURIZATION CAUSED THE DAMAGE. FURTHER INVEAug 25, 2005 · Beech A100SDR ABXA050215Pressure Panel · corrodedAREA OF EXFOLIATION ON UPPER PRESSURE PANEL, MAIN FRAME AREA. REMOVED AND REPLACED DOUBLERS IAW DC-9 SRM 51-30-5.Aug 22, 2005 · N956AX · Doug DC941SDR DHL2005806504Stiffener · crackedREF. NR. 041519) FWD ACCY COMPT RT PRESSURE BULKHEAD STIFFENER CRACKED 1 AT STA 8.000. REMOVED CRACKED STIFFENER IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED NEW STIFFENER (AL7075 INCH 0 INCH 0.071INCH) IAW SRM 53-3-3 FIG. 3. HEAT TREATED IAW SRM 51-1-1 PG. 1,Aug 19, 2005 · N806DH · Doug DC873FSDR 05FDEA02548Rib · crackedNR 2 FLAP TRACK CENTER FAIRING AFT FORMER IS CRACKED. REMOVED AND REPLACED RIB IAW SRM 51-30-2Aug 19, 2005 · N479FE · Boeing 727200SDR SWAA052440Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE VERTICAL BEAM WEB CRACKED AT BS 178 BULKHEAD, BETWEEN LBL 17.1 TO RBL 17.1, BETWEEN WL 212 TO WL 227. REPAIRED WEB PER SRM.Aug 14, 2005 · N696SW · Boeing 7373T5SDR SWAA052439Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT STR 7L. REPAIRED WEB PER SWA EA.Aug 14, 2005 · N690SW · Boeing 7373G7SDR USAA200508002Pressure Panel · crackedA .75 INCH CRACK FOUND IN LT MLG WHEEL WELL PRESSURE FLOOR WEB STA 665/LBL 30. INSTALLED DOUBLER PER TYPICAL REPAIR 53-60-04A & EA 81311.Aug 13, 2005 · N353US · Boeing 737301SDR 05FDEA02463Bulkhead · unknownPREVIOUS REPAIR AFT PIT AT 1183 BULKHEAD IS A MAJOR REPAIR IAW EO 7-5310-7-2344.Aug 13, 2005 · N479FE · Boeing 727200SDR UPS05845227Bulkhead · crackedAFT PRESSURE BULKHEAD CRACKED 1.5" LONG FS 1766 RBL 48 L11R. CUT OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAE DWG SRO 8530007.Aug 12, 2005 · N750UP · Doug DC871FSDR DHL2005806501Finger Doubler · corrodedCOCKPIT SUBFLOOR PRESSURE PANEL FINGER DOUBLER CORRODED (STA -67.000 TO -80.000). REMOVED CORROSION FROM FINGER DOUBLER IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FINGER DOUBLER IAW SRM 51-1-21 PG 1. FABRICATED FINGAug 12, 2005 · N806DH · Doug DC873FSDR UPS05845452Pressure Panel · corrodedPOPPED RIVET, PILLOWED SKIN, LT W/W CEILING, STA 940 OB ABOVE L24L. REMOVED CORROSION AND FOUND OUT OF LIMITS AT STA 940 L24L IAW SRM 51-1-8, FABRICATED AND INSTALLED FILLER, SPLICE DOUBLER FINGER DOUBLER AND TAPERED FILLER AT STA 940 L24L IAW SAA SK 750-8463Aug 10, 2005 · N750UP · Doug DC871FSDR CA050818003Bulkhead · cracked(CAN) CRACK ON FRONT PRESSURE BULKHEAD LT VERTICAL WEB, AT LT NOSE GEAR TRUNNION ATTACHMENT BRACKET TOP CENTER BOLT HOLE.Aug 9, 2005 · Bag JETSTM3212SDR 05FDEA02362Pressure Panel · crackedON STA 1510 CTR W/W ON WEB X=31.5 Z=-36 FOUND CRACK 1,75". REPAIR PER SRM 53-00-01 FIG 10 SHEET 5, 6, 7 VOL 1.Aug 9, 2005 · N564FE · Doug MD1010F
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