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 SWIA200516154Angle · crackedAFT PRESSURE BULKHEAD AFT SIDE; 2 ANGLES ARE CRACKED; 1 AT LBL40 AND 1 AT 4BL40 WL90 FS 625, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED LEFT HAND AFT PRESSURE BULKHEAD ANGLE PER 601R-35012 AND REO 601R-53-61-422. INSTALLED RIGHT HAND AFT PRESSURE BULKHEAD AOct 22, 2005 · N595SW · Cndair CL6002B19SDR 05FDEA03477Vertical Beam · damagedCOMPLY WITH EA 6-5310-92347 FUSELAGE - FR 54 BULKHEAD VERTICAL STIFFENER REPAIR. COMPLIED WITH EA 6-5310-92347 FUSELAGE FR 54 BULKHEAD VERTICAL STIFFENER REPAIR.Oct 21, 2005 · N445FE · Airbus A310203SDR 0501936624Bulkhead · crackedDURING "M" CHECK FOUND CRACK IN CANTED BULKHEAD WEB AT BS 260 ST 26L. REPAIRED PER EA 66-205518.Oct 19, 2005 · N624US · Boeing 747251BSDR UPS05845790Pressure Panel · corrodedINSPECTION TYPE:C1 MAIN CABIN SUB FLOOR, FUEL DUMP CHUTE BRACKET UNDER THE PLATE HAS HEAVY CORROSION AT 857 RBL 40. REMOVED DAMAGED AREA AND REPAIRED IAW SAA SK 813-822556 AND UPS EO DC8- 5310-23251-A.Oct 19, 2005 · N813UP · Doug DC873FSDR DJFA2005159Bulkhead · crackedDURING A ROUTINE MAINTENANCE VISIT, A CRACK WAS DISCOVERED IN THE PRESSURE BULKHEAD WEB AT FUSELAGE STATION 409.00 WHILE PERFORMING AD 97-24-02. THE CRACK WAS REPAIRED IAW EO NR 601-53-10-266, AND IN CONJUNCTION WITH DRAWING K600-31904. THE AIRCRAFT WAS RETUOct 19, 2005 · N627CW · Cndair CL6012A12SDR UPS05845791Bulkhead · crackedINSPECTION TYPE:C1 MAIN CABIN AFT PRESSURE BULKHEAD CRACKED L11R RBL 48. CUT OUT DAMAGED AREA 2 AND FABRICATED AND INSTALLED FINGER DOUBLER, DOUBLER AND 2 FILLER IAW SRM 51-1-20D, 51-3-0, 51-1-21 AND TR- 53-194.Oct 18, 2005 · N813UP · Doug DC873FSDR 05FDEA03443Bulkhead · damagedAFT CABIN STA 2007 RBL 103 TO 107, Z=-18, AFT PRESSURE BULKHEAD T-CHORD FOUND REPAIR PATCH . SNRM N0845: WORK ACCOMPLISHED AS PER EA#1-5310-87647 TITLE: FUSELAGE- MAIN FRAME- PRESSURE BULKHEAD BODY STA. Y = 2007.000, TEE CHORD REPAIR. CLASSIFIED MAJOR REPOct 18, 2005 · N574FE · Doug MD11SDR SWAA053246Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT AFT SIDE, LBL 40, WL 209. REPAIRED WEB PER SRM.Oct 18, 2005 · N316SW · Boeing 7373H4SDR ABXA050336Pressure Panel · corrodedDOUBLER CORRODED TOP OF RIGHT WHEEL WELL PRESSURE DECK IN MAIN CARGO, STA 980, RIGHT BUTT LINE 30. REMOVED, FABRICATED, AND INSTALLED DOUBLER AT TOP OF RIGHT WHEEL WELL PRESSURE DECK IN MAIN CARGO STA 980 RIGHT BUTT LINE 30 IAW DC8 SRM 51-1-21, 51-1-14, 51-9-Oct 17, 2005 · N826AX · Doug DC863FSDR LR7A05163Bulkhead · crackedDURING C-6 CHECK PER 02SB-382-5785-2, FOUND PRESSURE BULKHEAD WEB CRACKED. FS617 LBL61, WL240. REPLACED WEB IAW SRM SMP 583 51-60/70 AND AC43.13-1B, NR 0429.Oct 17, 2005 · N403LC · Lkheed 382GSDR LR7A05127Angle · crackedDURING C-6 CHECK PER HC5212, FOUND CARGO DOOR BULKHEAD WEB STIFFENERS CRACKED, FS 1023, RBL37. REPAIRED STIFFENER ANGLES PER SRM 51-140-19, NR 0107.Oct 17, 2005 · N403LC · Lkheed 382GSDR LR7A05126Angle · crackedDURING C-6 CHECK PER HC5212, FOUND CARGO DOOR BULKHEAD WEB STIFFENERS CRACKED, FS 1023, RBL34. REPAIRED STIFFENER ANGLES PER SRM 51-140-19, NR 0107.Oct 17, 2005 · N403LC · Lkheed 382GSDR LR7A05118Stiffener · crackedDURING C-6 CHECK PER HC5212, FOUND CARGO DOOR AFT BULKHEAD WEB STIFFENERS CRACKED FS 1023, RBL10. REPLACED WEB STIFFENERS IAW SRM SMP 583 FIGURE 51-70 AND AC43, 13-1B PARA 4-57 NR 0106.Oct 17, 2005 · N403LC · Lkheed 382GSDR LR7A05117Stiffener · crackedDURING C -6 CHECK PER HC5212, FOUND CARGO DOOR AFT BULKHEAD WEB STIFFENERS CRACKED FS 1023, RBL0. REPLACED WEB STIFFENERS IAW SRM SMP 583 FIGURE 51-70 AND AC43.13-1B PARA 4-57 NR 0106.Oct 17, 2005 · N403LC · Lkheed 382GSDR LR7A05116Bulkhead · crackedDURING C-6 CHECK PER HC5212, FOUND CARGO DOOR BULKHEAD WEB CRACKED LBL40. REPAIRED IAW SRM SMP 583 FIGURE 51-140-17, NR 0086.Oct 17, 2005 · N403LC · Lkheed 382GSDR PIDA20050181Pressure Panel · crackedEVIDENCE OF CRACK AT PRESSURE WEB AT BS663 AT LBL33. REPAIRED PRESSURE WEB IAW SRM 53-60-51.Oct 17, 2005 · N371PA · Boeing 737306SDR AWXA200501303Bulkhead · crackedMCN - DURING C16 CHECK DISCOVERED WEB CRACKED, 1.1 INCHES IN LENGTH, AT BL 5.7L, WL 180 AND BS 178. MAINTENANCE CUT OUT DAMAGED PART OF WEB AT BL 5.7L, WL 180 AND BS 178 IAW BOEING 737-300 SRM 53-10-08-2R 12 FIG 201. FABRICATED REPAIR WEB IAW BOEING 737-300 Oct 15, 2005 · N306AW · Boeing 7373G7SDR AWXA200501276Bulkhead · crackedMCN - MAJOR REPAIR - DURING C16 CHECK, DISCOVERED VERTICAL WEB CRACKED, .5 INCHES IN LENGTH, AT BS 180, WL 229 AND BL 17.1R. MAINTENANCE REMOVED DAMAGED AREA FROM VERTICAL WEB IAW BOEING 737-300 SRM 53-10-08-2R 12. FABRICATED REPAIR WEB AND TAPERED SHIMS IAWOct 15, 2005 · N306AW · Boeing 7373G7SDR AWXA200501275Bulkhead · crackedMCN - MAJOR REPAIR - DURING C16 CHECK, DISCOVERED VERTICAL WEB CRACKED, .05 INCHES IN LENGTH, AT BS 178, WL 193 AND BL 17.1L. MAINTENANCE REMOVED VERTICAL WEB IAW BOEING 737-300 SRM 51-40-02-0G. FABRICATED VERTICAL WEB IAW BOEING 737-300 SRM 51-40-02-0G. INOct 15, 2005 · N306AW · Boeing 7373G7SDR CA051013002Bulkhead · crackedREAR PRESS BULKHEAD CRACKED AT LBL 27.5, WL97.5, FS 621.11. REPAIRED PER: REO 601R-53-61-1285. INTEL FITTING, REPAIRED PER REO 601R-53-61-1230 UPPER OF TRACK: AS PER REO 601R-53-61-1458.Oct 13, 2005 · Cndair CL6002B19SDR CA051013001Bulkhead · crackedFOUND NUMEROUS CRACKS AT PRESSURE BULKHEAD MARKED BY BLACK MARKING REF 53-61-153 PAGE 9. PRESSURE BULKHEAD CRACKS AT STN 621 REPAIRED IAW REO 601R53-61-1230 AND PROD PERM CRJ-53-21664.Oct 13, 2005 · Cndair CL6002B19SDR SWAA053172Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT STR 23R, 5 O'CLOCK POSITION. REPAIRED WEB PER SWA EA.Oct 13, 2005 · N510SW · Boeing 7375H4SDR SWAA053171Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT STR 7R, 2 O'CLOCK POSITION. REPAIRED WEB PER SWA EA.Oct 13, 2005 · N510SW · Boeing 7375H4SDR 2006RC02001Bulkhead · cracked(CAN) PRESSURIZATION ERRATIC IN THE AIR. THE AIRCRAFT WAS TESTED ON THE GROUND AND LEAK WAS DETECTED WITH A 6 INCH CRACK LT OF THE OUTFLOW VALVE. A REPAIR DESIGN WAS CARRIED OUT.Oct 12, 2005 · Beech B200SDR CA051013007Bulkhead · crackedDURING A SPECIAL INSPECTION AFTER FINDING DAMAGE ON TWO OTHER AIRCRAFT, (SDR 20050829003 AND 20050928001) AFT PRESSURE BULKHEAD WAS FOUND CHAFFED BY THE CENTER INTERCOSTALS ADJACENT TO THE TAIL ACCESS DOOR. NDT WAS COMPLETED AND A CRACK FOUND.Oct 12, 2005 · Beech A100SDR USAA051199Bulkhead · crackedAFT PRESSURE BULKHEAD CRACKED. REPAIRED AS REQUIRED, DOUBLER INSTALLED EA 96994, DEFECT SIZE 1 INCH.Oct 12, 2005 · N300AU · Boeing 737301SDR ABXA050261Bulkhead · crackedAFT PRESSURE BULKHEAD DOOR UPPER LT CORNER 13 DOUBLER HAD RADIAL CRACK EXTENDING FROM STOP DRILL. CRACK EXCEEDED APPLICABILITY AND CRACK REPAIR LIMITS FOR PREVIOUS J060088-1 ANGLE REPAIR. STOP DRILLED CRACKS AND REPAIRED IAW SRM.Oct 11, 2005 · N962AX · Doug DC941SDR DL73S050607Bulkhead · damagedWHILE ACCOMPLISHING BOEING RECOMMENDED REWORK TO AN AFT PRESSURE BULKHEAD REDIAL STIFFENER REPAIR INSTALLED PER ER/A 089941-14AD, SEVERAL ELONGATED AND OVERSIZED HOLES WERE FOUND IN THE WEB AND STIFFENER. DAMAGE ALSO OCCURRED TO THE PAN DURING REWORK. INSTALOct 11, 2005 · N245WA · Boeing 737247SDR SWAA053125Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT DOME CAP, 1 O'CLOCK POSITION. REPAIRED WEB PER SWA EA.Oct 11, 2005 · N305SW · Boeing 7373H4SDR ASOA05854Bulkhead · crackedDURING A C-CHECK IN MCN, THE FORWARD PRESSURE BULKHEAD, FS 202.75, AT BL 23.71, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE FORWARD PRESSURE BULKHEAD FS 202.75, AT BL 23.71, IAW ASA EO 600-53-0217. (M)Oct 10, 2005 · N836AS · Cndair CL6002B19SDR SWAA053087Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT DOME CAP, 2 O'CLOCK AND 4 O'CLOCK POSITIONS. REPAIRED WEB PER SWA EA.Oct 9, 2005 · N305SW · Boeing 7373H4SDR AWXA200501322Vertical Beam · crackedMCN - DURING C18 CHECK DISCOVERED VERTICAL BEAM WEB CRACKED, .95 INCHES IN LENGTH, AT BS 178, WL 184 AND BL 17.1L. MAINTENANCE REMOVED DAMAGED AREA OF WEB IAW BOEING 737-300 SRM 53-10-08-2R 12 FIG 201. FABRICATED WEB AND SHIMS FOR VERTICAL BEAM IAW BOEING 73Oct 8, 2005 · N315AW · Boeing 7373S3SDR AWXA200501321Bulkhead · crackedMCN - DURING C18 CHECK DISCOVERED VERTICAL BEAM WEB CRACKED, 1.3 INCHES IN LENGTH, AT BS 178, WL 183 AND BL 5.7R. MAINTENANCE REMOVED DAMAGED AREA OF WEB IAW BOEING 737-300 SRM 53-10-08-2R 12 FIG 201. FABRICATED WEB AND SHIMS FOR VERTICAL BEAM IAW BOEING 737Oct 8, 2005 · N315AW · Boeing 7373S3SDR AWXA200501320Bulkhead · crackedMCN - DURING C18 CHECK DISCOVERED VERTICAL BEAM WEB CRACKED, 1.1 INCHES IN LENGTH, AT BS 178, WL 182 AND BL 17.1R. MAINTENANCE REMOVED DAMAGED AREA OF WEB IAW BOEING 737-300 SRM 53-10-08-2R 12 FIG 201. FABRICATED WEB AND SHIMS FOR VERTICAL BEAM IAW BOEING 73Oct 8, 2005 · N315AW · Boeing 7373S3SDR AWXA200501367Bulkhead · crackedDURING C18 CHECK DISCOVERED 178 BULKHEAD WEB CRACKED, 1.0 INCHES, AT BS 178, WL 207 AND BL 1.5R. MAINTENANCE CUTOUT DAMAGE ON WEB IAW BOEING 737-300 SRM 53-10-08-2R11 FIG 201. FABRICATED DOUBLER IAW BOEING 737-300 SRM 53-10-08-2R11 FIG 201. INSTALLED FABRICOct 7, 2005 · N315AW · Boeing 7373S3SDR AWXA200501323Bulkhead · crackedMCN - DURING C18 CHECK DISCOVERED WEB CRACKED AT FASTENER HOLE AT BS 178, WL254, BL 9R. MAINTENANCE CUT OUT AND REMOVED DAMAGED AREA OF WEB IAW BOEING 737-300 SRM 53-10-08-2R4 FIG 201. FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 53-10-08-2R4 FIG 201Oct 7, 2005 · N315AW · Boeing 7373S3SDR CALA0500340Bulkhead · corrodedCORROSION AT STA 1016, BL 0, FWD LWR PRESSURE BULKHEAD. REPAIRED PER DRAWING 65C28106.Oct 7, 2005 · N69333 · Boeing 7373T0SDR DLM88090303Pressure Panel · leakingMLG WHEEL WELL SLANT PRESSURE PANEL REPAIRED IAW 09-085387-12.Oct 5, 2005 · N980DL · Doug MD88SDR UPS05845733Bulkhead · crackedFOUND CRACK ON AFT PRESS BULKHEAD LBL 26, 65 INCHES FROM FLOOR CUT OUT DAMAGED AREA AT FS 1766 LBL26 IAW SRM 53-2-5 FIG 14, NDT AREA IAW SPM 06-10-01-001, NO CRACKS NOTED AT CUT OUT AREA. FABRICATED -15, -17 DOUBLERS AND -9, -11, -13 AND -19 FILLERS IAW SRM 5Oct 5, 2005 · N866UP · Doug DC873FSDR AWXA200501233Bulkhead · crackedDURING C18 CHECK DISCOVERED WEB CRACKED, 1.5 INCHES IN LENGTH, AT BS 178 FROM BL 17.5L TO BL 29.5L AND FROM WL 184.5 TO WL 240. MAINTENANCE REMOVED CRACKED WEB FROM BS 178 IAW BOEING 737-300 SRM 51-40-02-0G. FABRICATED NEW WEB IAW BOEING 737-300 SRM 51-30-01Oct 4, 2005 · N314AW · Boeing 7373S3SDR UPS05845778Pressure Panel · corrodedINSPECTION TYPE:C2 FUSELAGE FLOORBEAM HEAVY CORROSION STA 940 RBL 65. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS AT STA 940 RBL 65 IAW UPS EO DC8-5330-23084-A, SAA SK 866-832597, BOEING MESSAGE 1-133200277-3 AND FAA FORM 8100-9.Oct 3, 2005 · N866UP · Doug DC873FSDR UPS05845657Pressure Panel · corrodedC2 CORROSION UNDER DOUBLER ON LT W/W CEILING STA 960 LBL 57-62, CORROSION AT SAME LOCATION IN MAIN CABIN UNDER FLOORBEAM. REMOVED MLG LT WHEEL WELL HORIZ. PRESSURE PANEL WEB AT FS 960 LBL 57-62 IAW SAA SK 866-832452, AND UPS EO FABRICATED AND INSTALLED PRESSUOct 1, 2005 · N866UP · Doug DC873FSDR CALA050341Bulkhead · damagedRIVET HOLE ELONGATED AT AFT PRESSURE BULKHEAD WEB, STA 1016, BL 0. INSTALLED SKIN PER DRAWING 65C28106.Sep 30, 2005 · N69333 · Boeing 7373T0SDR 05FDEA03157Beam · damagedAFT LOWER CARGO BS 1183 BULKHEAD VERTICAL BEAM AT LBL 20 HAS FASTENERS INSTALLED WITH SHORT PITCH, (SIDE BY SIDE). COMPLIED WITH FED EX EA E7-5310-91297-FUSELAGE, BS 1183 AFT PRESSURE BULKHEAD SHORT ON CENTER FASTENER SPACING REPAIR. MAJOR REPAIR.Sep 29, 2005 · N267FE · Boeing 727233SDR COMA0570106Bulkhead · corrodedTHE LT AND RT LOWER BULKHEAD WEBS AT FS 280 ARE CORRODED FROM LBL 36 TO RBL 36. REMOVED THE CORRODED WEBS AND INSTALLED NEW WEBS IAW REO 670-53-11-052 REV A.Sep 28, 2005 · N367CA · Cndair CL6002C10SDR DL78K050594Bulkhead · canningOIL CANNING FOUND IN THE BS 1016 AFT PRESSURE BULKHEAD AT APPROX RBL 10 & WL 290. DAMAGE CUT OUT AND REPAIR DOUBLER INSTALLED.Sep 26, 2005 · N3737C · Boeing 737832SDR CA050928001Bulkhead · cracked(CAN) DURING A SPECIAL INSPECTION AFTER FINDING DAMAGE ON ANOTHER AIRCRAFT, (SDR 20050829003) THE SAME TWO AREAS OF THE AFT PRESSURE BULKHEAD WERE FOUND CHAFED BY THE TWO INTERCOSTALS ADJACENT TO THE TAIL ACCESS DOOR. NDT WAS COMPLETED AND THERE WERE NO CRACKSSep 23, 2005 · Beech A100SDR COMAO560518Bulkhead · crackedWHILE PERFORMING TASK INS-2-2-27L0005 ITEM NR 6, CLEANING OF THE RIGHT REAR AILERON QUADRANT LOCATED ON THE AFT WALL OF THE MLG WHEEL WELL, DISCOVERED A CRACK ON THE SEMI-PRESSURE BULKHEAD FS 559.00, BL 23L-23R. PERFORMED TEMPORARY REPAIR PER REO 601R-53-41-3Sep 22, 2005 · N931CA · Cndair CL6002B19SDR COMA0560517Bulkhead · crackedWHILE PERFORMING TASK INS-2-2-27L0005 ITEM NR 6, CLEANING OF THE RIGHT REAR AILERON QUADRANT LOCATED ON THE AFT WALL OF THE MLG WHEEL WELL, DISCOVERED A CRACK ON THE SEMI-PRESSURE BULKHEAD FS 559.00, BL 23L-23R. PERFORMED REO 601R-53-41-350.Sep 22, 2005 · N926CA · Cndair CL6002B19SDR COMA0560516Bulkhead · crackedWHILE PERFORMING TASK INS-2-2-27L0005 ITEM NR 6, CLEANING OF THE RIGHT REAR AILERON QUADRANT LOCATED ON THE AFT WALL OF THE MLG WHEEL WELL, DISCOVERED A CRACK ON THE SEMI-PRESSURE BULKHEAD FS 559.00, RBL 23L-23R. PERFORMED REO 601R-53-41-344.Sep 21, 2005 · N934CA · Cndair CL6002B19
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