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 SWAA053806Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE VERTICAL BEAM WEB CRACKED AT BS 178 BULKHEAD, LBL 5.7, WL 179. REMOVED AND REPLACED VERTICAL BEAM WEB PER SRM.Nov 29, 2005 · N683SW · Boeing 7373G7SDR ABXA050327Bulkhead · corrodedFORWARD LOWER CARGO STA 644 BULKHEAD SKIN WAS BULGED FROM LONGERON 30 TO LONGERON 29 LEFT, NUMEROUS RIVETS SHEARED. REMOVED AND REPLACED FINGER DOUBLER IAW DC9 SRM 51-30-1 AND 51-30-5.Nov 28, 2005 · N954AX · Doug DC941SDR ABXA050325Bulkhead · corrodedFOUND CORROSION LONGERON 29 LEFT AND ADJACENT LONGERON PRESSURE BULKHEAD TO FS 675 LEFT KEEL AREA. REPAIRED AREA IAW DC9 SRM 53-01.Nov 28, 2005 · N954AX · Doug DC941SDR 05FDEA03972Flange · crackedCLG WHEEL WELL/SPACE: 1EA CRACK 1 INCH LONG ON DOUBLER FLANGE UPPER SIDE LT VERTICAL BULKHEAD FROM STA 1421 TO 1431 LT SIDE X 31. REMOVED DOUBLER IAW SRM 51-35-01 PG 1/13 VOL 2. CLEANED UP CRACK REPAIRED IAW SRM 53-00-01 FIG 4 SHT 2 VOL 1 WITH FILLER AND REINov 28, 2005 · N68056 · Doug DC1010SDR SWAA053745Bulkhead · crackedDURING SCHEDULED D CHECK, FOUND FUSELAGE BS 178 BLKHD LT SIDE WEB CRACKED. REPAIRED BS 178 BLKHD WEB PER SRM.Nov 27, 2005 · N318SW · Boeing 7373H4SDR QXEA200501800Bulkhead · corrodedYYC - BULKHEAD AS FUSELAGE STATION 280 RIGHT LOWER WEB IS CORRODED. REPAIRED WEB IAW REO 670-53-11-052 REVISION A.Nov 24, 2005 · N604QX · Cndair CL6002C10SDR 05FDEA03952Bulkhead · crackedRT AIR CONDITIONING COMPT FOUND 1 CRACK 2.50" LONG ON BULKHEAD BETWEEN STA 575 AND STA 569 Z-60 X-24. REPAIRED CRACK IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F164142/N001142 AND IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1.Nov 24, 2005 · N68056 · Doug DC1010SDR ASOA051070Bulkhead · corrodedDURING A C-CHECK IN TUS, THE LOWER LEFT SIDE FS 280 BULKHEAD WEB WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LOWER LEFT SIDE FS 280 BULKHEAD WEB IAW ASA EC EO700-53-0062, REPAIR NR 2. (M)Nov 23, 2005 · N740EV · Cndair CL6002C10SDR DL78K050748Bulkhead · deformedTHE BS 1016 AFT PRESSURE BULKHEAD WEB AT LBL 5 AND WL 290 HAS A 5 INCH X 5.5 INCH X 0.156 INCH DEEP OIL CAN. THE BULKHEAD WEB DAMAGE WAS REMOVED AND REPAIR DOULBER WAS INSTALLED PER ER/A 451749-14.Nov 22, 2005 · N3732J · Boeing 737832SDR AWXA200501513Bulkhead · crackedMCN - DURING C19 CHECK DISCOVERED CRACK UNDER LT ANTENNA ATTACH BRACKET AT BS 178, WL 212 AND BL 5L. MAINTENANCE CUT OUT DAMAGED PART OF WEB IAW BOEING 737-300 SRM 53-10-08-2R11. FABBED DOUBLER AND SHIM IAW BOEING 737-300 SRM 53-10-08-2R11. INSTALLED FABRICNov 21, 2005 · N164AW · Boeing 73733ASDR AWXA200501586Bulkhead · crackedMCN - DURING C20 CHECK DISCOVERED VERTICAL WEB CRACKED, 1.31 INCHES, FROM WL 226 TO WL 234, BS 178 AND BL 17R. MAINTENANCE REMOVED VERTICAL WEB FROM WL 226 TO WL 234, BS 178 AND BL 17R IAW BOEING 737-300 SRM 53-10-08-2R17 FIG 201. FABRICATED NEW WEB IAW BOEINov 20, 2005 · N316AW · Boeing 7373S3SDR AWXA200501509Bulkhead · crackedMCN - DURING C19 CHECK DISCOVERED WEB CRACKED, .975 INCHES, AT FASTENER AT BS 178, WL 234 AND BL 10R. MAINTENANCE REMOVED SHEAR WEB IAW BOEING 737-300 SRM 53-10-51-2R8. FABRICATED SHEAR WEB IAW BOEING 737-300 SRM 53-10-51-2R8. INSTALLED FABRICATED REPAIR PANov 18, 2005 · N164AW · Boeing 73733ASDR 05FDEA03881Repair · unknownPERFORMED INSPECTION IAW EO 8-5100-7-5001-1P FOUND DOUBLER LENGTH 13.5 INCHES WIDTH 11 INCHES FWD NLG BULKHEAD LT STA 490 Z-40. STRIPPED AREA IAW SRM 51-21-01 VOL 2 PAR 33. REPLACED FASTENERS AS REQUIRE IAE SRM 53-30-00 FIG 6 VOL 1 AND TREATED AREA IAW SRM 5Nov 18, 2005 · N302FE · Doug DC1030SDR 05FDEA03880Repair · unknownPERFORMED INSPECTION IAW EO 8-5100-7-5001-1P FOUND DOUBLER LENGTH 11 INCHES WIDTH 13.5 INCHES FWD NLG BULKHEAD RT AT STA 490 Z-40. STRIPPED PAINT AREA IAW SRM 51-21-01 PAR 33 VOL 2. REPLACED FASTENERS AS REQUIRED IAW SRM 53-30-00 FIG 6 VOL 1. TREATED AREA INov 18, 2005 · N302FE · Doug DC1030SDR SWIA200516555Pressure Panel · crackedCARGO COMPARTMENT AFT PRESSURE WEB FS 621 LINTEL INSTALLATION CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED WEB IAW CRJ REO 601R-53-61-1230 REV C.Nov 17, 2005 · N411SW · Cndair CL6002B19SDR SWIA200516554Pressure Panel · crackedCARGO COMPARTMENT AFT PRESSURE WEB FS 621 LBL 27.5 WL 130 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. WEB REPAIR CARRIED OUT REF RII 53-401 & M-337.Nov 17, 2005 · N411SW · Cndair CL6002B19SDR SWIA200515934Bulkhead · crackedRT MLG BAY; REAR PRESSURE BULKHEAD IS CRACKED AT AILERON QUADRANT; FS 559.00; RBL 17.0 + RBL 10.0, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED REAR PRESSURE BULKHEAD AT FS 559.00, RBL 17.0 & RBL 10.0 IAW CRJ REO 601R-53-41-260 REV "A".Nov 17, 2005 · N411SW · Cndair CL6002B19SDR 05FDEA03834Bulkhead · crackedRT AIR CONDITIONING COMPT FOUND 1 CRACK 2 INCHES LONG ON BULKHEAD BETWEEN STA 482 AND STA 489 Z-60 X-24. REPAIRED CRACK IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1, FABRICATED PARTS IAW DETAIL PARTS TRAVELER F164141/N01141 AND IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1.Nov 16, 2005 · N68056 · Doug DC1010SDR SWAA053639Pressure Panel · crackedDURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 663, LBL 32. REPAIRED WEB PER SRM.Nov 16, 2005 · N512SW · Boeing 7375H4SDR SWAA053631Pressure Panel · crackedDURING SCHEDULED SERVICE CHECK, FOUND NLG W/W LEFT FWD PRESSURE SIDE WEB CRACKED AT BS 251.625, WL 177. REPAIRED WEB PER SWA EA & SRM.Nov 14, 2005 · N303SW · Boeing 7373H4SDR SWAA053604Stiffener · corrodedDURING SCHEDULED 1/4D CHECK, FOUND BS 1016 AFT PRESSURE BLKHD STIFFENER CHANNEL CORRODED AT 6 O'CLOCK POSITION. REPAIRED STIFFENER CHANNEL PER SWA ACO & BAC DRAWING.Nov 14, 2005 · N336SW · Boeing 7373H4SDR 05FDEA03799Repair · properFOUND FWD PRESSURE BULKHEAD STA 275 LT HAND SIDE FOUND REPAIR DOUBLER BETWEEN X 13, X28 AND Z-14, Z-27.7 BEAMS. PERFORMED A GVI OF DOUBLER IAW CONTINENTAL AIRLINES EC/RA #253C037 AND FEDEX EA#8-5310-79443B AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO#Nov 14, 2005 · N68056 · Doug DC1010SDR LR7A05190Pressure Panel · crackedDURING C-7 CHECK PER SB 382-57-85, FOUND PRESSURE WEB CRACKED 1/2 INCH FROM AFT FASTENER HOLE RUNNING TO AFT EDGE OF WEB, FS 557-617, WL257, RBL61. REPAIRED IAW SMP 583 57-70 AND 51-140-12, NR 0622.Nov 9, 2005 · N401LC · Lkheed 382GSDR LR7A05174Bulkhead · crackedDURING C-7 CHECK PER HSP57170, FOUND RT CW REAR WEB CRACKED TWO PLACES, 4MM AT FASTENER HOLE RT CWS76, WL262, FS597 AND 5MM AT FASTERNER HOLE CWS73, WL259, FS597. REPAIRED WEB IAW ED05-028-4 AND SMP 583 FIG 57-30-22, MEA 382-57-05-085, NR 0260.Nov 9, 2005 · N401LC · Lkheed 382GSDR 05FDEA03703Repair · undamagedFOUND FLUSH DOUBLER REPAIR AT AFT PRESSURE BULKHEAD LOWER SECTION STA 2007 FROM X25 TO X-25 LONGERON 48L TO 48R. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-5001 CRITERIA FOUND IN COMPLIANCE WITH SRM 53-40-00 PAG 9A.Nov 8, 2005 · N68056 · Doug DC1010SDR 2005FA0001514Bulkhead · crackedBULKHEAD CRACKED AROUND BOTH VERTICAL FIN FORWARD ATTACH BOLTS.Nov 8, 2005 · N8050G · Cessna 177RGSDR 2005FA0001513Bulkhead · crackedBULKHEAD CRACKED AROUND BOTH VERTICAL FIN FORWARD ATTACH BOLTS.Nov 8, 2005 · N8050G · Cessna 177RGSDR 05FDEA03660Pressure Panel · crackedRT MLG WHEEL WELL 2EA CRACKS ON VERTICAL WEB AT STA 1485 X-95 OUTBOARD SIDE. REPAIRED IAW SRM 53-50-00 FIG 2A. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F161133-29 REPAIR WEB, F161133-3 FILLER (QTY 2), F161133-31 STRAP, F161133-31A STRAP AND F161133-31B STRNov 7, 2005 · N302FE · Doug DC1030FSDR GTIA050268Pressure Blkhd · damagedTEAR ON AFT PRESSURE BULKHEAD IN NOSE WHEEL WELL, LOWER LT CORNER STA 110. REMOVED DAMAGED AREA, CLEANED SHARP EDGES, FAB FILLER AND DOUBLER FROM 7075-T6, TREATED PRIMED AND INSTALLED REPAIR IAW EA. (K)Nov 6, 2005 · N835NK · Doug DC983SDR ASOA051023Bulkhead · corrodedDURING A C-CHECK IN TUS, THE LEFT FS 280 BULKHEAD WEB WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE LEFT FS 280 BULKHEAD WEB IAW ASA EO 700-53-0062, REPAIR NR 2. (M)Nov 3, 2005 · N706EV · Cndair CL6002C10SDR CA051102008Bulkhead · cracked(CAN) WHERE THE JANITROL CABIN HEATER MOUNTS TO THE FORWARD CABIN ENTRANCE BULKHEAD FS234.5, A 4 INCH CRACK WAS DISCOVERED DURING A 6 YEAR C-CHECK INSPECTION. THE CRACK RUNS PARALLEL TO THE HEATER MOUNTING FLANGE. THE 5 OTHER AIRCRAFT OF THE FLEET ARE TO BE INov 2, 2005 · Cndair CL2151A10SDR SWAA053449Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT STR 5R. REPAIRED WEB PER SRM.Nov 2, 2005 · N318SW · Boeing 7373H4SDR CA051103003Bulkhead · cracked(CAN) DURING A SPECIAL INSPECTION AFTER FINDING DAMAGE ON 4 OTHER AIRCRAFT, (SDR 20050829003, 20050928001, 20051013007 AND 20051025004) THE AFT PRESSURE BULKHEAD WAS FOUND CHAFFED BY BOTH THE CENTER INTERCOSTAL AND THE OB INTERCOSTAL ADJACENT TO THE TAIL ACCESNov 1, 2005 · Beech A100SDR UPS05845755Pressure Panel · corrodedFOUND LT NOSE TUNNEL, UPPER CEILING PRESSURE PANEL HAS 2 SHEARED RIVETS CRACKS AND BULGING CORROSION AT APPROX STA -32 LBL65. REMOVED EXISTING REPAIR FINGER DOUBLER, FINGER DOUBLER "T" FITTING AND 2 ATTACH FITTINGS. REMOVED CORRODED AREA. FABRICATED AND INSNov 1, 2005 · N813UP · Doug DC873FSDR QXEA200501675Bulkhead · damagedYYC - DURING C3 CHECK, FUSELAGE STATION 280 LOWER WEB OF BULKHEAD HAS SEVERAL OVERSIZE HOLES FROM PREVIOUS REPAIR. REPAIRED IAW REO 670-53-11-052.Oct 31, 2005 · N603QX · Cndair CL6002C10SDR QXEA200501674Bulkhead · damagedYYC- DURING C3 CHECK, FUSELAGE STATION 280 BULKHEAD RIGHT HAND LOWER WEB HAS SEVERAL OVERSIZE HOLES FROM PREVIOUS REPAIR. REPAIRED LOWER WEB IAW CRJ-700 REO 670-53-11-052.Oct 31, 2005 · N603QX · Cndair CL6002C10SDR LR7A05196Bulkhead · crackedDURING B-2 CHECK FOUND BULKHEAD CRACKED 2 INCHES SPANWISE ORIGINATING AT STANDOFF ATTTACHMENT AT FS 1012, WL282, LBL5. REPAIRED WEB IAW SMP583 FIG 51-140-17, NR 2004.Oct 31, 2005 · N402LC · Lkheed 382GSDR ABXA050358Pressure Panel · corrodedCORROSION FOUND UNDER THREE FASTENERS ON PRESSURE WEB IN RT WHEEL WELL, STA. 857, RT BUTT LINE 27. CORROSION FOUND TO BE OUT OF LIMITS ON PRESSURE WEB IN RT WHEEL WELL, STA. 857, RT BUTT LINE 27 IAW SRM 51-1-8 AND 53-2-0. FABRICATED AND INSTALLED REPAIR IAW ROct 30, 2005 · N826AX · Doug DC863FSDR AWXA200501405Bulkhead · crackedMCN - DURING C13 CHECK DISCOVERED WEB CRACKED, 1.1 INCHES, AT BS 178, WL 180 AND BL 5.7R. MAINTENANCE CUTOUT DAMAGED PORTION OF BULKHEAD WEB IAW BOEING 737-300 SRM 53-10-08-2R12. FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 53-10-08-2R12. INSTALLED Oct 30, 2005 · N312AW · Boeing 7373S3SDR AWXA200501406Stiffener · crackedMCN - DURING C13 CHECK DISCOVERED VERTICAL CHORD CRACKED, .7 INCHES, AT AFT SIDE OF 178 BULKHEAD BL 5.7L AND WL 184. MAINTENANCE CUT OUT DAMAGED AREA OF FORWARD CHORD AT BL 5.7L IAW BOEING 737-300 SRM 53-10-08-2R5. FABRICATED FILLER IAW BOEING 737-300 SRM 53Oct 29, 2005 · N312AW · Boeing 7373S3SDR AWXA200501404Bulkhead · crackedMCN - DURING C13 CHECK DISCOVERED WEB CRACKED, .50 INCHES, AT BS 178, WL 185 AND BL 17.1R. MAINTENANCE CUTOUT DAMAGED PORTION OF BULKHEAD WEB IAW BOEING 737-300 SRM 53-10-08-2R12. FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 53-10-08-2R12. INSTALLEDOct 28, 2005 · N312AW · Boeing 7373S3SDR AWXA200501403Bulkhead · crackedMCN - DURING C13 CHECK DISCOVERED WEB CRACKED, .75 INCHES, AT BS 178, WL 230 AND BL 17.1R. MAINTENANCE CUTOUT DAMAGED PORTION OF BULKHEAD WEB IAW BOEING 737-300 SRM 53-10-08-2R12. FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 53-10-08-2R12. INSTALLEDOct 28, 2005 · N312AW · Boeing 7373S3SDR SWAA053402Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BLKHD WEB CRACKED AT RBL 17.1 & LBL 17.1, WL 227. REPAIRED WEB PER SRM.Oct 28, 2005 · N507SW · Boeing 7375H4SDR AWXA200501402Bulkhead · crackedMCN - DURING C13 CHECK DISCOVERED WEB CRACKED, 1.0 INCHES, AT BS 178, WL 218 AND BL 5.7R. MAINTENANCE CUTOUT DAMAGED PORTION OF BULKHEAD WEB IAW BOEING 737-300 SRM 53-10-08-2R9. FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 53-10-08-2R9. INSTALLED FAOct 27, 2005 · N312AW · Boeing 7373S3SDR AWXA200501401Bulkhead · crackedMCN - DURING C13 CHECK DISCOVERED WEB CRACKED, 1.5 INCHES, AT BS 178, WL 218 AND BL 12L. MAINTENANCE CUTOUT DAMAGED PORTION OF BULKHEAD WEB IAW BOEING 737-300 SRM 53-10-08-2R9. FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 53-10-08-2R9. INSTALLED FABOct 27, 2005 · N312AW · Boeing 7373S3SDR AWXA200501400Bulkhead · crackedMCN - DURING C13 CHECK DISCOVERED WEB CRACKED, 2.0 INCHES, AT BS 178, WL 218 AND BL 12R. MAINTENANCE CUTOUT DAMAGED PORTION OF BULKHEAD WEB IAW BOEING 737-300 SRM 53-10-08-2R9. FABRICATED DOUBLER AND FILLER IAW BOEING 737-300 SRM 53-10-08-2R9. INSTALLED FABOct 27, 2005 · N312AW · Boeing 7373S3SDR 05FDEA03544Rib · crackedLEFT WING L/E ON INTERNAL STRUCTURE FOUND 1 CRACK 0.50'' LONG ON RIB AT STA XORS 427. PERFORMED INSPECTION IAW NDT SRM 06, NO CRACK FOUND ON RIB AT STA XORS427 LT WING L/E ONLY PENCIL MARK.Oct 27, 2005 · N302FE · Doug DC1030FSDR ABXA050353Bulkhead · corrodedFOUND CORROSION ON RIGHT WHEEL WELL, STA 980, LONGERON 24 RIGHT, AFT BULKHEAD UNDER LOWER SIDE OF DIAGONAL FRAME. REMOVED BRACKET AT STA 980 IAW DC8 SRM 51-3-0, 51-1-S0D. REMOVED CORROSION IAW DC8 SRM 53-2-0. ORIGINAL MATERIAL MEASURED .047" AND .046", OUT Oct 25, 2005 · N826AX · Doug DC863FSDR SWAA053335Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BS 1016 BULKHEAD WEB CRACKED AT STR 7L. REPAIRED WEB PER BFG ER & SRM.Oct 25, 2005 · N316SW · Boeing 7373H4SDR CA051025004Bulkhead · crackedDURING A SPECIAL INSPECTION AFTER FINDING DAMAGE ON THREE OTHER AIRCRAFT, (SDR 20050829003, 20050928001 AND 20051013007) THE AFT PRESSURE BULKHEAD WAS FOUND CHAFFED BY THE CENTER INTERCOSTAL ADJACENT TO THE TAIL ACCESS DOOR. NDT WAS COMPLETED AND A CRACKS FOUOct 24, 2005 · Beech A100
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