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 SWAA054172Strap · crackedDURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BS 178 BULKHEAD VERTICAL STRAP CRACKED AT BL 0, WL 188. REPAIRED STRAP PER SWA EA.Dec 28, 2005 · N688SW · Boeing 7373Q8SDR SWAA054127Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT BL 0, WL 189. REPAIRED WEB PER SRM.Dec 27, 2005 · N688SW · Boeing 7373Q8SDR AWXA200600111Bulkhead · crackedMCN - DURING C19 CHECK DISCOVERED VERTICAL WEB CRACKED, .25 INCHES, AT BS 178, WL 176 AND FROM BL 5L TO BL 7L. MAINTENANCE CUT OUT CRACKED SECTION OF WEB IAW BOEING 737-300 SRM 53-10-08-2R12 FIG 201. FABRICATED REPLACEMENT WEB IAW BOEING 737-300 SRM 53-10-08Dec 26, 2005 · N168AW · Boeing 73733ASDR AWXA200600160Bulkhead · corrodedMCN - DURING C19 CHECK DISCOVERED CORROSION ON THE AFT PRESSURE BULKHEAD, LOWER FORWARD FACE SKIN, RT OUTBOARD SIDE OF THE CENTER CHANNEL AT BS 1016, WL 201 AND BL 2R. MAINTENANCE CUT OUT DAMAGED SECTION OF BULKHEAD IAW BOEING DWG 65C28106. RECEIVED AND INSTDec 24, 2005 · N168AW · Boeing 73733ASDR SWIA200516425Bulkhead · crackedCARGO COMPARTMENT AFT PRESSURE BULKHEAD WEB LBL 27.5, WL 130 CRACKED, ITEM FOUND AT C CHECK INSPECTION. WEB REPAIRED. REF. CRJ REO 601R-53-61-1541 REV "NC".Dec 23, 2005 · N407SW · Cndair CL6002B19SDR SWIA200516421Bulkhead · crackedRT MLG BAY, PRESSURE BULKHEAD IS CRACKED BESIDE AILERON QUADRANT ATTACH BOLT, FS 559.0, RBL 17, ITEM FOUND AT C CHECK INSPECTION. RT MLG BAY PRESSURE BULKHEAD REPAIRED. REF. CRJ REO 601R-53-41-260 REV "A".Dec 23, 2005 · N407SW · Cndair CL6002B19SDR AWXA200600062Bulkhead · crackedMCN - DURING C15 CHECK DISCOVERED 178 BULKHEAD WEB CRACED, 1 INCH, AT WL 212 AND BL 7L. MAINTENANCE REMOVED DAMAGED AREA AND MADE INSURANCE CUT OUT IAW BOEING 737-300 SRM 53-10-08-2R10. FABRICATED DOUBLER AND FILLERS IAW BOEING 737-30 SRM 53-10-08-2R10. INSDec 21, 2005 · N308AW · Boeing 7373G7SDR AWXA200600061Bulkhead · crackedMCN - DURING C15 CHECK DISCOVERED BS 178 BULKHEAD WEB CRACKED IN TWO PLACES, .975 INCHES AND 1.1 INCHES, AT WL 213 BL 7R AND WL 218 BL 10R. MAINTENANCE STOP DRILLED BOTH CRACKS IAW BOEING 737-300 SRM 53-10-09-2R10. FABRICATED DOUBLER, STIFFENERS, CLIPS, FILLDec 21, 2005 · N308AW · Boeing 7373G7SDR DJFA2005179Bulkhead · crackedDURING A SCHEDULED MAINTENANCE VISIT, A CRACK WAS DISCOVERED IN THE PRESSURE BULKHEAD WEB AT FUSELAGE STATION 409.00 WHILE PERFORMING AIRWORTHINESS DIRECTIVE 97-24-02, SERVICE BULLETIN 601-0501. THE CRACK IS LOCATED AT THE CORNER OF THE KEEL BEAM LINK CUTOUT Dec 21, 2005 · N664CW · Cndair CL6012A12SDR SWAA054057Pressure Panel · crackedDURING SCHEDULED 1/2D CHECK, FOUND NLG W/W RIGHT FWD SIDE PRESSURE PANEL CRACKED AT BS 243.7, WL 168.5. REPAIRED WEB PER SWA EA.Dec 19, 2005 · N688SW · Boeing 7373Q8SDR SWAA054056Pressure Panel · crackedDURING SCHEDULED 1/2D CHECK, FOUND NLG W/W LEFT FWD SIDE PRESSURE PANEL CRACKED AT BS 240, WL 168.6. REPAIRED WEB PER SWA EA.Dec 19, 2005 · N688SW · Boeing 7373Q8SDR C2XA05SH140Firewall · crackedSHV - DURING C-CHECK MAINTENANCE FOUND APU FIREWALL CRACKED AT THE RIGHT HAND LOWER MOUNT. MAINTENANCE INSTALLED DOUBLER ON THE APU FIREWALL AT THE RIGHT HAND LOWER MOUNT IAW EMB SRM 53-32-13. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Dec 18, 2005 · N13553 · Emb EMB145LRSDR SWAA053993Pressure Panel · crackedDURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 664, LBL 32. REPAIRED BEADED WEB PER SWA EA.Dec 18, 2005 · N511SW · Boeing 7375H4SDR C2XA05SH141Firewall · crackedSHV - DURING C-CHECK MAINTENANCE FOUND APU FIREWALL CRACKED AT MID RIGHT HAND SECTION (INSIDE). MAINTENANCE INSTALLED REPAIR DOUBLER ON APU FIREWALL AT MID RIGHT HAND SECTION IAW EMB 145 SRM 53-32-13 FIG 204. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Dec 18, 2005 · N13553 · Emb EMB145LRSDR SWAA053991Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE BULKHEAD WEB CRACKED AT BS 178, RBL 5.7, WL 187. REPAIRED BULKHEAD WEB PER SRM.Dec 16, 2005 · N501SW · Boeing 7375H4SDR ASOA01094ABulkhead · crackedDURING A C-CHECK IN MCN, THE FS 280 BULKHEAD WAS FOUND TO BE CRACKED OUTBOARD OF RBL 9 AND LBL 9, AND THE FLOOR SUPPORT ANGLE WAS FOUND TO BE CRACKED OUTBOARD OF LBL 9 AND CORRODED BETWEEN RBL 9 AND LBL 9. MAINTENANCE WILL REPAIR THE FS 280 BULKHEAD, OUTBOARDDec 15, 2005 · N840AS · Cndair CL6002B19SDR SWAA054036Pressure Panel · crackedDURING SCHEDULED C3 CHECK, FOUND NLG W/W UPPER CEILING WEB CRACKED AT BS 251.625, RBL 7.75 & LBL 7.75. REPAIRED WEB PER SWA EA.Dec 14, 2005 · N351SW · Boeing 7373H4SDR 2005UALA01447Bulkhead · ground damageBULKHEAD DAMAGE AT STATION 350 APPROXIMATELY 14 INCHES RIGHT OF FR 1. DAMAGE CAUSED BY IMPACT WITH GROUND EQUIPMENT. HORIZONTAL STIFFENER REPLACE, BULKHEAD WEB DOUBLER INSTALLED, FRAME REPAIR, AND VERTICAL STIFFENER DOUBLER INSTALLED.Dec 13, 2005 · N491UA · Airbus A320232SDR 05FDEA04282Bulkhead · crackedFOUND LT AIR CONDITIONING COMPT FOUND 1 CRACK 4" LONG ON SKIN OF BULKHEAD BETWEEN STA 584 AND STA 580 Z-46 BY 24. TRIMMED OUT CRACK AND INSTALLED FILLER AND 2 REPAIRED DOUBLERS IAW SRM 53-30-00 FIG 6 SHT 2 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F1Dec 13, 2005 · N68056 · Doug DC1010SDR COMA0560716Bulkhead · damagedHOLE IN AFT PRESSURE BULKHEAD FS 621 AND LBL 45. INSTALLED RIVET IN FS 621 AND LBL 45 AFT PRESSURE BULKHEAD IAW SRM 51-12-00 PG 21, SMALL HOLE REPAIR.Dec 13, 2005 · N721CA · Cndair CL6002B19SDR AU510001997Bulkhead · crackedREAR PRESSURE BULKHEAD EXTENDER NR 7 CLEAT CRACKED.Dec 12, 2005 · Beech 200BEECHSDR AU510001991Bulkhead · crackedREAR FUSELAGE BULKHEAD CRACKED. FOUND FOLLOWING REMOVAL OF FORWARD FIN ATTACHMENT FITTING.Dec 12, 2005 · Piper PA32300SDR AU510001983Bulkhead · crackedREAR FUSELAGE BULKHEAD CRACKED. FOUND FOLLOWING REMOVAL OF STEEL FORWARD FIN ATTACHMENT FITTING.Dec 12, 2005 · Piper PA28151SDR AU510001735Screw · defective(AUS) CONTROL COLUMN/ELEVATOR BELLCRANK TORQUE TUBE SUPPORT SCREWS PNO MS35206-228 (2OFF3) DEFECTIVE. SCREWS APPEAR TO HAVE BEEN OVERTORQUED DURING ASSEMBLY. (OTHER CAUSE: MANUFACTURING QUALITY CONTROL ISSUE ) (CASA NR 510001735)Dec 12, 2005 · Cessna 182SSDR AU510001598Frame · crackedFUSELAGE-BODY STATION 1809.5 BULKHEAD RT FORWARD OUTER CHORD CRACKED IN LOWER FORWARD HOLE. FOUND DURING INSPECTION IAW AD/B767/146 AMDT2 AND AAES AD ER NO B76-53-36F.Dec 12, 2005 · Boeing 767277SDR AU510001527Pressure Panel · corrodedFUSELAGE STRUCTURE PRESSURE WEB CORRODED. WEB IS LOCATED AT FS 46 IN THE MAIN LANDING GEAR WHEEL WELL.Dec 12, 2005 · Boeing 7272J4SDR LR7A05208Cap · crackedDURING 'B-3' CHECK PER HB5302, FOUND LOWER FLANGE OF BULKHEAD CAP CRACKED 3 INCHES AT FS902, WL195, RBL64. REPAIRED CAP IAW SMP583 FIG. 53-50-17. N/R NO. 0078.Dec 12, 2005 · N404LC · Lkheed 382GSDR SWAA053929Stiffener · corrodedDURING SCHEDULED 1/2D CHECK, FOUND BS 1016 AFT PRESSURE BULKHEAD ANGLE STIFFENER CORRODED AT BL 0. REPAIRED ANGLE STIFFENER PER ACO & SRM.Dec 12, 2005 · N511SW · Boeing 7375H4SDR SWAA053928Stiffener · corrodedDURING SCHEDULED 1/2D CHECK, FOUND BS 1016 AFT PRESSURE BULKHEAD CHANNEL STIFFENER CORRODED AT BL 0. REPAIRED CHANNEL STIFFENER PER ACO & SRM.Dec 12, 2005 · N511SW · Boeing 7375H4SDR USAA051492Pressure Panel · crackedFOUND CRACK FUSELAGE STATION 664 LBL 30. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED A NEW STIFFENER ANGLE AND SHIMS IAW TR 53-60-04, DEFECT SIZE: 2.3"Dec 12, 2005 · N783AU · Boeing 7374B7SDR C2XA05SH136Firewall · chafedSHV - DURING C-CHECK AFT SURFACE OF FR 81 IS CHAFED IN MUTIPLE LOCATION ON LOWER EDGE. MAINTENANCE REPAIRED AFT SURFACED OF FR 81 ON LOWER EDGE IAW EMB 145 EC5310-01359. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.Dec 9, 2005 · N12946 · Emb EMB145EPSDR SWAA053913Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND BS 1016 AFT PRESSURE BLKHD DOME WEB PANEL NR 6 CRACKED AT 9 O'CLOCK POSITION. REPAIRED DOME WEB PER SWA EA.Dec 8, 2005 · N511SW · Boeing 7375H4SDR QXEA200600263Bulkhead · damagedYYC- FORWARD SIDE OF FS 1690 HAS WEAR MARKS ON LT AND RT OUTBOARD AT 3 O'CLOCK AND 9 O'CLOCK POSITIONS. BLENDED OUT DAMAGE IAW CRJ 700 SRM 53-00-00-101-001-A01 AND CRJ 700 SRM 51-12-00-001-001-A01 PARA 7B WITHIN LIMITS LPI C/O ON BLEND REPAIR AREA AS OF BULKHDec 7, 2005 · N600QX · Cndair CL6002C10SDR QXEA200600222Bulkhead · corrodedYYC - LEFT FS 286 BULKHEAD LOWER WEB HAS CORROSION ALONG THE FLOOR LINE. FUSELAGE INT LEFT FS 280 LOWER BULKHEAD CORROSION REMOVED IAW REO 670-53-11-052 REV A REPAIR NR 1 REMAINING WEB THICKNESS .037 IN AFFECTED AREA. AREA TREATED PRIMED AND PAINTED IAW SRM Dec 7, 2005 · N600QX · Cndair CL6002C10SDR QXEA200600221Bulkhead · corrodedYYC - RIGHT FS 280 BULKHEAD LOWER WEB HAS CORROSION ALONG THE FLOOR LINE FUSELAGE INT RT FS 280 BULKHEAD LOWER WEB CORROSION REMOVED IAW REO 670-53-11-052 REV A REPAIR NR 1 REMAIN INT THICKNESS .038 OVER BLENDED AREAS. AREA TREATED PRIMED AND PAINTED IAW SRM Dec 7, 2005 · N600QX · Cndair CL6002C10SDR SWAA053868Stiffener · corrodedDURING SCHEDULED D-CHECK, FOUND AFT PRESSURE BULKHEAD RADIAL STIFFENER CORRODED AT BS 1017, LBL 10. REPAIRED RADIAL STIFFENER PER BFG ER.Dec 5, 2005 · N318SW · Boeing 7373H4SDR ASOA051060Bulkhead · corrodedDURING A C-CHECK IN MCN, THE LEFT SIDE AND RIGHT SIDE FS 280 BULKHEAD WEB WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACED THE LEFT SIDE AND RIGHT SIDE FS 280 BULKHEAD WEB IAW BOMBARDIER REO 670-53-11-052. (M)Dec 3, 2005 · N716EV · Cndair CL6002C10SDR 2005UALA01388Bulkhead · tool damageSEVERAL TOOL MARKS FOUND AROUND LH UPPER WIRE BUNDLE FEED THROUGH ON FWD SIDE OF BLKHD STA 1016. MAJOR REPAIR ACP'D PER AAR EA I050299IR, EXISTING DOUBLER REMOVED, NEW DOUBLER FABRICATED AND INST'D.Dec 3, 2005 · N921UA · Boeing 737522SDR CA051208008Bulkhead · crackedWHILE TROUBLESHOOTING A PRESSURIZATION SNAG ON THE AIRCRAFT UNDERGOING MAINTENANCE AT OUR FACILITY, DISCOVERED AN APPROXIMATELY 3.5 LONG CRACK IN A SECTION OF THE BULKHEAD LOWER FLANGE ATTACHED AT THE REAR SPAR AT FS 227. THE CRACK WAS CAUSING A MAJOR PRESSURDec 2, 2005 · Beech 200BEECHSDR 05FDEA04082Repair · unknownPERFORMED INSPECTION IAW EO NR 8-5100-7-5001-1P, FOUND ANGLE LENGTH 30" ON AFT CARGO BULKHEAD PRESSURE STA 2007 X =0 Z-19. PERFORMED A GVI OF REPAIR IAW SRM 53-40-00 FIG 16 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 RESTORED PADec 2, 2005 · N302FE · Doug DC1030SDR 05FDEA04075Repair · unknownPERFORMED INSPECTION IAW EO NR 8-5100-7-5001-1P, FOUND DOUBLER LENGTH 12" WIDTH 9" ON TOP INTERNAL BULKHEAD NLG AT STA 560 Z-38 X11. NO ACTION TAKEN IAW EO NR 8-5100-7-5001 P1 E3 ATTACHMENT "A" NOTE 3 TREATED AND PRIMED AREA IAW SRM 57-21-01 VOL 1.Dec 2, 2005 · N302FE · Doug DC1030SDR CA051206004Intercostal · crackedDURING A SPECIAL INSPECTION AFTER FINDING DAMAGE ON OTHER AIRCRAFT, THE AFT PRESSURE BULKHEAD WAS FOUND CHAFED BY BOTH THE CENTER INTERCOSTAL AND THE OUTBOARD INTERCOSTAL ADJACENT TO THE TAIL ACCESS DOOR. NDT WAS COMPLETED AND A CRACK FOUND AT THE OUTBOARD LODec 1, 2005 · Beech A100SDR 0501659927Door · not seatedIN CRUISE FLIGHT AT FL270 AN AIR LEAK AT THE AFT PRESSURE BULKHEAD DOOR WAS REPORTED. THE RED "CABIN PRESS" WARNING LIGHT ILLUMINATED AS THE CABIN ALTITUDE REACHED 10,500 FEET. THE MASKS DID NOT DEPLOY. THE RED BORDER CHECKLIST AND DESCENT TO 11,000 FEET WENov 30, 2005 · N8920E · Doug DC931SDR 05FDEA04035None · noneCONFORMITY INSPECTION RECORD FOR N524FE ITEM 8, 2007 AFT PRESSURE BULKHEAD INTERNAL HAD A SPLICE REPAIR AT 6 O'CLOCK POSITION. REPAIR IS PAINTED GRAY. FOUND REPAIR CARRIED OUT IN ACCORDANCE WITH SRM 53-40-00 FIGURE 6 VOLUME I. REPAIR CLASSIFIED AS MAJOR PNov 30, 2005 · N524FE · Doug MD11SDR LR7A05204Bulkhead · crackedDURING B-2 CHECK PER HB5302, FOUND LT SIDE BULKHEAD WEB WITH 1 INCH CRACK AT FS 1012, WL270, LBL63. REPLACED WEB IAW SMP583 CH 51-60 AND 51-70, NR 2082.Nov 29, 2005 · N406LC · Lkheed 382GSDR LR7A05200Bulkhead · crackedDURING B-2 CHECK PER HB5302, FOUND RT AFT FUSELAGE BULKHEAD OUTBOARD CAP AT FS 1012, WL270, RBL63. REPLACED OUTBOARD CAP IAW SMP583 CH 51-60 AND 51-70, NR 2069.Nov 29, 2005 · N406LC · Lkheed 382GSDR LR7A05199Bulkhead · crackedDURING B-2 CHECK PER HB5302, FOUND LT AFT FUSELAGE BULKHEAD OUTBOARD CAP CRACKED AT FS1012, WL270, LBL63. REPLACED OUTBOARD CAP IAW SMP583 CH 51-60 AND 51-70, NR 2068.Nov 29, 2005 · N406LC · Lkheed 382GSDR LR7A05198Bulkhead · crackedDURING B-2 CHECK PER HB5302, FOUND LT AFT FUSELAGE BULKHEAD INNER CAP BROKEN/WEB CRACKED AT FS1012, WL265-275, LBL63. REPLACED INNER CAP AND WEB IAW SMP583 CH 51-60 & 51-70, NR 2056.Nov 29, 2005 · N406LC · Lkheed 382GSDR 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 DC941
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