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 SWAA060477Bulkhead · corrodedDURING SCHEDULED 1/4D CHECK, FOUND BS 1016 AFT PRESSURE BULKHEAD WEB CORRODED ON RT FWD LOWER SIDE OF BL 0. REPAIRED WEB PER BAC DRAWING & SWA EA.Feb 8, 2006 · N310SW · Boeing 7373H4SDR UPS06146188Bracket · crackedINSPECTION TYPE:5YR AFT CARGO FWD BULKHEAD CENTER SUPPORT BRACKET CRACKED. REMOVED AND REPLACED SUPPORT BRACKET PER A300 SRM 51-40-21 AND 51-40-00.Feb 7, 2006 · N128UP · Airbus A300F4622RSDR 2006UALA00242Bulkhead · damagedAFT CARGO PIT FWD BULKHEAD STA 727 STRINGER 27R FWD ATTACHMENT FASTENERS 3RD AND 4TH FROM BOTTOM ARE WORKING. INSTALLED NEW STA 727 BULKHEAD FITTING AT STR 27R REF SRM 51-40-02.Feb 7, 2006 · N338UA · Boeing 737322SDR UPS06446224Bulkhead · crackedINSPECTION TYPE:C EMP - BS 2658 FIREWALL BULKHEAD FORWARD SIDE WL 350 RBL 10 FOUND CRACKED, CRACK LENGTH .875 INCH. BS 2658 BULKHEAD WL 350 RBL 10" FWD SIDE AREA REPAIRED AS PER SRM 53-10-04 FIG 30.Feb 5, 2006 · N522UP · Boeing 747200SDR 2006UALA00197Bulkhead · crackedFWD SIDE OF 1016 BULKHEAD FOUND 3 EACH CRACKS AT FASTENERS IN WEB ABOVE STIFFENER 7L RIVETS 7, 8, AND 9. *S/D* REMOVED DAMAGE INSTALLED FILLER, DOUBLER, TRIPLER SEALED EDGES, & DINOLED REF SRM 53-80-08.Feb 4, 2006 · N338UA · Boeing 737322SDR AWXA200600456Bulkhead · corrodedSAL - DURING C11 CHECK DISCOVERED LEVEL 2 CORROSION LOCATED ON WEB AT BS 1714, PRESSURE BULKHEAD, AT BL 25L UNDER AFT GALLEY AREA. CORROSION WAS FOUND TO BE OUT OF SRM LIMITS. MAINTENANCE FABRICATED AND INSTALLED REPAIR WEB AT BS 1714, PRESSURE BULKHEAD, AT Feb 2, 2006 · N913AW · Boeing 757225SDR ABXA060098Pressure Panel · corroded3 RIVET HEADS WERE SHEARED AND METAL WAS BULGING UNDER REINFORCEMENT STRAP, UPPER SURFACE OF RIGHT MAIN LANDING GEAR WHEEL WELL FORWARD OUTBOARD CORNER JUST OUTBOARD OF CEILING SERVICE LIGHT. WEB OUT OF LIMITS AFTER CORROSION REMOVAL MATERIAL LOSS 35%. REMOVFeb 2, 2006 · N842AX · Doug DC861SDR SWAA060394Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BLKHD WEB CRACKED BETWEEN LBL 15 TO RBL 10, WL 218. REPAIRED WEB PER SRM.Feb 2, 2006 · N362SW · Boeing 7373H4SDR 06FDEA0490Bulkhead · gougedBS 178 BULKHEAD FWD SURFACE, GOUGES JUST INBOARD OF NR 4 RADOME ALIGNMENT AND ATTACH PAD. REPAIRED BS 178 BULKHEAD IAW MM 51-20-0007.Feb 1, 2006 · N492FE · Boeing 727200SDR 06FDEA0489Bulkhead · gougedBS 178 BULKHEAD FWD SURFACE, GOUGES JUST INBOARD OF NR 2 RADOME ALIGNMENT AND ATTACH PAD. REPAIRED BS 178 BULKHEAD FWD SURFACE IAW SRM 53-10-1.Feb 1, 2006 · N492FE · Boeing 727200SDR 06FDEA0488Bulkhead · gougedBS 178 BULKHEAD FWD SURFACE, GOUGES JUST INBOARD OF NR 3 RADOME ALIGNMENT AND ATTACH PAD. REPAIRED BS 178 BULKHEAD IAW MM 51-20-0007.Feb 1, 2006 · N492FE · Boeing 727200SDR AMTA200600106Pressure Panel · corrodedNLG COMPT PRESS DECK FOUND WITH CORROSION BETWEEN FS 349-36 LBL 29-31. FORWARD PRESSURE DECK CORROSION DAMAGE BEYOND SRM 53-11-00 FIG 6 LIMITS. REPAIRED DAMAGED AREA IAW EER L1-53-00-00-11447 AND LOCKHEED DWG LCC-7622-500 REV A. CLEANED, PRIMED AND TREATED Jan 31, 2006 · N162AT · Lkheed 10113853SDR SWAA060381Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 1016 BLKHD WEB CRACKED NEXT TO DOME CAP AT STR 15L, STR 18R AND STR 21R. REPAIRED WEB PER SRM.Jan 31, 2006 · N310SW · Boeing 7373H4SDR DL73S060092Stiffener · corrodedCORROSION FOUND ON THE BS 1016 AFT PRESSURE BULKHEAD Z-STIFFENER AT STR 26R. REMOVED CORROSION, DAMAGE WITHIN ALLOWABLE LIMITS WITHOUT REINFORCEMENT. REF AD 2002-10-11, SB 737-53A-1075.Jan 30, 2006 · N319DL · Boeing 737232SDR C2XA06SH011Skin · dentedSHV - DURING C-CHECK THE SKIN UNDER THE RADAR ALTIMETER ANTENNA MOUNT WAS FOUND TO BE DIMPLED OUTWARD WITH AN EXTERNAL DENT OUTWARD. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC5330-01540. THE AIRCRAFT WAS APPROVED FOR RETURN TOJan 30, 2006 · N12921 · Emb EMB145LRSDR C1HA200682004Vertical Beam · crackedSTA 1183 BULKHEAD, VERTICAL BEAM AT LBL 36.83 IS CRACKED AT AFT RADIUS INBOARD SIDE AT WL 230. STOP DRILLED CRACK & INSTALLED REPAIR KIT P/N 65C34406-14, PER S/B 727-53-0192 FIG 2 REV 1 DATED MAY 30/91.Jan 30, 2006 · N682CA · Boeing 7272S7SDR SWIA200616360Bulkhead · crackedAFT SIDE AFT PRESSURE BULKHEAD RIGHT SIDE AT STR 13; CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CRACKED CLIP PER CRJ200 SRM 51-42-21.Jan 26, 2006 · N929SW · Cndair CL6002B19SDR EIA2006014Panel · crackedNOSE LANDING GEAR WHEEL WELL TOP PANEL FOUND CRACKED AT BS 320, RBL 20 AND BS 270, LBL 20. REPAIR DOUBLERS INSTALLED PER HAECO REPAIR SCHEME, R-53-00-35423, AND EIA ECRA 485-53-179-1.Jan 25, 2006 · N485EV · Boeing 747212BSDR 2006UALA00139Bulkhead · crackedCRACKS FOUND BETWEEN S3L-S5L AND S5L-S7L STA 1016 AFT BULKHEAD WEB. REMOVED CRACKS, ACCOMPLISHED DOUBLER, TRIPLER, AND TRIPLER FILLER REPAIR PER SRM 53-80-08 REPAIR 7 .Jan 25, 2006 · N337UA · Boeing 737322SDR AWXA200600431Bulkhead · crackedDURING C19 CHECK DISCOVERED BULKHEAD CRACKED, 1.6 INCHES IN LENGTH, AT BS 178, WL 207 AND FROM BL 1L TO BL 1R. MX CUT OUT DAMAGED SECTION OF BULKHEAD IAW BOEING 737-300 SRM 53-10-08-2R11. FABRICATED DOUBLER AND 4 FILLERS IAW BOEING 737-300 SRM 53-10-08-2R11.Jan 21, 2006 · N166AW · Boeing 73733ASDR UPS06846081Fitting · crackedINSPECTION TYPE:C3 STA 680 BETWEEN LONG 36 AND 35L AFT SIDE OF BULKHEAD FOUND CRACKED FITTING, VIEWED THROUGH STRESS PANEL OPENING. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND 21-1-20D.Jan 21, 2006 · N718UP · Doug DC871FSDR UPS06846080Fitting · crackedINSPECTION TYPE:C3 STA 680 BETWEEN LONGERON 36 AND 35R AFT SIDE OF BULKHEAD FOUND CRACKED FITTING, VIEWED THROUGH STRESS PANEL OPENING. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND 51-1-20D.Jan 21, 2006 · N718UP · Doug DC871FSDR SWIA200616435Bulkhead · crackedAFT PRESSURE BULKHEAD WEB FS 621 LBL 27.5 WL 130 CRACKED ITEM FOUND AT C CHECK INSPECTION. REPAIRED WEB IAW CRJ REO 601R-53-61-1541.Jan 19, 2006 · N429SW · Cndair CL6002B19SDR WRNA200600020Bulkhead · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE FORWARD SIDE OF THE FORWARD PRESSURE BULKHEAD AT -Z180 AND +Y1000. REPAIR WAS ACCOMPLISHED PER AVBORNE REPAIR REF: 25599-10-01-25-06, (AIRBUS TECHNICAL DISPOSITION 942.042586/004/2006) SMOOTH REWORK OF CORRODED ARJan 18, 2006 · N821SC · Airbus A300B4203SDR AWXA200600259Bulkhead · crackedMCN - DURING C19 CHECK DISCOVERED LT BS 178 BULKHEAD WEB CRACKED AROUND 3 FASTENERS, 1 INCH, AT WL 234 FROM BL 6.5L TO BL 17L. MAINTENANCE CUT OUT DAMAGED AREA OF WEB IAW BOEING 737-300 SRM 53-10-08-2R9. PERFORMED HFEC INSPECTION, NO CRACKS FOUND. FABRICATEJan 18, 2006 · N166AW · Boeing 73733ASDR ABXA060068Splice · corrodedFOUND LONGERON 23 LEFT AT P DOME SPLICE HAD CORROSION ON OUTBOARD FLANGE. REMOVED AND REPLACED LONGERON SECTION IAW DC9 SRM 53-02.Jan 18, 2006 · N908AX · Doug DC931SDR ABXA060067Bulkhead · corrodedAFT LOWER CARGO BULKHEAD WEB, STA 996 LEFT, CORRODED AT NUMEROUS AREAS. REMOVED AND REPLACED WEB IAW DC9 SRM 53-11-3.Jan 18, 2006 · N908AX · Doug DC931SDR ABXA060070Bulkhead · corrodedAFT PRESSURE BULKHEAD LOWER WEB HAD SURFACE CORROSION ON FORWARD AND AFT SIDE LONGERON 23 RIGHT TO 23 LEFT IN TEE CAP AREA. REPAIRED AFT PRESSURE BULKHEAD WEB IAW DC9 SRM 53-05.Jan 18, 2006 · N908AX · Doug DC931SDR 06FDEA0253Bulkhead · wornAIR CONDITIONING COMPT LT FOUND DEEP WEAR ON VERTICAL BULKHEAD STIFFENER AT STA 575 X 24 LT SIDE. BLENDED OUT WEAR IAW SRM 51-21-01 PART 34 VOL 2. MATERIAL REMOVED IS OUT OF LIMITS IAW SRM 53-00-01 FIG 1B VOL 1 AND SRM 53-12-01 FIG 15 ITEM 9 VOL 3. PERFORMEJan 18, 2006 · N68054 · Doug DC1010SDR 06FDEA0252Bulkhead · crackedAIR CONDITIONING COMPT LT FOUND CRACK 2 INCHES LONG ON VERTICAL BULKHEAD AT STA 575 X24 LT SIDE. TRIMMED OUT CRACK AND PERFORMED REPAIR IAW SRM 53-30-00 FIG 6 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F166291/N00291 AND IAW SRM 53-30-00 FIG 6 VOL 1.Jan 18, 2006 · N68054 · Doug DC1010SDR ABXA060066Bulkhead · crackedFORMER ON AFT PRESSURE BULKHEAD STA. Z74 RIGHT CRACKED. REMOVED AND REPLACED FORMER IAW DC9 SRM 51-30-2.Jan 17, 2006 · N908AX · Doug DC931SDR AWXA200600392Bulkhead · canningMCN - DURING C24 CHECK, DISCOVERED THE AFT PRESSURE BULKHEAD OIL CANNING JUST ABOVE STR 24L AT BS 1016, END FITTING BELOW APU DUCT. MAINTENANCE FABRICATED REPAIR CHANNEL, FILLER AND STRAP IAW BOEING 737-300S RM 53-80-08-2RF FIG 201. INSTALLED FABRICATED REPAJan 15, 2006 · N328AW · Boeing 7373B7SDR ABXA060065Structure · gougedAFT PRESSURE BULKHEAD 'T' CAP WAS GOUGED ABOUT 3/8" BELOW SKIN JUST TO THE RIGHT OF CENTER AT BOTTOM. NR 4 TEE CAP REMOVED AND REPLACED ON JC EA 53120035-006.Jan 13, 2006 · N908AX · Doug DC931SDR ABXA060063Repair · crackedAFT PRESSURE BULKHEAD LEFT UPPER CORNER 5910130-13 DOUBLER (ORIGINAL OEM) CRACKED FROM LEFT EOP. REPAIRED CORNER IAW REA D953-53106-MR.Jan 12, 2006 · N908AX · Doug DC931SDR ABXA060061Repair · crackedAFT PRESSURE BULKHEAD LEFT DOOR JAMB CORNER REPAIR DOUBLER CRACKED. REMOVED AND REPLACED DOUBLER IAW DC9 SRM.Jan 12, 2006 · N908AX · Doug DC931SDR K11A2008122472303Angle · corrodedCORROSION ON BULKHEAD LOWER CHORD ANGLE.Jan 11, 2006 · N723CK · Boeing 7272H3SDR 06FDEA0150Bulkhead · crackedRIGHT HAND MLG BAY BS 870 BULKHEAD IS CRACKED AT APU LOAD CONTROL VALVE AND DUCT PENETRATION. REPAIRED CRACK IAW EA 7-5310-96606.Jan 11, 2006 · N492FE · Boeing 727200SDR SWAA060123Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND VERTICAL BEAM WEB CRACKED AT BS 178 BLKHD, RBL 5.7, WL 184. REPAIRED WEB PER SRM.Jan 10, 2006 · N692SW · Boeing 7373T5SDR SWAA060120Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 1016 AFT PRESSURE BLKHD WEB CRACKED AT DOME CAP, 12 O'CLOCK POSITION. REPAIRED WEB PER SWA EA.Jan 10, 2006 · N673AA · Boeing 7373A4SDR 06FDEA0095Bulkhead · crackedNLG WHEEL WELL FOUND 2 CRACKS 4" LONG ON LT INTERNAL BULKHEAD AT STA 580 Z-43.5. TRIMMED OUT CRACK FABRICATED FILLER, 2 DOUBLERS AND INSTALLED (INTERNAL NLG) IAW SRM 53-30-00 FIG 6. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I010386/N00386-5, N00386-7, N0038Jan 9, 2006 · N563FE · Doug DC1010SDR 0601029Fitting · corrodedREPLACED FUSELAGE BULKHEAD LEFT FITTING DUE TO CORROSION. ALSO REPAIRED FUSELAGE SKIN AND DOUBLER DUE TO CRACK.Jan 6, 2006 · N767TW · Boeing 737230CSDR 0601028Stiffener · corrodedREPAIRED -579 STIFFENER AND PERFORMED BLEND OUT IN THE AFT PRESSURE BULKHEAD "Y" CHORD DUE TO CORROSION. REPAIRED AFT PRESSURE BULKHEAD WEB AND RADIAL STIFFENER AND REPAIRED FUSELAGE SKIN DUE TO ACCESS TO REPAIR AREA.Jan 6, 2006 · N767TW · Boeing 737230CSDR 0601037Bulkhead · crackedREPAIRED FUSELAGE AFT PRESSURE BULKHEAD WEB DUE TO CRACK.Jan 6, 2006 · N767TW · Boeing 737230CSDR ASOA06012Bulkhead · crackedDURING A C-CHECK, THE FS 280 BULKHEAD, OB OF LBL 9 AND RBL 9, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FS 280 BULKHEAD, OB OF LBL9 AND RBL 9, IAW EO 600-53-O123. (K)Jan 5, 2006 · N844AS · Cndair CL6002B19SDR ASOA06010SBulkhead · crackedDURING C-CHECK, THE FORWARD PRESSURE BULKHEAD, AT FS 202.75, AROUND THE BRAKE CABLE, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FORWARD PRESSURE BULKHEAD, AT FS 202.75, AROUND THE BRAKE CABLE, IAW REO. (K)Jan 4, 2006 · N844AS · Cndair CL6002B19SDR ASOA06010Bulkhead · crackedDURING A C-CHECK, THE FORWARD PRESSURE BULKHEAD, AT FS 202.75, AROUND THE BRAKE CABLE, WAS FOUND TO BE CRACKED BEYOND LIMITS. THE MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (K)Jan 4, 2006 · N844AS · Cndair CL6002B19SDR CA060321016Bulkhead · crackedTHE FOLLOWING FLOOR SUPPORTING STRUCTURE WAS FOUND TO BE UNSERVICEABLE IN THE CABIN AREA PN NR C3FS34-13 BULKHEAD LOWER STATION 133.33, C3FS13-27 BULKHEAD LOWER STATION 153.77, C3FS51-27 BULKHEAD LOWER STATION 174.2, C3FS58-15 BULKHEAD LOWER STATION 194.00 REPJan 3, 2006 · Dhav DHC3SDR SWAA060041Pressure Panel · crackedDURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE BEADED PRESSURE WEB CRACKED BETWEEN BS 663 TO BS 665, LBL 43. REPAIRED WEB PER SWA EA.Jan 3, 2006 · N688SW · Boeing 7373Q8SDR GUU2006F00008Pressure Panel · crackedSEVERAL SMALL CRACKS IN NOSE WHEEL WELL CEILING FROM NOSE WHEEL TIRE IMPACT DUE TO NOSE UP LANDING. DAMAGE LOCATION AT FUSELAGE STA 81, WATER LINE 100.00 AT CENTER BUTT LINE. REMOVED DAMAGE AREA AND INSTALLED EXTERNAL DOUBLER IAW MM. (K)Jan 1, 2006 · N53545 · Beech 1900DSDR UPS06445971Pressure Blkhd · crackedINSPECTION TYPE:C NOSE W/W BS 400 BULKHEAD PRESSURE PANEL FOUND CRACKED, CRACK LENGTH 1/4". NOSE W/W BS 400 B/H PRESSURE PANEL REPLACED AS PER SRM 51-10-01 PAGE 9 AND INSTALLED AS PER BOEING DWG NR 624U0005 SHT 1 AND SHT 9.Dec 29, 2005 · N520UP · Boeing 747212B
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