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 ABXA9701813Bulkhead Web · corrodedDURING C-CHECK, FOUND CORROSION ON THE AFT PRESSURE BULKHEAD WEB FWD SIDE, LONGERON 23R TO 23L. REPAIRED AFT PRESSURE BULKHEAD WEB IAW DC9 SRM 53-03.Nov 13, 1997 · N941AX · Doug DC932SDR ABXA9701812Bulkhead Radial · crackedDURING C-CHECK, FOUND AFT PRESS BULKHEAD RADIAL AFT SIDE AT FS 996, LONGERON 25L IS CRACKED IN THE RADIUS. REPAIRED RADIAL IAW DC9 ABX SSRM DRAWING K05159.Nov 13, 1997 · N941AX · Doug DC932SDR 9723761224Blkhd T-Chord · corrodedDURING M CHECK, FOUND CORROSION T CHORD OF AFT PRESSURE BULKHEAD AT FS 2007, RBL 24. REPAIRED PER EA 12-152774.Nov 11, 1997 · N224NW · Doug DC1030SDR 97ZZZX4845Bulkhead · crackedINSPECTION REVEALED A CRACK APPROXIMATELY 1.1250 INCHES LONG ON THE LT AFT SECTION OF THE FORWARD DOOR POST. CRACK STARTS ON THE REAR HOLE OF THE LOWER DOOR HINGE ATTACHMENT. CRACK PROGRESSES EITHER SIDE FROM HOLE.Nov 10, 1997 · N734UC · Cessna 172NSDR 97ZZZX4844Bulkhead · crackedINSPECTION REVEALED A CRACK APPROXIMATELY 1.1250 INCHES LONG ON THE LT AFT SECTION OF THE FORWARD DOOR POST. CRACK STARTS ON THE REAR HOLE OF THE LOWER DOOR HINGE ATTACHMENT. CRACK PROGRESSES EITHER SIDE FROM HOLE.Nov 10, 1997 · N734UC · Cessna 172NSDR 97ZZZX4815Bulkhead · misinstalledUPON INSPECTION OF AIRCRAFT, FOUND AFT FUSELAGE BULKHEAD IMPROPERLY RIVETED. RIVET HEADS CLEARLY HAVE DENTS ALMOST LOOKING LIKE WRONG SET WAS USED TO DRIVE RIVETS. MOST OF THE UPSET ENDS WERE NOT PROPERLY BURRED. ALL RIVETS WERE REMOVED AND REPLACED AND PRONov 8, 1997 · N132Z · Beech 58PSDR UPS97425197Bulkhead Angle · crackedINSPECTION TYPE-C, FOUND CRACK AT PRESS BULKHEAD ANGLE JUST BELOW STR 5 LT BS 2360. REPLACED ANGLE AT PRESS BULKHEAD BS 2360 STR 5 LT ACC SRM 51-30-02.Nov 6, 1997 · N677UP · Boeing 747123FSDR HALA9700247Bulkhead Clip · crackedDURING C-CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD (RT SIDE) OUT BOARD LOWER CLIP CRACKED AT LONGERON 14. REMOVED DAMAGED MATERIAL, VERIFIED DAMAGE CONTAINMENT BY HFEC, FABRICATED AND INSTALLED AND END CLIPS AND RADIUS BLOCKS PER DAC REPAIR DWG JO60110. Nov 5, 1997 · N661HA · Doug DC951SDR 97ZZZX4989Stiffener · corrodedDURING C-CHECK, CORROSION NOTED ON FORWARD FACE 1183 BULKHEAD STIFFENER, LOWER SECTION, AT RBL 18.Nov 1, 1997 · N352PA · Boeing 727225SDR 97ZZZX4988Stiffener · corrodedDURING C-CHECK, CORROSION NOTED ON STIFFENER FORWARD FACE BOTTOM OF BULKHEAD 1183 AT LBL 18.Nov 1, 1997 · N352PA · Boeing 727225SDR UPS97425281Bulkhead Doubler · misinstalledINSPECTION TYPE-C, FOUND DOUBLER INSTALLED ON AFT PRESSURE BULKHEAD WHO HAS INTERFERENCE WITH EO B747-5310-1332-C APU CUTOUT REINFORCEMENT. REPAIRED PRESSURE BULKHEAD AT BS 2360 ACC EFN 747-53-0849 (KLM DFX 97-270).Oct 30, 1997 · N677UP · Boeing 747123FSDR CALA9701524Bulkhead · holeINSPECTION FOUND A .5625 DIAMETER HOLE IN AFT PRESSURE BULKHEAD BETWEEN FLOOR SUPPORT BEAM AND LONGERON 41L AT STA 2007. REPAIRED IAW SRM 53-40-00.Oct 30, 1997 · N12064 · Doug DC1030SDR 97ZZZX4760Bulkhead · crackedINSPECTION REVEALED A CRACK IN THE LOWER DOOR HINGE LOCATION ON THE LEFT HAND DOORPOST. CRACK WAS APPROXIMATELY 1.6250 INCHES LONG. CRACK ORIGINATES AT AFT HINGE ATTACH HOLE AND PROGRESSES IN EITHER DIRECTION. DOORPOST WAS REPLACED.Oct 30, 1997 · N734EQ · Cessna 172NSDR 97ZZZX4759Bulkhead · crackedDURING TROUBLESHOOTING ON THE LEFT HAND DOOR HOLD OPEN STOP, NOTICED WHEN THE DOOR WAS OPENED AGAINST THE STOP, THE BOTTOM FUSELAGE DOOR HINGE ATTACHMENT MOVED. FURTHER INSPECTION REVEALED A CRACK IN THE AFT FORWARD DOORPOST APPROXIMATELY 2.75 INCHES LONG NECOct 30, 1997 · N734FX · Cessna 172NSDR 97ZZZX4756Bulkhead · crackedINSPECTION REVEALED A CRACK IN THE LOWER HINGE LOCATION ON THE LEFT HAND DOORPOST. CRACK WAS APPROXIMATELY 1.25 INCHES LONG. DOORPOST WAS REPLACED. NOTE: CRACK ORIGINATES AT AFT HINGE ATTACH HOLE AND PROGRESSES IN EITHER DIRECTION.Oct 30, 1997 · N733JS · Cessna 172NSDR CALA9701515Stiffener · crackedINSPECTION FOUND A 2 CRACK IN HORIZONTAL STIFFENER ON FORWARD FACE OF AFT PRESSURE BULKHEAD AT L13R. THE STIFFENER WAS REMOVED. NEW PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-30-5.Oct 29, 1997 · N14524 · Doug DC932SDR ABXA9701750Bulkhead Gusset · corrodedDURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD DOOR JAMB LOWER LEFT GUSSET CORRODED. REPLACED GUSSET IAW DC9 SRM 51-30-1 AND 51-30-5.Oct 29, 1997 · N987AX · Doug DC932SDR AALA972030Bulkhead Web · corrodedTUL - FOUND CORROSION UNDER STIFFENER ON 1183 BULKHEAD RBL 18 INCHES, 22 INCHES UP. REPAIRED WEB WITH DOUBLER SRM PER 53-10-9, PAGE 11 FIG 4. (M)Oct 28, 1997 · N730AA · Boeing 727227SDR USAA970308Skin · chafedPIT - DURING C-3 CHECK, FOUND 1 INCH LONG BY .029 INCH DEEP CHAF IN SKIN AT LEFT AFT SIDE OF REAR PRESS BULKHEAD JUST BELOW RADIAL 12. INSTALLED DOUBLERS PER EA 33652A. (M)Oct 27, 1997 · N931VJ · Doug DC931SDR DL72S972206Bulkhead Beam · crackedA CRACK WAS FOUND IN THE VERTICAL STIFFENER AT LBL 36.83 ON THE FWD SIDE OF THE BS 1183 BULKHEAD. THE CRACK IS APPROX 1 LONG AND IS LOCATED AT APPROX WL237 IN THE INBD RADIUS OF THE AFT CHORD. REPAIRED PER ERA 330932-14.Oct 27, 1997 · N518DA · Boeing 727232SDR 97UAL900802Bulkhead Angle · crackedAT STA Y=1156, TWO CRACKS WERE FOUND IN THE NYB6042-5 FWD PRESSURE BLKHD ANGLE. ONE CRACK IS AT X=+5.54 AND MEASURES APPROX. 1.2 INCHES. SECOND CRACK IS BETWEEN X=-5.54 AND X=-9.9 AND EXTENDED FROM UNDER AN EXISTING REPAIR DOUBLER. DOUBLER WAS REMOVED AND COct 27, 1997 · N1845U · Doug DC1010SDR WRLA97122Bulkhead · corrodedDURING SCHEDULED MAINTENANCE (B-CHECK), MAINTENANCE CONTRACTOR IDENTIFIED CORROSION ON THE AFT FUSELAGE PRESSURE BULKHEAD GALLEY SUPPORT ATTACH 'TEE', AT STA 2007, LBL 60. MAINTENANCE CONTRACTOR REPLACED CORRODED SUPPORT ATTACH 'TEE' PER SRM 53-40-00. AIRCRAOct 25, 1997 · N9MMAZ · Doug DC1030SDR UPS97824892Bkhd Intercostal · crackedINSPECTION TYPE-C, INTERCOSTAL HAS CORROSION AND IS CRACKED FS 70 BLKHD AFT SIDE RBL 20 TO RBL 35. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-1-21 AND DWG 5613064.Oct 25, 1997 · N801UP · Doug DC873FSDR DLL10972187Bulkhead · crackedFUSELAGE BULKHEAD FS 1363, LBL 80 REPAIR FOR CRACK IN LOWER CAP AND WEB. ONE INCH CRACK FOUND IN THE CAP AT LBL90. CAP FOUND SEVERED AT LBL78. 2.5 INCH CRACK FOUND IN WEB AT LBL 78. NEW SECTION OF CAP SPLICED IN AND WEB DOUBLER INSTALLED PER ER/A 363034-14Oct 24, 1997 · N716DA · Lkheed 10113851SDR AWXA9700626Bulkhead · crackedDURING SCHEDULED C-6 INSPECTION, FOUND POSSIBLE CRACK AT FASTENER AT BS 178, LBL 15, WL 184. REPAIRED BS 178 BULKHEAD LBL 15, WL 184, PER ER 3-53-12-21.Oct 24, 1997 · N328AW · Boeing 7373B7SDR VJ970332Bulkhead · damagedLEFT STATION 1038 FRAME IS CHAFFED. BLENDED CHAFFED AREA ON LEFT 1038 FRAME CAP NR 9912246-5 IAW DC-9 SRM 53-01 FIG 1 SHT 1. DIMENSIONS AS IS 2.50 INCH BY .375 INCH WITH .100 MATERIAL REMAINING MIN, BLEND WITHIN LIMITS IAW DC-9 SRM 53-01 FIG 1. (M)Oct 23, 1997 · N910VJ · Doug DC932SDR SWAA970937Bulkhead · crackedDURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 188, WL 197 TO 201.75, 197.25 TO 201.25, 208.25 TO 208.75, AND AT 211.25 TO 210.75. REPAIRED PER BOEING SRM.Oct 23, 1997 · N329SW · Boeing 7373H4SDR VJ9800018Bulkhead Angle · corrodedDURING C CHECK, FOUND CORROSION ALONG AFT PRESSURE BULKHEAD LOWER ATTACH ANGLE BL20 LT TO BL20 RT, AFT PIT. REMOVED LOWER T-CAP FROM BL20 LT TO BL20 RT, DRILLED NEW SECTION OF CAP, FABRICATED SPLICE DOUBLERS AND INSTALLED IAW DC9 SRM 53-04, FIG 9 , AND DAC FAOct 22, 1997 · N906VJ · Doug DC932SDR 9721299970Blkhd Doubler · crackedDURING L-CHECK, FOUND A CRACK IN THE -85 DOUBLER ON THE AFT PRESSURE BULKHEAD. REPAIRED PER EA 99-151775.Oct 22, 1997 · N9334 · Doug DC931SDR UPS97225116Blkhd Stiffner · chafedINSPECTION TYPE-D, HYD LINE FROM A-SYSTEM MODULE HAS CHAFED REAR PRESSURE BULKHEAD BS 1183 HORIZONTAL STIFFENER AT WL 208 LBL 30 APPROX. REPAIRED IAW SRS EO 97-34-011 UPS ENG FILE NUMBER 727-53-1974.Oct 20, 1997 · N921UP · Boeing 727180CSDR AU971356Bulkhead · cracked(AUS) FUSELAGE FORWARD PRESSURE BULKHEAD CRACKED IN ELEVEN LOCATIONS.Oct 19, 1997 · Boeing 737376SDR DLL19972198Bulkhead Web · corrodedFUSELAGE BULKHEAD FS 328 LBL 15 WL 127 REPAIR FOR CORROSION CUT OUT IN WEB. THE FS 328 NLG WHEEL WELL PRESSURE BULKHEAD WAS FOUND CORRODED AT WL 127, LBL 15. THE CORROSION REMOVAL RESULTED IN A 2.8 BY 1.6 RECTANGULAR CUT OUT IN THE WEB. A DOUBLER REPAIR WAS Oct 17, 1997 · N762DA · Lkheed 10113853SDR CALA9701484Bulkhead Web · corrodedINSPECTION FOUND CORROSION ON LOWER BULKHEAD WEB AT STA 996 FROM LONGERON 24L TO 25L. A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.Oct 17, 1997 · N12539 · Doug DC932SDR CALA9701483Bulkhead Web · corrodedINSPECTION FOUND AFT PRESSURE BULKHEAD WEB CORRODED AT STA 996, LONGERON 24L AND 25L. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 24.Oct 17, 1997 · N12539 · Doug DC932SDR AU971371Bulkhead · cracked(AUS) FORWARD DOOR POST BULKHEAD CRACKED IN RELIEF NOTCH ON LH SIDE.AIRCRAFT IS USED FOR PARACHUTING OPERATIONS.Oct 17, 1997 · Cessna 182PSDR AU971358Bulkhead · cracked(AUS) FUSELAGE FORWARD PRESSURE BULKHEAD CONTAINED THREE CHORD CRACKS AND SEVEN WEB CRACKSOct 17, 1997 · Boeing 737376SDR ABXA9701702Bulkhead Angle · crackedDURING C-CHECK, FOUND ANGLE ON THE AFT SIDE OF THE AFT PRESSURE BULKHEAD WAS FOUND CRACKED. THE ANGLE WAS REPLACED IAW DC-9 SRM.Oct 17, 1997 · N936AX · Doug DC931SDR UPS97824919Bulkhead · crackedINSPECTION TYPE-C, FS 680 PRESURE BULKHEAD HAS 8 INCH CRACK AT LOWER SPAR CHORD LBL 4 TO 12 AND 5 CRACK RBL 13 TO 18. REPAIRED IAW SRM 53-2-5, 51-1-21, AND 51-1-20D.Oct 15, 1997 · N801UP · Doug DC873FSDR UPS97824876Bulkhead Fitting · crackedINSPECTION TYPE-C, LONGERON 30R END FITTING AFT OF STA 8 BULKHEAD CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20 AND DWG 4641703.Oct 15, 1997 · N801UP · Doug DC873FSDR DL72W972117Bulkhead Web · crackedDURING INPSECTION OF STA 1183 BULKHEAD PER SPECIAL INSPECTION 4-69150-12, A CRACK WAS DISCOVERED JUST BELOW A STIFFENER AT LBL 30, WL 188 IN THE WEB. THE CRACK MEASURED 2.5 INCHES. THE WEB MATERIAL IS .050 2024-T3 CLAD. THE -12 SPECIAL INSPECTION CALLS FOR Oct 15, 1997 · N2817W · Boeing 727247SDR CALA9701438Bulkhead Tee · crackedAFT PRESSURE BULKEAD LOWER TEE CAP AT LONG 30 HAS BULGED SKIN UNDER BOLT HEADS STA 996. CUT OUT DAMAGED AREA OF SKIN. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-03 FIG 9. REPAIRED TEE CAP CRACKS BY CUTTING OUT DAMAGED AREA AND INSTALLING A REPAIR STROct 15, 1997 · N12539 · Doug DC932SDR 97FDEA00743Bulkhead Web · crackedNR 0392 004, WHILE WORKING (NR 0246) FOUND CRACK IN 740 BULKHEAD WEB AT BLO, WL 168 AND CORROSION AT LBL 6, WL 170 AND AT RBL 1 AND 2 WL 170.Oct 15, 1997 · N104FE · Boeing 72722CSDR DLL10972115Bulkhead Panel · crackedTHE FUSELAGE 1212 BULKHEAD PANEL WAS FOUND WITH A TYPICAL VERTICAL CRACK AS ADDRESSED BY LAC S/B 093-53-277. THE CRACK IN THIS CASE IS LOCATED AT RBL 6 AND IS APPROX 1.5 LONG. UPON REMOVAL OF THE CRACK, A SHORT FASTENER EDGE DISTANCE CONDITION RESULTED, REQUOct 14, 1997 · N719DA · Lkheed 10113851SDR 97FDEA00734Bulkhead Web · corrodedBS 1342 BULKHEAD CENTER WEB LT SIDE UPPER HAS ELONGATED AND WORN BOLT HOLES AND BOLT HOLE AREAS CORRODED. REPLACED LEFT UPPER SECTION PER SRM 51-10-1.Oct 14, 1997 · N465FE · Boeing 727225SDR 97FDEA00733Bulkhead Web · corrodedBS 1342 BULKHEAD CENTER WEB RT SIDE UPPER HAS ELONGATED AND WORN BOLT HOLES AND CORROSION IN BOLT HOLE AREAS. REMOVED AND REPLACED WEB SEGMENT PER SRM 51-10-1.Oct 14, 1997 · N465FE · Boeing 727225SDR CKSA97555Bulkhead · crackedDURING ROUTINE CPCP INSPECTION, FOUND FWD BULKHEAD CRACKED AROUND RIVETHEAD. INSTALLED REPAIR IAW B727 SRM 53-10-9 FIG 4. CORROSION TASK CARD NUMBER C53-100-01 PART 4 OF 6. NON-ROUTINE TASK CARD NUMBER 003115.Oct 13, 1997 · N729CK · Boeing 727223SDR CKSA97550Bulkhead · crackedDURING ROUTINE CPCP INSPECTION, FOUND 2 CRACKS FROM RIVET HOLES ON FWD FUSELAGE BULKHEAD 6 TO 8 DOWN AND 12 TO 18 FROM RIGHT SIDE. INSTALLED REPAIR DOUBLER IAW SB 727-53146. CORROSION TASK CARD NUMBER C53-100-01 PART 4 OF 6. NON-ROUTINE TASK CARD NUMBER 003Oct 13, 1997 · N729CK · Boeing 727223SDR ABXA9701678Blkhd Fitting · crackedDURING C-CHECK, FOUND FITTING CRACKED AT AFT PRESSURE BULKHEAD DOOR JAMB (RT SIDE BETWEEN 1ST AND 2ND RADIAL STIFFENER). REPLACED FITTING IAW DC9 SRM 51-30-2.Oct 13, 1997 · N954AX · Doug DC941SDR 9724986615Bulkhead · crackedDURING ARMAR, FOUND CRACK IN OUTER RING AT BULKHEAD AT FS 140. REPAIRED PER EA 66-152946.Oct 13, 1997 · N615US · Boeing 747251BSDR UPS97825081Bulkhead Tee · corrodedINSPECTION TYPE-D, FOUND CORROSION ON T FWD SIDE OF VERTICAL BEAM ON AFT PRESSURE BULKHEAD AT BOTTOM. REMOVED CORROSION FROM T-CAP, FABRICATED REPAIR ANGLE, TREATED, PRIMED AND INSTALLED IAW DACO FAX FILE 97-10-20-001, SK97725 AND DC8 SRM 51-1-8, 51-1-21, 51-Oct 11, 1997 · N805UP · Doug DC873F
Back to JASC 5312