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 COMA9960295Bulkhead Angle · crackedANGLE BRACKET ON REAR PRESSURE BULKHEAD, LEFT AFT SIDE IS CRACKED. REPLACED ANGLE BRACKET.Jun 12, 1999 · N946CA · Cndair CL6002B19SDR COMA9960294Bukkhead Angle · crackedANGLE BRACKET ON REAR PRESSURE BULKHEAD RIGHT AFT SIDE IS CRACKED. REPLACED ANGLE BRACKET.Jun 12, 1999 · N946CA · Cndair CL6002B19SDR DLL10991324Bulkhead Cap · crackedFS 1363 BLKHD CAP WAS FOUND CRACKED IN THE TYPICAL MANNER. REPAIRED PER ERA 367570-14AD.Jun 11, 1999 · N727DA · Lkheed 10113851SDR ABXA9900439Bulkhead Jamb · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD VENTRAL DOOR JAMB CRACKED AT STATION 1072 LEFT SIDE. REPAIRED IAW ABX REA D953-31706MR.Jun 11, 1999 · N954AX · Doug DC941SDR SWAA990997Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND LT AND RT SIDE BULKHEAD CRACKED, BS 178, BL 1, WL 189. REPAIRED BULKHEAD PER SRM.Jun 10, 1999 · N310SW · Boeing 7373H4SDR SWAA990996Bulkhead Chord · crackedDURING SCHEDULED 1/2D CHECK, FOUND LT AND RT SIDE CHORDS CRACKED, BS 178, BL 26, WL 207. REMOVED AND REPLACED CHORDS PER SRM.Jun 10, 1999 · N310SW · Boeing 7373H4SDR GTIA9901052Bulkhead Angle · corrodedMHV - T-ANGLE ON BULKHEAD AT FS 1127 RUNNING FROM LONG L6 AND R6 HAS 3 GROUND OUT AREAS AND CORROSION IN EACH AREA. REMOVED AND REPLACED T-ANGLE PER SRM 51-10-1 AND 51-30-5 AND 51-30-2. (M)Jun 10, 1999 · N130NK · Doug DC941SDR GTIA9901051Bulkhead T · corrodedMHV - T-EXTRUSION AT FS 1127 BULKHEAD IS CORRODED BEYOND USE. MACHINED T-EXTRUSION PER DC9 SRM 51-10 AND EXAMPLE ISSUED TO FLOOR IN BLANK CONDITION LOCATED AND DRILL REF A096S03L053. (M)Jun 10, 1999 · N130NK · Doug DC941SDR GTIA9901047Bulkhead Doubler · crackedMHV - STATION 1219-1244 FORWARD OF CANTED BULKHEAD DOUBLER WHERE HARNESS GOES THROUGH IS EXFOLIATING AND CRACKED AFT ACCESSORY AREA. FABRICATED NEW DOUBLER AND INSTALLED IAW DC9 SRM 53-01 FIG 4 SHT 3. (M)Jun 10, 1999 · N130NK · Doug DC941SDR DLL10991306Bulkhead Web · crackedDURING HFEC INSPECTION OF FS 1363 BLKHD LT WEB, ONE CRACK WAS FOUND AT LBL 42 AND WL 140. REPAIRED PER ERA 367563-14AD.Jun 10, 1999 · N727DA · Lkheed 10113851SDR AALA990866Bulkhead Angle · corrodedTUL - FOUND CORROSION ON AFT BULKHEAD 'T' ANGLE AT FLOORLINE IN AND OF RIGHT GALLEY SUPPORT ATTACH (36 INCH TO 42 INCH OUTBOARD OF CENTERLINE). REPAIRED PER ESO41000, DATED 06/10/99. (M)Jun 10, 1999 · N1764B · Doug MD11SDR SWAA990990Bulhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, LBL 12, WL 234. REPAIRED BULKHEAD PER SRM.Jun 9, 1999 · N324SW · Boeing 7373H4SDR 99ZZZX3137Bulkhead · crackedPILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THJun 6, 1999 · N9925B · Cessna 172RGSDR 99ZZZX3136Bulkhead · crackedPILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THJun 6, 1999 · N9925B · Cessna 172RGSDR 99ZZZX3135Bulkhead · crackedPILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THJun 6, 1999 · N9925B · Cessna 172RGSDR 99ZZZX3134Bulkhead · crackedPILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THJun 6, 1999 · N9925B · Cessna 172RGSDR 99ZZZX3133Bulkhead · crackedPILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THJun 6, 1999 · N93100 · Cessna 172RGSDR 99ZZZX3132Bulkhead · crackedPILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THJun 6, 1999 · N93100 · Cessna 172RGSDR 99ZZZX3131Bulkhead · crackedPILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THJun 6, 1999 · N93100 · Cessna 172RGSDR 99ZZZX3130Bulkhead · crackedPILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THJun 6, 1999 · N93100 · Cessna 172RGSDR 99ZZZX3129Bulkhead · crackedPILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THJun 6, 1999 · N9646B · Cessna 172RGSDR 99ZZZX3128Bulkhead · crackedPILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THJun 6, 1999 · N9646B · Cessna 172RGSDR 99ZZZX3127Bulkhead · crackedPILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THJun 6, 1999 · N9646B · Cessna 172RGSDR 99ZZZX3126Bulkhead · crackedPILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THJun 6, 1999 · N9646B · Cessna 172RGSDR 99ZZZX3125Bulkhead · crackedPILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THJun 6, 1999 · N5199U · Cessna 172RGSDR 99ZZZX3124Bulkhead · crackedPILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THJun 6, 1999 · N5199U · Cessna 172RGSDR 99ZZZX3123Bulkhead · crackedPILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THJun 6, 1999 · N5199U · Cessna 172RGSDR 99ZZZX3122Bulkhead · crackedPILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THJun 6, 1999 · N5199U · Cessna 172RGSDR DHL9970519CBulkhead Beam · crackedAT C CHECK, FWD SIDE OF BS 1183 BULKHEAD BEAM CRACKED BBL 36.8 LEFT WL 214, JUST ABOVE CABIN FLOOR. STOP DRILL, HFEC, INSTALLED REPAIR PER S/B 53A0173, 9.75 BY 5.75, N/R 3370.Jun 5, 1999 · N705DH · Boeing 72722CSDR USAA990496Bulkhead · crackedPIT - DURING Q-4 CHECK, FOUND 2 INCH CRACK AT WEB AT STATION 965 BULKHEAD LOWER INBOARD CORNER. INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 21. (M)Jun 4, 1999 · N934VJ · Doug DC931SDR SWAA990960Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND THROUGH EDDY CURRENT INSPECTION A CRACK AT BULKHEAD, BS 178 , LBL 13. REPAIRED BULKHEAD PER SRM.Jun 3, 1999 · N385SW · Boeing 7373H4SDR DHL9970504CBulkhead Beam · crackedAT C-CHECK, FWD SIDE OF 1183 BULKHEAD BEAM RADIUS OF AFT I/B FLANGE CRACKED WL 238 BBL 36. STOP DRILLED CRACK, HFEC, INSTALLED S/B REPAIR PER S/B 53-0192, N/R 3369.Jun 3, 1999 · N705DH · Boeing 72722CSDR 99ZZZM665Bulkhead Web · corrodedFORWARD BULKHEAD BONDING STRIP AT 11:00 O'CLOCK POSITION HAS CORROSION PITTING. CAUSE OF CORROSION DETERMINED TO BE ENVIRONMENTAL. CORROSION BLENDED AND FOUND BEYOND LIMITS IAW SRM 51-21-58. (M)Jun 3, 1999 · N973NA · Aerosp ATR42300SDR TWAA9908202Bulkhead Web · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION WITH POPPED RIVETS AND PILLOWING AT AFT PRESSURE BULKHEAD, STA 996 BETWEEN LONGERON 26L AND 28L. REMOVED CORROSION PER SPM 6-80-01 AND INSTALLED DOUBLER PER SRM 53-03, FIG 24.Jun 2, 1999 · N981Z · Doug DC931SDR AU990960Bulkhead · cracked(AUS) FORWARD PRESSURE BULKHEAD CRACKED IN THE FOLLOWING AREAS: 1. FORWARD SIDE WEB - TWO CRACKS. 2. LOWER AFT SIDE WEB - TWO CRACKS. 3. VERTICAL CHORD AFT SIDE - ONE CRACK. 4. RT SIDE CHORD RADIUS - ONE CRACK FOUND DURING ULTRASONIC AND EDDY CURREJun 2, 1999 · Boeing 737377SDR AALA990813Bulkhead Web · crackedTUL - APPROX 1 INCH CRACK IN STATION 870 BULKHEAD WEB AT APU LOAD CONTROL VALVE CUTOUT. STOP DRILLED CRACK AND INSTALLED REPAIR AS PER SRM 53-10-2 PAGE 261C. (M)Jun 2, 1999 · N703AA · Boeing 727223SDR AALA990812Bulkhead Angle · crackedTUL - FOUND STATION 870 BULKHEAD TO KEELBEAM ATTACH ANGLE CRACKED RIGHT W/W. REPLACED CRACKED ANGLE WITH NEW. (M)Jun 2, 1999 · N703AA · Boeing 727223SDR MWEA99316Ventral Door · not sealedTHE AFT CABIN VENTRAL DOOR BEGAN SQUEALING ON CLIMB-OUT. MAINTENANCE FOUND AFT PRESSURE DOOR NOT PROPERLY SEATED IN ITS BOTTOM CLEVIS AND RESEATED.Jun 1, 1999 · N300ME · Doug DC915SDR CALA9900605Bulkhead Tee · corrodedINSPECTION FOUND T-SECTION ON FORWARD FACE OF REAR PRESSURE BULKHEAD AT STA 2007 FROM POSITION X = 0.55L TO X = 0.65L CORRODED. THE CORRODED SECTION WAS REMOVED AND A SPLICE REPAIR WAS INSTALLED IAW SRM 53-40-00, FIGURE 16.Jun 1, 1999 · N83071 · Doug DC1030SDR SWAA990942Bulkhead Chord · corrodedDURING SCHEDULED 1/4D CHECK, FOUND CORROSION AT BS 1016 BULKHEAD LOWER CHORD BETWEEN STRINGERS 25R-26R. REPAIRED CHORD PER SWA RA NR 1-253-2087.May 29, 1999 · Boeing 7372H4SDR 99FDEA00195Bulkhead Web · crackedWHILE WORKING W/C 7-5430-7-2303L1 PT 6 DISCOVERED CRACK IN THE BS 1342 BULKHEAD WEB AT WL 252, LBL 17. *S/D* REMOVED AND REPLACED BULKHEAD WEB PER IAW FEDEX EA 7-5310-45235.May 28, 1999 · N234FE · Boeing 727247SDR AU990498Bulkhead · cracked(AUS) AFT LOWER DOORPOST BULKHEAD CRACKED ON BOTH SIDES. CRACK LENGTH 19.05 MM (0.75 INCH).May 26, 1999 · Cessna 172PSDR SWAA990921Bulkhead Chord · crackedDURING SCHEDULED 1/4D CHECK, FOUND RT SIDE CHORD CRACKED AT BS 178, RBL 26, WL 207. REMOVED AND REPLACED CHORD PER SRM.May 25, 1999 · Boeing 7372H4SDR EISA99123Bulkhead Web · gougedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND DRILL DAMAGE OF FS 1183 PRESSURE BULKHEAD AT WL 285 FROM LBL 18.2 TO RBL 18.2 (31 PLACES). REMOVED DAMAGED AREAS AND INSTALLED PERMANENT REPAIR PER ENGINEERING AUTHORIZATION (EA) NR 7-5310-77-C1529 ANDMay 24, 1999 · N312NE · Boeing 727223SDR CKSA99062Bulkhead Fitting · crackedDURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C CHECK AND CPCP TASK CARDS, FOUND AFT PRESSURE BLKHD TO FUSELAGE ATTACHMENT FITTING CRACKED AT STA 1792, WL 329, RBL .20. REMOVED CRACKED FITTING IAW SRM 53-40-01. REPAIR CARRIED OUT IAW SRM 53-21-02. INSTALLED REMay 24, 1999 · N102CK · Lkheed 1011385115SDR 99ZZZM396Bulkhead Web · gougedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND DRILL DAMAGE OF FS 1183 PRESSURE BULKHEAD AT WL 285 FROM LBL 18.2 TO RBL 18.2 (31 PLACES). REMOVED DAMAGED AREAS AND INSTALLED PERMANENT REPAIR PER ENGINEERING AUTHORIZATION (EA) NR 7-5310-77-C1529 ANDMay 24, 1999 · N312NE · Boeing 727223SDR USAA990530Bulkhead Skin · crackedCLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK AT 178 PRESSURE BULKHEAD SKIN, WL 201, RBL 4.75 INCH. INSTALLED DOUBLER T/R 53-10-07. (M)May 22, 1999 · N419US · Boeing 737401SDR USAA990529Bulkhead Skin · crackedCLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK AT 178 PRESSURE BULKHEAD SKIN, WL 198, RBL 4.75 INCH. INSTALLED DOUBLER T/R 53-10-07. (M)May 22, 1999 · N419US · Boeing 737401SDR USAA990528Bulkhead Skin · crackedCLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK AT 178 PRESSURE BULKHEAD SKIN, WL 201, RBL 7 INCH. INSTALLED DOUBLER T/R 53-10-07. (M)May 22, 1999 · N419US · Boeing 737401SDR USAA990527Bulkhead Skin · crackedCLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK AT 178 PRESSURE BULKHEAD SKIN, WL 198, LBL 4.75 INCH. INSTALLED DOUBLER T/R 53-10-07. (M)May 22, 1999 · N419US · Boeing 737401
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