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 ABXA9900709Stiffener · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD, AFT SIDE STIFFENER CRACKED AT BOTTOM OF VENTRAL DOOR CUTOUT. REPAIRED IAW DC9 SRM DRAWING K05159.Sep 3, 1999 · N959AX · Doug DC941SDR DHL9972732CBulkhead Angle · corrodedAT C CHECK, LWR FWD CARGO COMPARTMENT RT BULKHEAD PANEL LWR ATTACH ANGLE HAS CORROSION AT LWR END. CUT OUT CORRODED AREA PER SRM 51-10-1 17, INSTALLED ANGLE REPAIR AT FWD END USING .063 2024T3 17 X 4 PER SRM 51-40-3. ALODINED AND PRIMED PER SRM 51-10-2 N/R Sep 1, 1999 · N727DH · Boeing 727228SDR SWAA991448Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 8 -RBL 10. REPAIRED BULKHEAD PER SWA RA NR 1-353-2152.Aug 31, 1999 · N693SW · Boeing 737317SDR AWXA9900287Bulkhead Web · crackedC-CHECK, TWO CRACKS ON RT O/B BULKHEAD SHEAR WEB AT BS 727 STR 18A SHEAR BEAM. REMOVED WEB AND ATTCH PARTS IAW SRM 51-30-2. INSTALLED NEW WEB AND ATTACH PARTS. REMOVED AND REINSTALLED 3 STIFFENERS FROM 18A WEB.Aug 31, 1999 · N181AW · Boeing 737277SDR 99ZZZX3613Bulkhead · crackedDURING ROUTINE INSPECTION, FOUND ELEVATOR CONTROL CABLE TENSION LOW. ATTEMPT TO ADJUST, COULD NOT ATTAIN PROPER TEST. INSPECT CABLE ROUTING, NOT ABLE TO VERIFY PULLEY MOVEMENT. THERE ARE NO ACCESS PLATES OR PANELS TO VISUALLY INSPECT. ENTIRE TAIL GROUP WAS Aug 30, 1999 · N1850V · Cessna 140SDR USAA990836Bulkhead · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK STATION 666, LBBL 32.5 PRESSURE DECK. INSTALLED DOUBLER PER EA 65231. (M)Aug 29, 1999 · N397US · Boeing 7373B7SDR DL73K991937Bulkhead Web · crackedTHE FS 178 BULKHEAD WEB WAS FOUND WITH A .75 CRACK AT LBL 6.7 WL 208 AND ANOTHER .75 CRACK AT BL 0 WL 190. THERE WAS AN EXISTING DOUBLER REPAIR INSTALLED TO REPAIR OTHER PREVIOUS CRACK CUTOUTS. THE EXISTING DOUBLER WAS REMOVED, THE WEB INSPECTED, THE NEW CRAug 29, 1999 · N307DL · Boeing 737232SDR SWAA991438Bulkhead · crackedDURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 4.7. REPAIRED BULKHEAD PER SRM.Aug 27, 1999 · N349SW · Boeing 7373H4SDR 99ZZZX3707Bulkhead · crackedTHIS AIRCRAFT IS JUST ONE OF FOUR THIS YEAR (OF THE SAME MAKE AND MODEL) THAT HAVE HAD STC SA 8214SW FROM THE COMMANDER SERVICE CENTER (REMOVAL OF THE CLAMSHELL DOORS) THAT WERE FOUND WITH LARGE CRACKS INSIDE THE WHEELWELL ON THE AFT BULKHEAD.Aug 27, 1999 · N67FE · Gulstm 690CSDR DHL9972742CBulkhead Beam · crackedFOUND CRACK AT STA 1183 VERTICAL I BEAM RBL 36.83 O/B FLANGE WL 235. REMOVED FASTENERS AT BS 1183 AFT BLKHEAD VERTICAL BEAM RBL PER SRM 51-30-2, STOP DRILLED IAW NDT MANUAL 51-00-00 PART 6 FIGURE 4. NO FURTHER CRACK INDICATION NOTED. INSTALLED REPAIR KIT ONAug 26, 1999 · N727DH · Boeing 727228SDR MWEA99546Pan · crackedTHE AFT PRESSURE BULKHEAD PLUG DOOR HAS A CRACK ON PAN AT 11 O'CLOCK POSITION. MAINTENANCE FABRICATED AND INSTALLED DOUBLER.Aug 25, 1999 · N500ME · Doug DC914SDR ABXA9900669Bulkhead T-Cap · corrodedDURING C-CHECK, FOUND PRESSURE BULKHEAD T-CAP CORRODED AT STATION Y-617. REPAIRED T-CAP IAW ABX REA D953-32890 MR.Aug 25, 1999 · N945AX · Doug DC931SDR SWAA991407Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, UT INSPECTION INDICATES 5 EACH CRACKS ON BS 178 BULK HEAD, RBL 5 - LBL 57. REPAIRED BULKHEAD PER SRM.Aug 23, 1999 · N689SW · Boeing 7373Q8SDR MZZA99163Bulkhead Tee · corrodedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON BS 950 BULKHEAD LOWER T-CHORD BETWEEN S30 AND S29R. THE CORRODED LOWER T-CHORD WAS REMOVED AND REPLACED PER B727 CHAPTER 51-30-02 FIG 1-4. (M)Aug 23, 1999 · N79743 · Boeing 727224SDR CA990907068Bulkhead · corroded(CAN) DURING SCHEDULED MAINTENANCE, SEVERE CORROSION INCLUDING EXFOLIATION WAS FOUND ON THE LONGITUDINAL CANTED BULKHEAD, PN. 2412008-2. DAMAGE WAS NOTED AFTER THE SUBJECT AREA WAS CLEANED OF GREASE AND EXHAUST RESIDUE. CORROSION WAS ALSO FOUND ON THE BULKHAug 23, 1999 · Cessna 172RGSDR P2EA99250Bulkhead Web · crackedSJO - BULKHEAD WEB CRACKED AT BS 178, RBL 15, WL 218. REPAIRED IAW SRM 53-10-11 FIG 1. (M)Aug 22, 1999 · N204AU · Boeing 737247SDR P2EA99238Bulkhead Web · dentedSJO - AFT PRESSURE BULKHEAD WEB DENTED AT BS 1025, WL 196, RBL 8 INCHES. DEFECT SIZE, DEPTH .300 INCH. PRESSURE BULKHEAD SECTION BS 1025, WL 198.1, WL 198, RBL 7 INCH TO 11.20 REPAIRED PER SRM 53-10-4 FIG 3. (M)Aug 21, 1999 · N204AU · Boeing 737247SDR SWAA991397Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND THROUGH HFEC INSPECTON A 1.5 INCH LONG CRACK ON BS 178 BULKHEAD AFT SIDE, RBL1. REPAIRED BULKHEAD PER SRM.Aug 20, 1999 · N685SW · Boeing 7373Q8SDR ABXA9900682Bulkhead Tee · crackedDURING C-CHECK, FOUND A CRACK INDICATION IN THE AFT PRESSURE BULKHEAD NR 6 TEE CAP. REPAIRED IAW ABX EA 53-120037-006.Aug 20, 1999 · N945AX · Doug DC931SDR TWAA9911903Bulkhead · crackedDURING OP 16 MAINT CHECK, THE RT BULKHEAD WAS CRACKED 3 INCHES LONG, LOCATED 1 INCH ABOVE FLOOR AND 5 INCHES FROM SIDEWALL ON FWD SIDE, STA 965. REMOVED AND REPLACED BULKHEAD PER SPM 6-70-01.Aug 19, 1999 · N979Z · Doug DC931SDR TWAA9911902Bulkhead Angle · crackedDURING OP 16 MAINT CHECK, FOUND AFT PRESS BULKHEAD, FWD SIDE DIAGONAL BRACE ATTACH ANGLE ON PRESSURE BULKHEAD, STA 996 AT UPPER END, CRACKED BETWEEN LONGERON 3L AND 4L. REMOVED CRACKED ANGLE AND FABRICATED NEW ANGLE. PAINTED AND REINSTALLED IN ACCORDANCE WITAug 19, 1999 · N979Z · Doug DC931SDR SWAA991385Bulkhead Chord · crackedDURING SCHEDULED 1/4D CHECK, FOUND LEFT SIDE CHORD CRACKED, BS 178, LBL 29. REPAIRED CHORD PER SRM.Aug 19, 1999 · N685SW · Boeing 7373Q8SDR MZZA99161Bulkhead Web · corrodedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON T-STIFFENER JUST ATTACHED TO BS 950 PRESSURE BULKHEAD WEB FORWARD SIDE IN RT MLG WW/ THE CORRODED T-STIFFENER WAS REMOVED AND REPLACED PER SRM 51-30-2 FIGURE 1-4. (M)Aug 19, 1999 · N79743 · Boeing 727224SDR DLL19991857Bulkhead Web · damagedTOOLING DAMAGE WAS FOUND ON THE NLG WHEEL WELL BULKHEAD AT APPROX FS 416, RBL 22 ON THE LWR SURFACE O/B FILLET RADIUS INSIDE THE RT ECS COMPT (NLG BLKHD WEB CAP). DAMAGE DEPTH IS APPROX 0.060 BY 1 IN LENGTH (FWD/AFT) BY 0.5 (VERT). REPAIRED PER ERA 333433-14Aug 19, 1999 · N765DA · Lkheed 10113853SDR ABXA9900686Frame · crackedDURING C-CHECK, FOUND OUTBOARD END OF THE AFT PRESSURE BULKHEAD FRAME CRACKED AT LONGERON 15 LEFT. REPAIRED IAW DC9 SRM 51-30-5 AND 51-20-0.Aug 19, 1999 · N945AX · Doug DC931SDR 9904649758Channel · crackedDURING APB INSPECTIONS, A 1.25 CRACK WAS FOUND IN THE UPPER INBOARD BEND RADIUS OF THE LEFT CHANNEL 5910130-9. REPAIRED PER EA 97-169048.Aug 19, 1999 · N758NW · Doug DC941SDR SWAA991373Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 17.5. REPAIRED BULKHEAD PER SWA RA NR 1-53-2143.Aug 18, 1999 · N685SW · Boeing 7373Q8SDR DL733991830Bulkhead Web · crackedDURING HMV, THE FS 178 BULKHEAD WAS FOUND TO HAVE 7 CRACKS IN THE PRESSURE WEB. THIS DAMAGE WAS REPAIRED PER ERA 333450-14.Aug 17, 1999 · N311WA · Boeing 737347SDR DLM88991835Bulkhead Cap · crackedTHE OUTER CAP ANGLE OF THE FS 1463 CANTED BULKHEAD WAS FOUND WITH A 1 INCH CRACK IN THE HORIZONTAL SKIN ATTACH FLANGE. THE ADJACENT SKIN WAS ALSO CRACKED. THE CRACK WAS AT THE LT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE LOCATION. THE ATTACH ANGLE AND VAug 16, 1999 · N996DL · Doug MD88SDR DL73K991837Bulkhead Web · crackedWHILE ACCOMPLISHING LFEC INSPECTIONS OF THE AFT PRESSURE BULKHEAD WEB, A CRACK INDICATION WAS NOTED NEAR STRINGER 6R. INTERNAL HFEC INSPECTION CONFIRMED TWO CRACKED FASTENER HOLES AT THE WEB TO CAP INTERFACE AT STRINGER 6R. THE CRACKED AREA OF WEB WAS CUTOUTAug 14, 1999 · N329DL · Boeing 737232SDR DL73K991836Bulkhead Web · crackedTHE FS 178 BULKHEAD WEB WAS FOUND WITH TWO SMALL CRACKS AT WL 210, BL 5.7 LT & RT AND TWO SMALL CRACKS AT WL 233.5, BL 5.7 (LT & RT). THE WL 233.5 CRACKS WERE REPAIRED WITH DOUBLERS PER SRM 53-10-11. THE CRACKS AT WL 210 WERE JUST ABOVE A LARGE EXISTING WEBAug 14, 1999 · N325DL · Boeing 737232SDR ABXA9900651Angle · crackedDURING C-CHECK, FOUND FORWARD FACE OF AFT PRESSURE BULKHEAD, OUTBOARD LEFT ATTACH ANGLE, CRACKED AT LONGERON 15 LEFT. REPLACED ANGLE IAW DC9 SRM 51-30-1 AND 51-30-5.Aug 13, 1999 · N932AX · Doug DC933FSDR MWEA99488Bulkhead Panel · damagedTOOLING DAMAGE BY 6 RIVETS ON FORWARD BAG PIT AT AFT PRESSURE BULKHEAD BOTTOM BETWEEN LONGERON 28L AND 28R. MTC FABRICATED AND INSTALLED NEW BULKHEAD PANEL.Aug 12, 1999 · N600ME · Doug DC914SDR 9903679758Bulkhead · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND IN RIGHT SLANT PRESSURE PANEL FS 737. REPAIRED PER EA 97-168991.Aug 12, 1999 · N758NW · Doug DC941SDR SWAA991348Bulkhead Chord · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD RT CHORD CRACKED, RBL 28.5. REMOVED AND REPLACED RT CHORD PER SRM.Aug 11, 1999 · N524SW · Boeing 7375H4SDR SWAA991341Bulkhead · crackedDURING SCHEDULED 1/2D CHECK, FOUND THROUGH ULTRASONIC INSPECTION BS 178 BULKHEAD CRACKED, LBL 4.7. REPAIRED BULKHEAD PER SRM.Aug 11, 1999 · N308SA · Boeing 7373Y0SDR DL72W991810Bulkhead Beam · crackedFUSELAGE BULKHEAD FS 1183, RBL 26.83, VERTICAL BEAM, CRACK REPAIR. THE RBL 26.83 VERTICAL BEAM ON THE FS 1183 BULKHEAD WAS FOUND WITH A TYPICAL CRACK. THE BEAM WAS REPAIRED PER BOEING S/B 727-53-0182, REV 1 AND DOCUMENTED PER ER/A 367994-14AD.Aug 11, 1999 · N2817W · Boeing 727247SDR SWAA991335Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND THROUGH ULTRASONIC INSPECTION 3 EACH CRACKS AT BS 178 BULKHEAD, LBL 5 - RBL 5. REPAIRED BULKHEAD PER SRM.Aug 10, 1999 · N524SW · Boeing 7375H4SDR SWAA991322Bulkhead Web · oil cannedDURING SCHEDULED C3 CHECK, FOUND BS 1016 BULHEAD AFT FACE OIL CANNED AT STRINGER 6L, (DAMAGE IS 5 BY 7). REPAIRED BULKHEAD PER SRM.Aug 9, 1999 · Boeing 7372H4SDR 99ZZZX3331Bulkhead · buckledDAMAGE TO SUB-FLOOR FRAMES IN AFT CARGO AREA. FIVE BULKHEADS REQUIRED REPLACEMENT DUE TO DAMAGE POSSIBLY RELATED TO MISHANDLED FREIGHT. THE AREA OF DAMAGE IS AT THE CARGO DOOR ENTRANCE. SUBMITTER STATED THIS IS A RECURRING PROBLEM ON THESE AIRCRAFT FOR THE Aug 9, 1999 · N948FE · Cessna 208BSDR 9903649154Bulkhead · corrodedDURING PERIODIC CHECK, FOUND RIGHT SLANT PRESSURE PANEL ABOVE MAIN LANDING GEAR WHEEL WELL CORRODED FS 623, WL -55. REPAIRED PER EA 91-169010.Aug 9, 1999 · N8913E · Doug DC914SDR CALA9901080Blkhd Stiffener · corrodedINSPECTION FOUND BOTTOM CENTER RT STIFFENER CORRODED AT AFT PRESSURE BULKHEAD SIDE. REPAIRED IAW SRM 51-70-11, FIGURE 1.Aug 8, 1999 · N63305 · Boeing 7373T0SDR SWAA991307Bulkhead · crackedDURING SCHEDULED 1/4D CHECK, FOUND BS 178 BULKHEAD CRACKED, RBL 5. REPAIRED BULKHEAD PER SRM.Aug 6, 1999 · N326SW · Boeing 7373H4SDR MWEA99500Bulkhead Fitting · crackedRIGHT AND LEFT FITTINGS FOR PRESSURE BULKHEAD AT STATION 490 WAS CRACKED. MTC REMOVED AND REPLACED FITTINGS.Aug 6, 1999 · N80ME · Doug DC914SDR CA990817017Bolts · loose(CAN) DURING ROUTINE C-CHECK, FOUND SEVERAL PERIMETER BOLTS LOOSE AT THE AFT PRESSURE BULKHEAD TO FUSELAGE BUTT SPLICE STN 1016. TORQUE CHECK OF ALL 225 BOLTS REVEALED 183 WERE LOOSE AND 11 BOLTS SHANKED. ALL BOLTS WERE REMOVED AND HOLES CHECKED FOR DAMAGE. Aug 6, 1999 · Boeing 737217SDR 99ZZZX3117Bulkhead · 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 THAug 6, 1999 · N9741B · Cessna 172RGSDR 99ZZZX3116Bulkhead · 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 THAug 6, 1999 · N9741B · Cessna 172RGSDR 99ZZZX3115Bulkhead · 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 THAug 6, 1999 · N9741B · Cessna 172RGSDR 99ZZZX3114Bulkhead · 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 THAug 6, 1999 · N9741B · Cessna 172RGSDR UPS99230438Bulkhead Forging · corrodedINSPECTION TYPE:C, CORROSION ON LT BS 740 BULKHEAD FORGING BETWEEN STR 23L AND STR 24L. FITTING REPLACED IAW EO B727-5310-7477-E.Aug 5, 1999 · N941UP · Boeing 72722C
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