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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR EIA2003029Bulkhead · corrodedCANTED BULKHEAD AT B.S. 1241 RT, CORROSION AT BL0-RBL 5. C/A: REMOVED CORRODED SECTION, REPAIRED ER ECRA 481-53-177-2 AND SRM 53-10-01. INSTALLED DOUBLER PER 747 SRM 51-30-02, PGS 5-9, 38, 57-58. INSTALLED NEW WEB STA 1241-1265 BL4 TO RBL45, IAW SRM 51-SDR SWAA030466Bulkhead · crackedDURING SCHEDULED C3 CHECK, FOUND BS 1016 BULKHEAD CRACKED (4 EA) AT 8, 9, 10 AND 11.30 O'CLOCK POSITIONS RADIATING FROM RIVETS AT THE PERIPHERY OF THE PRESS PLUG. REPAIRED BULKHEAD PER SWA EA.SDR AWXA200300279Angle · crackedMCN - MAJOR REPAIR - DURING C-14 CHECK A 1 3/8" CRACK WAS FOUND ON FORWARD TEE CHORD, AFT SIDE OF BS 178 BULKHEAD WEB, LBL 5.7, WL 184. MAINTENANCE CUTOUT DAMAGED AREA OF FORWARD TEE CHORD, LBL 5.7, WL 184, BS 178; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKSSDR CA030228007Bulkhead · cracked(CAN) DURING ANNUAL INSPECTION, IT WAS DICOVERED THE BULKHEAD HAD A SUBSTANDARD REPAIR AT REAR FLOAT FITTING ATTACHMENT BRACKETS. PREVIOUS REPAIR REMOVED TO FACILITATE NEW REPAIR. BULKHEAD WAS FOUND TO BE CRACKED BEYOND REPAIR WITH A TOTAL OF 4 CRACKS WITHIN ASDR QXEA0300350Bulkhead · crackedFOUND TWO CRACKS BY LPI IN AFT PRESSURE BULKHEAD. REPAIRED IAW CRJ 700 MM TACK 51-23-00-390-810-A01 AND RO R-29-07.SDR AWXA200300287Bulkhead · crackedDURING C-18 CHECK 2 EACH CRACKS WERE FOUND ON BS 178 BULKHEAD WEB AT WL 190, BL 0, UNDER VOR/LOC ANTENNA MOUNT. MAINTENANCE CUTOUT CRACKED BS 178 BULKHEAD WEB AT WL 190, BL 0; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A DOUBLER,SDR 03FDEA00182Pressure Panel · gougedGOUGED AREA AT NLW UPPER WEB AT LT PRESSURE PANEL CUT OUT INBOARD SIDE, B.S 242. REMOVED DAMAGE AND REPAIRED IAW SRM 51-40-2. GOUGE WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1.SDR ABXA030110Bulkhead · crackedAFT PRESSURE BULKHEAD NR 4 CRACKED AT OUTBOARD END. INSTALLED NEW ANGLE IAW DOUGLAS DWG J060110.SDR 2003UALA00210Bulkhead · crackedSTATION 178 BULKHEAD UPPER RIGHT ANTENNA MOUNT UPPER OUTBOARD ATTACH POINT HAS CRACK INDICATION. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED REPAIR DOUBLER.SDR SWAA030415Pressure Panel · crackedDURING SCHEDULED 1/2D CHECK, FOUND BEADED WEB CRACKED AT BS 663, LBL 30. REPAIRED BEADED WEB PER SRM.SDR 0300281240Attach Angle · crackedDuring "L" check found crack in fuselage bulkhead upper attach angle at BS 2122.8. Repaired per EA 12-194259.SDR CA030228004Fitting · cracked(CAN) UPON A THREE HUNDRED HOUR INSPECTION 270 BULKHEAD FITTING 222-031-506-103A WAS FOUND CRACKED. TO REPAIR INCORPORATION OF TB 222U-94-72.SDR 03051620Bulkhead · damagedDURING HEAVY CHECK SEVERAL HOLES WERE DISCOVERED DRILLED THROUGH THE AFT PRESSURE BULKHEAD AT FS 621. MAINTENANCE PERSONNEL REPAIRED HOLES IAW BOMBARDIER REO.SDR SWAA030420Bulkhead · crackedDURING SCHEDULED C2 CHECK, FOUND BS 1016 BULKHEAD CRACKED (4 EA) AT 8:00 O'CLOCK POSITION RADIATING FROM RIVETS AT THE PERIPHERY OF THE PRESS PLUG. REPAIRED BULKHEAD PER SWA EA.SDR 0300459614Former · crackedDuring "H" check found crack in outboard end of aft pressure bulkhead horizontal former at Z=34 and X=40. Repaired per EA 96-194267.SDR AWXA200300240Frame · crackedDURING C-11 CHECK A 1 INCH CRACK WAS FOUND IN RADIUS OF RT OUTER CHORD OF 178 BULKHEAD AT WL 207. MAINTENANCE CUTOUT DAMAGED SECTION OF RT OUTER FRAME, BULKHEAD 178, WL 207; FABRICATED A NEW SECTION OF FRAME AND SPLICE ANGLES PER SB 737-53A1173, FIG. 61; INSTASDR UPS03240303Pressure Panel · crackedINSPECTION TYPE: C&SI, SUSPECT CRACK AT AFT END OF BEAD IN RIGHT MLG CEILING AT BS 940 RBL 58 APPROX. REPAIRED IN CONJUNCTION WITH 940 FITTING REPLACEMENT REF NRC 631320.SDR AWXA200300203Stiffener · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK A 1" CRACK WAS FOUND ON STIFFENER AT R/H AIR CONDITIONING BAY AFT BULKHEAD JUST ABOVE THE TURBO FAN EXHAUST DUCT. MAINTENANCE REMOVED CRACKED STIFFENER AT R/H AIR CONDITIONING BAY AFT BULKHEAD JUST ABOVE THE TURBO FAN EXHSDR MWEA030084Angle · damagedLOWER ANGLE SUPPORT FOR AFT PRESSURE BULKHEAD FORMER IS DAMAGED RIGHT OUTBOARD FORWARD SIDE. -- REMOVED AND REPLACED ANGLE.SDR CALA0300052Pressure Panel · crackedINSPECTION FOUND A 2.75 INCH CRACK IN RT WHEEL WELL PRESSURE DECK AT FS 663, RBL 35. REPAIRED IAW SRM 53-60-51, PAGE 213-231.SDR MWEA030107Bulkhead · crackedAFT PRESSURE BULKHEAD TEE IS DENTED AND CRACKED BEWEEN LONGERON 9 AND 12 RIGHT AFT OF AFT PRESSURE BULKHEAD STATION 1339. REMOVED AND REPLACED DAMAGED TEE SECTION.SDR MWEA030069Splice Plate · damagedNEW AFT PRESSURE BULKHEAD TEE AT STATION 1338 LONGERON 6 RIGHT AND 18 RIGHT REQUIRES NEW SPLICE PLATE AT FACTORY SPLICE LOCATION. -- FABRICATED AND INSATLLED LOWER AND UPPER NEW SPLICE PLATE.SDR MWEA030097Doubler · installedAFT PRESSURE BULKHEAD RIGHT SIDE SPLICE AT VENTRAL DOOR JAMB, REQUIRES DOUBLER INSTALLATION. -- FABRICATED AND INSTALLED REPAIR PART.SDR MWEA030103Splice · crackedRIGHT OUTBOARD SIDE OF AFT PRESSURE BULKHEAD IS DENTED AND CRACKED BETWEEN LONGERON 12 AND 9 RIGHT. -- FABRICATED AND INSTALLED NEW SPLICE AND AFT PRESSURE BULKHEAD.SDR MWEA030077Clip · crackedREMOVED AFT PRESSURE BULKHEAD ASSEMBLY LOCATED AT AIRCRAFT CENTERLINE OVER VENTRAL DOOR JAMB FRAME STATION 1338 TO FACILITATE OTHER MAINTENANCE. -- FOUND CLIP AND WEB CRACKED AND CLIP BENT LOCATED AND DRILLED AND INSTALLED STIFFENER AND NEW WEB AND INSTALLEDSDR 2003FA0000359Firewall · crackedDURING A PHASE 1 INSPECTION FOUND A CRACK IN THE FIREWALL AT THE LOWER ROW OF RIVETS ATTACHING THE BATTERY BOX TO THE FIREWALL. UPON REMOVAL OF BOX FOR REPAIR FOUND 2ND CRACK UNDER THE OUTBOARD VERTICAL ROW OF RANGE IN MFG SB FIREWALL INSPECTION.SDR UPS03240258Pressure Panel · crackedINSPECTION TYPE: C&SI, AIR LEAK COMING FROM WHAT APPEARS TO BE CRACK IN PRESSURE WEB IN NOSE W/W LEFT SIDE MIDWAY ON LT SIDE WALL. CRACKED AREA CUT OUT IAW SRM 51-40-2. DOUBLER & FILLER FABRICATED IAW SRM 51-40-2. HFEC C/O ON CUTOUT ON THE ABOVE AREA IAW NSDR MWEA030091Clip · bentUPPER AND LOWER ANGLE SUPPORT ON FORWARD SIDE OF AFT PRESSURE BULKHEAD FORMER IS BENT RIGHT OUTBOARD AREA SECOND FORMER DOWN FROM TOP. -- LOCATED AND DRILLED AND INSTALLED NEW CLIP.SDR DL738030152Frame · crackedFUSELAGE / R1 DOOR OPENING / FWD FRAME / LOWER STUB FRAME : CRACK REPAIR THE LOWER STUB FRAME OF THE R1 DOOR OPENING FWD FRAME ASSY WAS FOUND WITH 3 CRACKS AT THE LOWER DOOR STOP FITTING. THE CRACKS WERE CAUSSDR MWEA030076Clip · damagedREMOVED AFT PRESSURE BULKHEAD FORMER ASSEMBLY FROM FORWARD SIDE OF AFT OF AFT PRESSURE BULKHEAD AT STATION Z34 TO FACICLITATE OTHER MAINTENACE. -- REMOVED ASSEMBLY AND FORMER DRILLED UP AND INSTALLED NEW CLIP AND INSTALLED FORMER.SDR AUS20030138Frame · cracked(AUS) FUSELAGE BULKHEAD OUTER CHORD CRACKED AT STA 1809. FOUND DURING INSPECTION IAW AD/B767/146.SDR SWAA030330Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BULKHEAD WEB CRACKED ( 2 EA ) AT BS 178, WL 235 AND BL 11, LT AND RT. REPAIRED BULKHEAD PER SWA EA.SDR SWAA030313Doubler · corrodedDURING SCHEDULED D CHECK, FOUND LOWER CHORD DOUBLER CORRODED AT BS 1016, WL 191 AND LBL 5. REPAIRED DOUBLER PER SRM.SDR DL73K030140Bulkhead · crackedFUSELAGE / BULKHEAD / FS 178 / WEB AND SIDE CHORDS : CRACK REPAIR THE FS 178 BULKHEAD WEB AND SIDE CHORDS WERE FOUND WITH CRACKS TYPICAL OF BAC S/B 737-53-1173 AND AD 2000-05-29. THE WEB HAD SEVERAL SDR SWAA030314Pressure Panel · corrodedDURING SCHEDULED D CHECK, FOUND BULKHEAD SKIN CORRODED AT BS 1016, WL 192 AND BL 0. REPAIRED BULKHEAD SKIN PER SRM.SDR 2003UALA00149Bulkhead · crackedSTATION 178 BULKHEAD WEB CRACKED AT WL 199 LBL 5.7. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.SDR 2003UALA00146Bulkhead · crackedSTATION 178 BULKHEAD WEB CRACKED AT WL 199 RBL 5.7 MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.SDR EVAS092006Bulkhead · crackedDURING CARGO LOADING , 2.5 INCH DIAMETER HOLE FOUND WITH RADAL CRACK ON LT LOWER CORNER OF PRESSURE BULKHEAD. PERFORM REPAIR BY FINGER DOULBER AND TEE AT STATION 2007 X=-10 AND X=-70 RESPECTIVELY PERFORM CABIN PERSSURE LEAKAGE CHECK.SDR AALA20030141Bulkhead · crackedTUL - FOUND AFT PRESSURE BULKHEAD UPPER RIGHT FS 1338, CRACKED. REMOVED AND REPLACED. (M)SDR AWXA200300124Web · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK , A BULKHEAD WEB WAS FOUND CRACKED AT B.S. 178. CRACK WAS CONFIRMED WITH HFEC. MAINTENANCE REMOVED DAMAGED AREA OF BULKHEAD WEB BS 178; FABRICATED A REPAIR DOUBLER, FILLER, AND 3 EACH SHIMS; AND INSTALLED REPAIR PARTS IAWSDR SWAA030261Web · crackedDURING SCHEDULED SPECIAL VISIT, FOUND BS 1016 BULKHEAD WEB CRACKED AT 11, 12 AND 1 O'CLOCK POSITIONS. REPAIRED WEB PER SWA EA.SDR QXEA0300253Bulkhead · crackedPDX- 1.85 INCH CRACK IN AFT PRESSURE BULKHEAD AT NR 2 EDP SUCTION LINE FEED THROUGH. REPAIRED IAW HORIZON AIR EA R-54-64.SDR MWEA030052Bulkhead · crackedSTATION 965 RIGHT, FORWARD PYLON, BULKHEAD WEB HAS TWO SMALL CRACKS EMANATING FROM SNAPS AT OUTBOARD SIDE NEXT TO LONGERON 11 AND LONGERON 10. CUT OUT DAMAGE, FABRICATED DOUBLER, INSTALLED TWO EACH OF DOUBLERS AND PARTITION GUIDE.SDR MWEA030054Bulkhead · crackedAT APPROXIMATELY STATION 965 RIGHT FORWARD BULKHEAD WALL HAS A CRACK APPROXIMATELY SIX INCHES INBOARD OF OUTSIDE BULKHEAD ATTACH ANGLE, CRACK IS EMITTING FROM BOLT HOLE FOR THE LOWER SPAR. REMOVED DAMAGED WEB, FABRICATED AND INSTALLED WEB.SDR AUS20030346Bulkhead · cracked(AUS) FORWARD DOORPOST BULKHEAD CRACKED AS INDICATED IN AD/C207/32.2.SDR LR7A03006Skin Panel · crackedDURING SCHEDULED B2 INSPECTION PER JOB CARD HB3202 FOUND RMLG WHEEL WELL FS 617 AFT BULKHEAD SKIN CRACKED .5 IN. AT CENTER OF PANEL RBL 69, WL 184.REPLACED SKIN PANEL IAW SRM SMP 583 53-40-02 AND DWG 339149. NR 0040.SDR AWXA200300164Web · crackedLCQ - MAJOR REPAIR - DURING C-18 CHECK 2 EACH CRACKS WERE FOUND ON BS 178 BULKHEAD WEB AT LBL 5, WL 200 TO WL 201.25. MAINTENANCE CUTOUT CRACKS ON BS 178 BULKHEAD WEB AT LBL 5, WL 200 TO WL 201.25; PERFORMED HFEC INSPECTION OF CUTOUTS TO VERIFY NO CRACKS EXISTSDR AWXA200300162Web · crackedLCQ - MAJOR REPAIR - DURING C-18 CHECK 2 EACH CRACKS WERE FOUND ON BS 178 BULKHEAD WEB, APPROXIMATELY WL 196.75 TO WL 198, AT APRON OF RBL 5. MAINTENANCE CUTOUT CRACKS AT RBL 5, WL 196.75 AND WL 202; PERFORMED HFEC INSPECTION OF CUTOUTS TO VERIFY NO CRACKS EXISDR C2XA02SH188Firewall · crackedSHV- DURING C CHECK APU FIREWALL CRACKED AT TOP RIVET OF RIGHT HAND VERTICAL REINFORCEMENT. MAINTENANCE REMOVED DAMAGE AND REPAIRED CRACK IAW CONTINENTAL EXPRESS EC 5330-01202. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR 2003UALA00121Pressure Panel · crackedMLG WHEEL WELL PRESSURE PANEL CRACKED AT STA 670 LBL33, OUTBOARD AND AFT OF AILERON TOWER SHAFT. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER.
Back to JASC 5312