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 SWAA960040Bulkhead · crackedDURING SCHEDULED MAINT CHECK, FOUND BS 178 BULKHEAD CRACK INDICATIONS AROUND RIVET HEAD FWD SIDE, WL 234, RBL 0. REPAIRED PER BOEING SRM.SDR SWAA960032Bracket · crackedDURING SCHEDULED MAINT CHECK, FOUND BULKHEAD AT BS 351.2 ATTACH BRACKET CRACKED ON LEFT SIDE. REPAIRED PER BOEING SRM.SDR CAL960160Bulkhead · crackedMIA - INSPECTION FOUND A .5 INCH CRACK IN CANTED BULKHEAD WEB JUST FORWARD OF RUDDER TRIM ACTUATOR DRUM AT FS 1490, RIGHT SIDE. THE CRACKED WEB WAS REMOVED AND A BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-02. (M)SDR DL72S960105Blkhd Web · crackedFOUND ON E2 LETTER CHECK, STA 870 BULKHEAD WEB CRACKED 3 INCHES AT APU LOAD CONTROL VALVE CUTOUT, LWR END IN RT W/W. REPAIR PER SRM 53-10-9, TIME LIMITED INST.SDR AU960033Bulkhead · cracked(AUS) FUSELAGE BULKHEADS LOCATED AT FS 257.6 AND FS 271.92 CRACKED - BULKHEADS ARE LOCATED AT THE FORWARD AND AFT HORIZONTALSTABILISER STUB SPARS - FURTHER INVESTIGATION FOUND THAT THE CRACK WAS IDENTIFIED AS A SCORE MARKSDR AALA960054Blkhd Doubler · corrodedTUL - FOUND CORROSION ON SPADE PLATE, FORWARD FACE OF PRESSURE BULKHEAD STRINGER 1338 LONGERON 30. INSTALLED NEW SPADE PLATE ON FORWARD FACE OF AFT PRESSURE BULKHEAD. (M)SDR 96ZZZM507Blkhd Beam · crackedDURING C-CHECK, FOUND CABIN AFT BULKHEAD STATION 1183 WL 283 VERTICAL BEAM CRACKED RBL 3683. REMOVED FASTENERS, STOP DRILLED CRACK AND ALODINED STOP DRILLED HOLES PER SRM 51-30-2, 51-10-1, AND 51-10-2. VERTICAL BEAM REPAIR INSTALLED AT RBL 3683 STATION 1183 SDR 96ZZZM505Blkhd Beam · crackedDURING C-CHECK, FOUND AFT BULKHEAD STATION 1183 WL 283 LBL 26 VERTICAL BEAM CRACKED. REMOVED AND REPLACED VERTICAL BEAM PER BOEING SB 727-53-182 TYPE IV.SDR ABXA9600411Web · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE PYLON BULKHEAD AT FS 965 CRACKED JUST ABOVE THE FLOOR LINE AT RBL 50. REPLACED PYLON BULKHEAD WEB IAW DC-9 SRM CHAPTERS 51-30-1, 51-30-2 AND 51-30-5.SDR 9600732298Bulkhead · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON THE BS 1183 BULKHEAD TO STRINGER 30 JACK PAD FITTING. REPLACED THE FITTING PER SRM 51-10-1.SDR USAA970010Bulkhead Doubler · crackedPIT - DURING AGING VISIT 89K, FOUND 1.125 INCH CRACK IN 591013-13 BULKHEAD DOUBLER, 1.25 INCH CRACK IN 5910130-22 DOUBLER, .25 INCH CRACK IN 5910130-13 DOUBLER, 4.25 INCH CRACK IN THE RADIUS OF 5910130-13 DOUBLER. (M)SDR AU960119Bulkhead · cracked(AUS) FUSELAGE FORWARD DOOR POST BULKHEAD CRACKED IN BOTH RELIEF NOTCHES - CRACK LENGTH 5MM (0.196IN)SDR AU960018Bulkhead · cracked(AUS) FUSELAGE REAR BULKHEAD CRACKED IN AREA OF RH HORIZONTAL STABILISER FORWARD ATTACHMENT FITTINGSDR SWAA960009Bulkhead · crackedDURING SCHEDULED D-CHECK, FOUND BULKHEAD CRACKED 2 PLACES AT BS 178, LBL 5 TO 12 AT WL 201 TO 205, LBL 5.7. REPAIRED PER BOEING SRM.SDR SWAA960008Blkhd Web · crackedDURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178 BBL 0 WL 185. REPAIRED PER BOEING SRM.SDR CAL960135Blkhd Chord · corrodedSTATION 31J - INSPECTION FOUND BULKHEAD REINFORCEMENT CHORD CORRODED ON RIGHT OUTBOARD END AT BS 1176.9. THE CORRODED SECTION OF CHORD WAS REMOVED. A NEW CHORD ANGLE BRACKET REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-6, 51-40-3, 51-40-4, 51-10-1, 51-1SDR ABXA9700691Bulkhead Skin · crackedDURING C-CHECK, WHILE ACCOMPLISHING AD 85-01-02 THE AFT PRESSURE BULKHEAD WAS FOUND CRACKED AT THE RT DOOR JAMB 2 INCHES ABOVE THE FLOOR LINE. THE SKIN WAS REPAIRED IAW DC9 SRM 53-05, FIGURE 76.SDR USAA960020Fitting · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT STATION 727 BULKHEAD STIFFENER FITTING IN LOWER FORWARD RADIUS, BL 0 WL 202.5. REPAIRED PER EO 5394G176. (M)SDR 96ZZZX588Bulkhead · crackedWHILE PERFORMING INSPECTION REQUIRED BY CESSNA SB 95-10A, FOUND CRACK IN TAIL BULKHEAD AT STA 373.56. NEW BULKHEAD INSTALLED AND AREA REINFORCED WITH SK 421-143 KIT INSTALLATION. SUBMITTER SUGGESTS INSPECTION PER SB 95-10A AND KIT INSTALLATION ON 400 SERIES SDR 96ZZZX2787Bulkhead · crackedDURING ROUTINE ANNUAL INSP, DISCOVERED FWD CABIN DOORPOST BULKHEAD CRACKED ON LT AND RT SIDES AT WING LIFT STRUT ATTACH FITTINGS. INSP WAS DONE IAW CESSNA SEB 93-5 R1. PREVIOUS INSP OF THIS AREA DURING ANNUAL AND WHEN C/W CESSNA SEB 93-5, FAILED TO FIND THISSDR 96FDEA00015Chord · crackedSIN - BS 1000 BULKHEAD LOWER CHORD FOUND CRACKED AT LBL 9, APPROX 0.75 AND RBL 9, APPROX 0.75.SDR 96FDEA00014Stiffener · crackedBS 400 BULKHEAD STIFFENER FOUND WITH CORROSION CRACK AT BWL 118, ADJACENT TO S 42L. STIFFENER REPLACED AS PER FEDEX B747 SRM REV 76 51-30-02.SDR 9600651154Bulkhead · crackedDURING T-CHECK, FOUND VERTICAL CRACKS IN A FS 1787 BULKHEAD STANCHION AT LBL 9, 10 INCHES ABOVE THE CARGO FLOOR LINE. REPAIRED STANCHION PER EA 11-104463.SDR 96ZZZX807Box · crackedWHILE PERFORMING PHASE 1-5 INSPECTION, FOUND CRACK ON FORWARD PRESSURE BULKHEAD BOX. CRACK WAS AT RIVET WHICH CONNECTS INSTRUMENT PANEL ANGLE TO BULKHEAD. FACTORY HAD NO APPROVED REPAIR. DER FORM 8110 OBTAINED FOR REPAIR. SUBMITTER STATED THIS IS THE SECONSDR P5CA9600111Bracket · crackedFOUND 4 BRACKETS ATTACHED TO BS 1480 BULKHEAD CRACKED AND BENT. REPAIRED AND REPLACED AS REQUIRED IAW SRM 53-10-22.SDR ABXA9700688Blkhd Stiffener · crackedDURING C-CHECK, WHILE ACCOMPLISHING AD 85-01-02 A STIFFENER ON THE AFT PRESSURE BULKHEAD, UPPER LEFT CORNER WAS FOUND CRACKED. THE STIFFENER WAS REPLACED IAW DC-9 SRM 51-30-2.SDR UPS805480Blkhd Cap · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON BULKHEAD CAP FS 980 LONGERON 34R-35R. REPAIRED PER UPS E.O.SDR 96ZZZM181Bulkhead · crackedSTL - DURING OP-15, FOUND .25 INCH CRACK IN AFT RIGHT LAVATORY FORWARD BULKHEAD, AT OUTBOARD CORNER AT FLOOR LINE. REPAIRED LAVATORY BULKHEAD PER SRM 53-03, FIGURE 31.SDR USAA951360Bulkhead Web · gougedPIT - DURING Q-1/C-3 CHECK INSPECTION, FOUND TOOLING MARKS (GOUGES), 6 INCH BY 4 INCH AREA BETWEEN LONGERON 27L AT BOTTOM LT SIDE OF AFT PRESSURE BULKHEAD. INSTALLED DOUBLER TYPE REPAIR PER SRM 53-03, FIGURE 20. (X)SDR ABXA9600390Blkhd Tee · reqd trimDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THAT WHEN REPLACING THE AFT PRESSURE BULKHEAD LOWER TEE, THERE WAS A REQUIREMENT TO TRIM 1.0 INCH FROM THE TEE SECTION VERTICAL LEG. REPAIRED THE AFT PRESSURE BULKHEAD LOWER TEE IAW ABX REA D953-13901-MR.SDR ABXA9600056Blkhd Stiffener · crackedDURING 826AX MOD-DISCOVERED CRACK ON CENTER STIFFENER AT STATION 1766. REPAIRED HORIZONTAL STIFFENER AT AFT PRESSURE BULKHEAD IAW ABX REA D853-12702MR.SDR GTIA96NK036Bulkhead Web · corrodedDURING C-CHECK, FOUND FUSELAGE BULKHEAD WEB AT STATION Y996 FROM LONGERONS 23 RIGHT TO 23 LEFT AND BETWEEN -Z210 AND -Z240 CORRODED. REPLACED FUSELAGE BULKHEAD WEB IAW SRM 51-01 PARAGRAPH C, SRM 51-30-2, SRM 51-30-5. (M)SDR GTIA96NK031Bulkhead Tee · corrodedDURING C-CHECK, FOUND FUSELAGE BULKHEAD T-CHORD SECTION AT Y604 BETWEEN LONGERONS 28 RIGHT AND 28 LEFT CORRODED. REPAIRED FUSELAGE T-CHORD SECTION IAW DOUGLAS FAX ACTION NR 284374 DATED DEC 6, 1995 AND MD DWG 5934768 VIEW 'C' ZONE 3 AND VIEW 'B' ZONES 8 AND 9SDR USAA951417Blkhd Stiffener · crackedINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK STA 727 BULKHEAD STIFFENER FITTING LBL 25, WL 202.5. REPLACED FITTING. REPAIRED PER SRM 5-10-1. (X)SDR USAA951411Bulkhead · dentedINIT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH DENTED AREA PRESSURE BULKHEAD, STA 727, BULKHEAD RBL 40. REPAIRED OVERSIZED FASTENER HOLES AND INSTALLED REPAIR PER EO. WEIGHT CHANGE LESS THAN 1 POUND. REPAIRED PER EO 5394G068 AND BOEING DSDR 96ZZZM233Blkhd Support · corrodedMCI - DURING OP-16, FOUND CORROSION ON BULKHEAD SUPPORT MEMBER, FS 1320, LBL 25L TO LBL 31L. REPAIRED PER SRM 51-01, PAGE 1C AND TWA STANDARD PRACTICES. (M)SDR CKSA95157Blkhd Angle · corrodedKOSC - DURING C-CHECK INSPECTION, FOUND APB LEFT SIDE FLOOR TO BULKHEAD ANGLE CORRODED. REMOVED AND INSTALLED NEW ANGLE AS IT REQUIRED AS PER IAW DC-8 SRM 53-2-0. (M)SDR 9521039104Blkhd Ftg · crackedDURING H-CHECK, FOUND A CRACK IN THE RIGHT LAV FORWARD BULKHEAD, LOWER AFT INBOARD FITTING. REPLACED FITTING PER SRM 51-30-5.SDR CA960129005Bulkhead · cracked(CAN)WHAT APPEARED TO BE A 1" CRACK WAS DETECTED ON THE FORWARD FACE OF THE LIFT BEAM BULKHEAD P/N 222-031-506-003. IT WAS RADIATING FROM THE LOWER HOLE OF THE AFT LEFT TRANSMISSION NODAL BEAM TO AIRFRAME ATTACHMENT HI LOK PIN HOLE. AN ATTEMPT TO MAP OUT THE SDR CAL960040Bulkhead Fitting · corrodedINSPECTION FOUND CORROSION IN FORWARD CARGO BS 740 BULKHEAD FITTING AT S28L. THE CORROSION WAS CLEANED AND TREATED IAW SRM 51-10-2. L-ANGLE SPLICE WAS FABRICATED AND INSTALLED IAW SRM'S 51-30-2, 53-10-3, 51-10-2, AND 51-20-4. (X)SDR CAL960039Bulkhead Fitting · corrodedINSPECTION FOUND CORROSION IN FORWARD CARGO BS 740 BULKHEAD CORNER FITTING AT S28R. A NEW STRINGER SECTION AND REPAIR SPLICE WERE INSTALLED IAW SRM 51-30-2, SRM 53-10-3, AND ECRA 5340-01256. (X)SDR MWEA95487Blkhd Clip · crackedDURING D-CHECK, FOUND A CLIP CRACKED IN THE RT LAV PRESSURE BULKHEAD AT Z34, STA 996. FABRICATED A NEW CLIP IAW THE SRM 53-01 AND INSTALLED IAW SRM 51-30.SDR HALA95172Frames · crackedHNL - DURING D-CHECK AT SBA, FOUND FUSELAGE SIDEWALL STATION FRAME HAS 1.5 INCH CRACK AT FUSELAGE STATION 734 LEFT AND A 1 INCH CRACK AT FUSELAGE STATION 734 RT. THE CRACKS ARE IN THE RADIUS AT THE LOWER END OF THE FLOOR BEAM ATTACHMENTS. THESE ARE PSE 53.09SDR 95FDEA01890Blkhd Skin · dentedWHILE WORKING 7-5310-7-2301G1, FOUND DENT IN 1342 BULKHEAD SKIN APPROX WL 258 LT. REPAIRED DENT AT BS 1342 BULKHEAD, WL 258 LT. ALL WORK DONE PER FEDEX SRM 54-30-03 AND FEDEX EA 7-5310-26290.SDR DL72S954692Blkhd Web · crackedTHE BS 1183 BULKHEAD WEB WAS FOUND CRACKED IN TWO LOCATIONS AT RBL 18. THERE IS A 1 INCH CRACK AT WL 166.3 TO WL 167.5 AND A .1875 INCH CRACK AT WL 169. THE WEB IS A BONDED ASSEMBLY OF 2024-T3 CLAD WITH A LOCAL THICKNESS OF 0.050 INCH. THE CRACK LOCATIONS ASDR ABXA9600377Blkhd Fitting · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE UPSTANDING LEG OF THE SLANT PRESSURE PANEL FITTING AT FS 699. REPAIRED SLANT PRESSURE PANEL FITTING IAW ABX REA D953-13779-MR.SDR ABXA9600221Blkhd Web · corrodedDURING C-CHECK INSPECTION, FOUND BULKHEAD WEB AT STA 110 CORRODED AT LONGERONS 27R AND 25R. REPAIRED IAW ABX REA D953-13722-MR.SDR 96ZZZX1256Bulkhead · crackedCRACK IN THE RT RUDDER CABLE CUT-OUT HOLE AT THE RT UPPER OUTBOARD RADIUS. ALSO, CRACK FROM RT RUDDER STOP BOLT HOLE UPWARD TO BULKHEAD BEND RADIUS, THEN ALONG BEND RADIUS FOR .3750 INCH. SUSPECT CAUSED BY RUDDER SLAMMING AGAINST STOPS IN GUSTY WIND. SUBMITSDR GTIA96NK106Bulkhead Angle · corrodedDURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT Y218 FORWARD BULKHEAD LOWER ANGLE WITH CORROSION BETWEEN LONGERON 25L AND 25R. REPAIRED ANGLE IAW SRM53-01, FIG 2 SHEET 4. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-0, SDR CA951204007Stiffener · cracked(CAN)RAMP STA 10 BL45 BULKHEAD STIFFENER CRACKED. REPLACED.
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