JASC 5412
Service difficulty reports · 1,087
Reports filed under 5412 · Nacelle/Pylon, Bulkhead/Firewall, 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 = '5412' 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 = '5412' 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 08FDEA00096Bulkhead · damagedWHILE ACCOMPLISHING FX EO F-5450-7-5005 PT, THE NR 1 PYLON MID BULKHEAD FWD RT BOLT HOLE WAS REAMED PER STEP 3.C AND FIG. 9. TOLERANCE FOR MAX DIA SHOULD BE 0.3901- 0.3911". FINAL DIA AFTER REAMING IS 0.3925". HFEC INSPECTED MID BULKHEAD FWD RT BOLT HOLE PSDR DHL2008782002Firewall · crackedUPON INSPECTING THE NR 2 ENGINE FIREWALL, FOUND AN APPROX 2 1/4 INCH CRACK IN AFT WEB AT 8 O'CLOCK POSITION APPROX 6" FROM FLEX ADAPTER. REPAIR WILL BE MADE IAW SRM 54-10-01, 54-10-03 FIG 1 AND M/M 51-30-0.SDR DL76L080029Bulkhead · crackedDURING ACCOMPLISHMENT OF SB 767-54-0080, A CRACK WAS FOUND IN ONE OF THE FASTENER HOLES IN THE AFT BULKHEAD FITTING. THE HOLE WAS REAMED TO REMOVE THE CRACK AND A BUSHING WAS INSTALLED TO RETURN THE HOLE TO THE DESIGN DIAMETER PER ER/A INSTRUCTIONS.SDR DL76L080022Bulkhead · misrepairedDURING ACCOMPLISHMENT OF S/B 767-54-0080, SEVERAL OVERSIZE HOLES WERE FOUND IN THE MIDSPAR WEB AND AFT BULKHEAD WEB. THE HOLES WERE INSPECTED AND OVERSIZE FASTENERS WERE INSTALLED.SDR KCSA081004Bulkhead · gougedNR 4 PYLON UPPER FORWARD ENGINE MOUNT BULKHEAD CHORD NAC STA 128.95 HAS A DEEP GOUGE ON INBOARD SIDE JUST AFT OF CHORD BEND RADIUS AT NOSE COWL FORWARD FAIRING LATCH FITTING.SDR WRNA200800001Bulkhead · chafedDURING B-CHECK WHILE ACCOMPLISHING AD 2007-19-19, NR 1 PYLON STRUT FORWARD ENGINE MOUNT BULKHEAD CORD WAS FOUND WITH CHAFED RADIUS AT LOWER INBOARD END. FABRICATED AND INSTALLED REPAIR ANGLE IAW BOEING SKETCH SR1-733824930-1. THIS REPAIR IS TEMPORARY AND REQSDR LR7A07157Bulkhead · crackedDURING SCHEDULED C-3 CHECK, PER JOB CARD HC7201 FOUND NR 4 ENG NACELLE FWD BULKHEAD RT OUTER CAP TEE CRACKED AT FS 410R PPWL10. REPAIR ACCOMPLISHED IAW LAC MEA 382-54-07-081.SDR LR7A07156Bulkhead · crackedDURING SCHEDULED C-3 CHECK, PER JOB CARD HC7201 FOUND NR 3 ENG NACELLE FWD BULKHEAD RT OUTER CAP TEE CRACKED AT FS 410R PPWL10. REPAIR ACCOMPLISHED IAW LAC MEA 382-54-07-081.SDR SWIA200718804Firewall · crackedLEFT ENGINE FORWARD FIREWALL IS CRACKED AT 12:00 POSITION. REPAIRED IAW EMB120 SRM 51-70-00.
SDR UPS07551131Bulkhead · chafedINSPECTION TYPE:C NR 1 PYLON AFT ENG MOUNT BULKHEAD LWR O/B CORNER OUTER SURFACE IS CHAFED. COMPLIED WITH FINAL EA 757-5453-27-A1757 AND EO B757-5410- 27988-A.SDR KCSA071476Bulkhead · chafedNR 1 PYLON NAC STA 129 BULKHEAD CHORD ANGLE CHAFED.SDR AMTA200700490Bulkhead · gougedDURING MAINTENANCE INSPECTION AT SAA, ATA EO 757-54AD-2456D, THE MID BULKHEAD IB UPPER LUG HOLE WAS GOUGED. C/W SAA EA 757-5450-09-A1048-REV-A. (K)SDR KCSA071464Bulkhead · chafedNR 4 PYLON FWD ENGINE MOUNT BULKHEAD CHORD HAS CHAFING ON FWD OF NAC STA 128.SDR KCSA071458Bulkhead · chafedNR 2 PLYON BULKHEAD CHORD CHAFED AT NAC STA 129.SDR KCSA071457Bulkhead · chafedNR 1 PYLON BULKHEAD CHORD CHAFED AT NAC STA 129.SDR KCSA071455Bulkhead · wornNR 4 PYLON HYD LINE B-NUT WORN INTO NAC STA 221.9 BULKHEAD.SDR KCSA071454Bulkhead · wornNR 3 PYLON ENG PRESSURE LINE AT NAC STA 221.9 WORN INTO BULKHEAD.SDR KCSA071437Bulkhead · crackedNR 4 PYLON NAC STA 179 VERTICAL BULKHEAD HAS SHEARED FASTENER AND CRACKED (1 INCH) IN WEB.SDR KCSA071430Bulkhead · wornNR 1 PYLON FWD ENGINE MOUNT BULKHEAD STA 128.95 CHORD HAS DEEP WEAR AT O/B SIDE.SDR KCSA071429Bulkhead · wornNR 3 PYLON FWD ENG MOUNT BULKHEAD STA 128.95 HAS DEEP WEAR AT I/B LOWER AREA.SDR KCSA071426Bulkhead · crackedNR 4 PYLON STA 221.9 BULKHEAD WEB WHERE HYD LINE GOES THROUGH IS CRACKED .5 INCH.SDR KCSA071425Bulkhead · crackedNR 3 PYLON STA 221.9 BULKHEAD WEB WHERE HYD LINE GOES THROUGH IS CRACKED .75 INCH.SDR QXEA200701459Firewall · crackedC5 PDX - THERE IS A CRACK IN THE RIGHT FIREWALL ABOUT 2" LONG JUST ABOVE AND INBOARD OF THE RIGHT ENGINE FIRE EXTINGUSHING LINE. REPAIRED IAW RD8-54-2396.SDR CA070918007Bulkhead · cracked(CAN) DURING WINTER MAINTENANCE, REAR NACELLE BULKHEAD FOUND CRACKED IN THE RADIUS. BULKHEAD TO BE REPLACED. (TC NR 20070918007)SDR ABXA070299Bulkhead · damagedNR 2 PYLON AFT TORQUE BOX BULKHEAD SIDE BRACE ATTACH LUG HAD LOCK FASTENER HEAD SHEARED OFF LEFT SIDE. REPLACED BROKEN AND MISSING HI-LOKS IAW B767 MM 54-51-03, DC9 SRM 51-40-02, AND DWG 311T3180 AS PER RFTS 42887.SDR 07FDEA03297Bulkhead · corrodedREFERENCE TO SNRM N00486, CORROSION WAS DETECTED AFTER REMOVAL OF NR 3 PYLON AFT MOUNTING BEARING. COMPLIED WITH FEDEX EA NR 1-5410-112388, TITLE: NACELLES AND PYLONS, NR 3 PYLON AFT MOUNT BEARING HOUSING BORE, INTERIM (24 MONTHS) REPAIR. REPAIR CLASSIFIED ASDR 2007UALA03467Bulkhead · gougedNR 1 PYLON, GOUGED BULKHEAD FITTING AT NAC STA 237.39. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA. CUT OUT PREVIOUSLY TRIMMED FLANGE FROM BULKHEAD (P/N 311T3281). FABRICATED A REPAIR ANGLE & A REPLACEMENT BRACKET (272T0082-28) & A REPLACEMENT CLIP (31SDR UPS07550679Bulkhead · chafedINSPECTION TYPE:C NR 2 PYLON, AFT BULKHEAD (RT) OUTBOARD LOWER SURFACE CHAFED. BULKHEAD MILL WAS DONE ON TRAV T7/698748 PER PRELIMINARY 1 EA 757-5453-27-A1738. HFEC WAS DONE ON TRAV T7/698748 PER PRELIMINARY 1 EA 757-5453-27-A1738. 3. 1.25W X 2.1L X .040 REMSDR DL76S071066Bulkhead · crackedDURING HMV AT HAECO, THE NR 2 PYLON AFT BULKHEAD WAS FOUND CRACKED IN ONE HOLE.SDR UPS07550556Bulkhead · chafedINSPECTION TYPE:C NR 1 PYLON AFT BULKHEAD OUTBD SIDE LOWER CORNER CHAFED. BULKHEAD MILL WAS DONE ON TRAV NR T7/696069 PER PRELIMINARY 1 EA 757- 5453-27-A1725 STEP 1. HFEC WAS DONE ON TRAV NR T7/696069 PER PRELIMINARY EA 757-5453-27-A1725 STEP 2. BLEND IS 2.1SDR KCSA071270Bulkhead · crackedNR 2 PYLON, NAC STA 221.9 BULKHEAD LOWER FORWARD OUTBOARD CHORD IS CRACKED IN TWO PLACES.SDR KCSA071269Bulkhead · crackedNR 2 PYLON, NAC STA 221.9 BULKHEAD LOWER TOP CHORD CRACKED ON THE OUTBOARD SIDE.SDR KCSA071266Bulkhead · scratchedNR1 PYLON STA-221, AFT BULKHEAD HAS SCRATCH ABOVE HYDRULIC LINE FEED THROUGH.SDR UPS07550445Bulkhead · chafedINSPECTION TYPE:C NR 1 PYLON AFT BULKHEAD LOWER OUTBOARD CORNER IS CHAFED. BULKHEAD MILL WAS DONE ON TRAV T7/693383 PER PRELIMINARY 1 EA B757-5453-27-A1716. HFEC WAS DONE ON TRAVELER T7/693383 PER PRELIMINARY EA B757-5453-27-A1716. LENGTH OF BLEND 2.1X1.250SDR UPS07550420Bulkhead · chafedINSPECTION TYPE:C NR 1 PYLON AFT BULKHEAD LOWER OUTBOARD CORNER IS CHAFED. BULKHEAD MILL WAS DONE ON TRAV T7/693383 PER PRELIMINARY 1 EA B757-5453-27-A1716. HFEC WAS DONE ON TRAV T7/693383 PER PRELIM EA B757-5453-27-A1716. LENGTH OF BLEND 2.1 X 1.250W X .08SDR KCSA071240Bulkhead · crackedNR 3 PYLON FWD BULKHEAD FRAME AT NAC STA 221 O/B SIDE IS CRACKED 2 INCHES.SDR KCSA071233Bulkhead · crackedAPPROX 3 INCHES CRACK ON NAC STA 221 BULKHEAD WEB LT SIDE APPROX 12 INCHES ABOVE LOWER SPAR.SDR UPS07550242Bulkhead · chafedINSPECTION TYPE:C NR 2 PYLON AFT BULKHEAD LT LOWER/OUTER SURFACE HAS A CHAFED. BULKHEAD MILL AND NDT WERE DONE ON TRAV T7/689654. HFEC WAS DONE ON TR TRAV NR T7/689654. MILLED AREA 1.25W BY 2.1L BY .050 REMOVED ORIGINAL THICKNESS .200, .150 REMAINING. SHOTSDR UPS07550241Bulkhead · chafedINSPECTION TYPE:C NR 1 PYLON, AFT BULKHEAD (LT) LOWER, INNER AND OUTER SURFACE HAS A CHAFED/GOUGES. MILL AND NDT WERE DONE ON TRAV NR T7/689684. HFEC WAS DONE ON TRAV NR T7/689684. MILLED AREA 1.25W BY 2.1L BY .080 REMOVED ORIGINAL THICKNESS SHOT PEENED ARESDR UPS07550240Bulkhead · chafedINSPECTION TYPE:C NR 2 PYLON AFT BULKHEAD RT LOWER/OUTBD SURFACE HAS IS CHAFED. BULKHEAD MILL AND NDT WERE DONE ON TRAV T7/689654. HFEC WAS DONE ON TRAV NR T7/689654. MILLED AREA 1.25W" BY 2.1W BY .040 REMOVED, ORIGINAL THICKNESS .200 REMAINING .160. SHOT PSDR KCSA071193Bulkhead · chafedNR 1 PYLON, HYDRAULIC PRESSURE LINE UNION AT STA 221.9 BULKHEAD CHAFING THRU REPAIR DOUBLER.SDR UPS07550148Bulkhead · dentedINSPECTION TYPE:C GOUGE AT NR 1 LEFT AFT LOWER BULKHEAD (PANEL RACK). BULKHEAD MILL AND NDT WERE DONE ON TRAV T7/682612. FILLER WAS FABED REF TRAV T7/687613 PRELIMINARY 1 EA 757-5453-27-A1688. SHOT PEEN REWORK AREA PER SOPM 20-10-03 AND PRELIMINARY 1 EA 757SDR UPS07550145Bulkhead · chafedINSPECTION TYPE:C NR 2 PYLON AFT BULKHEAD LEFT LOWER OUTBOARD HAS A CHAFED. BULKHEAD MILL AND NDT WERE DONE ON TRAV T7/687615. FILLER WAS FABED REF TRAV T7/687616 PER PRELIMINARY 1 EA 757-5453-27-A1688. SHOT PEEN REWORKED AREA PER PER SOPM 20-10-03 AND PRELSDR DU4R2007131Bulkhead · chafedFOUND CHAFED LOWER OUTBOARD CORNER OF NR 2 PYLON AFT BULKHEAD. REPAIRED BY FABRICATING AND INSTALLING GUSSET 4.34 BY 2.88 BY 1.2 BY .100 FROM 7050-T7451 AND FILLER FROM 15-5PH.125 IAW DELTA ERA 461663-14AD DATED 6/7/07 REV ORIG APPROVED BY FAA FORM 8100-9, WISDR DU4R2007132Bulkhead · chafedFOUND CHAFED LOWER OUTBOARD CORNER OF NR 1 PYLON AFT BULKHEAD. REPAIRED BY FABRICATING AND INSTALLING GUSSET 4.34 BY 2.88 BY 1.2 BY .100 FROM 7050-T7451 AND FILLER FROM 15-5PH.125 IAW DELTA ERA 461663-14AD DATED 6/7/07 REV ORIG APPROVED BY FAA FORM 8100-9, WISDR KCSA071165Bulkhead · crackedNR 1 PYLON HAS APPROX 2.5 INCHES CRACK ON CLOSURE BULKHEAD WEB AT NAC STA 180 BETWEEN WL 138 AND WL 152.SDR UPS07549851Bulkhead · chafedINSPECTION TYPE:C NR 2 PYLON AFT BULKHEAD RIGHT LOWER, OUTER SURFACE CHAFED. BULKHEAD MILL AND NDT WERE DONE REF TRAV T7/679867. START .200 REMOVED .041 REMAINING .159X 1.25W X2.1L. SHOT PEENED REWORKED AREA PER SOPM 20-10-03, FINISHED REWORKED AREA PER SOPSDR UPS07549850Bulkhead · chafedINSPECTION TYPE:C NR 1 PYLON AFT BULKHEAD LT SIDE LOWER AREA CHAFED. BULKHEAD MILL AND NDT WERE DONE REF TRAVT7/679866. START .201 REMOVED .062 REMAINING .139 X 1.25W X 2.1L. SHOT PEENED REWORKED AREA PER SOPM 20-10-03. FINISHED REWORKED AREA PER SOPM 20-43SDR KCSA071158Bulkhead · chafedNR 1 PYLON HYDRAULIC PRESSURE LINE AT NAC STA 221.9 BULKHEAD IS CHAFING.SDR DL757070332Bulkhead · tool damageDURING ACCOMPLISHMENT OF EA 06-070332-03AD (SIP MOD), A HOLE WAS DAMAGED BY A BROKEN DRILL BIT ON THE NR 1 PYLON AFT BULKHEAD. THE DAMAGE REQUIRED THE HOLE TO BE OVERSIZED TO 0.640 AND OVERSIZED FASTENER INSTALLED PER BOEING APPROVAL, AS DETAILED IN ERA 46083
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