JASC 5400
Service difficulty reports · 1,907
Reports filed under 5400 · Nacelle/Pylon Structure, 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 = '5400' 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 = '5400' 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 P5CA9600750Sill · crackedCRACKED SILL ON NR 4 PYLON LEFT SAILBOAT DOOR. FABRICATED AND INSTALLED SILL PER BOEING SRM 51-30-02 AND 51-10-01.SDR C2XA96IA253Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT NACELLE FRAME 2 ATTACH ANGLE WAS FOUND TO BE CRACKED. MX REMOVED AND REPLACED THE ANGLE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA96IA252Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT NACELLE FRAME 2 ATTACH ANGLE WAS FOUND TO BE CRACKED. MX REMOVED AND REPLACED THE FRAME AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR DL72K962292S-Duct Web · crackedDURING ACCOMPLISHMENT OF EO 4-59253-12 OPN 0120, FOUND .5 INCH VISIBLE CRACK IN LOWER LT CORNER OF VERTICAL WEB CROSSING NR 2 ENG INLET S-DUCT AT STA 1303. STOP DRILLED CRACK PER SRM 53-10-4 PG 65, INSTALLED DOUBLER PER SRM 53-10-4.SDR DU4R9600014Doubler · crackedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND FINGERS DOUBLERS HAD NUMEROUS CRACKS AND CORROSION ON LT NR 1 ENGINE PYLON BOTTOM PANEL.SDR P5CA9600737Rib · corrodedLEVEL 1 CORROSION NR 1 PYLON FIRE BOTTLE SUPPORT RIB. REMOVED CORROSION PER BOEING SRM 51-10-01 TREATED PER BOEING SRM 51-10-02.SDR EISA96240Rib · crackedFOUND NR 3 ENGINE PYLON RIB CRACKED, ACCESS THROUGH PANEL 5510. BLENDED DAMAGED AREA, FABRICATED AND INSTALLED PER SRM 54-20-03. (M)SDR EISA96239Pylon · crackedFOUND NR 1 ENGINE PYLON TRAILING EDGE CRACKED JUST AFT OF BULB SEAL. FABRICATED NEW TRAILING EDGE ANGLES AND INSTALLED PER SRM 53-20-02. (M)SDR MALA965121Angle · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND REPAIR ANGLE ON LEFT NACELLE INBOARD LOWER 'WING TO NACELLE' ATTACH ANGLE CRACKED. REMOVED PREVIOUS REPAIR ANGLE, FABRICATED AND INSTALLED NEW REPAIR ANGLE IAW ARP 54-20-9101, REV. B. (X)SDR MWEA96481Angle · crackedDURING INSP, LT PYLON TO FUS UPPER ATTACH ANGLE WAS FOUND CRACKED AT STA 935, 965 AND 1019. COMPLETED REPAIRS IAW SRM 54-04, FIG 10.SDR MWEA96480Angle · crackedDURING INSP, RT PYLON TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED IN 2 PLACES FWD EDGE OF LEADING EDGE. INSTALLED A REPAIR IAW SRM 54-04, FIG 10.SDR C2XA96IA229Angle · crackedIAH - INSPECTION: 1C, 2C, 4C. TOTAL TIME: 12,085.2 HOURS. TOTAL CYCLES: 17,466. DURING A ROUTINE INSPECTION, THE LT NACELLE WAS FOUND TO HAVE A CRACKED SUPPORT ANGLE AT FRAME NR 2. MAINTENANCE REMOVED ANE REPLACED SUPPORT ANGLE AT NACELLE FRAME NR 2. SDR C2XA96IA228Angle · crackedIAH - INSPECTION 1C, 2C, 4C. TOTAL TIME: 12,085.2 HOURS. TOTAL CYCLES: 17,466. DURING A ROUTINE INSPECTION, THE RT NACELLE WAS FOUND TO HAVE A CRACKED SUPPORT ANGLE AT FRAME NR 2. MAINTENANCE REMOVED AND REPLACED SUPPORT ANGLE AT NACELLE FRAME NR 2. AIRSDR UPS96821304Doubler · crackedINSPECTION TYPE: CS2. NR 2 PYLON LOWER DOUBLER JUST ABOVE T-DOUBLER CRACKED ON FWD SIDE. REPAIRED PER UPS EO'S DC8-57-0717/-0726.SDR P5CA9600717Angle · tornNR 3 ENGINE INBOARD COWL INNER ANGLE TORN AT LATCH. REPAIRED COWL PER BAC SRM 51-10-02 AND 51-10-01.SDR 96FDEA01435V-Panel · missingUPON WALK AROUND, FOUND THE V-PANEL ON NR 3 ENGINE PYLON RIPPED AWAY. INSTALLED V-PANEL ON PYLON FARING. ALSO, REPAIRED DAMAGED PYLON FARING HONEYCOMB PANEL OUTBOARD PER DC-10 STRUCTURE REPAIR MANUAL 51-10-00.SDR MWEA96427Angle · crackedDURING INSP, FOUND ANGLE BENEATH LT PYLON AT STA 996 CRACKED 1 INCH. INSTALLED REPAIR IAW SRM 54-04, FIG 10.SDR UPS96421180Heat Shld Baffle · crackedINSPECTION TYPE-C, AT THE FWD LOWER SPAR WEB PYLON NR 4 HEAT SHEILD BAFFLE CRACKED AT SEVERAL PLACES. REPLACED HEAT SHIELD BAFFLE AT THE FWD LOWER SPAR WEB ACC SRM 51-3 0-02.SDR UPS96421179Heat Shld Baffle · crackedINSPECTION TYPE C, AT THE FWD LOWER SPAR WEB PYLON NR 1 HEAT SHIELD BAFFLE CRACKED AT SEVERAL PLACES. REPLACED HEAT SHIELD BAFFLE AT THE FWD LOWER SPAR WEB ACC SRM 51-30 -02.SDR UPS96421178Heat Shld Baffle · crackedINSPECTION TYPE-C, AT THE FWD LOWER SPAR WEB PYLON NR 3 HEAT SHIELD BAFFLE CRACKED AT SEVERAL PLACES. REPLACED HEAT SHIELD BAFFLE AT THE FWD LOWER SPAR WEB ACC SRM 51-30-02.SDR UPS96421177Spar Web · crackedINSPECTION TYPE-C, AT THE FWD LOWER SPAR WEB PYLON NR 2 HEAT SHIELD BAFFLE CRACKED AT SEVERAL PLACES. REPLACED HEAT SHIELD BAFFLE AT THE FWD LWR SPAR WEB ACC SRM 51-30-02.SDR 9619119910Spar · corrodedDURING M-CHECK, FOUND CORROSION ON THE LEFT PYLON FRONT LOWER SPAR CAP BEAVER TAIL. REPLACED SPAR CAP (P/N 5923937-1) PER SRM 54-04, FIG 13 AND DWG 9958161.SDR UPS96821105Angle · crackedINSPECTION TYPE-CS2, NR 4 PYLON DRAG ANGLE CRACKED .25 INCH LONG PAST STOP DRILL. REPAIRED ANGLE PER TASK CARD 8040-01, STEP 4.SDR MALA965097Angle · damagedDURING SCHEDULED MAINTENANCE IN MSP, A CRACK WAS NOTED IN THE LEFT INBOARD LOWER WING TO NACELLE SKIN PATCH. MAINTENANCE REPLACED THE LEFT INBOARD UPPER WING SKIN TO NACELLE ATTACH ANGLE, P/N 27-35112, LEFT INBOARD NACELLE FORMER, P/N 27-35025, STRINGER LOCATSDR 96ZZZM1296Angle · damagedDURING SCHEDULED MAINTENANCE IN MSP, A CRACK WAS NOTED IN THE LEFT INBOARD LOWER WING TO NACELLE SKIN PATCH. MAINTENANCE REPLACED THE LEFT INBOARD UPPER WING SKIN TO NACELLE ATTACH ANGLE, P/N 27-35112, LEFT INBOARD NACELLE FORMER, P/N 27-35025, STRINGER LOCATSDR UPS96520826Fuse Pin · crackedOUTBOARD FUSELAGE ON NR 2 ENGINE PYLON CRACKED. INBOARD AND OUTBOARD FUSELAGE PINS REPLACED. COMPLIED WITH EO B757-5440-0431-1 APPENDIX F, COMPLIED T/C 5001 (PW) REMOVAL AND INSTALLATION OF NR 2 (RT) ENGINE.SDR P5CA9601220Skirt Clamp · brokenSKIRT NR 4 CLAMP UNDER RETURN LINE BROKEN. CLAMP REPLACED PER MM 20-11-24.SDR P5CA9601219Skirt · corrodedSKIRT NR 4 SUPPORT RODS EYEBOLTS CORROSION. CORROSION REMOVED AND TREATED PER MM 51-21-03.SDR P5CA9601218Skirt · chafedSKIRT NR 1 FWD BRIDGE ABOVE PRESS MODULE CHAFED. SMOOTHED CHAFED AND AREA TREATED PER SRM 51-40-03.SDR P5CA9600603Bracket · chafedFOUND TRIANGLE BRACKET UNDER NR 2 PYLON AFT FAIRING CHAFED. INSTALLED NEW BRACKET WITH RIVET AS PER SRM 51-30-02.SDR USAABB96023Fairing · dislodgedCLT - FLT 41 - CREW NOTED, THAT SOMEWHERE BETWEEN TAKEOFF FROM CLT AND 8000 FEET, A NR 1 ENGINE PYLON COVER DEPARTED THE AIRCRAFT. FLIGHT RETURNED TO THE FIELD AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE PANEL. SUBMITTER STATES, MOST LIKELSDR UPS96420915Skate Angle · crackedINSPECTION TYPE: C. SKATE ANGLE PYLON NR 1 RT HAS CRACKS AT THE TWO FIRST FASTENER HOLES. REPAIRED IAW KLM DFX 96-180 / EFN 747-54-0132.SDR P5CA9600446Fairing · wornNR 4 PYLON INBOARD SIDE AFT FAIRING SECTION WORN NAC STA 270. FABRICATED AND INSTALLED NEW PART PER BOEING SRM 54-30-03.SDR MWEA96324Angle · crackedDURING D-CHECK, RT PYLON FRAME UPPER FLANGE FOUND CRACKED AT STA 1059 OUTBD OF FIREWALL. REPLACED ANGLE IAW SRM 51-302.SDR MWEA96317Fitting · crackedDURING D-CHECK, LT PYLON ATTACH FITTING WAS FOUND CRACKED IN AFT INBD CORNER OF THE CANNON PLUG COMPARTMENT. REPLACED CRACKED FITTING IAW SRM 51-01 AND 51-30-1.SDR MWEA96307Fitting · crackedDURING D-CHECK, A CRACKED FITTING WAS FOUND IN RT PYLON. FABRICATED A NEW FITTING IAW DAC SWG 4919864, INSTALLED IAW SRM 51-30-1 AND 51-30-5.SDR C2XA96IA179Angle · crackedIAH - DURING C-CHECK INSPECTION, THE ATTACH ANGLE ON THE LEFT ENGINE NACELLE FRAME 2 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE ATTACH ANGLE AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR C2XA96IA178Angle · crackedIAH - DURING C-CHECK INSPECTION, THE ATTACH ANGLE ON THE NR 2 FRAME OF THE RIGHT NACELLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE ANGLE AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR P5CA9600390Doubler · crackedCRACKED DOUBLER ON NR 4 PYLON LEFT SIDE AFT OF REAR MOUNT AREA. REMOVED DOUBLER, FABRICATED, AND INSTALLLED NEW DOUBLER PER BOEING SRM 54-10-03.SDR P5CA9600379Bracket · crackedNR 2 ENGINE AIR DUCT MOUNT ANGLE BRACKET IS CRACKED AT THE 6 O'CLOCK POSITION FORWARD OF MAIN GEARBOX. FABRICATED ANGLE AND INSTALLED IAW SRM 51-10-01.SDR P5CA9600598Acoustic Panel · debondedDEBONDING AT NR 3 NOSE COWL 11 O'CLOCK POSITION ACOUSTIC PANEL. REPAIRED PER BAC SRM 54-30-03 FIG 29.SDR AALA961060Spar Web · gougedTULE - FOUND GOUGE IN LOWER AFT SPAR WEB. REPAIRED PER ESO 7349 DATED 7-11-96. (M)SDR C2XA96IA170Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT NACELLE FRAME 2ATTACH ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THEAFFECTED ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.(M)SDR C2XA96IA169Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT NACELLE FRAME 2 ATTACHANGLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTEDANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.(M)SDR P5CA9600338Angle · crackedNR 1 OUTBOARD CORE COWL HAS CRACKED REPAIR ANGLE INSIDE TO EDGE AT BEND. REMOVED, FABRICATED AND INSTALLED ANGLE IAW BOEING SRM 51-30-02 AND 51-10-01.SDR P5CA9600333Angle · crackedNR 4 ENGINE PYLON UPPER END OF SUPPORT ANGLE CRACKED IN RADIUS INBOARD AND OUTBOARD STATION 221.9 ABOVE AFT ENGINE MOUNT INSIDE PANEL. INSTALLED DOUBLERS IAW BOEING SRM 54-10-03 FIG 19.SDR P5CA9600330Angle Bracket · crackedNR 4 ENGINE PYLON, ANGLE BRACKET BENT AND CRACKED INBD AFT. REMOVED, FABRICATED AND INSTALLED BRACKET PER BOEING SRM 51-32-01 AND 51-10-02.SDR P5CA9600329Bracket · crackedCRACKED SUPPORT BRACKET NR 4 PYLON, GENERATOR LEAD SUPPORT. REMOVED, FABRICATED AND REPLACED BRACKET PER BOEING SRM 51-30-02 AND 51-10-01.SDR 96FDEA01207Cowl Stiffener · crackedSNRM NR 4225, NR 2 ENGINE NOSE COWL BLKHD STIFFENER ON DUCT WEB CRACKED 10 O'CLOCK POS AS SEEN THROUGH PANEL 361 KL.SDR SCNA96189S-Duct · corrodedDURING MAINTENANCE INSPECTION, CORROSION WAS FOUND IN THE INLET OF THE S-DUCT ON ENGINE 2. REMOVED CORROSION, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH B727 SRM 54-10-03 FIGURE 8.
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