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 ABXA010800Strap · corroded#1 PYLON "T" CAP STRAP HAD CORROSION AT WING STATION 485.00, LOWER SPAR CAP, FORWARD SPAR. REMOVED AND REPLACED THE FORWARD SPAR STRAP, REMOVED AND REINSTALLED THE #1 PYLON "T" DOUBLER IAW DC-8 SRM 51-1-20D, 51-1-8.SDR 2002F00182Washer · looseFOUND LEFT PYLON FORWARD SUPPORT LOWER PLUG NR 2 PLI WASHER ROTATES. (M)SDR HNAA0200012Angle · cracked#1 NACELLE HORSECOLLAR FRAME FWD ANGLE CRACKED. REPAIRED ANGLE I.A.W. EO8-54-02-0177.SDR HNAA0200011Angle · cracked#1 NACELLE HORSECOLLAR FRAME FWD ANGLE CRACKED. REPAIRED I.A.W. EO8-54-02-0173.SDR ABXA010795Thrust Link · chafed#2 PYLON THRUST LINK CHAFED ON BOTTOM SIDE FROM PNEUMATIC DUCT CLAMP (REF. EA 5403277MR) REPAIR OR REPLACEMENT PER CARD 8821016, STEP 02.A) REPAIRED AREA IAW DC-8 SRM 51-1-8, MM 71-00-00, SB 54-92 AND REA D854-40959MR.SDR USAA020104Angle · crackedPIT - FOUND ANGLE CRACKED 1 INCH, VERTICAL ANGLE AT STATION 363. DEFECTIVE PART REPLACED WITH IDENTICAL PART. REPLACED CHANNEL PER NR 313A1355. (M)SDR USAA020105Channel · crackedPIT - FOUND CHANNEL CRACKED 12 INCHES, STATION 345-363. DEFECTIVE PART REPLACED WITH IDENTICAL P/N, REPLACED CHANNEL PER NR 313A1355. (M)SDR FPI2002F00000Channel · crackedTHESE AIRCRAFT HAVE AN UPPER AND LOWER FIREWALL CHANNEL AND THE UPPER ALMOST ALWAYS CRACKS BELOW THE ENGINE MOUNT BOLTS. THIS AIRCRAFT HAD BOTH THE LEFT AND RIGHT NACELLES UPPER FIREWALL CHANNELS CRACKED AND HAD TO BE REPLACED WITH NEW.SDR 2001UALA02431Splice · crackedPYLON SPAR ANGLE, LEFT AFT SPLICE CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SPLICE PLATE.SDR ABXA010577Web · crackedLEFT PYLON 45 DEGREE WEB JUST FORWARD OF AFT ENGINE MOUNT CRACKED AT LOWER ATTACH ANGLE. REPAIRED WEB IAW DC-9 SSRM K05159.SDR UPS01237219Hinge · crackedINSPECTION TYPE:C ENG. #2 PYLON, CRACK ON R/H COWLING HINGE CUTOUT AT BS 1376 CRACK ON HINGE CUTOUT STOP DRILLED IAW SRM 51-10-1 REPAIR CARRIED OUT IAW SMRO EO 2001-050-002 UPS ENGINEERING FILE NO 727-54-20016SDR GLBA2001217Panel · separatedPOST FLIGHT INSPECTION FOUND LEFT O/B COWL PANEL MISSING, REPLACED PANELSDR 01FDEA00870Fairing · missing01-329 #3 ENG INBD WING PYLON AFT LOWER FAIRING MISSING. ** S/D ** COMINGSDR 01FDEA00814Pylon · crackedNR 103 CRACK ON LH PYLON LWR SPAR BETWEEN RIB 6&7. R&R PER EO 6-5410-7-3000 A3 PART 3.SDR 01FDEA00813Pylon · crackedNR 102 CRACK ON LH PYLON LWR SPAR BETWEEN RIB 9 & 10. R&R PER EO 6-5450-7-3302B PART 5.SDR 01FDEA00812Pylon · crackedNR 100 CRACK ON RH PYLON LWR SPAR BETWEEN RIB 9 & 10. R&R PER EO 6-5450-7-3320B PART 6.`SDR 01FDEA00800Pylon · crackedNR 103 CRACK ON LH PYLON LWR SPAR BETWEEN RIB 6 & 7. ** S/D ** COMINGSDR 01FDEA00787Pylon · crackedNR 100 CRACK ON RH PYLON LWR SPAR BETWEEN RIB 9 & 10. ** S/D ** COMINGSDR 01FDEA00799Pylon · crackedNR 102 CRACK ON LH PYLON LWR SPAR BETWEEN RIB 9 & 10. ** S/D ** COMINGSDR ABXA010483Angle · crackedTHE UPPER PYLON ATTACH ANGLE WAS FOUND TO BE CRACKED AT THE FORWARD END. MAINTENANCE REPAIRED THE ANGLE IAW DC-9 SRM 54-04 FIG. 10.SDR HNAA0100059Angle · crackedL/H NACALLE HORSECOLLAR AFT FLANGE ANGLE CRACKED. REPLACED ANGLE.SDR HNAA0100058Angle · crackedR/H NACELLE HORSECOLLAR FRAME AFT FLANGE ANGLE CRACKED. REPLACED ANGLE.SDR 0104049858Fitting · corrodedDuring SUV the lower beavertail fitting on the #2 pylon was found with corrosion on the upper and lower surfaces that required replacement. Material AISI 4340 steel forging. Repaired per EA 98-170684SDR 0104029858Fitting · corrodedDuring SUV the lower beavertail fitting on the #1 pylon was found with corrosion on the upper and lower surfaces. Made from AISI 4340 steel forging.Repaired per EA 98-170683SDR 0104019858Fitting · corrodedDuring SUV the upper beavertail fitting on the no 1 pylon was found with corrosion on the upper and lower surfaces. Made from AISI 4340 steel forging.Repaired per EA 98-170682.SDR USAA010991Strut · crackedCLT - FOUND STRUT CRACKED 1.5 INCH, NR 2 PYLON INER CHORD FITTING AT LOWER INBOARD FASTENER HOLE. REPLACED NR 2 PYLON PER EA 85062, BOEING REPAIR NR 6-1171-RE-989. (M)SDR QXEA0101335Stringer · crackedPDX - LEFT-HAND NACELLE DECK STRINGER CRACKED IN TWO PLACES AT STATION XN264.5. REPAIRED IAW HORIZON AIR EA 2-54-95.SDR DHL2001363015Nose Cowl · crackedOn "A" check discrepancy--- #2 engine nose cowl lip cracked at 2 places, at the 8 0' clock position.1) Routed out cracked areas 3 each places nose lip 8 o' clock position I.A.W. A300 S.R.M. 54-30-00 page 731/732 figure 719 view K.2) made doubler repair from 20SDR USAA010919Doubler · crackedCLT - FOUND PYLON INT DOUBLER CRACKED .5 INCH, NR 1 PYLON PP STATION 107, LOWER FORWARD CORNER, PANEL NR 433AL. INSTALLED REPAIR DOUBLER PLATE PER EA 85055. (M)SDR UIEA01083AngleDURING INSPECTION FOUND NR 4 PYLON REAR ENGINE MOUNT OUTBOARD UPPER BULKHEAD ANGLE CRACKED AT FIRST FASTENER COMMON TO THE CENTER LINE OF PYLON. PYLON HAS KIN CAP IN PLACE (PCW). TRIMMED AWAY CRACKS. FABRICATED STRAP AND ANGLE. OVERSIZED EXISTING HOLES IN RSDR UIEA01073Fitting · crackedDURING INSPECTION, FOUND THE NR 4 PYLON STRUT TO DIAGONAL BRACE FITTING WITH ONE SHEARED FASTENER. OVERSIZED HOLE, HFEC OF OVERSIZED HOLE INDICATED A DEFECT IN THE ATTACH FITTING. REMOVED PYLON, REMOVED FITTING, FOUND RADIUS FILLER NOT INSTALLED. PERFORMED SDR UIEA01072Fitting · crackedDURING INSPECTION, FOUND THE NR 1 PYLON STRUT TO DIAGONAL BRACE FITTING CRACKED IN THE COMMON RADIUS OF THE HORIZONTAL TO VERTICAL SUPPORT FLANGE ALONG WITH ONE SHEARED FASTENER. REMOVED PYLON, REMOVED FITTING, FOUND RADIUS FILLER NOT INSTALLED. PERFORMED HFSDR 0104009865Fitting · corrodedDuring SUV the upper beavertail fitting on the No 2 pylon was found with corrosion on the upper and lower surfaces. Fitting AISI steel forging. Repaired per EA 98-183738SDR 0103969865Fitting · corrodedDuring SUV the lower beaver tail fitting on the no 2 pylon was found with corrosion on the upper and lower surfaces and 8 holes oversized. Discrepant beavertail is made from AISI 4340 steel forging.Repaired per EA 98-183737SDR USAA010770Channel · crackedCLT - FOUND CHANNEL CRACKED .75 INCH, BS 310.5, LBL 20, FORWARD SIDE OF FLOORBEAM. REMOVED AND REPLACED PER SRM 51-40-02. (M)SDR ABXA010367Doubler · crackedRIGHT PYLON INTERIOR UPPER ANGLE FORWARD OF AFT ENGINE MOUNT ABOVE ENGINE CANNON PLUGS CRACKED. INSTALLED DOUBLER IAW DC-9 REA D954-41543.SDR USAA010602Tie Clip · crackedCLT - FOUND STRINGER TIE CLIP CRACKED .25 INCH, BS 747, STRINGER 7L. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-02. (M)SDR USAA010596Frame · corrodedCLT - FOUND FRAME CORRODED APPROXIMATELY 4 SQUARE INCH AREA, BS 847, ABOVE STRINGER 25R. REMOVED DAMAGED SECTION, REPLACED SECTION PER BOEING DRAWING NR 65C35243 AND EA69063. (M)SDR UIEA01055Doubler · wornDURING INSPECTION OF NR 3 PYLON ACCESS PLATE CUTOUT (473AR) NAC STATION 290 WL 145, THE CONTACT AREA OF THE INNER SKIN TO LATCHES WAS FOUND WORN (THREE PLACES). AREAS TRIMMED OUT. HFEC INSPECTED AREAS FOR CRACKS, NONE FOUND. FABRICATED AND INSTALLED CRES-STSDR ERKR200100127Fitting · damagedNR 2 ENGINE PYLON, FORWARD MOUNT, OVERSIZE HOLES. DURING SCHEDULED MAINTENANCE INSPECTION OF THE AIRPLANE CRACKS WERE FOUND IN THE INBOARD AND OUTBOARD HANGER FITTING UPPER ATTACHMENT HOLES. THE CRACKS WERE REMOVED BY OVERSIZING, AND NDT INSPECTED TO ASSURE SDR ERKR200100126Fitting · damagedALTERNATE FASTENERS FOR NR 1 PYLON FWD INBOARD HANGER FITTING REWORK. A DEVIATION TO THE SERVICE BULLETIN 747-54A2203 WHICH CONSISTS OF USING LARGER FASTENER SIZES OF THE SAME TYPE AS LISTED IN THE SERVICE BULLETIN PER ECRA 3203-54-034-2.SDR CA010511005Rod · loose(CAN) AIRCRAFT ENROUTE TO MONTERREY, THE CREW WERE UNABLE TO RETARD THE LEFT HAND THROTTLE LOWER THAN 95 PERCENT. THE CREW RETURNED TO MEMPHIS AND CARRIED OUT QRH ABNORMAL 1-14. MECHANICS FOUND THE HOLD OPEN STRUT OF THE LT ENGINES UPPER CORE COWL JAMMED BETWSDR 2001UALA00251Web · crackedNR 2 PYLON UPPER WEB AT IDG CABLE HOLE ACCESS HAS TO CRACKS. INSTALLED REPAIR DOUBLER REF: 54-53-02.SDR 2001UALA00250Web · crackedNR 1 PYLON UPPER WEB AT IDG CABLE HOLE ACCESS HAS 2 CRACKS AT NP HOLES. INSTALLED REPAIR DOUBLER REF: SRM 54-53-02.SDR 2001UALA00246Web · crackedNR 1 PYLON WEB CRACKED AT OUTBOARD DRAIN HOLE JUST FORWARD OF IDG CUTOUT INSIDE PANEL 441DT. INSTALLED REPAIR DOUBLER REF: SRM 54-53-02.SDR TWAA0103803Structure · crackedDURING OP 15 MAINT CHECK NUMBER 2 ENGINE PYLON FAIRING STRUCTURE ON LOWER SIDE, FWD END HAD A CRACK BETWEEN TWO RIVETS. INSTALLED REPAIR PER SRM 54-01, PAGE 6.SDR QXEA0100116Stiffener · crackedPDX- LOWER FINGERNAIL DECK OUTBOARD FORE/AFT STIFFENER IS CRACKED AT GEARWELL WALL VERTICAL STIFFENER OF LEFT HAND NACELLE. REPAIRED IAW DHC-8 SRM 51-40-11 AND 51-20-16.SDR QXEA0100115Stiffener · chafedPDX- FINGERNAIL DECK STIFFENER CHAFED THIN AT XN232.0 TOP SIDE. REPAIRED IAW DHC-8 SRM 51-40-11 AND 51-20-16.SDR DHL2001367522Pylon · damagedC-CHECK, DAMAGED PYLON INSPECTED AND REMOVED FOR REPAIR. PYLON ROUTED FOR REPAIR. REPAIRED PYLON FITTED AND RE-INSTALLED ON AIRCRAFT PER AIRBUS A300 MM.SDR USAA002188Crossbeam · corrodedPIT - CROSSBEAM FOUND WITH WEAR AND CORROSION IN BEARING BORE, .006 DEPTH. LEVEL 1 CORROSION. OPEN BORE UP FOR OVERSIZE BEARING RECHAMFER MPI ROTO PEEN. INSTALLED NEW BEARING, TYP REP 54-50-09. (M)
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