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 95FDEA01393Spar Web · crackedNR 1 ENG PYLON UPPER SPAR WEB CRACKED AT OUTBOARD CORNER (APPROX 5). REMOVED AND REPLACED SPAR WEB. REPAIRED PER EA 8-5410-20129. REPLACED NR 1 PYLON AFT BULKHEAD FITTING AND REPAIRED UPPER WEB. SEE EA FOR DETAILS.SDR 95FDEA01311Spar Web · crackedNR 1 ENG PYLON UPPER SPAR WEB CRACKED AT O/B CORNER, APPROX 5 INCHES. REMOVED AND REPLACED SPAR WEB.SDR 9514156624Fitting · crackedDURING PERIODIC CHECK, FOUND A CRACK IN THE NR 3 STRUT DIAGONAL BRACE FORWARD ATTACH FITTING. REPLACED FITTING.SDR MALA954623Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE RT OUTBOARD UPPER FORWARD WING SKIN TO NACELLE ATTACH ANGLE CRACKED. THEY STOP DRILLED THE CRACK AND FABRICATED AND INSTALLED A REPAIR DOUBLER IAW FAIRCHILD ARP 54-20-9101. (M)SDR MALA954622Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE RT OUTBOARD LOWER FORWARD WING SKIN-TO-NACELLE ATTACH ANGLE CRACKED. THEY STOP DRILLED THE CRACK AND FABRICATED AND INSTALLED A REPAIR DOUBLER IAW FAIRCHILD ARP 54-20-9101. (M)SDR 96ZZZM413'S' Duct · corrosionDURING C-CHECK, FOUND NR 2 ENGINE 'S' DUCT STATION 1332 TO 1342 RIB 35 AT 6 O'CLOCK (BOTTOM) SKIN BULGED AND CRACKED. REMOVED CORROSION AS PER SRM 51-10-6 AND CUT DAMAGED SECTIONS 4 INCHES BY 5 INCHES AND 1 INCH BY 1 INCH TREATED AND PAINTED PER SRM 51-10-2, SDR 9514829990Angle · crackedDURING LINE CHECK, FOUND A CRACK IN THE LEFT PYLON UPPER SKATE ANGLE FS 1104. REPAIRED ANGLE PER EA 99-99246.SDR DLM88953583Angle · crackedA .75 INCH CRACK IN REPAIR ANGLE UPPER ATTACH ANGLE ON NR 1 ENG PYLON AT AFT END. CRACK WAS FOUND AT F-2 LTR CK. REPLACED ANGLE PER SRM 54-04A PG 17 FIG 4.SDR P5CA9500724Fairing Mount · crackedPYLON NR 2 INBOARD SIDE FAIRING MOUNT IS CRACKED. REPAIRED PER BOEING SRM 54-10-00.SDR MALA954606Angle · crackedMSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND THE LEFT NACELLE INBOARD WING TO NACELLE ATTACH ANGLE CRACKED AT THE 9TH RIVET HOLE OF THE FORWARD END. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW FAC ARP 54-20-9101. (X)SDR MALA954605Angle · crackedDURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE RIGHT NACELLE INBOARD UPPER WING SKIN TO NACELLE ATTACH ANGLE CRACKED AT THE 10TH RIVET HOLE OF THE FORWARD END. REPAIRS WERE COMPLETED BY INSTALLING A DOUBLER IAW FAC ARP 54-20-9101. (X)SDR DL72S953507S-Duct · crackedFWD EDGE OF UPPER S-DUCT INNER SKIN CRACKED AT APPROX 6 O'CLOCK POSITION. REPAIRED PER SRM 54-10-3 FIG 9.SDR CAL950762Skin · crackedHOU - INSPECTION FOUND A .5 INCH CRACK IN SKIN ON TOP SIDE OF NR 2 ENGINE PYLON. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-02. (M)SDR MALA954598Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, THE LEFT INBOARD WING TO NACELLE TRANSIT ANGLE WAS CRACKED. REPAIRS WERE COMPLETED BY STOP DRILLING THE CRACK AND INSTALLING A REPAIR DOUBLER IAW ARP 54-20-9101. (M)SDR 95ZZZX5739Bracket · screws looseNACELLE BRACKET SCREWS WORKED LOOSE CAUSING THE BRACKET TO CHAFE ON THE SKIN AND STIFFENER WHICH, IN TURN, CAUSED THE SKIN TO CRACK. SUBMITTER RECOMMENDS CHECKING THESE SCREWS ON A 25-50 HOUR BASIS. THIS IS THE SECOND AIRCRAFT FOUND WITH THIS CONDITION, BOTHSDR MALA954595Former · crackedMSP - DURING A SCHEDULED INSPECTION, THE LT INBD FORMER, PN 27-35025-067, AND STR, PN 27-35041-012, WERE FOUND CRACKED AT NACELLE STA 120.00. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING REPAIR DOUBLERS IAW FAC LAR NR 95-MALA-225. (X)SDR DL72S953510S-Duct · crackedINNER SKIN OF THE FWD SECTION OF S-DUCT IS BENT AND CRACKED AT APPROX 12 O'CLOCK POSITION. REPAIRED PER SRM 54-10-3.SDR P5CA9500710Stiffener · crackedCRACKED STIFFENER, NR 3 PYLON NACELLE, STATION 180 INBOARD SIDE, REPAIRED PER BOEING SRM 54-1003 FIG. 15.SDR CAL950828Channel · crackedHOU - INSPECTION FOUND A 10 INCH CRACK IN LEFT PYLON SPAR WEB CHANNEL ON INBOARD EDGE AT STATION 305-315. THE AREA WAS REPAIRED IAW SRM 51-10-02 AND IN REF TO BOEING DRAWING NR 313A1355. (M)SDR CAL950737Channel · crackedIAH - INSPECTION FOUND TWO 'Z' CHANNELS CRACKED AT TOP OF CANNON PLUG COMPARTMENT OF NR 1 ENGINE PYLON. THERE WERE THREE CRACKS MEASURING 4.125 INCHES, 1.5 INCHES AND 1.25 INCHES LONG. TWO NEW 'A' CHANNELS WERE FABRICATED AND INSTALLED IAW SRM 54-10-0, PAGE SDR 95ZZZM477Bracket · crackedDURING AREA 'A' INSPECTION, LEFT INBOARD TOP FORWARD COWL ATTACH BRACKET WAS FOUND TO HAVE A SMALL CRACK. WELDED CRACK AND RETURNED TO SERVICE.SDR 95ZZZM476Bracket · crackedDURING THE AND INSPECTION, FOUND CRACK IN THE TOP FORWARD TOP OUTBOARD COWLING ATTACH BRACKET. WELDED CRACK AND RETURNED TO SERVICE. (M)SDR 9519069925Angle · crackedDURING LINE CHECK, FOUND A CRACK IN THE RIGHT PYLON LOWER ATTACH ANGLE AT FS 1019. REPAIRED PER EA 99-98960.SDR P5CA9500760Brackets · crackedCRACKED LATCH SUPPORT BRACKETS, 2ND AND 4TH FROM FRONT ON NR 3 PYLON INBOARD TRAILING EDGE DOOR. REPLACED BRACKETS.SDR P5CA9500742Fairing · crackedCRACKED FAIRING NR 4 STRUT FORWARD. REPAIRED PER BOEING SRM.SDR P5CA9500698Fairing · crackedNR 3 PYLON LOWER AFT FAIRING CRACKED ON RIGHT SIDE AND HAS LOOSE AND MISSING FASTENERS ON BOTH SIDES. REPAIRED PER BOEING SRM 51-40-02.SDR ABXA9500847Angle · crackedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-8, FOUND LEFT UPPER PYLON ANGLE CRACKED ATSTA 860. REPAIRED IAW DC-9 SRM 54-04 FIG 10.SDR MALA954566Angle · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL FOUND THE LT NACELLE INBOARD LOWER WING SKIN TO NACELLE ATTACH ANGLE CRACKED AT SEVERAL RIVET HOLES ON THE FORWARD END. THEY REPLACED THE FORWARD 20 INCHES OF THE ANGLE AND INSTALLED A DOUBLER OVER THSDR COM11931Latch Assy · brokenLEFT ENGINE INBD NACELLE LATCH IS BROKEN. REPLACED LATCH.SDR PLGA716952Keel Web · crackedDURING A WING INSPECTION, THE LEFT ENGINE NACELLE OUTBOARD UPPER KEEL WEB (P/N 114-980022-1) WAS FOUND TO HAVE ONE CRACK ON THE FORWARD FLANGE. THE CRACK RAN VERTICALLY BETWEEN THE FORWARD ATTACHING RIVETS. THE KEEL WEB WAS REPAIRED IAW AERODESIGN ENGINEERINSDR PLGA716951Keel Web · crackedDURING RIGHT ENGINE CHANGE THE NACELLE INBOARD UPPER KEEL WEB (P/N 114-980021-2) WAS FOUND TO BE CRACKED ON THE FORWARD FLANGE. THE CRACK WAS APPROXIMATELY 4 INCHES IN LENGTH RUNNING VERTICALLY BETWEEN THE ATTACHMENT RIVETS ON THE FORWARD FLANGE. THE KEEL WASDR PLGA71095GKeel Web · crackedDURING INSPECTION THE LEFT ENGINE NACELLE OUTBOARD UPPER KEEL WEB (P/N 114-980022-1) WAS FOUND TO HAVE TWO CRACKS ON THE FORWARD FLANGE. BOTH CRACKS RAN VERTICALLY ON THE FLANGE. ONE CRACK WAS BETWEEN THE TWO CENTER ATTACH RIVETS APPROXIMATELY 1 INCH IN LENGSDR 96ZZZM597S-Duct · corrosionDURING D-CHECK, FOUND NR 2 ENGINE INLET 'S' DUCT HAS INNER SKIN BULGE AT 6 O'CLOCK BETWEEN 10-21 INCH FORWARD OF LOWER AFT EDGE. REMOVED FASTENERS PER SRM 51-30-2. CLEANED CORROSION INNER SKIN PER SRM 51-10-6 MATERIAL LOSS .003. FOUND CRACK AT BETWEEN 10-21SDR 95ZZZM259Fitting · crackedAFTER REMOVING NR 1 PYLON INTERMEDIATE PLANK FOR REPAIR, FOUND A CRACKED TEE FITTING ON THE INBOARD SIDE OF PYLON AT YN 336.750. REMOVED FITTING, FABRICATED NEW FITTING AS PER DOUGLAS DRAWING NR 5753022, TEE FITTING NR 3753027-2 UNDER DOUGLAS AT AUTHORIZATIONSDR P5CA9500648Bracket · crackedCRACKED BRACKET NR 1 PYLON NS 253 INTERNAL ON LEFT WALL. MANUFACTURED NEW BRACKETS PER BOEING SRM 54-10-02.SDR P5CA9500639Eye Bolts · corrodedPYLON SKIRT NR 1 SUPPORT ROD EYE BOLTS CORRODED. INSTALLED NEW ROD PER BOEING M/M 20-50-01.SDR P5CA9500607Angle · brokenBROKEN INTERNAL FRAME ANGLE CORNER NR 3 PYLON NS 270. REPAIRED PER BOEING SRM 54-10-02.SDR P5CA9500597Chord · crackedEDDY CURRENT INSPECTION PER SB 54-2159, FOUND CRACK IN NR 4 PYLON HORIZONTAL CHORD LEFT SIDE. REAMED HOLE, INSTALLED FREEZE PLUG PER BOEING SB 54-2159, CRACK CLEANED UP.SDR P5CA9500558Bracket · cracked2 CRACKS ON NR 2 PYLON SKIRT FORWARD MOUNTING BRACKET. FABRICATED NEW BRACKET PER BOEING SRM 54-50-02.SDR P5CA9500550Bracket · crackedCRACKED BRACKET NR 2 PYLON SKIRT RETURN MODULE MOUNTING BRACKET LEFT SIDE. MANUFACTURED NEW PART PER SRM 54-12-02, INSTALLED PER 51-30-02.SDR P5CA9500524Bracket · crackedCRACKED FORWARD SKIRT MOUTNING BRACKET NR 4 PYLON. REPLACED FITTING PER BOEING SRM 51-30-02.SDR P5CA9500523Bracket · damagedDAMAGE FWD SKIRT MOUTNING BRACKET NR 1 PYLON. INSTALLED NEW FITTING PER 51-30-02.SDR P5CA9500510Bracket · elongated holeCORROSION ON PNEUMATIC DUCT ATTACH BRACKET ON NR 3 NACELLE FIRE WALL NS 195 LEFT SIDE. ALSO, ELONGATED BOLT HOLE AND BADLY CHAFED. REPAIRED PER BOEING SRM 54-10-02. REPLACED FOR ELONGATED HOLE, NOT A LEVEL 2.SDR P5CA9500455Angle · wornANGLE WORN AND MISSING FASTENERS IN NR 3 PYLON SKIRT RIGHT FORWARD SIDE. REPAIRED PER BOEING SRM 51-40-01 AND 51-30-02.SDR P5CA9500380Hinge · brokenBROKEN HINGE AND LOOSE RIVETS ON BLOW OUT PANEL AT NR 3 RIGHT PYLON FAIRING DOOR. REPAIRED PER BOEING SRM 51-30-02.SDR P5CA9500379Fairing Door · corrodedCORROSION AND SMALL CRACK ON LOWER EDGE NR 2 PYLON FAIRING EXTERIOR SURFACE SKIN. REMOVED CORROSION AND CRACK PER BOEING SRM 51-10-01.SDR P5CA9500378Fairing Door · chafedNR 4 STRUT LEFT FAIRING DOOR INTERNAL LOWER CHORD SKIN IS GOUGED AND CHAFED BADLY. REPAIRED PER BOEING SRM 51-10-01, 53-50-00, AND 51-10-02.SDR 96ZZZX1862Apron · crackedDURING C-CHECK, FOUND NR 2 ENGINE UPPER APRON STRUCTURE CRACKED APPROXIMATELY 14 INCHES AFT OF UPPER ISOLATOR. REPAIRED IAW DC9 SRM CH 54. AIRCRAFT TT: 35,252. AIRCRAFT TC: 51,897.SDR P5CA9500240Fairing · damagedHOLE ON UNDER WING AT TRAILING EDGE FAIRING RIGHT SIDE NR 1 PYLON. REPAIRED PER 51-40-02.SDR P5CA9500239Doubler · gougedDEEP SKIN GOUGE LEFT SIDE NS 240 NR 1 PYLON. REPLACED DOUBLER PER BOEING SRM 51-30-02.
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