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 CWQR201005Line · chafedWHILE REPLACING A LINE ASSY CALLED OUT IN ASL750-29-22R1, DISCOVERED ANOTHER LINE ASSY CHAFED BEYOND LIMITS IN THE PYLON ACCESS AREA AFT OF THE AREA CALLED OUT IN THE ASL. BELIEVE INSPECTION CALLED OUT IN ASL750-29-22R1 SHOULD BE EXPANDED TO INCLUDE AFT ACCESSDR FDEA201003020590Insulation · tornNR 1 PYLON ELBOW DUCT METAL INSULATION IS TORN AND DAMAGED. REPAIRED IAW EA 6-3611-136623.SDR NSVA201049AUnknown · unknownAIRCRAFT REQUIRES MAJOR REPAIR FOR PERMANENT REPAIR OF MISC RIVET DEVIATION ON LT AND RT OUTBOARD NACELLE ALONG WITH LT AND RT INBOARD NACELLE IAW TD'S 340-54-09-18, 340-54-09-19, 340-54-09-20 AND 340-54-09-21.SDR DL757100278Bushing · unknownINCORPORATE VA 78786MAAD INTO EA 06-070332-03 (AD) TITLE B757 SIP-AUTHORIZATION TO MAINTAIN UPPER LINK WASHERS. INCORPORATED VA 78786MAAD INTO EA 06-070332-03(AD) AT SAA SAT REF NON ROUTINE CARD 149320.SDR HYIA2714MUnknown · unknownRT ENG SURGING AT CRUISE POWER. RESHAPED LEFT NOSE BOWL DUE TO PROP CABLE ROD END CLEARANCE.SDR DJF2008F00001Skin · crackedDURING ROUTINE MAINTENANCE THE LT INLET SKIN AT THE INLET TEMP PROBE WAS FOUND CRACKED. THE SDR WILL BE UPDATED UPON COMPLETION OF THE C/A. (K)SDR PNS2008F00005Structure · damagedAC TO BE EXTENSIVELY DAMAGED FROM AN APPARENT HARD LANDING. FLIGHT CREW STATED THEY WERE UNAWARE WHERE OR HOW THE DAMAGE WAS MADE. THE DAMAGE WAS NOTICED WHEN MAINT MOVE THE AC TO THE HANGER FOR OTHER MAINTENANCE. THE BULK OF THE DAMAGE CONSIST OF BOTH ENGISDR 08FDEA01339Structure · damagedPYLON NR 1, PYRAMID HOLE WITH CORROSION (FWD RT).SDR 2007UALA05044Unknown · unknownFLIGHT DIVERTED DUE TO RIGHT ENGINE CORE COWL PROBLEM.SDR CA070504001Line · leaking(CAN) FORWARD PYLON PRESSURE LINE FOUND CHAFED THROUGH CAUSING LEAK. DAMAGE CAUSED BY A DEFECTIVE HOSE CLAMP. (TC NR 20070504001)SDR SWIA200717766Nacelle · contaminatedUPON AIRCRAFT POWER DOWN CREW NOTICED SMOKE COMING FROM THE LEFT ENGINE NACELLE. INSPECTED ENGINE COMPARTMENT AND NOTED EXCESS GLYCOL. NO OTHER DISCREPANCIES NOTED.SDR 06FDEA1937Fastener · looseDURING AIRPLANE'S CONVERSION FROM P TO F/ACF, FOUND A LOOSE FASTENER AT STA YN 358.210 (REF. AMERICAN AIRLINES E.S. # ESO 7349 DATED 04 SEPT 86). THE FASTENER WAS REPLACED WITH MS21140-06 BLIND BOLT WITH INSPECTION AT "C" CHECK (REF BOECOM SVC-TUL-999/MEC).SDR 2006FA0000444Cowling · separatedAC WAS RETURNING TO HOME FIELD AFTER MAINTENANCE WHEN CREW HEARD A LOUD NOISE AND ELECTED TO RETURN TO DEPARTURE. AFTER ENGINE SHUT-DOWN, IT WAS DETERMINED THAT THE LT ENGINE UPPER AND LOWER COWLING HAD SEPARATED FROM THE AC IN FLIGHT. SB CONCERNING COWLING SDR 2006FA0000443Cowling · separatedAIRCRAFT WAS RETURNING TO HOME FIELD AFTER MAINTENANCE WHEN CREW HEARD A LOUD NOISE AND ELECTED TO RETURN TO DEPARTURE. AFTER ENGINE SHUTDOWN, IT WAS DETERMINED THAT THE LT ENGINE UPPER AND LOWER COWLING HAD SEPARATED FROM THE AC IN FLIGHT. SB CONCERNING COWSDR HNAA0600017Latch · unlatchedTWO INBOARD COWL LATCHES CAME LOOSE. INSPECTED AND SECURED LATCHES AS REQUIRED.SDR CIHA200579003Attach Angle · crackedNR 1 ENGINE ATTACH ANGLE, P/N 69-16977-1, CRACKED AT HOLE-P. EDDY CURRENT INSP VERIFIED. REMOVED & REPLACED NR 1 ENG ATTACH ANGLE P/N:69-16977-1 PER ACD (BACDRW) 65-72772.SDR 05FDEA04302Repair · noneNR 1 PYLON FOUND TWO BLEND OUTS ON THE OUTBOARD SKIN AREA BELOW THE TRUST REVERSER HINGE STA YN250. PERFORMED INSPECTION ON PREVIOUS REPAIR IAW 1275402-ESO7349 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2.SDR DL76S050754Bolt · incorrectTHE OUTBOARD SIDE LINK BOLT WAS TOO SHORT FOR PROPER INSTALLATION. A THINNER WASHER WAS INSTALLED REF AD 4002-16-12, 1-074906-03AD.SDR MALA050250Bulkhead · crackedDURING C2 CHECK IN YYC FOUND FWD NOSE COWL BULKHEAD 2 CRACKED STIFFENERS, NR 3 ENGINE. ITEM NR 23 P/N HC716H0022-208, ITEM NR 2 P/N HC716H0022-215.SDR 04FDEA02440Pylon · crackedNR 1 ENGINE AFT UPPER PYLON HAS CRACKED UNDER PNL 473CL. STOP DRILLED CRACK AND INSTALLED U-CHANNEL IAW A310/200 SRM 54-50-00 AND 54-54-11 FIG 201 AND 54-54-51 FIG 206 BETWEEN PYLON STA 1059 AND STA 1115.SDR EAHR200400002Tube · brokenPYLON TUBE, P/N 4110040-30, BROKEN AT UPPER CLUSTER.SDR DJFA200300004Cowling · missingAFTER DEPARTURE FROM WEST PALM THE PILOTS EXPERIENCED A VIBRATION AND A YAW IN THE AIRCRAFT. THE PILOTS DECIDED TO RETURN TO WEST PALM, AND AFTER LANDING WHEN THEY GOT OUT OF THE AIRCRAFT THEY NOTICED THE LT ENGINE COWL WAS COMPLETELY MISSING. THIS HAS HAPPENESDR C2XA03SH186Structure · dentedDURING C-CHECK THE NUMBER TWO UPPER COWLING INBOARD EDGE MEMBER WAS FOUND DENTED. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW EMB 145 SRM 54-10-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA03SH180Structure · chafedDURING C-CHECK THE NUMBER ONE LOWER COWLING AFT EDGE MEMBER WAS FOUND CHAFED. MAINTENANCE REMOVED AND REPLACED AFFECTED MEMBER IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR MALA030290Latch · malfunctionedDURING FLIGHT 2928 LT ENGINE COWL CAME LOOSE ON FWD CORNER. MAINTENANCE INSPECTED LATCHES FOR CONDITION AND SECURITY. CHECKS OK. INSPECTED HINGES VISUALLY, CHECKS OK. RESECURED LATCH.SDR AMTA200300190Shim · dislodgedNR 1 PYLON HAS MIGRATING SHIMS ON OUTBOARD LOWER SIDE OF PYLON. REPAIRED PYLON AND REPLACED SHIMS IAW EO 757-54SB-2456. (M)SDR AMTA200300191Shim · dislodgedNR 2 PYLON INBOARD AND OUTBOARD SHIMS HAVE EXCESSIVE GAP. COMPLIED WITH EO 757-54SB-2456. (M)SDR C2XA02SH162Stiffener · gougedSHV- DURING C CHECK NUMBER ONE COWLING STIFFENER AT STATION 2180 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH160Stiffener · gougedSHV- DURING C CHECK NUMBER ONE LOWER COWLING AFT STIFFENER WAS FOUND GOUGED. MAINTENANCE REMOVED AND REPLACED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH146Gusset · nickedSHV DURING C CHECK GUSSET WAS FOUND NICKED ON NUMBER 2 LOWER COWLING AT STAION XN=3167.5MM. MAINTENANCE REMOVED AND REPLACED AFFECTED GUSSET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH145Stiffener · gougedSHV- DURING C CHECK NUMBER 2 LOWER COWLING STIFFENER WAS FOUND GOUGED NEAR CENTER LINE AT STAION XN=2180.0MM. MAINTENANCE REMOVED DAMAGE AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR DL757021453Support Fitting · tool damageDURING ACCOMPLISHMENT OF PYLON MOD EO 6-70332-3AD, HOLE 5 IN THE LEFT WING SUPPORT FITTING HAD DAMAGE THAT REQUIRED REMOVAL PRIOR TO FASTENER INSTALLATION. REPAIRED PER ER/A 389427-14AD. REPAIR OVERSIZED HOLE, INSTALLED FREEZE PLUG, THESDR 2002UALA01804Web · cracked#1 PYLON UPPER WEB AT GENERATOR CABLE FEED-THROUGH HAS 2 EA CRACKS AT NUTPLATES. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIRED WEB WITH REPAIR DOUBLER.SDR 2002UALA01803Web · cracked#1 PYLON UPPER WEB AT ELECT. WIRE BUNDLE FEED-THROUGH HAS 2 EA. CRACKS AT NUTPLATES. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.REPAIRED WEB WITH REPAIR DOUBLER.SDR 2002UALA01802Web · cracked#1 ENG PYLON AFT UPPER WEB AT PNEUMATIC DUCT FEED-THROUGH IS CRACKED IN RADIUS. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIRED WEB WITH REPAIR DOUBLER.SDR 2002UALA01801Pylon · cracked#2 PYLON STRUT UPPER TORQUE BOX WEB AT GENERATOR FEED CABLE CUT-OUT IS CRACKED IN CORNER RADIUS. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.DOUBLER INSTALLED.SDR C2XA02SH133Rib · gougedSHV- DURING C CHECK THE RIGHT HAND UPPER COWLING MOST AFT REINFORCEMENT RIB WAS FOUND GOUGED OUTBOARD SIDE. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 135 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH132Rib · gougedSHV- DURING C CHECK LEFT HAND UPPER COWLING MOST AFT REINFORCEMENT RIB WAS FOUND GOUGED ON OUTBOARD SIDE. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 135 SRM 54-10-07.THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR ABXA020309Web · cracked#1 ENGINE STRUT AFT FAIRING SPAR WEB, FOUND ONE CRACK ON STIFFENER (P/N 313T1380-15), AND FOUR CRACKS ON WEB (P/N 313T1380-9). REPAIRED STRUT AFT FAIRING IAW REA B654-44936-MR.SDR C2XA02SH122Rib · gougedSHV- DURING C CHECK LEFT HAND LOWER COWLING WAS FOUND TO HAVE A GOUGE INSIDE INBOARD OF ACCESS TO AIR STARTER VALVE. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR ABXA020222Attach Angle · crackedPYLON LOWER ATTACH ANGLE FORWARD END WAS CRACKED. REPAIRED PYLON LOWER ATTACH ANGLE FORWARD END IAW DC-9 SRM 54-04 AND SSRM DWG #K07439.SDR ABXA020203Clip · cracked#1 PYLON ATTACH ANGLE INSIDE PANEL 8111 AT UPPER AFT ENGINE MOUNT STRAP HAD CRACK NEXT TO BOLT. REPLACED ANGLE IAW DC-9 DWG 9915500 AND DC-9 SRM 51-30-5.SDR ABXA020187Clip · crackedLOWER BOLT HOLE WAS CRACKED AT #2 ENGINE AFT MOUNT. REPLACED ANGLE IAW DC-9 SRM 51-30-5.SDR DHL2002363502Rib · crackedC-check/#2 pylon rib #22, rib is cracked at lower otb. corner.Corrective action/ reference pg. 2 rib removed & replaced,item #4.Fairing attach structure not required to remove & replace rib # 22 ref. pg. 2 item #4.Removal of angle not required for r&r of rib #SDR CYX2002F00001Strap · crackedDURING A 300 HOUR INSPECTION THE LEFT HAND AFT PYLON SUPPORT STRAP WAS FOUND CRACKED. THIS SUPPORT STRAP IS RIVETED TO THE UNDER SIDE OF THE UPPER CABIN ROOF BEAM LEFT HAND AFT CORNER. CRACK IS APPROXIMATELY 2.250 INCH IN LENGTH AND ORIGINATED IN A BEND RADISDR CYX2002F00000Strap · crackedDURING A 300 HOUR INSPECTION THE LEFT HAND AFT PYLON SUPPORT STRAP WAS FOUND CRACKED. THIS SUPPORT STRAP IS RIVETED TO THE UNDER SIDE OF THE UPPER CABIN ROOF BEAM LEFT HAND AFT CORNER. CRACK IS APPROXIMATELY 1.750 INCHES IN LENGTH AND ORIGINATED IN A BEND RSDR 02FDEA00408Pylon · crackedCRACK FOUND ON HOLE #7 AND #6 ON OVERWING REFUEL APARTURE. ** S/D ** COMINGSDR ABXA020104Flap Track · corrodedRIGHT WING INBOARD FLAP, INBOARD FLAP TRACK SHOWED EVIDENCE OF WEAR AND CORROSION. REPLACED THE RIGHT WING INBOARD FLAP, INBOARD FLAP TRACKS IAW DC-8 MM 27-51-03.SDR CW12002F00001Cable · brokenUPON CLOSING THE LEFT TOP ENGINE COWLING, WHEN THE CABLE WAS ACTUATED TO CLOSE THE COWLING THE END ENGAGING PIN BROKE. THE COWLING WAS NOT SECURED PROPERLY. THE COWLING CABLE BROKE AT THE THREADED END WHERE THE ENGAGEMENT PIN SCREWS ON.SDR ABXA010801Fitting · cracked#3 PYLON V-BLOCK SUPPORT FITTING HAD A CRACK IN IT. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D, 51-3-0, 51-1-23 AND 56-3-0.
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