JASC 5410
Service difficulty reports · 4,119
Reports filed under 5410 · Nacelle/Pylon, Main Frame, 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 = '5410' 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 = '5410' 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 QXEA200700803Diaphragm · crackedC4 PDX - LEFT NACELLE DIAPHRAGM CRACKED. REPAIRED IAW SRM 51-42-00.SDR QXEA200700855Support Angle · crackedC4 OKC - NR 1 ENGINE UPPER TRANS COWL SUPPORT ANGLE BEHIND 2ND FROM LATCH IS CRACKED. REPAIRED IAW REO670-78-33-800, AND SRM 51-42-13, 51-42-21.SDR SWIA200718244Door · detachedUPON LANDING, INFORMED BY RAMP THAT THE UPPER RIGHT ENGINE COWLING WAS MISSING. ON POST FLIGHT, FOUND DAMAGE TO THE RIGHT HORIZONTAL STABILIZER LEADING EDGE. REPLACED RIGHT HORIZONTAL LEADING EDGE ASSEMBLY. REPLACED UPPER FAN COWL CAMLOCK RECEPTACLE AND INSSDR EIA2007117Strap · gougedNR 3 PYLON LEFT SIDE AFT ACCESS 473CL FED VERTICAL FRAME, HORIZONTAL STRAP AND ANGLE SUPPORT HAS GOUGE. REMOVED GOUGE AND INSTALLED REPAIR ON NR 3 PYLON LEFT SIDE AFT ACCESS 473CL FWD VERT FRAME HORIZ STRAP AND ANGLE SUPPORT PER B747 SRM 54-11-03 FIG 1.SDR QXEA200700792Diaphragm · crackedC4 PDX - RIGHT NACELLE DIAPHRAGM CRACKED. REPAIRED IAW SRM 51-40-15, 51-42-05, 51-21-10,51-40-35.SDR ABXA070173Doubler · crackedNR 2 PYLON INTERIOR DOUBLER CRACKED AT AFT LOWER EDGE OF OUTBOARD STRUT DOOR. REMOVED AND REPLACED DOUBLER IAW B767 SRM.SDR 2007UALA01412Link · corrodedCORROSION - DIAGONAL SIDE BRACE LINK OF NR 4 PYLON INBOARD AFT (ECCENTRIC BUSHING AROUND AREA). [SUP 06-01-07] REPLACED DSB LINK OF PYLON NR 4 INBOARD AFT AT DSB. A/C RETURNED TO SERVICE.SDR QXEA200700750Diaphragm · damagedC4 PDX - LEFT NACELLE DIAPHRAGM REPAIR IS MISSING FASTENERS AND SMOKING LOCATED ABOVE OUTBOARD FLAP. REPAIRED IAW RD8/4-54-155 AND SRM 51-42-05.SDR QXEA200700756Diaphragm · bentC4 PDX - LEFT NACELLE OUTBOARD DIAPHRAGM WEB PLATE IS BENT AND HAS SOME BLOWN OUT HOLES. REPAIRED IAW SRM 54-30-10, 51-21-00, 51-42-05.SDR ABXA070169Strut · crackedINTERIOR STRUCTURE CRACKED STRUT TRAILING EDGE ASSEMBLY 447DB. REMOVED AND REPLACED CRACKED STRUCTURE IAW B767 SRM.SDR F3LA200700083Structure · failedNR 2 ENGINE COWLING DEPARTED AIRCRAFT. CAUSE UNKNOWN AT THIS TIME AND IS UNDER INVESTIGATION BY THE FAA. [SUP 05-15-07] THE NR 2 ENGINE FWD CANTILEVER ASSY SUSTAINED SIGNIFICANT DAMAGE. REMOVED AND REPLACED NR 2 ENGINE CANTILEVER ASSY. PER EA A9-57R-1187SDR NWAA071495636Support Beam · damagedDURING UPPER LINK BEARING REPLACEMENT NR 2 FAN COWL SUPPORT BEAM LOWER WEB WAS DAMAGED. REPAIRED PER EA 56-208439.SDR DHL2007788519Nose Cowl · crackedNR 1 ENG NOSE COWL 7:30 POS AFT EDGE SKIN IS WORN AND CRACKED. CUTOUT DAMAGED AREA (3.50" BY .90"). FABRICATED REPAIR DOUBLER 2024T3 .050 PO 9004690 (11.25" BY 3.50") AND FILLER 2024T3 .040 PO NR 9004779 (3.50" BY .90") IAW B727 SRM 54-30-3 FIG 8. TREATED ASDR DHL2007788518Skin · damagedNR 1 ENG NOSE COWL 9:00 POSITION AFT EDGE SKIN IS BROKEN OUT. CUTOUT DAMAGED AREA (3.50" BY .90"). FABRICATED REPAIR DOUBLER 2024T3 .050 PO NR 9004690 (8.25" BY 2.65") AND FILLER 2024T3 .040 PO NR 9004779 (3.50" BY .90") IAW B727 SRM 54-30-3 FIG 8. TREATED SDR DL76L070368Torque Box · crackedFOUND DURING HMV AT GSO, NR 2 PYLON NACELLE STRUT MID TORQUE BOX UPPER WEB IS CRACKED. REPAIRED IQW B767 SRM 54-53-02 FIG 201 REPAIR 2.SDR DL76L070367Acoustic Panel · delaminatedNR 2 ENGINE AFT ACOUSTIC PANEL AT APPROX 3:30 POSITION IS DELAMINATED. REPAIRED BY REMOVING DELAM AREA AND POTTING AREA IAW B767 - 300 SRM 54-00-01 REPAIR AND FIG 201. WORKED ON N/R20439 DURING HMV IN GSO.SDR DL76L070366Acoustic Panel · crackedFOUND DURING HMV AT GSO, NR 1 ENG FAN COWL ACOUSTICAL PANEL HAS A CRACK INSIDE OF A DENT AT THE 4 O`CLOCK POSITION JUST FWD OF THE FAN BLADES. REPAIRED BY REMOVING CRACKED AREA AND POTTING AREA IAW B 767 SRM 51-00-01 REPAIR NR 1 ENGINE 201.SDR DHL2007806584Door · wornNR 4 ENG LT/RT NACELLE INLET COWL WORN, STA YN 157.000 AT 12 O'CLOCK POS (EXTERIOR) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2, 3. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN (AL2024T3 0.080"SDR DHL2007806582Inlet · wornNR 3 ENG LT/RT NACELLE INLET COWL WORN STA YN 157.000 AT 12 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2, 3. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN (AL2024T3 0.080") AND SPLISDR CWQR200702Flange · crackedDURING A PHASE 1-4 INSPECTION A 2.5 INCH CRACK WAS FOUND ON THE ENGINE INLET FLANGE, THIS CRACK PASSES THROUGH (2) FASTENERS THAT ATTACH THE INLET TO THE FLANGE. AND ARE AT THE 3 O'CLOCK POSITION ON BOTH THE LT AND RT ENGINES.SDR 07FDEA01201Cowling · crackedNR 3 ENGINE FIXED COWL AFT UPPER LATCH CUTOUT IS CRACKED AT AFT END NEW COWL ASSY RECEIVED AND REPLACED REF MM 71-10-031-4 AND REF WC 74C300-01.SDR 07FDEA01130Fitting · corrodedCORROSION ON AFT BEAM (RIB 8) OF PYLON NR 1, REPAIR WAS PERFORMED BY OVERSIZING IAW EA 6-5451-106439 AND RAS/050001/005/2007 ISS.ASDR A6WA200740154Door · openPERFORMED AIR RETURN AFTER N1 FAN VIBRATION ON NR 2 ENGINE ASSOCIATED WITH AIRFRAME VIBRATION. VERTICAL DESCENT RATE LESS THAN 360 FPM AT TOUCHDOWN. LANDING WEIGHT 51,000 LBS. OVERWEIGHT LANDING INSPECTION NOT REQUIRED. RT ENGINE UPPER TRANSLATING COWL OPESDR DL76L070279Fitting · arcedFOUND ARCING TO LT PYLON MID STRUT FITTING OUTBOARD SIDE. REMOVED LT OTBD PYLON PANELS 437 ELX 437 AL. ALSO, REMOVED TOP WING TO PY ACCESS PANEL. REPAIRED WIRE W/SPLICE PER SWPM. PUMP OPS CKS NML. NEEDS CLAMP/PNLS REINSTALLED. INSTALLED CLAMPS AND CLOSESDR CA070321006Latch · loose(CAN) LT ENGINE UPPER COWL OPENED IN FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS FLYING THROUGH TURBULENCE WHEN THE COWL OPENED. DURING THE INSPECTION OF THE COWL, IT WAS FOUND THAT ALL 3 LATCHES WERE LOOSE. THE LATCHES WERE RE-ADJUSTED. (TC NR 20SDR TRAX200700406Cowling · missingTOP COWLING ON LEFT ENGINE NR 1 MISSING ON POSTFLIGHT. COWLING WAS PRESENT ON PREFLIGHT. IT WAS CHANGED IN MCN MTC OVERNIGHT.SDR UPS07M49676Fairing · dentedINSPECTION TYPE:C ENGINE NR 2 AIR INTAKE DUCT FAIRING NR 364DR EXTERIOR FACE FOUND DENTED AS MARKED (14 AREAS). DENT MEASURED FOUND OUT OF LIMIT PER SRM 51-71-00 VOL IIR38, DEPTH 0.068" WIDTH 1". 06 EA DENTS TRIMMED OUT PER SRM 51-71-00VOLIIR38. HFEC C/OUT PSDR USAA070197Angle · crackedNR 1 ENGINE PYLON AFT AREA, ANGLE TIE CRACKED. FABRICATED & INSTALLED NEW ANGLE PER BOEING DWG 65C26300 & SRM 51-10-02, DEFECT SIZE: 3 INCHES.SDR 07FDEA00844Ferrule · crackedNR 1 PYLON PRECOOLER FERRULE PAN CRACKED BETWEEN RIBS 4 AND 8. ACCOMPLISHED PERMANENT REPAIR IAW SB A310-54-2028.SDR 07FDEA00707Ferrule · crackedNR 2 PYLON PRECOOLER FERRULE WITH SEVERAL CRACKS. INSTALLED NEW FERRULE P/N A5461270000000 PER SRM 51-72-10. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".SDR 2007UALA00666Structure · corrodedCORROSION - BOTH DIAGONAL SIDE BRACE FITTING BORES AT NR 1 NACELLE. MAJOR REPAIR. CORROSION - BOTH DUAL SIDE BRACE FITTING BORES AT NUMBER 1 NACELLE. ACCOMPLISHED BORING THE DSB NACELLE STRUT AT NR 1. BOTH HOLES IN SPEC PER COA AND SB 747-54A2218 (FINAL HOSDR 2007UALA00665Structure · corrodedCORROSION ON BOTH DIAGONAL SIDE BRACE FITTING BORES AT NUMBER 4 NACELLE STRUT. ACCOMPLISHED BORING THE DUAL SIDE BRACE FITTING ON THE NACELLE STRUT AT NUMBER 4. BOTH HOLES DRESSED OUT PER COA AND SB 747-54A 2218 (FINAL HOLE DIA AFTER HONE=2.2454"). REASSEMSDR CA070302002Cowling · departed(CAN) FLIGHT 3808, REPORTED A LOUD NOISE SHORTLY AFTER DEPARTURE, ON LANDING DISCOVERED COWLING MISSING AND UNKNOWN DAMAGE TO HORIZONTAL STABILIZER, NO REPORTED INJURIES, SN 7849 (REG N456ZW). WHAT COLLATERAL DAMAGE TO HZ STAB AND OTHER AREAS? HZ STAB LEADINSDR SWIA200717831Support · crackedFOUND LEFT NACELLE WHEEL WELL LOWER SUPPORT FRAME (STRINGER NR 1) IS CRACKED, DISCOVERED DURING ROUTINE INSPECTION. REPLACED LOWER OUTBOARD SUPPORT FRAME IAW EMB 120 SRM 51-10-02.SDR 07FDEA00540None · noneNACELLES AND PYLONS MINOR DEVIATION TO SRM S DUCT HOUSING SKIN REPAIR. COMPLIED WITH EA 7-5410-102026 THIS ITEM CLEARED BY REPAIR PER SRM 54-10-3 FIG 4 WITH MINOR DEVIATION DOCUMENTED BY THIS EA.SDR UIEA200700078Blowout Door · chafedENGINE NR 1 AND NR 2, RT C-DUCT BLOW OUT DOOR ASSEMBLY HAS MISSING MATERIAL AND CHAFE MARKED. REPAIRED ACCOMPLISHED AS PER EO NR 4778A093 AND FAA FORM 8110-3.SDR UPS07849343Attach Fitting · crackedINSPECTION TYPE:C3 1ST CLIP FROM FWD C/S IS CRACKED NR 4 PYLON O/B SKATE ANGLE. REMOVED, FABRICATED AND INSTALLED CLIP IAW SRM 51-1-20D, DWG 5804007.SDR UPS07449308Baffle · crackedINSPECTION TYPE:C NR 2 PYLON NAC STA 180 VERT FLANGE L/R LOWER CLEATS BROKEN AND CRACKED. CRACK LENGTH .375 INCH. NR 2 PYLON NAC STA 180 VERTICAL BAFFLE AND CLEATS REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.SDR SWIA200718004Mount · crackedRIGHT NACELLE DECK AT OUTBOARD AFT TAIL PIPE MOUNT CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ON RIGHT NACELLE DECK AT OUTBOARD AFT TAIL PIPE MOUNT PER SRM 54-20-01 AND RII 54-900-1000 AND SRM 51-40-02 .SDR 07FDEA00338Structure · damagedNR 1 PYLON HOLE ''E'' IS CONICAL IN SHAPE AND ITS MAXIMUM HOLE DIAMETER IS OUT OF LIMITS. NDT HOLE, REAMED, FABRICATED CONICAL WASHER AND INSTALLED WASHER AND FASTENER REF WRI NR 54508487 AND EA NR 7-5450-106973.SDR UIEA200700033Access Panel · wornNR 2 PYLON RT ACCESS PANEL 463AR CUTOUT FOUND WORN AT TWO POSITIONS. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-272049267 AND FAA FORM 8110-9.SDR 2007F00005Latch · brokenLT IB COWL LATCH FOR THE NR 2 ENGINE TOP COWL BROKE. VISUAL INSP REVEALED THE LATCH LINK ASSY BROKE INTO 2 PIECES.SDR UPS07449063Fitting · crackedNR 3 PYLON FWD B/H I/B HANGER FTG AREA FASTENER REMOVED UPPERR HOLE AT T/R SYNC LOCK MOD HFEC INSP FOUND WITH CRACK INDICATION, CRACK LENGTH 0.030". NR 3 PYLON FWD BULKHEAD CHORD REPLACED AS PER SRM 51-10-01 P9.SDR UPS07M49398Longeron · chafedINSPECTION TYPE:C NR 1 ENG RIGHT CORE COWL AFT LWR EDGE FOUND WITH CHAFE MARK AS MARKED. DAMAGED LONGERON AT NR 1 ENG RIGHT CORE COWL AFT LWR EDGE AREA REMOVED PER SRM 51-31-01 V-II R38. NEW LONGERON FAB PER EN 1093-07. HOLES ON FAB LONGERON PICKED UP AS PESDR COMA0770002Cowl Door · chafedLEFT UPPER FAN COWL DOOR IS GOUGED AND RIB IS CHAFED FROM THE THRUST REVERSER FLEX DRIVE CABLE. REPAIRED DAMAGE IAW COMAIR EA 70-5414-01485.SDR SIMA200700803Cowling · departedLEFT INBOARD ENGINE COWLING DEPARTED AIRCRAFT ON TAKEOFF, POST INSPECT FOUND NUMBER 1 STARTER/GENERATOR, LEFT ELEVATOR AND LEFT HORIZONTAL STABILIZER DAMAGED.SDR QXEA200603348Diaphragm · crackedPDX C3 - ON THE OUTBOARD SIDE OF THE LEFT NACELLE THE DIAPHRAM ABOVE THE NR 3 FLAP TRACK IS CRACKED IN THE RADIUS. REPAIRED IAW DHC-8-400 SRM 51-40-07, 51-40-15, 51-42-05 AND RD 8/4-54-155.SDR 07FDEA00627Receptacle · crackedTHREE RECEPTACLES DEFECTIVE ON NR 3 PYLON STRUCTURE WHERE PANEL 5402 MOUNTS TO PYLON. REPLACED THE DEFECTIVE RECEPTACLES AT PYLON PANEL 5502 MOUNT AREA. IAW 727-200 SRM 51-30-2. REINSTALLED PANEL 5502.SDR CALA0600541Attach Fitting · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 1 PYLON INTERNAL STRUCTURE O/B CLIP AT STA 285.4. THE CLIP WAS REPLACED IAW SRM 51-10-02, PAGE 8 AND SRM 51-40-02.SDR CALA0600530Attach Fitting · crackedINSPECTION FOUND NR 1 PYLON STA 285.4 O/B MID SPAR FITTING ATTACHMENT AREA MOST FORWARD I/B HOLE UPPER CLIP CRACKED (1 INCH LONG). THE CLIP WAS REPLACED IAW SRM 51-10-02.
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