JASC 5414
Service difficulty reports · 4,361
Reports filed under 5414 · Nacelle/Pylon, Plate/Skin, 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 = '5414' 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 = '5414' 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 P5CA9600688Skin · gougedDEEP GOUGE IN NR 1 PYLON CAPSKIN BETWEEN NAC 193 AND 210. REPAIRED PER POLAR AIR CARGO MAINTENANCE AUTHORIZATION 5430-01:01.SDR USAAF96096Blowout Pnl · openCLT-HSV - FLT 546 - ON CLIMB-OUT REACHING 16,000 FEET, CREW FELT AIRFRAME VIBRATION. NO EMERGENCY DECLARED. RETURNED TO CLT. NO FURTHER INCIDENT DURING THE FLIGHT. MAINTENANCE FOUND RIGHT STUBWING BLOWOUT PANEL OPEN. REPAIRED BLOWOUT PANEL HINGE AND SECSDR DL76L962064Skin · crackedTWO CRACKS WERE REPORTED IN THE NR 2 ENGINE PYLON OUTBOARD STRUT SKIN AT THE FWD TORQUE BOX ACCESS HOLE. A .5 INCH CRACK WAS FOUND IN THE UPPER FORWARD CORNER AT APPROX NS 158. THE SECOND CRACK IS ALSO .5 INCH LONG AND IS IN THE UPPER AFT CORNER AT NS 192. SDR UPS96421159Skin · crackedINSPECTION TYPE-C, CRACK IN SKIN .75 INCH AT ACCESS PANEL CUTOUT NAC STA 207 LT. REPAIRED SKIN AT ACCESS PANEL CUTOUT NAC STA 207 LT, ACC SRM 54-30-03, FIG 17B.SDR P5CA9600652Panel · delaminatedDELAMINATED NR 3 ENGINE SLOT SEAL STRUT CLOSURE PANEL, SKIN PEELED OFF. REPLACED PANEL PER BOEING MAINTENANCE MANUAL 71-10-10.SDR RAAA96E9010Skin · crackedDURING ENGINE CHANGE PRE-INSTALL INSPECTION, FOUND .25 INCH CRACK AT FASTENER HOLE IN NR 3 NACELLE OUTBD SKIN AT NAC STA 41, AFT OF OUTBD UPPER ENG MOUNT POINT. REPAIRED PER SRM 54-2-1, FIG 3.SDR CALA9601166Skin · wornINSPECTION FOUND NR 3 ENGINE PYLON TOP PORTION OF APRON INBOARD CENTER SECTION WORN THROUGH. THE WORN SKIN AND LONGERON WERE REMOVED. REPLACEMENT SKIN AND LONGERON WERE FABRICATED AND INSTALLED IAW SRM 54-30-2, FIGURE 1 AND 51-30-2.SDR P5CA9600441Skin · damagedNR 3 PYLON RIGHT SIDE AFT MOUNT AREA SKIN DAMAGED BY SIDE COWLING. INSTALLED DOUBLER AND FILLER PER BOEING SRM 54-30-03.SDR P5CA9600412Skin · wornNR 3 PYLON RIGHT SIDE RIVETS PULLED THROUGH SKIN. REPLACED RIVETS PER BOEING SRM 51-30-02.SDR P5CA9600411Skin · wornNR 3 PYLON WORN WHERE HIT BY SIDE COWLING. BLENDED AREA PER BOEING SRM 54-10-01.SDR P5CA9600410Skin · gougedNR 3 PYLON GOUGED BY ENGINE SIDE COWL ON LEFT SIDE. REPAIRED PER BOEING SRM 54-30-03.SDR P5CA9600402Skin · crackedDURING B-CHECK, FOUND NR 1 PYLON SKIN CRACKED ON INBOARD SIDE AFT OF LOWER SLOT SEAL. REPAIRED PER BOEING SRM 54-30-03.SDR P5CA9600398Skin · crackedDURING B-CHECK, FOUND NR 2 ENGINE PYLON INBOARD AFT LOWER SKIN IS CRACKED AND FASTENERS FORWARD OF CRACK ARE WORKED LOOSE. FABRICATED AND INSTALLED REPAIR DOUBLER PER BOEING SRM'S 51-30-02, 54-30-03, AND 54-50-03.SDR UPS96420824Skin · crackedINSPECTION TYPE: C. CRACK IN PYLON SKIN AT ACCESS PANEL CUTOUT LT NAC STA 208. REPAIRED SKIN IAW SRM 54-30-03, FIG 17B.SDR UPS96420820Skin · wornINSPECTION TYPE: C. PYLON NR 1, WEAR DAMAGE IN PYLON LEADING EDGE SKIN LT NAC STA 211/216 AND WEAR DAAMAGE IN PYLON SKIN LT TOP SIDE NAC 220/225. REPAIRED LEADING EDGE SKIN IAW UPS EFN 747-54-0129, KLM 96-160. REPAIRED PYLON SKIN LT TOP SIDE IAW SRM 51-30-SDR P5CA9600342Panel · crackedNR 4 ENGINE PYLON LOWER EDGE PANEL CRACKED. REMOVED FABRICATED AND INSTALLED PANEL PER BOEING SRM 51-10-01.SDR P5CA9600337Skin · crackedNR 1 ENGINE INBOARD FAN COWL, TOP FORWARD HINGE HAS CRACK IN SKIN TOP SURFACE. WORKED AND BLENDED OUT CRACK IAW BOEING SRM 51-10-06, TREATED AND PRIMED IAW SRM 51-40-02.SDR P5CA9600334Skin · crackedNR 4 PYLON INBOARD SIDE LOWER SKIN FLANGE CRACKED. REMOVED, FABRICATED AND INSTALLED SKIN FLANGE IAW BOEING SRM 51-30-02 AND 54-12-01.SDR USAA960497Skin · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK LOWER AFT CORNER OF PYLON SKIN ACCESS OPENING STRINGER 727 L. CUT OUT CRACK, INSTALLED FILLER AND DOUBLER. REPAIRED PER EA 41241. (M)SDR USAA960599Skin · buckledYYC - DURING FC-06 CHECK, FOUND AFT SKIN BUCKLED TOP RIGHT NACELLE BETWEEN FRAME 2103-2738. INSTALLED DOUBLER PER FOKKER TS96.62079. (M)SDR DL757961476Skin · crackedTHE NR 2 ENGINE NACELLE STRUT SKIN WAS FOUND CRACKED JUST AFT OF NAC 107.7 ON THE I/B SIDE. THE CRACK WAS 1.5 INCH LONG AND EMANATES FROM THE UPPER FWD CORNER OF AN ACCESS HOLE BTW BULKHEADS AT STA 107.700 AND 116.050. THIS ER/A AUTHORIZES THE CRACK TO BE STSDR P5CA9600273Te Tip · crackedFOUND NR 2 ENGINE OUTBOARD PYLON TRAILING EDGE TIP HAD FASTENER MISSING AND CRACKED END. REMOVED PART, WELDED ON TRAVELER, INSTALLED PART IAW SRM 51-30-02.SDR DL757961292Skin · fatigueTHE NR 1 ENGINE NACELLE STRUT SKIN WAS FOUND CRACKED IN THE UPPER FWD CORNER OF 442 AT ACCESS PANEL. THE CRACK LENGTH MEASURED 1 INCH LONG. THE STRUT SKIN IN THIS LOCATION IS THREE LAYERS OF 0.080 CLAD 2024-T3 WHICH ARE STRUCTURALLY BONDED. AT LETTER CHECK,SDR DL72S961154Skin · crackedA 2 INCH CRACK IN NR 2 ENG INLET OUTER SKIN 3 FT FROM INLET LIP, 2 FT UP FROM FUSELAGE SKIN LT SIDE. REPAIRED PER M/M 54-30-0 FIG 801.SDR 96ZZZM1486Skin · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND SPOTS OF CORROSION ON UNDERSIDE, INBOARD EDGE OF 2 PYLON. REMOVED CORROSION IAW 51-10-3, FOUND SECTION TO BE OUT OF LIMITS IAW 54-01. FABRICATED DOUBLER, TREATED AND PRIMED REPAIR AND INSTALLED SDR P5CA9600220Skin · crackedDURING SCHEDULED ENGINE CHANGE, FOUND NUMEROUS CRACKS IN NR 2 PYLON BOTTOM PLATE. REPAIRED PER SRM 54-10-03, FIG. 3.SDR 96ZZZX2933Panel · debondedDURING POST-FLIGHT INSPECTION, THE BONDED ALUMINUM OUTER SKIN OF THE RT LOWER PYLON BOARD (ALUMINUM HONEYCOMB BONDED PANEL) WAS FOUND MISSING. SUBMITTER STATED IT APPEARS A BOND FAILURE AT THE LEADING EDGE OF THE PANEL ALLOWED THE AIRSTREAM TO PEEL THE SKIN FSDR DL72K960948Panel · crackedFOUND ON A2 LTR CK. ONE INCH CRACK AT PANEL 9524. REPAIRED PER M/M 54-30-0 PG 803/804.SDR 9609576623Skin · crackedDURING P-CHECK, FOUND A 2 INCH CRACK IN THE NR 3 PYLON INBOARD SKIN, NACELLE STA 180. REPAIRED SKIN PER EA 66-99629.SDR SWAA960203Panel · crackedDURING SCHEDULED C-CHECK, FOUND RT WING, AFT I/B PYLON PANEL CRACKED AT AFT BOTTOM PANEL(NR 5843R). REPAIRED PER BOEING SRM.SDR 96FDEA00717Panel · missingLT WING I/B FLAP FAIRING I/B SIDE DAMAGED. PANEL 416AR TORN LOOSE FROM NR 1 ENG PYLON. PANEL EXITED A/C AND STRUCK TO LT WING I/B FLAP FAIRING. REPLACED MISSING PYLON PANEL, RELEASED FLAP FAIRING PER CDL 27-1. REMOVED MOVEABLE FLAP TRACK FAIRINGS FROM LT NSDR 9607736634Skin · crackedDURING P-CHECK, FOUND A CRACK IN THE NR 1 PYLON INBOARD SKIN NACELLE STATION 175 WL 151. REPAIRED SKIN PER EA 66-99591.SDR CAL960448Skin · corrodedGSO - INSPECTION FOUND THE NR 2 ENGINE FORWARD OUTBOARD COWL OUTER SKIN CORRODED AROUND ENGINE RADIUS WARNING PLACARD. THE CORRODED SECTION OF SKIN WAS CUT OUT. A DOUBLER AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 54-30-2. (X)SDR 9607716634Skin · crackedDURING P-CHECK, FOUND A .8 INCH CRACK IN THE NR 3 PYLON INBOARD SKIN NACELLE, STATION 175 WL 151. REPAIRED SKIN PER EA 66-99590.SDR DL76L960749Skin · crackedTWO CRACK LOCATIONS HAVE BEEN REPORTED IN THE NR 2 ENGINE PYLON OUT'BD STRUT SKIN. THE CRACKS START FROM THE FWD TORQUE BOX ACCESS HOLE. A 1 INCH CRACK IS IN THE UPPER FWD CORNER AT NAC STA 158. SECOND CRACK IS IN THE UPPER AFT CORNER AT NAC STA 192 AND IS SDR 96ZZZM670Skin · debondedRIGHT LOWER AFT PYLON SKIN DELAMINATED BEYOND MANUFACTURE'S ACCEPTABLE LIMITS.SDR DL76L960505Skin · crackedTWO ADDITIONAL CRACKS WERE FOUND AT HMV, 2/96. ONE CRACK IS IN THE NR 2 PYLON, RT SKIN AND DOUBLER, AND IS 1.38 INCHES LONG, RUNNING DIAGONALLY UP AND AFT FROM THE UPPER AFT CORNER OF THE FWD TORQUE BOX ACCESS OPENING AT NAC STA 170. THE SECOND CRACK IS IN TSDR 9605526729Skin · crackedDURING P-CHECK, FOUND A .50 INCH CRACK IN THE NR 2 PYLON INBOARD SKIN OUTER LAYER AT NACELLE STA 175, WATER LINE 151. REPAIRED SKIN PER EA 67-99442.SDR UPS805587Skin · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 2 PYLON T/E HAS A 2.5 INCH CRACK AT LOWER AFT END. REPAIRED PER UPS EO.SDR UPS805586Skin · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 1 PYLON T/E HAS A .5 INCH CRACK AT LOWER AFT END. REPAIRED PER UPS EO.SDR AALA960284Skin · corrodedAFW - FOUND AND BLENDED DAMAGE ON THE RT PYLON INBOARD SIDE SKIN. FOUND THE BLEND EXCEEDED SRM LIMITS. REFINISHED BLENDED AREA PER SRM. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1141. TST: 43,462.33 HRS. CYCLES, 13,SDR 96ZZZM492'S' Duct Skin · corrodedDURING C-CHECK, FOUND NR 2 ENGINE 'S' DUCT INNER SKIN BULGED RIVET PULLED THROUGH 50 INCHES AFT OF SECOND ROW OF VORTEX GEN'S 6 O'CLOCK POSITION. CUT DAMAGED AREA 2 INCH BY 2 INCH PER SRM 54-10-3. INSTALLED CENTER ENGINE INTAKE DUCT SKIN DOUBLE REPAIR PER SRSDR 96ZZZM491'S' Duct Skin · corrodedDURING C-CHECK, FOUND NR 2 ENGINES 'S' DUCT INNER SKIN BULGED RIVET PULLED THROUGH 8 INCHES AFT OF SECOND ROW OF VORTEX GEN'S 6 O'CLOCK POSITION. CUT OUT DAMAGED AREA SKIN PER SRM 54-10-3 FIG 10. INSTALLED DOUBLER REPAIR PER SRM 54-10-3 FIG 10 IN NR 2 ENGINESDR USAA960166Skin · corrosionCLT - INSPECTION VISUALLY FOUND AN EXFOLIATION LEVEL 2 CORROSION BETWEEN SKIN AND DOUBLER 4 INCHES OUTBOARD PYLON SKIN IN AREA OF HEAT SHIELD NR 2 PYLON. REPLACED PYLON SKIN OUTBOARD AS PER USAIR EA 40605, EA 40669 AND USAIR EO 05492R274. (M)SDR USAA960165Skin · corrosionCLT - INSPECTION VISUALLY FOUND EXFOLIATION LEVEL 2 CORROSION BETWEEN SKIN AND DOUBLER, 2 INCHES LOCATED INBOARD PYLON IN AREA OF HEAT SHIELD NR 2 PYLON. REPLACED PYLON SKIN INBOARD AS PER USAIR 40605 AND USAIR EO 5492R274. (M)SDR DL76L960239Skin · crackedAT LETTER CHECK IN DFW, A .5 INCH CRACK WAS FOUND IN THE NR 2 ENGINE PYLON OUTBOARD STRUT SKIN. THE CRACK EMANATES FROM THE FORWARD TORQUE BOX ACCESS HOLE AT THE UPPER FORWARD CORNER AT APPROXIMATELY NAC STA 158 AND EXTENDS DIAGONALLY UPWARD AND FWD TO A FASTSDR P5CA9600056Skin · crackedFOUND CRACK IN SKIN FRONT SPAR NS 128.5 AT NR 4 PYLON. REPAIRED IAW SRM 54-12-02.SDR P5CA9600054Skin · crackedFOUND LEFT HAND SIDE SKIN NS 180 LOWER CORNER CRACKED ON INTERIOR SIDE. NEW STRAP FIRE SHIELD MANUFACTURED AND INSTALLED IAW SRM 54-12-02.SDR P5CA9600052Skin · chafedFOUND RT INTERIOR SKIN LOWER EDGE CHAFED ON NR 2 PYLON, NS 222. PATCHED AND RIVETED IAW SRM 54-12-02.SDR P5CA9600183Access Panel · delaminatedFOUND 5TH POD ACCESS PANEL AT UNDERWING ROOT DELAMINATED. REPAIRED IAW SRM 51-40-09 AND REINSTALLED IAW MM 57-44-02.
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