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 CALA9700320Skin · crackedINSPECTION FOUND A .50 INCH CRACK AT RIVET HOLE OF NR 1 ENGINE PYLON PANEL NR 5724. A DOUBLER WAS INSTALLED IAW ECRA 5430-01204.SDR P5CA9700321Skin · damagedSKIN DAMAGED AND TORN ON NR 4 ENGINE PYLON HORIZONAL FIREWALL OUTBOARD AND FORWARD OF THE AFT ENGINE MOUNT. FABRICATED AND INSTALLED REPAIR PER BAC SRM 51-30-02.SDR TWAA9713001Skin · crackedJFK - REPAIRED A 4 INCH CRACK ON THE NR 3 PYLON AT THE INBOARD SIDE OF THE PYLON LOWER FORWARD ACCESS HOLE 473CL. (M)SDR USAA970054Skin · crackedINT - DURING 'Q-1' CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK APPROXIMATELY NAC STA 210 SKIN. INSTALLED DOUBLER, REPAIRED PER EA 42018. (X)SDR P5CA9700283Skin · damageNR 3 SAILBOAT INBOARD DOOR INTERNAL SKIN PUNCTURED. ROUTED OUT AND SMOOTHED PUNCTURED AREA, FABRICATED FILLER AND DOUBLER, AND BONDED REPAIR MEMBERS I/A/W SRM 51-10-06.SDR P5CA9700279Skin · puncturedNR 1 LT SAILBOAT DOOR, TWO PUNCTURES IN OUTER SKIN. POTTED PUNCTURED ALUMINUM HONEYCOMB CORE AND BONDED REPAIR DOUBLER TO OUTER SKIN I/A/W SRM 51-40-06.SDR P5CA9700275Panel · chafedNR 4 PYLON 1/2 MOON SHAPED RT ENGINE MOUNT ACCESS PANEL CHAFED THROUGH. FABBED NEW PART AND REPLACED ACCESS PANEL I/A/W 51-10-01.SDR P5CA9700294Strip · crackedNR 3 PYLON - L/S UPPER WING TO PYLON STRIP CRACKED AT OLD WELD ABOVE ACCESS PANEL 472DL. WELDED PER BOEING SRM 51-30-02.SDR P5CA9700288Skin · crackedNR 2 PYLON SKIN CRACKED - OUTBOARD SIDE AT CORNER DOUBLER BELOW TEXAS DOUBLER. REPAIRED PER BOEING SRM 54-30-03.SDR P5CA9700287Skin · crackedNR 4 OUTBOARD - SAILBOAT DOOR - 484AR EDGE CRACKED BETWEEN BOTH FORWARD LOCK BRACKETS. REPAIRED PER BOEING SRM 51-40-06.SDR P5CA9700254Skin · damageNR 4 PYLON RT SIDE LOWER SKIN REPAIR STRAP GOUGED ALONG LOWER EDGE. REPAIRED PER BOEING SRM 53-30-01.SDR P5CA9700245Pylon · crackedNR 2 PYLON UPPER FWD CORNER CRACK IN PANEL. REPAIRED WELDED PER BAC 5975.SDR GTIA9700226Skin · looseYIP - LEFT ENGINE PYLON TRAILING EDGE LOOSE. REMOVED DAMAGED TRAILING EDGE AND INSTALLED NEW PER DC-9 SRM SEC 5402, FIGURE 5. (X)SDR P5CA9700224Skin · gougedGOUGES IN NR 4 PYLON LEFT SIDE NAC STA 145. REPAIRED PER BOEING SRM 53-30-01 AND 51-10-02.SDR F3LA97094Skin · crackedCLT - FOUND CRACK IN THE NR 2 ENGINE PYLON SCREW HOLE. INSTALLED NEW ANGLE, DOUBLERS AND FILLERS PER EA 57446, EA 57462, SRM 51-40-01 AND SRM 54-10-3. (M)SDR RRXA97023Plating · crackedON POST-FLIGHT INSPECTION, FOUND 1 EACH .50 INCH CRACK AND 1 EACH 5.50 INCH CRACK IN OTBD SIDE OF NR 1 PYLON AT YN 225.279. STOP DRILLED CRACK ON PYLON PANEL. FABRICATED TWO REPAIR DOUBLERS AND INSTALLED AND SEALED IAW DC-8 SRM TR 54-2-2, FIGURE 6, PAGE 20, SDR RRXA97021Plating · crackedON POST-FLIGHT INSPECTION, FOUND 1 EACH .50 INCH CRACK AND 1 EACH 5.50 INCH CRACK IN OUTBOARD SIDE OF NR 1 PLYON AT YN225.279. TEMPORARY REPAIR INSTALLED ON 970125 FOR ONE-TIME FERRY FLIGHT IAW DER APPROVED SKETCH B99-T01 FROM KMEM TO KMCN. STOP DRILLED CRACSDR P5CA9700195Panel · damagePANEL NR 531 AB NR 1 PYLON O/B TRIANGLE PANEL HAS ENLARGED SCREW HOLES. ALSO, FORWARD EDGE ERODED. REPAIRED BY APPLYING FIBERGLASS OVERLAYS AND PAINTED PER SRM 51-40-15 AND 51-24-11.SDR P5CA9700176Skin · damageNR 2 PYLON UPPER SKIN FLANGE IS CHAFED. REMOVED AND REPLACED WITH NEW STRAP IAW SRM 51-30-02.SDR P5CA9700067Panel · puncturedPUNCTURE ON INNER SKIN OF NR 3 PYLON OUTBOARD SAILBOAT PANEL. REPAIRED PER BAC SRM 51-40-06.SDR P5CA9700185Door · crackedNR 3 I/B SAILBOAT DOOR, FWD BLOW OUT DOOR HINGE CRACKED. REMOVED AND REPLACED HINGE IAW SRM 51-10-01.SDR P5CA9700184Door · crackedNR 3 I/B SAILBOAT DOOR, AFT COWL LOCK CRACKED IN RADIUS. FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-10-01.SDR P5CA9700028Skin · crackedNR 2 PYLON INBOARD SIDE CRACK IN PREVIOUS REPAIR. BLENDED OUT CRACK PER BOEING SRM 53-30-01, TREATED AND PAINTED PER 51-10-02.SDR P5CA9700001Skin · crackedCRACKED SKIN AT ACCESS PANEL 463CL AFT UPPER CORNER NACELLE STATION 195. REPAIRED PER BOEING SRM 54-30-03 PAGE 380.SDR CALA9700387Panel · crackedINSPECTION FOUND A 1 INCH CRACK AT CUTOUT OF NR 1 ENGINE PYLON PANEL NR 437DR. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-00-01, FIGURE 1 AND 2.SDR DL76L962715Skin · crackedA 2 INCH CRACK WAS FOUND IN THE NR 2 ENGINE PYLON O/B STRUT SKIN. THE CRACK EMANATES FROM THE FWD TORQUE BOX ACCESS HOLE. THE CRACK WAS REPAIRED PER A BAC MOD DWG. REV E TO ER/A PROVIDES BAC DER FAA APPROVAL.SDR DL76L962717Skin · crackedA CRACK WAS FOUND IN THE NR 1 PYLON I/B STRUT SKIN EMANTING FROM THE TORQUE BOX ACCESS HOLE. THE CRACK WAS REPAIRED PER BAC MOD DWG 311T3401.SDR COMA9610362Skin · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: LEFT AND RIGHT NACELLE LOWER SKINS DAMAGED. REMOVED AND REPLACED LT AND RT NACELLE LOWER SKINS IAW COMAIR ENGINEERING ORDER 54-005.SDR CKSA96339Skin · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: NR 1 PYLON SKIN DAMAGED AT STA YOP.270 INBOARD SIDE, APPROXIMATELY 3 INCH LONG HOLE. REPAIRED DAMAGED SKIN NR 1 PYLON IAW DC-8 SRM 54-2-1, 51-1-20D, 51-1-21, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82014.SDR CKSA96331Skin · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: NR 2 PYLON DAMAGED INBOARD SIDE UPPER STATION YIP.230 APPROXIMATELY 1 HOLE. REPAIRED INBOARD PYLON INBOARD SIDE SKIN IAW DC-8 SRM 54-2-1 FIGURE 7, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81996.SDR CKSA96328Skin · dentedDURING SEVERE TURBULENCE INSPECTION FOUND: DENT IN NR 2 PYLON INBOARD SIDE ABOVE ENGINE EXHAUST. REPAIRED DENT IAW DC-8 SRM 54-2-1 FIGURE 7, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81793.SDR CKSA96327Skin · damagedDURING SEVERE TURBULENCE INSPECTION FOUND: HOLE IN NR 2 PYLON INBOARD SIDE ABOVE ENGINE EXHAUST. REPAIRED HOLE IAW DC-8 SRM 54-2-1 FIGURE 7, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81792.SDR CA961126003Skin · cracked(CAN) SKIN ON THE NACELLE AFT CLOSURE FOUND CRACKED AT AREA DIRECTLY ABOVE THE LANDING GEAR FAIRING. THE REAR NACELLE BULKHEAD PASSES THROUGH THE CRACKED PLATE.SDR CALA9601869Skin · crackedINSPECTION FOUND A .50 INCH CRACK ON LT AND RT CORNERS OF NR 3 ENGINE PYLON FORWARD END. THE CRACKED AREAS WERE CUT OUT. TWO EACH DOUBLERS, FILLERS, AND TRIPLERS WERE FABRICATED AND INSTALLED IAW SRM 54-00-01, FIGURE 2A.SDR MALA965193Skin · damagedDURING MAINTENANCE IN MSP, MAINTENANCE FOUND THE LEFT INBAORD NACELLE HAD SEVERAL RIVETS PULLING THROUGH. COMPLETED REPAIR TO LEFT INBOARD NACELLE SKIN JUST AHEAD OF THE INBOARD GEAR DOOR BY INSTALLING A REPAIR DOUBLER IAW FAC SRM 54-90-40 PAGES 35-37. (M)SDR P5CA9600857Skin · crackedCRACK IN SKIN NR 1 PYLON AT NAC STA 180 WL 152, SLOT SEAL AREA. REPAIRED PER BOEING SB 54-2034 REV 4 AND POLAR MA 5430-02:01.SDR P5CA9600855Skin · crackedA .25 INCH CRACK ON NR 4 ENGINE PYLON INBOARD SIDE GOING INTO SCREW ABOVE HORSE SHOE PLATE NACELLE STA 222. REPAIRED PER BOEING SRM 54-30-03 FIG 35.SDR P5CA9600840Skin · crackedCRACK ON PLATE 453DR ON NR 1 PYLON. FABRICATED AND INSTALLED DOUBLER PER BAC SRM 51-30-02 AND 51-40-02.SDR P5CA9600835Skin · crackedCRACK APPROX .25 INCH GOING TO RIVET HOLE AT TOP AFT CORNER OF NR 2 PYLON CUTOUT FOR PANEL 463CL. DYE CHECK CONFIRMED CRACK, EDDY CURRENT CK PER BAC NDT MANUAL PART 6 AND INSTALLED DOUBLER PER BAC SRM 54-30-03.SDR DL757962425Skin · crackedTHE O/B SKIN OF THE NR 1 ENGINE PYLON WAS FOUND TO HAVE A CRACK CONTINUING BEYOND A PREVIOUS STOP DRILL OUT OF THE UPPER, FWD CORNER OF THE FWD ACCESS OPENING AT NS 112.92. WHEN ROUTED OUT, THE TOTAL LENGTH WAS 1.50 INCH. THE SKIN AT THIS LOCATION IS FABRICASDR ZIAA96071Panel · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. NR 1 PYLON EXT PANEL, RT YN220. REPLACED.SDR P5CA9600769Skin · damagedNR 3 ENGINE I/B O/B SAILBOAT FAIRING INNER SKIN HAS A HOLE. REPAIRED WITH METAL TO METAL BOND IAW SRM 51-40-06.SDR P5CA9600768Skin · damagedRIGHT HAND INBOARD SAILBOAT INNER SKIN HAS A HOLE. CLEANED, APPLIED FILLER, HOT BONDED DOUBLER IN PLACE IAW SRM 51-40-06.SDR P5CA9600789Skin · damagedDAMAGED SKIN ON PYLON LEADING EDGE FROM 11 O'CLOCK TO 7 O'CLOCK. TRIMMED DAMAGED AREA PER BAC SRM 54-30-01.SDR P5CA9600762Skin · crackedNR 2 PYLON LOWER FWD PYLON ACCESS PANEL 463CL CUTOUT HAS .5 INCH CRACK AT THE AFT UPPER END. STOP DRILLED CRACK AND INSTALLED DOUBLER IAW SRM 54-30-05.SDR DU4R9600006Skin · dentedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND HI-REACH DAMAGE ABOVE AND AFT OF LEFT ENGINE PYLON.SDR P5CA9600733Skin · crackedCRACK AT LOWER FORWARD ACCESS HOLE NR 4 PYLON, NR 483CL. REPAIRED PER BOEING SRM 54-30-03, TIME LIMITED REPAIR.SDR 97ZZZX945Skin · crackedDURING PHASE INSPECTION, FOUND CRACK IN PYLON SKIN ACROSS RIVET HOLE. THIS CRACK EMANATED FROM CORROSION OF THE SKIN. FURTHER INSPECTION REVEALED CORROSION ON VARIOUS MEMBERS IN THE PYLON.SDR DL72S962171Skin · crackedTWO CRACKS IN LT SIDE OF DOG HOUSE NR 2 ENG S-DUCT, 1 FT ABOVE FUSELAGE SKIN STA 1099. DYE CHECKED FOR CRACKS PER PS 900-6-3, 2 CRACKS FOUND. REPAIRED ONE CRACK PER MM 54-30-0 PG 802. REMOVED DAMAGED SECTION OF FWD LOWER AREA AND DRILLED REPAIR DOUBLER PER SDR MWEA96496Skin · corrodedDURING INSP, FOUND A SMALL AREA OF SURFACE CORROSION ON BOTTOM SKIN OF LT PYLON. FOUND CORROSION OUT OF LIMITS AND FABRICATED A REPAIR IAW SRM 54-01, FIG 2 AND INSTALLED IAW SRM 51-30.
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