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 MWEA98925Skin · chafedNUMBER 2 PYLON INBOARD SIDE OF LEADING EDGE AIRCRAFT SKIN CHAFED AT BOTTOM. MTC FABRICATED AND INSTALLED DOUBLER REPAIR.SDR 98ZZZX3312Skin · damagedDURING A ROUTINE ANNUAL INSPECTION, THE LOWER AFT RT NACELLE SKIN WAS FOUND CHAFING INTO THE WING SKIN DIRECTLY AFT OF THE FORWARD LOWER SPAR CAP. IT HAD ALSO CHAFED A LINE INTO THE SPAR CAP TO A DEPTH OF .008 INCH. BEECHCRAFT TECHNICAL SUPPORT WAS CONTACTEDSDR MALA976187Skin · chafedDURING 4,000 HOUR CHECK, CHAFING WAS FOUND ON LT I/B NACELLE SKIN. MAINTENANCE COMPLETED EO NR S54009, BLEND OUT THE CHAFING AREA SMOOTHLY, REINFORCED WITH DOUBLER, SEALED DOUBLER WITH NEW FASTENERS INSTALLED PER NAS1669-3 IAW SRM 51-20-42/43.SDR DL757981618Skin · crackedDURING INSPECTION OF A PREVIOUSLY ACCOMPLISHED REPAIR, AN ADDITIONAL CRACK WAS FOUND EMANATING FROM A PREVIOUS CUTOUT AT THE FWD UPPER CORNER OF THE ACCESS HOLE ON THE NR 2 ENGINE STRUT SKIN, AT THE OUTBD SIDE OF NAC STA 107.7. REPAIRED PER ERA 365391-14.SDR IXXA9800108Plating · damagedDURING ROUTINE C CHECK INSPECTION, HEAT STRESS WAS DETECTED ON NUMBER THREE PYLON INBOARD AND OUTBOARD PLANK PLATING. REPAIR ACCOMPLISHED REMOVAL OF AFFECTED AREAS, FABRICATION AND INSTALLATION OF NEW PLANK PLATINGS IN ACCORDANCE WITH DOUGLAS DRAWING 5753265 SDR ABXA9801102Panel · crackedNR 1 PYLON ACCESS PANEL LAND DOUBLER HAS A CRACK FROM CAM LOK HOLE TO EDGE OF DOUBLER, LENGTH 44. REPAIRED IAW ABX REA D854-23467MR.SDR CALA9801388Skin · crackedINSPECTION FOUND NR 1 PYLON TRAILING EDGE PANEL UPPER SKIN HOLES ELONGATED AND CRACKED. THE PYLON UPPER SKIN WAS REMOVED, NEW SKIN WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, 51-10-4, 51-10-3, 51-30-2.SDR CALA9801389Skin · corrodedINSPECTION FOUND NR 1 PYLON TRAILING EDGE PANEL LOWER SKIN DELAMINATED AND CORRODED. SKIN AND FINGER DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 54-30-0, 51-30-8, AND 51-30-2.SDR RRXA98344Plating · crackedDURING A MAINTENANCE VISIT, FOUND NUMBER 3 PYLON, LEADING EDGE WITH .5 INCH CRACK. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO ENGINEERING SKETCH REO-05083.SDR SWAA981506Skin · dentedDURING WALKAROUND CHECK, FOUND DENTED NR 1 ENG PYLON, AFT I/B END OF APPROX SIZE 7 X 250 DEEP FLANGE BENT AND RIVET PULLED. REPAIRED PER BOEING SRM.SDR SWAA981432Skin · crackedDURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOORBEAM AT RBL 13 BETWEEN BS 794 AND BS 847 AROUND MANY FASTENER LOCATIONS. REPAIRED PER BOEING SRM.SDR P5CA9801175Skin · loose#3 ENGINE PYLON EXTERNAL SKIN OUTBOARD LOWER HALF SKIRT PANEL HAS NUMEROUS LOOSE AND WORKING FASTENERS. REMOVED AND REPLACED FASTENERS PER 51-10-01.SDR P5CA9801139Skin · looseNR 2 PYLON INBOARD SIDE HAS MANY LOOSE FASTENERS. REMOVED AND REPLACED PER SRM 51-30-02.SDR P5CA9801138Skin · looseNR 1 PYLON OUTBOARD AFT LOWER SKIN HAS LOOSE FASTENERS. REMOVED AND REPLACED FASTENERS PER 51-30-20.SDR P5CA9801137Skin · looseNR 1 PYLON INBOARD AFT LOWER SKIN HAS LOOSE FASTENERS. FASTENERS REMOVED AND REPAIRED PER SRM 51-30-02.SDR P5CA9801126Skin · looseNR 2 ENGINE PYLON, EXTERNAL SKIN, LOOSE AND WORKING FASTENERS. REPAIRED PER SRM 51-30-02.SDR SWAA981188Skin · crackedDURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED I/B ENGINE PYLON PANEL ABOVE STATIONARY COWLING. REPAIRED PER BOEING SRM.SDR AU980713Keelson · cracked(AUS) LEFT NACELLE LEFT OUTBOARD KEELSON CRACKED FROM THE EDGE OF THE SKIN THROUGH THE LAST RIVET OF THE STIFFENER AND CONTINUES OUT AT AN ANGLE OF APPROXIMATELY 45 DEGREES. CRACK LENGTH 76.2 MM (3 INCHES). PART TOTAL CYCLES: 29,529.SDR CALA9801083Skin · crackedINSPECTION FOUND NR 1 ENGINE PYLON TRAILING EDGE CRACKED AND CHAFED. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-01, FIGURE 4.SDR 98ZZZX3205Skin · damagedMIA/MBJ - FLT JM 036 - ON WALK-AROUND INSPECTION, BIRD STRIKE FOUND ON NR 1 ENGINE. NO REPORT OF ABNORMAL ENGINE PARAMETERS. THE FOLLOWING STEPS, HOWEVER, WERE TAKEN: BIRD STRIKE INSPECTION CARRIED OUT PER AMM CHAPTER 72-00-00, PAGES 601-606. THERE WAS NO SDR CALA9800985Panel · crackedINSPECTION FOUND THREE .5 INCH CRACKS AT CORNER OF INNER DOUBLER ON NR 1 ENGINE PYLON PANEL NR 8103. THE CRACKED AREA WAS CUT OUT. A DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 54-01, FIGURE 4.SDR TWAA9809111Skin · delaminatedLAX - DURING C-CHECK, MAINTENANCE FOUND ON LEFT PYLON, AFT END LOWER INBOARD SIDE, DELAMINATION APPROX 7 IN BY 1.5 INCH. REPAIRED DELAMINATION PER SRM 51-70-10. (M)SDR IXXA9800087Plank · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON NUMBER FOUR PYLON INTERMEDIATE OUTBOARD PLANK AT STATION YIP 241. REPAIR ACCOMPLISHED STOP DRILLING CRACK, FABRICATION AND INSTALLATION OF AN INTERNAL AND EXTERNAL REPAIR DOUBLERS IN ACCORDANCE WITH DSDR 98ZZZM504Skin · gougedDURING SCHEDULED INSPECTION, FOUND ENGINE BLEED AIR DUCT CLAMP THREADED STUD HAD GOUGED A HOLE IN RT NACELLE INBOARD INNER SKIN SECTION. MAINTENANCE REMOVED AND REPLACED SKIN SECTION WITH IDENTICAL PIECE. (M)SDR TWAA9809113Skin · delaminatedLAX - DURING C-CHECK, MAINTENANCE FOUND APPROX 7 INCH BY 1.5 INCH DELAMINATION ON RT PYLON, INBOARD AFT SIDE. INSTALLED DOUBLER USING HOT BOND PROCEDURES PER SRM 51-70-10. (M)SDR TWAA9809112Skin · delaminatedLAX - DURING C-CHECK, MAINTENANCE FOUND ON RT PYLON, FORWARD AND BELOW LEFT SDIE DRAIN HOLE, A 3 INCH BY 1.5 INCH DELAMINATION. INSTALLED FABRICATED DOUBLERS USING HOT BOND PROCEDURES PER SRM 51-70-10. (M)SDR QXEA9800837Skin · crackedPDX - LEFT STUBWING FORWARD OUTBOARD LEADING EDGE CRACKED AT ENGINE COWL. REPAIRED IAW HORIZON AIR EA 4-54-41.SDR IXXA9800084Plank · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON NUMBER TWO PYLON OUTBOARD INTERMEDIATE PLANK PANEL AT STATION YN 190. REPAIR ACCOMPLISHED STOP DRILL CRACK, FABRICATION AND INSTALLATION AN INTERNAL AND EXTERNAL REPAIR DOUBLERS IN ACCORDANCE WITH FAASDR IXXA9800083Plank · wornDURING ROUTINE C CHECK INSPECTION, WEAR WAS DETECTED ON THE NUMBER FOUR PYLON UPPER INBOARD PLANK SIX INCHES FORWARD OF STATION YUS 297. REPAIR ACCOMPLISHED BLENDING, POLISH THE AFFECTED AREA IN ACCORDANCE WITH FAA DER APPROVED DRAWING COO-SJO-98-0351, FAX ACSDR DL767981132Skin · crackedNACELLES, NR 2 PYLON, TORQUE BOX, INBD STRUT SKIN, ACCESS CUTOUT: REPAIR FOR CRACK. THE NR 2 PYLON TORQUE BOX SKIN WAS FOUND WITH A CRACK IN THE UPPER AFT CORNER OF THE ACCESS CUTOUT AT NAC STA 231. THE CRACK WAS STOP DRILLED ON A TIME-LIMITED BASIS WITH A SDR P5CA9800793Skin · damagedNR 1 PYLON LEFT OUTER SKIN AT NAC STN 220 AND RT SKIN AT STN 233 FOUND DAMAGED. REPAIRED PER BOEING SRM 54-30-03.SDR CALA9800897Skin · crackedINSPECTION FOUND A .5 INCH CRACK COMING FROM CUTOUT FOR PANEL 5724 ON INBOARD SKIN OF NR 1 ENGINE PYLON. REPAIRED IAW ECRA 5430-01204.SDR 98ZZZM478Skin · crackedDURING C-CHECK INSPECTION DISCOVERED CRACKS ON THE INBOARD SIDE OF THE NR 1 PYLON SKIN AT THE SLOT SEAL POSITION, NACELLE STATION 180, WL 152. REPAIRED BY TRIMMING OUT THE CRACK IN THE SKIN, HFEC INSPECTING, FABRICATING AND INSTALLING REPAIR FILLER AND DOUBLESDR 98ZZZM475Skin · crackedDURING C-CHECK INSPECTION DISCOVERED A SKIN DENT AND CRACK IN THE NR 1 PYLON OUTBOARD SKIN AT NACELLE STATION 188, WL 148.5. REPAIRED BY BLENDING OUT THE DAMAGED OUTER SKIN, REMOVING THE EXISTING EXTERNAL CUTOUT CORNER DOUBLER, FABRICATING AND INSTALLING A RESDR 98ZZZM473Skin · chafedDURING C-CHECK INSPECTION DISCOVERED CHAFING DAMAGE ON THE UPPER EDGE OF THE NR 4 PYLON OUTBOARD SKIN. REPAIRED BY TRIMMING OUT THE DAMAGE, FABRICATING AND INSTALLING REPAIR STRAP AND EXTERNAL DOUBLER. REPAIRED IAW EVERGREEN AIR CENTER, ENGINEERING CHANGE/RESDR SWAA980884Panel · crackedDURING SERVICE CHECK, FOUND CRACKED LT PYLON INBOARD SIDE, AT PANEL 5742, DOUBLER AT AFT EDGE OF PANEL CUTOUT. REMOVED AND REPLACED PER BOEING SRM.SDR UPS98226833Skin · corrodedINSPECTION TYPE:C, CORROSION (C53-100-01.01-05) AND POPPED RIVET HEAD ON SKIN LAP LEFT SIDE OF NR 2 ENGINE INLET BS 1130-1145, LBL 20-30, WL 290. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-30-1 IN AND AREA OF 8 BY 8. DAMAGED SKIN REMOVED AND A STANDARD SSDR UPS98426584Skin · crackedINSPECTION TYPE N/A, CRACK FOUND ON PYLON NR 1 RT SIDE WHICH EXTENDS THE TRIMMING AREA REQUIRED BY SB 54-2034 IN FRONT OF STATION 180. REMOVED PREVIOUS REPAIR, TRIMMED EFFECTED CRACK, INSTALLED REPAIR PER SB 54-2034.SDR CALA9800751Skin · crackedA .5 INCH CRACK COMING FROM UPPER FWD CORNER OF NR 1 PYLON PANEL 5724. REPAIRED PYLON PER EC/RA 5430-01204.SDR P5CA9800837Cowl · disbondedNUMBER 1 ENG LT FAN COWL INNER SKIN IS DISBONDED AT THE BOTTOM EDGE. HOT BOND REPAIR C/OUT IAW SRM 51-40-06 FIG 17A.SDR P5CA9800848Skin · distortedNR 2 PYLON ACCESS PANEL 463EL IS DISTORTED AT FWD END. REMOVED AND REPLACED PANEL PER MM 54-32-00.SDR P5CA9800847Skin · debondedNR 1 PYLON ACCESS PANEL 453CL IS DEBONDED, CRACKED AND RUBBER PADS ARE MISSING FROM PANEL LATCHES. REMOVED AND REPLACED DOOR PER MM 54-32-00.SDR P5CA9800995Panel · damagedNUMBER 1 PYLON VALVE ACCESS PANEL CUTOUT DAMAGED AT AFT EDGE. ACCESS PANEL CUTOUT TRIMMED OFF AS PER SRM 51-10-01.SDR P5CA9800941Skin · debondedNUMBER ONE LEFT SAILPLANE DOOR OUTER SKIN IS DEBONDED. REPAIRED IAW SRM 51-40-06.SDR P5CA9800940Skin · chafedNUMBER 1 PYLON RIGHT SAILPLANE DOOR PRESSURE RELIEF PANEL INNER SKIN IS CHAFED THROUGH. REPAIRED IAW SRM 51-40-06 AND 51-30-02.SDR DL72S980994Skin · crackedC/W ERA 300554-14 CODE 4-54-31 PERM REPAIR, NACELLES/THINNER SKIN, NR 2 ENG FS 1151.68. TIME LIMITED. REMOVED DAMAGED SKIN, FABD REPAIR PER SRM 54-10-3 FIG 13. DYE CKD AND FOUND TO BE REMOVED PER PS 900-6-3 NR 1 REF N/R 398.SDR UPS98826627Skin · crackedINSPECTION TYPE:C/CK, OUTBOARD SIDE OF PYLON NR 1 CRACKED. REPAIRED PER EO 04609 AND DC8 SB 54 95 BY INSTALLING REPAIR DOUBLERS.SDR UPS98426586Skin · crackedINSPECTION TYPE-N/A, RT SIDE OF PYLON NR 2 IS CRACKED ON EXTERIOR SKIN IN FRONT OF STA 180 WHICH EXTENDS THE TRIMMING AREA, REPAIRED PER SB-54-2034. REMOVED PREVIOUS REPAIR, TREATED AND INSTALLED NEW REPAIR UP TO TRIMMING AREA PER SB-54-2034.SDR 98ZZZX1708Skin · wrinkledGYE - ON POST-FLIGHT INSPECTION, THE NR 3 ENGINE PYLON SKIN WAS FOUND WRINKLED AT STA YIP 217. INTERNAL PYLON INSPECTION REVEALED A BROKEN SPAR CAP AT STA YIP 217 REF SRM 54-3-0 PG 4A FIG 4, ITEM E. DACO NOTIFIED AND AIRCRAFT BEING PREPARED FOR 3 ENGINE FERRSDR AALA980651Panel · corrodedTUL - MILD CORROSION ON PANEL LANDING. REPLACED PANEL PER SRM 51-72-10-0. TST: 27,050.02 HOURS. CYCLES: 10,790. (X)
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