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 DL72S952982Skin · crackedCRACKS COMING OUT OF FASTENERS, FASTENER HOLES ON LEFT AND RIGHT SIDE OF SADDLE FAIRING NR 2 INTAKE VERTICAL STAB PANEL. FOUND DURING B-2 LTR CK. REPAIRED PER SRM 54-30-0.SDR 95ZZZM257Plank · crackDURING PREFLIGHT, FOUND CRACK ON NR 1 PYLON OUTBOARD SIDE LOWER PLANK STATION YN 277.8. REMOVED FASTENERS IN AREA FABRICATE DOUBLER FROM 7075-T6 .125 AND TRIPLERS FROM 7075-T6 .190 AND .160, LOCATE DRILL UP. TREATED AND PRIMED AND INSTALLED IAW DOUGLAS NR GLSDR P5CA9500490Skin · crackedCRACK ON LOWER EDGE NR 2 PYLON RIGHT SIDE DOOR FAIRING EXTERIOR SURFACE SKIN. REPAIRED PER BOEING SRM 51-30-02.SDR P5CA9500456Skin · wornWORN METAL IN RIGHT AFT SIDE NR 4 PYLON SKIRT. REPAIRED PER BOEING SRM 54-10-02 AND 51-30-02.SDR P5CA9500454Skin · crackedCRACK ON NR 1 PYLON SKIRT NEAR TO RIGHT AFT HYDRAULIC RESERVOIR MOUNTING BOLT. REPAIRED PER BOEING SRM 54-12-02 AND 51-30-02.SDR P5CA9500429Skin · crackedCRACK NR 2 PYLON OUTER SKIN NS 221. REPAIRED PER IAI EO MAN-747-54-83978.SDR ABXA9500797Le Skin · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A PREVIOUS REPAIR CORRODED AT THE LEADING EDGE OF THE RIGHT ENGINE PYLON. REPAIRED IAW ABX REA D953-11882-MR.SDR DL757952929Skin · crackedDURING HMV, NR 2 PYLON STRUT SKIN HFEC SHOWS CRACK INDICATIONS. REMOVED DAMAGE PER SRM 54-51-01. FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER PER SRM 54-51-01.SDR DLL13952858Skin · crackedAT HMV, INTERFACE BOX CRACKED, NR 3 PYLON FWD END. REPAIRED PER SRM 54-11-00 PG 812.SDR DL757952952Skin · crackedAT HMV, NR 1 ENGINE PYLON NACELLE/STRUT SKIN O/B SKIN NAC. STA. 107 HAD TIME LIMITED REPAIR FOR CRACK IN LIGHTENING HOLE. ACCOMPLISHED PERMANENT REPAIRS PER DL ERA 259151-14.SDR DL757952911Skin · crackedAT HMV, SET UP TO PERFORM TIME LIMITED REPAIR TO THE NACELLE/STRUT SKIN PER ERA 259151-14 CODE 6-54-31. REMOVED FASTENERS AND DYE CHECKED PER PS 900-6-3 NR 1. HFET REMOVAL OF CRACK OK. DRILLED UP AND INSTALLED DOUBLER AND TRIPLER PER ERA 259151-14.SDR 95ZZZX4119Skin · crackedNR 3 ENGINE PYLON - PRE-COOLER DUCT RIVETS LOOSE AND SKIN CRACKED AFT OF SHOULDER COWL. REMOVED DUCT ASSY. REPAIRED CRACK IAW PS-1 REPAIR DRAWING NR HC711H9006, REINSTALLED DUCT ASSY.SDR 95ZZZX3172Plank · crackedKDAY/KMEM - FLT 040 - DURING SERVICE CHECK, MAINTENANCE FOUND THE NR 1 PYLON INTERMEDIATE SIDE PLANK CRACKED AT STA YN 226. THE AIRCRAFT WAS FERRIED TO KMCN TO FACILITATE PERMANENT REPAIRS. SD - ZANTOP MAINTENANCE REMOVED SIDE PLANK TO FACILITATE REPAIR. RESDR DL757952798Skin · crackedAT HMV, THE NR 1 PYLON I/B SKIN WAS FOUND CRACKED PAST STOP DRILL ON TOP FWD CORNER OF CUTOUT FOR PANEL 433 AR. THE DAMAGE WAS REMOVED AND AREA DYE PENETRANT INSP PER PS 900-6-3 NR 01, NO CRACK FOUND. HFEC INSP, NO CRACK FOUND. DRILLED AND INSTALLED DOUBLERSDR DL757952797Skin · crackedAT HMV, THE NR 2 PYLON O/B SKIN WAS FOUND CRACKED AT TOP FWD CORNER OF CUTOUT FOR PANEL 443 AR. THE CRACK WAS ROUTED OUT PER SRM 54-51-01 DYE PEN. INSP PER PS 900-6-3, NO CRACK FOUND. DOUBLER PER SRM 54-57-01 WAS FABRICATED AND INSTALLED.SDR DL757952530Skin · crackedAT HMV, THE NR 1 PYLON O/B SKIN WAS FOUND TO BE CRACKED ON TOP AFT CORNER OF CUTOUT FOR PANEL 433 AT INSIDE OF STRUT BOX. THE DAMAGE WAS CUT OUT, HFEC OF CUTOUT WAS OK. DOUBLER WAS DRILLED AND REAMED TO FINAL SIZE AND INSTALLED PER SRM 54-51-01.SDR AALA951038Skin · gougedAFW - LEFT OUTBOARD PYLON SKIN BOTTOM EDGE, HAS GOUGE BEYOND SRM LIMITS AFTER BLEND-OUT. REFINISH BLENDED AREA PER B767-SRM. APPROVED FOR CONTINUED SERVICE PER ENGINEERING MRB 767-946. (M)SDR P5CA9500028Plate · crackedNR 3 PYLON LOWER RIGHT AFT PLATE CRACKED 2 INCHES LONG AND .75 INCH PAST STOP DRILL. REPAIRED PER BOEING SRM 51-40-02.SDR 95ZZZM173Plate · crackedFOUND NR 3 PYLON LOWER RIGHT AFT PLATE CRACKED 2 INCHES LONG AND .75 INCH PAST STOP DRILL. REPAIRED PER BOEING SRM 51-40-02.SDR 95ZZZM101Plank · crackedFLT 040 - KDAY-KMEM - DURING SERVICE CHECK, MAINTENANCE FOUND THE NR 1 PYLON INTERMEDIATE SIDE PLANK CRACKED AT STATION YN 226. THE AIRCRAFT WAS FERRIED TO KMCN TO FACILITATE PERMANENT REPAIRS.SDR P5CA9500015Skin · crackedRIVET HEAD CRACKED ON NR 4 PYLON AFT OF SLOT SEAT LEFT SIDE LOWER SECTION. REMOVED AND REPLACED DAMAGED RIVET PER BOEING SRM 51-30-02.SDR P5CA9500012Skin · looseNR 3 PYLON LOWER AFT ABOVE EXHAUST LOOSE AND MISSING RIVITS. INSTALLED ALL MISSING AND LOOSE AS PER BOEING SRM 51-30-02.SDR 95ZZZX3055Skin · looseNR 3 PYLON LOWER AFT ABOVE EXHAUST LOOSE AND MISSING RIVETS. INSTALLED ALL MISSING AND LOOSE RIVETS PER BOEING SRM 51-30-02. AIRCRAFT TOTAL TIME: 69560. AIRCRAFT TOTAL CYCLES: 17553.SDR 95ZZZM155Skin · looseNR 3 PYLON LOWER AFT ABOVE EXHAUST LOOSE AND MISSING RIVETS. INSTALLED ALL MISSING AND LOOSE RIVETS AS PER BOEING SRM 51-30-02.SDR P5CA9500229Skin · crackedA .25 INCH CRACK AT NS 222 AND .5 INCH CRACK AT NS 236. DISCOVERED AFTER REMOVAL OF DOUBLER NR 1 PYLON. REPAIRED PER BOEING SRM 54-30-03 PAGE 113.SDR P5CA9500214Skin · chafedCHAFED SKIN AT NR 1 NACELLE STRUT TOP SKIN AT NS 222. SMOOTHED OUT SKIN, WITHIN LIMITS PER BOEING SRM 54-10-01.SDR P5CA9500132Skin · damagedDAMAGE ON LOWER SPAR LEFT SURFACE SKIN APPROXIMATELY NS 230 NR 3 PYLON. REPAIRED PER BOEING SRM 54-30-03.SDR P5CA9500131Skin · looseLOOSE RIVETS ON NR 3 PYLON LEFT SURFACE SKIN. REPLACED RIVETS PER SRM 51-30-02.SDR P5CA9500129Skin · crackedCRACK WITH STOP DRILLED ENDS ON NR 3 PYLON LEFT SURFACE SKIN AT LOWER SPAR APPROXIMATELY NS 255. REPLACED SKIN PANEL.SDR P5CA9500128Skin · looseLOOSE RIVETS ON RIGHT EXTERIOR SURFACE SKIN ON NR 3 PYLON. REPLACED RIVETS PER BOEING SRM 51-30-02.SDR P5CA9500093Panel · corrosionSURFACE CORROSION ON SCREW HEADS AND RIVETS NR 2 PYLON FAIRING TO WING LEFT SIDE, ALSO LOOSE RIVETS. REPLACED LOOSE RIVETS PER BOEING SRM 51-30-02 AND CLEANED SURFACE CORROSION PER BOEING SRM 51-10-01.SDR P5CA9500081Skin · crackedCRACK ON NR 2 PYLON EXTERNAL SKIN ON RIGHT FORWARD LOWER SPAR EDGE. NEW STRAP FABRICATED PER BOEING SRM 54-10-02, INSTALLED PER BOEING SRM 51-30-02.SDR P5CA9500080Panel · dentedNR 2 DAMAGE (DENT) AND RIVET IS PENETRATING SKIN ON RIGHT FAIRING PYLON TO WING. DENT HAS BEEN REMOVED AND RIVET REPLACED AS PER BOEING SRM 51-30-02.SDR 95ZZZW788Skin · crackedDURING PHASE INSPECTION IN MSP, FOUND SMALL CRACK IN RT INBOARD NACELLE FORMER P/N 27-35025-968. THE REPAIRS WERE COMPLETED BY REPLACING THE FORMER, P/N 27-35025-968 AND SKIN PANEL, P/N 27-35001-180, IAW FAC SRM 51-00-00 PAGE 4, 51-40-00, 51-30-00 AND 54-90-1SDR 9508566622Skin · crackedDURING PERIODIC CHECK, FOUND A CRACK IN THE NR 2 PYLON INBOARD SKIN, NACELLE STA 174, NACELLE WL 151. REPAIRED PER EA 66-098523.SDR 9508325527Skin · crackedDURING PERIODIC CHECK, FOUND A ONE INCH CRACK IN THE NR 1 ENGINE NACELLE STRUT SKIN PANEL, NACELLE STA 115. REPAIRED PANEL P/N 311N3450-11, -13, -15 PER EA 55-98479.SDR ABXA9500397Skin · crackedDURING D-CHECK, FOUND NR 2 PYLON OUTBOARD LOWER SURFACE AND INNER SKIN CRACKED. REPAIRED IAW ABX REA D857-11163.SDR DL757952269Plate · crackedAT HMV, THE NR 2 PYLON WAS FOUND TO HAVE TWO CRACKS ON THE UPPER FWD CORNER OF THE I/B PLATE OPENING. THE DAMAGE WAS REMOVED AND HFEC OF AREA CHECKED OK. REPAIR DOUBLERS WERE DRILLED UP AND INSTALLED PER SRM 54-51-01.SDR DL757952268Plate · crackedAT HMV, THE NR 2 PYLON WAS FOUND TO BE CRACKED AT THE UPPER FWD CORNER OF THE O/B PLATE OPENING. THE CRACK WAS ROUTED OUT PER SRM 54-51-01. HFEC FOUND NO DEFECTS. REPAIR DOUBLER DRILLED UP AND INSTALLED PER SRM 54-51-01.SDR DL72W951981Skin · crackedFOUND ON B-2 LETTER CHECK, .25 INCH CRACK VERTICAL STABILIZER EXTERIOR SKIN AT RT SIDE FWD OF ACCESS PANEL 9524 NR 2 ENGINE INTAKE COWL. REPAIRED PER SRM 54-30-01.SDR 9507715518Skin · crackedDURING PERIODIC CHECK, FOUND CRACK IN THE NR 1 ENGINE NACELLE STRUT SKIN AT THE CUTOUT FOR ACCESS PANEL 433AL. REPAIRED PER EA 55-98206. MFG PART NUMBER 311N3450-15.SDR MALA954435Skin · damagedFLT NR 3203 - DURING THE POST FLIGHT INSPECTION IN MSP, THE CREW FOUND THE RIGHT INBOARD NACELLE SKIN DAMAGED AT THE MAIN LANDING GEAR DOOR EDGE. REPAIRS WERE COMPLETED BY REMOVING THE DAMAGED SECTION AND INSTALLING A DOUBLER IAW RD 8-54-377. (W)SDR DL757951814Skin · crackedAT HMV, FOUND NR 2 ENG STRUT CRACKED AT OVAL ACCESS HOLE AT FWD END OF STRUT RT SIDE ABOVE FWD ENG MOUNT. REPAIRED PER SRM 54-51-01 FIG 203.SDR AWXA9500239Panel · damagedPHX/JFK - FLT 290 - AIR TURNBACK, PANEL 911KT LOCATED ON TOP OF LT WING NR 1 ENGINE PYLON DEPARTED AIRCRAFT DURING TAKEOFF. PANEL WAS IMPROPERLY SECURED. AIRCRAFT RETURNED TO PHX LANDING UNEVENTFULLY. OVER WEIGHT LANDING INSPECTION C/W. PANEL REPLACED AND SDR DL757951682Skin · damagedAT HMV, PERM REPAIR OF NR 2 ENG NACELLE STRUT SKIN I/B WAS SCHEDULED. THE DAMAGE WAS ROUTED OUT, INSP FOR CRACKS (NONE DETECTED), AND DOUBLER AND TRIPLER WERE FABRICATED AND INSTALLED PER SRM 54-51-01.SDR 9505945526Skin · crackedDURING PERIODIC CHECK, THE NR 1 ENGINE NACELLE STRUT SKIN PANEL WAS FOUND WITH A CRACK COMING OUT OF THE 433AL ACCESS PANEL. CRACKS WERE APPROXIMATELY 0.75 INCH LONG IN THE SKIN, DOUBLER, AND TRIPLER. INSTALLED REPAIR PER NWA EA 55-98174. MFG PART NUMBER 31SDR SWAA95294Skin · crackedDURING SCHEDULED QUARTER D-CHECK, FOUND NUMBER 2 ENGINE STRUT INNER SKIN CRACKED AT O/B EDGE OF PANEL 5827R OPENING. CRACK RUNS BEYOND STOP DRILL AND UNDER CROWN SKIN. INSTALLED DOUBLER PER ACO 6135-54.SDR MALA954404Skin · crackedDURING A C-CHECK INSPECTION IN CKB, THE LEFT EXHAUST FINGERNAIL WAS FOUND TO HAVE THE DOVETAIL SUPPORT ANGLES AND THE LEFT AND RIGHT SIDE SKINS CRACKED. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING THE TOP HALF RING IAW WVAC EO-DHC-8-93-07 REVISION A.SDR MALA954403Skin · crackedDURING A C-CHECK INSPECTION IN CKB, THE RIGHT EXHAUST SHROUD WAS FOUND TO HAVE THE RIGHT BOTTOM ANGLE BY THE AFT HOLE CHAFED AND THE LEFT AFT SIDE SKIN CRACKED. REPAIRS WERE COMPLETED IAW WVAC EO-DHC8-93-7 REVISION A. (W)SDR DL72S951426Skin · crackedA .25 INCH CRACK AT PNL NR 9523 LT SIDE OF VERT STAB. FOUND AT D-2 LETTER CHECK. REPAIRED PER MM 54-30-0 PG 804.
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