JASC 5413
Service difficulty reports · 220
Reports filed under 5413 · Nacelle/Pylon, Longeron/Stringer, 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 = '5413' 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 = '5413' 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 EIAA970218Stringer · misdrilledDURING C-CHECK INSPECTION, DISCOVERED OVERSIZED FASTENER HOLES AT NAC STA 155.2 AT STR 2 (NR 1 PYLON) AND ALSO AT OUTBOARD AND INBOARD SKIN AT NAC STA 162.5. REPAIRED BY INSTALLING REPAIR STRAP AND CLIP, HFEC INSPECTING AND RESTORING FINISH TO AREA IAW EVERGRSDR SWAA970754Longeron · crackedDURING SCHEDULED D-CHECK, FOUND LONGERON ON LOWER I/B SIDE OF NR 1 PYLON CRACKED. REPLACED PER BOEING SRM.SDR SWAA970753Longeron · crackedDURING SCHEDULED D-CHECK, FOUND LONGERON ON LOWER I/B SIDE OF NR 2 PYLON CRACKED. REPLACED PER BOEING SRM.SDR ASAA9710053Longeron · chafedSEA - DURING 'C' CHECK, THE NR 2 ENGINE INBOARD FIXED COWL AFT UPPER LONGERON AND RIB WERE FOUND TO HAVE CHAFING MARKS. REPAIRED PER EA 5410-01018 AND BOEING SRM. (M)SDR EIAA970099Stringer · crackedHKG - DURING C5/D CHECK INSPECTION, DISCOVERED NR 2 PYLON NAC STATION 221 FORWARD FLANGE RADIUS ANGLE CRACKED PAST STOP DRILL HOLE. REPAIRED ACCOMPLISHED IAW SRM 54-10-03 FIGURE 19 AND SB 54-2042. (M)SDR SWAA970251Longeron · gougedDURING SCHEDULED D-CHECK, FOUND NR 2 PYLON LONGERON AND DOUBLER GOUGED. REPAIRED PER BOEING SRM.SDR COMA9710043Stringer · dentedTHE LEFT NACELLE OUTBOARD STRINGER NR 1 WAS DAMAGED BY THE FORWARD GEAR DOOR TENSIONER WHICH HAD DISCONNECTED BECAUSE THE RETAINING BOLT FELL OUT. THE LT STRINGER NR 1 HAD BEEN PREVIOUSLY REPAIRED BY INSERTION FOR THE SAME REASON. SINCE THE INSERTION REPAIR SDR COMA9610361Stringer · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: RIGHT NACELLE INBD STRINGER NR 1 DAMAGED. REMOVED AND REPLACED STRINGER IAW EMBRAER DOCUMENTS EDU-014/96 AND EST-420-96.SDR RAAA96E8025Longeron · damagedDURING SCHEDULED NR 1 CHECK, FOUND 1 INCH HOLE CHAFED IN NR 4 NACELLE INBD UPPER LONGERON AT NAC STA 103. REPAIRED PER SRM 54-2-3 FIG 1 AND 51-3-7 FIG 1 SHEET 4.SDR COMA9610256Stringer · crackedINSPECTION REVEALED A CRACK IN THE RIGHT NACELLE LT STRINGER 1. THE STRINGER WAS REPAIRED PER AERODESIGN REPORT NR 2000-1, DATED 8-17-96.SDR 96ZZZM1295Stringer · damagedDURING SCHEDULED MAINTENANCE IN MSP, A CRACK WAS NOTED IN THE LEFT INBOARD LOWER WING TO NACELLE SKIN PATCH. MAINTENANCE REPLACED THE LEFT INBOARD UPPER WING SKIN TO NACELLE ATTACH ANGLE, P/N 27-35112, LEFT INBOARD NACELLE FORMER, P/N 27-35025, STRINGER LOCATSDR CA960704008Longeron · cracked(CAN) STARBOARD ENGINE NACELLE LONGERON CRACKED. CRACK WAS APPROXIMATELY 10" AFT OF ENGINE MOUNT. CRACK FOUND IN AREA DESCRIBED IN SB 509 AND AD CF-81-07R4.SDR CA960626003Longeron · cracked(CAN) STARBOARD ENGINE NACELLE LONGERON FOUND CRACKED. CRACK WAS ABOUT 10 INCHES AFT OF THE ENGINE MOUNT. CRACK IS DESCRIBED IN SB 509 AND AD CF-81-07R4.SDR W8PA960040Longeron · gougedDURING C-CHECK, FOUND LEFT PYLON INBOARD UPPER LONGERON CRACKED. REPAIRED IAW SRM 51-40-02. (X)SDR CA951127008Stringer · corroded(CAN)DURING INSPECTION PHASE A SLIGHT BULGE IN THE SKIN ON THE OUTBOARD ENGINE NACELLE AT STN 135.O TO 171.0, WATER LINE 0.0 TO 111.0 BETWEEN RIVETS WAS DETECTED. AN NDT X-RAY REVEALED SLIGHT CORRO SION IN THE AREA OF THE RIVETS AND EXTENSIVE CORROSION ON A STSDR SRAA119504Skin · crackedON WALK-AROUND INSPECTION, FOUND NR 4 PYLON INBOARD SKIN AT STA 180 BULKHEAD AND FORWARD LOWER SPAR HAS CRACK FROM LOWER EDGE OF SKIN THROUGH 2 FASTENER HOLES, TOTAL LENGTH OF CRACK IS 2.25 INCHES. STOP DRILLED CRACK AND INSTALLED INTERIM REPAIR PER BOEING INSDR SRAA119503Skin · crackedON WALK-AROUND INSPECTION, FOUND NR 3 PYLON INBOARD SKIN AT STA 180 BULKHEAD AND FORWARD LOWER SPAR HAS CRACK FROM LOWER EDGE OF SKIN THROUGH 2 FASTENER HOLES, TOTAL LENGTH OF 1.5 INCHES. STOP DRILLED CRACK AND INSTALLED INTERIM REPAIR PER BOEING INSTRUCTION SDR CA951101203Longeron · cracked(CAN)CRACK FOUND IN THE LEFT NACELLE OUTBOARD LONGERON. INSPECTION IN THIS AREA REQUIRED BY AD CF-85-12R3. IT WAS NOTED THAT DURING REPLACEMENT THE SCREWS SECURINGTHE REINFORCING STRAP OF MOD 6/1655 HAD BEEN LOST AND WITH IT CLAMPING FORCE ON THE STRAP.SDR ABXA9500262Cap · crackedDURING C-CHECK INSPECTION, FOUND THE NR 1 ENGINE PYLON CLOSING RIB CAP CRACKED AT STA. YN-174. REPAIRED IAW ABX REA D954-11218-MR.SDR DL76S950828Longeron · wornDURING SHOP INSPECTION, NR 1 ENGINE CORE COWL LOWER LONGERON WAS FOUND WORN AT THE AFT HINGE FITTING. REPAIRED PER SRM 54-41-02 FIG 207.
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