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 QXEA0202253Longeron · damagedCKB - RIGHT HAND NACELLE OUTBOARD LONGERON HAS A FACTORY HOLE THAT IS OVERSIZED TO .267. REPAIRED IAW WVAC EO DH8S-54-0684 AND HORIZON AIR EA 6-54-167.SDR UPS02239960Longeron · crackedINSPECTION TYPE: C, ENGINE NR 2, LT NACELLE. CRACK ON UPPER LONGERON AT BS 1387 APPROX UNDER BLOCK (DOOR SHEAR). LONGERON REMOVED IAW SRM 51-30-02. NEW LONGERON MANUFACTURED IAW SRM 51-20-1. NEW LOGERON INSTALLED IAW SRM 51-30-02 & RE-PROTECTEDSDR CA020913012Longeron · cracked(CAN) NR 2 ENGINE NACELLE LONGERON CRACKED ON INBOARD SIDE.SDR QXEA0201404Longeron · damagedCKB- INBOARD LONGERON HAS 3 BAD FASTENER HOLES AT NACELLE STATION 141.66. REPAIRED IAW HORIZON AIR EA 6-54-108 AND WVAC EO DH8S-54-0515.SDR QXEA0200654Stringer · crackedPDX- LT NACELLE FINGERNAIL DECK FORE AND AFT LOWER STRINGERS ARE CRACKED. REPAIRED IAW DHC-8 SRM 51-40-11.SDR QXEA0101712Longeron · gougedPDX - RT NACELLE WHEEL WELL AT STATION ZN24.25 LOWER LONGERON XN125.50 HAS A GOUGE IN LONGERON LEFT FORWARD INBOARD SIDE. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-36.SDR XEA0101381Panel · crackedPDX - PANEL 422AT AT OUTBOARD FORWARD LATCH HAS CRACKED HORSE COLLAR SKIN AT .350 AND .300 INCH. REPAIRED IAW HORIZON AIR EA 2-71-159.SDR COOSDR010078Longeron · crackedENGINE NR 2, FORWARD FIREWALL-LONGERON, PN 65-53558-54 CRACKED.SDR QXEA0101340Stringer · crackedPDX - LEFT-HAND NACELLE DECK LOWER SURFACE STRINGER IS CRACKED AT STATION XN258.00. REPAIRED IAW HORIZON AIR EA 2-54-94, DHC-8 SRM 51-20-16 AND SRM 51-20-26.SDR QXEA0101339Stringer · crackedPDX - LEFT-HAND NACELLE DECK LOWER SURFACE STRINGER IS CRACKED AT STATION XN247.00. REPAIRED IAW HORIZON AIR EA 2-54-95 AND DHC-8 SRM 51-20-16 AND SRM 51-20-26.SDR QXEA0101338Stringer · crackedPDX - LEFT-HAND NACELLE DECK LOWER SURFACE STRINGER IS CRACKED AT STATION XN247.00. REPAIRED IAW HORIZON AIR EA 2-54-95, DHC-8 SRM 51-20-16 AND SRM 51-20-26.SDR QXEA0101337Stringer · crackedPDX - LEFT-HAND NACELLE DECK LOWER SURFACE STRINGER IS CRACKED AT STATION XN258.00. REPAIRED IAW HORIZON AIR EA 2-54-93, DHC-8 SRM 51-20-16 AND SRM 51-20-26.SDR QXEA0101336Stringer · crackedPDX - LEFT-HAND NACELLE DECK STRINGER CRACKED AT STATION XN272.00. REPAIRED IAW HORIZON AIR EA 2-54-95, DHC-8 SRM 51-20-16 AND SRM 51-20-26.SDR QXEA0101334Stringer · crackedPDX - LEFT-HAND NACELLE DECK STRINGER CRACKED AT STATION XN258.00. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-26.SDR COMA0110128Stringer · dentedDURING 2C-CHECK TASK 5410-442-04I, THE RIGHT NACELLE OUTBOARD STRINGER NR 1 WAS FOUND TO BE DENTED BY THE GEAR DOOR TENSIONER. THE STRINGER WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES AND EMBRAER REPAIR GST-1034/01, DATED 3/30/01.SDR COMA0110068Stringer · crackedDURING 2C CHECK TASK 5410-432-04I, THE LEFT NACELLE OUTBOARD STRINGER NR 1 WAS FOUND TO BE CRACKED JUST AFT OF NACELLE FRAME 10. THE STRINGER WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR CALA0001580Rib · crackedINSPECTION FOUND A 6 INCH CRACK IN NR 2 PYLON SAILBOAT FAIRING LOWER RIB. REPAIR WAS COMPLETED IAW ECRA 5412-01011, SRM 51-31-01, AND DOUGLAS DRAWING AVB7306.SDR F3LA00221Rib · damagedDURING C-3 CHECK INSPECTION, FOUND 6TH RIB FROM REAR OF NR 2 ENGINE RT OUTBOARD COWL DAMAGED THROUGHOUT ENTIRE LENGTH. MAINTENANCE INSTALLED NEW RIB PER SRM 51-30-0. (M)SDR AU000602Longeron · cracked(AUS) A CRACK APPROXIMATELY 44.5 MM (1.75 INCHES) WAS FOUND IN THE RT OUTBOARD ENGINE NACELLE LONGERON, APPROXIMATELY 24 CM (9.5 INCHES) AFT OF THE ENGINE MOUNT FITTING. THE CRACK ORIGINATED FROM BENEATH STRAP P/N C6WM1712-27 WHICH WAS FITTED IAW DHC MOD 6/16SDR 20001017AP002Longeron · corrodedAT SCHEDULED COMPLIANCE OF AD 99-26-11, RIGHT NACELLE LEFT UPPER LONGERON EDDY CURRENT INSPECTION REVEALED EIGHT AREAS OF CORROSION OUT OF LIMITS. REMOVED AND REPLACED DAMAGED LONGERON IAW FAA APPROVED DATA CONTAINED IN BOMBARDIER SERVICE BULLETIN 7-54-19. (SDR 20001017AP001Longeron · corrodedAT SCHEDULED COMPLIANCE OF AD 99-26-11, LEFT NACELLE RIGHT UPPER LONGERON EDDY CURRENT INSPECTION REVEALED ONE CRACK AND TWO AREAS OF CORROSION OUT OF LIMITS. REMOVED AND REPLACED DAMAGED LONGERON IAW FAA APPROVED DATA CONTAINED IN BOMBARDIER SERVICE BULLETINSDR COMA0010113Stringer · dentedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE RT NACELLE OUTBOARD STRINGER NR 1 WAS FOUND TO BE DENTED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND SRM 54-10-01 FIGURE 202.SDR AU000564Longeron · cracked(AUS) ENGINE NACELLE RIGHT OUTBOARD LONGERON CRACKED IN AN AREA APPROXIMATELY 254 MM (10 INCHES) AFT OF THE ENGINE MOUNT FITTING. CRACK LENGTH APPROXIMATELY 57.15 MM (2.25 INCHES). FOUND DURING INSPECTION IAW AD/DHC6/51.4 (DHC6 SB 6/509).SDR COMA0010099Stringer · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LT NACELLE OUTBOARD STRINGER NR 1 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3656-1-REV IR, 5-10-00.SDR DL76G000774Spar · crackedTHE FWD UPPER SPAR WEB OF THE NR 1 PYLON WAS FOUND WITH A .25 INCH TYPICAL CRACK IN THE AFT, O/B CORNER OF THE POWER FEEDER CABLE CUTOUT. THE CRACK IS TYPICAL OF BAC S/B 767-54-0090. THE CRACKED AREA WAS ROUTED OUT AND A REPAIR/MOD DOUBLER INSTALLED PER SDR 20000503SH024Rib · crackedREPLACED CRACKED PYLON TRAILING EDGE RIB (RT). (EIA ECRA 740-54-029-2). (X)SDR TWAA0002011Rib · crackedDURING OP 16 MAINT CHECK THE NUMBER 2 ENG PYLON, OTBD SUPPORT RIB WAS CRACKED AT THE FWD END. REPLACED PART PER DAC INSTALLATION PRINT 9915502 AND INSTALLED RIB PN 9915501-502.SDR TWAA0002009Rib · crackedDURING OP 16 MAINT CHECK, FOUND NR 2 ENGINE PYLON, INBD RIB WAS CRACKED AT THE FWD END. REPLACED PART PER DAC INSTALLATION PRINT 9915503 AND INSTALLED RIB 9915503-502.SDR QXEA9902697Stringer · damagedPDX - HOLE IN STRINGER XN176.5 AT STATION ZN17.04. REPAIRED IAW HORIZON AIR EA 9-54-238, FIGURE 2.SDR QXEA9902694Stringer · crackedPDX - EXHAUST DECK AFT LATERAL STRINGER HAS ONE CRACK. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-40-11.SDR HNAA9900084Stiffener · crackedNR 2 NAC AFT STIFFENER IS CRACKED. REMOVED AND REPLACED STIFFENER.SDR HNAA9900083Stringer · crackedNR 2 NAC INBOARD STRINGER BELOW THE DECK IS CRACKED JUST PRIOR TO PREVIOUS REPAIR. REMOVED AND REPLACED STRINGER.SDR HNAA9900082Stringer · crackedNR 2 NAC OUTBOARD STRINGER IS CRACKED IN TWO PLACES AT THE REPAIR. REMOVED AND REPLACED STRINGER.SDR HNAA9900089Stringer · crackedNR 1 NAC AFT STRINGER IS CRACKED. REMOVED AND REPLACED AFT STRINGER.SDR ABXA9900533Stringer · crackedCRACK ON BOTTOM SIDE OF NR 3 ENGINE STRINGER. REPAIRED IAW DC8 SRM 78-2-0.SDR LR7A99132Longeron · corrodedDURING C CHECK/BRIDGING INSPECTION PER HSP7180, FOUND NR 3 QEC S/N LMG 1369-31 UPPER RT SLOPING LONGERON CORRODED. REPLACED LONGERON IAW SMP 583 54-20-03, HSPO7180, AND SB 382-71-12, REV 92. NR 959.SDR LR7A99131Longeron · corrodedDURING C CHECK/BRIDGING INSPECTION PER HSP7180, FOUND NR 2 ENGINE QEC S/N 3769-24 LOWER RT LONGERON CRACKED AND CORRODED AT FWD INNERFLANGE FIRESHIELD HOLE. REPLACED LONGERON IAW DWG 362501 AND SB 382-71-12. NR 944.SDR LR7A99104Longeron · corrodedDURING C CHECK/BRIDGING INSPECTION PER HSP7180 FOUND NR 3 QEC RT UPPER SLOPING LONGERON CORRODED. REPLACED LONGERON IAW SRM 583-54-20-08 AND SB 382-71-12, REV 92. NR 349 AND 959.SDR 99ZZZX1467Indicator · malfunctionedTCAS/VSI INDICATOR SHORTED INTERNALLY CAUSING SMOKE IN THE COCKPIT WHILE AIRCRAFT WAS REPOSITIONING FROM JET AVIATION TO SIGNATURE FLIGHT SERVICES FOR NEXT DAY DEPARTURE.SDR USAA990153Longeron · crackedPIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK IN WEB AT LEFT PYLON LOWER FLANGE STATION 1030. STOP DRILLED AND INSTALLED DOUBLER PER SRM 54-01. (M)SDR C2XA99IA163Stringer · crackedDURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND RIGHT NACELLE PANEL 425 IMPROPERLY REPAIRED AT FORWARD INBOARD END. REMOVED RIVETS FROM EXISTING REPAIR AND FOUND EXTENSIVE DAMAGE TO STRINGER. REPLACED STRINGER IAW SRM 51-40-02 AND 51-70-04. AIRCRAFT APPRSDR SIMA990334Longeron · puncturedABI - DURNG MBV INSPECTION, A PUNCTURE DUE TO CHAFING WAS DISCOVERED IN RIGHT NACELLE OUTBOARD LOWER LONGERON AT NS 289.33. BLENDED DAMAGED SURFACE TO VERY FINE SURFACE TEXTURE. PERFORMED EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED REINFORCEMENSDR CALA9801464Longeron · crackedINSPECTION FOUND A 2.5 INCH CRACK ON END CAP (LONGERON) PANEL NR 2 ENGINE FAIRING. THE LONGERON WAS REMOVED AND A NEW LONGERON WAS INSTALLED IAW SRM 51-30-2.SDR 98ZZZX3095Pylon · corrosionDURING MAJOR AIRFRAME INSPECTION, FOUND CORROSION ON PYLON SKIN AND STRAPS P/N 78286-76070-20086-101, -102. PARTS WERE CONSIDERED UNSERVICEABLE AND REPLACED. EXHAUST GASES COULD HAVE POSSIBLY ACCELERATED THE CORROSION PROCESS. REGULAR CLEANING OF TAIL AND ASDR SWAA980422Longeron · crackedDURING SCHEDULED D-CHECK, FOUND NR 1 PYLON LONGERON CRACKED JUST FWD OF BUBBLE FAIRING. REMOVED AND REPLACED PER BOEING SRM.SDR EIAA980126Stringer · crackedHKG - DURING 'C5/D' CHECK INSPECTION, NR 1 PYLON, CRACKED STRINGER AT NAC 166 OUTBOARD SIDE OF PYLON. REPAIRED IAW SRM 52-40-04 FIG 2. (X)SDR CA971117003Longeron · corroded(CAN) HEAVY CORROSION FOUND ON UPPER AND LOWER SURFACES OF THE UPPER LONGERONS. SEVERE CORROSION FOUND ON LONGERONS FROM STA. XN50 TO XN79.0. THIS CORROSION WAS NOT EVIDENT UNTIL THE COWL SEALS AND LATCH PLATES WERE REMOVED. FURTHER SEVERE CORROSION WAS FOUND SDR CA971117002Longeron · corroded(CAN) HEAVY CORROSION FOUND ON UPPER AND LOWER SURFACES OF THE UPPER LONGERONS. SEVERE CORROSION FOUND ON LONGERONS FROM STA. XN50 TO XN79.0. THIS CORROSION WAS NOT EVIDENT UNTIL THE COWL SEALS AND LATCH PLATES WERE REMOVED. FURTHER SEVERE COROSION WAS FOUND USDR CA971117001Longeron · corroded(CAN) HEAVY CORROSION FOUND ON UPPER AND LOWER SURFACES OF THE UPPER LONGERONS. SEVERE CORROSION FOUND ON LONGERONS FROM STA.XN50 TO XN79.0. THIS CORROSION WAS NOT EVIDENT UNTIL THE COWL SEALS AND LATCH PLATES WERE REMOVED. FURTHER SEVERE CORROSION WAS FOUND USDR CA971010001Longeron · corroded(CAN) HEAVY CORROSION FOUND ON UPPER AND LOWER SURFACES OF THE UPPER LONGERONS. SEVERE CORROSION FOUND ON LONGERONS FROM STA.XN50 TO XN79.0. THIS CORROSION WAS NOT EVIDENT UNTIL THE COWL SEALS AND LATCH PLATES WERE REMOVED. FURTHER SEVERE CORROSION WAS FOUND U
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