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.

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.Dec 11, 2002 · N410QX · Bombdr DHC8401SDR 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-PROTECTEDDec 2, 2002 · N906UP · Boeing 72730CSDR CA020913012Longeron · cracked(CAN) NR 2 ENGINE NACELLE LONGERON CRACKED ON INBOARD SIDE.Sep 5, 2002 · Dhav DHC6SDR 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.Aug 6, 2002 · N404QX · Bombdr DHC8401SDR QXEA0200654Stringer · crackedPDX- LT NACELLE FINGERNAIL DECK FORE AND AFT LOWER STRINGERS ARE CRACKED. REPAIRED IAW DHC-8 SRM 51-40-11.Apr 16, 2002 · N351PH · Dhav DHC8202SDR 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.Oct 21, 2001 · N354PH · Dhav DHC8202SDR 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.Aug 21, 2001 · N379PH · Dhav DHC8202SDR COOSDR010078Longeron · crackedENGINE NR 2, FORWARD FIREWALL-LONGERON, PN 65-53558-54 CRACKED.Aug 20, 2001 · N767TW · Boeing 737230SDR 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.Aug 7, 2001 · N349PH · Dhav DHC8202SDR 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.Aug 7, 2001 · N349PH · Dhav DHC8202SDR 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.Aug 7, 2001 · N349PH · Dhav DHC8202SDR 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.Aug 7, 2001 · N349PH · Dhav DHC8202SDR 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.Aug 7, 2001 · N349PH · Dhav DHC8202SDR 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.Aug 7, 2001 · N349PH · Dhav DHC8202SDR 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.Apr 18, 2001 · N463CA · Emb EMB120RTSDR 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.Mar 12, 2001 · N462CA · Emb EMB120RTSDR 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.Oct 14, 2000 · N14075 · Doug DC1030SDR 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)Aug 4, 2000 · N118RW · Boeing 7372Y5SDR 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 6/16Jun 6, 2000 · Dhav DHC6300SDR 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. (May 26, 2000 · N706GA · Dhav DHC7102SDR 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 BULLETINMay 23, 2000 · N706GA · Dhav DHC7102SDR 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.May 19, 2000 · N263CA · Emb EMB120RTSDR 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).May 15, 2000 · Dhav DHC6300SDR 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.May 11, 2000 · N258CA · Emb EMB120RTSDR 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 Apr 20, 2000 · N155DL · Boeing 7673P6SDR 20000503SH024Rib · crackedREPLACED CRACKED PYLON TRAILING EDGE RIB (RT). (EIA ECRA 740-54-029-2). (X)Feb 4, 2000 · N940F · Doug DC933FSDR 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.Jan 31, 2000 · N925L · Doug DC932SDR 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.Jan 31, 2000 · N925L · Doug DC932SDR QXEA9902697Stringer · damagedPDX - HOLE IN STRINGER XN176.5 AT STATION ZN17.04. REPAIRED IAW HORIZON AIR EA 9-54-238, FIGURE 2.Dec 19, 1999 · N825PH · Dhav DHC8102SDR QXEA9902694Stringer · crackedPDX - EXHAUST DECK AFT LATERAL STRINGER HAS ONE CRACK. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-40-11.Dec 19, 1999 · N825PH · Dhav DHC8102SDR HNAA9900084Stiffener · crackedNR 2 NAC AFT STIFFENER IS CRACKED. REMOVED AND REPLACED STIFFENER.Jun 11, 1999 · N914HA · Dhav DHC8102SDR HNAA9900083Stringer · crackedNR 2 NAC INBOARD STRINGER BELOW THE DECK IS CRACKED JUST PRIOR TO PREVIOUS REPAIR. REMOVED AND REPLACED STRINGER.Jun 11, 1999 · N914HA · Dhav DHC8102SDR HNAA9900082Stringer · crackedNR 2 NAC OUTBOARD STRINGER IS CRACKED IN TWO PLACES AT THE REPAIR. REMOVED AND REPLACED STRINGER.Jun 11, 1999 · N914HA · Dhav DHC8102SDR HNAA9900089Stringer · crackedNR 1 NAC AFT STRINGER IS CRACKED. REMOVED AND REPLACED AFT STRINGER.Jun 10, 1999 · N914HA · Dhav DHC8102SDR ABXA9900533Stringer · crackedCRACK ON BOTTOM SIDE OF NR 3 ENGINE STRINGER. REPAIRED IAW DC8 SRM 78-2-0.May 26, 1999 · N816AX · Doug DC863FSDR 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.Apr 11, 1999 · N404LC · Lkheed 382GSDR 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.Apr 11, 1999 · N404LC · Lkheed 382GSDR 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.Apr 11, 1999 · N404LC · Lkheed 382GSDR 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.Mar 22, 1999 · N76FD · Amd FALCON50MYSTSDR 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)Feb 27, 1999 · N937VJ · Doug DC931SDR 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 APPRFeb 16, 1999 · N31711 · Emb EMB120RTSDR 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 REINFORCEMENFeb 2, 1999 · N202KD · Saab 340BSDR 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.Aug 15, 1998 · N14245 · Boeing 7372C0SDR 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 AJul 27, 1998 · N376AL · Skrsky S76ASDR SWAA980422Longeron · crackedDURING SCHEDULED D-CHECK, FOUND NR 1 PYLON LONGERON CRACKED JUST FWD OF BUBBLE FAIRING. REMOVED AND REPLACED PER BOEING SRM.Mar 27, 1998 · N332SW · Boeing 7373H4SDR 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)Feb 17, 1998 · N471EV · Boeing 747273CSDR 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 Sep 30, 1997 · Dhav DHC7102SDR 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 USep 30, 1997 · Dhav DHC7102SDR 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 USep 30, 1997 · Dhav DHC7102SDR 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 USep 30, 1997 · Dhav DHC7102
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