JASC 5400
Service difficulty reports · 1,907
Reports filed under 5400 · Nacelle/Pylon Structure, 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 = '5400' 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 = '5400' 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 QXEA9800693Strut · damagedNR 1 THRUST STRUT IS DAMAGED IN TWO LOCATIONS APPROXIMATLEY 7 AFT IN FORWARD END AND 10 FORWARD ON AFT END. REPAIRED IAW FOKKER SRM 54-40-03, PAGE 201 TO 203 AND HORIZON AIR EA 4-71-81.SDR AALA984114Fire Seal · wornAFW - FOUND WEAR ON INBOARD AND OUTBOARD OF LEFT PYLON FIRE SEAL AND 2 GAUGES ON PYLON AFT OF PNL 416BR. BLENDED DAMAGED AREA PER SRM, VERIFIED NO CRACKS AND REFINISH PER SRM. (M)SDR 98FDEA00324Fitting · crackedSTA-LAX - NR 3 PYLON HAS A HIGH FREQUENCY EDDY CURRENT CRACK INDICATION IN THE OUTBOARD ENGINE TRUSS FITTING AS PER FED-EX EO 8-5410-7-3323 PT W. COMPLIED WITH REPAIR AND TERMINATING MOD EO 8-5410-7-3323 PT 4.SDR TWAA9809303Fitting · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT PYLON WITH CORROSION ON FRONT SPAR LOWER BEAVER TAIL FITTING. REMOVED CORROSION ON BEAVER TAIL FITTING PER SRM 54-04, FIG 13. ROTOPEENED REWORKED AREA PER SRM 54-04, FIG 13, AND PLATED PER SRM 54-04, PAGE 53, ITSDR 98ZZZM456Fairing · crackedDURING AIRCRAFT CLEANING, THE LEFT PYLON AFT METAL FAIRING WAS FOUND TORN. THIS ITEM IS NOT IDENTIFIED IN THE GIV IPC OR THE GIV SRM. GAC IS AWARE OF THIS PROBLEM AND DOES HAVE A HAND DRAWING OF THE FAIRING. GULFSTREAM NEEDS TO ADDRESS THE PROBLEM WHEN THISSDR P5CA9800918Fairing · crackedNUMBER 2 PYLON LEFT SIDE SKIRT FAIRING AT NAC STA 153 CRACKED. REPAIRED AS PER SRM 51-40-02.SDR P5CA9800939Angle · crackedNR 1 ENG HYDRAULIC RESERVOIR INBD AND OUTBD SUPPORT ANGLE CRACKED AT MID AREA. REPAIRED PER SRM 51-30-02.SDR ABXA9800374Angle · crackedDURING C-CHECK, FOUND THE RIGHT PYLON INTERIOR ATTACH ANGLE CRACKED AT THE AFT ENGINE MOUNT UPPER SPAR LUG. REPLACED ANGLE IAW DC9 SRM 51-30-1 AND 51-30-5.SDR P5CA9800838Fairing · delaminatedNR 2 PYLON V FAIRING IS DELAMINATED. REPAIRED IAW SRM 51-40-06 FIG 17.SDR UPS98226746Web · crackedINSPECTION TYPE:D, SUSPECT CRACK ON LT WEB AT BS 1387 IN SUPPORT STRUCTURE ABOVE HORIZONTAL FIREWALL ENGINE NR 2. HFEC CARRIED OUT IAW B727 NDT MANUAL PART 6 51-00-00 FIG 4. CRACK CONFIRMED WEB REPLACED WITH WEB FABRICATED AND INSTALLED IAW DRG 657 555.SDR UPS98226745Web · crackedINSPECTION TYPE:D, SUSPECT CRACK ON RT WEB AT BS 1387 IN SUPPORT STRUCTURE ABOVE HORIZONTAL FIREWALL ENGINE NR 2. HFEC CARRIED OUT IAW B727 NDT MANUAL PART 6 51-00-00 FIG 4 . CRACK CONFIRMED WEB REPLACED WITH WEB FABRICATED AND INSTALLED IAW DRG 6517 555.SDR ARWA980481Strap · crackedDURING D-CHECK, FOUND NR 1 ENGINE PYLON, UPPER SUPPORT STRAP HAS A CRACK. REMOVED SUPPORT STRAP. FABRICATED NEW STRAP AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY DRAWING NR 5753033, 5753000 AND SRM 51-1-20D. WORK ACCOMPLISHED UNDER ARROW AIR FSDR P5CA9801000Bracket · crackedNR 1 PYLON GAP PANEL AREA CLOSURE SPAR RT SIDE FAIRING AFT BRACKET CRACKED. REPAIRED PER SRM 51-10-01 AND 51-10-02.SDR DHL9870737CInlet · crackedAT C-CHECK, CENTER INLET OUTER HOUSING DELAMINATED AND CRACKED FROM BS 1116 TO BS 1151 12 O'CLOCK TO 3 O'CLOCK POSITION. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8, 75 BY 38, 20 BY 38. N/R 4891.SDR DHL9870736CFitting · crackedAT C-CHECK, CENTER ENGINE INLET DUCT HOUSING ATTACH FITTING CRACKED AT STA 1130 RT SIDE I/B SIDE. REMOVED AND REPLACED ATTACH FITTING PER S/B 54-011, N/R 4829.SDR P5CA9800948Bracket · crackedNUMBER 1 PYLON CRACKED BRACKET AT MIDSPAR WEB STIFFENER AT NACELLE STA 211. BRACKET REPLACED AS PER SRM 51-10-01.SDR WTAA980070Nacelle · bird strikeSMF - BIRD STRKE TO RIGHT WING OUTBOARD NACELLE. MAINTENANCE INSPECTED AREA FOR DAMAGE. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)SDR MWEA98489Angle · crackedLEFT PYLON VERTICAL STIFFENER CRACKED FORWARD INBOARD CORNER OF ELECTRICAL CONNECTOR PANEL. MTC REMOVED CRACKED ANGLE FABRICATED AND INSTALLED REPLACEMENT ANGLE.SDR WTAA980066Nacelle · bird strikeSMF - BIRD STRIKE TO RIGHT NACELLE ON LANDING. MAINTENANCE INSPECTED AREA FOR DAMAGE. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)SDR DL72W981016S-Duct · crackedNR 2 ENG INLET DUCT INTERNAL UPPER S-DUCT CRACKED AT 9 O'CLOCK AT STA 1151. BLENDED AREA AND DYE CHECKED AND TREATED AND PAINTED AREA, NO MORE CRACKS WERE FOUND. ALL WORK PERFORMED PER ERA 331669-14 OK PER PRI 331669-14.C/W ERA 33169-14.SDR DL72W981015S-Duct · crackedNR 2 ENG INLET DUCT INTERNAL TWO CRACKS AT 3 O'CLOCK AND 11 O'CLOCK AT STA 1151 DOGHOUSE SIDE. REMOVED DAMAGE PER SRM 54-10-3 FIG 13. FABRICATED DOUBLER AND FILLER PER SRM 54-10-3 FIG 13. DYE CHECKED AREA PER PS 900-6-3 NR 1. NO CRACKS FOUND. OK TO INSTALSDR 98FDEA00274Stiffener · crackedNR 2 INLET INTERNAL 7TH RIB AFT OF FWD WEB ANGLE STIFFENER CRACK, 7:00 POSITION. *S/D* REMOVED ANGLE STIFFENER AND FABRICATED NEW STIFFENER IN REF SRM 51-00-01. INSTALLED STIFFENER REF SRM 54-10-00. 4-16-98.SDR 98FDEA00273Web · crackedNR 2 ENG INLET INTERNAL WEB BETWEEN 7TH AND 9TH RIB AFT OF FWD WEB CRACKED, 7:00 POSITION. *S/D* REMOVED RIB AND FABRICATED NEW RIB REF SRM 51-00-01. INSTALLED NEW RIB REF SRM 54-10-00. 4-16-98.SDR 98ZZZX1609Nacelle · crackedSMALL CRACK DISCOVERED AT LOWER RT CORNER OF ENGINE NACELLE AT OIL COOLER INTAKE. VIBRATION RUB AREA ADJACENT TO CRACK WAS DOWN TO BARE METAL.SDR 99ZZZM530Rib · crackedNR 1 PYLON INBOARD RIB NR 1 NUTPLATE AREA CRACKED. REPAIRED ABOVE DAMAGE TO INBOARD NR 1 PYLON NUTPLATE MOUNT STRIP FOR PANEL 451AT PER RIL HC546H9017, SEE WO BX5024 FOR REPAIR PIECE HEAT TREAT AND PLATING. (M)SDR UPS98226432Web · crackedINSPECTION TYPE-C, SUSPECT CRACK ON WEB ABOVE NR 2 ENGINE HORIZONTAL FIREWALL RT SIDE AT BS 1380. NEW WEB FABRICATED AND INSTALLED IAW DRAWING 65-17555.SDR UPS98426585Doubler · misrepairedINSPECTION TYPE-N/A, PREVIOUS DOUBLER REPAIR ON PYLON NR 3 LT SIDE FOUND INSTALLED ON THE AREA WHERE IT WILL INTERFERE WITH THE INSTALLATION OF NEW DOULBLER PER SB-54-2034. REMOVED PREVIOUS REPAIR, INSTALLED NEW REPAIR PER SB 54-2034.SDR TWAA9809305Fitting · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ON NR 1 PYLON FRONT SPAR LOWER BEAVER TAIL FITTING. REMOVED CORROSION ON BEAVER TAIL FITTING PER SRM 54-04, FIG 13. ROTOPEENED REWORKED AREA PER SRM 5-04, FIG 13 AND PLATED PER SRM 54-04, PAGE 53, ITEM 4.SDR UPS98226206Web · crackedINSPECTION TYPE-C, CRACK ON WEB ABOVE NR 2 ENGINE HORIZONTAL FIREWALL RT SIDE AT BS 1381. NEW WEB FABRICATED AND INSTALLED IAW DRAWING 65-17555.SDR UPS98226205Web · crackedINSPECTION TYPE-C, CRACK ON WEB ABOVE NUMBER 2 ENGINE HORIZONTAL FIREWALL LT SIDE AT BS 1381. NEW WEB FABRICATED AND INSTALLED IAW DRAWING 65-17555.SDR SWAA980439Angle · crackedDURING SCHEDULED C2 CHECK, FOUND PANEL ATTACH ANGLE ON TOP OF PYLON CRACKED, INBD SIDE. REMOVED AND REPLACED PER BOEING SRM.SDR CALA9800577Bracket · corrodedINSPECTION FOUND NR 2 PYLON UPPER PYLON TRAILING EDGE ATTACH BRACKET CORRODED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 54-32-02, 51-38-01, FIGURE 13, 51-21-01, 51-31-01.SDR P5CA9800708Fasteners · corrodedLEVEL 1 CORROSION ON NR 3 PYLON AFT STRUT DIAG BRACE AFT END LARGE HI-LOK HEADS. SURFACE CORROSION REMOVED PER SRM 51-10-01.SDR P5CA9800706Fasteners · corrodedANCHOR NUTS SURFACE CORROSION ON NR 3 PYLON NAC STA 379 TO 417. CORROSION REMOVED AND RETREATED PER SRM 51-01-01 AND 51-10-02.SDR P5CA9800543Fairing · crackedNR 4 PYLON, V FAIRING LEFT FWD CRACKED. REPAIRED FAIRING PER SRM 51-40-03.SDR P5CA9800537Fasteners · looseNR 4 PYLON INSIDE STRUT AT STA 221.9 LOOSE FASTENERS. REMOVED AND REPLACED FASTENERS PER SRM 51-30-02.SDR P5CA9800535Bracket · crackedNR 1 PYLON FILTER MOUNT BRACKED CRACKED, 2 EA. REPLACED PER SRM 51-40-03.SDR EIAA980161Doubler · crackedMZJ - DURING 'C4' CHECK INSPECTION, NR 2 PYLON OUTBOARD DOUBLER HAS A CRACK FROM CORNER RADIUS GOING INTO FASTENER HOLE STATION 180. INSTALLED NEW DOUBLER IAW SRM 51-10-02, 51-30-02, 51-30-05, AND S/B 747-54-2034. (M)SDR SWAA980279Support · crackedDURING SCHEDULED D-CHECK, FOUND L/W PYLON I/B T/E SUPPORT LONGERON UNDER SPRING DOOR ASSY IS CRACKED. REPAIRED PER BOEING SRM.SDR SWAA980278Angle · crackedDURING SCHEDULED D-CHECK, FOUND NR 1 PYLON UPPER AFT I/B L-CLIP CRACKED. REPAIRED PER BOEING SRM.SDR SWAA980277Angle · crackedDURING SCHEDULED D-CHECK, FOUND NR 1 PYLON AFT LOWER L STIFFENER CRACKED. REPAIRED PER BOEING SRM.SDR SWA980266Angle · crackedDURING SCHEDULED D-CHECK, FOUND R/W PYLON L-ANGLE STIFFENER CRACKED AT I/B SIDE. REMOVED AND REPLACED PER BOEING SRM.SDR ABXA9800202Stiffener · crackedDURING C-CHECK, FOUND STIFFENER CRACKED ON NR 2 PYLON WHERE THROTTLE CABLE PASSES THROUGH OUTBOARD SIDE OF PYLON. REPLACED STIFFENER IAW DACO DWG 9958220 AND DC9 SRM 51-30-2.SDR P5CA9800579Nut Plate · damagedNR 3 AFT ENGINE STRUT L/R 4 DAMAGED NUT PLATES. REMOVED AND REPLACED PER SRM 51-30-02.SDR P5CA9800576Strap · crackedNR 1 PYLON INTERNAL STRAP CRACKED AT STA 207. REPLACED PER SRM 51-10-01.SDR P5CA9800574Fasteners · missingNR 3 PYLON AFT FIXED FAIRING 4 ANCHOR NUTS MISSING. REPLACED FASTENERS PER SRM 51-10-01.SDR ABXA9800193Angle · crackedDURING C-CHECK, FOUND THE LEFT UPPER PYLON ATTACH ANGLE CRACKED BETWEEN STATION 1054 AND 1064. REPAIRED ANGLE IAW DC9 SRM 54-04.SDR ABXA9800157Stiffener · crackedDURING C-CHECK, FOUND NR 1 ENGINE PYLON STIFFENER CRACKED, (6 ABOVE FUEL SHROUD). REPLACED STIFFENER IAW DC9 SRM 51-30-2 AND 51-30-5.SDR P5CA9800736Brace · chafedNR 1 PYLON O/B SIDE DIAGONAL BRACE CHAFED FWD END. EDDY CURRENT C/W PER NDT PART 6 54-40-03 WITHIN LIMITS PER SRM 54-40-01. BLEND OUT AREA SHOT PEENED AND TREATED PER SRM 54-40-01 AND 51-70-00.SDR P5CA9800459Angle · crackedCRACK ON LEADING EDGE UPPER HORIZONTAL WEB INBOARD ATTACH ANGLE. REPAIRED PER BAC SRM 51-30-03.
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