JASC 5410
Service difficulty reports · 4,119
Reports filed under 5410 · Nacelle/Pylon, Main Frame, 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 = '5410' 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 = '5410' 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 DL76S060601Fitting · damagedDURING MODIFICATION OF THE PYLON MIDSPAR FITTING, TWO HOLES WERE DAMAGED DURING FASTENER REMOVAL. THE HOLES WERE OVERSIZED TO REMOVE THE DAMAGE AND OVERSIZED FASTENERS WERE INSTALLED. REF AD2004-16-12.SDR QXEA200601981Structure · damagedPDX C3 LEFT HAND NACELLE EXHAUST DECK HAS A PREVIOUS REPAIR FILLER CRACKED, AFT END OF DECK AT APPROXIMATELY STATION XN302.00. REPAIRED IAW RD 8/4-54-044, DHC-8-400 SRM 54-35-20-350-802 AND 51-42-05.SDR QXEA200601984Support Beam · crackedPDX C3 LEFT HAND NACELLE, NR 3 FLAP TRACK MOUNTING SUPPORT BEAM HAS 7/8" CRACK IN TOP EDGE RADIUS. REPAIRED IAW HORIZON AIR EA 6-54-426 AND RD 8/4-54-368.SDR 2006UALA01401Support · wornNR 1 ENG PYLON INBOARD AND OUTBOARD NACELLE FAN COWL SUPPORT CHORD WORN STATION 166 TO 206. MAJOR REPAIR: BLENDED COWL SUPPORT.SDR USAA060875Channel · crackedLEFT ENGINE O/B PYLON VERTICAL CHANNEL AT UPPER END CRACKED. REPAIR FRAME DOUBLER IAW EA 97854, DEFECT SIZE: 1 INCH.SDR USAA060876Attach Fitting · crackedLEFT ENGINE L/B PYLON VERTICAL CHANNEL ATTACH CLIP CRACKED. REPAIR CLIP DOUBLER IAW EA 97854, DEFECT SIZE: 4 INCHES.SDR HALA0600479Angle · crackedNR 1 ENGINE PYLON O/B SKIRT FAIRING 3RD ANGLE FWD OF THE AFT ENGINE MOUNT CRACKED. REMOVED CRACKED SKIRT O/B SIDE OF PYLON AND INSTALLED NEW ANGLE PER SRM 51-40-04, AND SRM 51-40-02.SDR KCSA061184Doubler · gougedNR 3 PYLON INTERNAL DOUBLER (FOR EMERGENCY FUEL DRAIN TUBE) IS GOUGED OR CRACKED AT NAC STA 190, RT SIDE.SDR AALA20060803Retainer · damagedAFW - LEFT AND RIGHT HAND PYLON SKINS INBOARD AND OUTBOARD AT STATION 250 HAS GROOVE WORN FROM THRUST REVERSER SEAL RETAINER. BLENDED GROOVE PER MRB NUMBER 767 2842 AND PERFORMED HIGH FREQUENCY EDDY CURRENT INSPECTION. NO CRACKS FOUND. SYSTEM GROUND CHECKESDR QXEA200601862Diaphragm · crackedPDX C3 - RIGHT NACELLE OUTBOARD DIAPHRAGM IS CRACKED. REPAIRED IAW DHC-8-400 SRM 51-42-00 AND 51-42-05.SDR QXEA200601861Diaphragm · crackedPDX C3 - LEFT OUTBOARD NACELLE DIAPHRAGM IS CRACKED. REPAIRED IAW DHC-8-400 SRM 51-42-05, 51-40-15 AND 51-40-07.SDR CA060612003Nut · crackedONE (1X) NUT FOUND CRACKED.SDR 06FDEA1942Filler · crackedNR2 ENGINE SAIL TAIL FILLER AT EXHAUST NOZZLE HAS NUMEROUS CRACKS AS MARKED, 2 DEEP CHAF MARKS AND RIGHT FWD CORNER IS BROKEN. REMOVED SAIL TAIL FILLER IAW SRM 51-31-01. REPAIRED FILLER AS REQUIRED BY WELDING CRACKS AND CHAF MARKS ON MAE TRAVLER T6/593345.SDR DHL2006754515Structure · chafedLOWER FUSELAGE COWL FLANGE ANTI-CHAFE AREA IS WORN, AFT OF BULKHEAD (MARKED STA 1343). REMOVED FASTENERS LWR FUSELAGE AFT BULKHEAD STA 1343 IAW B727 SRM 51-30-2. CUT OUT DAMAGE AREA IAW B727 SRM 54-10-3 FIG 1 DIM 6.25 X .5 INCHES. FABRICATED ANGLE REPAIR FRSDR 06FDEA1879Repair · misinstalledCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED ON THE LT WING LOWER SURFACE OUTBD OF PYLON. EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR NEW REPAIR ACCOMPLISHED PER E.A.6-5710-99711 REPAIR EVALUATED PER GSDR MALA060310Structure · chafedDURING 2 YEAR CHECK IN BNA FOUND LT NACELLE, AT NS 197, IS CHAFED OUT OF LIMITS AT THE 3:00 POSITION AND HAS BEEN REPAIRED IAW MESABA EOS54162.SDR MALA060311Structure · chafedDURING 2 YEAR CHECK IN BNA FOUND RT NACELLE AT NS197 IS CHAFED OUT OF LIMITS AT THE 3:00 POSITION AND HAS BEEN REPAIRED IAW MESABA EO S54163.SDR QXEA200601204Latch · looseMFR FLIGHT NR 2148 NACELLE DOOR LATCH LOOSE. MAINTENANCE SECURED LATCH. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.SDR IWV2006F00000Channel · crackedDURING COMPLIANCE WITH AD 2005-12-13 BY INSTALLATION OF SPAR MOD KIT SK402-47B IT WAS DISCOVERED THAT THE LT NACELLE OB ENGINE SUPPORT BEAM CHANNEL PN 56541111 HAD A 1.75 INCH CRACK RUNNING LONGITUDINALLY ON THE IB RADIUS. THE AREA OF THE CRACK IS IN A LOCATSDR 06FDEA1664Support Fitting · corrodedNR 1 ENG PYLON ON FWD ENG MOUNT CASTING O/B OF PYLON HAS CORROSION ON FWD AND AFT SIDES IN SEVERAL AREAS. COMPLIED WITH FED EX EA 7-5410-99512 ON NR 1 ENGINE PYLON ON FWD ENG MOUNT CASTING O/B OF PYLON ON FWD AND AFT SIDES.SDR 06FDEA1663Support Fitting · corrodedNR 1 ENG PYLON HAS CORROSION ON FWD ENG SUPPORT FITTING WEB FWD LWR I/B JUST ABOVE LWR HORIZONTAL FLANGE COMMON TO EO 7-5410-7-3304 P9 PAGE 12 FIG 2. *S/D* COMPLIED WITH FED EX EA 7-5410-99512.SDR UIEA200600091Brace · chafedPYLON NR 3 DIAGONAL BRACE OUTBOARD SIDE ON ZONE 4 HAS TWO CHAFED AREAS. BLENDED OUT 2 AREAS, ACCOMPLISHED HFEC PER NDT MANUAL D6-7170, PART6 RT4 NO DEFECTS NOTED. ROTO PEEN AREAS, TREATED AND PRIMED AS PER BOEING SB 747-54-2198. REQUIRES REPETATIVE INSPECTISDR 2006UALA00814Flange · wornNR 1 PYLON FAN COWL UPR CHORD (311A1519) WAS FOUND WITH A 0.050 GROOVE WORN ON HORIZ FLANGE OF THE OTBD CHORD DAMAGE WAS CAUSED BY FAN COWL WEARING ON LWR SURFACE OF HORIZ FLANGE OF CHORD. NR 1 PYLON FAN COWL UPPER CHORD (311A1519) WAS REPAIRED PER AAR EA I06SDR MALA060285Rib · chafedDURING 2 YEAR CHECK IN BNA, FOUND RT NACELLE, FORWARD RIB IS CHAFED AT THE 3:00 POSITION. THE DAMAGE HAS BEEN REPAIRED IAW MESABA EO#S54158. REF: EAMS WORK ORDER 213802 TASK 4502.SDR QXEA200601290Rivet · looseYYC - C4 LEFT NACELLE, INBOARD SIDE, STATION XN122, BELOW WING LEADING EDGE, SEVERAL RIVETS ARE LOOSE. REPAIRED IAW RD8-54-1193.SDR MALA060271Fairing · chafedLT ENGINE LOWER DECK IS CHAFED OUT OF LIMITS AND HAS BEEN REPAIRED IAW MESABA EO NR S54095. REF: EAMS WORK ORDER 213801 TASK 4503.SDR MALA060272Fairing · chafedRT ENGINE LOWER DECK IS CHAFED OUT OF LIMITS AND HAS BEEN REPAIRED IAW MESABA EO S54095. REF: EAMS WORK ORDER 213801 TASK 4504.SDR ABXA060239Angle · crackedNR 2 ENGINE STRUT CLOSEOUT ANGLE WAS CRACKED JUST AFT OF THE OUTBOARD MID SPAR FITTING (INBOARD FASTENER OF THE CLOSEOUT FITTING ON THE OUTBOARD SIDE). REMOVED AND REPLACED CLOSEOUT FITTING IAW BOEING DWG 311T3150 AND BOEING SRM 51-40-2.SDR QXEA200601052Structure · crackedYYC - C4 RIGHT NACELLE LOWER COWL RIGHT SIDE FORWARD LATCH MATTING SURFACE CRACKED. REPAIRED IAW RD 8-71-030, ISSUE 3.SDR QXEA200600867Fastener · loosePDX - C4 THERE ARE EIGHT LOOSE/WORKING RIVETS ON RIGHT NACELLE, TOP SKIN, JUST AFT OF HORSE COLLAR ALIGNMENT PIN. REPLACED IAW DHC-8-200 SRM 51-40-20.SDR ABXA060235Beam · crackedNR 2 PYLON OUTBOARD BEAM WAS CRACKED AT AFT LATCH PIN RECEPTACLE. REPAIRED AREA IAW REA B654-53516-MR.SDR USAA060490Fastener · looseNR 2 PYLON UPPER SPAR FITTING ROTATED. REMOVED FASTENERS, REPLACED WITH OVERSIZED PER EA97464, DEFECT SIZE: .325 X .4520, 4 EA.SDR ASAA0640279Angle · crackedNR 2 PYLON AFT FAIRING 5843R SUPPORT CROSS ANGLE CRACKED AT FASTENER HOLE 14 INCHES BELOW WING SKIN. REPAIRED PER EA 51 40 01168.SDR MALA060180Structure · chafedDURING 2 YEAR CHECK IN BNA, FOUND LT NACELLE, INTAKE COMPARTMENT, LOWER DECK, IS CHAFED OUT OF LIMITS AND HAS BEEN REPAIRED IAW MESABA EO#S54095. REF: EAMS WORK ORDER 213644, TASK 4504.SDR QXEA200600885Strut · gougedPDX: LOWER AFT INBOARD ENGINE NACELLE STRUT FORWARD INBOARD FLANGE GOUGED. MAINTENANCE REPAIRED IAW RD 8/4-54-326, HORIZON EA 6-54-397 AND PSM 1-84-7A, PART 1 CHAPTER 51-00-06.SDR MALA060158Flange · chafedLEFT NACELLE, AT NS 197 IS CHAFED ON THE INBOARD FLANGE. REPAIRED IAW MESABA EOS54153.SDR MALA060159Flange · chafedRIGHT NACELLE, AT NS 197 IS CHAFED ON THE INBOARD FLANGE. REPAIRED IAW MESABA EOS54154.SDR QXEA200600716Structure · crackedYYC - C4 LEFT HAND NACELLE REAR DECK UNDER FINGERNAIL DECK IS CRACKED A RIVET FOR HYDRAULIC LINE BRACKET AT FORWARD SIDE OF REAR WHEEL WELL BULKHEAD. REPAIRED IAW HORIZON AIR EA 2-54-263 AND RD 8-54-2148 ISSUE 1.SDR 06FDEA1027Skin · damagedACCOMPLISH MAINTENANCE B-CHECK. NR 2 ENGINE CRK FOUND WITH ABOUT 4 INCHES ON AIR INLET INTERIOR SKIN SURFACE BETWEEN NR 5 AND NR 6 HOURS. REPAIRED PER CMM 71-11-05 FIG 603. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.SDR 2006UALA00471Fitting · crackedNR 2 PYLON MIDSPAR FITTING LOWER TANG AT INBOARD CLOSEOUT ANGLE HAS 2 EACH CRACKS COMING OUT OF THE INBOARD BOLT HOLE. 2 CRACKS EMANATING FROM INBD BOLT HOLE OF CLOSEOUT ANGLE INSTALLED OVER NR 2 PYLON MIDSPAR FITTING LOWER TANG WAS FOUND. THE CLOSEOUT ANGLE SDR QXEA200600680Drag Angle · crackedYYC C4, RIGHT HAND NACELLE, INBOARD DRAG ANGLE AT AFT FASTENER HOLE CRACKED. REPAIRED IAW RD 8-57-1053, ISS 2.SDR QXEA210600677Drag Angle · crackedYYC C4, LEFT HAND NACELLE, INBOARD SIDE, DRAG ANGLE INSIDE NACELLE AT REAR SPAR IS CRACKED ACROSS ONE RIVET. REPAIRED IAW RD 8-57-1053, ISS 2.SDR UPS06446629Structure · crackedNR 4 PYLON REAR ENGINE MOUNT BULKHEAD FOUND CRACK AT RT FWD FRAME WEB, CRACK LENGTH 7/16". REAR ENG MOUNT BULKHEAD FRAME 4 REPLACED AND REPAIRED AS PER HX RS NR R54-53-35457 CONTINUED TO INSP. THE REAR ENGINE MOUNT BULKHEAD PER THE REQUIREMENTS OF THE HX RS SDR QXEA200600696Strut · chafedYYC C4, RIGHT HAND NACELLE, LOWER OUTBOARD SIDE STRUT HAS CHAFFING DAMAGE TO INBOARD SIDE. REPAIRED IAW HORIZON AIR EA 2-54-261 AND RD 8-54-2146, ISSUE 1.SDR QXEA200600679Heat Shield · crackedYYC C4 , LEFT HAND NACELLE INTERNAL AFT END, OUTBOARD DISHED HEAT SHIELD IS CRACKED IN THREE CORNER, XN224.0, ZN0.0. REPAIRED IAW DHC-8-200 SRM 51-40-11, PAGES 1-4.SDR CA060301006Cowl Latch · damagedINSPECTION PERSONNEL AT VIKING AIR HAVE DISCOVERED A REOCCURRENCE OF SUBSTANDARD COWL LATCHES; THIS ISSUE WAS PREVIOUSLY RAISED, AND ADDRESSED THROUGH 2 SERVICE BULLETINS - TB/7 (FOR THE TURBO BEAVER) AND 6/34 (FOR THE TWIN OTTER).SDR CA060301005Cowl Latch · damagedINSPECTION PERSONNEL AT VIKING AIR HAVE DISCOVERED A REOCCURENCE OF SUBSTANDARD COWL LATCHES; THIS ISSUE WAS PREVIOUSLY RAISED, AND ADDRESSED THROUGH 2 SERVICE BULLETINS, TB/7 (FOR THE TURBO BEAVER) AND 6/34 (FOR THE TWIN OTTER).SDR MALA060107Structure · chafedDURING 2 YR CHECK IN BNA FOUND RIGHT NACELLE AT NS 197 IS CHAFED ON THE OUTBOARD SIDE. THE DAMAGE HAS BEEN REPAIRED IAW MESABA EOS54152.SDR MALA060108Structure · chafedDURING 2 YEAR CHECK IN BNA FOUND LEFT NACELLE, AT NS 197 IS CHAFED ON THE OUTBOARD SIDE. THE DAMAGE HAS BEEN REPAIRED IAW MESABA EOS54151.SDR MALA060104Bridge · chafedDURING 4K BRIDGE CHECK IN BNA FOUND LT NACELLE AT NS 197 IS CHAFED AND HAS BEEN REPAIRED 2/27/06 IAW MESABA EOS54150.
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