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.

SDR QXEA0200103Angle · crackedPDX - LT EXHAUST FINGERNAIL HAS A CRACK ON THE INBOARD BARREL TO SIDE SKIN CLOSING ANGLE. REPAIRED IAW DHC-8 RD 8-54-240 AND SRM 51-40-00.Jan 17, 2002 · N356PH · Dhav DHC8202SDR GTIA012218Web · crackedFTW - NR 1 ENGINE PYLON LOWER SURFACE AFT HINGE PANEL OUTBOARD LOWER WEB CRACKED AT ANGLE. REMOVED WEB. FABRICATED NEW WEB. INSTALLED WEB. REMOVED DAMAGED SECTION OF ANGLE. FABRICATED REPAIR ANGLE AND DOUBLERS. INSTALLED REPAIR ANGLE AND DOUBLERS IAW DC9Jan 17, 2002 · N12536 · Doug DC932SDR USAA020046Fitting · corrodedCLT - FOUND LUG/BORE CORRODED, INBOARD SIDE LOAD FITTING MOUNT LUG. REBORED/BLENDED/REWORK OF LUG/BUSHED PER EA 85775. (M)Jan 15, 2002 · N604AU · Boeing 757225SDR USAA020045Fitting · corrodedCLT - FOUND FITTING LUG/BORE WITH CORROSION. REWORKED LUG PER EA 85775. (M)Jan 15, 2002 · N604AU · Boeing 757225SDR ASOA02025Access Panel · brokenFLT 4318 - DURING CLIMB-OUT OF ATL, PASSING 500 FEET THE PILOT FELT A NOTICEABLE RHYTHMIC VIBRATION. AFTER PASSING 2000 FEET THE PILOT INCREASE THE AIRSPEED AND THE VIBRATION SUBSIDED. A PASSENGER RELAYED TO THE CREW THAT ONE OF THE ACCESS PANELS ON THE RIGHJan 15, 2002 · N640AS · Aerosp ATR72SDR 0200109603Rib · crackedDuring HCK in ATL the lower cap of the pylon closong rib YN165 was found cracked. Repaired per EA 96-185454.Jan 14, 2002 · N603NW · Doug DC932SDR SWIA200210677Web · crackedNACELLE WEB ON INBOARD RIGHT NACELLE CRACKED. INSTALLED NEW INBOARD FITTING AFT OF FRAME 13 AT NACELLE STATION 2425, SRM 51-10-02 AND 51-40-02.Jan 12, 2002 · N229SW · Emb EMB120ERSDR FPI2002F00004Channel · crackedUPPER U-CHANNEL ON ENGINE FIREWALL, BOTH LEFT AND RIGHT HAND ENGINE NACELLES. CRACK DEVELOPED WHERE ENGINE MOUNT BOLT RUNS THROUGH FIREWALL. PROBABLE CAUSE IS NORMAL ENGINE VIBRATION.Jan 11, 2002 · N9098Q · Beech 58SDR USAA020028Sleeve · damagedPIT - FOUND SLEEVE RIGHT WITH 3 INCH PUNCTURE, INNER AND OUTER SKIN AND HONEYCOMB CORE 6 INCH EDGE PANEL. COMPOSITE REPAIR IAW 54-30-70 FIG 201 AND SRM 51-70-17 PER EA 85845. (M)Jan 11, 2002 · N447US · Boeing 7374B7SDR QXEA0200063Web · damagedPDX - WEB RIVET HOLES FOR SPR BOX INBOARD BRACKET HOLES ARE ELONGATED. REPAIRED IAW HORIZON AIR EA 4-54-214.Jan 11, 2002 · N355PH · Dhav DHC8202SDR QXEA0200064Angle · crackedPDX - TWO CRACKS NOTED IN VERTICAL ANGLE ADJACENT TO FORWARD SPAR AND NACELLE. REPAIRED IAW DHC-8 SRM 51-40-11 AND SRM 51-40-00.Jan 9, 2002 · N355PH · Dhav DHC8202SDR QXEA0200004Strut · gougedPDX - NR 1 ENGINE INBOARD LOWER THRUST STRUT IS GOUGED AND CHAFED. REPAIRED IAW DHC-8-200 RD 8-54-036.Jan 3, 2002 · N374PH · Dhav DHC8102SDR UPS02237531Web · crackedINSPECTION TYPE:C+SI VERTICAL LT WEB CRACKED OVER ENGINE NR 2 HORIZONTAL FIREWALL AT BS 1376 APPROX. WEB REPLACED IAW DWG 65-17555.Jan 2, 2002 · N940UP · Boeing 727185CSDR UPS02237530Web · crackedINSPECTION TYPE:C+SI VERTICAL RT WEB CRACKED OVER ENGINE 2 HORIZONTAL FIREWALL AT BS 137 6 APPROX. WEB REPLACED IAW DWG 65-17555.Jan 2, 2002 · N940UP · Boeing 727185CSDR QXEA0102132Strut · gougedPDX - TWO GOUGES ON NR 2 ENGINE OUTBOARD LOWER TORQUE STRUT AT BOTTOM END. REPAIRED IAW RD 8-54-036.Dec 20, 2001 · N816PH · Dhav DHC8102SDR BJN2001F00004Latch · unlatchedDURING FLIGHT, THE SR FLIGHT ATTENDANT NOTIFIED THE CAPTAIN THAT A PIECE OF COWLING WAS LOOSE. THE CAPT CONFIRMED THAT THE NACELLE FAIRING THAT LIES BETWEEN THE WING AND THE ENGINE COWLING WAS LOOSE, THE COWLING LATCH HAD COME UNDONE AND THE FAIRING WAS AJAR Dec 3, 2001 · N789TM · Boeing 737282SDR 0104849856Web · crackedDuring Line check in ATL, the LH pylon closure rib at STA yn164 was found cracked at the lightening hole lower edge. Repaired per EA 98-185355.Nov 30, 2001 · N765NC · Doug DC951SDR UPS01837335Fitting · crackedINSPECTION TYPE:B NR 3 ENGINE PYLON AFT SPAR TO CANTED RIB FITTING CRACKED.Nov 24, 2001 · N802UP · Doug DC873FSDR SWIA200110461Channel · wornLEFT NACELLE OUTBOARD J-CHANNEL HAS DEEP GROOVES AT AFT END OUTBOARD OF AFT GEAR DOOR AREA. REPLACED J-CHANNEL REPAIR SECTION IAW EMB TECH. SUPPORT ENGINEERING APPROVAL, REF SST-1003/97 AND EMB120 SRM 51-40-02.Nov 21, 2001 · N199SW · Emb EMB120ERSDR 2002FA0000665Structure · corrodedDURING INSPECTION OF THE WING NACELLE BAGGAGE COMPARTMENT STRUCTURE CORROSION WAS DISCOVERED UNDER THE TRIM AND CARPETS. UPON REMOVAL OF THE NACELLE BAGGAGE COMPARTMENT TRIM AND CARPETS SEVER SURFACE CORROSION WAS DISCOVERED. MAJOR SECTION OF THE NACELLE STRNov 20, 2001 · N333SF · Cessna 411ASDR CA011123007Support · cracked(CAN) CRACKS FOUND AT ONE LOCATION WHILE PERFORMING REPEAT INSPECTION: FS 640, BL 0.0 (UPPER WEB).THIS WAS FOUND WHILE PERFORMING THE SB A601R-53-059.DISCREPANCIES WILL BE REPAIRED USING BOMBARDIER DISPOSITIONS.Nov 20, 2001 · Cndair CL6002B19SDR ARWA20011116Strap · crackedDURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND: NR 4 PYLON ACCESS DOOR 409 RT WITH TEMPORARY REPAIR, AFTER EVALUATION, FOUND CRACK ON OUTBOARD UPPER STRAP AT STA YUS 217. REPLACED STRAP IAW DC8 SRM 54-3-2,FIG 35, ITEM 5, NOTE 10. ACCOMPLISHED SB 54-70. Nov 20, 2001 · N1808E · Doug DC862SDR CA011123002Beam · cracked(CAN) THE ENGINE SUPPORT BEAM UPPER WEB CRACKED AT FS 640 RBL 9.5 AT 7.6 INCHES LONG AND ANGLE CRACKED AT 0.23 INCHES. THIS WAS FOUND WHILE PERFORMING THE SB A601R-53-059.DISCREPANCIES WILL BE REPAIR USING BOMBARDIER DISPOSITIONS.Nov 19, 2001 · Cndair CL6002B19SDR F3LA200100122Pylon · gougedDURING C-1 CHECK, INSPECTION REPORTED GOUGE IN NR 1 ENGINE PYLON, AFT OTBD LOWER CORNER. REMOVED GOUGE PER SRM 51-10-2. FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-2.Nov 18, 2001 · N270FL · Boeing 7372L9SDR CA011122012Support · cracked(CAN) CRACKS FOUND AT THREE LOCATIONS WHILE PERFORMING REPEAT INSPECTION. FS 640, BL 0.0 TO LBL 9.50, WL 199.6 DISCREPANCIES WILL BE REPAIRED.Nov 14, 2001 · Cndair CL6002B19SDR GTIA012309Doubler · brokenNR 2 ENGINE PYLON UPPER OUTBOARD LE STRUCTURE FRAME HAS BROKEN DOUBLER. REMOVED BROKEN DOUBLER. INSTALLED DOUBLER IAW DC9 SRM 51-30-2. (M)Nov 13, 2001 · N12536 · Doug DC932SDR QXEA0101908Mount Bracket · crackedPDX - RIGHT NACELLE FINGERNAIL MOUNTING BRACKET STIFFENER AND MOUNTING POINT ARE CRACKED. REPAIRED IAW EA 6-54-32 AND 6-54-34.Nov 12, 2001 · N407QX · Dhav DHC8*SDR QXEA0101907Mount Bracket · crackedPDX - LEFT NACELLE FINGER NAIL MOUNTING HOLES AND MOUNTING BRACKET ARE CRACKED. REPAIRED NACELLE DECK AND STIFFENER IAW EA 6-54-31, AND EA 6-54-33.Nov 12, 2001 · N407QX · Dhav DHC8*SDR CA011122008Support · cracked(CAN) ENGINE SUPPORT BEAM CRACKED ON TOP WEB 7TH RIVET OUT TO LEFT OF BL 0 AT AFT ROW OF RIVETS. CRACK IS FROM RIVET TO AFT EDGE OF MATERIAL. AIRCRAFT FERRIED FROM CINCINNATI TO HOT SPRINGS FOR REPAIR.Nov 9, 2001 · Cndair CL6002B19SDR 0104139916Rib · crackedDuring Hck at ATL, the pylon closing rib was found cracked at sta YN 176 LHS, at the portion of the lower cap. A new lower cap section was installed and spliced with repair angle. Material 0.040 TI-6AI-4V titanium. Repaired per EA 99-185300Nov 8, 2001 · N949N · Doug DC932SDR QXEA0101865Fitting · corrodedPDX - NR 2 NACELLE AFT MOUNT BEAM AT ENGINE CHATTER PROOF BOLT END HAS SURFACE CORROSION ON FORWARD LUG. REPAIRED IAW FOKKER SRM 51-01-04.Nov 5, 2001 · N482US · Fokker F28MK4000SDR 0103949869Angle · crackedDuring Line MTC., activities at the ATL base MTC. The lower angle (9959159-58) angle was found cracked at the 176 RHS at the aft end portion of the lower cap of the pylon closing rib. A new lower cap section was installed and spliced with a repair angle. 0.040Nov 3, 2001 · N778NC · Doug DC951SDR QXEA0101779Structure · chafedPDX - THERE IS A CHAFE IN THE RIGHT NACELLE ON THE OUTBOARD SIDE OF THE FIREWALL FLANGE APPROXIMATELY 3.5 INCHES DOWN FROM PREVIOUS REPAIR. REPAIRED IAW RD8-54-081.Nov 3, 2001 · N830PH · Dhav DHC8102SDR UPS01437324Frame · crackedINSPECTION TYPE:C #4 PYLON NAC STA 221 FRAME SEVERAL LOOSE AND SHEARED FASTENERS ON LHS 1/2" CRACK EMINATING FROM FASTENER HOLE. THE PYLON STA 221 FRAME WAS REPAIRED AS PER HX RS-53-34698 / UPS-HKG -01-00114H CONTINUE INSP REQUIRE PER SB 747-54A2202 AT 18 Nov 1, 2001 · N521UP · Boeing 747200SDR UPS01437329Frame · crackedINSPECTION TYPE:C #4 PYLON NAC STA 235.94 APPROX PYLON VALVE ACCESS PNL #483EL CUTOUT FWD FRAME CRACKED AS MARKED. CUTOUT FWD FRAME CRACK STOP DRILLED & NDT INSPECTION CONFIRMED CRACK FREE BEYOND DRILLED HOLE AS PER NTM PT6, 51-00-00 FIG 4 AND FRAME REPAIROct 30, 2001 · N521UP · Boeing 747200SDR QXEA0101704Angle · crackedPDX - RIGHT NACELLE HAS CRACKED CLOSING ANGLE ON THE OUTBOARD SIDE OF FIREWALL. REPAIRED RIGHT NACELLE IAW RD 8-54-806, RD 8-54-109, SRM 51-40-00 AND SRM 51-40-11.Oct 29, 2001 · N361PH · Dhav DHC8202SDR QXEA0101749Bracket · crackedPDX - NR 1 ENGINE INBOARD FIREWALL BRACKET IS CRACKED. REPAIRED IAW HORIZON AIR EA 2-54-111.Oct 25, 2001 · N354PH · Dhav DHC8202SDR 01FDEA00915Fairing · delaminatedPYLON NR 2 AFT FAIRING EDGE LT SIDE IS DISBONDED AND MISSING RIVETS. REMOVED AND REPLACED TRAILING EDGE PER EA 8-5410-56153 & SRM 54-12-02.Oct 25, 2001 · N377FE · Doug DC1010SDR 01FDEA00914Skin · crackedN 192 & N 351 #2 ENG INLET, AFT SIDE CRACK IN SKIN. R&R SKIN PER SRM 54-10-00 & 55-31-01 & EA 8-5410-56140.Oct 25, 2001 · N377FE · Doug DC1010SDR 0103929607Angle · crackedDuring Hck at ATL Base Maintenance, an existing repair angle was found cracked at sta 176 RHS at the aft portion of the lower cap of the pylon closing rib. Also, the lower cap was found trimmed at this location. The existing repair angle was removed and discarOct 24, 2001 · N607NW · Doug DC932SDR QXEA0101769Stiffener · crackedPDX - UNDERSIDE FINGERNAIL DECK OUTBOARD STIFFENER CRACKED. REPAIRED IAW DHC-8 SRM 51-40-11.Oct 23, 2001 · N354PH · Dhav DHC8202SDR ABXA010644Bolt · improperSTRUT FASTENERS INSTALLATION GRIP LENGTH NOT PER DRAWING, RIGHT STRUT. REPAIRED AREA IAW REA B654-42146MR.Oct 21, 2001 · N791AX · Boeing 767281SDR ABXA010629Bolt · improperSTRUT FASTENERS INSTALLATION GRIP LENGTH NOT PER DWG, LEFT STRUT. REPAIRED AREA IAW REA B654-42145MR.Oct 21, 2001 · N791AX · Boeing 767281SDR QXEA0101730Support · chafedPDX - NR 2 NACELLE AFT OVERBOARD DRAIN TUBE CHAFING ON UNDERSIDE OF FINGERNAIL SUPPORT DECK. REPAIRED IAW RD 8-54-097.Oct 21, 2001 · N354PH · Dhav DHC8202SDR QXEA0101714Bracket · crackedNR 2 ENGINE OUTBOARD FIREWALL BRACKET IS CRACKED. REPAIRED IAW RD 8-54-109, PAGES 1, 2, AND 3.Oct 18, 2001 · N354PH · Dhav DHC8202SDR QXEA0101711Fitting · corrodedPDX - RT MAIN LANDING GEAR H MEMBER WHERE ACTUATOR FITTING IS INSTALLED HAS PITTING CORROSION. REPAIRED IAW RD 8-54-921.Oct 17, 2001 · N354PH · Dhav DHC8202SDR CA011101011Web · cracked(CAN) TWO CRACKS FOUND ON ENGINE SUPPORT BEAM AT THE LOWER WEB FS 630, LBL 36, RBL 36 WHILE PERFORMING SB A601R-53-059. AREA TO BE REPAIRED IAW REO 601R-53-61-361.Oct 15, 2001 · Cndair CL6002B19SDR CA011101010Web · cracked(CAN) TWO CRACKS FOUND ON ENGINE SUPPORT BEAM AT THE LOWER WEB FS 630, LBL 36, WHILE PERFORMING SB A601R-53-059.AREA TO BE REPAIRED IAW RBO 601R-53-61-361.Oct 15, 2001 · Cndair CL6002B19SDR CA011101009Web · cracked(CAN) TWO CRACKS FOUND ON ENGINE SUPPORT BEAM AT THE LOWER WEB FS 630, BL R36. WHILE PERFORMING SB A601R-53-059.AREA TO BE REPAIRED IAW REO 601R-53-61-361.Oct 15, 2001 · Cndair CL6002B19SDR CA011101008Beam · cracked(CAN) TWO CRACKS FOUND ON ENGINE SUPPORT BEAM. ONE EACH AT THE CUT OUT FOR THE ACCESS PANELS.Oct 12, 2001 · Cndair CL6002B19
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