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 AALA20061160Clamp · looseDFW - WING BODY OVERHEAT LIGHT NUMBER ONE ILLUMINATED ON CLIMB-OUT. ACCOMPLISHED PROCEDURE AND LIGHT EXTINGUISHED. LANDED AUA WITHOUT INCIDENT. ACCOMPLISHED BITE CHECK OF THE COMPARTMENT OVERHEAT DETECTION UNIT. FOUND FAULT CODE 14. FOUND LOOSE CLAMP OUTBDec 3, 2006 · N931AN · Boeing 737823SDR USAA061357Angle · crackedNR 1 PYLON INBOARD SIDE UPPER T/E AFT END CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 51-10-02, DEFECT SIZE: 1 INCH.Nov 26, 2006 · N405US · Boeing 737401SDR USAA061358Angle · crackedNR 1 PYLON JUST ABOVE FLAP CUTOUT I/B FWD SIDE OF CROSSOVER BEAM CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 51-10-02 AND DRAWING 65C26300, DEFECT SIZE: 1 INCH.Nov 26, 2006 · N405US · Boeing 737401SDR USAA061359Angle · crackedNR 1 PYLON JUST ABOVE FLAP CUTOUT CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS, DEFECT SIZE: 1 INCH.Nov 26, 2006 · N405US · Boeing 737401SDR USAA061360Angle · crackedNR 1 PYLON LOWER SIDE OF FLAP CUTOUT CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 51-10-02 AND DRAWING NR 65C26300.Nov 26, 2006 · N405US · Boeing 737401SDR 2007FA0000110Stud · brokenON POST-FLIGHT INSPECTION, MAINTENANCE CREW FOUND NR 2 ENGINE COMPRESSOR FOD. WE DISCOVERED A MISSING COWL FASTENER STUD IPC ITEM 16 FIG 53-20-03 PAGE 0. WHEN FASTENER FAILS, THE LOCKING TAIL OF STUD FALLS INSIDE THE ENGINE AIR PLENUM AND THEN INGESTED BY ENNov 25, 2006 · N88CP · Skrsky S76CSDR 06FDEA04078Structure · crackedPYLON NR 2 AT STA YID 453.322 UPPER SURFACE ON HORIZ WEB STRUCTURE FOUND CRACK 2.5" LONG. REMOVED AFT PYLON UPPER FAIRING (RIF SRM 54-52-02 VOL 3). PERFORMED REPAIR IAW EA# 8-5450-103662. REINSTALLED FAIRING IAW SRM 54-52-02 VOL 3.Nov 21, 2006 · N395FE · Doug MD1010FSDR DL76S060990Web · crackedTHE NR 1 STRUT MIDSPAR WEB WAS FOUND CRACKED. THE CRACKED WEB REINFORCED WITH A DOUBLER.Nov 16, 2006 · N125DL · Boeing 767332SDR COMA0660627Fairing · brokenFLIGHT 5221 - RAMP PERSONNEL REPORTED A PIECE OF DEBRIS WAS FOUND ON RAMP. A/C RETURNED BACK TO TUL AND WAS INSPECTED AND FOUND TO HAVE A DAMAGED RIGHT LOWER STANG FAIRING. REMOVED AND REPLACED RIGHT LOWER STANG FAIRING.Nov 10, 2006 · N959CA · Cndair CL6002B19SDR KCSA061500Support Bracket · crackedNR 4 PYLON INTERNAL FRAME SUPPORT BRACKET IS CRACKED AT NAC STA 270, OUTBOARD SIDE OF TOP FRAME.Nov 10, 2006 · N702CK · Boeing 747146SDR CA061110006Frame · broken(CAN) DURING INSPECTION FOR SB NR 59, C046-23 FOUND BROKEN AT THE EAR AS DESCRIBED IN THE SB PART, ON ORDER FOR REPLACEMENT AND A KIT KI-185 TO PREVENT VIBRATION OF THE TUBE WILL BE INSTALLED. FRAME WILL BE SENT TO MFG FOR EVALUATION IAW THEIR REQUEST. (TC NRNov 9, 2006 · Robsin R44RAVENIISDR QXEA200603460Web · crackedC3 PDX - LEFT DIAPHRAGM WEB ON NR 1 NACELLE JUST INBOARD OF OUTBOARD FLAP CRACKED STATION XN 210, YN-18, ZN 20. REPAIRED IAW SRM 51-42-45 AND 51-40-07.Nov 1, 2006 · N413QX · Bombdr DHC8402SDR NSVA200600183Latch · malfunctionedLEFT ENGINE COWL POPPED OPEN ON TAKEOFF. UPON AIRCRAFT ARRIVAL AT GATE, FOUND LT INBOARD COWLING UNLATCHED. INSPECTED ENGINE COMPARTMENT AND COWLING (LATCHES, MOUNTS ETC.) FOR ANY DAMAGE AND FOUND NONE. LATCHED AND SECURED COWLING.Oct 26, 2006 · N352CJ · Saab 340BSDR ABXA060298Stiffener · crackedSTIFFENER CRACKED AT FORWARD LOWER CORNER OF PANEL 437 BL CUTOUT INSIDE. REPAIRED CRACKED STIFFENER IAW REA B654-54-930 MR.Oct 24, 2006 · N748AX · Boeing 767232SDR ABXA060297Structure · crackedCRACKED STRUCTURE JUST BELOW PANEL 437BR OPENING AT FORWARD LOWER CORNER. REPAIRED AREA IAW REA B654-64932.Oct 24, 2006 · N748AX · Boeing 767232SDR 2006UALA02059Angle · crackedNR 1 PYLON MIDSPAR CLOSEOUT ANGLE CRACKED AT BOTH INBD FASTENERS. STOPPED DRILLED CRACK. INSTALLED STRAP AND FILLER REPAIR.Oct 24, 2006 · N658UA · Boeing 767322SDR QXEA200603440Structure · crackedPDX C4 - LEFT NACELLE AFT CROSS SPRINGER ON TOP OF AFT NACELLE DECK CRACKED 11" FORWARD OF AFT END OF DECK. REPAIRED IAW DHC-8-200 SRM 51-40-11.Oct 23, 2006 · N362PH · Dhav DHC8202SDR TRAX200600897Beam · crackedENGINE BOX BEAM HAS A CRACK AT RT LOWER ACCESS PANEL FORWARD IB CORNER. CRACK IS APPROXIMATELY 1.5- 2 INCHES LONG. REPAIRED RIDE SIDE LOWER BOX BEAM WEB AT ACCES PANEL REF REO 11/01/06 01R-53-61-366 (CLOSED 11/01/06)Oct 18, 2006 · N909EV · Cndair CL6002B19SDR HALA0600821Angle · crackedCRACK NR 1 PYLON IB CLOSE OUT ANGLE OF MID SPAR FITTING. REPAIRED CRACK ON NR 1 PYLON IB CLOSE OUT ANGLE OF MID SPAR FITTING, IAW HAL M105 NR 585051.Oct 9, 2006 · N585HA · Boeing 767300SDR VOX2006F00000Latch · brokenLATCH LINK BROKE ON TOP ENGINE, COWLING LEFT AIRCRAFT. NO DAMAGE TO REST OF AIRCRAFT. RECOMMEND INSTALLING SCREW ON BOTH SIDES OF COWLING SECURING COWLING TO BACK UP IF LATCH BREAKS. (K)Oct 6, 2006 · N60FL · Mtsbsi MU2B60SDR QXEA200602720Bracket · crackedC3 PDX - LEFT NACELLE TRAILING WING TO OUTBOARD NACELLE DIAPHRAGM BRACKETS IS CRACKED. REPAIRED IAW SRM 51-40-10 AND 51-42-05.Oct 5, 2006 · N414QX · Bombdr DHC8402SDR QXEA200602650Bracket · crackedC3 PDX-LT NACELLE TRAILING WING TO OB NACELLE DIAPHRAM BRACKET IS CRACKED. REPAIRED IAW SRM 51-40-10 AND SRM 51-42-05.Oct 3, 2006 · N414QX · Bombdr DHC8402SDR QXEA200602698Channel · chafedRT NACELLE STATION XN121 FIREWALL SEAL CHANNEL WORN THROUGH ABOVE OIL COOLER. REPAIRED IAW SRM 51-40-11.Oct 2, 2006 · N360PH · Dhav DHC8202SDR QXEA200602672Attach Bracket · wornC4 YYC - LEFT ENGINE COWL SIDE DOOR 414AR HOLD OPEN ROD ATTACHMENT BRACKETS ON AFT END OF DOOR ARE WORN. REPAIRED IAW EA 2-71-335.Sep 30, 2006 · N350PH · Dhav DHC8202SDR QXEA200602675Retainer · gougedC4 YYC - LEFT NACELLE XN121, ZN21 SEAL RETAINER IS GOUGED THROUGH AT INBOARD AND OUTBOARD ENDS. REPAIRED IAW SRM 51-40-11.Sep 30, 2006 · N350PH · Dhav DHC8202SDR DXTA200601619Door · departedRIGHT SIDE ENGINE COWL DEPARTED AIRCRAFT IN FLIGHT. INSTALLED SERVICEABLE COWLING, REMOVED FROM N947QS S/N 750-0047. AIRCRAFT FERRIED TO MANUFACTURER FOR FOR INVESTIGATION OF CAUSE.Sep 28, 2006 · N962QS · Cessna 750SDR QXEA200602696Panel · damagedC4 YYC - NR 2 NACELLE TOP STRUCTURE INBOARD AND OUTBOARD FILLET PANELS BETWEEN XN110 AND XN127 HAS 7 LOOSE RIVETS. REPAIRED IAW SRM 51-40-00.Sep 27, 2006 · N360PH · Dhav DHC8202SDR QXEA200602692Fastener · looseNR 2 NACELLE OB SIDEWALL EXTERIOR HAS 5 LOOSE RIVETS AT STA XN178 AND ZN24.25. REPAIRED IAW SRM 51-40-00.Sep 27, 2006 · N350PH · Dhav DHC8202SDR QXEA200602697Skin · damagedC4 YYC - NR 2 NACELLE HORSE COLLAR EXTERIOR SKIN PANEL HAS LOOSE RIVETS AT TOP ENGINE MOUNT AREA. REPAIRED IAW SRM 51-40-00.Sep 27, 2006 · N360PH · Dhav DHC8202SDR NOCA13906Frame · missingAFTER TAKEOFF RIGHT ENGINE EGT CLIMBED O 863 DEGREES CELCIUS. UPDATED (10/04/06) PERFORMED FIM TASK 71-03-00 FIG 116 AND NO FAULTS FOUND IN INSP, PERFORMED TEST NR 3 IP/HP COMPRESSOR AIRFLOW TEST. ACCOMPLISHED TEST NR 13 TAKEOFF POWER TEST AND NO ABNORMALITISep 23, 2006 · N756NA · Boeing 75728ASDR QXEA200602616Bolt · missingC3 PDX - 5 JO BOLTS EITHER MISSING OR PULLED THROUGH LEFT NACELLE TOP AFT OUTBOARD AT XN210.00. REPAIRED IAW RD8/4-54-154.Sep 21, 2006 · N410QX · Bombdr DHC8402SDR QXEA200602615Bolt · missingC3 PDX - CONTINUATION FROM N/R 156603 - 5 JO BOLTS EITHER MISSING OR PULLED THROUGH LEFT NACELLE TOP AFT OUTBOARD AT XN210.00. REPAIRED IAW RD8/4-54-154.Sep 21, 2006 · N410QX · Bombdr DHC8402SDR QXEA200602611Support · crackedC3 PDX - LEFT NACELLE OUTBOARD FLAP TRACK SUPPORT CENTER IS CRACKED ON TOP FLANGE 4 RIVETS FROM AFT END. REPAIRED IAW RD8/4-54-378.Sep 21, 2006 · N410QX · Bombdr DHC8402SDR QXEA200602613Diaphragm · crackedC3 PDX - LEFT NACELLE DIAPHRAGM CRACKED. REPAIRED IAW RD8/4-54-155.Sep 21, 2006 · N410QX · Bombdr DHC8402SDR QXEA200602608Support · crackedC3 PDX - LEFT NACELLE OUTBOARD FLAP TRACK SUPPORT CASTING IS CRACKED ON TOP FLANGE LAST RIVET AFT. REPAIRED IAW RD8-54-378.Sep 21, 2006 · N410QX · Bombdr DHC8402SDR 2006UALA01760Structure · damagedNR 1 PYLON CANTILEVER STRUCTURE DAMAGED FROM CONTACT WITH JET WAY.Sep 13, 2006 · N855UA · Airbus A319131SDR DL757060744Fitting · misrepairedTHE NR 1 PYLON INBOARD MID SPAR FITTING WAS INCORRECTLY OVERSIZED. THE HOLE WAS OVERSIZED TO THE NEXT SIZE FASTENER AND A LARGER FASTENER WAS INSTALLED REF 2003-18-05.Sep 12, 2006 · N632DL · Boeing 757232SDR QXEA200602485Diaphragm · crackedC3 PDX - RIGHT NACELLE OUTBOARD DIAPHRAGM IS CRACKED. REPAIRED IAW SRM 51-42-05, 51-42-15.Sep 9, 2006 · N410QX · Bombdr DHC8402SDR QXEA200602385Panel · chafedPDX - C3 CHECK- NR 1 ENGINE STUBWING AFT PANEL CHAFED AGAINST EMPENNAGE SKIN. STRIPPED PAINT AROUND AREA FOR INSPECTION. BLENDED DAMAGE AS PER SRM 51-12-00. WITHIN LIMITS. TREATED AND PAINTED AREA.Aug 23, 2006 · N602QX · Cndair CL6002C10SDR QXEA200602381Cowling · chafedPDX- C3 CHECK- LEFT UPPER TRANSCOWL INBOARD RETAINER IS CHAFED WITH CONTACT FROM THE FAN COWL. REPAIRED AREA AS PER CRJ-700 SRM 51-12-00-001-001-A01. REPAIR FOUND TO BE WITHIN LIMITS .139" REMAINING. NO CRACKS NOTED. TREATED AND PAINTED.Aug 23, 2006 · N602QX · Cndair CL6002C10SDR QXEA200602382Intake · chafedPDX- C3 CHECK- LEFT UPPER FAN COWL IS CHAFED FROM CONTACT WITH THE CORE COWL RETAINERS. REPAIRED PER CRJ-700 SRM 51-12-00-001-001-A01. NO CRACKS NOTED. TREATED AND PAINTED AREA.Aug 23, 2006 · N602QX · Cndair CL6002C10SDR MALA060516Structure · chafedDURING 4 K CHECK IN BNA, FOUND LT ENGINE, LOWER FORWARD DECK IS CHAFED OUT OF LIMITS, AND HAS BEEN REPAIRED IAW MESABA EO NR S54095. REF: EAMS WORK ORDER 214264 TASK 4508.Aug 14, 2006 · N439XJ · Saab 340BSDR BSAASDR0619Latch · malfunctionedDURING CRUISE, A PASSENGER REPORTED TO THE CREW THAT THE RT FWD COWLING HAD COME LOOSE. WHEN THE CREW LANDED, THEY NOTED A YAW UPON TOUCHDOWN. THE IB FWD COWL LATCH HAD COME LOOSE FIRST, ALLOWING THE COWLING TO CONTACT THE SPINNER SCREWS. THE IB AFT COWL LATCHAug 8, 2006 · N173YV · Beech 1900DSDR QXEA200602075Strut · scratchedPDX C4 NR 2 NACELLE UPPER OUTBOARD ENGINE SUPPORT STRUT LIGHTLY SCRATCHED ON FORWARD END FITTING INBOARD RIB, INBOARD OF BOLT HEAD. REPAIRED IAW HORIZON AIR EA 2-54-292.Aug 7, 2006 · N351PH · Dhav DHC8202SDR CALA0600284Stiffener · crackedINSPECTION FOUND NR 2 PYLON I/B CLIP, FRAME, AND STIFFENER CRACKED AT STA 275. THE CLIP, FRAME, AND STIFFENER WERE REPLACED IAW SRM 51-10-02.Jul 31, 2006 · N67158 · Boeing 767224SDR WRLA2006032Plate · corrodedDURING "C" CHECK IN SAT FOUND NR 1 ENG LEFT FAN COWL CENTER U BOLT PLATE HAS FRETTING CORROSION. REMOVED CORROSION FROM BOLT PLATE, MATERIAL LOSS WAS 0.030 FOUND TO BE OUT OF LIMITS IAW DC10 SRM 51-00-01 FIG 1A. FABRICATED NEW BOLT PLATE, TREATED AND PRIMED. Jul 26, 2006 · N303 · Doug DC1030FSDR WRLA2006033Rub Strip · corrodedDURING "C" CHECK IN SAT FOUND NR 1 ENG LT CORE COWL FWD RUB STRIP AND RH CORE COWL AFT RUB STRIP HAVE CORROSION. REMOVED & REPLACED NR 1 ENG LT CORE COWL FWD RUB STRIP FROM 6 TO 12 O'CLOCK POSITION AND REMOVED & REPLACED RT CORE COWL AFT RUB STRIP FROM 3 TO 6Jul 23, 2006 · N303 · Doug DC1030FSDR WRLA2006031Nose Cowl · crackedDURING "C" CHECK IN SAT FOUND NR 1 ENG NOSE COWL UPPER RH INNER ACOUSTICAL PANEL LOWER FWD CORNER HAS A COMBINATIONOF CRACK .7" CIRCUMFERENTIAL THAT EXTENDS BEYOND 2 FASTNERS AND .6" LONGITUDINAL AND CORROSION. DAMAGE FOUND TO BE TOO EXCESSIVE PER DC10 SRM VOLJul 21, 2006 · N303 · Doug DC1030FSDR UPS06847651Drag Angle · crackedINSPECTION TYPE:C1, 3 POSSIBLE CRACKS ON BULKHEAD FWD OF CENTER SPAR UPPER BOLT IB DRAG ANGLE. REMOVED, FABRICATED AND INSTALLED DRAG ANGLE IAW SRM 51-1-21, DWG 5615767 AND 51-1-20D.Jul 19, 2006 · N806UP · Doug DC873FSDR QXEA200601919Bracket · chafedPDX C4 - RIGHT NACELLE GRAVEL GUARD LOWER FOUR RECEPTICAL MOUNT BRACKETS HAVE LIGHT CHAFE DAMAGE OF MATING SURFACE. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-20-16 AND SRM 51-20-36.Jul 18, 2006 · N358PH · Dhav DHC8202
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