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 HNAA2013032100140Heat Shield · crackedNR 2 NACELLE AFT HEAT SHIELD IS CRACKED AT TOP AFT STIFFENER AND 1 BOTTOM INBD STIFFENER. R & R WITH MADE REPAIRED PARTS. INSTALLED IAW SRM 51-42-05.Mar 21, 2013 · N336EX · Dhav DHC8311SDR DALA1307960184Splice Plate · mismanufacturedRING DOUBLER WITH TWO EXISTING HOLES LESS IAW DWG AT LT SIDE OF UPPER SPAR WEB ON NR 2 PYLON. REPAIRED IAW PRI 511844-14AD REV 1 AND ER/A 511844-14AD REV ORIG.Mar 15, 2013 · N184DN · Boeing 767332SDR 2014FA0000107Plate · gougedA GOUGE WAS DISCOVERED ON THE OTBD EDGE OF THE NR 1 PYLON REINFORCING PLATE. THE DAMAGE IS LOCATED OTBD OF RIB 8, FWD OF THE FRONT SPAR, THE GOUGE WAS BLENDED IAW SRM 51-73-00, RESULTING IN A BLENDOUT MEASURING 2.21" LONGITUDINALLY BY .013" DEPTH. THE WIDTH Mar 12, 2013 · N631VA · Airbus A320214SDR C77A20130313009Heat Shield · chafedNR 2 ENGINE PYLON, NR 1 HEAT SHIELD HAS CHAFE MARK 5.0" X 0.500" WIDE AT A DEPTH OF 0.040", PYLON STATION: XP 5847.0. REMOVED DAMAGE AND INSTALLED DOUBLER USING PRINCIPLES OF SRM 54-50-23 ON WO 681213-435 IAW ETD 2013-170-003367-A AND COMPASS EA E170-54-014, Mar 9, 2013 · N747CZ · Emb ERJ170100LRSDR FDEA201302270475Ferrule · crackedNR 2 PYLON FERRULE IS CRACKED COMPLIED WITH EA 6-5450-T0300139 REV NR PS P1 - NACELLES/PYLON PRECOOLER FERRULE CRACK ON NR 2 PYLON REF WR 54-50 6954.Feb 27, 2013 · N803FD · Airbus A310324SDR CWQR20130225011Heat Exchanger · crackedDURING A SCHEDULED INSPECTION, HEAT EXCHANGER SIDE PLATE HAD THREE CRACKS ABOUT .35 INCH LONG. OPPOSITE SIDE OF THE HEAT EXCHANGER WAS CRACKED IN TWO OF THE FOUR CORNERS. A NEW EXCHANGER WAS INSTALLED. PREFORMED A LEAK CHECK ON THE DEFECTIVE UNIT AND FOUNDFeb 25, 2013 · N349QS · Cessna 680CESDR GLBA2013022800188Plenum · debondedLT OTBD PLENUM PANEL DEBONDED APPROX 5" FROM THE TOP OF PANEL TO APPROX 15" DOWN, THE FULL WIDTH OF THE HONEYCOMB. REPAIRED IAW WITH A FIELD REPAIR.Feb 19, 2013 · N220GL · Beech 1900DSDR CA130905010Fairing · missing(CAN) ON ARRIVAL HAD THE "FWD PYLON FAIRING ASSY" MISSING ON THE NR 1 ENGINE. 5 OF THE 7 SCREWS WERE STILL IN THEIR PRESENT LOCATION. NO OTHER DAMAGE TO ACFT WAS FOUND. A NEW PANEL WAS INSTALLED. IN ORDER TO MAKE A COMPARISON, AN INSPECTION WAS CARRIED OUT Feb 17, 2013 · Emb ERJ190100IGWSDR HNAA20130200057Diaphragm · crackedDIAPHRAGM IS CRACKED ON RT FINGERNAIL AT STA XN215, OTBD LOWER CORNER. R & R DIAPHRAGM IAW STRUCTURAL REPAIR MANUAL 51-42-051.Feb 14, 2013 · N975HA · Dhav DHC8102SDR HNAA2013021400056Drag Angle · crackedLT NACELLE TO WING INBD DRAG ANGLE IS CRACKED. REPAIRED LT DRAG ANGLE IAW RD8-57-1053 AND RD8-51-0015. HIGH FREQUENCY EDDIE CURRENT WAS COMPLIED WITH IAW RD8-57-1053. NO DEFECTS NOTED.Feb 14, 2013 · N975HA · Dhav DHC8102SDR HNAA2013021400055Drag Angle · crackedRT NACELLE TO WING OTBD DRAG ANGLE WAS FOUND TO BE CRACKED. REPAIRED DRAG ANGLE IAW EA 16-2013-042. HIGH FREQUENCY EDDIE CURRENT WAS COMPLIED WITH IAW EA 16-2013-042. NO DEFECTS FOUND.Feb 14, 2013 · N975HA · Dhav DHC8102SDR HNAA2013021400053Structure · crackedLEFT NACELLE FWD DOOR OPENING, OTBD CORNING IS CRACKED. STOP DRILLED AND TRIMMED AWAY CRACK, FILLED AND SEALED IAW RD8-54-119.Feb 14, 2013 · N975HA · Dhav DHC8102SDR ASOA20130209260Doubler · corrodedACFT IS FOR A ESCALATION WORK WHEN THE FUSELAGE WAS FOUND CHAFED FROM CONTACT FROM A LANYARD INSIDE RT PYLON. MX INSTALL A DOUBLER OVER BLENDED AREA THAT WAS CHAFED FROM STRINGER 67 TO 68 IAW EC 5330-02698. ALL WORK WAS DONE AND WILL BE RELEASED AT THE END OFeb 9, 2013 · N12122 · Emb EMB145XRSDR A6WA2013021804666Fireshield · gougedGOUGE ON FIRESHIELD ON RIGHT LOWER CORE COLW LEADING EDGE. INSTALLED DOUBLER ON TO RIGHT LOWER CORE COWL LEADING EDGE TRIM STRIP.Feb 8, 2013 · N415AW · Cndair CL6002B19SDR HNAA2013020800041Structure · crackedLEFT ENGINE COWL OPENING IS CRACKED, XN 125.50. HFEC INSPECTION WAS DONE IAW RD8-54-1315. NO DEFECTS NOTED.Feb 8, 2013 · N975HA · Dhav DHC8102SDR HNAA2013020800039Drag Angle · crackedRT NACELLE TO WING OTBD DRAG ANGLE WAS FOUND CRACKED. DRAG ANGLE WAS REPAIRED IAW EA 16-2013-042. COMPLIED WITH HFEC INSPECTION. REINSTALLED ACCES SKIN PANEL IAW RD8-51-0015 AND SRM 51-42-05.Feb 8, 2013 · N975HA · Dhav DHC8102SDR UIEA2013021900099Stop · looseNR 1 PYLON AFT BULKHEAD OTBD STOP PAD FOUND LOOSE. (NR 1 PYLON AFT BULKHEAD SIDE LOAD FITTING WORN FASTENER HOLES REPAIRED IAW R1 NO R1-5400-10146 REV B.)Feb 4, 2013 · N476MC · Boeing 74747UFSDR UIEA2013021900097Frame · chafedNR 2 ENG RT CORE COWL INNER FACE NR 2 FRAME FOUND CHAFED. (NR 2 ENG RT CORE COWL INNER FACE NR 2 FRAME CHAFING MARK AREA REPAIRED IAW CN13-0428).Feb 4, 2013 · N476MC · Boeing 74747UFSDR UIEA2013021900096Frame · chafedNR 1 ENGINE LT CORE COWL NR 2 INTERIOR FRAME FOUND CHAFING MARK. (NR 1 ENG LT CORE COWL NR 2 INTERIOR FRAME CHAFING MARK AREA REPAIRED IAW SRM 54-45-02-2R1, REP 1, FIG 201.)Feb 4, 2013 · N476MC · Boeing 74747UFSDR DALA13006323213Structure · gougedDURING INSPECTION, FOUND LT PYLON PYRAMID MATING FACE AFT GUIDE PIN HOLE HAS GOUGE. REMOVED GOUGE IAW A320 TRM 54-51-18. CHECKED LIMITS: AREA 1L=0.284" W=0.062" D=0.063"; AREA 2 L=0.299" W=0.049" D=0.053". FOUND TO BE OUT OF LIMITS IAW TRM 54-51-18 FIG 2. ACFeb 4, 2013 · N313US · Airbus A320211SDR DALA13006313213Structure · gougedDURING INSPECTION, FOUND LT PYLON PYRAMID MATING FACE MID GUIDE PIN HOLE HAS GOUGE. REMOVED GOUGE IAW TRM 54-51-18. CHECKED LIMITS: AREA 1L=0.446" W=0.022" D=0.046"; AREA 2 L=0.338" W=0.047" D=0.080"; AREA 3 L=0.360" W=0.071" D=0.156". FOUND TO BE OUT OF LIMFeb 4, 2013 · N313US · Airbus A320211SDR UIEA2013020500070Access Panel · damagedDURING C3 CHECK, DAMAGE TO THE NR 4 PYLON, LT ACCESS PANEL NR 482IL WAS FOUND WITH A CRACK APPROX 6.0" IN LENGTH ON THE LOWER RADIUS AREA. ACCOMPLISHED AN INTERIM REPAIR.Feb 4, 2013 · N476MC · Boeing 74747UFSDR A6WA2013021804665Retainer · crackedLEFT LOWER PYLON DIVIDER PANEL SEAL RETAINER CRACKED. REMOVE AND REPLACE SEAL AND SEAL RETAINER PER SRM.Feb 1, 2013 · N415AW · Cndair CL6002B19SDR A6WA201302050665Structure · chafedCHAFE ON LEFT ENGINE UPPER CORE COWL FWD AT 11 O`CLOCK POSITION. REMOVED & REPLACED REBATE DISH WITH SERVICEABLE IAW SRM 51-22-00.Jan 30, 2013 · N412AW · Cndair CL6002B19SDR UALA2013013000569Door · damagedNR 2 ENGINE ACCESS DOOR ASSY DAMAGED.Jan 30, 2013 · N768UA · Boeing 777222SDR DALA13005093214Shackle · gougedDURING INSPECTION, FOUND NR 2 ENG PYLON AFT SHACKLE 1EA SIDE HAS GOUGED MARK AROUND THE BUSHING HOLE. BLENDED DAMAGE IAW SRM 51-73-00, CHECKED LIMIT DIMENSION DEPTH=.010" MAX ALLOW .006". FOUND TO BE OUT OF LIMIT IAW ER/A 507720-14MA. RECEIVED NEW SHACKLEJan 29, 2013 · N314US · Airbus A320211SDR 7AHR20130129011Rib · wornRT ENGINE COWL HAS AREA OF DAMAGE, AREA NR 7 RIB. REMOVED DAMAGE RIB ANGLE IAW SRM 51-40-3. FABRICATED NEW REPAIR ANGLE IAW SRM 51-40-3. INSTALLED NEW REPAIR ANGLE TO NR 7 RIB IAW SRM 51-40-3.Jan 29, 2013 · N842AL · Boeing 737290CSDR 7AHR20130129007Strap · wornNR 2 ENGINE UPPER FIXED COWL HAS A CHAFED STRAP. RUB STRAP DOUBLER FOUND TO BE WORN BEYOUD LIMITS IAW SRM 54-10-1. FABRICATED REPAIR PARTS IAW SRM 51-20-1. INSTALLED STRAP DOUBLER IAW SRM 51-30-2.Jan 29, 2013 · N842AL · Boeing 737290CSDR DALA1704200181Spar · crackedNR 2 PYLON MID SPAR WEB CRACKED.Jan 25, 2013 · N181DN · Boeing 767332SDR A6WA201302054666Structure · damagedELONGATED HOLES ON RIGHT ENGINE LOWER CORE COWL ALIGNMENT PIN HOLES. REPAIRED IAW CMM 71-12-01 REPAIR SRS109.Jan 25, 2013 · N412AW · Cndair CL6002B19SDR DALA1302210649Structure · damagedON WALK AROUND FOUND NR 1 ENG INBD FAN COWL. DELAMINATED ON INBD LOWER LEADING EDGE. APROX 3 IN X 3 IN DELAMINATION. REMOVED RT FAN COWL. WIP 644787. APPLIED PERMANENT REPAIR IAW SRM 51-70-17, PARA 4GT. REINSTALLED RT FAN COWLINGS.Jan 21, 2013 · N649DL · Boeing 757232SDR FDEA201301110083Mount · corrodedNR 2 ENG PYLON FWD ENG MOUNT FITTING, ALL 4 TENSIL BOLT HOLES AND SPOT FACES HAVE OXIDATION AT UPPER SURFACE. ALL TENSILE BOLT HOLES IN LIMITS AFTER OXIDATION REMOVAL IAW FSRM 54-51-81, 2 FIG, 104 SHT 2. BOTH INBD AND OTBD AFT SPOTFACES FOUND TO BE OUT OF LIJan 11, 2013 · N664FE · Airbus A300F4605RSDR UALA2013011100190Rub Strip · damagedNR 4 ENGINE INBRD REV T/E RUB STRIP DAMAGED. REMOVED AND REPLACED DAMAGED RUB STRIP.Jan 10, 2013 · N181UA · Boeing 747422SDR UALA2013010700066Nose Cowl · dentedDAMAGE TO NR 2 NOSE COWL AT 6:00 POSITION. REPLACED NR 2 NOSE COWL PER AMM.Jan 6, 2013 · N214UA · Boeing 777222SDR CA121221014Latch · damaged(CAN) MFG HAS FOUND, DURING PRODUCTION INSPECTIONS, THAT THERE EXISTS A POSSIBILITY THAT THE PIVOT PIN IN COWL LATCH, PN C6EC1002-95 CAN BECOME DISLODGED FROM THE LATCH HOUSING. MFG IS IN THE PROCESS OF NOTIFYING THE OPERATING FLEET OF THIS SITUATION.Dec 18, 2012 · Dhav DHC6*SDR HALA2012120400234Channel · crackedNR 2 ENGINE STRUT HAS CRACKED CHANNEL ON AFT WEB OF LOWER FACED FAIRING. REPLACEMENT CHANNEL FABRICATED AND INSTALLED.Dec 4, 2012 · N580HA · Boeing 76733AERSDR IXXA2013041500001Structure · crackedNR 2 ENGINE-RT CORE COWL CRACKED 1.5", STA NAC. 272.30 AND STA NAC 261.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, DEC 3, 2012. DWG NR ED 5544, NOVEMBER 07,2012. REMOVED FASTENERS IAW SRM 51-40-02. TRIMMED OUT DAMAGED AREA IAW DWG NR ED 5544 NOV 07,20Dec 3, 2012 · N791AX · Boeing 767281SDR DALA1255830183Bushing · crackedNR 1 PYLON STRUT LOWER SPAR FITTING BUSHINGS HAVE SEALANT CRACKED AND BUSHINGS REPLACED IAW SRM 54-53-90, FIG 201.Dec 1, 2012 · N183DN · Boeing 767332SDR DALA1255820183Bushing · crackedNR 2 PYLON STRUT LOWER SPAR FITTING BUSHINGS HAVE SEALANT CRACKED AND BUSHINGS REPLACED IAW SRM 54-53-90, FIG 201.Dec 1, 2012 · N183DN · Boeing 767332SDR HYIA20121203002Beam · crackedDURING A SCHEDULED MX EVENT, THE RT ENGINE ASSY WAS REMOVED FOR A SCHEDULED TIME CHANGE. UPON REMOVAL, A CRACK WAS DISCOVERED AT THE RT NACELLE CROSSOVER BEAM IN THE AREA OF TURBOCHARGER BRACKET HOLE LOCATIONS. LOCATION OF CRACK RELATIVE TO RT NACELLE CROSSOVDec 1, 2012 · N1361G · Cessna 402CSDR DALA1255760183Bushing · crackedNR 2 PYLON STRUT FWD UPPER SPAR FITTING BUSHINGS HAS SEALANT CRACKED AND HAVE BEEN REPLACED IAW SRM 54-53-90, FIG 201.Nov 29, 2012 · N183DN · Boeing 767332SDR DALA1255750183Bushing · crackedNR 1 PYLON STRUT FWD UPPER SPAR FITTING BUSHING HAS SEALANT CRACKED AROUND BUSHING AND THE BUSHING HAS BEEN REPLACED IAW SRM 54-53-90, FIG 201.Nov 29, 2012 · N183DN · Boeing 767332SDR HYIA20121126003Beam · corrodedSEVERE CORROSION WAS DISCOVERED BETWEEN RT NACELLE OTBD ENGINE BEAM AND LOWER NACELLE SKIN. RIGHT NACELLE OTBD BEAM HAT CHANNEL WHICH IS SANDWICHED BETWEEN BEAM AND LOWER NACELLE SKIN, IS SEVERELY CORRODED. REMOVED RT NACELLE OTBD ENGINE BEAM , PERFORMED DETNov 24, 2012 · N1361G · Cessna 402CSDR DALA1255111607Bolt · wrong partNR 1 ENGINE AFT PITCH LOAD FITTING FASTENER REMOVED FOUND TO BE DIFFERENT GRIP LENTH FROM THOSE STATED IN EA 01-451812-03, AD OPN 2801 TO VERIFY. EARN NR N1607B-0056 RAISED AND NR 1 ENGINE AFT PITCH LOAD FITTING INSTALLED IAW ERA 507119-14 AD, REV 0 SDR RAISENov 23, 2012 · N1607B · Boeing 767332SDR DALA1255101607Bolt · wrong partNR 2 ENGINE AFT PITCH LOAD FITTING FASTENER REMOVED. FOUND TO BE DIFFERENT GRIP LENGTH FRON THOSE STATED IN EA 01-451812-03AD, OPN 2801 TO VERIFY. EARN NR 1607B-0057 RAISED AND NR 2 ENG AFT PITCH LOAD FITTING INSTALLED IAW ERA 507119-14AD PRI REV 0 SDR RAISEDNov 23, 2012 · N1607B · Boeing 767332SDR FDEA201211194098Door · missingNR 1 ENGINE PYLON FORWARD FAIRING INBD AFT BLOWOUT DOOR MISSING. PERFORMED DECAY PRESSURE CHECK IAW MM 36-00-01-5, NO LEAKS OR OTHER DEFECTS NOTES. REPLACED MISSING PRESSURE RELIEF DOOR IN REF SRM 51-30-01 AND COMPLIED WITH EA 8-5410-164823, PART 3 (NO 1 ENGNov 19, 2012 · N385FE · Doug MD1010FSDR FDEA201211154040Support Angle · crackedANGLE CRACKED NR 1 PYLON INBD SIDE NAC STA 102.1. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED NEW SUPPORT ANGLE IAW SRM 51-40-05 AND INSTALLED IAW SRM 51-40-02 AND DWG 311N3510, REV C.Nov 15, 2012 · N994FD · Boeing 75723ASDR FDEA201211154039Angle · crackedANGLE CRACKED NR 2 PYLON INBD SIDE NAC STA 102.1. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED NEW SUPPORT ANGLE IAW SRM 51-40-05 AND INSTALLED IAW SRM 51-40-02 AND DWG 311N3510, REV C.Nov 15, 2012 · N994FD · Boeing 75723ASDR CA121113002Attach Angle · cracked(CAN) DURING INSPECTION, CRACKS WERE FOUND IN THE FORWARD PORTION OF THE NR 2 NACELLE OTBD ATTACHMENT ANGLE. SECTION CONTAINING CRACKS WAS REPLACED IAW RD 8-57-1053. SIMILAR FINDINGS ON THE AFT PORTION OF THE NR 1 NACELLE INBD DRAG ANGLE FWD PORTION OF THE Nov 13, 2012 · Dhav DHC8301SDR UALA2012110606372Access Panel · damagedENGINE MOUNT ACCESS DOOR (436BR ) ON NR 1 ENGINE HAS MISSING FASTENER. REMOVED PANEL 161-1051 (436BR) AND DEFERRED PER CDL 54D. INSTALLED NEW PANEL ON NR 1 PYLON PANEL NR 436BR.Nov 6, 2012 · N653UA · Boeing 767322
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