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 UPS00434318Bracket · crackedINSPECTION TYPE:C, PYLON NR 4 CRACK FOUND IN HYD RES SUPPORT BRACKET. BRACKET REPLACED.Nov 3, 2000 · N675UP · Boeing 747123SDR ASAA0040123Structure · damagedPAE DURING SCHEDULED MAINTENANCE CHECK, FOUR HOLES WERE DAMAGED ON THE NR2 PYLON OUTBOARD SID OF AFT HINGE FITTIN MOUNT AT NACELLE STA 224. REPAIRED IN ACCORDANCE WITH EA 5430-01078.Oct 26, 2000 · N774AS · Boeing 7374Q8SDR ASAA0040124Fairing · gougedPAE DURING MAINTENANCE INSPECTION FOUND N1 ENGINE SLEEVE TO STRUT FAIRING OUTBOARD SIDE, HAS A GOUGE IN THE CENTER AREA 6 INCHES LONG AND .5 INCHES WIDE. REPAIRED IN ACCORDANCE WITH EA 5450-01051.Oct 26, 2000 · N774AS · Boeing 7374Q8SDR DL72L002109Structure · damagedAFT END OF DOGHOUSE 6 O''CLOCK POSITION DOUBLER PEELED BACK ON BOTH SIDES OF INLET SKIN BUTT JOINT. REMOVED DAMAGE PER SRM 54-10-3D FIG 801D. DYE PENETRANT INSP AREA, NO CRACKS FOUND SRM 54-10-10-3D. CHEMICAL TREATED PER 900-2-4 NR 02. APPLIED EPOXY PRIMEOct 25, 2000 · N508DA · Boeing 727232SDR DL72L002094Fitting · crackedDURING INSPECTIONS REQUIRED BY AD 97-05-08 6 CRACKS WERE FOUND IN THE NR 1 FORWARD ENGINE PYLON AND ONE CRACK WAS FOUND IN THE NR 3 PYLON. ERA 396334-14AD OVERSIZES THE FASTENER HOLES TO REMOVE THE CRACK PER FEDEX AVIATION SERVICES S/B 2000-5410A01 AT HMV.Oct 24, 2000 · N508DA · Boeing 727232SDR AALA2001742Angle · crackedTUL - NR 3 ENGINE PYLON UPPER OUTBOARD ANGLE AT FIREWALL AFT OF FORWARD ENGINE MOUNT CRACKED BETWEEN FASTENERS. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-10-1. (M)Oct 18, 2000 · N883AA · Boeing 727223SDR 0003999940Attach Angle · crackedDURING L-CHECK, FOUND CRACK IN RIGHT HAND PYLON UPPER ATTACH ANGLE AT BS 996. REPAIRED PER EA 99-17403 AND SRM 54-04 FIGURE 10. REF LOG PAGE 1510889.Oct 18, 2000 · N3322L · Doug DC932SDR DL72L002040Frame · crackedCHANNEL WORN/DAMAGED ALONG LWR FLANGE 5 O CLOCK TO 6 O CLOCK POSITION AT NR 2 ENG FWD COWL CUTOUT. REPAIRED PER MM 53-11-0 PG 801.Oct 17, 2000 · N504DA · Boeing 727232SDR DL72S001995Frame · chafedNR 2 ENG CUTOUT FRAME LIP WORN THROUGH 9:00 POS STA 1352. REPAIRED PER MM 53-11-0 PG 801.Oct 10, 2000 · N515DA · Boeing 727232SDR 20001113SH016Structure · damagedIAD/SAL - FLT 581 - AT THE GATE, PREVIOUS TO FLIGHT, A TRACTOR HIT THE ENGINE NR 1. A HOLE OF 6 INCHES BY 3 INCHES WAS DONE ON THE FAN COWL AND A HOLE OF 2 INCHES BY 1 INCH WAS DONE ON THE INBOARD FAN COWL. THE AIRCRAFT REMAINED ON GROUND AT IAD STATION FOR Oct 6, 2000 · N458TA · Airbus A320233SDR QXEA0002861Stiffener · crackedPDX- LEFT HAND NACELLE AFT UPPER DECK RIGHT HAND LONGITUDINAL STIFFENER ON BOTTOM SIDE IS CRACKED 4 INCHES FROM FORWARD END. REPAIRED IAW DHC-8 SRM 51-40-01 AND 51-20-00.Sep 30, 2000 · N366PH · Dhav DHC8202SDR QXEA0002860Stiffener · crackedPDX- LEFT HAND NACELLE AFT UPPER DECK LEFT HAND LONGITUDINAL STIFFENER ON BOTTOM SIDE IS CRACKED IN TWO PLACES 4 AND 12 INCHES FROM FORWARD END. REPAIRED IAW DHC-8 SRM 51-40-11 AND 51-20-00.Sep 30, 2000 · N366PH · Dhav DHC8202SDR QXEA0002858Stiffener · crackedPDX- LEFT HAND NACELLE AFT UPPER DECK FOURTH STIFFENER FROM AFT ON TOP SIDE IS CRACKED THROUGH, 6 INCHES FROM RIGHT HAND END. REPAIRED IAW DHC-8 SRM 51-40-11.Sep 30, 2000 · N366PH · Dhav DHC8202SDR QXEA0002857Stiffener · crackedPDX- LEFT HAND NACELLE AFT UPPER DECK SECOND STIFFENER FROM AFT ON TOP SIDE IS CRACKED IN TWO PLACES, 7 INCHES AND 13 INCHES FROM RIGHT HAND SIDE. REPAIRED IAW DHC-8 SRM 51-40-11.Sep 30, 2000 · N366PH · Dhav DHC8202SDR QXEA0002856Stiffener · crackedPDX- LEFT HAND NACELLE, AFT UPPER DECK AFT STIFFENER ON TOP SIDE IS CRACKED 5.5 INCH FROM RIGHT HAND END. REPAIRED IAW DHC-8 SRM 51-40-11.Sep 30, 2000 · N366PH · Dhav DHC8202SDR QXEA0002859Angle · chafedPDX- ATTACHING ANGLE FOR LEFT HAND NACELLE EXHAUST THUMBNAIL CHAFED AROUND RIGHT HAND AFT NUT PLATE HOLE. REPAIRED IAW DHC-8 RD 8-54-163.Sep 29, 2000 · N366PH · Dhav DHC8202SDR CA001103010Fitting · cracked(CAN) CRACK DETECTED VISUALLY IN WEB OF RIGHT ARM OF THE NR 1 ENGINE FORWARD MOUNT FITTING. THE ENGINE WAS REMOVED TO FACILITATE LAP JOINT MODIFICATION AND REMOVAL TASK CARD CALLS FOR INSPECTION OF ALL ENGINE MOUNTS.Sep 19, 2000 · Boeing 737230CSDR MALA000603Structure · chafedFOUND DURING C-CHECK, THE LT NACELLE DECK IS CHAFED AT ACCESS NACELLE PANEL 452AL, REFER TO CELSUIS TASK CARD 4522, W/O 18829. MAINTENANCE REMOVED DAMAGED AREA OF NACELLE DECK IAW SRM 54-10-30. NDT PERF FVNDT006EC, NO CRACKS NOTED. FABRICATED REPAIR DOUBLERSep 13, 2000 · N449XJ · Saab 340BSDR MALA000588Strap · chafedFOUND DURING C-CHECK, THE FORWARD ATTACH FLANGE ON RT ENGINE COWL CHAFED AT 464AT. REFER TO CELSIUS TASK CARD 4524, W/O 18816. MAINTENANCE BLENDED CHAFED FWD FLANGE ON RT ENG COWL 464AT IAW 51-70-40. CHAFE EXCEEDS ALLOWABLE LIMITS REF SRM 51-10-10, REMOVED Sep 7, 2000 · N414XJ · Saab 340BSDR EISA20000174Angle · crackedNR 1 ENGINE NOSE COWL AFT SECTION AT BULKHEAD FLANGE CRACKED. REMOVED, FABRICATED REPAIR ANGLE AND FILLER, DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED IAW B727-200 SRM 51-10-2, 54-10-3.Sep 1, 2000 · N12305 · Boeing 727231SDR 20001212AP008Support Bracket · crackedNR 4 ENGINE FIRE LOOP MOUNT TUBE AT 12:00 POSITION ABOVE HIGH PRESSURE TURBINE CRACKED. REMOVED AND REPLACED FIRE LOOP SUPPORT BRACKETS IAW AMM 26-11-01. (M)Aug 30, 2000 · N742SA · Boeing 747230BSDR 20001212AP007Support Bracket · crackedNR 3 FIRE LOOP SUPPORT BRACKET AT 1:00 POSITION ABOVE THE DIFFUSER AT THE ELECTRICAL CONNECTION TO THE LOOP IS CRACKED. REMOVED AND REPLACED FIRE LOOP SUPPORT BRACKETS IAW AMM 26-11-01. (M)Aug 30, 2000 · N742SA · Boeing 747230BSDR 20001212AP006Support Bracket · crackedNR 2 FIRE LOOP SUPPORT BRACKET AT 1:00 POSITION ABOVE THE DIFFUSER AT THE ELECTRICAL CONNECTION TO THE LOOP IS CRACKED. REMOVED AND REPLACED FIRE LOOP SUPPORT BRACKETS IAW AMM 26-11-01. (M)Aug 30, 2000 · N742SA · Boeing 747230BSDR 20000911SH009Structure · corrodedWHILE C/W A DETAILED VISUAL INSPECTION OF THE LEFT PYLON SPIGOT BALL JOINT HOLE AS DIRECTED BY A310 MPD TASK NR 545017-02-1, CORROSION WAS NOTED. AFTER CORROSION REMOVAL, THE SPIGOT BALL JOINT HOLE EXCEEDED THE ALLOWABLE LIMITS SPECIFIED IN SB A310-54-2019. Aug 28, 2000 · Airbus A310322SDR 20000911SH008Structure · corrodedWHILE C/W A DETAILED VISUAL INSPECTION OF THE RIGHT PYLON SPIGOT BALL JOINT HOLE AS DIRECTED BY A310 MPD TASK NR 545017-02-1, CORROSION WAS NOTED. AFTER CORROSION REMOVAL, THE SPIGOT BALL JOINT HOLE EXCEEDED THE ALLOWABLE LIMITS AS SPECIFIED IN SB A310-54-201Aug 28, 2000 · Airbus A310322SDR MALA000632Stiffener · crackedFOUND DURING C-CHECK, LOWER STIFFENER CRACKED ON ENGINE COWL 453CL. REFER TO CELSUIS TASK CARD 4516, W/O 18783. MAINTENANCE STOP DRILLED CRACK, FABRICATED REPAIR FROM 301 1/4 .032 REF SRM 51-20-20. 51-40-60, FAY SEALED AND INSTALLED REF SRM 51-20-50 AND 51-4Aug 23, 2000 · N447XJ · Saab 340BSDR C2XA00IA325Frame · crackedNDT INSPECTION OF NR 1 NACELLE, NR 1 FRAME REVEALED A CRACK IN THE HORIZONTAL REINFORCING RIB JUST OUTSIDE OF THE OUTER, UPPER BOLT HOLE ON THE INBOARD END OF FRAME. REMOVED CRACKED FRAME, RECEIVED NEW FRAME, LOCATED AND DRILLED FRAME IAW EMB-20 SRM 51-25-00.Aug 21, 2000 · N26714 · Emb EMB120RTSDR MWEA00724Bracket · crackedMKE - FOUND CRACK ON ANGLE BRACKET LEFT PYLON AREA FUSELAGE STATION 945 LONGERON 14 LEFT. REMOVED AND REPLACED LEFT BRACKET. (M)Aug 14, 2000 · N502ME · Doug DC932SDR MWEA00689Flange · crackedMKE - RIGHT PYLON LEADING EDGE UPPER ATTACH FLANGE ON INBOARD UPPER SIDE HAS A CRACK APPROX 6 INCH AFT OF LEADING EDGE TIP. FABRICATED AND INSTALLED REPAIR ANGLE. (M)Aug 11, 2000 · N602ME · Doug DC932SDR EISA20000102Firewall · chafedDURING ROUTINE C-CHECK INSP, FOUND NR 1 ENGINE FIREWALL CHAFED AT FS 1257. FABRICATED REPAIR DOUBLER AND INSTALLED IAW 54-10-3, 51-10-3.Jul 24, 2000 · N311NE · Boeing 727223SDR RRXA11063Fastener · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO NR 2 ENGINE LEFT CORE COWL, FWD HINGE MOUNT 4EA FASTNERS, DAMAGE EXCEEDED LIMITATIONS IAW DC-10 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-21-01. RECEIVED PART AND INSTALLED 4EA FASTNERS IAW DC-10 SRMJul 6, 2000 · N68042 · Doug DC1010FSDR C2XA00IA254Frame · crackedDURING CONTINENTAL EXPRESS C-CHECK INSPECTION, NDI TESTING REVEALED A CRACK IN THE RIGHT NACELLE NR 1 FRAME. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAME, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jul 6, 2000 · N15713 · Emb EMB120RTSDR C2XA00IA253Frame · crackedDURING CONTINENTAL EXPRESS C-CHECK INSPECTION, NDI TESTING REVEALED A CRACK IN THE LEFT NAELLE NUMBER ONE FRAME. MAINTENANCE REMOVED AND REPLACED HE AFFECTED FRAME, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jul 6, 2000 · N15713 · Emb EMB120RTSDR COMA0010209Bulkhead · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LEFT NACELLE BULKHEAD SUPPORT AT FRAME 14 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #3712-1, IR, 6/24/00.Jun 28, 2000 · N259CA · Emb EMB120RTSDR MWEA00534Angle · crackedMKE - LEFT PYLON LEADING EDGE INBOARD UPPER ATTACH ANGLE IS CRACKED WHERE PYLON MEETS FUSELAGE. MAINTENANCE FABRICATED AND INSTALLED NEW ANGLE. (X)Jun 19, 2000 · N700ME · Doug DC914SDR UPS00433331Angle · crackedINSPECTION TYPE:C, 2 CRACKS CONFIRMED AND END OF CRACKS MARKED IN FRAME AT 12 O''CLOCK POSITION NAC STA 222 FWD OF BULKHEAD. REPAIR CARRIED OUT IAW QUERY NOTE 9/2000 AND SRM 54-14-03 FIG 13. TRIMMED OUT CRACKED FRAME FLANGE AND FABRICATE/ INSTALL FILLERS ANDJun 14, 2000 · N521UP · Boeing 747212BSDR AALA20000878Rib · corrodedTUL - RIB CORRODED ON BOTH SIDES LOWER OUTBOARD FAIRING BOLT HOLE. REMOVED AND REPLACED WITH NEW RIB, RIB 17A, RIGHT PYLON. (X)May 24, 2000 · N14061 · Airbus A300B4605RSDR 20000523SH022Beam · damagedLT AND RT ENGINE BEAMS (INBD AND OTBD) BUCKLING AND HEAT DAMAGE. GENERAL CORROSION BEHIND ENGINES. LT AND RT ENGINES CANTED BULKHEADS. CORROSION AND HEAT DAMAGE. LT AND RT WING LOWER SPAR CAPS, OVERSIZED HOLES WITH RIVNUTS INSTALLED. LT AND RT ENGINE NACMay 23, 2000 · N306 · Cessna 402BSDR AWXA0000304Panel · crackedC-CHECK, NR 2 ENG PYLON PLUME SUPPRESSION HAS 2 SMALL CRACKS IN AFT PANEL. REMOVED AND REPLACED PLUME PANEL IAW S/B 737-54-1034 (NEW PART).May 11, 2000 · N327AW · Boeing 7373Q8SDR MALA000320Cowling · chafedFOUND DURING C-CHECK, ENGINE COWL 453 DR-4TH RIB FROM AFT IS CHAFED. REFER CELSIUS TASK CARD 4532.May 9, 2000 · N407XJ · Saab 340BSDR MWEA00424Nut Plate · crackedRIGHT PYLON TRAILING EDGE ATTACH STRUCTURE IS CRACKED AT FORWARD INBOARD NUT PLATE ON TOP SIDE. FABRICATED AND INSTALLED NEW ANGLE.May 9, 2000 · N900ME · Doug DC915SDR MWEA00423Frame · chafedRIGHT PYLON HAS A CHAFED FRAME LOCATED AFT OF HYDRAULIC FLEX LINES. FABRICATED AND INSTALLED REPAIR DOUBLER.May 9, 2000 · N900ME · Doug DC915SDR C2XA00IA127Frame · crackedDURING CONTINENTAL EXPRESS C-CHECK, THE RIGHT NACELLE FRAME ONE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAME IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5410-01034, AND THE AIRCRAFT WAS APPROVED FOR REMay 8, 2000 · N16729 · Emb EMB120RTSDR F3LA00077Channel · damagedDURING C-7 CHECK INSPECTION, FOUND NR 2 ENGINE INBOARD COWL BOTTOM CHANNEL DAMAGED AT FORWARD END. MAINTENANCE REMOVED DAMAGED SECTION OF LOWER CHANNEL. FABRICATED REPLACEMENT CHANNEL AND REPAIRED PER SRM 51-30-02 AND 51-30-01. (M)May 6, 2000 · N270FL · Boeing 7372L9SDR CA000802022Frame · cracked(CAN). WHILE AIRCRAFT WAS AT SOGERMA FOR A C12 INSPECTION, EXTENSIVE CRACKING WAS FOUND ON BOTH NR 1 AND NR 2 PYLON LOWER SPAR CANTILEVER STRUCTURE.. MPD INSPECTION TASK WAS RAISED TO COVER THIS AREA Z1421-01-1. REPAIRED WERE CARRIED OUT I.A.W. SRM 54-52-11, FMay 3, 2000 · Airbus A310304SDR QXEA0001184Structure · damagedYYC- GOUGE MARKS ON RIGHT HAND NACELLE HORIZONTAL, BH AT INBOARD SIDE APPROX STATION XN240.0. REPAIRED IAW DHC-8 RD 8-54-1274 AND HORIZON AIR EA 9-54-244.Apr 27, 2000 · N829PH · Dhav DHC8102SDR C2XA00IA109Frame · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT ENIGNE LOWER COWLING WAS FOUND TO HAVE A CRACKED FRAME. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAME, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Apr 26, 2000 · N13958 · Emb EMB145SDR EIA2000150Angle · crackedHAECO-HKG - NR 3 PYLON UNDERWING SKIRT FAIRING OUTBOARD SKATE ANGLE FORWARD FASTENER HOLE FOUND CRACKED. NR 3 PYLON UNDERWING OUTBOARD SKATE ANGLE REPLAED PER SRM 51-10-01. (M)Apr 21, 2000 · N482EV · Boeing 747212BSDR EIA2000128Frame · crackedNR 1 PYLON HOSESHOE FRAME AT NAC STATION 221.9 CRACKED AT FORWARD LOWER AREA. CRACK APPROX .075 INCH ALONG THE RADIUS OF THE FRAME. TRIMMED OFF, REINFORCED AREA, AND COMPLETED REPAIR PER EO 54-747-1046-90. (M)Apr 21, 2000 · N482EV · Boeing 747212BSDR EIAA2000120Structure · crackedHAECO-HKG - NR 4 PYLON HORSESHOE FRAME UPPER HORIZONTAL ANGLE HAD CRACK AT LEFT NAC STA 221. REPLACED NR 4 PYLON HORSESHOE FRAME UPPER HORIZONTAL ANGLE PER SRM 51-10-01 AND SRM 51-30-02. (X)Apr 21, 2000 · N482EV · Boeing 747212B
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