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 VNAA0602008Cowling · damagedAFTER LANDING THE CREW REPORTED DAMAGE TO THE RIGHT ENGINE LOWER TRANSLATING COWL. MAINTENANCE REMOVED & REPLACED THE COWL WITH A SERVICEABLE UNIT. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.Feb 17, 2006 · N207PS · Cndair CL6002B19SDR P5CA0601447Lug · elongatedNR 3 ENGINE CORE COWLING - AFT HINGE SUPPORT ASSEMBLY - INTERIM REPAIR TO AFT LUG. REPAIRED PER BOEING 8100-9 DATED 03FEB2006.Feb 15, 2006 · N534MC · Boeing 7472F6BSDR MALA060073Structure · chafedRT NACELLE, INLET DECK IS CHAFED FROM THE INTAKE HARNESS. THE DAMAGE HAS BEEN REPAIRED IAW MESABA EOS54095.Feb 14, 2006 · N430XJ · Saab 340BSDR CA060221006Panel · crackedWHILE UN-COWLING, RT ENGINE MAINTEANCE FOUND A PIECE OF STAINLESS STEEL IN THE LOWER SECTION OF COWL. INVESTIGATION REVEALED A HOLE IN THE LT SIDE OF ASPIRATOR ASSEMBLY ABOVE THE OIL COOLER. THE ASPIRATOR WAS REPLACED AND AIRCRAFT SINCE RETURNED TO SERVICE. Feb 11, 2006 · Swrngn SA226TCSDR CALA0600044Structure · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 2 PYLON I/B AFT HORSE COLLAR AT LOWER NUT PLATE. THE AFT HORSE COLLAR WAS REMOVED AND REPLACED IAW SRM 51-10-2.Feb 9, 2006 · N14324 · Boeing 7373T0SDR UPS06146202Plate · chafedINSPECTION TYPE:5YR NR 2 ENG PYLON STRINGER FAIRING FWD UPPER OUTBD MOUNT STRAP HAS DEEP CHAFE. REMOVED AND REPLACED MOUNT STRAP A300 SRM 51-40-00.Feb 8, 2006 · N128UP · Airbus A300F4622RSDR UPS06146201Plate · chafedINSPECTION TYPE:5YR NR 2 ENG PYLON STRINGER FAIRING FWD UPPER MOUNT STRAP HAS DEEP CHAFE (INBD MOUNT STRIP). REMOVED AND REPLACED PER A300 SRM 51-40-00.Feb 8, 2006 · N128UP · Airbus A300F4622RSDR UPS06146200Plate · chafedINSPECTION TYPE:5YR NR 1 ENG PYLON STRINGER FAIRING FWD UPPER INBD MOUNTING STRIP HAS DEEP CHAFE. REMOVED AND REPLACED MOUNTING STRIP PER A300 SRM 51-40-00.Feb 8, 2006 · N128UP · Airbus A300F4622RSDR UPS06146199Plate · chafedINSPECTION TYPE:5YR NR 1 ENG PYLON STINGER FAIRING, FWD UPPER OUTBD MOUNTING STRIP HAS DEEP CHAFE. REMOVED AND REPLACED MOUNTING STRIP PER A300 SRM 51-40-00.Feb 8, 2006 · N128UP · Airbus A300F4622RSDR UPS06146185Angle · crackedINSPECTION TYPE:5YR, NR 1 ENGINE PYLON STRINGER FAIRING, CRACKED STIFFENER, OUTBOARD, AFT MOST. REMOVED AND REPLACED STIFFENER PER A300 SRM 51-40-00.Feb 8, 2006 · N128UP · Airbus A300F4622RSDR UPS06146184Angle · crackedINSPECTION TYPE:5YR, NR 1 ENGINE PYLON STRINGER, CRACKED STIFFENER, INBD, AFT MOST. REMOVED AND REPLACED STIFFENER PER A300 SRM 51-40-00.Feb 8, 2006 · N128UP · Airbus A300F4622RSDR 2006UALA00257Bushing · migratedNR 2 ENG PYLON INBOARD MIDSPAR FITTING OUTBOARD LUG BUSHING MIGRATED. NR 2 ENG PYLON INBD MIDSPAR FITTING OUTBD LUG BUSHING WAS FOUND MIGRATED. 4 EACH MIDSPAR BUSHINGS WERE FABRICATED PER SRM 54-53-90, REPAIR 3 & REPLACED PER GN-MM 01-0- 01-013.Feb 8, 2006 · N642UA · Boeing 767322SDR 06FDEA0595Door · wornNR 2 NACELLE DOORS DEEP WEAR ON FRAME LOWER RT SIDE AFT INLET DUCT STA 2200. TRIMED OUT DAMAGED TO FRAME FABRICATED AND INSTALLED REPAIR CHANNEL IAW SRM 54- 00-01 FIG 11 AND 54-10-00 FIG 14 VOL 1 FABRICATED PART IAW DETAIL PART TRAVELER F166598/N00598 AND Feb 8, 2006 · N68054 · Doug DC1010SDR UPS06146197Angle · crackedINSPECTION TYPE:5YR, NR 1 ENG STRINGER FAIRING, 2ND STIFFENER FWD FROM TRAILING EDGE, OUTBD SIDE IS CRACKED THROUGH RIVET AT BOTTOM END. REMOVED & REPLACED STIFFENER PER A300 SRM 51-40-00.Feb 7, 2006 · N138UP · Airbus A300F4622RSDR ARWA20060210Structure · crackedDURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 3 PYLON FOOT STOOL I/B SIDE WITH 1 - 3/4" CRACK. REMOVED AND REPLACED NR 3 PYLON FOOT STOOL FITTING IN ACCORDANCE WITH DC8 S/B AS7-99 REVISION 1 DATED 09/03/93 AND DC8 S/B AS7-87, REVISION NR 2, DATED 01Feb 3, 2006 · N784AL · Doug DC863FSDR UPS06146193Angle · crackedINSPECTION TYPE:5YR, NR 1 ENG AFT PYLON OTBD MEMBER SECTION ANGLE IS CRACKED AT JOGGLE. REMOVED AND REPLACED ANGLE PER A300 SRM 51-40-21.Feb 3, 2006 · N138UP · Airbus A300F4622RSDR UPS06146192Structure · crackedINSPECTION TYPE:5YR, NR 1 ENG AFT LOWER PYLON MEMBER SECTION IS CRACKED AT THRU HOLE FOR PNEUMATIC LINE. REMOVED AND REPLACED MEMBER SECTION PER A300 SRM 51-40-21.Feb 3, 2006 · N138UP · Airbus A300F4622RSDR CA060127001Door · separated(CAN) ON ARRIVAL TO BASE, THE DOOR FOR THE REFUEL PANEL WAS FOUND TO HAVE SEPARATED FROM THE NACELLE. THE HINGES, HINGE ATTACHMENT BOLTS AND SMALL FRAGMENTS OF THE COMPOSITE PANEL REMAINED ATTACHED. (TC NR 20060127001)Jan 27, 2006 · Dhav DHC8301SDR CALA0600030Stiffener · crackedINSPECTION FOUND A 4.25 INCH CRACK IN NR 1 PYLON I/B STIFFENER AT NAC STA 285. THE STIFFENER WAS REPLACED IAW ECRA 5420-01447.Jan 23, 2006 · N73152 · Boeing 767224SDR 2006UALA00103Fairing · damagedNR 1 ENGINE PYLON AFT FAIRINGS HAVE SUSTAINED HEAT DAMAGE TO LWR WEBS, STIFFENERS, CHORDS AND LWR PORTION OF THE FRAMES. NR 1 ENGINE PYLON AFT FAIRINGS HAVE SUSTAINED HEAT DAMAGE TO LWR WEBS, STIFFNERS, CORDS AND LWR PORTION OF THE FRAMES. INTERIM REPAIR WJan 20, 2006 · N795UA · Boeing 777222SDR USAA060041Repair · unknownFOUND NR 1 ENGINE NOSE COWL AT 4 O'CLOCK POSITION. UPDATED SDA AS REQUIRED IAW SRM 54-10-01, DEFECT SIZE: 5" BY 8".Jan 17, 2006 · N775AU · Boeing 7374B7SDR QXEA200600152Diaphragm · crackedPDX: FOUND NR 2 NACELLE OUTBOARD DIAPHRAGM CRACKED. MAINTENANCE REPAIRED IAW Q400 SRM 51-40-05 AND SRM TASK 51-42-05-330-801 AND 51-42-05-800-801.Jan 12, 2006 · N400QX · Bombdr DHC8402SDR UPS06446039Web · crackedINSPECTION TYPE:C NR 3 PYLON REAR MOUNT B/H FWD AND AFT OB FRAME WEB FOUND CRACKS. ( FWD FRAME .3125 INCH AND 1.375 INCHES ) ( AFT FRAME .1875 INCH AND 1INCH ) NR 3 PYLON REAR MOUNT B/H REPAIRED IAW HX RS NR R54-53-35416 AND UPS ENGINEERING FILE NR 747-54-20Jan 4, 2006 · N520UP · Boeing 747200SDR QXEA200600060Stiffener · crackedPDX - RIGHT HAND NACELLE, FINGERNAIL DECK LOWER SURFACE, OUTBOARD STIFFENER IS CRACKED 4" FROM FORWARD END. REPLACED IAW DASH8-200 SRM 51-40-11.Jan 3, 2006 · N379PH · Dhav DHC8202SDR UPS06445988Frame · crackedINSPECTION TYPE:C NR 4 PYLON I/B SIDE OF NAC STA 236 VERTICAL FRAME CRACKED, JUST FWD OF PYLON VALVE, CRACK LENGTH : 2.5". VERTICAL FRAME REPLACED AS PER SRM 51-10-01 P.9 AND INSTALLED AS PER SRM 51-30-02.Jan 1, 2006 · N520UP · Boeing 747212BSDR UPS06445987Frame · crackedINSPECTION TYPE:C NR 1 PYLON NAC STA236 I/B VERTICAL FRAME BOTTOM CRACKED, CRACK LENGTH 2.75". VERTICAL FRAME REPLACED AS PER SRM51-10-01 P.9 AND INSTALLED AS PER SRM 51-30-02.Jan 1, 2006 · N520UP · Boeing 747212BSDR UPS06146001Structure · crackedINSPECTION TYPE:5YR NR 2 ENG AFT LWR PYLON MEMBER SECTION IS CRACKED IN 2 EA PLACES RT AND LT AT JOGGLE. REMOVED AND REPLACED MEMBER SECTION IAW SRM 51-40-00.Dec 28, 2005 · N137UP · Airbus A300F4622RSDR UPS06146000Structure · cracked5YR N2 ENG AFT LWR PYLON MEMBER SECTION IS CRACKED IN 2 EA PLACES RT AND LT AT JOGGLE. REMOVED AND REPLACED RT AND LT MEMBER SECTIONS IAW SRM 51-40-00.Dec 28, 2005 · N137UP · Airbus A300F4622RSDR UPS06145995Angle · crackedNR 1 ENG AFT LWR PYLON MEMBER SECTION IS CRACKED 2 PLACES IB AND OB AT JOGGLE. REMOVED AND REPLACED IB AND OB MEMBER SECTION ANGLES IAW SRM 51-40-21 ON NR 882061.Dec 27, 2005 · N137UP · Airbus A300F4622RSDR UPS06145994Angle · crackedNR 1 AFT LWR PYLON MEMBER SECTION IS CRACKED 2 EA PLACES IB AND OB AT JOGGLE. REMOVED AND REPLACED IB AND OB MEMBER SECTION ANGLES IAW SRM 51-40-21 ON NR 882061.Dec 27, 2005 · N137UP · Airbus A300F4622RSDR UPS06145993Structure · crackedNR 1 ENG AFT LWR PYLON LWR SECTION IS CRACKED FWD, AFT THROUGH PRESS LINE MOUNT HOLE. REMOVED AND REPLACED MEMBER SECTION IAW SRM 51-40-21.Dec 27, 2005 · N137UP · Airbus A300F4622RSDR QXEA200501865Bracket · wornPDX - THE NACELLE FRAME BRACKET AND BUSHING FOR THE OPERATING MECHANISM FORWARD MAIN LANDING GEAR DOOR RIGHT NACELLE IS WORN. REPAIRED IAW DHC-8-200 SRM 51-20-26, PAGE 7, PARAGRAPH 5A-1-4.Dec 22, 2005 · N347PH · Dhav DHC8202SDR C1HA200593005Attach Angle · crackedWHILE PERFORMING AD 2005-19-24, FOUND NR 1 ENG PYLON CORD ANGLE CRACKED FWD PYLON FIREWALL P/N 69-16977-1. REMOVED CRACKED ATTACH ANGLE AND INSTALLED NEW ATTACH ANGLE 69-16977-1 REF BAC BWG 65-72772.Dec 22, 2005 · N293AS · Boeing 727212SDR ABXA060012Strap · crackedPYLON UPPER REAR SPAR STRAP BROKEN APART AT NR 2 PYLON. REMOVED AND REPLACED SPAR STRAP IAW SRM 51-30-1 AND 51-30-5.Dec 21, 2005 · N932AX · Doug DC933FSDR MALA050886Cowling · openCREW NOTED AFTER TAKEOFF, THE RT IB COWLING WAS UNLATCHED. AIR RETURN TO MEM. POST FLIGHT INSPECTION REVEALED DAMAGE TO COWLINGDec 18, 2005 · N428XJ · Saab 340BSDR IXXA05SMN283SFitting · crackedDURING ROUTINE C CHECK INSPECTION, NR 2 ENGINE COWL DOOR RAIL FITTING CRACKED 1, AT STA 254.324 (RT SIDE). REMOVED FASTENERS IAW DC8 SRM 51-3-0, DC8 SRM 51-1-21, DC8 SRM 51-1-21A. PERFORMED STOP HOLE, FABRICATED DOUBLER (17-4PH STAINLESS FLAT BAR) IAW ENG SHDec 16, 2005 · N722CX · Doug DC872SDR CALA0600012Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN NR 1 PYLON O/B FRAME CHORD DURING ATTACH CLIP REMOVAL AT UPPER CLIP ADJACENT AREA, NAC STA 285.45. THE FRAME CHORD WAS REPLACED IAW ECRA 5420-01444.Dec 16, 2005 · N76151 · Boeing 767224SDR CALA0600011Clip · crackedINSPECTION FOUND A 1.5 INCH CRACK IN NR 1 PYLON LT NACELLE STRUT FRAME CLIP AT NAC STA 285.45. THE FRAME CLIP WAS REPLACED IAW ECRA 5420-01444.Dec 16, 2005 · N76151 · Boeing 767224SDR C1HA200581019Attach Angle · crackedWHILE PERFORMING AD 2005-19-24, FOUND NR 1 ENG PYLON FIREWALL ATTACH ANGLE P/N 69-16977-1 CRACKED NEXT TO MOUNT FITTING. REMOVED AND INSTALLED ATTACH ANGLE P/N 69-16977-1 REF BOEING PRINT 65-72772.Dec 15, 2005 · N681CA · Boeing 7272S7SDR AMTA200501223Drag Strut · corrodedNR 1 PYLON DRAG STRUT AFT INBOARD LUG FOUND WITH CORROSION AS PER W/C 554I5406. CORROSION REMOVED AND FABRICATION OF BUSHING CARRIED OUT AS PER REPAIR CARD R056 AND EER 11664 LOG PAGE 756294 ALSO SEE MACH NR 5410/759, WO NR 288222 NRC 3083. (M)Dec 14, 2005 · N163AT · Lkheed 10113853SDR AU510002190Fairing · damagedNR 3 ENGINE LOWER RT COMPRESSOR FAIRING DAMAGED WITH A PIECE MISSING.Dec 12, 2005 · Boeing 747438SDR QXEA200501823Stiffener · damagedPDX: LT NACELLE FINGERNAIL SUPPORT DECK, UPPER SURFACE, OUTBOARD STIFFENER IS DAMAGED APPROX 40" FWD OF AFT END OF DECK. FRESH BLEND WITH CRACK. MAINTENANCE REPAIRED IAW HORIZON AIR EA 6-54-379 AND NDTM PART 6, 51-00-02.Dec 10, 2005 · N403QX · Bombdr DHC8402SDR ABXA050360Rib · crackedAFT UPPER SPAR STRAP ANGLE CRACKED JUST INBOARD OF AFT MOUNT. REMOVED AND REPLACED ANGLE WITH NEW ANGLE IAW DC9 SRM 51-30-05.Dec 9, 2005 · N972AX · Doug DC941SDR QXEA200501772Stiffener · damagedPDX: LT NACELLE FINGERNAIL SUPPORT DECK UPPER SURFACE OB STIFFENER IS DAMAGED APPROX 40" FWD OF AFT END OF DECK. MAINTENANCE PERFORMED A FRESH BLEND WITH CRACK MAPPED FOR ENGINEERING. COMPLIED WITH STEP 1 OF EA 6-54-379. HFEC BLENDED AREA IAW 1-84-7A, PT-6-Dec 9, 2005 · N403QX · Bombdr DHC8402SDR CALA0500428Frame · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 2 PYLON FRAME (HORSE COLLAR FITTING) AROUND LOCK FASTENER COLLAR. THE NR 2 PYLON HORSE COLLAR WAS REMOVED AND REPLACED IAW SRM 51-10-2.Dec 9, 2005 · N14308 · Boeing 7373T0SDR 2005UALA01423Bushing · migratedNR 2 PYLON DIAGONAL BRACE FITTING FWD-STRUT ATTACH, INBD SIDE BUSHING IS MIGRATED. NR 2 PYLON DIAGONAL BRACE FITTING FWD-STRUT ATTACH, INBD SIDE BUSHING WAS MIGRATED. BUSHING MIGRATION CAUSE IS UNKNOWN. THE BUSHING WERE REPLACED PER SRM 54-53-90.Dec 8, 2005 · N644UA · Boeing 767322SDR 2005UALA01422Bushing · migratedNR 1 PYLON OUTBD MIDSPAR FITTING OUTBD LUG, BUSHING IS MIGRATED. NR 1 PYLON OUTBD MIDSPAR FITTING OUTBD LUG, BUSHING WAS MIGRATED. THE BUSHING MIGRATION IS UNKNOWN. IT WAS REPLACED PER SRM 54-53-90.Dec 8, 2005 · N644UA · Boeing 767322SDR 2005UALA01421Bushing · migratedNR 1 PYLON INBD MIDSPAR FITTING, INBD AND OUTBD LUG BUSHINGS MIGRATED. NR 1 PYLON INBD MIDSPAR FITTING, INBD AND OUTBD LUG BUSHINGS WERE MIGRATED. CAUSE OF BUSHING MIGRATIONS IS UNKNOWN. BUSHINGS WERE REPLACED PER MM 54-53-90.Dec 8, 2005 · N644UA · Boeing 767322SDR ABXA050334Clip · crackedRIGHT FORWARD PYLON HAD A CRACKED ATTACH BRACKET INBOARD AND AFT SIDE RIGHT BUTT LINE 30 APPROXIMATELY AT FLOOR SURFACE. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-5.Dec 3, 2005 · N954AX · Doug DC941SDR 05FDEA03929Frame · crackedNR 1 ENG NOSE INLET COWL INTERIOR AFT BULKHEAD CHORD ANGLE IS CRACK AT 7 O`CLOCK POSITION CAN BE VIEWED FROM OUTBOARED SIDE. REMOVED AND REPAIRED CRACKED CHORD ANGLE IAW DC10 SRM 54-11-00, FIG 1C VOL 1. N/R # N00405, W/O NR 00030375.Nov 21, 2005 · N310FE · Doug DC1030
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