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 FDEA202012063046Frame Angle · crackedNR 2 PYLON UPPER RT PANEL SUPPORT IS CRACKED APPROXIMATELY STA 156. REPAIRED PER B757 SRM 54-51-71-2R AND 51-70-11-0G FIG 1.Dec 6, 2020 · N780FD · Boeing 757222SDR SWIA202055976Stiffener · missingL/H ENGINE UPPER TRANS COWL Z STIFFNER COMMON TO THE COAMING LATCH DOOR HAS 2EA MISSING FASTENER (C-CHECK) RO 2/5/2021 INSTALLED NEW L/H ENGINE UPPER TRANS COWL Z STIFFENER COMMON TO THE COAMING LATCH DOOR PN-CN624-2038-901. REF CRJ-700 SRM 51-42-13-001-00Dec 5, 2020 · N716EV · Cndair CL6002C10SDR SWIA202055974Coaming · chafedL/H ENGINE UPPER TRANS COWL LATCH COAMING HAS HEAVY CHAFFE AROUND HOLE LOCKING AREA (C-CHECK) RO 2/5/2021 REMOVED AND INSTALLED NEW L/H ENGINE UPPER TRANS COWL LATCH COAMING PN-CN624-2061-905. REF CRJ-700 SRM 51-42-13-001-001-A01, REO 670-54-21-1207 REV A Dec 5, 2020 · N716EV · Cndair CL6002C10SDR DALA2020120403972Bushing · corrodedDURING UPPER LINK REMOTION MAINTENANCE FOUND DISPLACED AND CORRODED BUSHING ON RT PYLON FITTING. FITTING REPLACED PER SRM.Dec 3, 2020 · N703TW · Boeing 7572Q8SDR DALA2020120403971Bushing · corrodedDURING INSPECTION MAINTENENANCE FOUND CORROSION LEVEL 2 BUSHINGS ON LT PYLON ATTACH FITTING.Dec 3, 2020 · N703TW · Boeing 7572Q8SDR SWIA202055973Landing · cracked*LEFT ENG LOWER TRANS COWL LATCH DOOR LANDING CRACKED. (MARKED) (C-CHECK) RO 2/5/2021 REMOVED AND INSTALLED NEW LATCH COAMING REF BOMBARDIER REO 670-54-21-1207 REV A, DATED 2015-08-27. / COMPLIED WITH 51-900-1002-SKYNov 30, 2020 · N716EV · Cndair CL6002C10SDR FDEA202011293053Frame · crackedNR 2 PYLON CENTER FITTING AT STA 329 INBOARD SIDE CRACKED. ACCOMPLISHED FRAME CRACK REPAIR AT NAC 329, IAW B767 SRM 54-52-71-2R.Nov 29, 2020 · N170FE · Boeing 7673S2FSDR JJBA20201125021Frame · corrodedRIGHT ENGINE, FORWARD FRAME AFT FLANGE TO COMPOSITE OUTER BYPASS DUCT HAS MULTIPLE LOCATIONS OF CORROSION AROUND CIRCUMFERENCE APPROXIMATELY 60 PERCENT OF THE CIRCUMFERENCE. UPON FURTHER EVALUATION THE LOCATIONS OF CORROSION FOUND ON RIGHT ENGINE, FORWARD FRANov 25, 2020 · N17138 · Emb EMB145XRSDR DALA2020112403858Acoustic Liner · delaminatedACOUSTIC LINING NR 2 ENGINE DELAMINATING REPAIRED, PER ERA 469315-14MA.Nov 23, 2020 · N840MH · Boeing 767432ERSDR IPXA2020112362720Fitting · corrodedINSPECTION TYPE: SEG 4 RT WING NR 2 PYLON DRAGLINK FITTING 653N0002-14 HAS CORROSION. REPLACED FITTING, PER EO B757-5720-69617-E.Nov 23, 2020 · N462UP · Boeing 75724APFSDR DALA2020112303818Spar · crackedDURING INSPECTION MAINTENANCE FOUND A CRACK ON PYLON STRUT LOWER SPAR WEB WIRING CUT OUT CORNER AT NSTA223 AND REPAIRED, PER ERA 588468-14.Nov 23, 2020 · N830MH · Boeing 767432ERSDR 2020F00447Door · delaminatedREPAIR OF RIGHT ENGINE UPPER COWL DOOR DAMAGE. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ27776M1 DATED NOV 10, 2020.Nov 16, 2020 · N359QS · Cessna 680ASDR AALA202011149003Beam · crackedAIRCRAFT IN BASE MAINTENANCE. NR 1 ENGINE PYLON AFT OUTBOARD BEAM HANGAR IS CRACKED. REPLACED NR 1 ENGINE PYLON AFT OUTBOARD BEAM HANGER, PER AMM 54-51-17-401.Nov 13, 2020 · N802AW · Airbus A319132SDR AALA202011149002Beam · crackedAIRCRAFT IN BASE MAINTENANCE. NR 1 ENGINE PYLON CENTER INBOARD BEAM HANGER IS CRACKED. REPLACED NR 1 ENGINE PYLON CENTER INBOARD HANGER BEAM, PER AMM 54-51-17.Nov 13, 2020 · N802AW · Airbus A319132SDR AALA202011149001Beam · crackedAIRCRAFT IN BASE MAINTENANCE. NR 1 ENGINE PYLON AFT BEAM HANGER IS CRACKED. REPLACED NR 1 ENGINE PYLON AFT INBOARD HANGER BEAM, PER AMM 54-51-17.Nov 13, 2020 · N802AW · Airbus A319132SDR HYIA20201116001Beam · crackedDURING MAINTENANCE A CRACK WAS DISCOVERED ON THE INBOARD FACE OF THE RIGHT HAND INBOARD ENGINE BEAM IN THE AREA OF THE VERTICAL ATTACH CHANNELS FOR THE CROSSOVER BEAM. THIS CRACK WAS DISCOVERED AFTER CHANGING THE CROSSOVER BEAM VERTICAL ATTACH BRACKET P/N: 56Nov 12, 2020 · N991AA · Cessna 402CSDR FDEA202011112827Beam · damagedNR 2 PYLON INBOARD LATCH BEAM MISSING NUTPLATE. REMOVED NR 2 PYLON INBOARD LATCH BEAM, IAW B767 SRM 54-52-71-2R. REPAIRED LATCH BEAM, IAW B767-SRM 54-52-71-2R. REINSTALLED NR 2 PYLON INBOARD LATCH BEAM, IAW B767 SRM 54-52-71-2R.Nov 11, 2020 · N130FE · Boeing 7673S2FSDR IPXA2020111062236Heat Shield · crackedINSPECTION TYPE: A300 NR 2 PYLON SHIELD ASSEMBLYY HAS FLANGE BENT AND CRACKED, AS MARKED. COMPLIED WITH EA 300-6741-27-A2517 & UPS EO A300-5740-78436-A.Nov 10, 2020 · N138UP · Airbus A300F4622RSDR IPXA2020112162628Fitting · gougedINSPECTION TYPE: 4C NR 3 ENGINE OUTBOARD FAN COWL FWD MOUNT FITTING IS GOUGED. REPAIRED GOUGED NR 3 ENGINE OUTBOARD FAN COWL FWD MOUNT FITTING, IAW VT-SAA EA 011-7110-01-A8699 REV IR AND UPS EO MD11-7110-78456-A. (MINOR)Nov 2, 2020 · N272UP · Doug MD11FSDR GTIA2020110235422Duct · chafedDURING INSPECTION PYLON NR 1 AIR DUCT BETWEEN RIB 8 & RIB 9 FOUND CLAMP ATTACHMENT CHAFING IN THE STRUCTURE SURFACE RAF 2551952-2 CREATED REF LTPR NRI 5001021057-0010. PERFORMED REPAIR AS PER EO 5452-2002 REV 00 AS PER AIRBUS RDAS REF 80844733/007/2020 ISSUENov 2, 2020 · N609NK · Airbus A320232SDR SWIA202055318Structure · damagedPAINT IS PEELING OFF ON ONE SPOT (POSSIBLE SCRATCH) ON THE RIGHT SIDE OF THE FUSELAGE (MID-SECTION, FORWARD OF THE LOWER PART OF THE ENGINE COWL). PAINT PEELING FROM RIGHT SIDE OF THE FUSELAGE IS WITHIN LIMITS, IAW CRJ 700 SRM 53-00-00. C-CHECK RO 1/6/2021.Oct 31, 2020 · N755SK · Cndair CL6002C10SDR SWIA202053835Beam · chafedCHAFE DAMAGE NOTED ON LT UPPER TRANSCOWL HINGE BEAM. C-CHECK RO 11/3/2020. REPAIRED CHAFE DAMAGE, REF MHIRJ REO. COMPLIED WITH SKYWEST TASK CARD.Oct 31, 2020 · N783SK · Cndair CL6002C10SDR SWIA202053834Beam · chafedCHAFE DAMAGE NOTED ON LT LOWER TRANSCOWL HINGE BEAM. C-CHECK RO 11/3/2020. REPAIRED CHAFE DAMAGE, REF MHIRJ REO. COMPLIED WITH SKYWEST TASK CARD.Oct 31, 2020 · N783SK · Cndair CL6002C10SDR SWAA2021071626530Rib · corrodedPANEL 424 #2 ENGINE OB COWL HAS CRACK AT ACCESS DOOR CUTOUT ON INTERIOR RIB SUPPORT AT LATCH SIDE / REMOVED CRACKED SHIELD AT # 2 ENG O/B COWL PNL 424 IAW SRM 51-40-02-0G-0 DRILLED NEW SHIELD IAW SRM 51-40-05-0G-0 AND CMM 71-13-30 INSTALLED NEW SHIELD IAW SRM Oct 28, 2020 · N8656B · Boeing 7378H4SDR IPXA2020111562401Tee Fitting · gougedINSPECTION TYPE: 2C NR 2 ENGINE LOWER AFT PYLON FAIRING FORMER TEE IS GOUGED. REPAIRED CRACKED FORMER TEE, IAW VT-SAA EA 011-5450-01-A8703 REV I/R AND UPS EO MDAA-5450-78510-A. (MINOR)Oct 27, 2020 · N287UP · Doug MD11FSDR FDEA202010272659Beam · wornNR 1 PYLON AFT FAIRING, OUTBOARD LATCH BEAM FWD NUTPLATE LOOSE. REPAIRED NR 1 PYLON OUTBOARD LATCH BEAM, IAW B767 SRM 54-52-71-2R AND BOEING DWG 313T2380 REV E.Oct 27, 2020 · N168FE · Boeing 7673S2FSDR FDEA202010262656Beam · wornNR 2 PYLON INBOARD LATCH BEAM FWD NUTPLATE IS MISSING REPAIR NR 2 INBOARD PYLON LATCH BEAM, PER B767 SRM 54-52-71-2R B DWG 313T2380 REV E, B.Oct 26, 2020 · N168FE · Boeing 7673S2FSDR FDEA202010262655Beam · wornNR 2 PYLON OUTBOARD LATCH BEAM FWD NUTPLATE IS MISSING REPAIRED NR 2 OUTBOARD PYLON LATCHBEAM, IAW B767 SRM 54-52-71-2R BOEING DWG 313T2380 REV E AND 313T2380 REV B.Oct 26, 2020 · N168FE · Boeing 7673S2FSDR FDEA202010242640Shear Tie · crackedNR 1 PYLON AFT BULKHEAD TO AFT FAIRING INBOARD ATTACH CLIP CRACKED AT NAC STA 298 RT. REMOVED AND REPLACED SHEAR TIE, PER B767 SRM 51-40-02 & BOEING DWG 313T2310 REV B.Oct 24, 2020 · N168FE · Boeing 7673S2FSDR FDEA202010232606Spar · crackedCRACK INDICATION FOUND APPROXIMATELY 0.25" IN LENGTH DURING ULTRASONIC INSPECTION AT RIGHT HAND SIDE UPPER SPAR ASSEMBLY (TAIL PYLON) STATION YID 408.500 ON THE VERTICAL FLANGE OF THE UPPER CAP. CRACK AREA AT RIGHT HAND SIDE UPPER SPAR ASSEMBLY (TAIL PYLON) SOct 23, 2020 · N591FE · Doug MD11FSDR TAMF20201022003Nose Cowl · dentedDURING WALK AROUND WERE FOUND TWO DENTS ON ENGINE 1 INLET COWL 6 O´CLOCK POSITION. ACTION TAKEN: IN ACCORDANCE WITH AMM 71-61-41-04 CONF 22 THE COWL-AIR INTAKE WAS REPLACED.Oct 20, 2020 · N335QT · Airbus A330243FSDR FDEA202010192561Shear Tie · crackedNR 2 PYLON INBOARD WING FITTING CLIP IS CRACKED ON FWD END. REMOVED AND REPLACED SHEAR TIE P/N 313T3310-1156, IAW BAC DWG 313T2310 REV AND B767 SRM 51-40-02.Oct 19, 2020 · N147FE · Boeing 7673S2FSDR FDEA202010162530Structure · delaminatedNR 1 ENGINE INBOARD FAN COWL HAS LARGE AREA OF EXPOSED COMPOSITE MATERIAL. REMOVED AND REPLACED INBOARD FAN COWL, IAW B757 AMM 7-1-11-04-4.Oct 16, 2020 · N798FD · Boeing 757222SDR FDEA202010102523Door Frame · gougedNR 2 ENGINE LT SIDE, APPROXIMATELY STA YTN 133, 6 O`CLOCK POSITION, GOUGED METAL ON FWD LT FAN COWL LAND. MARKED DOT NR 45. REMOVED GOUGED DOOR JAM & REPLACED WITH FABRICATED DOOR JAM, REF SRM 51-31-01, DWG AJC 7415.Oct 10, 2020 · N562FE · Doug MD1010FSDR 17LR20201009001Support Web · crackedONCE AGAIN IN SEPTEMBER 2017 ALPHA AIRCRAFT REPAIR STATION INDUCTED WHAT WE THOUGHT WAS A SPECIAL HARD LANDING INSPECTION PER OPERATOR WORKSCOPE AND AS WE WERE GAINING ACCESS TO BOTH LT AND RT ENGINE NACELLES TO WING ATTACH AREAS AND KEELSON WEBS FOR LOWER RIBOct 9, 2020 · Swrngn SA227*SDR V0XD20200610007Shield · gougedRT LOWER COWLING HAS TWO GOUGES OUT OF LIMITS IN THE FIRE SHIELD. CORRECTIVE ACTION TO BE ACCOMPLISHED ON AVMAX W/O: 80889 W/C: 4082.Oct 6, 2020 · N921FJ · Cndair CL6002D24SDR ASMF202101002Acoustic Panel · damagedDURING TRANSIT CHECK, IT WAS DETECTED A SEVERAL SCRATCHES ON LEFT ENGINE INNER BARREL ACOUSTIC PANEL INLET COWL. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A SEVERAL SCRATCHES OF 2.00 LENGTH AT 6 HRS AND 5:30 HRS POSITION WITH 4.5 AND 3.0 FROM THE Oct 4, 2020 · N368AR · Boeing 73786JSDR DALA2021012200455Cover · missingTHE INBOARD COWL HOIST COVER IS MISSING ON LEFT ENGINE. CONTRACT MAINTENANCE FORWARDED THE DISCREPANCY TO NEF 71- 10-02. COWL HOIST SCREW COULD NOT BE INSTALLED, PER AIPC 71-11-05-10 ITEM 95. OK TO CONTINUE. ATL 22JAN21 THE NR 1 ENGINE WAS CHANGED WITH A NOct 3, 2020 · N896AT · Boeing 717200SDR ASMF202011015Acoustic Panel · damagedDURING TRANSIT CHECK, IT WAS DETECTED SEVERAL NICKS ON RIGHT ENGINE INNER BARREL ACOUSTIC PANEL. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A NICK OF 0.187 LENGTH, 0.046 WIDTH FROM 2.5" DISTANCE OF AFTER EDGE OF INNER BARREL ACOUSTIC PANEL AT 12 HROct 1, 2020 · N997AM · Boeing 73776QSDR ASMF202011014Acoustic Panel · damagedDURING TRANSIT CHECK, IT WAS DETECTED A SEVERAL NICKS ON RIGHT ENGINE INNER BARREL ACOUSTIC PANEL INLET COWL. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING SEVERAL NICKS AL 2:30 HRS, 8 HRS AND 9:30 HRS POSITION. THE WO´S 7058591 AND 7058631 WERE ISSUOct 1, 2020 · N368AR · Boeing 73786JSDR IPXA2020101361261Rib · damagedINSPECTION TYPE: 2C NR 1 PYLON FAIRING 439AL FWD RIB IS DAMAGED. REMOVED AND REPLACED DAMAGED NR 1 PYLON FAIRING 439AL FWD RIB, IAW MD-11 SRM 51-35-01 (MINOR).Oct 1, 2020 · N258UP · Doug MD11FSDR DALA2020100503274Spar · crackedDURING C CHECK THE NR 2 PYLON MID SPAR WEB WAS FOUND CRACKED ON THE INBOARD SIDE AT NAC STA 290 ALONG WITH THE CLOSEOUT C/W ERA 575999-14.Oct 1, 2020 · N841MH · Boeing 767432ERSDR DALA2020100103230Flange · crackedDURING INSPECTION FOUND NR 1 PYLON STRUT UPPER SPAR HORIZONTAL FLANGE RT SIDE ED CRACKED AT N STA 230. REPAIRED, PER ERA 587940-14.Oct 1, 2020 · N829MH · Boeing 767432ERSDR DALA2020100103229Flange · crackedDURING INSPECTION FOUND NR 2 PLYLON INBOARD HORIZONTAL FLANGE CRAKED AT NAC STA 230. REPAIRED, PER ERA 587941-14.Oct 1, 2020 · N829MH · Boeing 767432ERSDR ASMF202011013Acoustic Panel · dentedDURING OVERNIGHT CHECK AT MEX STATION, IT WAS DETECTED A SEVERAL DENTS AND A NICK ON LEFT ENGINE INNER BARREL ACOUSTIC PANEL INLET COWL. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A SEVERAL DENTS WITH 2.875" AND 1.500"OF SEPARATION; A DENT OF 0.500Sep 30, 2020 · N342AM · Boeing 7378Z9SDR ASMF202011012Acoustic Panel · damagedDURING OVERNIGHT CHECK AT MEX STATION, IT WAS DETECTED SEVERAL DENTS AND A NICK ON BOTH ENGINES INNER BARREL ACOUSTIC PANEL INLET COWL. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A DENT OF 0.0110" DEPTH, 1.000" WIDTH, A DENT OF 0.0012" DEPTH, 0.125Sep 29, 2020 · N997AM · Boeing 73776QSDR ASMF202011241011Acoustic Panel · damagedDURING OVERNIGHT CHECK AT MEX STATION, IT WAS DETECTED A SEVERAL DENTS AND NICKS ON BOTH ENGINES INNER BARREL ACOUSTIC PANEL INLET COWL. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A DENT OF 0.001" DEPTH AND 0.187" WIDTH; A DENT OF 0.002" DEPTH AND Sep 29, 2020 · N788XA · Boeing 737752SDR ASMF202011010Acoustic Panel · dentedDURING TRANSIT CHECK, IT WAS DETECTED SEVERAL NICKS, DENTS AND GOUGE ON BOTH ENGINES INNER BARREL ACOUSTIC PANEL. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING SEVERAL NICKS ON BOTH ENGINE INNER BARREL ACOUSTIC PANEL OF 0.093 LENGTH, OF 0.187" LENGTH Sep 27, 2020 · N368AR · Boeing 73786JSDR ASMF202011009Acoustic Panel · dentedDURING TRANSIT CHECK, IT WAS DETECTED A SEVERAL DENTS ON LEFT ENGINE INNER BARREL ACOUSTIC PANEL INLET COWL. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A DENT OF 0.281" WIDTH AND 0.013" DEPTH, TWO DENTS OF 0.500" WIDTH AND 0.006" DEPTH, A DENT OF 0Sep 27, 2020 · N950AM · Boeing 737852SDR UIEA2020092802102Fitting · gougedNR 2 PYLON INBOARD SIDE LOAD FITTING IS GOUGED BEHIND PANEL 447. BLENDED GOUGE ON NR 2 PANEL INBOARD REPAIRED, IAW DOC 47416 REA 03.Sep 25, 2020 · N658GT · Boeing 767281
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