JASC 5415
Service difficulty reports · 1,305
Reports filed under 5415 · Nacelle/Pylon, Attach Fittings, 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 = '5415' 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.
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 = '5415' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR AALA202202023390Sleeve · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON SPIGOT SLEEVE. REPLACED PYLON SPIGOT SLEEVE PER TASK CARD 26C42554031.SDR DALA2021111507023None · noneSHIP 3257 CORROSION BEARING OUTBOARD SIDE AFT POSITION AT AFT ATTACH FITTING ON RH PYLON. CORRECTIVE ACTION: REPLACED BEARING PER A320 AMM 54-51-17. (2015780)SDR DALA2021111507018None · noneSHIP 3266 LT PYLON SPIGOT FITTING BEARING HAS CORROSION AND IS FROZEN IN BEARING. CORRECTIVE ACTION: R/R LT PYLON SPIGOT FITTING IAW SRM 54-51-12. (2015375)SDR DALA2021111507017None · noneSHIP 3266 #2 PYLON SPIGOT BEARING CORRODED AND FROZEN IN RACE. CORRECTIVE ACTION: R/R LOWER SPIGOT FITTING IAW A320 SRM 54-51-12. JOB COMPLETE. (2015337)SDR YENA2021102000688Attach Fitting · corrodedDURING HEAVY MAINTENANCE, CORROSION: AFTER BUSHING REMOVAL - FOUND CORROSION AT HOUSING OF INBD/OUTBD AFT FITTING IN LH PYLON ; REF TOMX NR 00548: HOUSING OF INBD/OUTBD AFT FITTING IN LH PYLON WAS REPAIRED IAW ETI - 190-21-817 REV 6, ETD-2021-190-031064 REV B.SDR AALA202110115258Nut · looseAIRCRAFT IN BASE MAINTENANCE: LOOSE AFT ATTACH FITTING LUG PYLON TO WING UPPER ATTACHMENT NUT ON RIGHT PYLON. INSTALLED CORRECTLY NEW TAB WASHER AND NUT ATTACH FITTING LUG PYLON TO WING UPPER ATTACHMENT ON RIGHT PYLON PER AMM 54-51-17-400-002-A.SDR AALA202110082221Nut · looseAIRCRAFT IN BASE MAINTENANCE: LOOSE AFT ATTACH FITTING LUG PYLON TO WING UPPER ATTACHMENT NUT ON RIGHT PYLON. INSTALLED CORRECTLY NEW TAB WASHER AND NUT ATTACH FITTING LUG PYLON TO WING UPPER ATTACHMENT ON RIGHT PYLON PER AMM 54-51-17-400-002-A.SDR AALA202109244129Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION OF LOWER SPIGOT FITTING ON RH ENGINE PYLON BETWEEN RIB 4 AND RIB 5 AT UPPER SPAR, MEASURING L=13.0 IN, W=1.312 IN, D=0.009 IN. REPLACED FITTING WITH NEW IAW SRM 54-51-12-300-002 AND DRAWINGS R54612042 AND R54612043.SDR DALA2021092105647None · noneSHIP 668 #2 PYLON UPPER LINK ATTACH POINT ON PYLON HAS BOTH BUSHING WITH SOME FORM OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED #2 PYLON UPPER FWD SPAR FITTING, I/B AND O/B BUSHING IAW B757 SRM. (1953206)SDR AALA202109223432Spigot · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION MEASURING L=13.00 IN, W=1.3125 IN, D=0.010 IN, ON LEFT ENGINE PYLON LOWER SPIGOT FITTING LOCATED BETWEEN PYLON RIB 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-002.SDR IPXA2021090773641Shear Tie · damagedINSPECTION TYPE:N/A#2 PYLON AFT PYLON O/B SIDE SKIN ATTACHMENT LUG IS DAMAGEDREPAIRED AREA IAW EO A300-5450-81319-F AND COMPLETED INSTALLATION PER AIRBUS DWG R5460328SDR HYIA20210827001Fitting · crackedDURING NDT INSPECTION AS NOTED IN SID 57-10-16, A CRACK WAS DISCOVERED ON THE RIGHT HAND INBOARD NACELLE FITTING. (P/N: 5292029-22) THIS CRACK MEASURES APPROXIMATELY .123 INCHES LONG ON THE OUTBOARD LOWER LEG OF THE FITTING, AND IS CONSISTENT WITH OTHER CRACKSSDR SWAA2021082408890Strut · cracked#2 ENG AFT DTRUT FAIRING AFT BUCKHEAD INBD FITTING HAS 1' CRACK / REMOVE & REPLACE AFT STRUT AFT BULKHEAD WITH NEW UNIT SRM 51-40-02. REF SA-M 326 A1102208.SDR SWAA2021081104978Support Fitting · cracked#1 ENG PYLON AFT STRUT FAITING SUPPORT FITTING CRACKED INTO RADIUS CRACK VERIFIED WITH B737 NDT PART 6 51-00-00 PROC 23.COMPLIED WITH E.A 21-154-02194. PERFORM REPETITIVE INSPECTIONS EVERY 8 DAYS AND PERMANENT REPAIR WITHIN 60 DAYS PER EA 21-154-02194.PERFORM SDR SWAA2021081104977Support Fitting · cracked#2 ENGINE; AFT STRUT FAIRING SUPPORT FITTING CRACKED THROUGH RADIUS CRACK VERIFIED WITH B737 NDT PART 6 51-00-00 PROCEDURE 23.C/W EA 21-154-02194 PREFORM REPETITIVE INSPECTION EVERY 8 DAYS AND PERMANENT REPAIR IN 60 DAYS. PREFORM GVI ON END OF CRACK FOR ANY PRSDR SWAA2021080990181Fitting · damaged#1 ENGINE AFT O/B PYLON FITTING HAS DAMAGE FROM MAKING CONTACT WITH AFT UPPER METAL FIRE SEAL ON O/B T/R.(MARKED) ; / [01] REMOVED DAMAGE ON #1 ENGINE AFT O/B GSE BOOTSTRAP FITTING.MEASURING 1INCH DOWN FROM TOP OF STRUT BOX TO FORWARD O/B FLANGE EDGE OF FITTINSDR HYIA20210625001Fitting · crackedDURING NDT INSPECTION AS NOTED IN SID 57-10-16, A CRACK WAS DISCOVERED ON THE RIGHT SIDE OF THE RIGHT HAND OUTBOARD NACELLE FITTING. THIS CRACK MEASURES APPROXIMATELY .097 LONG AND IS CONSISTENT WITH OTHER CRACKS FOUND USING THE LIGHTED BORESCOPE INSPECTION TESDR FDEA202106171559Panel · crackedPFM E.O. NACELLES /PYLONS INSP FOUND NO.2 PYLON O/B SIDE PNL AT RIB 8 HAS CRACK ALONG FRONT SCREW HOLE IAW WORK CARD SEQ 000960 INSPECTION OF PYLON SIDE PANELS AT RIB 8 AIRBUS SBA300-54- 6015 R03 & A310-54-2018 R03 E.O. 6-5450-7-5003 H PT4 SUBSTEP A. THRUSDR SWAA2021051473017Attach Fitting · damaged#1 PYLON AFT O/B PRECOOLER ATTACH FITTING HAS DAMAGE TO THE BORE ; /SDR SWAA2021051473016Attach Fitting · damaged#1 PYLON AFT O/B PRECOOLER ATTACH FITTING HAS DAMAGE TO THE BORE ; /SDR REXA2021060200402Attach Bracket · crackedLH ENGINE LOWER AFT HINGE LINE FAIRING ATTACH BRACKET IS BROKE. - REMOVED BROKEN BRACKET FROM L/H ENGINE, LOWER AFT HINGE LINE FAIRING AND INSTALLED NEW IAW CRJ 700 SRM 51-42-21-001-001-A01 AND 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.SDR IPXA2021051269314Skin · crackedINSPECTION TYPE:C12CRACK DAMAGE WAS FOUND ON NO.1 PYLON OUTBD SKIN ASSEMBLY(P/N:311T2450-25) NEAR NAC STA 237.5PERFORM REPAIR I.A.W BOEING SR 4-5075409410 AND UPS EO B767-5430-80330-ASDR UIEA2021050101040Fastener · worn#2 ENG I/B NACELLE STRUT ACCESS PANELS FOR HYD RESERVOIR (SAILBOATS) HAVE SMOKING RIVETS AT LATCH POSITIONS ON I/B SIDE.(<DIV>REMOVED AND REPLACED LOOSE FASTENERS AT #2 ENG I/B NACELLE STRUT ACCESS PANEL PER B767-300 SRM 51-40-02-06-0.</DIV>)SDR FDEA202104170940Support · cracked#2 ENG PYLON, R/H SIDE JUST FWD OF BOAT TAIL, INNER FIRE SEAL ATTACH SKIRT PNL CRACKED AT AFT SECTION (MARK). REMOVED AND REPLACED APRON SUPPORT P/N AVB7050-42 AT NOTED LOCATION REF SRM 51-31-01 VOL 2.SDR HYIA20210407001Fitting · crackedDURING NDT INSPECTION AS NOTED IN SID 57-10-16, A CRACK WAS DISCOVERED ON THE LEFT HAND INBOARD NACELLE FITTING. (P/N: 5292029-21) THIS CRACK MEASURES APPROXIMATELY .095 INCHES LONG ON THE OUTBOARD LOWER LEG OF THE FITTING, AND IS CONSISTENT WITH OTHER CRACKS SDR IPXA2021042968771Attach Angle · crackedINSPECTION TYPE:A300FAIRING 475AL TE PANEL IB ATTACH FLANGE HAS (1) PREVIOUS WELD CACKED AT FASTENER HOLEREPAIRED IAW SREO A300-5450-21297SDR IPXA2021040867971Attach Angle · damagedINSPECTION TYPE:CROB ATTACH ANGLE ON #1 PYLON I/B OUTER SKIN TO USE ON AIRCRAFT N129UPREMOVED AND REPLACE IAW SRM 51-40-21SDR UIEA2021032900733Skate Angle · cracked#1 ENG PYLON PNL 437DB FWD ATTACH RH SIDE SKATE ANGLE ON BOTTOM OF WING HAS 5IN LENGTH CRACK.(<P>REMOVED DAMAGED SECTION OF SKATE ANGLE AND REPAIRED IAW FAS EA 21027 REV. IR</P>)SDR SIMA20210401001Fitting · crackedRIGHT ENGINE FORWARD LOWER YOKE-PYLON FORWARD LINKAGE FITTING IS CRACKED-C/A-REPAIRED IAW ERS-EM54MR-698.SDR DALA2021033001884Attach Fitting · not reportedSHIP 3254 REMOVE AND RE-INSTALL AFT ATTACH FITTING SLEEVE AND BOLT UPPER POSITION ON LH PYLON. CORRECTION ACTION:RE-INSTALLED PYLON TO WING AFT ATTACH-FITTING BOLT AND SLEEVE AS PER A320 FAM AMM 54-51-17. (1767755)SDR AALA202103299023Mount · wornAIRCRAFT WAS GROUNDED: #2 ENGINE PYLON BOTTOM SKIN MOUNTING PLATE BETWEEN RIB 7 AND RIB 8 HAS WORN ACCESS HOLE WHERE HYDAULIC LINES GO INTO THE PYLON DUE TO THE LINES CHAFFING THE MOUNTING PLATE. REPAIRED MOUNTING PLATE PER AARD 57-21-11-1.SDR DALA2021032501788Drag Fitting · damagedSHIP 692 LH ENG DRAG FTG CLAMP-UP AND DIAG BRACE BHEC INSP, HOLE #3 UNINSPECTABLE REF AMDS. CORRECTIVE ACTION: REF ERA 590601-14AD REV ORG FOR REPAIR. (1763639)SDR DALA2021032501785Structure · scratchedSHIP 692 SCRATCH NOTED IN HOLE #8 DURING VISUAL INSP. SECTION OF STEP 26 OF ORIGINATING TASK CARD REF. AMDS CARD. CORRECTIVE ACTION: REPAIRED PER ERA 590589-14AD ORG. (1763481)SDR SWIA2021071459466Attach Fitting · chafedRH ENGINE COUNTERBALANCE SPRING LOWER ATTACH STRUCTURE IN THE PYLON IS CHAFED/GOUGED (C-CHECK RO 7/10/2021) REMOVED RH ENGINE COUNTER BALANCE SPRING LOWER ATTACH BRACKET, REPAIRED BRACKET IAW REO 670-54-51-057 REV --, DATED 2021-04-17, AND REINSTALLED RSDR FDEA202102280514Attach Angle · cracked#1 PYLON, NAC STA 377, SUPPORT FRAME HAS CRACKED ATTACH CLIP REMOVED & REPLACED CLIP IAW BAC DWG 313T3380 REV FSDR AALA202103019006Plate · damagedAIRCRAFT IN BASE MAINTENANCE: LEFT WING PYLON LOWER SURFACE PLUMBING ACCESS MOUNTING PLATE HAS ELONGATED HOLES BETWEEN RIB 7 AND RIB 8. REPLACED MOUNTING PLATE PER SRM 57-21-11-300-005.SDR DALA2021022401079Attach Fitting · corrodedDURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON ATTACH FITTINGS OF UPPER LINK NAC STA.159.26 PYLON LT. LUG HOLE WAS REPAIRED AND BUSHING REPLACED PER SRM. (LP 1738192)SDR DALA2021022401078Lug · corrodedDURING INITIAL INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2. LUG HOLE REPAIRED AND BUSHING REPLACED PER SRM. (LP 173819)SDR HYIA20210222001Fitting · crackedDURING NDT INSPECTION AS NOTED IN SID 57-10-16, A CRACK WAS DISCOVERED ON THE LEFT HAND INBOARD NACELLE FITTING. (P/N: 5292029-21) THIS CRACK MEASURES APPROXIMATELY .145 INCHES LONG ON THE INBOARD LOWER LEG OF THE FITTING, AND IS CONSISTENT WITH OTHER CRACKS FSDR HYIA20210208001Fitting · crackedDURING MAINTENANCE A CRACK WAS IDENTIFIED ON THE INBOARD LEG OF THE RIGHT HAND INBOARD NACELLE FITTING, (P/N: 5292029-22) THIS CRACK MEASURES APPROXIMATELY .157 INCHES LONG AND WAS DISCOVERED USING THE LIGHTED BORESCOPE INSPECTION PROCEDURE AS OUTLINED IN TEXTSDR DALA2021020800719Bearing · corrodedDURING INSPECTION MAINTENANCE FOUND #1 PYLON UPPER LINK FWD INBOARD BEARING RACE SHOWS SIGNS OF CORROSION. UPPER LINK BEARING WAS REPLACED. (LP 1721886)SDR DALA2021020800718Bearing · corrodedDURING INSPECTION MAINTENANCE FOUND #1 PYLON UPPER LINK FWD OUTBD BEARING RACE WITH SIGNS OF CORROSION AND REPLACED. (LP1721883)SDR MK1Y01292021004Support Beam · wornFAN COWL SUPPORT BEAM LINK FOUND WITH WORN BUSHING (8 EA) AT FWD AND AFT ATTACHMENT POINTS.SDR SWAA2021031850916Fastener · crackedSEVERAL FASTENERS PULLING THROUGH ONE FASTENER CRACKED 6 O'CLOCK POSITION #2 ENGINE INLET / REPAIRED SEVERAL FASTENERS PULLING THROUGH AND ONE FASTENER CRACKED AT 6 O'CLOCK POSITION ON #2 ENGINE INLET PER SRM 54-10-01-1A-2 ALLOWABLE DAMAGE 2.SDR FDEA202101180148Attach Angle · crackedNR 1 PYLON AFT FIXED FAIRING FRAME AFT OF HYD BAY, AFT INBOARD SIDE CENTER ATTACH CLIP CRACKED. REMOVED DAMAGE CLIP, LOCATED, DRILLED AND INSTALLED NEW CLIP (P/N 313T3380-69), IAW B767 SRM 51-40-02 & BAC DWG 313T1380, REV C.SDR FDEA202101170143Attach Angle · crackedNR 2 PYLON AFT BULKHEAD TO AFT FAIRING INBOARD ATTACH CLIP IS CRACKED AT APPROXIMATELY NAC STA LT. REMOVED OLD CLIP AND INSTALLED NEW CLIP, IAW BAC DWG 313T2310 REV.SDR LR7A2021011402768Drag Fitting · corrodedDURING P4-LAS SCHEDULED C-3 CHECK WHILE PERFORMING SB 382-57-85 APPENDIX B INSPECTION, FOUND THE NR 2 ENGINE NACELLE INBOARD LOWER DRAG FITTING CORRODED. REPAIR BY REPLACEMENT ACCOMPLISHED, IAW LOCKHEED SMP583 SRM, CH 51-60 & 51-70 NR 1000348558.SDR LR7A2021011402759Drag Fitting · damagedDURING P4-LAS SCHEDULED C-3 CHECK WHILE PERFORMING SB 382-57-85 APPENDIX B INSPECTION, FOUND THE NR 3 ENGINE INBOARD LOWER NACELLE DRAG FITTING HOLES ARE DAMAGED. REPAIR BY REPLACEMENT ACCOMPLISHED, IAW LOCKHEED SMP583 SRM, CH 51-60 & 51-70 NR 1000322779.SDR IPXA2021020665384Attach Bracket · crackedINSPECTION TYPE: SEG FAIRING 485 ALIB ATTACH BRACKET FOR FORWARD RIB HAS CRACK AT LOWER PORTION. R & R FAIRING PER ACCESS 104 WORK CARD AND IPC 54-54-06-020.SDR SIMA20210105003Yoke · crackedDURING IMBV INSPECTION, QC FOUND RT PYLON FWD LOWER YOKE FITTING CRACKED. C/A: REMOVED AND REPLACED RT FWD LOWER YOKE FITTING, IAW ERS-EM-54MR-698.
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