JASC 5414
Service difficulty reports · 4,361
Reports filed under 5414 · Nacelle/Pylon, Plate/Skin, 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 = '5414' 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 = '5414' 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 KCSA081340Skin · crackedINBOARD SIDE OF NR 3 PYLON EXTERIOR SKIN CRACKED .500 IN NAC STA 176 FROM EDGE OF SKIN EXTENDING UNDER PREVIOUS REPAIR DOUBLER. (A)SDR 08FDEA03029Skin · chafedNR 1 PYLON PANEL 437 LL IS CHAFED AT THE FASTENER HOLES. BLENDED AREA IAW DC/MD-10 SRM 54-00-01, VOL I, FIG 1-A. ORIGINAL MATERIAL THICKNESS 0.071 IAW DC/MD-10 SRM 54-51-0 AND FOUND TO BE OUT OF LIMITS 54-00-01, VOL I, FIG 1-A. UT GAUGE USED IS T8225P. MASDR 08FDEA03021Panel · chafedNR 3 PYLON PANEL 488 AL IS CHAFED. FABRICATED DOUBLER AND FILLER IAW SRM 51-21-01;VOL II; FIG 2-B. ALODINED AND PRIMED FILLERS IAW SRM 51-21-01; VOL II. INSTALLED REPAIR PARTS IAW SRM 54-00-01; VOL I; FIG 2-B AND EA 8-5480-123601.SDR 08FDEA03020Panel · chafedNR 1 PYLON PANEL 438 OL IS CHAFED IN 2 PLACES. FABRICATED DOUBLER AND FILLER IAW SRM 51-21-01; VOL II; FIG 2-B. ALODINED AND PRIMED FILLERS IAW SRM 51-21-01; VOL II. INSTALLED REPAIR PARTS IAW SRM 54-00-01; VOL I; FIG 2-B AND EA 8-5480-123601.SDR 08FDEA03022Panel · chafedNR 1 PYLON PANEL 437 FR IS CHAFED AT FASTENER HOLES. NR 1 PYLON PANEL 437 FR WAS CHAFED BEYOND ALLOWABLE LIMITS REQUIRED SRM REPAIR IAW DC/MD-10 SRM 54-00-01, VOL I. MATERIAL ID FOR SRM REPAIR 2024-T3, 0.071, PO 614899.4 IAW DC/MD-10 SRM 54-51-02, VOL III. SDR DALA1102935534Skin · crackedEA 55-212961 SECTION I ISSUED FOR NR2 PYLON, RT SIDE SKIN CRACK AT NAC STA 132. FOLLOW ON ACTION IS REQUIRED. COMPLIED WITH ER/A 488115-14 REV ORIGINAL PERMENANT REPAIR ACCOMPLISHED COMPLETED.SDR USAA920081414Skin Panel · crackedCLT -MAJOR REPAIR- Q3 CHECK- CRACKED NR 1 PYLON SKIN PANEL, NAC 189,50. REPAIRED NR 1 PYLON SKIN PANEL AT NAC 189.50 IAW US AIRWAYS TYPICAL REPAIR 54-30-07. (A)SDR F3LA200800490Skin · dentedDURING C-CHECK INSP NOTED THAT THE DAMAGE ON NR 1 ENGINE INLET COWL REQUIRES PERMANENT REPAIR OF DENT AT THE 2 O`CLOCK POSITION. MAINT REPAIRED DAMAGED AREA IAW CMM 54-10-00, REPAIR PROCEDURE NR 23. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCESDR UPS08652866Skin · crackedNR 2 PYLON LT MOST FWD PYLON STRUT ACCESS CUTOUT CRACKED AT AFT UPPER CORNER (CRACK LENGTH 1" APPROX). NR2 PYLON LT MOST FWD PYLON STRUT ACCESS CUTOUT AFT UPPER CORNER SKIN REPAIRED IAW HX RS NR R54-51-36029 AND UPS EO NR B767-5430- 30063-A.SDR KCSA081321Skin · damagedNR 2 PYLON INBOARD NAC STA-220 SKIN DAMAGED. (A)SDR KCSA081320Skin · chafedNR 2 PYLON INBOARD SKIRT CHAFED THROUGH RUB STRIP AT NAC STA-220. (A)SDR KCSA081316Skin · crackedNR 3 PYLON LT SKIN AT NAC STA-208 HAS TWO CRACKS BELOW DOUBLER. (A)SDR 08FDEA02810Skin · corrodedSURFACE CORROSION FOUND ON PYLON NUMBER TWO LEFT SIDE INNER SKIN FORWARD OF ACCESS PANEL 443LL, PPS 126 TO PPS 181. EVALUATE AND RECTIFY. REPLACED LEFT SIDE INNER SKIN FORWARD OF ACCESS PANEL 443LL OF PYLON NUMBER TWO IN ACCORDANCE WITH BOEING DRAWING 311SDR 08FDEA02809Skin · corrodedSURFACE CORROSION FOUND ON PYLON NUMBER ONE LEFT SIDE INNER SKIN AFT OF ACCESS PANEL 433CL. EVALUATE AND RECTIFY. REPLACED LEFT SIDE INNER SKIN AFT OF ACCESS PANEL 433CL OF PYLON NUMBER ONE IN ACCORDANCE WITH BOEING DRAWING 311N5046, BOEING DRAWING 311N5002,SDR 2010F00085Skin · damaged(KADY) AN ENLARGED HOLE WAS FUND ON THE OTBD SKIN AT NAC STA 286.50.SDR UPS08552837Skin · corrodedINSPECTION TYPE-C, CORROSION ON LWR STRUT OF THE NR1 ENGINE CNA 6 O'CLOCK POSITION PPS206. REPLACED SKIN OF LWR STRUT SKIN MATERIAL THICKNESS OUT OF LIMITS.SDR 2010FA0000355Skin · corroded(KADY) CORROSION AT NR 1 PYLON OTBD CAP SKIN. MINOR REPAIR ACCOMPLISHED BY BLEND OUT THE CORROSION AND APPLY FINISH TREATMENT.SDR 2010F00083Skin · corroded(KADY) CORROSION AT NR 4 PYLON OTBD CAP SKIN. MINOR REPAIR ACCOMPLISHED BY BLEND OUT THE CORROSION AND APPLY FINISH TREATMENT.SDR 2010F00084Skin · cracked(KADY) CRACK WAS FOUND NR 3 PYLON INBD SKIN.SDR 2008UALA03619Skin · crackedNR 1 PYLON STRUT I/B SIDE STRUT ACCESS HOLE FOR PANEL 416BR AFT UPPER CORNER SKIN IS CRACKED. STOP DRILLED CRACK. FABRICATED & INSTALLED 2EA DOUBLERS. HFEC INSP, NO CRACK PAST STOP DRILL.SDR 08FDEA02397Panel · crackedFOUND CRACK ON PYLON NR 2 RIB 8A SIDE PANELS INBOARD/OUTBOARD SIDE DOUBLER REPAIR PERFORMED IAW SRM 54-51-31 PB201.SDR 08FDEA02354Panel · corrodedPYLON NUMBER TWO RIGHT SIDE STRUT SKIN CUTOUT AT ACCESS PANEL 443AR FOUND CORROSION, FROM PPS100 TO PPS126. EVALUATE AND RECTIFY. REPLACED PYLON NUMBER TWO STRUT SKIN CUTOUT PANEL 443AR IN ACCORDANCE WITH BOEING DRAWING 311N5002 ID0014, SRM 51-10-02 REV SDR 08FDEA02353Panel · corrodedPYLON NUMBER ONE RIGHT SIDE SKIN CUTOUT AT ACCESS PANEL 433GR FOUND CORROSION, FROM PPS 100 TO PPS 120. EVALUATE AND RECTIFY. REPLACED PYLON NUMBER ONE SKIN CUTOUT PANEL 433GR IN ACCORDANCE WITH BOEING DRAWING 311N5002 AND SRM 51-10-02 REV 93.SDR FDEA200806172288Skin · corrodedSTRUT NR 2 INBD SIDE OF SKIN AT APPROX PPS 200.50 HAS EXFLOIATED CORROSION (APPEARS TO BE TRAVELING UNDER FRAME/CORD ALSO). REMOVED SKIN IAW SRM 51-40-02. REMOVED CORROSION AT STA 157, ORIGINAL MATERIAL THICKNESS .090", REMAINING THICKNESS .062", OUT OF LIMITSDR 08FDEA02288Skin · corrodedSTRUT NR 2 INBOARD SIDE OF SKIN AT APPROX PPS 200.50 HAS EXFOLIATED CORROSION (APPEARS TO BE TRAVELING UNDER FRAME/CORD ALSO). REMOVED SKIN IAW SRM 51-40-02. REMOVED CORROSION AT STA 157, ORIGINAL MATERIAL THICKNESS .090 INCH, REMAINING THICKNESS .062 INCH, SDR 08FDEA02207Panel · chafedON THE NR 2 ENGINE ABOUT 7 O'CLOCK POSITION THE COWL RING COVERING THE NR 2 ENGINE ADAPTER RING IS CHAFED BY THE LEFT FAN COWL. REMOVED COWL RING PANEL FROM THE NR 2 ENGINE IAW DC/MD-10 SRM 51-31-01; VOL II. MATERIAL ID FOR THE NEW PANEL IS CLAD 2024-T6, 0.0SDR 08FDEA02189Panel · crackedNR 3 PYLON PANEL 487 FL IS CHAFFED IN THE INNER SURFACE. BLENDED AREA AND FOUND A CRACK ON THE OUTBD ATTACH FLANGE. BLENDED THE AREA AND FOUND A CRACK ON THE ATTACH FLANGE. ORIGINAL MATERIAL THICKNESS 0.071 IAW DC/MD-10 SRM 54-51-01; VOL III. MATERIAL REMASDR 08FDEA02164Panel · chafedNR 3 PYLON PANEL 488 GL IS CHAFED ON THE INNER SKIN.SDR 08FDEA02140Panel · chafedNR 1 PYLON PANEL 438 GL HOLE IS CHAFED. FABRICATED A NEW AUB 7036-27 SKIN IN REF TO FEDEX EA 8-5480-116987 AND REASSEMBLED THE PANEL IN REF TO FEDEX EA 8-5480-116987 "NACELLES/PYLONS - NR 1 PYLON AFT "V" FAIRING PANEL DAMAGED - REPAIR".SDR 08FDEA02094Panel · chafedNR 3 PYLON PANEL NR 487 HR IS CHAFED AT THE INNER SURFACE. BLENDED CHAFED AREA AND FOUND TO BE OUT OF LIMITS REF DC/MD-10 SRM 54-00-01; VOL I. FABRICATED A NEW PANEL REF DAC DWG NR AUB7108; REV J. ALODINED AND PRIMED REF DC/MD-10 SRM 51-21-01; VOL II. INSSDR KCSA081270Skin · crackedNR 4 PYLON I/B SKIN CRACKED AT FWD LOWER ACCESS PANEL CUTOUT.SDR DL76L080795Skin · crackedNR 2 PYLON I/B SIDE TRAPEZOIDAL CUTOUT UPPER FWD CORNER PYLON SKIN HAS CRACK. REPAIRED I/B STRUT SIDE SKIN AT AFT TRAPEZOIDAL ACCESS DOOR NR 2 PYLON PER SRM 54-53-01 REPAIR 7 FIG 201 SHTS 1-4.SDR DL757080782Fitting · damagedDURING HMV AT SAA, A HOLE WAS MISDRILLED COMMON TO THE NR 2 PYLON MIDSPAR FITTING, WEB, CHORD AND DOUBLER. THE HOLE WAS REAMED, BUSHED, AND REDRILLED PER BOEING INSTRUCTIONS.SDR 08FDEA01978Skin Panel · corrodedCORROSION ON PYLON NUMBER ONE LT INNER STRUT SKIN NEAR ACCESS PANEL 433BL CUTOUT, PPS 124.76. EVALUATE AND RECTIFY. REPLACED PYLON NUMBER ONE LT INNER STRUT SKIN NEAR ACCESS PANEL 433BL CUTOUT IN ACCORDANCE WITH BOEING DRAWING 311N5002 ID 0013 REVISION E, 31SDR 08FDEA01977Skin Panel · corrodedSURFACE CORROSION ON PYLON NUMBER TWO LEFT SIDE PANEL INNER SKIN FORWARD OF ACCESS PANEL 443HL, PPS 124 TO PPS 200. EVALUATE AND RECTIFY. PYLON NUMBER TWO LEFT SIDE SKIN PANEL LOCATED FORWARD OF ACCESS PANEL 443HL REPLACED IN ACCORDANCE WITH BOEING DRAWSDR 08FDEA01976Skin · corrodedCORROSION FOUND ON PYLON NUMBER ONE INNER STRUT SKIN NEAR ACCESS PANEL 433JR CUTOUT, PPS 162.8. EVALUATE AND RECTIFY. PYLON NUMBER ONE RIGHT SIDE PANEL SKIN NEAR ACCESS PANEL 433JR CUTOUT REPLACED IN ACCORDANCE WITH BOEING DRAWING 311N5002 ID 0014 REVISION ESDR NWAA082625649Skin · crackedDURING "M" CHECK FOUND CRACKS IN NR 2 PYLON RT SKIN AT NAC STA 132. REPAIRED PER EA 56-212996 SECT 1. SECTION 2 REQUIRES FOLLOW UP INSPECTION BY 19 MAY 09. (A)SDR 08FDEA01826Panel · chafedNR 2 PYLON AFT LOWER FAIRING PANEL 485 AL; FWD UPPER RT ATTACH PLATE IS CHAFED ON THE INNER SURFACE. REMOVED ATTACH PLATE & INSTALLED A NEW ATTACH PLATE PER SRM 51-40-21 PARA 6. LOCATED & DRILLED HOLES PER SRM 51-40-21 PARA 6. ALODINED PER SRM 51-21-10. PSDR 08FDEA01821Skin · corrodedPYLON NUMBER TWO INNER SKIN OF ACCESS PANEL 443BR FOUND WITH SURFACE CORROSION, FROM PPS 126 TO PPS 151. EVALUATE AND RECTIFY. PYLON NUMBER TWO INNER SKIN OF ACCESS PANEL 443BR, REPAIRED BY AERO MECHANICAL INDUSTRIES INC. (AMII) IN ACCORDANCE WITH EA NR FSDR 08FDEA01819Skin Panel · corrodedPYLON NUMBER TWO LEFT FORWARD STRUT SKIN CUT OUT AT ACCESS PANEL 443GL FOUND CORROSION, FROM PPS 100 TO PPS 126. EVALUATE AND RECTIFY. REPLACED PYLON NUMBER TWO STRUT SKIN CUT OUT PANEL 443GL IN ACCORDANCE WITH BOEING DRAWING 311N5002 AND SRM 51-10-02 RESDR 08FDEA01800Panel · chafedNR 1 PYLON PANEL 437 EL IS CHAFED AT THE HINGE AND THE HINGE IS WORN. REMOVED AND REPLACED P/N AUB7038-37 HINGE ASSY AUB7038-39 HINGE IAW DC10/MD 10 SRM 51-35-01 VOL II; BLENDED AREA IAW DC/MD10 SRM 54-00-01 VOL I; FOUND TO BE OUT OF ALLOWABLE LIMITS IAW DC/MSDR 08FDEA01793Panel · chafedNR 1 PYLON PANEL NR 414 ER HAS CHAFING ON THE MATING SURFACE. REPAIRED THE IAW SRM 54-52-51, FIG 203.SDR 08FDEA01780Panel · damagedNR 1 PYLON PANEL 483 GL HAS 1 FASTENER HOLE WALLOWED OUT. ANNEALED TITANIUM IAW E.A. 8-5480-116981. FORMED & FABBED IAW DWG AUB 7036. REMOVED & INSTALLED DRAIN TUBE IAW E.A. 8-5480-116981. INSTALLED IAW SRM 51-35-01. LOCATED & DRILLED HOLES IAW SRM 51-3SDR 08FDEA01722Nose Cowl · corrodedNR 1 ENGINE NOSE COWL L/E HAS NUMEROUS AREAS OF PITTED CORROSION ALONG THE ENTIRE CIRCUMFERENCE OF EXTERNAL SKIN. REMOVED THE CORROSION IN REF TO DC/MD-10 SRM 51-21-01; VOL II AND FOUND TO BE OUT OF LIMITS IN REF TO DC/MD-10 SRM 54-00-01; VOL I. REMOVED &SDR 08FDEA01639Panel · chafedNR 3 PYLON PANEL 487 FL IS CHAFING AT THE INNER SURFACE. BLENDED OUT. ORIGINAL MATERIAL 0.071 IAW SRM 54-51-02; VOL III. MATERIAL REMOVED 0.027. MATERIAL REMANING 0.044; AND FOUND TO BE OUT OF LIMITS IAW SRM 54-00-01; VOL I; WTG T8225P. REMOVED THE SEALSDR 08FDEA01621Panel · damagedNR 1 PYLON 437ER HAS DAMAGED FASTENER HOLES. FABBED DOUBLER TO REPAIR FASTENER HOLE DAMAGE REF DC/MD-10 SRM 54-00-01; VOL III. ALODINED & PRIMED DOUBLER REF DC/MD-10 SRM 51-21-01; VOL II. INSTALLED DOUBLER REF DC/MD-10 SRM 51-35-01; VOL II.SDR USAA920080881Skin · crackedPIT - MAJOR REPAIR - CRACKED RIGHT PYLON SKIN, NACELLE STATION 224, AT ACCESS OPENING 5828R. REPAIRED RIGHT PYLON SKIN, NACELLE STATION 224, AT ACCESS OPENING 5828R IAW USAIRWAYS TYPICAL REPAIR 54-30-07.SDR 08FDEA01488Structure · crackedNR 2 ENGINE LEFT FWD COWLING OUTER AFT CORNER MULTIPLE LAYERS OF SHEET METAL ARE CRACKED. REMOVED DAMAGED AREA REF SRM 51-40-2. MATERIAL ID AT 2024 T3 .080 REF SRM 65-10-3 A48140 FOR DOUBLER. MATERIAL ID AT 2024 T3 .100 A 11734 REF SRM 54-30-2 FOR FILLER. SDR 08FDEA01483Skin · crackedCRACK ON INNER PERFORATED SKIN OF OUTER DUCT ASSEMBLY AT THREE O'CLOCK SIDE STRUT LOCATION. TO EVALUATE AND RECTIFY. REPAIR CRACK ON INNER PERFORATED SKIN OF OUTER DUCT ASSEMBLY AT THREE O'CLOCK SIDE STRUT LOCATION. A NEW REPAIR DOUBLER WAS FABRICATED AND ISDR 08FDEA01479Skin · dentedPYLON NUMBER ONE RIGHT FORWARD SKIN FOUND DENT. EVALUATE AND RECTIFY. REPLACED PYLON NUMBER ONE RIGHT FORWARD SKIN IN ACCORDANCE WITH B757- 200, SRM 51-10-02 AND BOEING DRAWING NUMBER 311N5002. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100 CRITERIA.
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