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 G60A200800015Skin · crackedNR 2 PYL PANEL 437HL HAS CRACKS.SDR G60A200800014Panel · crackedNR 2 ENG PYLON PANEL 437DR HAS CRACK NEAR BASE OF FIN.SDR USAA920080374Skin · crackedCLT - MAJOR REPAIR - Q5 CHECK - NR JK-81-54500/8, NR 1 PYLON LEFT SKIN CRACKED AT ACCESS PANEL 5924L. REPAIRED NR 1 PYLON LEFT SKIN IAW USAIRWAYS TYPICAL REPAIR 54-50-07.SDR EIA2008009Skin · crackedNR 2 PYLON PRECOOLER EXHAUST CUTOUT EDGE, NR 3 STIFFENER NAC STATION 248 TO 234 HAS 2 EACH CRACKS IN SKIN DOUBLER TRIPLER, CRACKS EXTEND FROM CUTOUT EDGE AND RUN UNDER STIFFENER. REMOVED DAMAGE AND STIFFENER, NDT AREA, FABRICATED REPAIR PARTS AND INSTALLED PESDR KCSA081042Skin · chafedPYLON NR 1 OUTER SKIN CHAFED WING L/E STA 1124 NAC STA 263.SDR 08FDEA00265Panel · corrodedNR 1 NACELLE STRUT I/B SKIN PANEL ASSY PN: 311N5046-34 HAS AREAS OF CORROSION C/M TO THE INNER SKIN SURFACE BETWEEN PP STA 153.9 AND PP 176 REMOVED CORROSION IAW SRM 54-50-01. ORIGINAL MATERIAL THICKNESS, 0.090", AFTER CORROSION REMOVAL, 0.063" AT PP STA 15SDR WRLA2008015Fairing · crackedDURING C-CHECK INSPECTION, FOUND 2 INCH CRACK IN NR 1 ENGINE LOWER RIGHT AFT SECTION FAIRING. REPAIRED PER ENGINEERING INSTRUCTION NR W2008A57B-059 REV.00. REF EGAT NRC U05004.SDR KCSA081031Skin · crackedNR 4 PYLON I/B SKIN CRACKED AT UPPER AFT CORNER OF THE FWD LOWER ACCESS PANEL OPENING AT NAC STA 208.SDR KCSA081030Skin · crackedNR 4 PYLON I/B SKIN CRACKED AT FWD LOWER ACCESS PANEL OPENING AT NAC STA 197.SDR KCSA081029Skin · crackedNR 3 PYLON I/B SKIN HAS A CRACK AT AFT UPPER CORNER OF ACCESS PANEL OPENING AT NAC STA 208.SDR UPS08M51688Fairing · crackedINSPECTION TYPE:1C FROM DMI LOG D339585 TAIL ENG PYLON LOWER AFT FAIRING CRACK REPAIRS REF EO MD11-5450-25730. REMOVED INTERIM REPAIR DOUBLERS, CUTOUT DAMAGE/CRACKS, FABRICATED, AND INSTALLED REPAIR FILLERS & DOUBLERS IAW MD-11 SRM 54-00-01 FIG 4 , 51-31-01, SDR 08FDEA00191Skin · dentedNR 1 NACELLE STRUT O/B SIDE SKIN HAS TWO DENTS, AT CUT OUT AREA OF ACCESS PANEL 433BL, AT APPROXIMATELY NAC STA 136.675, OUTBOARD SKIN HAD TWO DENTS MEASURING 1.6" WIDE BY .126" DEEP AND 1.9" WIDE BY .10" DEEP. BOTH FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01,SDR UPS08M51616Panel · dentedINSPECTION TYPE:C NR 2 PYLON PANEL 457GR HAS A DENT ON ITS SKIN. REPAIR ACCOMPLISHED PER EA 11-5400-27-A1772 AND UPS EO NO MD11-5480-28541-A.SDR USAA920080411Skin · crackedMCN - MAJOR REPAIR - C20 CHECK - CRACKED NR 2 PYLON SKIN PANEL, PYLON STATION 261. REPAIRED NR 2 PYLON SKIN PANEL, PYLON STATION 261 IAW USAIRWAYS EA 100219.SDR DHL2007873508Skin · wornNR 4 ENG RT NOSE COWL UPPER EXTERNAL SKIN WORN AT STA YN 147.534 AT 12 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1.2. REMOVED FASTENERS IAW SRM 51-1-21, CUT OUT DAMAGE SECTION AND FABRICATED NE SKIN AND SPLICE IAW SRM 71-5SDR CA071219006Skin · cracked(CAN) BOTH THE LT AND RT REPAIR DOUBLERS THAT ARE IDENTIFIED AS ITEM -1 ON THE ATTACHED REO601R-53-61-358, REVISION A, WERE FOUND CRACKED DURING AN INSPECTION OF THE ENGINE SUPPORT BEAMS AT A HEAVY CHECK VISIT. THIS AC CAME INTO OUR AIRLINE OPERATION AT APPROSDR COMA0770081Door · dentedLEFT ENGINE LOWER FAN COWL DOOR DENTED BEYOND LIMITS. REPAIRED LEFT ENGINE LOWER FAN COWL DOOR IAW REO 670-54-14-019.SDR MASA200700880Skin · tornFOUND DAMAGE TO THE NR 2 ENGINE NACELLE. DAMAGE IS A TEAR IN THE LOWER SKIN PANEL AND EXCEEDS THE LIMITS. MX PERFORMED REPAIR.SDR EIA2007205Skin · crackedNUMBER 2 PYLON PRECOOLER LOWER SKIN, TWO CRACKS FOUND AT AFT UPPER CORNER. REPAIR PER 54-50-35916. PERFORM DVI PER ECRA 489-54-010-1.SDR EIA2007204Skin · crackedNUMBER 3 PYLON PRECOOLER EXHAUST LOWER CUTOUT AFT AREA CRACKED. REPAIRED PER 54-50-359, PERFORM DVI PER ECRA 489-54-010-1. PER HAECO 5192.SDR COMA0770071Cowl Door · damagedRIGHT ENGINE LOWER FAN COWL DOOR I/B AFT CORNER IS DAMAGED. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 54-14-00 AND 51-14-00.SDR TRAX200701818Skin · crackedENGINE SUPPORT BOX BEAM UPPER SKIN HAS 17/32 INCH CRACK AT AFT CENTER SECTION JUST I/B OF RBL 9.500 SEE AFDL 311351 ITEM 2.SDR F3LA200700339Fairing · crackedDURING C4/S1 CHECK, INSPECTION REPORTED NR 1 ENGINE FAN OUTLET FAIRING INSTALLATION HAD CRACKS AT THE 7 O'CLOCK AND 9 O'CLOCK POSITIONS. REMOVED AND REPLACED NR 1 ENGINE FAN OUTLET FAIRING IAW SRM 51-44-11, 51-42-11 AND AMM 51-75-12-300-003.SDR EIA2007218Skin · crackedNR 2 PYLON INBOARD SIDE AFT OF THRUST REVERSER SLEEVE INSPECTION PANEL 463AR. CUTOUT HAS 2 AREAS OF DAMAGE. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 490-54-005-2.SDR DHL2007801539Skin · crackedNR 4 ENG NACELLE INLET COWL LT EXTERNAL SKIN CRACKED 1" STA YN 132.000 AT 9 O'CLOCK POS. (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 10-16-07, EVA B271-00015 REV IR DATED 10-12-07. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-21A, CUT OUTSDR DLM88071494Skin · gougedDUE SPLSKD SRM REPAIR 53-04 DENT/GOUGE NR 2 PYLON ABOVE LGN 19R FWD OF STA 1309. REPAIRED PER SRM 53-04D FIG 12B CLASS 2. REINSPECT DUE AT 15000 CYCLES. DATA RETRIEVAL SENT.SDR SWAA075700Skin · crackedDURING SCHEDULED SPV CHECK, FOUND NR 1 ENGINE UPPER PYLON T-CROWN CRACKED. REPAIRED PYLON PER ER.SDR CALA0700675Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN NR 2 PYLON ACCESS PANEL 5824 CUTOUT ON UPPER FORWARD CORNER, NAC STA 258. THE CRACK WAS STOP DRILLED AND A PERMANENT REPAIR WAS INSTALLED IAW ECRA 5430-01204.SDR DHL2007801520Skin · wornNR 1 ENG NACELLE INLET COWL UPPER SKIN WORN STA YN 150.000 AT 12 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION. FABRICATED NEW SKIN (AL2024T3 0.080") AND SPLICSDR DHL2007801521Skin · wornNR 2 ENG NACELLE INLET COWL UPPER SKIN WORN AT 12 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED NEW SKIN (AL2024T3 0.080") AND SPLICE (STEEL TYPSDR UIEA200700463Skin · crackedNR 4 PYLON LT SKIN WAS FOUND A CRACK AT THE 483 AL ACCESS PANEL CUTOUT LOWER AFT CORNER. DEFECTIVE CRACK AREA INTERIM REPAIRED AS PER BOEING MESSAGE NR 1-656345659-3 AND ATLAS XEO NR 54-102307.
SDR UIEA200700462Skin · crackedNR 4 PYLON LT SKIN WAS FOUND CRACK AT 483AL ACCESS PANEL CUTOUT LOWER AFT CORNER.SDR QXEA200701602Skin · debondedC4 PDX - RIGHT ENGINE PYLON TRAILING EDGE ASSEMBLY LOWER SKIN IS DISBONDED AND TORE. REPAIRED IAW SRM 54-53-01, 51-75-00, AND 51-42-13.SDR AMTA200700491Skin · crackedUPON REMOVAL OF HEAT SHIELD ON NR 1 STRUT OB SIDE FOUND SKIN, INTERNAL DOUBLER AND SHIM CRACKED AT PRECOOLER LANDING APPROX PP STA 182.00. (K) REPAIRED PER SAA EA 757-5450-09-A1018. (M)SDR CALA0700577Skin · crackedNR 1 ENG PYLON CRACKED AT ACCESS PANEL 5727. INSTALLED DOUBLER PER ECRA 5430-01230.SDR 2007UALA04161Skin · damagedNR 1 PYLON NAC STA 140 OUTBOARD SIDE SKIN FASTENER HOLE ELONGATED THRU SKIN AND DOUBLER. 11-01-07 MAJOR REPAIR ACCOMPLISHED. REAMED HOLES 1, 2, AND 3 TO BE TRUE ROUND AND CONCENTRIC. ACCOMPLISHED HFEC. INSTALLED FASTNERS IN HOLES 2 AND 3. MACHINED FREEZSDR K11A2008121572011Skin · damagedCENTER ENGINE AIR INTAKE DUCT HAS SKIN DAMAGE AT AFT EDGE, 9 O’CLOCK POSITION.SDR 07FDEA04386Panel · crackedFOUND CRACK (ABOUT 6MM) AT PYLON NR 2 RIB 8 OUTBOARD SIDE WALL DOUBLER REPAIR PERFORMED IAW SRM 54-51-31 FIG 201.SDR K11A2008121572009Skin · crackedCENTER ENGINE AIR INTAKE DUCT HAS SKIN CRACK, 4 O`CLOCK POSITION.SDR DL76L071277Skin · crackedCRACK AT FACTORY CUTOUT ON INBOARD SKIN OF NR 2 PYLON. CRACK WAS STOP DRILLED AND DOUBLERS INSTALLED.SDR QXEA200701475Skin · crackedC5 PDX - ON NR 1 NACELLE SKIN AT THE FORWARD INBOARD CUTOUT RADIUS FOR THE FORWARD GEAR DOOR. THE NACELLE SKIN IS CRACKED 1/4" LONG. REPAIRED IAW RD8-54-873.SDR DL757071247Skin · crackedNAC STA 128 CUTOUT FOR THE CENTER THRUST REVERSER FORWARD EQUALIZATION ROD ON THE NR 2 PYLON HAD A CRACK IN THE AFT HOLE AND EDGE DAMAGE ON THE FORWARD HOLE. DAMAGE WAS TRIMMED OUT AND A DOUBLER AND TRIPLER WERE INSTALLED.SDR 07FDEA04250Panel · wornWEARED HOLES IN LATERAL PANELS (INBOARD AND OUTBOARD), RIB 8 UPPER SPAR OF PYLON NR 1 LT. REPAIR PERFORMED BY INSTALLATION OF BUTTERFLY DOUBLERS ON BOTH PANELS IAW SRM 54-51-31/CONFIG 2/PB 201.SDR DL757101123Skin · crackedNR 2 PYLON OTBD SKIN CTR T/R MOUNT, FWD EQUALIZATION ROD CUTOUT REPAIR IAW ERA 464134-14, C/W ERA 464134-14.SDR 07FDEA04084Panel · damagedFOUND DAMAGED HOLES ON BUTTERFLY REPAIR DOUBLERS AT INBOARD AND OUTBOARD SIDEWALL PANEL, PYLON NR 1 LT. REPAIR PERFORMED BY INSTALLING NEW DOUBLERS ON SIDEWALL PANELS IAW SRM 54-51-31/FIG 201.SDR 07FDEA04082Panel · damagedFOUND DAMAGED HOLES ON BUTTERFLY REPAIR DOUBLER AT INBOARD SIDEWALL PANEL, PYLON NR 2 RT. REPAIR PERFORMED BY INSTALLING NEW DOUBLER ON SIDEWALL PANEL IAW SRM 54-51-31/FIG 201.SDR 07FDEA04030Panel · crackedCRACK (ABOUT 8MM) FOUND AT INBOARD SIDE WALL PANEL, RIB 8, PYLON NR 2 REPAIR PERFORMED IAW SRM 54-51-31 FIG 201.SDR ABXA070308Panel · missingON WALKAROUND, MAINTENANCE FOUND NR 2 ENGINE INBOARD PYLON PANEL MISSING. DEFERRED 57076. C/W REA B654-56397, APPLIED SPEED TAPE. DEFERRED IAW REA B654-56397 AND GMM CHAPTER 1, SECTION 7.04 FOR MX TRACKING. CLEARED: DI 57076, INSTALLED NEW PANEL 446BL IAW SDR 2007UALA03726Skin · damagedNR 2 PYLON FWD I/B SIDE SKIN AT NAC STA 125 HAS EXISTING FASTENER HOLE ELONGATED. HFEC INSPECTED, NO DEFECTS NOTED. INSTALLED 2EA FREEZE PLUGS.SDR DU4R2007173Skin · damagedFOUND CHAFED NR 2 PYLON AFT WEB FITTING CHAFED AT BOTTOM LT CORNER. REPAIRED BY FABRICATING AND INSTALLED REPAIR HFEC NO RELEVANT INDICATIONS, FABRICATING AND INSTALLING REPAIR GUSSET 4.34" BY 2.88" BY 1.2" FROM 7050-T7451 IAW DELTA ERA 463490-14AD DATED 9-12
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