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.

SDR 2010F00120Skin · delaminatedPYLON NR2, SKIN PYLON NR2 DELAMINATION ( RT INNER SIDE ) BETWEEN NAC STA 201.4 TO NAC STA 286,00.Jun 2, 2010 · N765SA · Boeing 7472F6BSDR 2010F00119Skin · delaminatedPYLON NR 2, SKIN PYLON NR 2 DELAMINATION ( RT INNER SIDE )BETWEEN NAC STA 201.4 TO NAC STA 286,00.Jun 2, 2010 · N765SA · Boeing 7472F6BSDR WRLA20100601363Skin Panel · crackedCRACK - NR 4 PYLON RIGHT SIDE ACCESS DOOR (482ER) SURROUND SKIN CRACK NRC U05004 ISSUED. REPAIRED CRACK AREA AT NR 4 PYLON STRUT NAC STA 227.27 NAC WL 155 IAW SRM 54-50-01 REPAIR 2 FIG 701 REV 76 AND REF JOB CARD ATTACHING SHEET 025021, 025824. COND CHECK NJun 1, 2010 · N741WA · Boeing 7474H6SDR FDEA201006011754Skin · crackedNR 1 ENGINE NACELLE STRUT AT FAIRING, LOWER AFT SECTION RT SIDE WITH CRACK. NR 1 ENGINE NACELLE STRUT AFT FAIRING SKIN R & R IAW SRM 51-40-02, REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Jun 1, 2010 · N937FD · Boeing 7572T7SDR 2010FA0000493Skin · corrodedPYLON NR 3 UPPER DSB LOWER WING SKIN WAS CORROSION LEVEL 2May 20, 2010 · N765SA · Boeing 7472F6BSDR IPXA10560370Skin · corrodedINSPECTION TYPE:C4, CORROSION ON NR 1 PYLON SKIN EXTERIOR SURFACE RT SIDE 6" AFT OF NR1 PYLON ACCESS PANEL NR433GR. DAMAGE CLEANUP BEYOND ALLOWABLE LIMITS CUTOUT DAMAGED SKIN AND INSTALLER RE-INFORCEMENT DOUBLER.May 15, 2010 · N454UP · Boeing 75724APFSDR FDEA201005151545Skin · crackedNR1 PYLON OTBD LATERAL WALL AT RIB 4A PRECOOLER HAS 1 EA CRACK. REPAIRED NR1 PYLON PRECOOLER LATERAL WALL AT RIB 4A IAW SRM 54-52-31, PB201, FIG 202.May 15, 2010 · N404FE · Airbus A310203SDR UIEA201000157Skin · crackedDURING MX WALKAROUND, MX FOUND 2EA CRACKS ON THE NR2 RT ENGINE CORE COWL OUTER SKIN. 1EA CIRCUMFERENTIAL CRACK IS APPROX 0.5 IN. LONG AND THE OTHER CRACK IS APPROX 2.0 IN. LONG. THE LENGTH AND THE SPACING OF THE CRACKS EXCEED THE SRM LIMITS. DISPOSITION IS TO May 11, 2010 · N412MC · Boeing 74747UFSDR UIEA201000156Skin · delaminatedDURING MX WALKAROUND, THE NR4 LT FAN COWL INNER AND OUTER SKINS WERE FOUND WITH DELAMINATION. EO: 4471A055 - PART 1 - TIME LIMITED REPAIR THE PART 1 TIME LIMITED REPAIR INSTALLS THROUGH BOLTS TO RESTORE THE CAPABILITY OF THE DISBONDED AREA AND IS FAA APPROVED May 10, 2010 · N498MC · Boeing 74747UFSDR KCSA101030Skin · damagedNR 3 PYLON TOP CAP SKIN IS DAMAGED AT NAC STA 221.9, WL 190.52.May 1, 2010 · N715CK · Boeing 747209BSDR KCSA101029Skin · damagedNR 2 PYLON TOP CAP SKIN IS DAMAGED AT NAC STA 221.9, WL 190.52.May 1, 2010 · N715CK · Boeing 747209BSDR KCSA101028Skin · chafedNR 4 PYLON HAS A CHAFE IN THE EXTERNAL SKIN AT NAC STA 205 NEAR THE TOP INBOARD SIDE.May 1, 2010 · N715CK · Boeing 747209BSDR AALA20100421TUL08Skin · crackedTRAILING AFT INBOARD UPPER HOLE INDICATES A CRACK AND OUTBOARD UPPER AFT HOLE INDICATES A CRACK. ACCOMPLISHED DOUBLER REPAIR IN ACCORDANCE WITH EA B757-54-010091 AND FAA-AD CARD F1566AC.Apr 21, 2010 · N625AA · Boeing 757223SDR NSVA201079Skin · damagedMAJOR REPAIR OF LT NACELLE INBOARD SKIN REPAIR DOUBLER AT STA 203 IAW TD 340-54-10-05.Apr 20, 2010 · N193CJ · Saab 340BSDR FDEA201004191227Panel · wornNR 2 ENG PYLON PANEL 457 CL LOWER LATCH CONTACT AREA IS WORN. INTERNAL DOUBLER BEING REPLACED ON NON-ROUTINE N00442. NO FURTHER MX REQUIRED , COPY ATTACHED. ALSO SEE SDR TRACKING NR 10-1226.Apr 19, 2010 · N361FE · Doug MD1010FSDR SWIA201024234Skin · crackedRIGHT AFT NACELLE, OUTBOARD SIDE, SKIN CRACKED. (C CHECK)REPLACED RIB AND SKIN PER SRM.Apr 15, 2010 · N297SW · Emb EMB120ERSDR FDEA201004151200Panel · corrodedNR 1 ENGINE NACELLE STRUT ACCESS PANEL NR 433GR CUTOUT AREA AT STA 120, INTERNAL SURFACE CORROSION. CORRODED PANEL NR 433GR R & R IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Apr 15, 2010 · N937FD · Boeing 7572T7SDR FDEA201004091126Skin · mismanufactured3EA FASTENER HOLES MIS- LOCATED IN THE INBD SKIN PANEL ASSY, PN 311N5046Y54, COMMON TO THE INBD 311N5220-52, BATHTUB FITTING AND 1EA C/M TO THE PN 311N5220-54, MID-CHORD. REMOVED DAMAGE FROM HOLES "B" AND "C" TO SIZE .408, AND HOLE "A" TO SIZE .567, AND PERFORApr 9, 2010 · N924FD · Boeing 757204SDR 2010FA0000437Skin · crackedNR 3 ENG PYLON AFT LWR SPAR FIREWALL SKIN 1.5 INCH CRACK.Apr 6, 2010 · N708SA · Boeing 7472B5FSDR 2010FA0000436Skin · crackedNR 3 ENG LT PYLON ACCESS PANEL CRACKED.Apr 6, 2010 · N708SA · Boeing 7472B5FSDR A6WA201040271Cowling · chafedLT LOWER CORE COWL CHAFED IN CTR APPROX 6 " FROM DOME. REPAIRED IAW CMM 71-12-01, REPAIR NO SRS064 & REO 601R-71-12-3976.Apr 6, 2010 · N440AW · Cndair CL6002B19SDR 2010FA0000434Skin · crackedNR 3 ENG LT SIDE COWL SKIN CRACK. INSTALL EXTERNAL REPAIR DOUBLER.Apr 5, 2010 · N708SA · Boeing 7472B5FSDR 2010FA0000432Skin · crackedNR 4 PYLON AFT FAIRING DOOR LT SIDE CRACKED. BONDING EXTERNAL REPAIR DOUBLER.Apr 5, 2010 · N708SA · Boeing 7472B5FSDR ABXA201004120046Skin · chafedNR 1 NACELLE STRUT, FWD TORQUE BOX, OUTBOARD SKIN HAS 2 SMALL CHAFE AREAS JUST BELOW ACCESS PANEL 432AL. REPAIRED IAW REA B654-58718.Mar 27, 2010 · N769AX · Boeing 767281SDR ABXA201004120045Skin · chafedNR 1 NACELLE STRUT FWD TORQUE BOX OUTBOARD SKIN HAS TWO LONG CHAFES AT METAL STRIP FOR T/R SEAL. REPAIRED IAW REA B654-58712-MR.Mar 27, 2010 · N769AX · Boeing 767281SDR UIEA201000072Skin · crackedDURING C-CHECK, CRACKING WAS FOUND IN THE 65B94052-1, NR3 PYLON RT SKIN ASSY AT THE NAC STA 248 PRECOOLER EXHAUST. THE CRACK WAS REPAIRED BY TRIMMING OUT THE DAMAGE AND RESTORING THE SURFACE FINISH IAW RFTA 00664-0006, REV A AND REA MF00664R0006, REV A (FIG 1 Mar 26, 2010 · N540MC · Boeing 747243FSDR UIEA201000071Skin · crackedDURING C-CHECK, CRACKING WAS FOUND IN THE 65B94052-1 NR 2 PYLON RT SKIN ASSY AT THE NAC STA 248 PRECOOLER EXHAUST. CRACK WAS REPAIRED BY TRIMMING OUT THE DAMAGE AND RESTORING THE SURFACE FINISH IAW RFTA 00664-0005, REV A AND REA MF00664R0005, REV A (FIG 1 & 2Mar 26, 2010 · N540MC · Boeing 747243BSDR IPXA10559206Panel · chafedINSPECTION TYPE:C4, NR 2 ENGINE PYLON PANEL NR 443FR CUTOUT HAS CHAFING ON AFT SURFACE (MARKED). REPAIRED PLATE IAW ATS ER NR 10-2179.Mar 20, 2010 · N451UP · Boeing 75724APFSDR A6WA201040206Skin · crackedRT ENG LOWER CORE COWL INBD L/E IS BENT AND CRACKED. REPAIRED IAW CMM 71-12-01.Mar 10, 2010 · N436AW · Cndair CL6002B19SDR FDEA201003010584Panel · chafedNR 3 PYLON PANEL 487 CL INTERNAL VENT DOUBLER IS CHAFED. CHAFED AREA MEASURES 0.016 REMAINING AND IS OUT OF LIMITS IAW SRM 54-00-01; VOL I. REMOVED, FABRICATED AND INSTALLED DOUBLER IN REF TO EA 8-5458-136634.Mar 1, 2010 · N570FE · Doug MD1010FSDR FDEA201003010574Skin · chafed1 ENGINE LT FAN COWL INNER SKIN IS CHAFED. BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 54-00-01, FIG 1-A, VOL I. REMOVED LT FAN COWL TO FOM IAW AMM 71-13-01. REMOVED DAMAGED DOUBLERS; MATERIAL ID; FABRICATED NEW METAL DOUBLERS; PREPPED AND BONDED IAW SRMar 1, 2010 · N570FE · Doug MD1010FSDR FDEA201003010573Skin · chafedNR 1 ENG RT FAN COWL INNER SKIN IS CHAFING THE OIL TANK. REMOVED ACCESS DOOR IAW SRM 51-31-01, VOL II. DOOR INNER SKIN FOUND TO BE OUT OF LIMITS IAW SRM 54-00-01, FIG 1-A, VOL I WITH 100 PERCENT MATERIAL LOSS. INSTALLED NEW ACCESS DOOR, PO NR 677295.1 IAW SMar 1, 2010 · N570FE · Doug MD1010FSDR FDEA201003010568Skin · gougedNR 3 ENG LT FAN COWL INNER SKIN IS GOUGED. REPAIRED NR 3 ENG LT FAN COWL INNER SKIN BY REMOVING GOUGE AREA AND FABRICATED A FILLER AND DOUBLER AND BONDING IT IAW SRM 54-00-01, FIG 7-A; VOL I.Mar 1, 2010 · N570FE · Doug MD1010FSDR FDEA201003010566Skin · gougedNR 3 ENG RT FAN COWL INNER SKIN IS GOUGED. REMOVED DAMAGE & APPLIED AN INTERNAL FILLER AND EXTERNAL DOUBLER REPAIR. SEALED AND PRIMED IAW SRM 54-00-01, FIG 1-A VOL I; SRM 54-31-01, VOL III; SRM 51-71-00, VOL II AND SRM 51-38-01, VOL II.Mar 1, 2010 · N570FE · Doug MD1010FSDR 22AA201000057Skin · wornDURING "C" CHECK, NR 2 ENG LT CORE COWL UPPER AFT RUB STRIP FOUND WORN TO COWLING SKIN. NON-ROUTINE NR 0198, WORN COWLING SKIN AREA AT NR 2 ENG LT CORE COWL UPPER AFT RUB STRIP AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED Feb 24, 2010 · N478CT · Doug DC1030FSDR USAA2010022590446Skin · crackedCLT - Q5 - MAJOR REPAIR - CRACK IN LEFT PYLON SKIN PANEL 5728L ACCESS HOLE. REPAIRED LEFT PYLON SKIN IAW TYPICAL REPAIR 54-30-07.Feb 24, 2010 · N453UW · Boeing 7374B7SDR 2010FA0000366Door · delaminated(KADY) DISBOND (24.0" X 3.5") WAS FOUND BETWEEN OUTER SKIN (65B90036-2) AND ALUMINUM HONEYCOMB CORE (65B90036-18) OF THE NR 1 RT STRUT FAIRING DOOR (65B90032-28).Feb 23, 2010 · N749SA · Boeing 747300SDR SWIA201023904Skin · chafedRIGHT NACELLE WEBBED SKIN CHAFED. (C CHECK) REPLACED SKIN PER SRM.Feb 22, 2010 · N298SW · Emb EMB120ERSDR SWIA201023900Skin · chafedLEFT AND RIGHT NACELLE WEBBED SKIN CHAFED. (C CHECK) REPLACED SKINS PER SRM.Feb 22, 2010 · N298SW · Emb EMB120ERSDR 2010FA0000369Door · delaminatedDISBOND (21.0" X 5.0") WAS FOUND BETWEEN OUTER SKIN (65B90036-2) AND ALUMINUM HONEYCOMB CORE (65B90036-18) AND CRACK (2.0", 1.3" LONG) ON OUTER SKIN (65B90036-2) OF THE NR 1 LT STRUT FAIRING DOOR (65B90032-29).Feb 20, 2010 · N749SA · Boeing 747300SDR DL76L100676Skin · crackedNR 1 PYLON ACCESS PANEL 436AR CUTOUT SKIN FOUND CRACKED. REPAIRED IAW ERA 479024-14AD, REV 0.Feb 18, 2010 · N172DN · Boeing 767332SDR 2010FA0000327Skin · damaged(KADY) SHARP NICK AND GOUGES AT NR 4 LT SIDE COWL SKIN NAC STA 165.0. MINOR REPAIR ACCOMPLISHED BY TRIM OUT THE DAMAGED SKIN AND INSTALL REPAIR PARTS.Feb 16, 2010 · N749SA · Boeing 747300SDR 22AA201000042Skin · wornDURING "C" CHECK , NR 2 ENGINE LT CORE COWL UPPER SKIN FOUND WITH WEAR MARKS. NON-ROUTINE NR 440, WEAR MARKS ON NR 2 ENGINE LT CORE COWL UPPER SKIN AREA REPAIRED IAW EN 1007-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030FSDR 22AA201000040Skin · crackedDURING "C" CHECK, NR 2 ENGINE RT CORE COWL FWD LOWER SKIN FOUND WITH CRACK. NON-ROUTINE NR 439, CRACK AREA AT NR 2 ENGINE RT CORE COWL FWD LOWER SKIN AREA REPAIRED IAW EN 1009-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030FSDR UIEA201000159Access Panel · crackedCRACKS WERE FOUND IN THE NR 3 PYLON INBD ACCESS PANEL 472FL AS SHOWN IN FIGURE 1. NR 3 PYLON ACCESS PANEL 452FL CRACKED AREA REPAIRED IAW EO 4454A095.Feb 9, 2010 · N412MC · Boeing 74747UFSDR UALA2010021000514Skin · damagedNR 1 NACELLE STRUT OTBD SIDE SKIN AT THRUST REV HINGE AREA, 2ND LIGHTENING HOLE, APPROX 7:30 POS, ONE CRACK IN SKIN EXTENDING APPROX .185" BEYOND END OF EXISTING SKIN TRIM OUT REPAIR. ROUTED OUT DAMAGE AND ACP HFEC INSP AND VERIFIED WEB PANEL CRACK FREE. WORFeb 9, 2010 · N538UA · Boeing 757222SDR UALA2010021000513Skin · damagedNR 2 NACELLE STRUT OB SIDE SKIN AT THRUST REV HINGE AREA, AFT LIGHTNING HOLE AT 1:30 POS, ONE CRACK IN SKIN EXTENDING APPROX .185" BEYOND END OF EXISTING SKIN TRIM OUT REPAIR. ROUTED OUT DAMAGE. ACP HEFC INSP AND VERIFIED CRACK FREE ON WEB PANEL.Feb 9, 2010 · N538UA · Boeing 757222SDR UALA2010021000512Skin · crackedNR 2 NACELLE STRUT SIDE SKIN IB SIDE FWD ACCESS HOLE IS CRACKED AT THE 11:00 POS, APPROX .50" INCH LONG. MAJOR REPAIR ACCOMPLISHED: STOP DRILLED CRACK. ACP HFEC INSP FOR CRACK TERMINATION. FABRICATED AND INSTALLED DOUBLER.Feb 9, 2010 · N538UA · Boeing 757222SDR FDEA201002090370Skin · corrodedNR 1 PYLON RT INNER SKIN HAS CORROSION RUNNING INTO SPLICE, ACCESS THRU PANEL 433HR AND 433JR. CORROSION ON SKIN BLENDED OUT OF LIMITS IAW SRM 54-50-01, FIG 101, DETAIL II. REPLACED SKIN ASSY WITH PN 311N5046Y54, SKIN PANEL ON SERVICABLE PARTS TAG NR 1455B2 Feb 9, 2010 · N924FD · Boeing 757204SDR FDEA201002090369Skin · corrodedNR 2 PYLON TORQUE BOX ASSY RT AND LT SIDE INNER SKIN SURFACE HAVE CORROSION RUNING DOWN THE LOWER CHORD. INSTALLED NEW SKIN PN 311N5046Y53, IAW SRM 51-40-02, DWG 311N5002, AND EO F-5450-7-5003, P5, CORROSION ON SKIN BLENDED OUT OF LIMITS PER SRM 54-40-02. REFeb 9, 2010 · N924FD · Boeing 757204
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