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 FDEA201008132987Skin · dentedNR 2 PYLON FOUND INNER DOUBLER WITH A DENT AT PANEL NR 443BR CUTOUT. REPAIR CARRIED OUT IAW EA F-5450-139381. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201008132986Skin · crackedNR 2 PYLON FOUND INNER DOUBER CRACKED AT PANEL NR 443AR CUTOUT FWD LOWER SIDE. REPAIR CARRIED OUT IAW EA F-5450-139381. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201008132985Skin · corrodedNR 2 PYLON FOUND CORROSION ON INNER DOUBLER AT PANEL NR 443GL CUTOUT FWD LOWER AND MID LOWER SIDE. REPAIR CARRIED OUT IAW EA F-5450-139381. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201008132984Skin · crackedNR 2 PYLON FOUND INNER DOUBLER CRACKED AT PANEL NR 443GL CUTOUT FWD LOWER SIDE. REPAIRED IAW EA F-5450-139381, CLASSIFIED AS MAJOR.SDR FDEA201008132983Skin · corrodedLT PYLON PANEL 433BL CORROSION ON MATING SURFACE. CORROSION DAMAGE REPAIRED IAW EA F-5450-139382.SDR FDEA201008132982Skin · corrodedLT PYLON PANEL 433JR CORROSION ON INTERIOR MATING SURFACE TO PYLON. CORROSION ON LT PYLON PANEL 433JR REPAIRED IAW EA F-5450-139382.SDR FDEA201008132981Skin · crackedNR 1 PYLON PANEL CUTOUT 433AL HAS CRACK AT LOWER FWD CORNER. NR1 PYLON PANEL CUTOUT CRACKED SKIN REPAIRED IAW EA F-5450-139382. CLASSIFIED AS MAJOR.SDR UVVR2010081300014Skin · corroded(UVVR) EXTERIOR SURFACE OF SKINS ON LOWER ENGINE COWLINGS SHOW EVIDENCE OF CORROSION AROUND RIVET HEADS. PAINT IS BLISTERING.SDR A6WA201040595Panel · chafedPYLON PANEL 412DB HAS KNIFE EDGES REPLACED (2 EA) SEPARATORS ON PYLON PANEL 412DB IAW CRJ 200 51-77-00, 51-42-06, 51-42-13.SDR WRLA20100811433Skin · damagedDENT AND GOUGE ON NR 3 ENG PYLON AFT FAIRING SKIN AT YPN=245, ZPN=20.SDR VGQY2010081000075Skin · crackedNR 2 PYLON, PYLON SKIN FOUND CRACK AT PANEL 463AR CUTOUT AREA. NO SRM REPAIR. HFEC INSPECTION CARRIED OUT PER SA NDTPM D6-7170 REV 134 PART 6 51-00-00 FIGURE 23 ON PYLON NR 2 PANEL SKIN 463AR CUTOUT AREA. FOUND NO CRACK EVIDENT.SDR A6WA201040740Panel · chafedCHAFE ON EDGE AT PANEL 412DB DIVIDERS. R & R PANLE 412DB DIVIDERS.SDR DALA1018940186Panel · crackedNR 2 PYLON STRUT RT MOST FWD NR 426 BR PANEL CUTOUT CRACKED. REPAIRED AS IAW SRM 54-53-01, FIG 201, REPAIR 6.SDR UALA2010080902891Nose Cowl · damagedACFT TAXIED INTO JETWAY DAMAGING LT ENGINE NOSE COWL. FOUND DAMAGE AT 12 O'CLOCK POS. DAMAGE 2 DENT ONE IS 12 IN WIDE X 8 IN LONG X 2 IN DP. THE OTHER IS 18 IN LONG X 4 IN WIDE X 1 IN DP. ENG 1 INLET L/E BEYOND ALLOWABLE DAMAGE LIMITS OF SRM. REPLACED INLSDR WRLA20100806422Skin · crackedCRACK ON OUTBOARD SKIN OF NR 1 ENGINE LOWER AFT FAIRING.SDR IPXA0M62008Skin · crackedINSPECTION TYPE:4C, NR 3 PYLON FAIRING 488EL OTBD SIDE SKIN HAS CRACK AT RIVET AT MARKED. REMOVED EXISTING DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER AND FILLER AT NR 3 PYLON FAIRING 488EL OTBD SIDE SKIN REF DWG AUB7562 , SRM 51-38-01, SRM 54-0SDR IPXA10562047Panel · chafedINSPECTION TYPE:C2, NAC-STRUT NR1 STRUCTURE OF PANEL NR 434BL HAS CHAFED AFT BLENDED AND TREATED IAW ER 10-3669.SDR R61A20100324Panel · crackedWHILE AC WAS IN FOR HEAVY CHECK, A MAJOR REPAIR WAS ACCOMPLISHED. RIGHT ENGINE OUTBOARD PYLON PANEL WAS FOUND CRACKED. MAINTENANCE REQUESTED EMB ENGINEERING SUPPORT AND RECEIVED ETD 2010-170/05893 FOR THE REPAIR. MAINTENANCE REPAIRED THE PANEL PER THE EMB ESDR IPXA10561459Channel · chafedINSP TYPE:C2, PANEL 445BL IC CHAFED ON INNER SURFACE. REMOVED FABRICATED AND INSTALLED NEW CHANNEL ON PANEL 445BL.SDR KCSA101091Repair · damagedREMOVE AND INVESTIGATE NR 2 PYLON INBOARD SKIN REPAIR AT NAC STA 175.SDR IPXA10561262Splice · gougedINSPECTION TYPE:C2, NR 2 PYLON INBD PLATE IS GOUGED JUST AFT OF PANEL NR 441AT. R & R SPLICE PLATE IAW SRM51-40-02-0G.SDR AALA20100630TUL03Bullnose · crackedLEFT WING PYLON AREA INBOARD BULLNOSE CRACKED, MARKED. STOP DRILLED CRACK PER SRM 51-10-02-0G. REPAIRED CRACK PER SRM 57-41-01-6 AND RE-ASSEMBLED.SDR DALA1020220662Skin · damagedAFTER REMOVAL OF LT SKIN ON NR2 PYLON, FOUND DAMAGED HOLE AT STA 114 UPPER CHORD AREA.SDR FDEA201006302266Skin · corrodedNR1 PYLON AT STA 144-170 SKIN HAS CORROSION. REMOVED CORROSION ON NR 1 PYLON SKIN STA 144-170 IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01 FIG 101 DETAIL III. ORIG MATERIAL .090 EXFOLIATED BEYOND LIMITS. L=12" W=3". REMOVED AND REPLACED SKIN ISDR UALA2010070102344Skin · crackedNR 2 NACELLE STRUT SKIN CRACKED AT ACCESS PANEL 442AL CUTOUT. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA, FOUND 3 CRACKS TOTAL, FABRICATED & INSTALLED A CRES REPAIR DOUBLER AND FILLERS.SDR FDEA201006302228Skin · damagedNR 2 NACELLE STRUT AFT FAIRING LOWER SEGMENT SKIN JUST AFT OF PP STA 276.93 WITH SEVERAL LOOSE FASTENERS. UPON EVALUATION FOUND HOLES ELONGATED TO REPLACE SKIN. AFT FAIRING LOWER SEGMENT JUST AFT OF PPSTA 276.93, NR 2 ENG NACELLE STRUT, AFT FAIRING SKIN ANDSDR WGFY2010FA0000493Skin · corrodedPYLON NR 3 UPPER DSB LOWER WING SKIN WAS CORROSION LEVEL 2.SDR WGFY2010FA0000489Skin · corroded(WGFY) PYLON NR 4 UPPER DSB LOWER WING SKIN WAS CORROSION LEVEL 2, REFER TO JOB CARDS NR 54-812-01-04. MFG MESSAGE: YDK-SOF-10-0011-04B/18 MAY 2010, YDK-SOF-10-0011-09B/03 JUNE 2010, YDK-SOF-10-0011-11B/05JUNE 2010. PERFORM REPEAT DVI INSPECTION OF THE SUSDR CA100707011Access Panel · departedDURING FLIGHT FROM CPH/DENMARK TO HAM/GERMANY BOTH NOSE ACCESS COWL DOORS FROM THE LT ENGINE WERE LOST. AFTER INSPECTION OF THE AIRCRAFT DAMAGED WAS FOUND AT: LT ENGINE NOSE COWL LT TR-TQ BOX AND CASCADE LT ACCESS COWL, UPPER AND LOWER LT FUSELAGE BETWEEN FS SDR UIEA2010062400033Skin · dentedDURING WALKAROUND INSPECTION IN HKG, MAINTENANCE FOUND DAMAGE TO THE NR 2 ENGINE RT FAN COWL DENT DAMAGE, BELOW THE SERVICE OIL DOOR (REF FIGURE 1). DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS; SCHEDULE REPEASDR NSVA2010104Skin · damagedPERM REPAIR FOR RT NACELLE OUTBOARD SKIN STA 203 TD 339-12.SDR IPXA10560890Panel · corrodedINSPECTION TYPE:C3, PANEL NR 426FR INNER SURFACE HAS AREAS OF CORROSION REPLACED PANEL 426FR IAW SRM 54-30-01-1A, SRM 51-21-01-0G.SDR IPXA10560889Panel · corrodedINSPECTION TYPE:C3, PANEL NR 426GR INNER SURFACE HAS AREAS OF CORROSION. REPLACED PANEL NR 426GR IAW SRM 54-30-01-1A, SRM 51-20-01-0G.SDR IPXA10560888Panel · corrodedINSPECTION TYPE:C3, PANEL 415HL INNER SURFACE HAS AREAS OF CORROSION. REPLACED PANEL NR 415HL IAW SRM 54-30-01-1A, SRM 51-21-01-0G.SDR IPXA10560887Panel · corrodedINSPECTION TYPE:C3, PANEL NR 425HL INNER SURFACE HAS AREAS OF CORROSION. REPLACED PANEL NR 425HL IAW SRM 54-30-01-1A, SRM 51-21-01-0G.SDR IPXA10560886Panel · corrodedINSPECTION TYPE:C3, PANEL NR 415GL INNER SURFACE HAS AREAS OF CORROSION REPLACED PANEL NR 415GL IAW SRM 51-10-02, SRM 54-30-01-1A.SDR A6WA201040447Panel · gougedT/E OF UPPER TRANSLATING COWL PANEL 444AT GOUGED. BLEND, NDT, TREAT AREA (PROTECT UNFINISH) AND RECORD REO NR ON COMPONENT SERIAL PLATE IAW REO 601R-78-33-3935.SDR HNAA2010063000164Skin · damagedABOUT 10 RIVETS ARE WORKING ON OTBD SIDE OF NR2 NACELLE AT XN134.68 TO ZN 24.60 (BELOW AND AFT OF OTBD IGNITER BAY DOOR). REPAIRED IAW EO8-54-10-0275.SDR HALA2010061500263Skin · damagedETOPS SIGNIFICANT SYS - FOUND NR 1 ENG INLET COWL INNER SKIN AT 12 O'CLOCK
POS HAS IMPACT DAMAGE (APPROX .2500" X .2500"). REPAIRED IAW SRM 51-70-03 INLET COWL 12 O'CLOCK POS NR 1 ENG.SDR A6WA201040606Panel · chafedPANEL 422DB DIVIDERS ARE KNIFE EDGED. INSTALLED NEW SEPARATORS ON PANEL 422DB.SDR WRLA20100607409Skin · crackedCRACKED NR 2 INLET LIP OUTER SKIN CRACK AT 5-7 O'CLOCK.SDR WRLA20100607407Skin · crackedCRACK AT NR 2 ENG INLET LIP INNER SKIN INNER SURFACE CRACK AT 6 O'CLOCK.SDR USAA2010071491422Skin · corrodedMCN - C22 - MAJOR REPAIR - THREE BULGES IN LEFT UPPER PYLON SKIN ALONG CENTER SEAM AT NAC STA 204 TO NAC STA 248 & BETWEEN BL2R TO BL2L. REPAIRED LEFT UPPER PYLON SKIN ALONG CENTER SEAM AT NAC STA204 TO NAC STA 248 & BETWEEN BL2R TO BL2L IAW EA 130422.SDR USAA2010071491419Skin · corrodedMCN - C22 - MAJOR REPAIR - THREE BULGES IN LEFT UPPER PYLON SKIN ALONG CENTER SEAM AT NAC STA 204 TO NAC STA 248 & BETWEEN BL2R TO BL2L. REPAIRED LEFT UPPER PYLON SKIN ALONG CENTER SEAM AT NAC STA 204 TO NAC STA 248 & BETWEEN BL2R TO BL2L IAW EA 130422.SDR USAA2010060491061Skin Panel · crackedCLT - Q3 - MAJOR REPAIR - CRACK EMANATING FROM LEFT PYLON SKIN PANEL CUTOUT NR 5727 AT FORWARD CORNER. REPAIRED LEFT PYLON SKIN PANEL CUTOUT NR 5727 AT FORWARD CORNER IAW TYPICAL REPAIR 54-30-07.SDR A6WA201040568Guide · crackedRT PYLON PANEL DIVERTER GUIDE HAS CRACK. R & R DIVERTER GUIDE.SDR WGFY2010FA0765014Skin · delaminated((WGFY)) PYLON NR 3 LT INNER SKIN DELAMINATION (BETWEEN NAC STA 201.60 TO 240.00) PERFORMED DVI OF THE REPAIR ZONE AT THE REPEAT "C" CHECK, PERFORM REPEAT DVI INSPECTION PER SB 747 54A2182R2 REQUIREMENT AT 1200 FLIGHT CYCLE INTERVAL NOT TO EXCEED 24 MOUNTHSSDR A6WA201040566Retainer Seal · crackedLT PYLON SEPARATOR PANEL NR 412DB SEAL RETAINER CRACKED AND SEAL WORN. R & R LT PYLON PANEL NR 412DB SEAL AND SEAL RETAINER PN 601-37003-65 AND PN 601-337003-303 IAW SRM 51-42-06, 51-40-11 AND AMM 54-63-01.SDR A6WA201040565Retainer Seal · crackedRT PYLON PANEL 422DB CRACKED SEAL RETAINER REMOVED AND REPLACED. SEAL RETAINER IAW SRM 51-42-06, R & R SEAL IAW AMM 54-63-01.SDR WGFY2010FA0765011Skin · delaminated((WGFY)) PYLON NR 2, SKIN PYLON NR 2 DELAMINATION (RT INNER SIDE ) BETWEEN NAC 201,4 TO NAC STA 286,00. PERFORM A REPEATED DVI OF THE SUBJECT REPAIRED AREAS AT EVERY "C" CHECK OR 18 MONTHS, WHICH EVER OCCURS FIRST.
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