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 USAA960008Skin · corrosionCLT - INSPECTION VISUALLY FOUND EXFOLIATION LEVEL 2 CORROSION BETWEEN SKIN AND DOUBLER OUTBOARD PYLON SKIN IN AREA OF HEAT SHIELD NR 1 PYLON. REPLACED SKIN NR 1 PYLON OUTBOARD SIDE PER USAIR EA NR 40605. (M)SDR USAA960007Skin · corrosionCLT - INSPECTION VISUALLY FOUND EXFOLIATION LEVEL 2 CORROSION BETWEEN SKIN AND DOUBLER INBOARD PYLON SKIN IN AREA OF HEAT SHIELD NR 1 PYLON. REPLACED SKIN IN NR 1 PYLON INBOARD SIDE AS PER EA NR 40605. (M)SDR USAA960003Skin · delaminationPIT - DURING Q-1 INSPECTION, FOUND SKIN DELAMINATION LEFT STUB WING TO FUSELAGE AT STATION 24011 TO 26011. INSTALLED DOUBLER REPAIR PER USAIR EA NR 29492B AND EA NR 31703. (M)SDR USAA960000Skin · delaminationPIT - DURING Q-1 INSPECTION, FOUND SKIN DELAMINATION RIGHT STUB WING TO FUSELAGE AT STATION 24011-26011. INSTALLED DOUBLER REPAIR PER USAIR EA NR 29492B AND EA NR 31703. (M)SDR ABXA9600427Skin · dentedDURING 826AX MOD, DISCOVERED A DENT AT NR 3 ENGINE PYLON, STATION YN 141.00, PYLON LOWER SURFACE. REPAIRED NR 3 ENGINE PYLON THAT WAS DENTED ON THE LOWER SURFACE AT STATION YN 141.00 IAW ABX REA D854-12587MR.SDR USAA951363Skin · crackedPIT - WHILE ACCOMPLISHING X-RAY INSPECTION OF PYLON AREA IN BOS, MAINTENANCE DISCOVERED A .25 INCH CRACK IN SKIN AT STA 965, LONGERON 14L. AIRCRAFT WAS MAINTENANCE FERRIED TO PIT FOR REPAIR. INTERIM EXTERNAL DOUBLER REPAIR INSTALLED PER USAIR EA NR 31838. ASDR AALA952151Skin · damagedAFW - FOUND SIDE SKIN DAMAGE IS BEYOND SRM LIMITS AFTER BLEND OUT. SIDE SKIN BLENDED AND FINISHED PER MRB 767-1098. SIDE SKIN IS ACCEPTABLE FOR CONTINUED SERVICE WITH NOTED CONDITION PER ENGINEERING MRB 767-1098. (M)SDR DL757954798Skin · crackedPYLON SKIN CRACKED NR 2 PYLON O/B SIDE AT FWD ACCESS HOLE, 1 PLACE. REMOVED FASTENERS/CRACK PER SRM 54-51-01 AND INSTALLED DOUBLER PER SRM 54-51-01.SDR DL757954797Skin · crackedPYLON SKIN CRACKED NR 2 PYLON I/B SIDE AT FWD ACCESS HOLE, 2 PLACES. DRILLED OUT ALL FASTENERS, CUT OUT DAMAGED AREA, DRILLED AND INSTALLED REPAIR PER 54-50-01 PG 207.SDR P2RA950038Panel · crackedPHX - DURING C-CHECK, NR 1 PYLON HAS A CRACK AND MISSING MATERIAL FROM INTERNAL WEB ON LOWER AFT PANEL. MAINTENANCE REMOVED AND REPLACED DAMAGED AREA PER SRM 54-00-00. (M)SDR P2RA950041Panel · buckledPHX - DURING B-CHECK, NR 1 PYLON PANEL NR 474DR HAS LOWER LEADING EDGE AND TRAILING EDGE BUCKLED. REPAIRED PANEL PER SRM 51-42-20. (M)SDR P2RA950040Panel · buckledPHX - DURING B-CHECK, NR 1 ENGINE PYLON PANEL NR 474CR BUCKLED ON LOWER TRAILING EDGE. REPAIRED PANEL PER SRM 51-42-20. (M)SDR P2RA950037Panel · crackedPHX - DURNG B-CHECK, NR 1 ENGINE PYLON PANLE NR 475CL HAS LOOSE FASTENERS AND CRACK PROGRESSING TOWARD FASTENERS HOLE. REMOVED AND REPLACED LOOSE FASTENERS PER SRM 51-30-1. INSTALLED DOUBLER OVER CRACK CONDITION PER SRM 51-30-1. (M)SDR P2RA950036Panel · crackedPHX - DURING B-CHECK, NR 1 ENGINE PYLON PANEL NR 483DL WAS CRACKED AND BUCKLED. REPAIRED PANEL PER SRM 51-42-20. (M)SDR UPS405133Skin · crackedMAINTENANCE REPORTED NR 3 ENGINE PYLON INBOARD SIDE SKIN DOUBLER AFT OF SLOT SEAL FAIRING HAS CRACK AT INNER RADIUS OF DOUBLER EXTENDING INTO BASE METAL. REPAIRED IAW EO B747-5430-7704B.SDR UPS405132Skin · crackedMAINTENANCE REPORTED NR 3 ENGINE PYLON INBOARD SIDE SKIN DOUBLER AFT OF SLOT SEAL FAIRING HAS CRACK AT INNER RADIUS OF DOUBLER EXTENDING INTO BASE METAL. REPAIRED IAW EO B747-5430-7704B.SDR UPS405135Skin · delaminatedMAINTENANCE REPORTED LEFT WING L/E INBOARD OF NR 2 PYLON HAS DELAMINATION. REPAIRED IAW SRM 51-40-09.SDR DL72K954418Skin · crackedFOUND DURING A-2 LTR CHK, NR 2 ENG NOSECOWL SKIN CRACKED .75 INCH AT 1ST RIB AFT OF LIP. REPAIRED PER MM 54-30-0 PAR 1.SDR DL72K954417Skin · crackedITEM FOUND DURING A-2 LTR CHK, 1.25 INCH CRACK AT FASTENERS AFT LWR CORNER PANEL 9516 RT SIDE NR 2 ENG DUCT HOUSING. REPAIRED PER B727 MM 54-30-0 PAR 1.SDR MALA954700Skin · crackedDURING A SCHEDULED INSPECTION IN MSP, INSPECTORS NOTICED A CRACK IN THE RIGHT LOWER INBOARD NACELLE SKIN TO LOWER WING SKIN ATTACH ANGLE. MAINTENANCE PERSONNEL REMOVED THE CRACKED ATTACH ANGLE AND REPLACED IT WITH A NEW ANGLE IAW ARP 54-20-9101. (M)SDR UPS804942Skin · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 2 PYLON TRAILING EDGE SKIN CRACKED 1 INCH LONG ABOVE FWD DRAIN TUBE RT SIDE. REPAIRED PER UPS EO DC8-5420-4308-A.SDR DL72K954219Skin · crackedFOUND ON A2 LETTER CK, 1 INCH CRACK AT FASTENER NUMBER 2 ENGINE INLET OUTER SKIN LT SIDE FWD OF SADDLE PANEL. REPAIRED PER MM 54-30-0.SDR USAA951195Skin · corrosionCLT - CLT INSPECTION VISUALLY FOUND CORRODED SKIN PAST LIMITS OF EO 5492R274 PART IV STEPS 2 AND 3, ON NR 2 PYLON. REPAIRED SKIN PER DRAWING 013N8774. (M)SDR USAA951193Skin · corrosionCLT - CLT INSPECTION VISUALLY FOUND CORRODED SKIN PAST LIMITS OF EO NR 5492R274 PART IV STEPS 2 AND 3 LOCATED AT NR 2 ENGINE PYLON INBOARD. REPAIRED SKIN PER DRAWING 012N8774 AND EA 40036. (M0SDR P5CA9500816Fireshield · delaminatedNR 1 ENGINE RT CORE COWL UPPER FAIRING LOWER SKIN DELAMINATED. REMOVED DAMAGED FIRESHIELD, FABRICATED NEW COUPLER AND INSTALLED IAW SRM 54-30-03.SDR DL76L954197Skin · crackedAT LETTER CHECK, FOUND 2 CRACKS IN NR 2 ENGINE PYLON O/B STRUT SKIN. REPAIRED PER DL ERA 2 71983-14.SDR CAL950874Skin · crackedHOU - INSPECTION FOUND A 1 INCH CRACK IN OUTER SKIN AT INBOARD SIDE OF PYLON OF NR 1 ENGINE PYLON ACCESS CUT OUT. A REPAIR WAS INSTALLED IAW ECRA 5430-01204. (X)SDR DL76L954198Skin · crackedTWO CRACKS HAVE BEEN REPORTED IN THE NR 2 ENGINE PYLON O/B STRUT SKIN. THEY BOTH GO THROUGH BOTH SHEETS OF THE BONDED SKIN ASSEMBLY. REPAIRED PER DL ERA 271951-14.SDR MALA954635Skin · crackedDURING A SCHEDULED INSPECTION IN MSP, A CRACK WAS NOTED ON THE RIGHT NACELLES INBOARD KEELSON WEB BETWEEN THE MAIN SPAR AND THE MAIN LANDING GEAR DRAG BRACE. REPAIRS WERE COMPLETED BY STOP DRILLING THE CRACK AND INSTALLING A REPAIR DOUBLER AS PER LIMITED AUTHSDR 9514626624Skin · crackedDURING PERIODIC CHECK, FOUND A .25 INCH CRACK IN THE NR 1 PYLON INBOARD SKIN AT NACELLE STATION 175, WATER LINE 151. REPAIRED SKIN PER EA 66-99085.SDR RAAAE895028Skin · crackedDURING SCHEDULED NR 4 CHECK, FOUND NR 1 NACELLE LOWER INBOARD AFT NACELLE SKIN CRACKED AT NACELLE STA 43.0, LOWER. REPAIRED PER SRM 54-2-1, FIGURE 3. (X)SDR 96ZZZX2924Skin · damagedDURING RETRACTION TEST OF LANDING GEAR, THE LEFT INBOARD AFT GEAR DOOR CAUGHT ON THE LOWER EDGE OF NACELLE SKIN. REPAIRED PER SRM 54-2-1, FIGURE 3.SDR CAL950837Skin · crackedHOU - INSPECTION FOUND A .25 INCH CRACK IN NACELLE STRUT SKIN OF NR 1 ENGINE AT PANEL 5754 CUTOUT AND PANEL 5725 CUTOUT. A DOUBLER WAS INSTALLED IAW ECRA 5430-01024. (M)SDR CAL950830Skin · crackHOU - INSPECTION FOUND A .75 INCH CRACK IN NACELLE STRUT SKIN OF NR 2 ENGINE AT PANEL 5824 CUTOUT. THE CRACK WAS STOP DRILLED AND A DOUBELR WAS INSTALLED IAW ECRA 5430-01204. (M)SDR UPS404352Skin · damagedWHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND PYLON NR 4 NAC: STA 225, SKIN DAMAGED BY WEAR ON TOP OF PYLON, OUTBOARD SIDE. SKIN REPAIRED ACC: S.R.M. 54-30-03 FIG 17A.SDR DL757953603Skin · crackedDURING HMV, FOUND NR 2 PYLON SKIN CRACKED ON OUTBD SIDE, JUST AFT OF NAC STA 107.70. REPAIRED PER SRM 54-51-01 PG 206 TO 210.SDR EISA95336Skin · corrodedDURING INSPECTION AT AERO CORP IN LAKE CITY, FL, NR 2 ENGINE PYLON HAS CORROSION BULGING ON RIGHT SIDE AT LOWER EDGE OF SKIN UPPER SURFACE. REMOVED FASTENERS IAW SRM 51-30-2. CLEANED CORROSION IAW SRM 51-10-6 (AT APPROXIMATELY STATION 1352 ONLY). OK TO ALODSDR EISA95306Skin · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE NR 2 ENGINE PYLON HAS CORROSION BULGES ON LEFT SIDE AT LOWER SIDE OF SKIN UPPER SURFACE. REMOVED, FABRICATED AND INSTALLED THREE SKIN PANELS, ONE RAIN GUTTER DUE TO OUT OF SRM LIMITS IAW B727 SRM SDR 9512979994Skin · damagedDURING ACCEPTANCE CHECK, FOUND RIGHT PYLON TRAILING EDGE SECTION LOWER SKIN TO SECOND RIB WITH ELEVEN LOOSE FASTENERS AT END OF RIB. REPAIRED LOWER SKIN SECTION PER EA 99-094743 AND SRM 51-30-2.SDR P5CA9500703Skin · crackedSKIN CRACK AT NR 4 PYLON, FORWARD ACCESS DOOR CUTOUT 1.75 INCH LONG, TERMINATES AT FASTENER. REPAIRED PER BOEING SRM 54-30-03 FIG 17B.SDR DL733953295Skin · wornAT HMV, INSPECTION FOUND THE NR 2 PYLON CHAFED ON THE I/B SIDE AT WING L/E. BLENDED WEAR DAMAGE, INSTALLED REPAIR PER SRM 54-50-01 FIG 203.SDR DL733953276Skin · wornAT HMV IN ATL, INSPECTION FOUND THE NR 2 PYLON CHAFED ON THE O/B SIDE AT WING L/E. BURNISHED AREA AND INSTALLED DOUBLER PER SRM 54-50-01 FIG 203.SDR DL733953300Skin · wornAT HMV, INSPECTION FOUND THE I/B SIDE OF NR 1 PYLON WORN AT WING L/E. BLENDED AREA AND INSTALLED DOUBLER PER DL ERA300634-14 AND SRM 54-50-01 FIG 203.SDR USAA950976Nacelle · damagedCLT - DURING A CMV-1 INSPECTION, FOUND A 2 INCH BY 3.5 INCH TEAR AND DENT AT NR 2 NACELLE STRUT RIGHT SIDE PP STATION 134.5. INSTALLED DOUBLER, FILLERS, SKIN. (M)SDR DL72W953367Skin · damagedDURING HMV, FOUND TEMP REPAIRED INSTALLED RIGHT SIDE AFT AND ABOVE PANEL 9516. REPAIRED PER MM 53-30-0 PAGE 801 AND 802.SDR UPS403885Skin · damagedWHILE IN FOR C-CHECK, MAINTENANCE FOUND DAMAGE ON OUTER SKIN OF PYLON NR 4 AT STA 210. REPAIRED IAW SRM 54-30-03.SDR UPS403884Skin · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK ON OUTER SKIN OF PYLON NR 4 OF ACCESS PANEL AT STA 195, LT. REPAIRED IAW SRM 54-30-03.SDR AALA951262Skin · wornAFW - FOUND A GROOVE WORN IN THE LEFT PYLON INBOARD AND OUTBOARD SIDE SKINS. BOTH GROOVES WERE CAUSED BY AN ANGLE ON THE THRUST REVERSER RUBBING ON THE SIDE SKINS. BLENDED AND REFINISHED GROOVES. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINESDR 95ZZZM258Plank · crackedDURING PREFLIGHT, FOUND CRACK AT NR 1 INTERMEDIATE PYLON PLANK, PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR, FABRICATE NEW DOUBLER AND TRIPLER, TREATED, PRIMED AND INSTALLED IAW DAC GL PO 1505.SDR DL733953126Skin · wornAT HMV, INSP FOUND THE O/B SIDE OF NR 2 PYLON WORN AT WING L/E AREA. ACCOMPLISHED REPAIRS PER SRM 54-50-01 PG 219.
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