JASC 5414
Service difficulty reports · 4,357
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 AALA202504017850Skin Panel · wornAIRCRAFT IN BASE MAINTENANCE: WEAR MARKS ALONG THE RIGHT WING FIXED LEADING EDGE UPPER SKIN PANEL UPPER SURFACE, JUST INBOARD OF ENGINE STRUT. REMOVED AND INSTALLED NEW RIGHT WING FIXED LEADING EDGE SKIN PANEL. PER B737NG SRM 51-40-02.SDR SWIA2025062400318Panel · crackedR/H ENGINE NACELLE & PYLON LANDING FOR PNL 422AB (BENT/CRACKED) LOC. FWD INBD (MARKED) (C-CHECK RO 06/23/2025)REMOVED AND INSTALLED NEW RIB, PYLON STRUCT P/N 601-37004-86 ,REF. CRJ-200 SRM 51-42-06 , REF. CRJ-200 SRM 51-42-21 , REF.CRJ-200 SRM 51-45-00 AND DRSDR CALA2025031902942Skin · damaged#1 ENG PYLON AFT FIXED FAIRING LOWER SKIN PANEL HAS 1EA CHAFED RIVIT HEAD WITH MATERIAL LOSS. ESFR COMPLETE RMVD AND RPLD 1EA RIVET AT #1 ENG AFT FIXED FAIRING LOWER SKIN PNL IAW A320 SRM 51-42-11.SDR CALA2025031902941Skin · damaged#1 ENG PYLON AFT FIXED FAIRING INBD SIDE SKIN IS CRACKED AND HAS BROKEN/MISSING RIVETS. ESFR COMPLETE RMVD AND RPLD SKIN AT #1 ENG PYLON AFT FIXED FAIRING I/B IAW A320 SRM 54-54-11SDR AALA202503284914Skin Panel · wornAIRCRAFT IN BASE MAINTENANCE: WEAR MARKS ALONG THE LEFT WING FIXED LEADING EDGE UPPER SKIN PANEL UPPER SURFACE, JUST INBOARD OF ENGINE STRUT. REMOVED AND REPLACED LEFT HAND WING FIXED LEADING EDGE UPPER SKIN ASSEMBLY INBOARD ENGINE NUMBER 1. PER B737 SRM 51-40SDR IPXA2025041047242Skin · corrodedRH PYLON INSIDE PANEL 443CR FWD LOWER CORNER HAS CORROSION. DOT 28-45. ACOOMPLISHED STEP 23 INSTALLED REPAIR DOUBLER I.A.W EA# 757-5450-27-A3854 PRELIMINARY 3 AND SRM 51-40-02-OG. REVIEWEDSDR IPXA2025031647242Skin · corrodedRH PYLON INSIDE PANEL 443CR FWD LOWER CORNER HAS CORROSION. DOT 28-45 NOT ABLE TO REMOVE NOTED MEASUREMENTS. ALL MEASUREMENTS WERE ADDED TO CPCP AND SDR TASKS.SDR AALA202503269186Access Door · gougedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND NACELLE STRUCTURE UPPER FRAME AT FRONT ACCESS DOOR 434CL FOUND GOUGE MARK INSIDE AREA. PERFORMED BLEND OUT 1EA GOUGE AT LEFT HAND NACELLE STRUCTURE UPPER FRAME AT FRONT ACCESS DOOR 434CL INSIDE AREA. PERB777-300 SRM54-53SDR CALA2025031702848Skin · puncturedFOUND HOLE ON NUMBER 1 ENGINE PYLON FORWARD OF PRECOOLER. THIS LOGPAGE IS FOR ESFR REPORTING PURPOSES. SEE BAM N/R 2414981 FOR WORK PERFORMED. ADDED ESFR INFORMATION.SDR DALA2025031602000Access Panel · crackedSHIP 3116 CRACK ON ACCESS PANEL 413DL ON LH PYLON. CORRECTIVE ACTION: REPAIRED ACCESS PANEL 413DL PYLON L/H AS PER ER/A #540187-14MA. (0851394)SDR IPXA2025031757783Access Panel · delaminatedR/H PYLON ACCESS DOOR FOUND TO BE DELAMINATED DUE TO PYLON BLEED AIR LEAKAGE. R/R PRESSURE RELIEF ACCESS DOOR (PANEL # 443 LL, AMM 06-43-00) AT RT PYLON STRUT LOCATION PER AMM 54-53-01/401.SDR IPXA2025031157783Access Door · delaminatedR/H PYLON ACCESS DOOR FOUND TO BE DELAMINATED DUE TO PYLON BLEED AIR LEAKAGE.SDR 2025FA0000176Skin · noneREPAIR - ENG #1 EX NOSE INLET COWL SKIN - UNDOCUMENTED FLUSH REPAIRS.SDR 2025FA0000167Skin · not reportedREPAIR - ENG#2 - L/H CORE COWL INNER SKIN, AFT OF THE PRECOOLER VENT, UNDER THE PANEL 314T3210.SDR 2025FA0000166Skin · not reportedREPAIR - ENG #1 - L/H CORE COWL INNER SKIN. AFT OF THE PRECOOLER VENT, UNDER THE PANEL 314T3210.SDR NACA2025030700001Skin · corrodedNO.2 ENG INLET COWL INNER SKIN L/E SKIN BULGE BETWEEN 5 O'CLOCK ~ 7 O'CLOCK POSITION. REPLACED NO.2 ENG INLET COWL REF B737 AMM 71-11-01 PAGE 401~427 REV100, PME: 005115 DATE DUE: MAR 26 2025 200~1000IN-LBFSDR VNAA202503070003Skin · wornCHAFE DAMAGE TO INNER SIDE OF LH PYLON UPPER SKIN BTW FS1098.20 - FS1108.00 AND PBL59.90 - PBL69.30. CHAFE DAMAGE TO INNER SIDE OF LH PYLON UPPER SKIN BTW FS1098.20 - FS1108.00 AND PBL59.90 - PBL69.30 WAS REPAIRED PER REO 690-54-51-061 REV.--.SDR IXXA20250422005Landing · corroded#2 PYLON OTBD STRUT ATTACH ACCESS PANEL LANDING (A/C SIDE) HAS PITTING. REF HAECO WO 320011 NR 34926SDR CALA2025030500478Access Panel · missingPDA 2 REFERENCE LP 4049048: PANEL NACELLE STRUT ACCESS ENG N2 MISSING PANEL 436 BL REPLACED 436 BL PANEL ON E2 INBOARD PYLON NACELL. REF AMM 54-53-98.SDR UIEA2025022700173Skin · corrodedCORROSION ON #4 ENG LH CORE COWL SKIN BETWEEN NSTA 222 AND NSTA 230.(<P>1. REPAIR THE DAMAGE AREA IAW EI #T2025A54M-196 REV 0 AND REF DWG #314T4210 SH 7 REV-C, 344T4210 SH 8 REV D AND 314T4210 SH 5 REV B. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR UIEA2025022700174Skin · corrodedCORROSION ON #2 ENG LH CORE COWL SKIN BETWEEN NSTA 222 AND NSTA 230.(<P>1. REPAIR THE DAMAGE AREA IAW EI #T2025A54M-198, REV 0 AND REF DWG #314T4210 SH 20 REV D, 314T4210 SH 18 REV C AND 314T4210 SH 1 REV C. 2. JOB COMPLETED.</P>)SDR SWAA2025041404155Skin · damaged#2 ENGINE NOSE COWL LIP SKIN HAS A WORKING FASTENER AT 10 O CLOCK POSITION<[01] #2 ENGINE INLET COWL REPLACED GENERAL FAULT RESOLVED ON OTHER FAULT TTG8Q00S72VD;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.SDR DALA2025022501449Skin · damagedSHIP 3312 UT INSPECTION PYLON NO.1 LATERAL PANELS OF THE AREA OF FASTENERS NEAR THE UPPER EDGE OF THE EXTERNAL SURFACE OF THE HOLE IN THE FRONT ON THE LEFT AT RIB 8 LEVEL A CRACK APPROXIMATELY 3MM LONG WAS FOUND. CORRECTIVE ACTION: REPAIRED PER A330 SRM 54-51-SDR DALA2025021801185Access Panel · crackedSHIP 3122 CRACK ACCESS PANEL 423DL ON RH PYLON. CORRECTIVE ACTION: REPAIRED BY WELDING ACCESS PANEL 423DL RH PYLON AS PER ER/A 540187-14MA. (0815680)SDR JR2R20250212346Access Panel · chafedRH PYLON PANEL, 429NR, CHAFED IN MULTIPLE PLACES REQUIRING ENGINEERING APPROVALSDR CALA2025022600444Skin · gougedNRO.2 EG INBOARD PYLON ATTACH WING LANDIENG EDGE FILLET PANEL HAS DEEP GOUGE REF ARR N/R 9934107 REMOVED AND REPLACED SKIN CLOSEOUT 611A AT R/W L/E INBOARD OF PYLON AS PER B737-800 SRM 51-40-02-0G-0 AND DWG# 116A4008. WORK ACCOMPLISHED BY V918489 REMOVED AND RSDR CALA2025022600450Skin · gougedL/W L/E I/B OF PYLON SKIN GOUGED REF AAR N/R 9934263 REMOVED AND REPLACED SKIN AT L/W L/E INBOARD OF PYLON AS PER B73 37-800 SRM 51-40-02-0G-0 AND DWG# 116A4008. REMOVED AND REPLACED SKIN AT L/W L/E INBOARD OF PYLON AS PER B737-800 SRM 51-40-02-0G-0 AND DWG# SDR CALA2025021100332Scuff Plate · worn#1 PYLON BOTTOM SCUFF PLATE AFT OF AFT ENGINE MOUNT HAS WEAR PER HAECO LCQ N/R 9294185/42185. RMVD AND RPLD SCUFF PLATE AFT OF AFT ENGINE MOUNT ON #1 PYLON IAW A319 SRM 54-51-12-300-003 THIS REPAIR REQ SRI EVERY 4900FC 1200FH FROM EMBODIMENT SUBSEQUENT INSP ASDR IPXA2025021195005Skin · corroded#2 ENGINE OUTBD PYLON INNER SKIN AFT OF THE MID SPAR FITTING HAS CORROSION. DOT 8-002. RESTORED SURFACE PROTECTION IN #2 ENG, OUTBD PYLON INNER SKIN IAW SRM 51-20-01 P/N ALODINE1132 BTCH 0004336881 PRIME P/N 02-013-8 BTCH 4263196.SDR IPXA2025021194979Skin · corrodedNR 2 ENGINE OUTBD PYLON INNER SKIN FWD OF VENT PANEL OPENING HAS SURFACE CORROSION AND PROTECTIVE COATING DETERIOATED. DOT 8-001. RESTORED SURFACE PROTECTION IN #2 ENG, OUTBD PYLON INNER SKIN IAW SRM 51-20-01 P/N ALODINE1132 BTCH 0004336881 PRIME P/N 02-013-8SDR IPXA2025021192630Skin · corrodedPYLON #1 INNER SURFACE, JUST FWD OF 433CL HAS AREA OF CORROSION. DOT IS ON OUTSIDE OF PYLON. DOT 142-15.SURFACE HFEC PERFORMED ON BLENDED AREA OF #1 PYLON INNER SURFACE JUST FWD OF 433CL PANEL. NO DEFECTS FOUND IAW NTM 51-00-19.SDR GTIA2025020638727Skin · dentedDENT ON EXTERNAL SKIN INBOARD FAN COWL ON ENGINE 2 DAMAGE AREA: LENGTH 3.00IN, WIDTH 1.001IN, DEPTH 0.006IN, TIHCKNESS N/A RAF-01 3634033-02 GENERATED.-REPAIRED EXTERNAL SKIN INBOARD FAN COWL ON ENGINE 2 IAW EA #5414-2505 AND AE EA #54-0004-25 PART #1 PERMANENSDR VNAA20250330008Skin · wornWEAR ON AFT EDGE OUBD SIDE OF UPPER/LOWER FWD CORE COWL AT RH ENGINE. AFT EDGE OUBD SIDE OF UPPER FWD CORE COWL AT RH ENGINE WAS REPAIRED PER REO 670-54-23-1288 REV. - -. LOWER FWD CORE COWL AT RH ENGINE MUST BE REPLACED UNDER NRC 00122.SDR CALA2025020400287Skin · crackedSUPPORT TASK NO.2 PYLON I/B PNL 443CL CUTOUT SKIN FOUND SUSPECT CRACKED. WORK TRANSFER NON ROUTINE WO.4342845. DIP TO INSPECT THE REPAIR AREA AT #2 PYLON I/B STRUT SKIN AT 5450-02988 PART 2 ON OR BEFORE 02 FEBRUARY 2027 443CL ACCESS DOOR CUTOUT PER THE LATEST SDR SCNA20250127028Fastener · looseMULTIPLE SMOKED FASTENERS ON THE R/H WING JUST INBOARD OF THE #2 ENGINE PYLON WHEN PRESSING ON PANEL IT APPEARS THAT THE FASTENERS ARE LOOSE AND MAYBE SHEARED. ACCOMPLISHED REPAIR ON RH WING LOWER FIXED TRAILING EDGE PANEL I/B OF #2 PYLON IAW B737-800BCF SRMSDR UIEA2025011600073Access Panel · looseENG 1, INNER ACCESS PANEL 432 FL, PIPE "FIRE PROTECTION" WITH NUT LOOSE.(<P>ENG 1, INNER ACCESS PANEL 432 FL, PIPE "FIRE PROTECTION" NUT WAS TORQUED AND VERIFIED IAW AMM 20-11-00-910-801. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025011000013Inlet · corrodedCORROSION AT ENG 1 INLET COWL, INBD SIDE (INSIDE ACCESS PANEL) AT 8:00 O'CLOCK.(<P>ENG 1 INLET COWL WAS REPLACED IAW AMM 71-11-01-004-002-H00. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025011000014Inlet · corrodedENG 1, INLET COWL, ZONE 411, WITH POINTS OF CORROSION INNER ACCESS 412, AT INNER BARREL SKIN SURFACE, AT 12 HRS POSITION.(<P> ENG 1, INLET COWL WAS REPLACED IAW AMM 71-11-01-004-002-H00. NO FURTHER DEFECTS NOTED</P>)SDR JR2R20250115013Skin · damaged#2 ENG INLET COWL INTERNAL STRUCTURE ABOVE FADEC HAS MULTIPLE SCRIBE LINES.SDR JR2R20250115995Skin · damaged#1 ENG INLET COWL INTERNAL STRUCTURE ABOVE FADEC HAS MULTIPLE SCRIBE LINES.SDR EE4Y20250121534Skin · crackedDURING MAINTENANCE INSPECTION, IT WAS FOUND A EXISTING REPAIR INSTALLED BUT AT THE REPAIR RECORDS IS MISSING THE MATERIALS TRACEABILITY. DUE TO THIS SITUATION AND PER CUSTOMER REQUESTS THE REPAIR WAS REMOVED, AND NEW REPAIR WILL BE INSTALLED FOLLOWING REPAIR ISDR EE4Y2025010921514Skin · crackedDURING MAINTENANCE INSPECTION, IT WAS FOUND A EXISTING REPAIR INSTALLED AS PER CUSTOMER RECORDS PER ETD2022-190-037536 INSTRUCTIONS BUT AT THE REPAIR RECORDS IS MISSING THE MATERIALS TRACEABILITY. DUE TO THIS SITUATION AND PER CUSTOMER REQUESTS THE REPAIR WAS SDR IXXA20250201003Nose Cowl · gouged#2 ENGINE, INLET COWL, INNER LOWER SUFACE IS GOUGED. REF HAECO WO 320010 NON ROUTINE 30331SDR SWAA2025010682960Skin · pulled#1 ENG INNER INLET COWL LIPSKIN HAS ONE PULLED THROUGH FASTENER IN SEGMENT 3<[01] COMPLIED WITH EA 25-171-00023; REF TTG8Q00XYR35. THIS REMAINS ON TLD.SDR DALA2025010300056Access Door · missingSHIP 177 FOUND NACELLE STRUT ACCESS DOOR MISSING FROM INBOARD OF NO.1 ENGINE. CORRECTIVE ACTION: FWD TO CDL 54-53-02. NO "M" PROC NOTED. DISPATCH APPROVED. (6940342)SDR DALA2025010300058Panel · missingSHIP 171 FOUND #2 RH PYLON PANEL MISSING. CORRECTIVE ACTION: REPLACED #2 RH PYLON PANEL REF B767-300 AMM 54-53 (6940149)SDR CALA2024123003188Access Panel · missingPDA 2 AC ARRIVED TO LAX AT 2023HRS ON 12/28/24. WHILE PERFORMING WALK AROUND INSPECTION TECHS NOTICED PANEL 433JR MISSING FROM THE #1 ENG PYLON INBOARD SIDE. INSTALLED PANEL 433JR.SDR CALA2024123001689Panel · missingNUMBER 1 ENG PYLON MISSING PANEL INBOARD PHOTO ATTACHED. REFERENCE IPC 54-53-01-05 ITEM 208. PN MFG 311N5049-155. 1 SHOWING IN STOCK AT EWR. PART ORDERED.SDR SWIA2025031701226Cowling · chafedS/N 0368LH ENGINE INTERNAL. LOWER CORE COWL HAS MULTIPLE CHAFES AND GOUGES. FLAGGED (C-CHECK RO 3/14/2025) REPAIRED LH ENGINE INTERNAL, LOWER CORE COWL AT MULTIPLE CHAFES AND GOUGES. SEE CONTINUATION CARD FOR FURTHER DETAILS. ALL STEPS OF REO 670-54-23SDR DALA2024122311926Skin · crackedSHIP 3308 RH ENG LAPF LOWER SKIN CRACKED. CORRECTIVE ACTION: DOUBLER REPAIR AS PER PW MANUAL 51A702 CMM 54-56-11. (0724691)
Back to JASC 5414