JASC 5414
Service difficulty reports · 4,360
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 DALA2022032401985None · none" SUPPLMENTAL INFOMATION' SHIP 1200 #1 ENG OUTBOARD NACELLE STRUT ACCESS DOOR MISSING/ DAMAGED . CORRECITVE ACTION: FORWARD TO CDL 54-53-02 ACCESS DOOR PLACED IN FWD E&E M.C.O POUCH. INSTALLED NEW ACCESS DOOR PER B767 - 300 AMM 5453. AC OK FOR SVC (8717701)SDR DALA2022030801502None · noneRIGHT ENGINE INBOARD TR V-BLADE SEGMENT HAS CORROSION PIT ON THE LOWER SEGMENT. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0120:7830-2007-RH/ 001 00099 COMPLIED WITH ER/A 597672-14 PRI REV 0, ER/A 597672-14 PRI REV 1 AND FINAL ER/A 597672-14 REV ORIGINAL. (SDR DALA2022030401415None · none'SUPPLMENTAL INFOMATION' SHIP 1200 ON ARRIVAL FOUND NACELLE STRUT ACCESS DOOS MISSING ON #1 ENGINE INBOARD SIDE. CORRECTIVE ACTION: FWD TO CDL 54-53-02. MCC CONTACTED. DISPATCH APPROVED. INSTALLED NEW ACCESS DOOR PER B767-300 AMM 54-53 AC OK FOR SVC. (8148037)SDR DALA2022030701449None · noneSHIP 174 UPON ARRIVAL FOUND NBR 1 ENG NACELLE STRUT ACCESS DOOR MISSING. CORRECTIVE ACTION: INSTALLED #1 ENG NACELLE STRUT ACCESS DOOR. REF B767-300 AMM 54- 53 (8257766)SDR DALA2022030101288Skin · crackedER/A 271951-14 REV E, DURING HCK AT STAG, CRACKING WAS FOUND ON THE #2 PYLON, RH SKIN AT NAC STA 156-172. CORECTIVE ACTION: PER ERA 271951-14 REV F, DTE ANALYSIS FOR THE SECTION III REPAIR COMPLETED. DAMAGE TOLERANCE ASSESSMENT HAS ESTABLISHED THAT THIS IS A CSDR DALA2022030401414None · noneSHIP 189 ON WALK AROUND FOUND #1 ENG RT HAND SIDE NACELLE STRUT ACCESS PANEL MISSING 436BR. CORRECTIVE ACTION: ON WALK AROUND FOUND #1 ENG RT HAND SIDE NACELLE STRUT ACCESS PANEL MISSING 436BR. (8151814)SDR MASA20220223112None · noneTHE RH INLET COWL LIPSKIN WAS FOUND TO HAVE CORROSION DAMAGE. THE MINIMUM REMAINING THICKNESSES IN THE BLENDED AREA ES 0.059. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 54-11-05-001-001-A01, FIGURE 54-11-05-991-801, ITEM 1, (REV. 37 DATSDR AALA202202010095Plate · elongatedAIRCRAFT WAS GROUNDED: MAINTENANCE FOUND HYDRAULIC LINE MOUNTING PLATE HOLE ELONGATED ABOVE PYLON ON LOWER WING SKIN ON #2 ENGINE PYLON. REPAIRED MOUNTING PLATE PER AARD 57-21-11-1.SDR SWAA2022031065358Plate · crackedCRACK SEAL PLATE ACCESS PANEL 431AL AT LT WING 2022-55356 / [01] REPLACED SEAL PLATE LOCATED ACCESS PANEL 431AL AT LT NACELLE STRUT. IAW B737-700 SRM 51-40-02-0G-0.;[02] REPLACED SEAL PLATE LOCATED ACCESS PANEL 431AL AT LT NACELLE STRUT. IAW B737-700 SRM 51-40SDR SWAA2022031065360Plate · crackedCRACK ACCESS PANEL 431AR SEAL PLATE LT PYLON 2022-55358 / [01] REPLACED SEAL PLATE ON ACCESS PANEL 431AR LT PYLON IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9.;[02] REPLACED SEAL PLATE ON ACCESS PANEL 431AR LT PYLON IAW B737-700 SRM 51-40-02 AND SRM 51-10SDR SWAA2022031065367Plate · crackedCRACK ACCESS PANEL 441AR SEAL PLATE RT PYLON 2022-55367 / [01] REPLACED SEAL PLATE ON ACCESS PANEL 441AR RT PYLON IAW B737-700 SRM 51-40-02-0G;[02] REPLACED SEAL PLATE ON ACCESS PANEL 441AR RT PYLON IAW B737-700 SRM 51-40-02-0GSDR DALA2022012700559None · noneSHIP 3267 CORROSION INNER BORE LOWER SPIGOT FITTING JOINT ON LH PYLON. CORRECTIVE ACTION: REPLACED LOWER SPIGOT FITTING ON LH PYLON AS PER A320 SRM 54-51-12. (2099984)SDR SWAA2022021055434Access Panel · delaminatedSUPPLEMENTAL INFORMATION: INNER LINER MATERIAL SHOWS EVIDENCE OF DELAMINATION AND OVER 90% MATERIAL DETERIORATION ; ACCESS PANEL 431DR / [01] REMOVED AND REPLACED ALUMINIUM FOIL DAMAGE AT PANEL 431DR IN REF B737-700 SRM 51-70-14-2R-3; [02] VERIFIED WORK PERFORSDR DALA2021121707853None · noneSHIP 3358 ELONGATED HOLE ACCESS PANEL 453AR ON LH PYLON. CORRECTIVE ACTION: REF ER/A 595663-14 FOR CORRECTIVE ACTION. (2053094)SDR MASA20211123569None · noneRH UPPER FAN COWL DOOR HINGE FITTING (PN -CN622-0306-206) AND ITS MATING STRUCTURE, THE PYLON TIE BAR (PN -CN624-4203-207) WERE FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-14-05-001-001-A01, 54-24-01-001-002-A01, EA12-2021SDR DALA2021112307209None · noneSHIP 3321 DENT UPPER FWD PYLON LEADING EDGE AREA ON RH PYLON. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON UPPER FWD PYLON LEADING EDGE AREA ON RH PYLON AS PER ER/A 595352-14. (2024255)SDR DALA2021111807127None · noneSHIP 3305 ELONGATED HOLE ACCESS PANEL 453AR ON LH PYLON. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR INSTRUCTIONS ON HOLE LOCATED ON ACCESS PANEL 453AR INBOARD SIDE OF LH PYLON ON ENGINE#1 AS PER ER/A 595259-14. (2020248)SDR DALA2021111807123None · noneSHIP 3305 ACCESS PANELS 453AL IN THE LH PYLON WERE FOUND WITH ELONGATED HOLES. A330 SRM 54-57-11 DOES NOT PROVIDE ADL NOR REPAIR INSTRUCTIONS FOR THIS SCENARIO. CORRECTIVE ACTION: MAINTENANCE CORRECTIVE ACTION PERFORMED REF ER/A 595259-14. (2020216)SDR DALA2021111807122None · noneSHIP 3305 TWO DENTS HAVE BEEN FOUND IN THE UPPER SURFACE OF THE FWD SIDE IN THE LH PYLON. DAMAGES HAS BEEN EVALUATED AS PER A330 SRM 54-50-00- 283-008, RESULTING IN AN OUT OF LIMITS SITUATION SINCE D IS LESS THAN 20XT. CORRECTIVE ACTION: PERFORMED PERMANENT RESDR DALA2021111507051None · noneSHIP 3321 DENT UPPER FWD PYLON SKIN LH PYLON. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS LOC UPPER FWD SKIN ON LH PYLON RIB 01 TO RIB J08 SECTION 1 AS PER ER/A 595358-14. (2016071)SDR DALA2021111507047None · noneSHIP 3305 ELONGATED HOLE ACCESS PANEL 463AR ON RH PYLON. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON HOLE ACCESS PANEL 463AR ON RH PYLON AS PER SECTION I ER/A 595258-14. (2016049)SDR DALA2021111507046None · noneSHIP 3305 ELONGATED HOLE ACCESS PANEL 463AL ON RH PYLON 2 EA. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON HOLE ACCESS PANEL 463AL ON RH PYLON 2 EA SECTION I AS PER ER/A 595258-14. (2016047)SDR DALA2021111206982None · noneSHIP 3359 PANEL 462CR OF THE RH PYLON WAS FOUND WITH WEAR DAMAGES IN THE INNER SIDE (3 INSTANCES). DAMAGES WERE EVALUATED AS PER A330 SRM 54-53-11-283-006. HOWEVER, P1 EXTENDS TO AN EXCLUDED AREA, TOGETHER WITH THE FACT THAT SAID REFERENCE DOES NOT PROVIDE INSSDR SWAA2022011052052Skin · delaminated#1 ENGINE IB THRUST REV MID TRAILING EDGE AREA DELAMINATED. 8-25 ; / [01] CUT OUT THE DAMAGED SKING A CIRCULAR SHAPE; NO CORE DAMAGED AT #1 ENG IB TRUST REVERSER MID TRAILING EDGE. REF B737-700 SRM 54-30-01-2R-1 PARAGRAPH 4 C (2). PREPARED AREA TO APPLY DRY OUSDR N6WA2021102205None · noneL/H PYLON SKIN AT FS 1099, UPPER #9 HI-LOC IS SHEERED. REMOVED FASTENERS, REAMED HOLE SIZE,NDT HOLES,INSTALLED NEW FASTNERS IAW REO 670-54-51-062SDR MASA20211022515Skin · damagedWEAR DAMAGE ON THE SKIN OUTER PANEL OF THE LOWER FAN COWL DOOR WHICH WAS SUBSEQUENTLY BLENDED OUT. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 54-14-01-001-A01, FIGURE 54-14-01-991-801, ITEM 1A, EA 80-2021-144.SDR SWAA2021111731793Access Panel · delaminatedNR 2 PYLON ACCESS PANEL 431ER EDGE DELAMINATED. PREPARED PANEL 431ER FOR REPAIR OF THE FIBER GLASS IAW SRM 51-70-062R-7. REPAIRED AT PANEL 431ER IAW SRM 51-70-06-2R-7. RESTORED FINISH AT #2 PYLON ACCESS PANEL 431ER IAW AMM 51-21-73-370-803.SDR DALA2021101206255None · noneSHIP 3306 SEVERAL DENTS WERE FOUND ON LH PYLON FORWARD FAIRING DOOR ASSY. 451CR & 451CL. DENTS WERE EVALUATED AND SOME OF THEM WERE FOUND OUT OF LIMITS DUE TO SHORT DISTANCE BETWEEN DENT EDGE AND MEMBER SUPPORT. CORRECTIVE ACTION: REF ER/A 594533-14. (1979434)SDR DALA2021101106227None · noneSHIP 3306 TWO DENTS WERE FOUND IN THE UPPER SURFACE OF THE FWD SIDE IN THE LH PYLON. DAMAGE HAS BEEN EVALUATED, RESULTING IN AN OUT OF LIMITS DUE TO SHORT DISTANCE BETWEEN DENT EDGE AND MEMBER SUPPORT. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS AS PER ERSDR CALA2021101101842Skin · corrodedTRANSCRIBED FROM HAECO GSO NR LP 9288730 (SUPPORT TASK) #1 PYLON PANEL 433JR CUTOUT INNER SKIN CORRODED REPAIRED SKIN PER HAECO REO G-23376 REV IR AND UAL EC/RA 5451-01 348 REV IR HAECO GSO MECH V899890 INSP QC340SDR DALA2021092805827None · noneSHIP 190 NACELLE STRUT ACCESS DOORS NO.2 PYLON INBD MISSING. CORRECTIVE ACTION: #2 ENGINE INBD NACELLE STRUT ACCESS DOOR. (LP 8092252)SDR DALA2021092005619None · noneSHIP 3357 ELONGATED HOLE ACCESS PANEL 453AR. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON ACCESS PANEL 453AR ON LH PYLON ASPER ER/A 594032-14. (1954186)SDR DALA2021092305719None · noneSHIP 190 RIGHT PYLON INBOARD ACCESS PANEL MISSING. CORRECTIVE ACTION: REPLACED NACELLE STRUT ACCESS DOOR ON #2 ENGINE. PLACARD/CDL REMOVED. (LP 8092228)SDR SWAA2021110917686Spar · corrodedLEFT HORIZONTAL STABILIZER; FRONT SPAR CLEVIS 'F' CORROSION ; / [01] SUMMARY EA 21-155-02692 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULT TTG8Q006HUND.; [02] SUMMARY EA 21-155-02692 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULTSDR HALA2021091300134Skin · crackedSHIP 390 TWO CRACKS WERE FOUND IN THE LIP SKIN OF #2 ENGINE INLET COWL. THE DRILL DEPTH OF THE CRACKS ARE OUT OF LIMITS. CORRECTIVE ACTION: ER/A 593988-14 TO BE ACCOMPLISHED. (1945228)SDR DALA2021091005373Access Door · missingSHIP 189 #1 ENGINE O/B NACELLE STRUT ACCESS DOOR MISSING. CORRECTIVE ACTION: FORWARD TO CDL 54-53-02 PLACARD INSTALLED.SDR DALA2021091005370Access Panel · missingSHIP 187 #1 PYLON IB ROUND ACCESS PANEL MISSING. FORWARD TO CDL 54-53-02. (LP 6383311)SDR UIEA2021083101921Screw · missing# 2 ENGINE I/B PYLON ACCESS PANEL MISSING SCREW(<P>REPLACED MISSING SCREW AT #2 ENG. I/B PYLON ACCESS PANEL IAW B767-3 SRM 57-40-02.</P>)SDR IPXA2021090773645Panel · crackedINSPECTION TYPE:A300PANEL 413BL HAS INTERNAL WEB CRACKED IN 1 AREA AS MARKED.FABRICATED DOUBLER IAW SRM 54-52-51.SDR DALA2021082505023Skin · damagedSHIP 6714 DURING REMOVAL OF #1 ENG MAINTENANCE NOTICED THE TOOLING WOULD NOT SEAT PROPERLY ON THE LH PYLON FWD BLKD, THE INBD AND OTBD SKINS ON THE PYLON EXTEND TO FAR PAST THE EOP. CORRECTIVE ACTION: ACCOMPLISHED TRIM OF I/B & O/B SKINS FWD EDGE ON L/H PYLON,SDR DALA2021082304959Skin · corrodedSHIP 6801 CORROSION ON LH (OUTBRD) CORE COWL, 6:00 O?CLOCK POSITION (AROUND LATCHES) AT ENGINE #1. (IN REFERENCE TO NRC 00308). CORRECTIVE ACTION: SUMMARY OF NRC 00447: LH (OUTBOARD) CORE COWL OF ENG. #1 WAS REPLACED PER. B757-200 AMM 71-11. (1917818)SDR DALA2021081704759Access Panel · damagedSHIP 3355 ELONGATED HOLE ACCESS PANEL 463AL AND 463AR RH PYLON (2 EA). CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR INSTRUCTIONS ON ACCESS PANEL 463AL AND 463AR ASPER ER/A #593331-14 PRI REV.0 AND REV.ORIGINAL. (1914612)SDR DALA2021081804792Access Panel · crackedSHIP 196 MAINTENANCE FOUND NO.2 PYLON ACCESS PANEL 426BR CUT OUT CRACK. CORRECTIVE ACTION: REPAIRED PER SRM 54-53-01. (LP 1913825)SDR CALA2021081801350Skin · crackedB767-54-3-7007 - NO.1 PYLON RH SIDE 436BR ACC PANEL CUTOUT FOUND CRACKED AS MARKED. REF N/R L/P 9130427. NO.1 PYLON RH SIDE 436BR ACCESS PANEL CUTOUT REPAIRED. AS PER EC RA 5451-01329 REV. ATTACH MAINTENANCE WORK SHEET FORM 44.0008 IT EM 1 TO 27 ACCOMPLISHED.SDR A6WA202109087871Skin · damagedNUMBER 2 ENGINE LOWER COWL HAS DAMAGE ON THE LOWER EDGE OF CORE BETWEEN XN170.73 AND XN176.5. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED DOUBLER REPAIR TO NUMBER 2 ENGINE LOWER COWL ON THE LOWER EDGE OF CORE BETWEEN XN170.73 AND XN176.5. P/N 228-50162-4SDR DALA2021082204940Panel · crackedSHIP 1707 DURING WALK AROUND FOUND RT NACELLE PANEL 447ELX CRACKED. REPAIRED PER ERA 593500-1. (LP 9794228)SDR DALA2021081704757Access Panel · damagedSHIP 3355 ELONGATED HOLE ACCESS PANEL 453AR AND ACCESS PANEL 453AL LH PYLON. PERFORMED PERMANENT REPAIR INSTRUCTIONS ON ACCESS PANEL 453AR AND 453AL ASPER ER/A 593330-14 PRI REV.0 AND REV. ORIGINAL. (1913064)SDR P5CA2021080900299Skin · damagedBROKEN - SKIN #2 ENG RH CORE COWL INTERIOR PRECOOLER EXHAUST DUCT L/E(<P>ACCOMPLISHED #2 ENG RH CORE COWL DAMAGE REPAIR REFER TO JOB CARD ATTACHING SHEET CONTROL NUMBER 0307488. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR SWAA2021082098970Skin · cracked#2 ENG. O/B FAN COWL SKIN HAS A CRACK AT AFT UPPER EDGE AREA. ; / CUT OUT CRACKED AREA AND REMOVED EXISTING FASTENERS ARUOUND DAMAGED AREA PER B737-700 SRM 51-10-02-0G-0 AND SRM 51-40-02-0G-0.VERIFIED; [03] PERFORMED HFEC INSP ON CUT OUT AREA. IAW B 737 NDT PASDR 2021F00179Skin · dented26.07.2021 21:36 SEVERAL DENTS IN LEFT ENGINE TRANSLATING SLEEVE OUTER SKIN. DURING TRANSIT CHECK, IT WAS DETECTED A DENT IN LEFT ENGINE TRANSLATING OUTER SKIN. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING DENT IN LEFT ENGINE TRANSLATING SLEEVE OUTER
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