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 U2RA202007110002Panel · damagedDURING ACCOMPLISHMENT OF TASK CARD 54-804-00-03, ENLARGED BOLT HOLE NOTED ON NUMBER 3 PYLON PANEL NUMBER 472ER. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER NUMBER 20298-8.SDR U2RA202010160007Skin · dentedDURING ACCOMPLISHMENT OF TASK CARD 71-802-01-04, DENT WITH GOUGES WAS NOTED ON THE SKIN OF NUMBER 4 ENGINE LEFT CORE COWL OUTER SURFACE AT NACELLE STATION 182.5. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20SDR U2RA202007100004Skin · chafedDURING ACCOMPLISHMENT OF TASK CARD 71-814-01-01, CHAFING WAS NOTED ON DOUBLER OF NUMBER 1 ENGINE LEFT CORE COWL INNER FACE AFT SIDE FRAME. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER 20316-10.SDR IPXA2020072988350Skin · crackedINSPECTION TYPE:4C, NR 2 PYLON LOWER AFT SECTION BOX INSTL. SKIN IS CRACKED BETWEEN STA. YID544.298 AND ZID 389.2 L/H SIDE.REPAIRED CRACKED #2 PYLON LOWER AFT SECTION BOX INSTL. SKIN L/H SIDE BETWEEN STA. YID 544.298 AND ZID 389.2 IAW EA 011-5430-01-A8430 REVSDR IPXA2020072458156Skin · damagedINSPECTION TYPE:2C#3 ENGINE NOSE COWL L/E SKIN HAS A DRILL START AT 6:00 POS.REPAIRED DAMAGED #3 ENGINE NOSE COWL L/E SKIN AT 6:00 POS IAW MD-11 SRM 54-15-02 REPAIR 1. (MINOR)SDR U2RA2020101612Skin · crackedDURING ACCOMPLISHMENT OF TASK CARD 54-812-00-01, CRACK NOTED ON NUMBER 1 ENGINE PYLON LEFT AFT FAIRING DOOR INNER SURFACE. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20316-9B.SDR U2RA202010160011Skin · crackedDURING ACCOMPLISHMENT OF TASK CARD 54-812-00-04, CRACK NOTED ON NUMBER 4 ENGINE PYLON LEFT AFT FAIRING DOOR INNER SURFACE. ACCOMPLISHED REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20316-9A.SDR IXXA20200720027Skin · crackedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE SCHEDULED VISIT. IN COMPLIANCE OF TASK CARD 71-834-00-01, "GVI - ZONAL - CORE COWL PANELS - ENGINE 1" THE FOLLOWING DISCREPANCY WAS NOTED: #1 OUTBD CORE COWL EXTERNAL SKIN CRACKED. CONFIRMED BY EDDY CURRENT. REMOVED ASDR SWIA2020082551985Skin · chafedRH ENGINE LOWER INNER CORE COWL INNER SKIN CHAFFED ON REPAIR. REMOVED AND FABRICATED NEW REPAIR DOUBLER PER CRJ 700 SRM, FABRICATED DOUBLER OUT OF AISI 321 CRES STAINLESS STEEL .010, LOCATED DRILLED AND INSTALLED WET WITH RED RTV -106 / AND RESTORED FINISH OSDR FDEA2020070631440Panel · crackedNR 2 PYLON PANEL 443JL CRACKED. RECEIVED NEW PANEL PART 311N5049-157.SDR DALA2020080652726Access Panel · crackedNR 1 ENGINE PYLON PANEL 471AL, OUTBOARD MID FASTENER CRACKED AROUND EDGE. COMPLIED WITH REPETITIVE INSPECTION OF NR 1 ENGINE PYLON PANEL 471AL OUTBOARD MID FASTENER. TEMP REPAIR WAS SPEED TAPE IAW SRM 54-50-00-283-005, FIG 10. PERFORMED PERMANENT REPAIR ONSDR IXXA20200720031Skin · crackedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE SCHEDULED VISIT. NR 1 OUTBOARD PYLON EXTERNAL SKIN IS CRACKED AT AFT UPPER CORNER OF PANEL 432AL CUTOUT. FABRICATED, LOCATED, DRILLED AND INSTALLED A DOUBLER, TRIPLER, FILLERS AND RUB STRIP IAW REA 42414REA08.SDR IXXA20200720032Skin · crackedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE SCHEDULED VISIT.SKIN CRACK AT NCC STA 211.75-237.5. REPAIRED SKIN CRACK AT NCC STA 211.75-237.5 COMMON TO THE NUMBER ONE STRUT OUTBOARD SKIN PANEL, USING AMES REPAIR DOCUMENT 47414REA08 REV 1R DATED 6-30-2020. APPROVED OSDR UIEA2020070201476Skin · corrodedCORROSION - SKIN, NR 2 PYLON LT CORE COWL UPPER REAR SKIRT FAIRING ACCESS PANEL 462XJL EXTERIOR SURFACE. REMOVED DAMAGED SKIN IAW SRM 51-40-02 REV 46. INSTALL NEW SKIN IAW SRM 51-40-02, 51-40-05, AND 51-40-08, REV 46, DWG NR 311U4570 SH 1 REV A. JOB COMPLETESDR FDEA202006281380Skin Panel · delaminatedNR 1 PYLON NACELLE I/B SIDE DOOR 433GR HAS DELAMINATED O/B SKIN AT TOP HINGE AREA AND INNER SEAL DETERIORATED. REPAIRED NR 1 PYLON PANEL 433GR PER SRM 51-70-17-OG,B757 DWG 311N5049 REV E.SDR SWIA2020072751420Skin · wornLEFT ENGINE UPPER TRANS COWL HAS COWL SLIDER WEAR AND RIDGES WORN. (C-CHECK) RO 7/23/2020 REPAIRED LEFT SIDE ENGINE UPPER TRANS COWL SLIDER REF MHI REO AND REO. . SEE CONTINUATION FOR DETAILS.SDR 2020F00301Doubler · corrodedNR 2 NACELLE STRUT DOOR (443LL) HAS CORROSION ON FWD BOTTOM CORNER ON DOOR LANDING. ACCOMPLISHED REPAIR IAW ENGINEERING ORDER CONTROL 20191, TITLED REPAIR-DOUBLER, INBOARD NACELLE SIDE SKIN PANEL ASSEMBLY NR 2 ENG, PPS 176.25.SDR IPXA2020072458180Skin · chafedINSPECTION TYPE:3C#3 ENG PYLON FWD APRON I/B SIDE IS CHAFED THROUGH SUPPORT BEAM AND APRON SKIN.REPAIRED APRON SKIN AND SUPPORT BEAM ON #3 PYLON FWD APRON I/B SIDE BETWEEN YWN=144.300 AND YWN=155 AND BETWEEN XWN=8.000 AND XWN=9.350 IAW EA 011-5410-01-A8374 REVSDR SWIA2020080751641Panel · chafed*LH ENGINE UPPER FAN COWL PANEL 432AT IS CHAFFED ON INNER SKIN AND STIFFENER. LH ENGINE UPPER FAN COWL INNER SKIN BLENDED AND FOUND WITHIN LIMITS IAW SRM. STIFFENER REPAIRED IAW SRM.SDR IPXA2020052635673Skin · corrodedINSPECTION TYPE:SEG 1 PYLON O/B ON LOWER WING SURFACE HAS BARE METAL AND PITTING CORROSION. REMOVED CORROSION IAW SRM 51-74-10. IN LIMITS SRM 57-20-12SDR IPXA2020052255627Skin · crackedINSPECTION TYPE:SEG3UPPER SKIN RH PYLON #8 HOLE HAS CRACK INDICATIONSREPAIRED PER EO BY REMAINING HOLE TO REMOVED DAMAGE B757-5720-76605-ASDR IPXA2020052055562Longeron · crackedINSPECTION TYPE:SEG#1 ENG AFT PYLON FAIRING 475AL HAS A CRACKED LONGERONREMOVED AND INSTALLED NEW LONGERON IAW SRM 51-40-21SDR CALA2020052200978Skin · crackedCRACK INDICATION NOTED ON HOLE # 10 AT R/W PYLON UPPER SKIN DRAG FITTING , CRACK POSITION 2 O''CLOCK , DEPTH APPROX < 0.030" REF AAR NR 9606729 REPAIRED HOLE #10 AT #2 PYLON UPPER DRAG FITTING PER EC/RA 5720-03191.INITIATE A DTA DIP LOGPAGE TO READ AS FOLLOWSSDR CALA2020052200977Skin · cracked2EA CRACKS INDICATION NOTED ON HOLE # 8 AT R/W PYLON UPPER SKIN DRAG FITTING , CRACK POSITIONS 2 O''CLOCK AND 7 O''CLOCK , DEPTH APPROX 0.030" < REF AAR NR 9606727 REPAIRED HOLE #8 AT #2 PYLON UPPER DRAG FITTING PER ECRA 5720-03191 .INITIATE A DTA DIP LOGPAGSDR CALA2020052200975Skin · crackedDURING NDT HFEC ROTO INSPECTION OF #1 PYLON UPPER DRAG FITTING IAW NDTM PART 6, 51-00-16 CRACK INDICATIONS WERE FOUND AT HOLE #10 - CRACK POSITION :- 4:0''CLOCK; CRACK DEPTH :-0.340"; CRACK SIZE :- 0.040" REF AAR NR 9606672 REPAIRED HOLE #10 PER ECRA 5720-0219SDR CALA2020052200979Skin · crackedCRACK INDICATION NOTED ON HOLE # 9 AT R/W PYLON UPPER SKIN DRAG FITTING , CRACK POSITION 11 O''CLOCK , DEPTH APPROX < 0.030" REF AAR NR 9606728 REPAIRED HOLE #9 AT #2 PYLON UPPER DRAG FITTING PER EC/RA 5720-03191.INITIATE A DTA DIP LOGPAGE TO READ AS FOLLOWSSDR IPXA2020052635657Panel · corrodedINSPECTION TYPE:C 1DISCOLORATION AND CORROSION ON THE INBD LWR PANEL ( P/N:323U8740-2 ) OF PYLON#1REPAIR I.A.W SRID:3-4724318089 AND EO B747-5450-76610-ASDR IPXA2020052635656Panel · corrodedINSPECTION TYPE:C1DISCOLORATION AND CORROSION ON THE INBD LWR PANEL ( P/N:323U8740-1 ) OF PYLON#4REPAIR IAW SRID:3-4724318305 AND EO B747-5450-76609-ASDR IPXA2020052635655Panel · corrodedINSPECTION TYPE:C1DISCOLORATION AND CORROSION ON THE INBD LWR PANEL ( P/N:313U8740-1 ) OF PYLON#3REPAIR I.A.W BOEING SRID:3-4724318505 AND UPS EO B747-5450-76611-ASDR FDEA202005180972Fairing · crackedPYLON NO.1 AFT FAIRING CRACKED AT HEATSHIELD JUST ABOVE DRAIN OUTLETS CRACKED FAIRING REMOVED IAW SRM 51-40-02, OVERSIZED HOLES FOUND ON FAIRING SUPPORT STRUCTURE, REPAIR CARRIED OUT IAW FEDEX EA # F-5430-T0353727 P1 TITLE NACELLES / PYLON- SKIN/ PLATES / SDR 2020F00302Doubler · corrodedNR 2 NACELLE STRUT DOOR (443LL) HAS CORROSION ON FWD BOTTOM CORNER ON DOOR LANDING. ACCOMPLISHED REPAIR IAW ENGINEERING ORDER CONTROL 20191, TITLED REPAIR-DOUBLER, INBOARD NACELLE SIDE SKIN PANEL ASSEMBLY NR 2 ENG, PPS. 176.25.SDR U2RA2020050430001Panel · missingNUMBER 4 ENGINE PYLON OUTBOARD SIDE DOOR PANEL MISSING. ACCOMPLISHED MAJOR REPAIR IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING INC ENGINEERING ORDER NUMBER 20159.SDR FDEA202004300860Access Panel · cracked#2 PYLON, OUTBOARD, HINGED PANEL 443AR, INNER SURFACE CRACKED. REPAIRED INNER SURFACE OF #2 PYLON, OUTBOARD, HINGED PANEL 443AR IAW B757 SRM 51- 70-17-0G RESTORED FINISH IAW B757 AMM 51-21-14 B757 AMM 51-21-15. MINOR REPAIRSDR UIEA2020040200654Access Panel · torn#4 PYLON ACCESS PNL #482BL INNER SURFACE CORNER FOUND TORN(<P>#4 PYLON ACCESS PNL #482BL INNER SURFACE TORN AREA PERFORMED METAL HOT BOND REPAIR AS PER RI #: RI-54-50-13970 REV A REV DATE 12MAR2020.</P>)SDR DALA2020033102102Skin · puncturedNO 1 PYLON AFT STRUT FAIRING O/B SIDE INNER SKIN FOUND PUNCTURE AT NAC STA 400. REPAIRED PER 51-70-10 (LP 1540384)SDR IPXA2020041754295Fairing · crackedINSPECTION TYPE:A300#2 PYLON LOWER AFT FAIRING 485AL CRACKEDREPLACED RIB AND CLIP IAW SRM 51-40-21SDR DALA2020032001972Access Door · dentedNO.1 ENG ACCESS DOOR 431AT UPR SURFACE FOUND DENT REPAIRED PER SRM 51-70-17. (LP 1532653)SDR SWAA2021082030975Panel · delaminatedRIGHT ENGINE PYLON PANEL DELAMINATED. PANEL # 441 BL MOD / C/W EA 1-754-2502 REV IR. ACCOMPLISH DVI INSPECTIONS TO ENSURE THERE IS NO DAMAGE PROPAGATION AND REPLACE SPEED TAPE AS REQUIRED. ACCOMPLISH PERMANENT REPAIR AS PER SRM 54-50-70 OR APPLICABLE PERMANENTSDR P5CA2020031900101Seal · brokenBROKEN - SEAL ASSY, NO. 2 PYLON AFTER FAIRING SIDE PANEL (PNL NO. 446CL) LOWER EDGE.(<P>IAW AMM 71-00-02-004-002 REV. 129 REMOVED THE PANEL NO. 446CL. REMOVED DAMAGED PARTS IAW SRM 51-40-02 REV. 112. INSTALL NEW PARTS IAW SRM 51-40-02 REV. 112 AND DWG NO. 311TSDR CALA2020032000645Access Door · missingPDA 2 STRUT ACCESS DOOR 436AR DISCOVERED TO BE MISSING FROM NO1 PYLON INBOARD POSITION. REF L/P 4626150 PLACED ON CDL DISPATCH DESK: 62 DATE: 27-FEB-20- RT PYLON PNL 436AR MISSING CDL COMPLIANT ITEM DISCOVERED PART NUMBER 311T3065-16, PAINTED, STENCILED AND INSDR DALA2022070604714None · noneSHIP 176 #2 ENGINE O/B NACELLE STRUT PRESSURE RELIEF DOOR IS MISSING. CORRECTIVE ACTION: REINSTALLED #2 ENGINE NACELLE STRUT PRESSURE RELIEF DOOR. OK FOR SERVICE. (7200848)SDR DALA2020030901716Paint · broken(AIRCRAFT 5648, L/P 1515411) BROKEN PAINT AROUND OF FASTENERS # 2,3,4,5,7,8,9, AND 10 AT LH ENG DRAG FTG LH PYLON. CORRECTIVE ACTION: REPAIR ON DRAG FTG LH PYLON WAS PERFORMED PER ETI-57-20-034 REV. 5 ER/A 585688-14 AD REV. ORIGINAL.SDR DALA2020022601418Skin · crackedMTC TASK-RH PYLON LEFT UPPER SKIN BTW NAC STA221 AND 237 FOUND FASTENER HOLE CRACK. RH PYLON LEFT UPPER SKIN BETWEEN NAC STA221 AND 237 FASTENER HOLE CRACKED AREA REPAIRED AS PER PRI585196-14AD REV.0. PRI585196-14AD REV.0 COMPARED AND COMPLIED WITH ER/A585196-SDR DALA2020022421368Skin · cracked(AIRCRAFT 674, L/P 1499351) LH WING #1 PYLON #2 HOLE HAS A CORROSION INDICATION AT 3 O CLOCK POSITION LOOKING AFT. INDICATION ON FITTING. AA# 5720-01100-0101A. CORRECTIVE ACTION: REPAIRED I/B AND O/B DRAG FITTINGS AND UPPER SKIN ON LEFT WING IAW ER/A# 585022-1SDR DALA2020022421367Skin · cracked(AIRCRAFT 674, L/P 1499344) LH WING #1 PYLON #5 HOLE HAS AN INDICATION IN THE CRACK INDICATION ZONE PER B757 NDTM 51-00-16 AT 9 OCLOCK POSITION LOOKING AFT. INDICATION ON FITTING. AA# 5720-01100-0101A. CORRECTIVE ACTION: REPAIRED LEFT WING I/B AND O/B DRAG FITSDR DALA2020022421366Skin · cracked(AIRCRAFT 674, L/P 1499333) LH WING #1 PYLON #10 HOLE HAS A CORROSION INDICATION AT 9 O CLOCK POSITION LOOKING AFT. INDICATION ON FITTING. AA# 5720-01100-0101A. CORRECTIVE ACTION: REPAIRED LEFT WING I/B AND O/B DRAG FITTINGS AND UPPER SKIN IAW ER/A# 585022-14ASDR DALA2020022421365Skin · cracked(AIRCRAFT 674, L/P 1499322) LH WING #1 PYLON #3 HOLE HAS 2 EA INDICATIONS IN THE CRACK INDICATION ZONE PER B757 NDTM 51-00-16 AT 3 AND 9 OCLOCK POSITION LOOKING AFT. 9 OCLOCK INDICATION ON FITTING AND 3 O CLOCK INDICATION IN UPPER SKIN. AA# 5720-01100-0101A. CSDR DALA2020022421364Skin · cracked(AIRCRAFT 674, L/P 1499317) LH WING #1 PYLON #4 HOLE HAS AN INDICATION IN THE CRACK INDICATION ZONE PER B757 NDTM 51-00-16 AT 3 OCLOCK POSITION LOOKING AFT. INDICATION IN FITTING. AA# 5720-01100-0101A. REPAIRED LEFT WING I/B AND O/B DRAG FITTINGS AND UPPER SKISDR DALA2020022101323Skin · cracked(AIRCRAFT 674, L/P 1498576) RH ENG. #2 PYLON #4 HOLE HAS A CORROSION INDICATION AT 5 OCLOCK POSITION LOOKING AFT. INDICATION IN THE TOP SKIN. CORRECTIVE ACTION: ACCOMPLISH ON ER/A 585020-14AD REV. O.SDR DALA2020022101322Skin · cracked(AIRCRAFT 674, L/P 1498567) RH ENG #2 PYLON #2 HOLE HAS 2EA INDICATIONS IN THE CRACK INDICATION ZONE ON THE X-Y DISPLAY PER B757 NDTM 51-00-16 AT 3 AND 9 O CLOCK POSITION LOOKING AFT. BOTH INDICATIONS IN THE TOP SKIN AA# 5720-01100-0101B. CORRECTIVE ACTION: AL
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