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 IXXA20241001001Skin · worn#2 ENGINE PYLON UPPER SKIN IS WORN IN SEVERAL SPOTS APPROX 9" AFT OF THE FWD EDGE. HAECO WO 320008 NON ROUTINE 40535SDR CALA2024082802307Skin · crackedPYLON #1 SKIN AT NACELLE L/E GAP PANEL INB LOWER CORNER NEXT TO WS260 WITH CRACK. REPAIRED PANEL IN LOWER CORNER NEXT TO WS 260 IAW B757-300 SRM 5 7-41-01-2R-3. REMOVED AND REINSTALLED THE GAP PANEL IAW B757 SRM 51-40-02-0G. OPERATIONAL TEST - DUCT LEAK DETECTSDR JR2R20240827940Panel · corroded429ABR HAS MULTIPLE SPOTS OF CORROSION ON PANEL LANDING. REPAIRED.SDR JR2R20240827935Panel · chafed419 CHAFED ON LOWER AFT SIDE OF PANEL. REPAIREDSDR JR2R20240827936Panel · chafed419NR HAS BARE METAL SPOT ON BACK OF PANEL. REPAIREDSDR IPXA2024090566979Skin · corroded#2 PYLON OUTBD INNER SKIN FWD OF THE VENT PANEL OPENING HAS CORROSION. DOT 8-004. VERIFIED, ACCOMPLISHMENT OF WORK PER UPS EO 91221-REQ 1 AND VT MAE EA 757-5450-27-A3676 REV. FAA 8100 APPROVAL ATTCHED.SDR DALA2024080807891Web · gougedSHIP 3149 GOUGE WEB ON UPPER AREA AT LEVEL RIB09 IB AND OB SIDE ON LH PYLON. CORRECTIVE ACTION: REPAIRED PER ER/A 619728-14. (0489696)SDR IPXA2024091406967Skin · dented(STR) #2 ENG NOSE COWL OUTER SURFACE HAS MULTIPLE DENT AS MARKED. 74-005 ATA CODE 71. INSTALLED #2 ENG NOSE COWL 1EA ACCESS PANEL AT 2 OCLOCK POSITION REF. BOEING MD 11 SRM 51-31-01-0G-0 TW: ID: 21-515 DUE: 28-NOV-2024 AND SEALED REF.BOEING MD 11 SRM 51-41-01-SDR CALA2024080902182Access Panel · missingPDA 2 REF LP 8839646 PANEL #446AL MISSING ON #2 IB STRUT. OK TO CONTINUE.SDR SWAA2024080920650Panel · delaminatedDELAM FOUND ON FWD LOWER CORNER OF PANEL 434AR<[01] 04 - REPAIRED PER [SRM 54-50-70-2R-3-D01231 (REPAIR 3 - ENGINE STRUT AFT FAIRING SKIN PANELS-PERMANENT)];[02] C/W<BR>AUDIT C/WSDR SWAA2024072918588Skin · pulledNO 1 ENGINE INLET COWL OUTER BARREL INBD SKIN HORIZONTAL SEAM HAS PULLED THROUGH FASTENER ON UPPER SKIN LOCATED FOURTH FROM AFT SIDE OF BARREL.<[01] COMPLIED WITH EA 24-171-02074. REFERENCE TSR 2024005276.SDR JR2R20240727413Panel · chafedLH PYLON PANEL 419UR HAS CHAFING ON INTERIOR SURFACE. REPAIREDSDR SWAA2024082617345Skin · cracked# 1 PYLON REQUIRES REMOVAL FOR THE REPAIR OF LOWER THE SUPPRESSOR SKIN CRACK<[01] REMOVED #1 PYLON (STRUT FAIRING) FOR FOM PER AMM 54-52-04.;[02] INSTALLED #1 ENGINE AFT PYLON PER AMM 54-52-04.;[03] VERIFIED 2. DANIEL TAYLOR (TECHNICIAN); 13-AUG-2024 16:43 UTCSDR IPXA2024081487080Skin · corrodedNR 1 I/B FWD PYLON SKIN HAS CORROSION AT INTERNAL AND EXTERNAL SURFACE. JOB HAS BEEN ACCOMPLISHED PER UPS EO-91010-REQ1 AND VT MAE EA 757-5450-27-A3658 REV- WITHOUT ANY DEVIATIONS.SDR CALA2024072502100Skin · crackedNO.1 PYLON STA 231 UPPER SPAR ELECT CABLE CUTOUT SKIN FOUND CRACKED TRANSFER REF. NON-ROUTINE HX NRC WO.3334709. NO.1 PYLON STA 231 UPPER SPAR WEB CUTOUT AT NAC STA 231 INTERIM REPAIR AS PER EC/RA 5450-02942 REV ORIG PART 1 ITEM A AND CREATED DIP L/P 8704630.SDR IXXA202400724003Skin · chafedSEVERAL CHAFFE MARKS IN THE UPPER SURFACE OF THE PANEL, ON TOP OF THE RIGHT PYLON, WHERE THE FWD FAIRING 441AT (DOGHOUSE PANEL)SDR IXXA20240724001Skin · chafed#1 PYLON FWD NACELLE STRUT FAIRING UPPER SKIN IS CHAFED IN 4EA SPOTS LOCATED JUST AFT OF THE INLET AT THE 12:00 POSITIONSDR CALA2024071800242Access Panel · missingPDA 2 R/H ENGINE STRUT PRESSURE RELIEF DOOR/ACCESS PANEL 443CL FOUND MISSING ON ARRIVAL. PHOTO ADDED. NIL STOCK LHR. CDL APPLIED. DISPATCH DESK: 67 NAME: AC DATE: 19-MAR-24- OK TO PLACE PDA 2 R/H ENGINE STRUT PRESSURE RELIEF DOOR/ACCESS PANEL 443CL FOUND MISSDR IPXA2024083060457Skin · corrodedNR 2 ENGINE INBD PYLON INNER SKIN AFT OF THE FWD HINGE PANEL HAS EXFOLIATION CORROSION. DOT 8-006 AND IN RED. COMPLETED REPAIR IAW EO-90940-REQ 1 AND EA 757-5450-27-A3651. REPAIRED #2 I/B SKIN IAW EO-90940 REQ1 & EA 757-5450-27-A3651A REV -. AUDIT COMPLETE.SDR IPXA2024081860457Skin · corrodedNR 2 ENGINE INBD PYLON INNER SKIN AFT OF THE FWD HINGE PANEL HAS EXFOLIATION CORROSION. DOT 8-006 AND IN RED. VERIFIED PARTS. OPENSDR IPXA2024081260701Skin · corrodedNR 1 ENGINE INBD PYLON INNER SKIN AFT OF THE FWD HINGE PANEL HAS EXFOLIATION CORROSION, DOT 8-004. AUDIT COMPLETE. OPENSDR IPXA2024081760669Skin · corrodedNR 1 ENGINE INBD PYLON INNER SKIN AFT OF THE SQUARE PANEL OPENING HAS EXFOLIATION CORROSION. DOT 8-003. ACCOMPLISHMENT OF E.O. AS PER UPS EO-90941-REQ1 AND VT-MAE EA 757-5450-27-A3650, REV. -. WITHOUT ANY DEVIATIONS.SDR CALA2024071800243Access Panel · missingPDA 2 ON AIRCRAFT ARRIVAL, LEFT ENGINE INBOARD PYLON PANEL 436AR MISSING. REPORTING SDR FOR PDA 2.SDR DALA2024071607172Skin · crackedCRACK ON EXTERNAL SKIN AT APRON, FIVE INCHES FWD OF LOWER AFT CORNER APROX RH ENGINE. SUMMARY OF NRC 00268: EXTERNAL SKIN AT APRON, FIVE INCHES FWD OF LOWER AFT CORNER APROX RH ENGINE WAS REPAIRED PER B717-200 SRM 54-50-01-2R PRCEDURE 2, REPAIR 2. (LP #0449618SDR VNAA202508200025Skin · dentedDISCREPANCY: DENT ON INLET COWL AT 6 O´CLOCK POSITION AT LH ENGINE PREVIOUSLY MARKED AND WHITOUT TRACKING FOR PSA. DENT ON INLET COWL AT 6 O´CLOCK POSITION AT LH ENGINE PREVIOUSLY MARKED AND WHITOUT TRACKING FOR PSA WAS REPAIRED PER REO 690-54-11-560 REV- ANSDR VNAA20250820004Skin · dentedDENT ON INLET COWL SKIN AT 6 O'CLOCK POSITION LH ENGINE. DENT ON INLET COWL SKIN AT 6 O'CLOCK POSITION LH ENGINE WAS REPAIRED PER REO 690-54-11-560 REV- - AND PER 670-54-11-1108 REV. NC.SDR IXXA20240708002Skin · chafed#1 PYLON FWD NACELLE STRUT FAIRING UPPER SKIN IS CHAFFED IN 4EA SPOTS LOCATED JUST AFT OF THE INLET AT THE 12:00 POSITIONSDR IXXA20240708001Skin · chafedTHERE ARE SEVERAL CHAFFE MARKS IN THE UPPER SURFACE OF THE PANEL, ON TOP OF THE RIGHT PYLON, WHERE THE FWD FAIRING 441AT (DOGHOUSE PANEL) HAS CHAFFED INTO THE SKIN.SDR CALA2024071001999Skin · crackedB767-54-3-0008 #1 PYL PNL 436BL CUTOUT SKIN FOUND CRACKED. TRANSFER REF. NON-ROUTINE WO.3277610 NR 1 PYLON LH SKIN NO.436BL ACCESS PANEL CUTOUT PERMANENT REPAIRED AS PER EC/RA 5450-02947 REV.- ATTACHED FORM 44-0008 ITEM 1 TO ITEM 33.SDR SWAA2024081308035Skin · corroded#1 ENGINE INLET COWL HAS CORROSION ON BARREL SKIN 1 INCH AFT OF THE INLET LIP AT 12 O'CLOCK POSITION. MARKED<[01] #1 ENGINE INLET COWL REPLACED (FAULT WAS RESOLVED ON ANOTHER FAULT) TTG8Q00S70S4;[02] VERIFIED CORRECTIVE ACTION #1SDR HNAA2024071900574Skin · damaged71-2123 PROFILE DAMAGED ABOVE OF AIR STATER VALVE ACCESS DOOR BTWEEN XN3167.5 AND XN2905.0. RAR PROFILE IAW SRM 51-40-02SDR IPXA2024071941894Skin · crackedLEFT PYLON HAS A CRACK ABOVE INBD SERVICE PANEL, ABOUT 1.5 INCHES LONG. MARKED. ALL REPAIR STEPS ACCOMPLISHED PER EO-90663-REQ2. LEFT ACCESS DOOR REINSTALL ADDRESSED ON T3F18E004TVDV. SHEETMETAL REPAIR IS COMPLETE.SDR IPXA2024061441894Skin · crackedLEFT PYLON HAS A CRACK ABOVE INBD SERVICE PANEL, ABOUT 1.5 INCHES LONG. MARKED. PERFORMED CONDUCTIVITY TEST ON CORD MATERIAL 7075 T6XXX IAW NDT 51-00-00. ALL 4 CORDS WERE CONSISTENT WITH A IAC OF 33. OPENSDR MK1Y20240602012Skin · damagedREPAIR - ENG #1 LH CORE COWL EXISTING BLEND OUT STRAP, P/N 314T3210U261.SDR SWAA2024061491767Skin · crackedCRACK ON OUTBOARD FAN COWL SKIN 1 INCHES OF UPPER EDGE AND 2 INCHES OF FWD EDGE ENG 1 2024-340205<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30; S/N: B23379002; DUE DATE: 18-FEB-25.;[02] TOOL USED EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600D; S/N: 220272712; DSDR CALA2024053001648Skin · crackedGEN ITEM: 63-5410-1-2501 #1 PYLON O/B SIDE ACCESS 436BL PYLON SKIN CRACKED FWD UPPER CORN ER & AFT CHAFE STRIP IS LOOSE/DAMAGED UPPER & LWRSDR IPXA2024062084697Doubler · crackedFAULT- #2 ENGINE PYLON OUTBD ACCESS HOLE INNER SKIN HAS A CRACK GOING THRU HILOK AT THE 3 0CLOCK POSITION. REMOVED 2EA FASTENERS IAW SRM 51-40-02-0G AND CRACK EVALUATED IAW SRM 54-51-01-1A-1 ALLOWABLE DAMAGESDR UIEA2024052500443Skin · crackedNO.3 ENG - RH CORE COWL AFT EDGE EXTERNAL SKIN CRACK FOUND AT CENTER AREA AS MARKED(<P>NO.3 ENG - RH CORE COWL AFT EDGE SKIN REPAIRED IAW EA NO : EA-1971A099 REV 0. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052500445Skin · crackedNO.3 ENG - RH CORE COWL EXTERNAL SKIN CRACK FOUND JUST BELOW THE EXHAUST LOUVER AS MARKED(<P>REPAIRED IAW SRM 54-45-01-2R-4 REPAIR 4. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052400438Skin · corrodedPYLON #1 UPPER SURFACE, CORROSION DAMAGE ON THE BUSHING OF THE INBD LUG OF FWD UPPER SPAR FITTING.(<P>REPAIR FOR CORROSION DAMAGE ON THE BUSHING OF THE INB LUG OF FWD UPPER SPAR FITTING WAS ACCOMPLISHED IAW TRE 6754190 ISSUED DATE MAY 16,2024. FAA FORM 8100-9 SDR CALA2024060301685Skin · crackedDURING THE INSPECTION, IT WAS FOUND A CRACK ON THE ACCESS PANEL 436BR ON THE PYLON #1 INBOARD SIDE. ACCOMPLISHED REPAIR AS PER SRM 54-53-01-2R-7 FIG 201 DETAIL 1.SDR CALA2024060301683Access Panel · crackedACCESS PANEL 446BL HAS A CRACK AROUND THE CUT OUT PYLON #2 ON THE INBOARD SIDE.SDR JR2R20240525446Panel · chafedRH PYLON PANEL 419ML CHAFED. REPAIRED.SDR IXXA2024061402Skin · gouged#2 PYLON SKIN AND BULLNOSE PANEL 441AT RUBBING AND CAUSED GOUGES ON THE SKIN AT THE FORWARD EDGESDR NACA2024051200001Skin · crackedFOUND RH PYLON IB SKIN CRACK AT NAC STA 170.78 BELOW PANEL 442 AL. THE CRACK LENGTH IS 1.4". RH PYLON INBOARD SKIN CRACK REPAIRED IAW EO 767-54-0007SDR COEA2024051415759Access Panel · crackedDURING A SCHEDULED MAINTENANCE INSPECTION, CRACKS WERE DISCOVERED ON THE L/H ENGINE AFT INBOARD ACCESSORY PANEL 421CR. A TEMPORARY REPAIR WAS PERFORMED ON THE L/H ENGINE AFT INBOARD ACCESSORY PANEL PER TEXTRON REF: DQ44226M1. REPLACED THE L/H ENGINE AFT INBOASDR IXXA2024050101Panel · cracked#1 OB STRUT PANEL CRACKEDSDR IXXA2024041704Skin · cracked#1 ENGINE INBOARD CORE COWL OUTER SKIN CRACKED.SDR AALA202404176083Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: PANEL 441EL EDGE HAS DELAMINATION. ACCOMPLISHED PERMANENT REPAIR ON PANEL 441EL. PER B737-NG SRM 54-50-70-2R-2.SDR AALA202404178451Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: PANEL 431ER EDGE HAS DELAMINATION. ACCOMPLISHED PERMANENT REPAIR ON PANEL 431ER. PER B737-NG SRM 54-50-70-2R-2.
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