JASC 5400
Service difficulty reports · 1,907
Reports filed under 5400 · Nacelle/Pylon Structure, 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 = '5400' 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 = '5400' 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 IPXA2023040792711Skin · corrodedINSPECTION TYPE:C13#2 ENG PYLON O/B AFT SKIN WITH CORROSIONREPAIRED PER VTMAE EA# 757-5450-27-A3185 REV- AND UPS EO# B757-5430-86514-ASDR IPXA2023040792713Skin · corrodedINSPECTION TYPE:C13#1 ENG PYLON I/B AFT SKIN WITH CORROSIONREPAIRED PER VTMAE EA# 757-5450-27-A3186 REV- AND UPS EO# B757-5430-86513-ASDR HYIA20230321001Fitting · crackedDURING SCHEDULED NDT INSPECTION AS NOTED IN SID 57-10-16, A CRACK WAS NOTED ON THE LEFT HAND INBOARD NACELLE FITTING P/N: 5292029-21. THE CRACK MEASURES .125 INCHES LONG AND IS CONSISTENT WITH OTHERS FOUND USING THE LIGHTED BORESCOPE INSPECTION TECHNIQUE (TEXTSDR SWAA2023032017188Bracket · crackedNO.1 ENG AFT STRUT FAIRING AFT OUTBOARD BRACKET CRACK FOUND CRACK LOCATED IN THE AFT STRUT FAIRING AFT OUTBOARD BRACKET<[01] COMPLIED WITH EA 23-154-00886 REF TTG8Q00JVBTPSDR FDEA202303160448Fitting · cracked#1 PYLON, UPPER SKIN, DRAG BRACE ATTACH FITTING, HOLE #4 HAS BEEN REAMED TO 1ST OVERSIZE, AT 0.5770 NDT IS STILL RECEIING CORRROSION INDICATIONS. WORK ACCOMPLISHED PER E.A.# F-5740-T0373301 P1, EA TITLE WINGS-ATTACH FITTINGS-LH WING, UPPER SKIN, DRAG FITTISDR GTIA2023031437041Profile · crackedCRACK FOUND ON PYLON #2 1B PROFILE RIB 4-7. RAF-01 2857333-02 CREATED.-VERIFIED NR # 5001220618-0010;0030 AND TC # 1003947071-0010. REPAIR HAS BEEN ACCOMPLISHED I.A.W SPIRIT EA 5457-2305 REV. 00.SDR EE4Y2023031017379None · corrodedDURING INSPECTION #1 ENGINE LH PYLON AFT MOVABLE FAIRING ACCESS PANEL 477AL, FIXED CUTOUT INTERNAL AFT LOWER CORNER WITH CORROSION WAS FOUND.PERMANENT REPAIR WAS PERFORMED IAW A319 SRM54-55-12-300-006 FIGURE 001 SHEET 1 AND SHEET 2 REV 140 DATED 02-01-2022. THSDR YENA2023031400235Unknown · unknownDURING HEAVY MAINTENANCE: THE LEFT INBD PYLON SPAR CRACKED; REF TOMX NRC 00283 WO 2162 INBD SPAR AT LH PYLON WAS REPLACED PER EMB-190 SRM 51-43-03 AND SRM 51-43-04, ETI-190-23-516 REV. 2, ETD2023-190-003959 REV. A & E23-131-01.'SDR MK1Y20230305020None · noneENGINE #2 – LH CORE COWL, NAC STA 264.50, UPPER CORNER EDGE: DURING MAINTENANCE INSPECTION, SHOP FOUND A 0.9" LONG CRACK ON AN INCOMING REPAIR AT THE NOTED AREA. IN ADDITION, THE EXISTING REPAIR CONFIGURATION IS MISSING SEAL-FLEX P/N S700S1310-1, FILLER P/N 22SDR MK1Y20230305019None · noneENG #2 FAN COWL OUTER SKIN: 8 (EIGHT) DENTS WERE FOUND WITH CLOSE GAPS IN THE OUTER SKIN OF THE ENG #2 FAN COWL, ON THE OUTBD SIDE BT 4 O'CLOCK TO 5 O'CLOCK.SDR 2023FA0000110None · noneFOUND MULTIPLE WELDING REPAIRS ON ENGINE #1 BETWEEN 2-6 O'CLOCK ON EXHAUST OUTER FACE SHEET.SDR 2023FA0000109None · noneFOUND MULTIPLE WELDING REPAIRS ON ENGINE #1 BETWEEN 2-6 O'CLOCK ON EXHAUST OUTER FACE SHEET.SDR 2023FA0000108None · noneFOUND WELDING REPAIR BETWEEN 2-8 O'CLOCK ON ENGINE #2 EXHAUST NOZZLE OUTER SLEEV OUTER SKIN.SDR MK1Y20230305016None · noneENGINE #2 CF6-80C2B6F, EXHAUST, NAC STA 332.34 AND NAC STA 360.73: SHOP FOUND A DENT WITH SHARP CREASE ON THE EXTERNAL EXHAUST SKIN LOCATED ON ENGINE 2 NAC STA 332.34, BT 6 TO 5 O’CLOCK. SIZE: L=0.50”, Y=0.020, A=0.47 A/Y=23. IN ADDITION, SHOP FOUND ANOTSDR MK1Y20230305015None · noneENGINE #2 CF6-80C2B6F STRUT, AFT FAIRING PANEL ASSY, BETWEEN NAC STA 304.54 AND NAC STA 308.00: SHOP FOUND AN EXISTING REPAIR ON THE OUTBD SIDE OF STRUT #2 IN THE OUTER SKIN PANEL LOCATED BELOW ACCESS DOOR BT NAC STA 304.54 TO 308.00. SIZE OF THE REPAIR: 3.5"XSDR MK1Y20230305013None · noneENGINE # 2 OUTBD CORE COWL SKIN: DURING MAINTENANCE INSPECTION AT IAI FOUND UNDOCUMENTED DOUBLER REPAIR ENG # 2 OUTBD CORE COWL AROUND FWD LATCH CUTOUT BT NAS STA 264.37 TO 270.57 AT 6 O’CLOCK.SDR MK1Y20230305012None · noneENGINE #2 INBD CORE COWL SKIN: DURING MAINTENANCE INSPECTION AT IAI FOUND EXISTING HAT FRAME REPAIR NOT ACCORDING TO SRM ON INBD CORE COWL ENG #2 NAC STA 303.75 BT 11 TO 12 O’CLOCK.EXTERNAL DOUBLER SIZE: 1.7”X7.1”. ENGEL PATCH SIZE: 6”X4” APP. P/N: 224-2301-51SDR MK1Y20230305011None · noneENGINE #2, BT NAC STA 268.7 TO 303.7 AND BT 9 TO 10 O'CLOCK: DURING MAINTENANCE INSPECTION SEVERAL SCRATCHES DAMAGE WERE FOUND ON CORE COWL SKIN. FASTENERS REMOVED, AND INSTALLED AFTER THE AREA WAS BLENDED PER SRM 51-40-02. SMOOTHING WAS PERFORMED IN THE AREA SDR MK1Y20230305010None · noneENGINE #1 OUTBD CORE COWL SKIN: DURING MAINTENANCE INSPECTION AT IAI FOUND TWO EXISTING UNDOCUMENTED DOUBLER REPAIRS ON OUTBD CORE COWL. M0149 – LOCATED NAC STA 268 TO 283 AT 6 O'CLOCK SIZE 15"X4.8". M0151 – LOCATED NAC STA 303.75 BT 11 TO 12 O'CLOCK SIZE 1.6"SDR MK1Y20230305009None · noneSTRUT FAIRING SKIN, INBD SIDE: EXISTING UNDOCUMENTED 2.8"X1.4" DOUBLER REPAIR ON THE INBD SIDE OF STRUT FAIRING SKIN BELOW DOOR PANEL BT STA 304.54 – 307.34.SDR UIEA2023022300180None · noneENGINE #1, INLET COWL LIP SKIN WAS FOUND WITH GOUGE OUT OF LIMITS AT 8 O CLOCK POSITION(<P>IT WAS REPAIRED PER COLLINS REPAIR FORMAT #CV23-01267-REPAIR AND BOEING SR 4-5692112122.</P>)SDR UIEA2023022300182None · noneLH PYLON - UPPER SKIN - WEAR DAMAGE BETWEEN NAC STA 149.43 TO NAC STA 139.73 FOUND OUT OF LIMITS (IT WAS EXCEEDED THE MAXIMUM DEPTH).(<P>IT WAS REPAIRED PER BOEING SR 4-5704143162</P>)SDR FDEA202303030370Spar · crackedRH PYLON LWR SPAR FOUND CRACK BETWEEN RIB6 AND RIB7 AT STIFFENER END BY EDDY CURRENT INSPECTION COMPLID WITH EA: 6-5450-T0373394 P1. TITLE: NACELLES/PYLON - WING PYLON/STRUT - #2 ENGINE PYLON LOWER SPAR CRACK BETWEEN RIB 6&7 - REPAIR. REPAIRED THE RH PYLONSDR FDEA202303030368Panel · crackedLH PYLON O/B SIDE PANEL AT RIB8 FOUND 1EA CRACK. REPAIRED THE CRACKED LH PYLON O/B SIDE PANEL AT RIB8 PER EO: 6-5450-7-5003 I PT3 & A300-600 SRM54-51-31-201-2. EO TITLE: NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB8. AIRBUS SB A300-54-6015 R03 SDR FDEA202303030367Panel · crackedLH PYLON I/B SIDE PANEL AT RIB8 FOUND 1EA CRACK. REPAIRED THE CRACKED LH PYLON I/B SIDE PANEL AT RIB8 PER EO: 6-5450-7-5003 I PT3 & A300-600 SRM54-51-31-201-2. EO TITLE: NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB8. AIRBUS SB A300-54-6015 R03 SDR 2023F00073Firewall · crackedWHILE CHANGING #1 ENGINE MOUNTS A CRACK WAS FOUND IN THE PYLON FIREWALL.SDR CALA2023030300606Fastener · missingPDA 3 REF L-P3899302 FASTENER MISSING ENG2 PYLON OUTER PANEL 482AR. REPLACED FASTENER REF IPC 54-53-11-01A, TOMC ANDERSON NOTIFIED.SDR CALA2023030300604Fastener · missingPDA 3 1 FASTENER MISSING FROM EACH LOGPAGE 3778276 (PANEL414FR), 3778267 (PANEL482AR), 3778271 (PANEL414AR)AND 3778263 (PANEL192FB). ALL FASTENERS REPLACED ON THE RESPECTIVE PANELS. TOMC NOTIFIED.SDR SWAA2023032821494Flange · crackedRIGHT # 2 ENGINE INBD T/R FRONT FLANGE CRACKED AT 10 O'CLOCK POSITION<[01] REPAIRED #2 ENGINE INBD T/R PER EA# 23-178-00707. REFERENCE LINE #764 OF THIS WORK ORDER FOR DETAILS.;[02] INSPECTION C/W REPAIRED #2 ENGINE INBD T/R PER EA# 23-178-00707. REFERENCE LINSDR UIEA2023022600193Panel · noneNO.3 PYLON ACCESS PANEL 472EL FASTENER HOLE FOUND WORN(<P>NO.3 PYLON ACCESS PANEL 472EL P/N: 311U2060-137 FABRICATED AND REPLACED IAW RI-54-00-16085 REV.A</P>)SDR FDEA202303010357Skin · corrodedRIGHT WING PYLON UPPR FITTING #2 HOLE HAS CORROSION IN SKIN AT 3 O'CLOCK POSITION. 1) PERFORMED REPAIR OF SKIN ON R/H WING UPPER PYLON FITTING HOLE #2 IAW SRM 57-20- 01-2A REPAIR 8 & EA # F-5730-T0372934 A P1 WINGS - PLATES AND SKINS - RH WING, UPPER SKIN ASDR SWIA20230503228Unknown · crackedEVALUATE POSSIBLE CRACK ON LEFT ENG. PYLON CANTED RIB. (MARKED) (C-CHECK RO 4/30/2023) REMOVED AND INSTALLED 1 EA NEW LOWER DRAG BRACE ON LH ENGINE PYLON PN 601-37030-1 PER CRJ 200 SRM 51-42-21 AND DWG # 601-37003 REV T. SEE CONTINUATION FOR FURTHER DETSDR SWAA2023040711125Panel · elongatedELONGATED HOLE ON PLATE LOCATED ON ACCESS PANEL 431AT LT PYLON (2 E/A ) 2023-142871<[01] REPLACED PLATE LOCATED ON ACCESS PANEL 431AT LT PYLON (2 E/A ) IAW B737-700 SRM 51-10-02;[02] REPLACED PLATE LOCATED ON ACCESS PANEL 431AT LT PYLON (2 E/A ) IAW B737-700 SSDR SWAA2023032010748Panel · delaminatedNO-2 PYLON STRUT PANEL 441EL EDGE DELAMINATED MKD<[01] MEASUREMENTS;[02] REPAIRED EDGE DAMAGE AT #2 PYLON STRUT PANEL #441EL AS PER BOEING &37 SRM 51-70-04-2R-6.MATERIAL USED EY3804 PO# 1799597;RESTORED ORIGINAL FINISHED.;[03] VERIFIED STEP 2SDR CALA2023022700560Cowling · missingPDA 2 MISSING MASTER CHIP DETECTOR ACCESS PANEL 424CR ON ENG 2. DIMENSIONS 5X7 INCHES. AIPC REF 71-11-04. REMOVED AND REPLACED ENGINE #2 FAN COWL RH OUTBOARD PER EC/RA #5420-01600. REF AMM 71-11-04.SDR IPXA2023032592234Bracket · brokenINSPECTION TYPE:CPYLON L/H REAR SIDE BRACKET BROKENREMOVED, FABRICATED, AND REPLACED IAW SRM 57-26-10 AND SRM 51-40-21SDR A6WA202302268507Bonding Plate · corrodedL/H UPPER PYLON TRAILING EDGE BONDING PLATES HAVE CORRODED FASTENERS. ******AIRCRAFT REMOVED FROM SERVICE********** REMOVED 12 RIVETS FROM LH UPPER PYLON BONDING PLATES IAW CRJ-200 SRM 51-42-13 INSTALLED 12 RIVETS IAW CRJ-200 SRM 51-42-13 REPLACED LH UPPER BONSDR A6WA202302268489Plate · corrodedL/H LOWER PYLON TRAILING EDGE BONDING PLATES HAVE CORRODED FASTENERS. ******AIRCRAFT REMOVED FROM SERVICE********** REMOVED AND REPLACED LH LOWER BONDING PLATE IAW AWAC SUPPLEMENT NO: 15-335.SDR EE4Y2023022417258Fairing · damagedDURING THE STRUCTURAL INSPECTION WAS FOUND AT ENGINE #1 AFT PYLON MOVABLE FAIRING INBOARD SKIN WITH CRACK AND SEVERAL FAIRING ATTACHMENT HOLES ELONGATED.WAS REPAIRED FOLLOWING EMBRAER REPAIR INSTRUCTIONS UNDER ETD2023-190-001051 REV / AND APPROVED ON ANAC F-20SDR EE4Y2023022417256Fairing · damagedDURING THE INSPECTION PROCESS, IT WAS FOUND AN EXISTING REPAIR WITHOUT RECORDS. WAS REPAIRED FOLLOWING EMBRAER REPAIR INSTRUCTIONS UNDER ETD2022-190-036364 REV / AND APPROVED ON ANAC F-200 FORM PROVIDED BY EMB.SDR EE4Y2023022417250Fairing · damagedDURING THE STRUCTURAL INSPECTION, IT WAS FOUND AN EXISTING REPAIR LOCATED AT ENGINE #2 AFT PYLON MOVABLE FAIRING.
SINCE THE PREVIOUS OPERATOR DID NOT PROVIDE REPAIR RECORDS, IT WAS REMOVED IN ORDER TO PERFORM A NEW ONE
FOLLOWING REPAIR INSTRUCTIONS UNDER ETDSDR EE4Y2023022417246Lug · corrodedDURING THE ACCOMPLISHMENT OF SB, FOUND THE RH PYLON, INBOARD AND OUTBOARD SPARS LUGS BUSHING WITH CORROSION. WAS REPAIRED FOLLOWING EMBRAER REPAIR INSTRUCTIONS UNDER ETD2022-190-037426 AND APPROVED ON ANAC F-200 FORM PROVIDED BY EMB.SDR EE4Y2023022417245Fairing · damagedDURING THE STRUCTURAL INSPECTION, IT WAS FOUND AT ENGINE #1 AFT PYLON MOVABLE FAIRING SKIN WITH CRACK. WAS REPAIRED FOLLOWING EMBRAER REAPAIR INSTRUCTIONS UNDER ETD2022-190-037760 REV A AND APPROVED ON ANAC F-200 FORM PROVIDED BY EMB.SDR IPXA2023030491514Skin · corrodedINSPECTION TYPE:SEG1#2 ENGINE PYLON INBD SKIN AT THE FWD HINGE DOOR INNER AFT LIP HAS A EXFOLIATION CORROSIONCORROSION FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED THE #2 ENGINE PYLON INBD FWD SKIN PER SRM 51-40-02SDR DALA2023022101261None · noneAIRCRAFT 3155, UPPER PYLON FORWARD FAIRING ON L ENGINE MISSING. CORRECTIVE ACTION: INSTALLED COVER IN PLACE IAW ER/A 606310-14 REV ORIGINAL SECTION I. (LP 4077852)SDR DALA2023022201322None · noneCORROSION ON L-22LH, Y STA 845 AT FILLET FAIRING STRUCTURE. SUMMARY OF NRC 00277: CORROSION LEVEL 2. LONGERON STA 845 STR 22LH WAS REPLACED PER DWG 5911420 REV: AE AND B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2636166)SDR IPXA2023030591540Skin · corrodedINSPECTION TYPE:SEG1*MAJOR REPAIR* #1 ENGINE OUTBD PYLON SKIN OF VENT 433CL OPENING HAS EXFOLIATION CORROSION ON THE INNER SKINREPAIR PER UPS RCD 271422 AND VT MAE EA 757-5450-27-A3154 REV-SDR IPXA2023030391502Skin · corrodedINSPECTION TYPE:SEG1#2 ENGINE PYLON OUTBD EXTERIOR SKIN BELLOW PANEL 443AR HAS BULDGING CORROSIONREPAIRED PER EA 757-5450-27-A3152 REV-SDR SWAA2023032303901Bracket · crackedCRACK ON BRACKET LOCATED ON OUTBOARD SIDE RT PYLON TRUST REVERSER AREA AT ENGINE 2 2023-116946<[01] REPLACED BRACKET LOCATED ON OUTBOARD SIDE RT PYLON TRUST REVERSER AREA AT ENGINE 2. IAW. B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 311A2683 SHEET 26 RESDR IPXA2023030591549Skin · corrodedINSPECTION TYPE:SEG3*MAJOR REPAIR* #2 ENG PYLON O/B SKIN HAS CORROSION INSIDE FWD OF VENT OPENINGACCOMPLISHED REPAIR ON SKIN PER UPS EO B757-5430-86081-A VT MAE EA 757-5450-27-A3149 REV- AND UPS RCD 270869
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