JASC 5420
Service difficulty reports · 3,949
Reports filed under 5420 · Nacelle/Pylon Miscellaneous 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 = '5420' 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 = '5420' 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 ASAA0947060Bushing · looseNR 2 ENG OUTBOARD FUSE PIN PYLON BUSHING IS LOOSE. REMOVED AND REPLACED NR 2 ENG PYLON O/B BUSHING FOR FUSE PIN IAW EA 400 54EA 02499.SDR ASAA0947059Bushing · looseNR 2 ENG I/B FUSE PIN BUSHING FELL OUT UPON CLEANING. REMOVED AND REPLACED NR 2 ENG PYLON I/B FUSE PIN BUSHING PER EA 400 54EA 02499.SDR DALA1052240623Structure · crackedNR 2 PYLON RT SIDE UPPER CHORD CRACK REPAIRED IAW ERA 477880-14.SDR DL757100193Structure · damagedNR 1 PYLON RT SKIN INBD SUBSTRUCTURE LWR CHROD FOUND 2 EA INCOMING HOLES O/S AFT OF STA 116.5. ACCOMPLISHED ERA 478031-14AT SAT SAA REFERENCE NON ROUTINE CARD 136558.SDR DL757091726Angle · crackedANGLE CRACKED INSIDE PYLON (TOP O/B) UNDER O/B THRUST REVERSER ACCESS HOLE LOCATED AFT OF MIDDLE HINGE. REMOVED OUTSIDE PYLON CLOSEOUT PANEL. COMPLETED REPAIR PER PRI/ERA 477880-14 REV 5, 4 NOV 2009.SDR UIEA201000172Strip · missingTHE L/E STRIP ON THE NR 3 RT FAN COWL WAS FOUND WITH APPROX 20" MISSING. "DISPOSITION WAS TO APPLY 1 LAYER OF SPEED TAPE. DVI EVERY FLIGHT CYCLE AND REPLACEMENT OF THE FAN COWL AT THE NEXT "A" CHECK".SDR CA091120002Rod · loose(CAN) DURING FLIGHT THE CREW COULD NOT RETARD THE LT THROTTLE. ENG WAS SHUTDOWN AND AN UNEVENTFUL LANDING MADE. IT WAS SUBSEQUENTLY FOUND THE UPPER COWL SUPPORT ROD HAD COME OUT OF ITS STORAGE CLIP AND FALLEN ONTO THE THROTTLE LINKAGE.SDR WRLA20091101295Support Angle · crackedCRACK - NR 3 ENG PRECOOLER COMPARTMENT WIRE SUPPORT ANGLE CRACK ABOUT 2 INCHES. REPAIRED THE CRACK AREA IAW MD11 SRM 54-00-00 FIG 208 REV 41.SDR DL757091720Structure · crackedDUE ERA 477174-14 REV ORIG CODE 6-54-31. PERMANENT REPAIR NR 1 PYLON. CRACK AT UPPER FWD CORNER OF ACCESS HOLE NAC STA 107. ACCOMPLISH PERMANENT REPAIR INSTRUCTIONS WITHIN 6000 FLIGHT HOURS OR WITHIN 18 MONTHS WHICHEVER OCCURS FIRST COMPLETED PERSDR IPXA09657884Support Angle · crackedINSPECTION TYPE:C NR 1 PYLON RT INTERNAL VERTICAL FRAME UPPER ATT SUPPORT CLIP CRACKED AT NAC STA 285.45 (CRACK LENGTH 1 INCH). NR 1 PYLON RT INTERNAL VERTICAL FRAME UPPER ATT SUPPORT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45 SDR FDEA200910263675Web · wornNUMBER 2 PYLON 311N5040-6 UPPER AFT WEB IS WORN AT APPROX. PPS 162 - 172. BLENDED WORN AREA AT APPROX PPS 170.90. ORIGINAL MATERIAL THICKNESS .063", AFTER REWORK .054"; D=.009", L=1.0", W=.700". FOUND TO BE OUT OF LIMITS PER SRM 54-50-01, NOTE "B", DETAIL 3.SDR FDEA200910263667Fairing · gougedNUMBER 2 PYLON AFT STRUT FAIRING LOWER FOUND 2 GOUGED MARKS. REPAIR CARRIED OUT IAW EA NR F-5480-131057. REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 CRITERIA.SDR SWIA200923172Channel · crackedRIGHT NACELLE CHANNEL CRACKED. (C-CHECK) REPLACED CHANNEL PER SRM.SDR SWIA200923170Fitting · crackedLEFT NACELLE WHEEL WELL INTERNAL VERTICAL FITTING CRACKED. (C-CHECK) REPLACED FITTING PER SRM.SDR A6WA200940733Bracket · crackedRT T/R PDU HARNESS BRACKET FOUND CRACKED. RT T/R PDU HARNESS BRACKET REPLACED IAW SRM 51-42-06. (K)SDR A6WA200940734Bracket · crackedRT ENG INBD T/R STOW/THROTTLE LOCK OUT SWITCH BRACKET AT 9 O`CLOCK POS FOUND CRACKED. (K)SDR TIPR20090028Panel · burnedNR 2 PYLON AFT FAIRING INBOARD PANELS SCORCHED, NAC STA 285.94 - NAC STA 352. REPAIRED PER B767-200 SRM 54-50-70 FIG 201 SHEET 1-11.SDR F3LA2009101600202Support · crackedREFERENCE NON-ROUTINE C071806. DURING DEN C3 C-CHECK, INSP NOTED THE NR 2 ENG OTBD PYLON RIB SUPPORT WAS CRACKED ABOUT RIB 7. MX REMOVED AND REPLACED SUPPORT IAW SRM 51-42-11, SRM 51-44-11, SRM 51-26-00, SRM 54-52-12 AND SRM 51-42-00.SDR FDEA200910123540Channel · crackedNR 2 PYLON LBL 12.5", PP STA 170, PP WL 157 HAS A HORIZONTAL FORMED U ANGLE CRACKED. CRACKED U-CHANNEL ON NR 2 PYLON AT PP STA 170, LBL 12.5", PP WL 157, REMOVED AND REPLACED IAW SRM 51-40-02 REV. 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR FDEA200910123539Stiffener · crackedNR 2 PYLON OTBD SKIN AT PP STA 185.35, WL 151.33 STIFFENER PN 311N5220-56 FOUND CRACKED AT TOP CORNER. (APPROX. 0.75" LENGTH) CRACKED STIFFENER ON NR 2 PYLON AT PP STA 185.35, WL 151.33, REMOVED AND REPLACED IAW SRM 51-40-02 REV 98. REPAIR IS CLASSIFIED AS MISDR FDEA200910123538Stiffener · crackedNR 2 PYLON RBL 13", PP STA 185, PP WL 160 HAS A VERTICAL STIFFENER L ANGLE CRACKED. CRACKED STIFFENER ON NR 2 PYLON AT PP STA 185, RBL 13", PP WL 160, REMOVED AND REPLACED IAW SRM 51-40-02 REV 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR FDEA200910123537Support · crackedNR 1 PYLON PP STA 169 RBL 13", PP WL 160, HAS A FORMED EXTRUSION CRACKED. NUT PLATES ATTACHED. CRACKED FORMED SUPPORT ON NR 1 PYLON AT PP STA 169, RBL 13", WL 160, REMOVED AND REPLACED IAW SRM 51-40-02 REV 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 SDR FDEA200910123536Channel · crackedNR 2 PYLON U CHANNEL PP STATION 170 TO PP STATION 185, LBL 13" PP WL 164, HAS A CRACK AT LBL 13" AT LOWER SCREW HOLE. CRACKED CHANNEL ON NR 2 PYLON FROM PPSTA 170 TO PP STA 185, LBL 13" TO RBL 13" , PP WL 164. REMOVED AND REPLACED IAW SRM 51-40-02 REV 98. RSDR FDEA200910123535Angle · crackedNR 1 PYLON RBL 12.5, PP STATION 171, PP WL 161 HAS L-ANGLE CRACKED. CRACKED ANGLE ON NR 1 PYLON AT PPSTA 171, RBL 12.5 REMOVED AND REPLACED IAW SRM 51- 40-02 REV. 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR FDEA200910123534Angle · crackedNR 2 PYLON, LBL 12.5", PP STA 169, PP WL 158 HAS A VERTICAL ANGLE CRACKED. CRACKED ANGLE ON NR 2 PYLON AT PP STA 169, LBL 12.5". REMOVED AND REPLACED IAW SRM 51-40-02 REV 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR A6WA200940741Bracket · crackedLT ENG AT 6 O`CLOCK POSITION BRACKET CRACKED FOR T/R ORANGE HARNESS. LT ENG AT 6 O`CLOCK BRACKET FOR T/R ORANGE HARNESS REPLACED IAW SRM 51-42-06. (K)SDR C2XA09TY254Fitting · crackedLEFT ENGINE FORWARD YOKE LOWER LINKAGE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW EC 5450-01028.SDR FDEA200910083502Angle · crackedNR 2 PYLON LBL 13" PP STATION 167, PP WL160 HAS A FORMED HORIZONTAL ANGLE CRACKED. CRACKED ANGLE AT NR 2 PYLON LBL 13" PP STATION 167, PP WL160, REPLACED IAW SRM 51-40- 02 REV. 98. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR TIPR20090027Panel · burnedDURING MAINTENANCE VISIT (C-CHECK) AT TIMCO GSO, FOUND NR 1 PYLON AFT FAIRING INBOARD FIXED PANELS 2 EACH SCORCHED, NAC285- NAC352.47. REPAIRED PER B767-200 SRM 54-50-70 FIG 201 SHEET 1-11.SDR FDEA200910063485Support · crackedNR 1 ENG PYLON ACCESS PANEL 413 BL HAS 2 EA CRACKS AT SEAL SUPPORT CORNERS. REMOVED SEALS AND RETAINERS AND FABRICATED 2 EA DOUBLERS REF SRM 54-52-51; FIG 205. INSTALLED REPAIR DOUBLERS REF SRM 51-40-21; PARA 6. REINSTALLED SEALS AND RETAINERS SRM 54-52-5SDR DL757091652Hinge Fitting · damagedWHILE WORKING EA 06-070332-03 REV H OPN 0138 FOUND 8 EA HOLES OVERSIZED ON NR 1 PYLON LT AND RT HINGE FITTINGS. ACCOMPLISHED ER/A 477151-14AD DATED OCT 17, 2009 AT SAA SAT ON N/R CARD 135693.SDR USAA2009100592706Angle · crackedCLT - Q6 - MAJOR REPAIR - CRACK FOUND ON NR 1 PYLON ANGLE AT AFT OUTBOARD CORNER. REPLACED NR 1 PYLON ANGLE AT AFT OUTBOARD CORNER IAW B737 SRM 51-10-02.SDR FDEA200909293423Stiffener · crackedNR 1 PYLON LBL 13", PP STA 184, PP WL 160 HAS A VERTICAL STIFFENER ANGLE CRACKED. REMOVED AND REPLACED IAW SRM 51-40-02 REV. 98. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR IPXA09557532Attach Bracket · crackedINSPECTION TYPE:C1 WHILE WORKING CUSTOMER CARD 822126 FOUND WIRE CONDUIT ATTACH BRACKET C CRACKED IN HALF UNDER PANEL 435AL. REMOVED, FABRICATED AND INSTALLED REPLACEMENT BRACKET PER SRM 51-40-02.SDR IPXA09557507Bracket · crackedINSPECTION TYPE:C1 CRACKED ANGLE ON NR 2 NACELLE STRUT OUTBOARD STRUCTURE AT LOWER FWD ATTACH AREA OF PANEL 445AR. REMOVED AND REPLACED BRACKET PER SRM 51-40-02.SDR IPXA09557506Bracket · crackedINSPECTION TYPE:C1 NR 1 ENGINE AFT PYLON STRUCTURE RT CUTOUT FOR PANEL 435AR FWD LOWER ANGLE BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET PER SRM 51-40-02.SDR NWAA093359946Web · buckledDURING ENGINE CHANGE FOUND PYLON VERTICAL WEB BUCKLED BETWEEN UPPER AND LOWER SPARS FOR AFT ENGINE MOUNT AT XN39.250. REPAIRED PER EA 99-216590.SDR SIMA200926704Structure · crackedDURING MAINTENANCE INSPECTION FOUND THE OUTBOARD TRANS COWL EXTRUSION CRACKED. AIRCRAFT REMOVED FROM SERVICE.SDR FDEA200909183329Support Bracket · crackedLT WING BOTTOM SKIN LWR SURFACE; PYLON AFT FAIRING SUPPORT BRACKET IS CRACKED AROUND THE FASTENER BETWEEN RIBS 7 AND 8. REMOVED HYD LINES AND UNIONS IAW AMM 20-23-12-0 AND AMM 54- 54-00-4. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-40-21, PARA 7 AND SSDR C2XA09TY237Structure · corrodedTYS - A/C CURRENTLY IN C-CHECK AND INSPECTION FOUND CORROSION IN TWO HOLES ON THE NR 2 ENGINE INLET. MAINTENANCE REAMED THE HOLES AND INSTALL BUSHINGS TO REMOVE THE CORROSION. ALL WORK WAS ACCOMPLISHED IAW EC5420-01158 AND WILL BE RELEASED AT THE END OF THESDR USAA2009092292592Bearing · corrodedSAL - C8 - MAJOR REPAIR - CORROSION ON RIGHT PYLON SPIGOT BALL JOINT BEARING AT RIB 4 TO RIB 10, Z480. REPLACED RIGHT PYLON SPIGOT BALL JOINT BEARING AT RIB 4 TO RIB 10, Z480 IAW JOB CARD 26C40054035.SDR HALA200909150406Skate Angle · crackedNR 2 PYLON OTBD SKATE ANGLE CRACKED AT FWD END. FWD END OF OTBD SKATE ANGLE FABRICATED DWG 112T7054. FABRICATED PART INSTALLED (PN 112T7054). SB 767-57-0023 AND SRM 51-40-02 REV 81, AUG.15 2009, D634T210.SDR USAA2009092392606Ball Joint · corrodedSAL - C8 - MAJOR REPAIR - CORROSION ON LEFT PYLON SPIGOT BALL JOINT. REPLACED LEFT PYLON SPIGOT BALL JOINT IAW JOB CARD D5463003800000.SDR C2XA09TY233Inlet · corrodedTYS ACFT CURRENTLY IN A C-CHECK STATUS AND INSPECTION FOUND THE NR 1 ENGINE INLET ATTACH FLANGE WITH CORRODED HOLES. MAINTENANCE REAMED THE HOLES AND INSTALL BUSHIONS TO REMOVE THE CORROSION. ALL WORK WAS ACCOMPLISHED IAW EC 5420-01158.ALL WORK ACCOMPLISHED ANSDR ASAA0946530Support · chafedLEFT WING AFT NR 1 PYLON LWR DRAIN INNER SUPPORT FOR DRAIN HAS FASTENERS CHAFED THROUGH INNER STRUCTURE. REPAIRED PER EA.SDR FDEA200909023247Support Angle · missingPYLON ANGLE NR 1 SUPPORT FOUND MISSING DURING REMOVAL. REPLACED. INSTALLED FABRICATED SUPPORT ANGLE ON PYLON NR 1 IAW EO F-2910-7-5002 A PT1 STEP 10. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR DL757091463Structure · damagedAFTER REMOVAL OF LT SIDE NR 2 PYLON, FOUND 1 EA HOLE TO BE .500 AT LT STA 116.05. C/W ERA 476264-14 REV O.SDR Q2S2010F00000Doubler · missingPYLON NR 4 LEFT SAILTAIL FAIRING FWD REPAIR PATCH MISSNG. REPAIRED CARRIED OUT IAW EN: 1392-09.SDR C2XA09TY225Structure · corrodedNR 1 ENG INLET HAS CORROSION INSIDE FASTENER HOLES. REAMED HOLES TO REMOVE CORROSION AND INSTALLED BUSHINGS IAW EC5420-01158B. AIRCRAFT STILL IN C-CHECK.SDR DL757091361Structure · damagedNR 1 PYLON LOWER CHORD HAS AN ELONGATED HOLE AT APPROX STA 122 I/B (RT) SIDE. C/W AT SAA - SAT ON N/R 143961 JOB 83477300001.
Back to JASC 5420