JASC 5420
Service difficulty reports · 3,946
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 COEA2024030508738Panel · crackedDURING A SCHEDULED MAINTENANCE INSPECTION, A CRACK WAS FOUND ON THE L/H ENGINE INBOARD PLENUM PANEL AFT SIDE MIDDLE STIFFENER. A TEMPORARY REPAIR WAS PERFORMED ON THE L/H ENGINE INBOARD PLENUM PANEL PER TEXTRON DOCUMENT REF: DQ43349M1. REPLACED THE PANEL IAW SDR SWAA2024040157668Web · crackedCRACK WEB INBOARD FAN COWL LOC . INTERNAL AREA ACCESS DOOR 413AR ON ENGINE 1 2024-145968<[01] REPLACED WEB INBOARD FAN COWL LOC . INTERNAL AREA ON ACCESS DOOR 413AR AT ENGINE 1 IAW B737-800 SRM 51-10-02 ITEM 9 AND CMM 71-13-30. SEE INDIVIDUAL SIGN-OFF BELOW;[0SDR SWAA2024031556779Web · cracked2 ENG. INBD. OTBD. FAN COWL WEB CRACKED AT OIL SERVICE OPENING.<[01] REMOVED AND REPLACED WEB PER SRM 51-10-02;[02] C/WSDR SWAA2024031556780Web · cracked#1 ENG. INBD. FAN COWL WEB CRACKED AT OIL SERVICING DOOR OPENING.<[01] REMOVED WEB PER SRM 51-40-02.;[02] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]SDR GTIA2024022037926Bracket · burnedREF AEROMAN W/O 2024-53/1 NR 2024-38966. BURNED SHACKLES DUE TO SHORT CIRCUIT INBOARD SIDE OF RH PYLON. RAF-01 3499899-02 GENERATED.-PERFORMED PERMANENT REPAIR OF PYLON GRACKET IAW EA-54-0028-024. THIS REPAIR IS CATEGORY A. INSPECTION NOT REQUIREDSDR JJBA20240226060Bracket · crackedIN LH ENG PYLON, LH ENG PYLON STRUCTURE FWD PRECOOLER BRACKET IS CRACKED AND BENT. LH ENG PYLON STRUCTURE FWD PRECOOLER BRACKET REMOVED AND REPLACEDSDR CALA2024021500424Web · cracked#1 PYLON MOST AFT CLOSE OUT WEB IS CRACKED. REF AMES (ILN) NRC 166320-0400-0166. NEW CLOSEOUT WEB P/N 313T3355U233 INSTALLED (M&E 76-7831-3-0155). SEE PARTIAL WORK ACCOMPLISHED ON BACK FOR MORE DETAILS, IAW B767-300 SERM 51-40-02. FORM 46-0024 COMPLETED (SSFR)SDR ASAA2024020948003Plate · corrodedLESSOR ITEM: PYLON #2 L/H FITTING BASEPLATE P.N. D5461020320000 HAS FRETTING GROUNDED - YES. ALL WORK ACCOMPLISHED ON NON ROUTINE 35903AC FLIGHT HOURS 34712:52, AC CYCLES 11812, W.V. 015SDR SWAA2024022050883Bracket · brokenNR 1 PYLON OUTBOARD SIDE FAN COWL SUPPORT BEAM BONDING WIRE GD4182 IS BROKEN. R & R #1 PYLON OUTBOARD SIDE FAN COWL SUPPORT BEAM BONDING WIRE GD4182 AND BRACKET IAW AMM 70-00-01-400-801-G0, SWPM 20-20-10, & SRM 51-40-02-OG-0, TESTED GOOD. R & R NR 1 PYLON SDR CALA2024021200377Angle · cracked#1 PYLON INSIDE I/B ARROW HEAD PANEL AT AFT END, L ANGLE IS CRACKED. REF AMES (ILN) NRC 166320-0400-0162. REMOVED DAMAGED ANGLE AND INSTALLED NEW PN 313T3355-287 UAL. SEE CWO NO 166327-0400-0002 FOR PART FAB IAW B767-300 SRM 51-40-02. SEE PARTUIAL WORK ON BACSDR CALA2024021200375Strap · cracked#1 PYLON AFT V WEB AFT STRAP WHERE STRINGER PANEL ATTACHES IS CRACKED. INSTALLED NEW STRAP PN 313T3380-660 IAW B767-300 SRM 51-40-02. S EE PARTIAL WORK ACCOMPLISHED FOR MORE DETAILS FORM 46-0024 (SSFR ) SEE NON-ROUTINE 166320-0400-0168 FOR DETAILSSDR SWAA2024022749558Intercostal · crackedPANEL 414 COWL ASSY - FAN - #1 ENGINE INBOARD INTERCOSTAL CRACKED JUST BELOW SERVICE DOOR.<[01] REMOVED AND INSTALLED NEW INTERCOSTAL PER SRM 51-10-02;[02] C/WSDR SWAA2024022749559Intercostal · crackedPANEL 424 COWL ASSY - FAN - #2 ENGINE OUTBOARD INTERCOSTAL CRACKED JUST BELOW SERVICE DOOR.<[01] REMOVED AND INSTALLED NEW INTERCOSTAL PER SRM 51-10-02SDR DALA2024020701622Support Bracket · crackedSHIP 3313 CRACK SUPPORT BRACKET LOC AT MIDDLE UPPER AREA I/B SIDE ON LH PYLON. CORRECTIVE ACTION: COMPLIED WITH PRI 615510-14 REV ORIGINAL AND PRI REV 0. (0189791)SDR CALA2024020200299Angle · cracked#1 ENGINE PYLON I/B AND O/B SIDE HAS 2 EA. PANEL ATTACH STRAPS CRACKED ON AFT PYLON FRAME STA 410.SDR SWAA2024022245806Support Web · crackedCRACK INBOARD FAN COWL SUPPORT WEB ON ENGINE 1 2024-61365<[01] REPLACED INBOARD FAN COWL SUPPORT WEB ON ENGINE 1 IAW B737-800 SRM 51-40-02-0G-0.;[02] REPLACED INBOARD FAN COWL SUPPORT WEB ON ENGINE 1 IAW B737-800 SRM 51-40-02-0G-0.SDR SWAA2024020244972Bracket · crackedDOT #114-010. LEFT ENGINE CORE COOLING TUBE BRACKET CRACKED AT THE 9:00 POSITION.<SDR DALA2024012401062Web · gougedSHIP 3124 GOUGE WEB LOC. BTW RIB08 TO RIB09 UPPER SPAR AT BLEED DUCT AREA ON LH PYLON. CORRECTIVE ACTION: REPAIRED PER ER/A 614973-14. (0168701)SDR IPXA2024012228251Support · cracked*SDR FILED OPEN* FAULT - CRACK - RIB, NO.1 PYLON INSIDE OF MID TORQUE BOX SUPPORT, CAN ACCESS FROM PANEL #436AR (REPLACE) OK TO WORKSDR IPXA2024012228280Support · cracked*SDR FILED OPEN* FAULT - CRACK - RIB, NO.1 PYLON INSIDE OF MID TORQUE BOX SUPPORT, CAN ACCESS FROM PANEL #436AL (REPLACE) OK TO WORKSDR SWAA2024011942353Bracket · crackedDOT A24-7 NUMBER ONE ENGINE O/B FAN COWL AFT HOLD OPEN ROD STOW BRACKET CRACKED.<[01] AUDIT CWSDR SWAA2024022341615Shield · crackedNUMBER 2 ENG OUB FAN COWL INNER SHIELD UPPER EDGE CRACKED @ OIL SERVICE ACCESS PANEL MKD DOT<[01] REMOVED AND REPLACED INNER SHIELD AT NO-2 ENGINE O/B FAN COWL AT OIL SERVICE ACCESS PANEL PER BOEING 737-800 SRM 51-40-02-0G-0;[02] VERIFIED REPLACEMENTSDR SWAA2024022341617Shield · crackedNUMBER 1 ENG INB FAN COWL ASSY INNER SHIELD CRACKED @ ENG OIL SERVICE PANEL MKD DOT<[01] REMOVED AND REPLACED INNER SHIELD AT NO-1 ENG INB FAN COWL ASSY AT ENG OIL SERVICE PANEL PER BOEING 737-800 SRM 51-40-02-0G-0;[02] VERIFIED REMOVED;[03] VERIFIED REPLACEMESDR SWAA2024022141602Support Angle · cracked#2 ENGINE O/B FAN COWL ENGINE OIL SERVICE DOOR AFT DOOR CUTOUT FRAME SUPPORT ANGLE CRACKED DOT# T695<[01] O/B FAN COL SUPPORT ANGLE REPLACEDSDR SWIA2024031100109Stand Off · crackedL/H UPPER TRANSCOWL INBD "A" BRACKET IS CRACKED. (C-CHECK RO 3/10/2024) INSTALLED 1 EA. NEW STAND-OFF P/N CN624-2082-201 ON L/H UPPER TRANS COWL, REF. REO 670-54-21-971, REV. B, 2023-11-28SDR SWAA2024020638563Support Bracket · brokenBROKEN SUPPORT BRACKET ON INBOARD FAN COWL LOC. AFT POSITION ON ENGINE 2 2023-784458<[01] REPLACED SUPPORT BRACKET ON INBOARD FAN COWL LOC. AFT POSITION ON ENGINE 2 IAW B737-700 SRM 51-40-02;SRM 51-10-02 AND GOODRICH AEROSTRUCTURES 71-13-30; PAGE: 10050 AND PASDR DALA2024010800306Unknown · unknownSHIP 6817 DURING REPAIR PROCESS OF WEB IN REFERENCE TO NRC.00372 WAS DRILLED OUT LOWER WEB AT FAN COWL SUPPORT BEAM AT NAC.STA 100 APPROX BTW. 11 TO 2 O CLOCK HOUR POSITION AT LH ENGINE. CORRECTIVE ACTION: LOWER WEB AT FAN COWL SUPPORT BEAM AT NAC.STA 100 APPRSDR IPXA2024010334304Unknown · unknown*SDR FILED OPEN* FAULT - CRACK ANGLE, INTERNAL AFT INBOARD UPPER SLAT EDGE OF NO.1 PYLON AFT NACELLE STRUT FAIRING(REPLACE) OK TO WORKSDR IPXA2024012426549Channel · crackedFAULT - CRACK - CHANNEL, NO.1 ENG PANEL NO.437DB TRIANGLE SUPPORT (REPAIR) REVIEW COMPLETESDR IPXA2024012425988Angle · crackedFAULT - CRACK - CLIP NO.2 PYLON AFTER LOWER FAIRING AFTER INNER SIDE, LH FAIRING PNL SUPPORT BRACKET(REPLACE) REVIEW COMPLETESDR IPXA2024012425690Web · cracked**SUPPLEMENTAL SDR**FAULT - CRACK - WEB, INTERNAL AFTER LOWER SIDE OF NO.2 PYLON AFTER FAIRING PNL NO.447DB (REPLACE) REVIEW COMPLETESDR IPXA2024010326549Unknown · unknown*SDR FILED OPEN* FAULT - CRACK - CHANNEL, NO.1 ENG PANEL NO.437DB TRIANGLE SUPPORT (REPAIR) OK TO WORKSDR IPXA2024010325690Unknown · unknown*SDR FILED OPEN* FAULT - CRACK - WEB, INTERNAL AFTER LOWER SIDE OF NO.2 PYLON AFTER FAIRING PNL NO.447DB (REPLACE) OK TO WORKSDR FXTA2024032129001Support · crackedLH LOWER ENGINE COWLINGS HAVE STRUCTURE CRACKED UNDER THE ICE VANE DOOR LINKAGE CASTING ATTACHMENTS. P/N: 7852122-28 & 7852122-27 CRACKEDSDR IPXA2024012401671Angle · crackedFAULT - CRACK - ANGLE, NO. 1 ENG L/H AFT FAIRING DOOR HINGE BEAM ANGLE AT #4(REPLACE) REVIEW COMPLETESDR IPXA2024010301671Unknown · unknown*SDR FILED OPEN* FAULT - CRACK - ANGLE, NO. 1 ENG L/H AFT FAIRING DOOR HINGE BEAM ANGLE AT #4(REPLACE) I.A.W. AMM 54-53-02-004-002, REV.140, REMOVED NO.4 L/H HINGE BOLT OF NO.1 L/H FAIRING DOOR.SDR IPXA2024010301641Unknown · unknown*SDR FILED OPEN* FAULT - CRACK - ANGLE, NO. 1 ENG R/H AFT FAIRING DOOR HINGE BEAM ANGLE AT #4.(REPLACE) I.A.W. AMM 54-53-02-004-002, REV.140, REMOVED NO.4 R/H HINGE BOLT OF NO.1 R/H FAIRING DOOR.SDR IPXA2024010378974Unknown · unknown*SDR FILED OPEN* FAULT - CRACK - CLIP, INTERNAL AFTER OUTBOARD SIDE FRAME OF NO.1 PYLON AFTER FAIRING, NAC STA 376.20 (REPLACE) PAPER OKSDR SWAA2024012935039Web · cracked#2 O/B ENG COWL HAS CRACK ON WEB FWD SIDE OF ENG OIL ACCESS DOOR.(MARKED)<[01] REMOVED AND REPLACED WEB IAW SRM 51-40-02;[02] C/W INSP REMOVED AND REPLACED WEB IAW SRM 51-40-02SDR CALA2023122003693Stiffener · crackedNUMBER 1 PYLON NACELLE STRUT AFT TORQUB BOX (INT) O/B STIFFENER AT NAC. WL 1436 AND NAC STA 265.4-295 FOUND DAMAGE. REPLACED AS PER SRM 51-10-02 AND FASTENER INSTALLED AS PER SRM 51-40-02SDR SWAA2023122929493Web · crackedCRACK INBOARD FAN COWL WEB ON ENGINE 1 2023-748582<[01] REPLACED WEB AND FASTENERS OF INBOARD FAN COWL ENG 1 IAW B737-700 SRM 51-40-02;[02] CORRECT STEP 1: REPLACED WEB AND FASTENERS OF INBOARD FAN COWL ENG 1 IAW B737-700 SRM 51-40-02 AND GOODRICH AEROSTRUCTURSDR SWAA2023122929148Web · crackedCRACK WEB INBOARD FAN COWL LOC. INTERNAL AREA ACCESS DOOR 414AR ON ENGINE 1 2023-750505<[01] REPLACED WEB INBOARD FAN COWL LOC. INTERNAL AREA ACCESS DOOR 414AR ON ENGINE 1 IAW B737-700 GOODRICH AEROSTRUCTURES CMM 71-13-30 AND SRM 51-10-02 ITEM 9 AND SRM 51-40-SDR SWI2024022000122Bracket · crackedR/H LWR TRANSCOWL INBD "A" BRACKET IS CRACKED. (C-CHECK RO 2/19/2024) INSTALLED NEW I/B "A" BRACKET (PN CN624-2082-201) INTO R/H LWR TRANSCOWL REF REO# 670-54-21-971, REV B, DATED 11/28/23, CRJ 700 SRM 51-42-14-001-001-A01, AND SRM 51-42-20-001-001-A01 SDR VNAA2023120320021Rub Strip · corrodedHN 118777 DISCREPANCY: RH LOWER CORE COWL AFT RUB STRIP HAS FRETTING CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED RH LOWER CORE COWL AFT RUB STRIP IAW CRJ-900 SRM 54-23-00-201-006-A01.SDR SWI2024F00001Bracket · crackedR/H LWR TRANSCOWL OTBD "A" BRACKET IS CRACKED. (C-CHECK RO 1/19/2024) INSTALLED 1EA. NEW A-BRACKET P/N CN624-2082-201 ON R/H LOWER TRANS COWL, REF. REO 670-54-21-971, REV. B, DATED 2023-11-28. COMPLIED WITH SKYCARD 51-900-1002-SKYSDR SWAA2023122125576Support Bracket · broken#1 ENGINE FAN COWL SUPPORT BRACKET IS BROKEN<[01] REMOVED/REPLACED #1 ENGINE FAN CASE FAN COWL SUPPORT BRACKET IAW SOPM 20-50-01 / AIPC 71-00-51-14.;[02] VERIFIED CORRECTIVE ACTIONS STEP 1 AND MEASUREMENTS TABLE.SDR CALA2023112903501Bracket · crackedFWD PANEL SUPPORT BRACKET IN I/B SIDE OF #2 PYLON ABOVE CORE COWL FOR PANEL 446CL IS CRACKED. REF AMES NRC 164541-0400-0175. REMOVED & REPLACED FWD PANEL SUPPORT BRACKET IAW B767 SRM 51-40- 02 SECTION 7. SEE PARTIL WORK ACCOMPLISHED FOR WORK COMPLETED EC /RA 5SDR SWAA2024010424359Web · crackedCRACK INBOARD FAN COWL WEB ON ENGINE 1 2023-719998<[01] REPLACED WEB INBOARD FAN COWL ON ENGINE 1 IAW B737-800 SRM 51-40-02 AND CMM 71-13-30.;[02] CERTIFIED STEP 1 COMPLETEDSDR SWAA2023120523637Shield · cracked#2 ENGINE O/B FAN COWL OIL ACCESS DOOR SHEILD IS CRACKED<[01] REMOVED AND REPLACED #2 ENGINE O/B FAN COWL OIL ACCESS DOOR SHEILD PER SRM 51-40-02-0G-0 AND CMM 71-13-30;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2023111420571Cowl Door · crackedNUMBER 1 ENGINE I/B FAN COWL HAS CRACK FWD OF THE FORWARD LATCH APPROXIMATELY 9 INCHES LONG GOING THROUGH 2 RIVETS<[01] REMOVED AND REPLACED #1 I/B FAN COWL PER AMM 71-11-02;[02] VERIFIED THE FOLLOWING:<BR>REMOVED AND REPLACED #1 I/B FAN COWL PER AMM 71-11-02
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