JASC 5350
Service difficulty reports · 6,124
Reports filed under 5350 · Aerodynamic Fairings, 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 = '5350' 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 = '5350' 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 V0XD20190425001Channel · crackedAFT WING TO BODY FAIRING AFT C-CHANNEL CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED AFT C-CHANNEL (P/N:670-39251-1) IAW CRJ700 SRM 51-41, 51-40-11, 51-42-06, 51-25-21, 51-25-06, 51-21-11, AMM 53-82-83, AND PERFORMED BOMBARDIER MOD SUM IS670538200021 REV CSDR SWAA2022030810790Fairing · elongated193 B PANEL HAS SEVERAL OVERSIZE & ELONGATED HOLES / R/R PANEL 193 B PER 53-51-21 AMMSDR SWAA2022030884452Fairing · elongatedFASTENER HOLE ENLARGED AT POSITION 17 ON PANEL 193B / REMOVED AND REPLACED PANEL PER SRM 51-20-07 AND SRM 51-40-02SDR SWAA2022030705802Fairing · noneWING TO BODY PANEL 193B HAS SEVERAL FASTENER HOLES ENLARGED. / REPAIRED FASTENER HOLES ON PANEL 193B PER SRM 51-70-05 REPAIR #8. PRIMED PER AMM 51-21-72 RESTORED TOPCOAT PER AMM 51-21-73SDR HALA201904121186Radome · damagedDURING PUSH BACK, FOUND DMG 10" BOTTOM AFT OF RADOME. PERFORMED PRELIMINARY HFEC SURFACE SCAN OF PUNCTURE ON LOWER NOSE FWD OF PRESSURE BULKHEAD/CENTERLINE PER AIRBUS NTM TASK 51-10-08. CRACK IS APPROX 3/4" IN LENGTH W/ PUNCTURE IN UN-PRESSURIZED AREA. REMOVESDR DALA2019041102394Cam · out of positionTHE VERY AFT END OF 48 SECTION: TAILCONE RELEASE LANYARD CAM ASSEMBLY IS CLOCKED INCORRECTLY. NRC 001-0251:5300-2004/002 00198: ADJUSTED CAM REF B717 AMM 53-52-03.SDR FDEA2019041100779Pin · worn[TAILCONE - L/H, TOP ALIGNMENT PIN IS WORN ON P/N AKC7520......, 2019-04-10] REPAIRED IN REF TO SRM 53-80-07 FIG 201SDR FDEA2019041100778Frame · crackedTAILCONE, L/H MIDDLE ALIGNMENT PIN, HOLE WORN ON FRAME P/N AKC 7520-3. INSTALLED REPAIR DOUBLER PER SRM 53-80-07 FIG 201 VOL 2.SDR SWAA2022030782144Former · crackedLOWER FAIRING FORMER AT BS 663 RBL 27 IS CRACKED / REPAIRED PER: EA 1-757-16198 REV IR AND ATS ER 19-02781 REV IRSDR IPXA201904224268Intercostal · crackedINSPECTION TYPE 4C, TAILCONE R/H CENTER GUIDE PIN INTERCOSTAL IS CRACKED.REMOVED AND REPLACED CRACKED TAILCONE R/H CENTER GUIDE PIN INTERCOSTAL IAW MD-11 SRM 51-33-01 AND 51-35-01. (MINOR)SDR FDEA201904080774Retainer · corrodedEVIDENCE OF CORROSION ON RH MLG WHEEL WELL CUT OUT FWD EDGE SEAL RETAINER REMOVED CORROSION IAW SRM 51-10-02 REPAIRED AREA IAW E.A. # F-5350-T0346239 P1SDR DALA2019040802290Frame · crackedAFT TAIL CONE CTR FRAME CRACKED AT GUIDE PIN 4:00. REMOVED R/H LWR CANTED FRAME. DRILLED NEW CANTED FRAME. INSTALLED R/H LWR TAIL CONE CANTED FRAME PER DWG 9911843.SDR SWAA2022030791011Fairing · noneWING TO BODY FAIRING PANEL 193B; FASNTER HOLE LOCATION #1 IS ENLARGED. MOD / R+R'D THE 193B PANEL PER AMM 53-51-21SDR SWAA2019040931511Fairing · delaminatedWING TO BODY FAIRING 193B PANEL EXTERIOR SURFACE FORWARD LEADING EDGE R/H CORNER DELAMINATED. / REPAIRED PANEL IAW EA.SDR SWAA2022030726004Panel · delaminatedPANEL 193B HAS DELAMINATION ON EDGE BAND / REPAIRED DELAMINATION DAMAGE ON EDGE BAND ON PANEL 193B IAW SRM 51-70-05-2R-6.SDR SWAA2022030747656Panel · delaminatedON MV3 WALKAROUND. FOUND PANEL 193AL TO BE DELAMINATED AT PANEL LEADING EDGE. DELAMINATION MEASURES APPROX 13 INCHES FROM TOP TO BOTTOM & 2 INCHES FRONT TO BACK. MOD / REMOVED AND REPLACED PANEL PER SMR 51-10-02SDR SWAA2022030746160Fairing · delaminatedA/C BAY PANEL 192BL LEADING EDGE DELAMINATING. / EVALUATED; PREPPED; CLEANED AND REPAIRED EDGE DAMAGE TO A/C BAY PANEL 192BL IAW B737 SRM 51-70-08; PAR 3 (A-G) REV. 66SDR SWAA2022030702406Fairing · elongatedWING TO BODY FAIRING PANEL 193B HAS ENLARGED FASTENER HOLES AT LOCATION 2;3;5;24;29;31;32;35;36; 37 & 38 MOD / RR PER AMM. 51-40-02 ONLY PN OFF/ON: 149A7652-5 SN OFF/ON: NSN / NSNSDR SWAA2022030756319Fairing · elongated8 WING TO BODY FAIRING PANEL HOLES ELONGATED / INSTALLED LARGE AREA TINNERMAN/DIMPLED WASHERS AS PER AMM 20-60-11 & SRM 51-40-02SDR DALA2019040202076Cable · tornAWR IN REFERENCE AMDS 5350-4287 STEP 4 TORN ON TAILCONE KEVLAR CABLE WAS FOUND. KEVLAR CABLE WAS REPLACED PER MD-88 AMM 20-30-01 AND MD-88 AMM 20-10-17-201. (LP1012703)SDR SWAA2022030736765None · crackedSUPPLEMENTAL INFORMATION: LOWER FAIRING FORMER AT BS 663 RBL 27 IS CRACKED / REPAIRED PER: EA 1-757-16150 REV IR AND ATS ER 19-02652 REV IRSDR SWAA2022030438593Panel · delaminatedPANEL 192AL HAS A DELAMINATED DENT ON THE EXTERNAL SURFACE / DAMAGE ON EXTERNAL SURFACE OF PANEL 192AL REPAIRED IAW SRM 51-70-05-2R-2 PARA 4 A-K. 59644U 4/13/19SDR SWAA2022030445642Panel · debondedACCESS PANEL 192BL FORWARD LOWER CORNER DISBANDED. (MARKED) / DISBANDED FORWARD LOWER CORNER ON ACCESS PANEL 192BL REPAIRED IAW SRM 53-40-70-2R-1 TABLE 202 AND IAW SRM 51-70-05-2R-10. DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1 PARA 4B(8). DAMAGE GREASDR SWAA2022030445643Panel · crackedACCESS PANEL 195BL COMPOSITE CRACKED AROUND FASTENER HOLE. (MARKED) / REPAIRED CRACKS AROUND FASTENER HOLE ON ACCESS PANEL 195BL PER SRM 53-40-70-2R-1 AND SRM 51-70-05-2R-8SDR SWAA2022030482110Panel · crackedFAIRING PANEL 194GR HAS CRACKS AROUND FASTER HOLES TOP MIDDLE SIDE ON INTERNAL SURFACE / REPAIRED FASTENER HOLE TOP SIDE MIDDLE ON INTERNAL SURFACE ON FAIRING PANEL 194GR IAW SRM 51-70-05-2R-6 7062U 4-18-19SDR SWAA2022030460639Panel · delaminated193B BODY FAIRING PANEL HAS DELAMINATION AT ATTACHMENT HOLE #16 / R/R PANEL 193B IAW AMM 53-51-21SDR SWAA2022030425960Support · crackedCRACKED SUPPORT TAB FOR BODY FAIRING PANEL 192E B.S.540+12 RBL5. MARKED / REMOVED AND REPLACED SUPPORT TAB FOR BODY FAIRING PANEL 192E B.S. 540+12 RBL 5 PER SOPM 20-50-01. 57006U 09APR19 AND IPC 53-12-11-25. 57006U 09APR19SDR SWAA2022030456955Panel · delaminatedPANEL 193B HAS 1' AREA OF DELAMINATION ASSOCIATED WITH DENT; CRACK ON INTERIOR SURFACE. MARKED ON PANEL. / REMOVED AND REPLACED 193B PANEL PER AMM 53-51-21.SDR SWAA2022030456956Panel · elongatedPANEL 193B FASTENER HOLES 38EA. ARE ELONGATED AND WORN AT COUNTER SINK. / REMOVED AND REPLACED 193B PANEL PER AMM 53-51-21.SDR SWAA2022030481322Panel · elongatedPANEL 193B HAS MULTIPLE FASTENER HOLES THAT ARE ELONGATED DUE TO WEAR. / REPAIRED ELONGATED FASTENER HOLES ON PANEL 193B I.A.W. B737 SRM 53-40-70-22-1 AND 51-70-05-2R-8. RESTORED PROTECTIVE FINISH I.A.W. B737 AMM 51-21-81-370-802SDR SWAA2022030451671Panel · crackedFOUND 1/4' CRACK IN BODY FAIRING PANEL 194FR (RIGHT SIDE) DAMAGED WITH ALLOWABLE LIMITS PER SRM PER SRM 53-60-70-1A-1 APPLIED SPEED TAPE PER SRM. S/I 7531033 **MX NOTE FOR VISABILITY** ( MX NOTE ) / REPAIRED DAMAGE PER SRM 53-60-70-2R-1. CL #61179SDR SWAA2022030451672Panel · crackedFOUND 1/4' CRACK IN BODY FAIRING PANEL 194FR (RIGHT SIDE) DAMAGED WITH ALLOWABLE LIMITS PER SRM PER SRM 53-60-70-1A-1 RE-INSPECT EVERY 8 DAYS ( MX NOTE ) / (ITEM RESOLVE UNDER MDDR: 71997) REPAIRED PER SRMSDR SWAA2022030436757Panel · delaminatedSUPPLEMENTAL INFORMATION: PANEL 193AL HAS A DELAMINATION ON THE INNER SKIN AT 2' 10' FROM I/B EDGE 18' FROM AFT EDGE / PANEL 193AL WITH DELAMINATION ON THE INNER SURFACE AT 2' 10' FROM I/B EDGE 18' FROM AFT EDGE WAS REPAIRED IAW SRM 51-70-05-2R-1 57545U 3-28-1SDR R61A2019041025368Fairing · corrodedCORROSION WAS FOUND AT AFT CENTER WING TO BODY FAIRING RT AFT FLANGE. FLANGE WAS REPLACED IAW SRM 51-41-02.SDR SWAA2022030421017Panel · delaminated193B PANEL ON LOWER SURFACE HAS A 1/2 INCH PUNCTURE WITH DELAM 1/2' IN DIAMETER. 7' FROM L/E OF PANEL 18' FROM T/E OF PANEL JUST L/H SIDE OF CENTER LINE OF PANEL. MOD / R/R CENTER WING TO BODY PANEL 193B IAW AMM 53-51-21.SDR SWAA2022030436753Former · crackedLOWER FAIRING FORMER AT BS 663 LBL 27 IS CRACKED / REPAIRED PER:EA 1-757-16130 REV IR AND ATS ER 19-02399 REV IRSDR SWAA2022030404631Panel · crackedWING TO BODY FAIRING PANEL 195CL IS CRACKED IN AFT CORNER / REPLACED PANEL 195CL WITH A SERVICABLE PANEL ON CARD NUMBER T904057.SDR SWAA2022030301262Panel · delaminatedPANEL 193AL IS DELAMINATED ON THE LEADING EDGE. DAMAGE IS APPROXIMATELY 14' X 2'. / REMOVED AND REPLACED PANEL 193AL PER 51-53-21SDR DALA2019032001826Lanyard · unsecureTAILCONE KEVLAR LANYARD LOOP NOT SECURED TO RELEASE CAM. REINSTALLED KEVLAR LANYARD LOOP TO RELEASE CAM PER AMM 53-53. VERIFIED LANYARD INSTALLED. (LP5741857)SDR SWAA2022030346553Panel · delaminatedPANEL 193AL IS DELAMINATED ON THE FWD EDGE. DAMAGE IS 6' DOWN FROM THE TOP EDGE AND 3' X 1 1/2'. ALSO 11' DOWN FROM THE TOP EDGE AND 1' X 1'. MOD / ** TLD CLOSED ON MTSI ** REMOVED AND REPLACED PANEL 193AL PER AMM 53-51-21.SDR SWAA2022030440074Fairing · elongated-REF DEFECT NO:G636781; FIVE FASTENER HOLES WITH VARYING DEGREES OF ELONGATION IN UNDERLYING STRUCTURE.-REF DEFECT NO:G636770; FASTENER PULLED THRU PANEL 193AR. -REF DEFECT NO:G636786; PANEL 193AR HAS FOUR DAMAGED HOLES. / DAMAGE ON PNL 193AR AND DAMAGE ON UNDSDR SWAA2022030440073Fairing · delaminatedWHILE INSPECTING PANEL 193AR ELONGATED HOLES AN AREA OF DELAMINATION WAS NOTED MEASURING 1.35' IN DIAMETER. / REPAIRED DELAMINATION DAMAGE TO PANEL 193AR IAW SRM 51-70-05-2R-2 57885U 07-05-19SDR SWAA2022030440063Fairing · elongatedWING TO BODY FAIRING PANEL 193B #1 AND #2 FASTENER HOLES ENLARGED. SCREWS PULLING THROUGH PANEL. / REMOVED AND REPLACED WING TO BODY PNL 19313. AMM 53-51-21SDR SWAA2019031530690Panel · erodedWING TO BODY FAIRING PANEL 193B ERODED ALONG OUTER EDGES OF PANEL. REPAIRED PANEL PER SRM.SDR RU3A20190312007Panel · damagedMAJOR REPAIR ENGINEERING ORDER (EO),18-28-45 CENTER WING SKIN FILLET PANEL FASTENER HOLE REPAIR, TO REPAIR DAMAGED/ELONGATED FASTENER HOLES NEAR THE LEADING EDGE OF THE CENTER WING SKIN. THIS EO ALSO PROVIDES INSTRUCTIONS TO FABRICATE A REPLACEMENT WING-TO FUSSDR CALA2019031500406Access Door · dentedEXTERNAL FUSELAGE AT TAILCONE ACCESS DOOR APPROX BS1034 FOUND A DENT AT LOWER CENTER AREA REF N/R 9885924 INSTALLED DOUBLER REPAIR AND FILLER AT DAMAGE AREA BS1034, BL0 PER REF SRM 53-80-01 REPAIR NR 3 - LOWER CENTER AREA AND UNITED ECRA 5331-02336.SDR IPXA2019031440063Splice · chafedINSPECTION TYPE:2C TAIL CONE LOWER INTERNAL SPLICE SKIN HAS CHAFE DAMAGE. REMOVED, FABRICATED AND REPLACED INTERNAL SPLICE SKIN IAW DWG AKC7541 AND SRM 51-31-01. (MINOR)SDR SWAA2022030413774Fairing · elongatedWING TO BODY PANEL 193B HAS SEVERAL HOLES THAT ARE OVER SIZED/ WORN/ ELONGATED. / REMOVED AND REPLACED 193B PER AMM 53-51-21.SDR IPXA2019032540456Intercostal · crackedINSPECTION TYPE:2C TAIL CONE RT CENTER GUIDE PIN INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG AKC7520 AND SRM 51-35-01. (MINOR)SDR IPXA2019031540095Doubler · chafedINSPECTION TYPE:2C TAIL CONE INTERNAL DOUBLER IS CHAFED AT STA. 5162 AND X=-36. REPAIRED CHAFED TAIL CONE INTERNAL DOUBLER AT STA. 2165 AND X=-36 IAW EO MD11-5350-66790-A APPX. A. (MINOR)
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