JASC 5350
Service difficulty reports · 6,121
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 IPXA2024032049265Fairing · crackedLH BODY FAIRING AREA UPR SIDE STA 1341 FRAME STRUCTURE HAS CRACKED. 74-079 TREATED AND PRIMED REPAIR PARTS I.A.W MD-11 SRM 51-21-01-0G-0 PAR 26 AND 33. RE INSTALLED L/H BODY PNL SUPPORT RIB AT STA 1341 I.A.W MD-11 SRM 51-35-01-0G-0SDR JJBA20240117021Fairing · crackedRH WING, AT TOP WING TO BODY FAIRING, ANGLE AFT SPAR II CRACKED. ANGLE REPLACEDSDR DALA2024011100500Unknown · unknownWTBF LONGERON CRACKED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 012-0001:5110-2001/002 00004 REMOVED AND REPLACED WTBF LONGERON PER AMDS WC 5352-01038-07A. (LP# 0147007)SDR IPXA2025030430302Tail Cone · deterioratedTAIL CONE WORKING PLATFORM RH SIDE NON-SKID DETERIORATED . INSTALLED TAIL CONE WORKING PLATFORM R/H SIDE IN REF. TO BOEING MD11 AMM 53-21-05-400-801.SDR IPXA2024021630343Tail Cone · delaminatedEXTENDED TAIL CONE 03EA WORKING PLATFORM DELAMINATED. 74-059 INSTALLED 02 EA WORK PLATFORM ON EXTENDED TAILCONE IN REF WITH MD-11 AMM 53-21-05-400-801. FABRICATED FLOOR PANEL EXTENDED TAIL CONE PLATFORM P/N AKC7646-2SAAU ON TRAVELER# 7002878017.SDR IPXA2024021630405Support Angle · crackedTAIL CONE LH PATIO DOOR FWD SIDE 01EA ANGLE SUPPORT HAS CRACKED. 74-061 LOCATED, DRILLED AND INSTALED ANGLE SUPPORT ( CLIP ) AT TAIL CONE L/H PATIO DOOR FWD SIDE IN REF MD11 SRM 51-31-01 AND SRM 51-35-01SDR IPXA2024021630370Access Panel · gougedTAIL CONE RH PATIO DOOR FWD SIDE ACCESS PANEL AND METAL PLATE HAS GOUGED. 74-060 LOCATED, DRILLED AND INSTALLED NEW METAL PLATE AT TAIL CONE R/H PATIO DOOR FWD SIDE, IAW MD11 SRM 51-31-01. P/N AKC7506 / BTCH # 0004230476.SDR IPXA2024010930343Unknown · unknown(COMP) EXTENDED TAIL CONE 03EA WORKING PLATFORM DELAMINATED. 74-059 APPROVEDSDR IPXA2024010930302Unknown · unknown(APG) TAIL CONE WORKING PLATFORM RH SIDE NON-SKID DETERIORATED . 74-056 APPROVEDSDR IPXA2024010930405Unknown · unknown*SDR FILED OPEN* (STR) TAIL CONE LH PATIO DOOR FWD SIDE 01EA ANGLE SUPPORT HAS CRACKED. 74-061 APPROVEDSDR IPXA2024010930370Unknown · unknown(STR) TAIL CONE RH PATIO DOOR FWD SIDE ACCESS PANEL AND METAL PLATE HAS GOUGED. 74-060 APPROVEDSDR IPXA2025022694133Fairing · puncturedRIGHT AFT WING TO BODY FAIRING HAS 2 EACH PUNCTURES€¦.MARKED WITH YELLOW GREASE PENCIL. PREPARE AND APPLIED PLIES WITH EA 9390 BATCH 4303218 AND 04-009-0002 BATCH 4297288 AND CURED IAW-757-200-SRM-51-70-17-0G-0 PARA 4.B. 8-11. RESTORED PROTECTIVE COATING WITHSDR IPXA2024010694133Unknown · unknownRIGHT AFT WING TO BODY FAIRING HAS 2 EACH PUNCTURES€¦.MARKED WITH YELLOW GREASE PENCIL. FOUND DAMAGE TO BE WITHIN LIMITS FOR DEFERRAL, ITEM REQUIRES REINSPECTION EVERY A CHECK AND REPAIR NO LATER THAN NEXT C CHECK, APPLIED TAPE TO SEAL THE PANEL IAW SRM 53-00SDR HALA20240103003Unknown · unknownBIRD STRIKE ON CLIMB-OUT IN SMF. PERFORMED BIRD STRIKE INSPECTIN PER AMM 05-51-14. FOUND DAMAGE TO LEFT HAND SIDE OF RADOME. NO OTHER DAMAGE NOTED. FERRY FLIGHT REQUIRED. REMOVED AND REPLACED RADOME PER AMM 53-15-11. SECURITY CHK GOOD. OK FOR SVC.SDR SWAA2024010336700Radome · delaminatedRADOME DELAMINATING<[01] REMOVED AND REPLACED NOSE RADOME IAW AMM 53-52-00. NO DEFECTS NOTEDSDR DALA2023122810693Unknown · unknownMAINTENANCE FOUND THE KEVLAR CABLE FOR THE RELEASE MECHANISM INSIDE TAILCONE TO BE TORN. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00061: CABLE ASSEMBLY WAS REPLACED PER B717SDR DALA2023122410553Unknown · unknownSHIP 3261 DISC: CREW REPORTS WTB FAIRING 191DT MISSING ON WALKAROUND. C/A: REMOVED PANEL 191DT PER A320 AMM 53-35-11(840719) UPON INSPECTION FOUND WINDOW BETWEEN FR 44L AND FR43L GOUGED. REMOVED WINDOW PER A320 AMM 56-21-13(845719). REPLACED WINDOW PER A320 AMSDR DALA2024012601168Fairing · damagedSHIP 3161 1"BY 1" HOLE IN COMPOSITE FAIRING JUST BELOW REFUEL PANEL ON BELLY OF A/C RT SIDE. CORRECTIVE ACTION: REPAIRED PANEL PER A319 SRM 53-35-11-300-007, OK FOR SERVICE. (5374405)SDR CALA2023122603730Radome · damagedRADOME NEEDS REPLACEMENT DUE TO BIRD STRIKE REF LOG PAGE 6617687 REPLACE RADOME ACC AMM 53-12-01/401 REV 99 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1752908 SN OFF 0008 RADOME, WT/GOLD OFF 27-5351-9-0001 0008 ON 27-5351-9-0001 0020. BIRDSTRIKE INSPECTION PESDR SWI2024F00020Support · crackedAFT FUSELAGE, WING TO BODY FAIRING SUPPORT STRUCTURE, LEFT SIDE, CONNECTING ANGLE IS CRACKED AT APPROX. FS 909.00. (C-CHECK RO 1/24/2024) REMOVED AND NSTALLED ALL FABRICATED PARTS REF REO 670-53-82-478 REV -A DATED 2014-11-12. SEE CONTINUE CARD FOR DETAILSSDR IPXA2023121930291Boot · damagedDAMAGE ON RADOME BOOT **10 FLT HOUR ** R&R RADOME I/A/W AMM 53-12-01-902-008.SDR IPXA2023121530291Unknown · unknown*SDR FILED OPEN* DAMAGE ON RADOME BOOT **10 FLT HOUR ** DEFERRED RADOME BOOT DAMAGE PER SREO-12211-REQ002 ALTERNATE REPAIR.SDR UIEA2023121200993Unknown · unknownLH WING, LWR SIDE OF BODY SPLICE PLATES BETWEEN L5 AND L10 WITH FUEL LEAK(<P> LH WING, LWR SIDE OF BODY SPLICE PLATES BETWEEN L5 AND L10 WITH FUEL LEAK. THE FUEL LEAK WAS REPAIRED AND THE TEST WAS SATISFACTORY. AMM 28-11-00-308-013. REV 140 22AUG2023.</P>)SDR UIEA2023121200994Unknown · unknownRH WING, LWR SIDE OF BODY SPLICE PLATES BETWEEN REAR SPAR AND L10 WITH FUEL LEAK(<P>RH WING, LWR SIDE OF BODY SPLICE PLATES BETWEEN REAR SPAR AND L10 WITH FUEL LEAK. THE FUEL LEAK WAS REPAIRED AND THE TEST WAS SATISFACTORY. AMM 28-11-00-308-013 REV 140 22AUG20SDR UIEA2023121200995Unknown · unknownRH WING LOWER SURFACE WING-TO-BODY SPLICE WBL 97.95 FUEL LEAK(<P>RH WING LOWER SURFACE WING-TO-BODY SPLICE WBL 97.95 FUEL LEAK. THE FUEL LEAK WAS REPAIRED AND THE TEST WAS SATISFACTORY. AMM 28-11-00-308-013. REV 140 22AUG2023.</P>)SDR YENA2023121501583Unknown · unknownFLT#1605, MCO-SJO. (AIRCRAFT PERFORMED AN AIR TURN BACK TO MCO) ' FA REPORTED LOUD THUMPING SOUND COMING FROM OUTSIDE THE AIRCRAFT; REMOVED AND REPLACED FAIRING AS PER THALES AMM 44-33-24. OPS CHECK OK. 8THR732B.'SDR SWAA2024011230147Panel · delaminatedBODY FAIRING PANEL 193CR EDGE AREA DELAMINATED MKD DOT<[01] APPLIED PERMANEMT REPAIR ON DAMAGE AREA AS MARKED ON PANEL 193CR AS PER B737 SRM 51-70-04-2R-13 PARAG 4-D-G; MATERIAL USED PO#1608196; PO#2040614; EQUIPMENT USED: TEMPERATURE CONTROL ID 160354; VACCUMSDR SWAA2023121329610Fairing · delaminatedWING TO BODY PANEL 193AL HAS DELAMINATION ON TRAILING EDGE.<[01] ACCOMPLISHED PERMANENT REPAIR IAW SRM 51-70-05-2R-10.SDR SWAA2024011528272Panel · delaminatedPANEL 193B HAS COMPOSITE DELAMINATION TO PANEL FACE SHEET AT LOWER ANTI-COLLISION LIGHT ASSY.<[01] REMOVED DAMAGE PER SRM 53-40-70-2R-1 AND SRM 51-70-05-2R-7;[02] VERIFIED REMOVED DAMAGE PER SRM 53-40-70-2R-1 AND SRM 51-70-05-2R-7;[03] POTTED CORE PER SRM 51-7SDR UIEA2023120700976Radome · unknownNOSE RADOME HAS MULTIPLE SMALL PUNCTURE DAMAGES AND DELAMINATION DUE TO FOD.(<P>ACFT AOG FOR NEW RADOME. R/R RADOME IAW AMM 53-12-01. NO FURTHER DEFECTS NOTED</P>)SDR DALA2023120710040Unknown · unknownSHIP 3265 DISC: RT WING-TO-BODY FAIRING PANEL FOUND DAMAGED ON ARRIVAL. C/A: PERFORMED A WALK AROUND FOR FURTHER DAMAGE, NO ADDITIONAL DAMAGE FOUND. REMOVED RT WING TO BODY FAIRING PANEL(WIP 706495). REPLACED RT WING-TO-FUSELAGE FAIRING PANEL(192DT) PER A320 ASDR SWAA2024011528019Fairing · elongated#3 FLAP TRACK FAIRING; AFT TAIL CONE HAS MISSING/LOOSE FASTENERS WITH ELONGATED HOLES<[01] LOCATED AND DRILLED #3 FLAP TRACK FAIRING; AFT TAIL CONE PER SRM 51-40-02;[02] LOCATED AND DRILLED #3 FLAP TRACK FAIRING; AFT TAIL CONE PER SRM 51-40-02<BR>PANEL ISSUE OSDR SWIA2024022200003Radome · crackedBIRD STRIKE. NOSE IS CRACKED AND DENTED. BIRD REMAINS FOUND NEAR ENGINE AND IN THE CRACKS ON THE NOSE (FLIGHT 3754 FILED CLOSED)COMPLIED WITH BIRD STRIKE INSP PER CRJ 900 AMM 05-51-25. REF AML1257481, 1257461, 1258140, 1257126, 1257667, 1257939 AND 1257572 FOSDR SWAA2024011225695Bracket · crackedLEFT WING TO BODY FAIRING FWD SUPPORT BRACKET CRACKED @ FASTENER TAIL INB OF FIXED L/E FAIRING MKD DOT<[01] REMOVED AND REPLACED FWD SUPPORT BRACKET AT LEFT WING TO BODY FAIRING I/B OF FIXED L/E PER BOEING 737-800 SRM 51-40-02-0G-0;[02] VERIFIED ALL STEPSSDR SWAA2023121525200Radome · crackedNOSE RADOME RUBBER BOOT HAS MULTIPLE CRACKS<[01] REMOVED AND REPLACED RADOME PER MM 53-52-00. SEE CARD [TTG8Q00PX78K FOR TOOLING AND SIGH OFFS.SDR SWAA2023112924970Panel · delaminatedHOLE/DELAMINATION; R/H FWD O/B WING-TO-BODY FAIRING PANEL 193AR REF TTG8Q00NW80K<[01] REMOVED AND INSTALLED PANEL 193AR IAW AMM 53-51-21SDR DALA2023113009868Unknown · unknownSHIP 3328 ACRFT DUE TO TEMPORARY REPAIR OF DAMAGE ON PANEL 191AB BELLY FAIRING. CORRECTIVE ACTION: INSPECTION MUST BE ACCOMPLISHED EVERY 7 DAYS FOR SPEED TAPE CONDITION. SEE SEQ 4979938. SRM A330 51-77-13-911-009. ON 28NOV23, C/W REP CHK FOUND SPEED TAPE TO BESDR SWAA2023112424020Panel · delaminatedPANEL 193AL LEADING EDGE DELAMINATED<[01] REMOVED AND REPLACED 193AL PANEL PER AMM 53-51-21-401.SDR SWAA2023122123723Fairing · delaminatedREF. CARD: 23-153-02955-TLD. PERFORM PERMANENT REPAIR AT WTB FAIRING 193AL; L/E AREA WITH EROSION & DELAMINATION DAMAGE.<[01] REPAIRED DAMAGE AREA AT FAIRING PANEL #193AL AS PER SRM 51-70-04-2R-13 .MATERIAL USED BMS9-3-7781 PO#1738579;[02] VERIFIED STEP # 1SDR JJBA20231127020Radome · delaminatedELECTRICAL SMELL AND VISIBLE ARCING AT RADOME WHILE RADAR ON AND IN CLOUDS. PERFORMED DVI OF RADAR. OPS CHECKED. STBY SWITCH IN NORMAL POSITION, OPS CHECKED GOOD - NO FAULTS FOUND. PERFORMED DVI OF RADOME. FOUND DELAMINATION ON RADOME AND BOTH BONDING JUMPERS SDR DALA2023112209647Unknown · unknownSHIP 3359 DURING C CHECK IN MSP, THE P/N F53470127203 AND F53485241216 FUSELAGE SKINS WERE FOUND WITH CHAFING DAMAGE AT SEVERAL LOCATIONS DUE TO CONTACT WITH WASHERS ON THE 198GB WTBF PANEL. MTC HAS REWORKED THE MAJORITY OF THE DAMAGE LOCATIONS PER SRM 51-73-0SDR SWAA2023121429108Panel · deterioratedPNL 193AR HAS 2 AREAS OF DETERIORATED COMPOSITE.<[01] ACCOMPLISHED REPAIR OF PNL 193R REF SRM 53-40-70-2R-1. SEE WORK STEPS FOR WORK PERFORMED.;[02] CERTIFIED WORK STEPS ACCOMPLISHED TO REPAIR PANEL #193R.SDR SWAA2023112023223Panel · delaminatedWING-TO-BODY FAIRING PANEL 193B DELAMINATED.<[01] LOCATED AND DRILLED FASTENERS HOLES ON NEW 193B PANEL IAW SRM 51-40-06;[02] R/R PANEL 193B PER AMM 53-51-21SDR SWAA2023112021657Tail Cone · delaminatedTAIL-CONE RH SIDE HAS A DENT MEASURING 10 LONG 2 WIDE AND .106 DEEP. DENT HAS AREAS THAT ARE DELAMINATED.<[01] APPLIED SPEED TAPE TO TAIL CONE RH SIDE AND COMPLIED WITH EA - 23-153-03378.SDR SWAA2023111721856Tail Cone · delaminatedTAIL CONE RH SIDE HAS A DENT 12 FWD OF ELEVATOR INDEX PLATE MEASURING 3 LONG 3 WIDE AND .087 DEEP. DENT IS DELAMINATED. DAMAGE IS WITHIN 4 OF PREVIOUS DENT.<[01] C/W EA: 23-153-03381;[02] EDIT STEP 3 TO INDICATE 'YES'SDR DALA2023111609447Unknown · unknownSHIP 3119 GOUGE ACCESS PANEL 194AB BELLY FAIRING AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER ER/A 612784-14. (0066503)SDR DALA2023111609445Unknown · unknownSHIP 3119 GOUGE ACCESS PANEL 193AB BELLY FAIRING AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER ER/A 612784-14. (0066494)SDR SWAA2023111420714Panel · crackedWING TO BODY FAIRING PANEL 193CL FASTENER HOLE CRACK AND PLY DAMAGE<[01] REMOVED AND REPLACED AFT WING TO BODY FAIRING PANEL 193 CL REF. AMM 53-51-21SDR IPXA2023111343755Unknown · unknownR/H WTB, T-CHORD STA 1220, FOUND EXFOLIATED CORROSION. REMOVED T-CHORD STA 1220 IAW SRM 51-40-02-0G. VERIFIED T-CHORD AT STA. 1220 REMOVED.SDR IPXA2023111343694Unknown · unknown*** SDR FILED OPEN *** FAULT: R/H WTB, T-CHORD, RBL 63, FOUND EXFOLIATED CORROSION. REMOVED T-CHORD AT RBL 63.0 BETWEEN FS 1180 TO FS 1240 IAW B757 SRM 51-40-02-0G. REMOVED STRAP FROM T-CHORD AT RBL 63.0 BETWEEN FS 1180 TO FS 1240 IAW B757 SRM 51-40-02-0G APPR
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