JASC 5350
Service difficulty reports · 6,118
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 IPXA2026042579144Access Panel · corrodedFWD, LT LOWER WTB PANEL LANDING INSIDE ACCESS PANEL 193AL HAS SURFACE CORROSION.SDR IPXA2026042579384Structure · corrodedLEFT AFT WTB FAIRING STRUCTURE LOWER CHORD AT APRROX. BS 1200 - 1220, HAS EXFOLIATION CORROSION.SDR DALA2026041502381Radome · damagedBIRD STRIKE AFTER T/O AT 10 AGL. POST FLT FOUND BIRD GUTS AND BLOOD ON LEFT UNDERSIDE OF NOSE CONE AND RT LEADING EDGE SLAT BETWEEN FUSELAGE AND NR 2 ENG. INSPECTED ACFT AND FOUND DAMAGE TO RAYDOME REQUIRING REPLACEMENT. RADOME REPLACED ON LOG 8378175. CLEANESDR IPXA2026041337727Intercostal · corrodedRIGHT WING TO BODY INTERCOSTAL AT BS 1040 TO 1060, RBL 46 IS EXFOLIATED AROUND NUTPLATE LOCATIONS. INSTALLED NEW TEE FITTING AND REINSTALLED 1EA ANGLE AND REINSTALLED 1EA BONDING JUMPER IAW SRM 51-40-02-0G-0.SDR IPXA2026050237740Tee Angle · corrodedRIGHT WING TO BODY TEE ANGLE AT BS 1060, RBL 8.8 - 43 WAS CORRODED UNDER NUTPLATES. INSTALLED A NEW TEE ANGLE IAW SRM 51-40-02. WORK COMPLETE.SDR IPXA2026042837717Tee Fitting · corrodedRIGHT WING TO BODY T-FITTING AT BS 1060 RBL 65 IS EXFLOIATED AROUND NUTPLATE LOCATIONS REVIEWED. REMOVED THE T FITTING IAW SRM 51-40-02. INSTALLED T FITTING AT RT WING TO BODY IAW 1060, RBL 65 I.A.W. B757-200 SRM 51-40-02.SDR IPXA2026042837737Tee Fitting · corrodedRIGHT WING TO BODY TEE FITTING AT BS 1045, RBL 46 TO RBL 67 HAS EXFOLIATION CORROSION ON UPPER SURFACE. INSTALLED NEW TEE FITTING IN RT WING AT BS 1045, RBL 46 TO RBL 67 IAW SRM 51-40-02-0G-0.SDR CALA2026041315292Radome · no discrepancyBIRD STRIKE FO SIDE NOSE ACCOMPLISHED INSPECTION PER AMM 05-51-14/601, FOUND BLOOD RIGHT SIDE AFT OF RADOME AND SOME ON # 2 ENG INLET. CLEANED AREA, NO DAMAGE FOUND. DEBRIEFED INBOUND CREW. THEY TOLD ME ENGINE PARAMETERS NORMAL, NO ODOR IN CABIN, AIRCRAFT FLEWSDR IPXA2026041323730Tee Angle · corrodedRH WING TO BODY T-CHORD AT BS 1040 HAS CORROSION AROUND NUTPLATE HOLES. BLENDED AREA AROUND THE NUTPLATES HOLES TO REMOVE THE CORROSION PER SRM 51-10-02-0G-0 AND AFTER PERFORMED EVALUATION T-CHORD AT STA 1040 WAS FOUND TO BE WHITIN ALLOWABLE LIMITS. PER SRM 5SDR MASA20260420084Rib · corrodedDURING HEAVY CHECK INSPECTIONS ON CFII, CORROSION FOUND ON WTBF STRUCTURE LOWER FLANGE AT RIB45 BETWEEN LBL30 AND RBL30. CORROSION AT RIB 45 REMOVED BY BLEND-OUT IAW SRM 51-10-03 AND FOUND TO BE WITHIN LIMITS IAW SRM 53-04-02 AD01 REV 46 DEC 03/21.SDR IPXA2026041423711Tee Fitting · corrodedLH WING TO BODY TEE - FITTING AT BS 1040 FWD EDGE HAS CORROSION. REMOVED TEE ANGLE ON BS 1037.67 LT WTB SIDE. IAW SRM 51-40-02. INSTALLED TEE ANGEL AT STA 1040 AT THE L/H WING TO BODY. IAW SRM 51-40-02-0G.SDR IPXA2026042104911Tee Angle · corrodedR/H WHEEL WELL FAIRING SUPPORT STRUCTURE TCHORD HAS CORROSION, BTWN STA 1040 AND STA 1060 AT RBL 62. LOCATED AND DRILLED NEW T-CHORD I.A.W. B757-200PF SRM 51-40-05.SDR DALA2026041502392Frame · corrodedER/A 633493-14; A220-100 / FWD AND CNTR WING TO BODY FAIRING / FRAME / FR40, LBL 15 - RBL 15 / FR36, LBL 20 - RBL 20 / CORROSION. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH 633493-14, SECTION II REPETITIVE INSPECTION WITHIN EVERY 1,000 FLIGHT HOURS FSDR IPXA2026041984059Angle · corrodedRIGHT WTB PANEL LANDING, 2ND FROM FWD, AT UPPER WING ROOT HAS SURFACE CORROSION. 83-021. ATA 53-030 INSTALLED (3EA) NUTPLATES ON FWD SUPPORT ANGLE AND (3EA) NUTPLATES ON AFT SUPPORT ANGLE AT RT WTB UPPER WING ROOT STA-925, WL-208.1. I.A.W. SRM 51-40-02-0G-0 PASDR IPXA2026042783844Support Channel · corrodedAFT WTB LOWER FAIRING PANEL LANDING CHORD AT APPROX. BS 1217 HAS EXFOLIATED CORROSION. 83-015. REMOVED 1EA EXFOLIATED CHORD (CHANNEL) AT AFT WTB LOWER FAIRING AREA BTW BS 1180 AND 1220 RBL 7 IAW SRM 51-40-02-0G-0. INSTALLED 1 E/A NEW PART CHANNEL SUPPORT AND RSDR IPXA2026043083949Support Angle · crackedSTR- RH AFT WTB LOWER FAIRING PNL LANDING SUPPORT BRACKET HAS EVIDENCE OF A CRACK. 83-018. REMOVED SUPPORT BRACKET AT RH AFT WTB LOWER FAIRING PNL IAW B757-200PF SRM 51-40-02-0G-0 REV 124- 20 SEP 2025. INSTALLED SUPPORT BRAKET AND ATTACHED BEAM AT STR - RH AFTSDR IPXA2026042884007Angle · corrodedRIGHT WTB FWD PANEL LANDING AT UPPER WING ROOT HAS SURFACE CORROSION. 83-020. REMOVED (1EA) FWD SUPPORT ANGLE AND (1EA) AFT SUPPORT ANGLE FROM RH WTB UPPER WING ROOT STA-900, WL-208.1 I.A.W. B757-200PF SRM 51-40-02-0G-0 PARAG.7. INSTALLED FWD AND AFT SUPPORT ASDR IPXA2026042383844Support Channel · corrodedAFT WTB LOWER FAIRING PANEL LANDING CHORD AT APPROX. STA. 1217 HAS EXFOLIATED CORROSION.SDR IPXA2026042383814Tee Angle · corrodedAFT WTB LOWER FAIRING PANEL LANDING CHORD AT STA. 1220 HAS EXFOLIATED CORROSION. REMOVED EXFOLIATED CHORD FROM AFT WTB LOWER FAIRING AREA AT STA 1220 BTW RBL 30 AND LBL 30 REF B757 SRM 51-40-02-0G-0. INSTALLED 1 E/A NEW PART CHORD TEE P/N 149N7701-36 B/N 00SDR IPXA2026041570441Fairing · dentedNUMBER 3 AFT FAIRING, RIGHT SIDE SKIN ONE DENT. REMOVE THE DENT MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200 F FOR 240 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG.SDR IPXA2026040487396Support Bracket · corrodedWING TO BODY FAIRING STR, RH FWD UPPER WING, BTW STA 1080-1100, 1EA PANEL SUPPORT BRACKET HAS CORROSION. REMOVED CORROSION FROM WING TO BODY FAIRING STR, RH FWD UPPER WING, BTW STA 1080-1100. EVALUATED, TOTAL THICKNESS: 0.080, MATERIAL LOSS:0.003IN (4%), MATESDR IPXA2026041587231Angle · corrodedWING TO BODY FAIRING RH, FWD UPPER WING, BTW STA 900-920, 2EA PANEL SUPPORTS CORRODED. DOT 23-077. INSTALLED 2 NEW BRACKETS I.A.W. B757-200PF SRM 51-40-02. REVIEWEDSDR VNAA202604010033Strap · corrodedRBL 45 FAIRING SUPPORT STRAP IS CORRODED AT FS 847. REMOVED AND REPLACED FS 847 RBL 45 FAIRING SUPPORT STRAP PN# SH670-39166-5 IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-45-00-001-001-A01 & 51-23-00-001-001-A01.SDR VNAA202604010036Angle · corrodedANGLE IS CORRODED ATTACHED TO LOWER FAIRING SUPPORT WEB AT F.S.939 BETWEEN RBL2 AND LBL28. REMOVED UNSERVICEABLE FS939 BL0 SUPPORT ANGLE (P/N: SH670-39189-1) AND LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE FS939 BL0 SUPPORT ANGLE (P/N: SH670-39189-1) IAWSDR IPXA2026040965063Intercostal · corrodedTHROUGH ACCESS PANEL 198BR FAIRING STRUCTURE AT STA 1040 TO 1060 RBL 65 WITH CORROSION. REMOVED FAIRING STRUCTURE AT STA 1040 TO 1060 RBL 65 OUT OF LIMITS IAW SRM 53-00-71-1A-1. INSTALLED NEW INTERCOSTAL AT BS 1040 - 1060, RBL 65, IAW SRM 51-40-02.SDR IPXA2026041150506Tee Fitting · corrodedCORROSION FOUND AT STA 1180 TO STA 1240 L/H TEE CHORD. WTB SUPPORT AFT FUSELAGE. INSTALLED NEW T-CHORD.IAW B757-200PF, SRM 51-40-02. REVIEWEDSDR SWAA2026042784398Panel · debondedPANEL 194CR HAS DISBONDS ON OUTER SURFACE. PANEL 194CR WAS REPAIRED IAW SRM 51-70-05-2R-2.SDR IPXA2026041621262Support · corrodedWING TO BODY WEB SUPPORT FROM BS 1180 - 1240, LBL 63 CORRODED. INSTALLED NEW WEB SUPPORT IAW SRM 51-40-02.SDR IPXA2026041311405Tee Fitting · corrodedT-CHORD STA 1060 L/H SIDE WITH CORRODED. REMOVED T-CHORD STA 1060 L/H IAW B757-200PF, SRM 51-40-02. OUT OF LIMITS IAW B757-200PF, SRM 53-00-71-1A-1 DATAIL IX. INSTALLED TCHORD STA 1060 LBL 56 TO 75 IAW B757-200PF SRM 51-40-02-0G-0. INSTALLED NEW CENTER SECTIOSDR IPXA2026040911700Tee Fitting · corrodedWTB TEE CHORD SUPPORT AT STA 1220 R/H HAS CORROSION INSTALLED WTB TEE CHORD SUPPORT AT STA 1220 R/H IAS 757-200PF SRM 51-40-02.SDR DALA2026040102120Radome · damagedSHIP 3247 DISC: BIRDSTRIKE WHILE FLARING TO LAND IN SMF RWY 35R. APPEARED TO BE DOVE SIZED. WALK-AROUND SHOWED STRIKE ON RADOME CAPT'S SIDE DIVERTER STRIP. CONTRACT MX NOTIFIED. C/A: PERFORMED BIRD STRIKE INSP PER A320 AMM 05-51, NO OTHER DAMAGE NOTED. REMOVEDSDR YENA2026033100363Skin · damagedDURING HEAVY MAINTENANCE: AFT FUSELAGE/ TAILCONE/ SKIN PANEL BTWN FR84-85 AND STGR16R/20R/ EXISTING REPAIR DOUBLER AND DISPREPANT HOLES/ PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-0025-26 COVER & PART 1 /2/ AIRBUS RDAF 70574427/048/2026#A /3/ MX244. DESCRSDR SWAA2026050483697Access Panel · elongatedELONGATED HOLES ON ACCESS PANEL 193CR WING TO BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 193CR WING TO BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-10, REPAIR 10.SDR SWAA2026050483698Access Panel · elongatedELONGATED HOLE ACCESS PANEL 194CR BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 194CR BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-04-2R-9 REPAIR 9.SDR REXA2026042300317Bracket · corrodedCORROSION ON ANGLES SUPPORTS OF REFUEL/DEFUEL CONTROL PANEL AT FAIRING 192BB. ANGLES SUPPORTS OF REFUEL/DEFUEL CONTROL PANEL AT FAIRING 192BB WAS REPLACED PER CRJ/900 SRM 51-42-10-001-001-A01SDR REXA2026042300316Bracket · corrodedCORROSION ON ANGLES SUPPORTS OF REFUEL/DEFUEL CONTROL PANEL AT FAIRING 192BB. ANGLES SUPPORTS OF REFUEL/DEFUEL CONTROL PANEL AT FAIRING 192BB WAS REPLACED PER CRJ/900 SRM 51-42-10-001-001-A01SDR REXA2026042300300Fairing · corrodedCORROSION ON SETTLEMENT AREA OF FUSELAJE FAIRINGS 196DR, 195DL, 195BB AND 195AB. CORROSION ON SETTLEMENT AREA OF FUSELAGE FAIRINGS 196DR, 195DL, 195BB AND 195AB WERE REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01. SETTLEMENT AREA SUPPORT OF FAIRINGS 196DR, 195DLSDR SWAA2026050483295Access Panel · crackedCRACK ACCESS PANEL 193AL AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 193AL AT LOWER FUSELAGE IAW B737-800 SRM 51-70-04-2R-2 REPAIR 2.SDR SWAA2026050483152Access Panel · delaminatedDELAMINATED ACCESS PANEL 191D AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 191D AT LOWER FUSELAGE IAW B737-700 SRM 51-70-05-2R-2 REPAIR 2.SDR SWAA2026043083161Drain Mast · crackedCRACKED ACCESS PANEL 194FL BODY FAIRING, APU SHROUD AND HYDRAULIC DRAIN. REPLACED APU SHROUD AND HYDRAULIC DRAIN MAST FUSELAGE EXTERIOR ON ACCESS PANEL 194FL IAW AMM 28-25-07-020-801 AND AMM 28-25-07-420-801.SDR SWAA2026041683357Access Panel · damagedELONGATED HOLE ON ACCESS PANEL 193D BODY FAIRING. REPAIRED ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9.SDR HNAA2026043000363Angle · crackedLEFT WING TO BODY FAIRING, UPPER LATERAL ANGLE CRACKED AT FR49. REPAIRED ANGLE IAW SRM 53-23-12SDR AALA202606227189Seal · missingAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO DFW DUE TO THE FLIGHT CREW REPORTING THAT ON CLIMB OUT A LOUD CONTINUOUS POPPING SOUND HEARD IN CABIN RIGHT SIDE OF AIRCRAFT NEAR WHEEL WELL AREA. SOUND RESEMBLED POPCORN POPPING. CHSDR AALA202603257189Seal · missingAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO DFW DUE TO THE FLIGHT CREW REPORTING THAT ON CLIMB OUT A LOUD CONTINUOUS POPPING SOUND HEARD IN CABIN RIGHT SIDE OF AIRCRAFT NEAR WHEEL WELL AREA. SOUND RESEMBLED "POPCORN"POPPING. CSDR SWAA2026042882077Access Panel · delaminatedDELAMINATED ACCESS PANEL 193CL. REPAIRED ACCESS PANEL 193CL IAW SRM 51-70-05-2R-6, REPAIR 6.SDR KCSA202603201011Frame · crackedCRACK IN FRAME 3 ON LT AFT STRUT INBD SIDE FAIRING ACCESS PANEL 434CR CUTOUT UPPER FASTENER HOLE.SDR MASA20260318022Tail Cone · corrodedTAILCONE CORRODED ON OUTER SURFACE AT FRAME 100, STRINGER L9L. THE CORROSION REMOVED BY BLENDING OUT IAW 51-10-03, FOUND WITH IN LIMITS IAW SRM 53.31-01, ADO 1, FIG 106, TABLE 101. HFEC INSPECTION CARRIED OUT, NO CRACKS FOUND IAW SRM 51-23-04, SRM 51-23-05, SSDR IPXA2026032391466Fairing · debondedDISBOND, FUSELAGE RT SIDE AFT WING TO BODY PANEL 198CR EXTERNAL SURFACE. PERFORMED NDT/UT FOR REWORKED AREA PLUS 6'' AROUND HEATED AREA I.A.W 767 NTM PART1 51-01-01 REV:143. RESULT:NO DEFECT FOUND. IAW SRM 51-70-14-0G-0 REV.94, & AMM 51-21-10-377-003 REV.147 SDR SWAA2026042280031Access Panel · damagedELONGATED HOLE ACCESS PANEL 191FL BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 191FL BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-04-2R-9 REPAIR 9.SDR SWAA2026042280125Access Panel · crackedCRACK ACCESS PANEL 195CR BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 195CR BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-04-2R-10 REPAIR 10.
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