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.

SDR SWAA2026042280027Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 193AL BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 193AL BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-10 REPAIR 10.Mar 15, 2026 · N927WN · Boeing 7377H4SDR SWAA2026031679121Access Panel · delaminatedWING-TO-BODY FAIRING PANEL 192BL LEADING EDGE DELAMINATION. APPLIED REPAIR PLIES PER SRM 51-70-05. REQIURES PAINT FINISH. PANEL 192BL REMOVED IAW SRM 51-40-02. APPLIED PERMANENT REPAIR PER SRM 53-40-70-2R-1 AND SRM 51-70-05.Mar 12, 2026 · N8699A · Boeing 7378H4SDR SWAA2026041378849Support · crackedRH WING TO BODY FAIRING SUPPORT BS 500I IS CRACK (MARKED).<[01] REMOVED AND INSTALL NEW SUPPORT AT R/H WING TO BODY FAIRING BS 500I PER SRM 51-40-02; DWG 116A3110 REV- A AND IPC 57-40-00-52;[02] VERIFIED CORRECTIVE ACTIONMar 11, 2026 · N8631A · Boeing 7378H4SDR SWAA2026040978319Panel · delaminatedPANEL 192K HAS LARGE DELAMINATION ON OUTER SURFACE.<[01] REPLACED PANEL 192K IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-12-11-01 ITEM 200.;[02] PANEL 192K WITH LARGE DELAMINATION ON OUTER SURFACE WAS REPLACED WITH A SERVICEABLE PANEL PER SRM 51-10-02-0G-0 PARA 9Mar 10, 2026 · N8631A · Boeing 7378H4SDR SWAA2026041677951Tail Cone · debondedFUSELAGE SECTION 48 DISBONDING COMMON TO TAIL CONE LOWER AREA LOC. AT 5.5IN FROM FWD EDGE. REPAIRED TAIL CONE LOWER AREA IAW SRM 51-70-04-2R-2, REPAIR 2.Mar 9, 2026 · N7729A · Boeing 73776NSDR SWAA2026041677950Tail Cone · debondedFUSELAGE SECTION 48 DISBONDING COMMON TO TAIL CONE RT SIDE. DAMAGE 1 LOC. AT 7.5IN FROM FWD EDGE AND DAMAGE 2 LOC. AT 11.5IN FROM FWD EDGE. REPAIRED TAIL CONE RT SIDE 2EA IAW SRM 51-70-04-2R-2, REPAIR 2.Mar 9, 2026 · N7729A · Boeing 73776NSDR VNAA2026031014307Radome · damagedBIRDSTIKE ON RADOME. / DUE TO BIRD STRIKE ON NOSE RADOME, NOSE RADOME WAS DENTED AND PUNCTURED INWARD BUT DIDN€™T HAVE ANY DAMAGE OR CONTACT WITH THE SURROUNDING STRUCTURE. PERFORMED REMOVAL AND INSTALLATION OF NOSE RADOME IAW AMM 53-81-80-000/400/801-A01.Mar 9, 2026 · N517AE · Cndair CL6002C10SDR SWAA2026042077392Access Panel · delaminatedDELAMINATED FWD EDGE ACCESS PANEL 193CR BODY FAIRING AT LOWER FUSELAGE. REPAIRED FWD EDGE ACCESS PANEL 193CR BODY FAIRING AT LOWER FUSELAGE IAW SRM 51-70-05-2R-6 REPAIR 6.Mar 7, 2026 · N8638A · Boeing 7378H4SDR REXA2026080601510Support Fitting · damagedELONGATED HOLE ON FWD LEFT SUPPORT FITTING AT FAIRING 193AB FWD LEFT SUPPORT FITTING AT FAIRING 193AB WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01.Feb 26, 2026 · N297PQ · Cndair CL6002D24SDR SWIA2026022475927Doubler · chafedDOUBLER UNDER TRAILING EDGE OF FUSELAGE TO WING FAIRINGS 195DL & 196DR JUST AFT OF FS985 BETWEEN BL5L & BL4R IS CHAFED. REPAIRED DOUBLER UNDER TRAILING EDGE OF FUSELAGE TO WING FAIRINGS 195DL AND 196DR JUST AFT OF FS985 BETWEEN BL5L AND BL4R REF REO 670-53-00Feb 24, 2026 · N732SK · Cndair CL6002C10SDR REXA2026080601522Strap · corrodedCORROSION AT SUPPORT STRUCTURE STRAP BTW FAIRING ACCESS PANEL 193AL & 193AR TO FAIRING ACCESS PANEL 193AB STRAP P/N: CC670-39052-4S AND STRAP P/N: CC670-39052-3S ON FAIRING ACCESS PANEL 193AB WAS REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01 AND CRJ-900 SRM 51Feb 23, 2026 · N297PQ · Cndair CL6002D24SDR REXA2026080601521Strap · corrodedCORROSION AT SUPPORT STRUCTURE STRAP BTW FAIRING ACCESS PANEL 193AL & 193AR TO FAIRING ACCESS PANEL 193AB STRAP P/N: CC670-39052-4S AND STRAP P/N: CC670-39052-3S ON FAIRING ACCESS PANEL 193AB WAS REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01 AND CRJ-900 SRM 51Feb 23, 2026 · N297PQ · Cndair CL6002D24SDR SWAA2026022473176Panel · delaminatedPANEL 192 BL IS DELAMINATED ON FWD LEADING EDGE SKIN. COMPLIED WITH EA 26-153-00501.Feb 22, 2026 · N8699A · Boeing 7378H4SDR SWAA2026033172773Panel · damagedELONGATED HOLE ON ACCESS PANEL 192HR, WING TO BODY FAIRING. REPAIRED THE ACCESS PANEL 192HR IAW SRM 51-70-04-2R-10, REPAIR 10.Feb 20, 2026 · N8633A · Boeing 7378H4SDR HNAA2026030400196Angle · crackedRIGHT OVERWING FAIRING 4TH ANGLE CRACKED. R A R ANGLE IAW SRM 51-40-02Feb 16, 2026 · N644AE · Emb EMB145LRSDR HNAA2026030200164Angle · crackedRIGHT OVERWING FAIRING 5TH ANGLE CRACKED. CUTOUT PERFORMED, REPAIR DOUBLER AND FILLER INSTALLED IAW SRM 57-20-01 AND EO1-57-26-0079Feb 16, 2026 · N644AE · Emb EMB145LRSDR HNAA2026022000144Fairing · crackedLEFT OVERWING FAIRING CRACKED AT 2ND ANGLE. RAR ANGLE IAW SRM 51-40-02Feb 16, 2026 · N644AE · Emb EMB145LRSDR SWAA2026032370675Access Panel · damagedELONGATED HOLE ON ACCESS PANEL 194E OF BODY FAIRING. REPAIRED THE ACCESS PANEL 194E OF THE BODY FAIRING IAW SRM 51-70-05-2R-10 REPAIR 10.Feb 13, 2026 · N245WN · Boeing 7377H4SDR SWAA2026021370191Fairing · delaminatedRIGHT WING TO BODY PANEL 191FR, LEADING EDGE LOWER CORNER DELAMINATED. PERFORMED A REPAIR IAW SRM 53-30-70-2R, REPAIR 1.Feb 12, 2026 · N8667D · Boeing 7378H4SDR SWAA2026031369993Access Panel · crackedCRACKED ACCESS PANEL 193B ON THE BODY FAIRING. REPAIRED THE ACCESS PANEL 193B IAW SRM 51-70-04-2R-6, REPAIR 6.Feb 11, 2026 · N240WN · Boeing 7377H4SDR DXTA2026021306860Fairing · damagedHIT A HERD OF DEER JUST PRIOR TO V1, AIRCRAFT NEEDS INSPECTION FOR ANY DAMAGE. BELLY FAIRING FRAME 6 AND BELLY FAIRING C CHANNEL. DAMAGE TO THE LT MLG DOOR. THE DOOR ROD IS BENT. THE RIVETS ATTACHING THE FWD HINGE PLATE ASSEMBLY FOR THE LT GEAR DOOR TO THE AIFeb 10, 2026 · N901QS · Cessna 680ASDR REXA2026032700255Support · corrodedCORROSION ON SETTLEMENT AREA OF BODY FAIRING ACCESS PANELS 195AB, 195BB, 196AR AND 195AL AT AFT BODY FAIRING SUPPORT STRUCTURE. CORROSION ON SETTLEMENT AREA OF BODY FAIRING ACCESS PANELS 195AB, 195BB, AND 195AL WAS REMOVED AND EVALUATED WITHIN LIMITS CRJ900 SFeb 10, 2026 · N918XJ · Cndair CL6002D24SDR SWAA2026021369768Radome · delaminatedNOSE RADOME HAS A DELAMINATION AT 4 O`CLOCK, 4 INCHES FROM AFT EDGE, MEASURES 9 INCHES BY 14 INCHES. R & R NOSE RADOME IAW AMM 53-52-00.Feb 10, 2026 · N8608N · Boeing 7378H4SDR SWAA2026031369630Access Panel · delaminatedDELAMINATED ACCESS PANEL 191AL, BODY FAIRING. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.Feb 9, 2026 · N240WN · Boeing 7377H4SDR IPXA2026030320044Tee Angle · corrodedRIGHT FUSELAGE BS 1147 TEE ANGLE GOUGED AND CORRODED. INSTALLED A NEW TEE ANGLE, TWO STRAPS, & ONE ANGLE IAW SRM 51-40-02.Feb 9, 2026 · N427UP · Boeing 75724APFSDR IPXA2026030320240Tee Angle · corrodedLOWER FUSELAGE BS 1220, LT SIDE TEE ANGLE EXFOLIATED.Feb 9, 2026 · N427UP · Boeing 75724APFSDR IPXA2026022611384Support · crackedCRACKED BRACKET, RT AFT WING TO BODY FAIRING SUPPORT, BS 1480, RBL 100. REMOVED THE DAMAGE SUPPORT IAW SRM 51-40-02-0G, REV 105, & INSTALLED A NEW SUPPORT IAW SRM 51-40-02-0G, REV 106, & DWG 65B15085, SHT 17, REV H.Feb 9, 2026 · N581UP · Boeing 7474R7FSDR IPXA2026022611393Support · crackedCRACKED BRACKET, LT AFT WING TO BODY FAIRING SUPPORT, BS 1480, LBL 100. REMOVED THE DAMAGED BRACKET IAW SRM 51-40-02-0G, REV 105, & INSTALLED A NEW SUPPORT IAW SRM 51-40-02-0G, REV 106, & G DWG 65B15085, SHT 17, REV H.Feb 9, 2026 · N581UP · Boeing 7474R7FSDR IPXA2026030360879Intercostal · corrodedRIGHT WING TO BODY INTERCOSTAL, BS 1040 - 1060, RBL 60 CORRODED. INSTALLED A NEW INTERCOSTAL IAW SRM 51-40-02-0G.Feb 5, 2026 · N427UP · Boeing 75724APFSDR IPXA2026030359670Tee Angle · corrodedRIGHT WING TO BODY TEE ANGLE AT BS 1040 - 1059, RBL 40, INLET STRUCTURE CORRODED.Feb 5, 2026 · N427UP · Boeing 75724APFSDR IPXA2026022760898Intercostal · corrodedRIGHT WING TO BODY INTERCOSTAL, BS 1040.2, RBL 40 - 60 CORRODED. INSTALLED A NEW INTERCOSTAL IAW SRM 51-40-02-OG.Feb 5, 2026 · N427UP · Boeing 75724APFSDR IPXA2026022860882Intercostal · corrodedRIGHT WING TO BODY INTERCOSTAL AT BS 1040 - 1060, RBL 65 CORRODED. APPLICATION OF CIC ON INTERCOSTAL.Feb 5, 2026 · N427UP · Boeing 75724APFSDR IPXA2026030360752Tee Angle · corrodedLEFT WING TO BODY, BS 1030 BEHIND PANEL 197AL TEE ANGLE CORRODED AT LBL 26. INSTALLED A NEW TEE ANGLE IAW SRM 51-40-02.Feb 5, 2026 · N427UP · Boeing 75724APFSDR SWAA2026022667832Panel · debondedPANEL 191FR, OUTER SKIN HAS MULTIPLE AREAS WITH DEEP SANDING DAMAGE WITH DEBONDS. THE PANEL 191FR OUTER SKIN WAS REPAIRED IAW SRM 51-70-05-2R-2, & SRM 53-30-70-2R-1.Feb 5, 2026 · N247WN · Boeing 7377H4SDR IPXA2026021961043Shim · corrodedFAULT/STR/ZONE 100 EXTERIOR RIGHT SIDE. WINGB / BODY PANEL 198KR STRUCTURE HAS CORROSION. REMOVED 01 EA SHIM LOCATED BTW STA 1180 TO STA 1240 AND RBL57. IAW B757-200 SRM 51-40-02 INSTALLED SPACER SHIM IAW SRM B757-200 TASK: 51-40-02Feb 5, 2026 · N427UP · Boeing 75724APFSDR IPXA2026030841896Tee Angle · corrodedRIGHT WING TO BODY TEE ANGLE AT BS 1060, RBL 10 - 40 HAS CORROSION AT NUTPLATE HOLES. INSTALLED TEE-ANGLE AND PLATES AT RT WING TO BODY IAW SRM 51-40-02.Feb 4, 2026 · N427UP · Boeing 75724APFSDR IPXA2026030443086Tee Fitting · gougedFAULT - STR - Z100 - LH UPPER WING TO BODY T-CHORD AT STA 1147 HAS GOUGE ON EDGE DOT 5698-08 INSTALLED T-CHORD AT LH WING STA 1147 I.A.W. B757 SRM 51-40-02.Feb 4, 2026 · N427UP · Boeing 75724APFSDR IPXA2026030342999Tee Angle · corrodedLEFT WING TO BODY TEE ANGLE, BS 1260, BEHIND PANEL 197LL, CORRODED.Feb 4, 2026 · N427UP · Boeing 75724APFSDR IPXA2026030340724Tee Angle · corrodedLEFT WING UNDER UPPER WING TO BODY PANEL 195BL HAD CORROSION. INSTALLED A TEE ANGLE IAW SRM 51-40-02.Feb 4, 2026 · N427UP · Boeing 75724APFSDR IPXA2026030341147Doubler · corrodedRIGHT WING TO BODY TEE ANGLE, BS 1040 - 1059, RBL 40 - 60, INLET STRUCTURE HAD CORROSION. INSTALLED RAMP EXHAUST DOUBLER & PAX EXHAUST ASSY AT RT WING TO BODY TEE ANGLE IAW SRM 51-40-02-OG.Feb 4, 2026 · N427UP · Boeing 75724APFSDR SWAA2026022667464Panel · debondedPANEL 192AL OUTER SKIN HAS 4EA TIGHTLY GROUPED DEBONDED. PANEL 192AL WAW REPAIRED IAW SRM 51-70-05-2R-2, & SRM 53-40-70-2R-1.Feb 4, 2026 · N247WN · Boeing 7377H4SDR IXXA2026020403Bracket · corrodedLOWER FUSELAGE WING TO BODY PANEL SUPPORT BRACKET HAS CORROSION AT WIRING CLAMP HOOKUP BETWEEN LEFT WHEEL WELL AND GEARFeb 4, 2026 · N752CX · Boeing 7572G5SDR SWAA2026031267264Access Panel · crackedCRACKED ACCESS PANEL 192F LOWER FUSELAGE. REPLACED ACCESS PANEL IAW AMM 34-32-11-400-802.Feb 3, 2026 · N8629A · Boeing 7378H4SDR CALA2026020213512Fairing · contaminatedA/C PACKS SMELL TERRIBLE DURING CLIMBOUT AND DESCENT, ODOR APPEARS FROM RESIDUAL DEICING FLUID FROM FOWARD WING TO BODY FAIRING PANELS. CONFIRMED COLOR., CONSISTENCY, AND ODOR OF FLUID. NO OIL ODOR FROM ENGINE BLEED DUCTS OR APU DUCT, (PACKS RUNNING). NO OIFeb 2, 2026 · N788UA · Boeing 777222SDR SWAA2026022666682Tail Cone · delaminatedDELAMINATION LOCATED ON AFT TAIL CONE RT SIDE APROX 25 FROM APU EXHAUST AND 19 FROM BOTTOM OF RUDDER. REMOVED DAMAGE TO AREA IAW SRM 51-70-05-2R-0. C/W INSPECTION OF DAMAGE REMOVAL TO AREA PER 51-70-05-2R-0. PERFORMED TAP TEST IAW 51-10-06. NO DELAMINATION Feb 1, 2026 · N8532S · Boeing 7378H4SDR IPXA2026020600994Angle · corrodedFAULT- CRACK- BRACKET, FWD LOWER WING TO BODY INTERNAL ATTACH BRACKET OF THE CORROSION AT STA 986 LBL 4. (REPLACE) 1. REMOVE DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV.64. 2. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.64 AND BOEING DWG NO.65B0676 SH2 REV.G. 3Jan 28, 2026 · N578UP · Boeing 74745ESDR DALA2026020300802Frame · crackedDURING AIRFRAME VIBRATION INVESTIGATION FOUND WTBF FRAME ASSEMBLY INBD END THAT ATTACHED TO LONGERON DEVELOPED A 1.25" L-CRACK REF A220 IPD 53-82-84-10AAB-941A-D. ITEM -75 P/M C02382115-001. REMOVED FRAME 48 OF WTBF SUPPORT STRUCTURE IAW AMP 220 53-82. INSTALLJan 28, 2026 · N309DU · Airbus BD5001A11SDR SWAA2026022464680Former · crackedLEFT WING TO BODY FAIRING FORMER CRACKED, BS 500D BETWEEN STRINGER 19L & 20L. EVALUATED CRACK ON THE WING TO BODY FAIRING, FOUND TO BE OUT LIMITS AND WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02 PAR 9. REMOVED AND REPLACED THE WING TO BODY FAIRING FORMEJan 27, 2026 · N922WN · Boeing 7377H4SDR SWAA2026020364600Access Panel · delaminatedDELAMINATED INTERNAL AREA ON ACCESS PANEL 193CR BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED THE ACCESS PANEL IAW SRM 51-70-05-2R-1, REPAIR 1.Jan 25, 2026 · N7734H · Boeing 7377BDSDR HNAA2026030400185Access Panel · crackedTAIL CONE / OIL SERVICE ACCESS PANEL / CRACKED ACCESS PANEL AREA / AT HINGE. COMPLIED WITH PERMENANT REPAIR OF THE APU COWLING OIL SERVICE DOOR CUTOUT MOLDING PER PIEDMONT AIRLINES ESR P/111585 REV: 12JULY22, AND EMB 145 SRM 53-32-23-RE ITEM 3 FIGURE 202, ANDJan 22, 2026 · N642AE · Emb EMB145LR
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